Maintenance Schedule for
B737-700
Hamburg International Revision No. 19 dated Jul 23/08 List of Effective Pages
please enter the number and date of this revision into „Record of Revision List“. Chapter / Section
Pages
Issue date
List of Eff. Pages Approval Sheet Record of Revision Record of Eff. Temp. Rev.
Page 1 of 1 Page 1 of 1 Page 1 - 2 Page 1 of 1
Jul 23/08 Jul 23/08 Jul 23/08 Jul 23/08
Table of Contents
Page 1 - 3
Jul 23/08
Introduction Highlights Item Revision Highlights
Page 1 - 2 Page 1 - 23
Jul 23/08 Jul 23/08
ATA Break-Down
Page 1 - 5
Jul 23/08
List of Effective Items
Page 1 - 7
Jul 23/08
Introduction
Page 1 - 28
Jul 23/08
Nat. and Internat. Special Requirements
Page 1 of 1
Jul 23/08
Aircraft Zones
Page 1 - 11
Jul 23/08
Items
see List of Eff. Items
Jul 23/08
Explanation Component Maintenance Section Page 1 - 6 Items Component Maintenance Section
see List of Eff. Items
Jul 23/08
Jul 23/08
Please note that Revision 19 dated Jul 23/08 of Maintenance Schedule for 737-6/-7/-8 A/C of Hamburg International is a complete issue.
Lufthansa Technik Form 30835-95 (HAM TB 3) Printed in the Federal Republic of Germany
Customer Engineering FRA WE Page 1 of 1
Maintenance Schedule for
B737-700
Hamburg International Revision No. 19 dated Jul 23/08 Record of Revision List Revision No.
Revision Date
Approval Date
Mar 24/99
Apr 26/99
1
Aug 02/99
Sep 02/99
2
Oct 27/99
Nov 22/99
3
Apr 13/00
Apr 26/00
4
Jan 11/01
Mar 09/01
5
Jun 12/01
Jul 31/01
6
Dec 11/01
Jan 11/02
7
Jun 26/02
Aug 28/02
8
Oct 17/02
Nov 28/02
9
Dec 18/02
Jan 14/03
10
Apr 29/03
May 22/03
11
Jun 13/03
Jun 24/03
12
Dec 02/03
Jan 16/04
13
Jun 03/04
Jul 15/04
14
Mar 18/05
Apr 26/05
15
Nov 30/05
Jan 16/06
16
Apr 25/06
May 10/06
17
Sep 05/06
Oct 10/06
18
Mar 22/07
Aug 06/07
19
Jul 23/08
First Issue
Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany
Revision No.
Revision Date
Approval Date
Customer Engineering FRA WE
Page 1 of 2
Maintenance Schedule for
B737-700
Hamburg International Revision No. 19 dated Jul 23/08 Record of Revision List Revision No. First Issue
Revision Date
Date incorp. / Sign
Revision No.
Revision Date
Date incorp. / Sign
Mar 24/99
1
Aug 02/99
2
Oct 27/99
3
Apr 13/00
4
Jan11/01
5
Jun 12/01
6
Dec 11/01
7
Jun 26/02
8
Oct 17/02
9
Dec 18/02
10
Apr 29/03
11
Jun 13/03
12
Dec 02/03
13
Jun 03/04
14
Mar 18/04
15
Nov 30/05
16
Apr 25/06
17
Sep 05/06
18
Mar 22/07
19
Jul 23/08
Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany
Customer Engineering FRA WE
Page 2 of 2
Maintenance Schedule for
B737-700
Hamburg International Revision No. 19 dated Jul 23/08 Record of Eff. Temporary Revision List Temp. Rev. No.
Date
Approval Date
Lufthansa Technik Form 30839-95 (HAM TB 3) Printed in the Federal Republic of Germany
Temp. Rev. No.
Date
Approval Date
Customer Engineering FRA WE
Page 1 of 1
MAINTENANCE SCHEDULE
HHI
737-6
TABLE OF CONTENTS HIGHLIGHTS ATA BREAK DOWN LIST OF EFFECTIVE ITEMS INTRODUCTION 1
GENERAL .................................................................................................................................................................................................................1 1.1 Validity .................................................................................................................................................................................................................1 1.2 Responsibilities.....................................................................................................................................................................................................2 1.3 Average Utilization...............................................................................................................................................................................................2 1.4 Operator’s Statement ............................................................................................................................................................................................3 1.5 Authority Approval...............................................................................................................................................................................................4 1.6 Explanation of Regulation ....................................................................................................................................................................................4 1.6.1 Flight Program ..............................................................................................................................................................................................4 1.6.2 Normal Standard Flight Time ........................................................................................................................................................................5 1.6.3 Maintenance Station ......................................................................................................................................................................................5 1.7 Revision Procedure...............................................................................................................................................................................................5 1.8 Reliability Monitoring Program ...........................................................................................................................................................................6 1.8.1 Aircraft Reliability Monitoring ......................................................................................................................................................................6 1.8.2 Engine Condition Monitoring ........................................................................................................................................................................7 1.8.3 Component Reliability Monitoring ................................................................................................................................................................7 1.9 Reference Documents...........................................................................................................................................................................................7
2
MAINTENANCE PROGRAM ................................................................................................................................................................................8 2.1 2.2
Line Maintenance .................................................................................................................................................................................................8 Base Maintenance.................................................................................................................................................................................................9
Date: 23-jul-2008
TABLE OF CONTENTS
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HHI
737-6
2.3 Time Controlled Maintenance ..............................................................................................................................................................................9 2.4 Zonal Inspection Program.....................................................................................................................................................................................9 2.4.1 Enhanced Zonal Analysis Procedure (EZAP)..............................................................................................................................................10 2.5 Structure Program...............................................................................................................................................................................................10 2.6 (Not used) ...........................................................................................................................................................................................................10 2.7 Corrosion Prevention and Control Program (CPCP)..........................................................................................................................................10 2.8 Identification of Type Certification and MRB Requirements ............................................................................................................................11 2.8.1 MSI, SSI, AWL and CMR .............................................................................................................................................................................11 2.9 Component Maintenance Program .....................................................................................................................................................................12 2.10 Inspection Techniques.....................................................................................................................................................................................12 2.11 Task Codes ......................................................................................................................................................................................................15 2.12 (Not used) ........................................................................................................................................................................................................17 2.13 Parking, Storage and Return to Service ..........................................................................................................................................................17 2.13.1 Parking .....................................................................................................................................................................................................17 2.13.2 Storage......................................................................................................................................................................................................17 2.13.3 Return to Service ......................................................................................................................................................................................18 2.13.4 Special Regulations for Parked or Stored Aircraft ..................................................................................................................................18 2.14 Authority Requirements ..................................................................................................................................................................................18 2.14.1 Approval of Maintenance Schedule by Authority .....................................................................................................................................18 2.14.2 Interval Escalation Procedure..................................................................................................................................................................19 2.14.3 Permitted Variations to Task Frequencies ...............................................................................................................................................19 2.15 (Not used) ........................................................................................................................................................................................................20 2.16 (Not used) ........................................................................................................................................................................................................20 2.17 (Not used) ........................................................................................................................................................................................................20 2.18 Maintenance Requirements for Specific Aircraft Operations .........................................................................................................................20 2.18.1 MNPS Maintenance Procedures ..............................................................................................................................................................20 2.18.2 RVSM (Reduced Vertical Separation Minimum) Capability ....................................................................................................................20 2.18.3 CAT II / CAT III Operation ......................................................................................................................................................................20 3
FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS..........................................................................................................21 3.1 3.2
Revision Column ................................................................................................................................................................................................21 ITEM Column.....................................................................................................................................................................................................21
Date: 23-Jul-2008
TABLE OF CONTENTS
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HHI 3.3 3.4 3.5 3.6 3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14 4
DESCRIPTION Column ....................................................................................................................................................................................22 ZONE Column....................................................................................................................................................................................................23 ACCESS Column ...............................................................................................................................................................................................23 STRUCTURE Column .......................................................................................................................................................................................23 REFERENCES Column .....................................................................................................................................................................................24 THRESHOLD/INTERVAL Column..................................................................................................................................................................25 TASK Column ....................................................................................................................................................................................................25 EFFECTIVITY Column..................................................................................................................................................................................25 BY Column......................................................................................................................................................................................................25 REP Column....................................................................................................................................................................................................26 LEV Column ...................................................................................................................................................................................................26 ITEM REVISION DATE Column ..................................................................................................................................................................26
WEIGHING .............................................................................................................................................................................................................27 4.1 4.2 4.3
5
737-6
Weighing Periods................................................................................................................................................................................................27 Weighing Procedure ...........................................................................................................................................................................................27 Weighing Results................................................................................................................................................................................................27
AIRCRAFT ..............................................................................................................................................................................................................28
NATIONAL AND INTERNATIONAL SPECIAL REQUIREMENTS AIRCRAFT ZONES ITEMS EXPLANATION COMPONENT MAINTENANCE SECTION (Page 1-6) ITEMS COMPONENT MAINTENANCE SECTION
Date: 23-Jul-2008
TABLE OF CONTENTS
Page: 3 of 3
MAINTENANCE SCHEDULE
HHI
737-6
Introduction Highlights General: Note “Which ever comes first” has been deleted from Items as it is explained within Chapter 2.1.
Chapter 1.3
Average Utilization
Relation between utilization and Flight Length Sensitive Thresholds from MPD Section 9 added (Already introduced with TR 001/07)
Chapter 1.7Revision Procedure Revision Procedure revised (Already introduced with TR001/07)
Chapter 1.9Reference Documents Documents revised and added
Chapter 2.4.1 Enhanced Zonal Analysis Procedure (EZAP) Chapter added based on MPD/MRB
Chapter 2.10
Inspection Techniques
Fuel Airworthiness Limitation CDCCL description added.
Chapter 2.18
Maintenance Requirements for Specific Aircraft Operations
Chapter added
Chapter 2.18.1
MNPS Maintenance Procedures
Chapter added
Chapter 2.18.2
RVSM (Reduced Vertical Separation Minimum) Capability
Chapter added
Date: 23-Jul-2008
HIGHLIGHTS
Page 1 of 2
MAINTENANCE SCHEDULE
HHI
Chapter 2.18.3
737-6
CAT II / CAT III Operation
Chapter added
Chapter 3.7Reference column Examples revised
Chapter 5 Aircraft D-AKIA,AHID,AHIE and AHIF phased out.
Date: 23-Jul-2008
HIGHLIGHTS
Page 2 of 2
HHI
MAINTENANCE SCHEDULE
737-6
Item Revision Highlights ITEM
DATE
05111- 00000
23-jul-08
TYPING ERROR IN NOTE (I) CORRECTED.
05145- 00000
23-jul-08
REFERENCES REVISED.
05195- 00000
23-jul-08
ACCESS PANELS REVISED ACCORDING TO MRB REV SEP 2007.
23-jul-08
REFERENCES REVISED EDITORIALLY.
05210- 01000
23-jul-08
AMM REFERENCE ADDED.
05553- 01000
23-jul-08
REFERENCES REVISED.
05560- 00000
23-jul-08
REFERENCES REVISED.
05571- 02000
23-jul-08
REFERENCES REVISED.
05841- 01000
23-jul-08
INTERVAL REVISED FROM 4800 CYC/18 MTH TO 4800 CYC/24 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
05900- 20290
23-jul-08
MPD JUN.08 OEM TASK 20-290-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20300
23-jul-08
MPD JUN.08 OEM TASK 20-300-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20310
23-jul-08
MPD JUN.08 OEM TASK 20-310-00:
Date: 23-jul-08
REVISION
HIGHLIGHTS
Page 1 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20320
23-jul-08
MPD JUN.08 OEM TASK 20-320-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20330
23-jul-08
MPD JUN.08 OEM TASK 20-330-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20340
23-jul-08
MPD JUN.08 OEM TASK 20-340-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20350
23-jul-08
MPD JUN.08 OEM TASK 20-350-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20360
23-jul-08
MPD JUN.08 OEM TASK 20-360-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
Date: 23-jul-08
HIGHLIGHTS
Page 2 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
REVISION
05900- 20370
23-jul-08
MPD JUN.08 OEM TASK 20-370-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20380
23-jul-08
MPD JUN.08 OEM TASK 20-380-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20390
23-jul-08
MPD JUN.08 OEM TASK 20-390-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20400
23-jul-08
MPD JUN.08 OEM TASK 20-400-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20410
23-jul-08
MPD JUN.08 OEM TASK 20-410-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20420
23-jul-08
MPD JUN.08 OEM TASK 20-420-00:
Date: 23-jul-08
HIGHLIGHTS
737-6
Page 3 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20430
23-jul-08
MPD JUN.08 OEM TASK 20-430-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20440
23-jul-08
MPD JUN.08 OEM TASK 20-440-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20450
23-jul-08
MPD JUN.08 OEM TASK 20-450-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20460
23-jul-08
MPD JUN.08 OEM TASK 20-460-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20470
23-jul-08
MPD JUN.08 OEM TASK 20-470-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
Date: 23-jul-08
HIGHLIGHTS
Page 4 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
REVISION
05900- 20480
23-jul-08
MPD JUN.08 OEM TASK 20-480-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20490
23-jul-08
MPD JUN.08 OEM TASK 20-490-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20500
23-jul-08
MPD JUN.08 OEM TASK 20-500-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20510
23-jul-08
MPD JUN.08 OEM TASK 20-510-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20520
23-jul-08
MPD JUN.08 OEM TASK 20-520-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20530
23-jul-08
MPD JUN.08 OEM TASK 20-530-00:
Date: 23-jul-08
HIGHLIGHTS
737-6
Page 5 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20540
23-jul-08
MPD JUN.08 OEM TASK 20-540-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20550
23-jul-08
MPD JUN.08 OEM TASK 20-550-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20560
23-jul-08
MPD JUN.08 OEM TASK 20-560-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20570
23-jul-08
MPD JUN.08 OEM TASK 20-570-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20580
23-jul-08
MPD JUN.08 OEM TASK 20-580-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
Date: 23-jul-08
HIGHLIGHTS
Page 6 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
REVISION
05900- 20590
23-jul-08
MPD JUN.08 OEM TASK 20-590-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20600
23-jul-08
MPD JUN.08 OEM TASK 20-600-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20610
23-jul-08
MPD JUN.08 OEM TASK 20-610-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
05900- 20620
23-jul-08
MPD JUN.08 OEM TASK 20-620-00: ADDED TASK. TASK ADDED BASED ON ENHANCED ZONAL ANALYSIS PROCEDURE (EZAP) AS APPROVED BY THE NOVEMBER 2006 EZAP WORKING GROUP.
081000 01000
23-jul-08
REFERENCE REVISED.
233011 00000
23-jul-08
REVISED AMM REFERENCE.
250000 09001
23-jul-08
ITEM DELETED DUE TO NON-APPLICABILITY.
254008 00000
23-jul-08
EDITORIAL CORRECTION OF ITEM DESCRIPTION.
256401 71000
23-jul-08
AMTOSS REFERENCE 25-64-00-71 DELETED AND CORRECT AMM REFERENCES ADDED.
Date: 23-jul-08
HIGHLIGHTS
737-6
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MAINTENANCE SCHEDULE ITEM
DATE
REVISION
256601 40000
23-jul-08
ITEM DLELETED; COVERD BY CMS-ITEMS CM2566 000010 AND CM2566 00020.
270000 00000
23-jul-08
SB REFERENCE REVISED DUE TO RELEASE OF SB REVISION 1.
270000 12000
23-jul-08
MPD FEB.08 REVISED ACCESS PANEL TO ADD 334JB, 344JB AND DELETE 315A, 333BB, 333EB, 334AB, 334BB, 343BB, 343EB, 344AB, 344BB. ACCESS PANEL WAS REVISED TO REFLECT APPLICABLE ACCESS REQUIREMENT.
23-jul-08
REFERENCES REVISED.
270000 25000
23-jul-08
MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOTE WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
270000 32000
23-jul-08
MPD FEB.08 REVISED ACCESS PANEL TO ADD 211A, 211B. ACCESS PANEL WAS REVISED TO ADD ACCESS PANELS 211A AND 211B FOR THE INSPECTION OF CABLE WITHIN PILOTS CONTROL QUADRANT. REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED TO CORRECT THE WING CENTER SECTION STATION FROM "BS 520 TO 727" TO "BS 520 TO 667.75" AND TO INCLUDE "CABLE WITHIN PILOTS CONTROL QUADRANT" WHICH WAS PROVIDED IN THE TASK CARD 27-230-00-02. ADDED ACCESS NOTE. ACCESS NOTE WAS ADDED TO REFLECT THE APPROPRIATE ACCESS REQUIREMENT.
23-jul-08
REFERENCES REVISED.
23-jul-08
MPD JUN.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS FOR ACCOUNTABILITY ALL TASKS. THE ADDITION OF THE TASK WAS APPROVED BY 2006 ISC.
270000 35000
Date: 23-jul-08
HIGHLIGHTS
737-6
Page 8 of 23
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MAINTENANCE SCHEDULE ITEM
DATE
REVISION
272100 03000
23-jul-08
MPD OCT.07 REVISED ZONE TO ADD 117, 211, 212 AND DELETE 134. ZONE WAS REVISED TO ADD THE REQUIRED ZONE 117,211 AND 212 AREA WHERE THE TASK PROCEDURE IS PERFORMED. AFTER REVIEWING THE TASK PROCEDURE, ZONE 134 WERE DETERMINED AS BEING NOT REQUIRED FOR THE TASK. REVISED ACCESS PANEL TO ADD 117A. ACCESS PANEL 117A WAS ADDED AS THE AMM TASK PROCEDURE REQUIRES ACCESSING INTO EE COMPARTMENT.
23-jul-08
ZONE 133 DELETED ACCORDING TO MRB REV SEP 2007.
273101 75000
23-jul-08
SB 737-55A1082 DELETED FROM EFFECTIVITY NOTE AS THIS SB IS NOT RELATED TO THIS MS ITEM.
273134 21500
23-jul-08
MPD JUN.08 REVISED ACCESS PANEL TO ADD 334PT, 344PT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENT FOR THIS TASK.
23-jul-08
SB 737-55A1082 DELETED FROM EFFECTIVITY NOTE AS THIS SB IS NOT RELATED TO THIS MS ITEM.
274181 01000
23-jul-08
SB 737-27A1277 R1 ADDED AS A REFERENCE. THIS SB CONTAINS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER TRIM ACTUATOR.
274181 21000
23-jul-08
INTERVAL REVISED TO HAVE THE SAME INTERVAL LIKE THE LUBRICATION TASK MS 270000 00000 AS RECOMMENDED BY BOEING IN SB. SB REFERENCE REVISED DUE TO RELEASE OF SB REVISION 1.
275106 21000
23-jul-08
EDITORIAL REVISION OF REFERENCES.
23-jul-08
MPD OCT.07 OEM TASK 27-166-00: REVISED ZONE TO DELETE 112, 117, 118. ZONE WAS REVISED BY DELETING 112,117 AND 118 BECAUSE THE ACTUAL WORKING ZONE IS INSIDE THE FLIGHT
Date: 23-jul-08
HIGHLIGHTS
737-6
Page 9 of 23
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MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION DECK WHOSE ZONE IS DEFINED BY ZONES 211 AND 212. REVISED ACCESS PANEL TO ADD 211A, 211B. ACCESS PANEL WAS REVISED TO ADD 211A AND 211B WHICH ARE ACCESS TO THE INSIDE OF CONTROL STAND. DELETED ACCESS NOTE. "EXTENDED FLAPS" WAS DELETED FROM ACCESS NOTE BECAUSE EXTENSION OF FLAP IS NOT NECESSARY TO PERFORM THE DETAIL INSPECTION OF FLAP LEVER SENSOR WHICH IS LOCATED IN THE CONTROL STAND IN THE FLIGHT DECK.
276100 21000
23-jul-08
MPD JUN.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS FOR ACCOUNTABILITY OF ALL TASKS. THE ADDITION OF THE TASK WAS APPROVED BY 2006 ISC.
276200 21000
23-jul-08
REFERENCES EDITORIALLY REVISED.
280000 06000
23-jul-08
ACCESS PANELS UPDATED ACCORDING TO MPD. (ISSUED WITH TR001/07)
23-jul-08
FAILURE EFFECT CATEGORY "9" ADDED AND DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
280000 76000
23-jul-08
FAILURE EFFECT CATEGORY "9" ADDED AND DESCRIPTION REVISED, INTERVAL CHANGED FROM 5 YRS TO 6 YRS ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
281100 01000
23-jul-08
NEW CMR MAR 08 REVISION, ITEM UPDATED.
281331 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
281341 21000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
282111 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
Date: 23-jul-08
HIGHLIGHTS
Page 10 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
282151 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
282200 20000
23-jul-08
MPD OCT.07 REVISED AIRPLANE NOTE. AIRPLANE NOTE WAS REVISED BY ADDING THE WORD "TASK" TO CLARIFY THE INTENT OF THE TASK.
282200 21000
23-jul-08
MPD OCT.07 REVISED AIRPLANE NOTE. AIRPLANE NOTE WAS REVISED BY ADDING THE WORD "TASK" TO CLARIFY THE INTENT OF THE TASK.
282211 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
282211 72000
23-jul-08
NEW ITEM ACCORDING ALI 28-AWL-24.
282502 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
284100 01000
23-jul-08
DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
284100 28000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
284100 29000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
23-jul-08
TASK UPDATED ACCORDING TO 28-AWL-03.
291104 20000
23-jul-08
NEW TASK ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
292100 70000
23-jul-08
INTERVAL TRANSFERRED FROM NOTE (I) TO INTERVAL COLUMN.
320000 31000
23-jul-08
DESCRIPTION REVISED.
320000 63000
23-jul-08
MPD JUN.08
Date: 23-jul-08
737-6
REVISION
HIGHLIGHTS
Page 11 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
320000 64000
23-jul-08
MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
320000 65000
23-jul-08
MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
320000 66000
23-jul-08
MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
320000 67000
23-jul-08
MPD JUN.08 REVISED ACCESS NOTE. ACCESS NOT WAS REVISED FROM "FORWARD CARGO COMPARTMENT CEILING PANELS" TO "FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO
Date: 23-jul-08
HIGHLIGHTS
Page 12 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION B.S. 540". REVISION TO ADD "FLOOR PANELS BETWEEN B.S.396 TO B.S. 540" WAS APPROVED BY OCTOBER 2006 ISC.
320000 68000
23-jul-08
MPD FEB.08 REVISED TASK PROCEDURE. TASK PROCEDURE WAS REVISED TO ADD AMM TASKS 32-31-22-211-801, 20-20-31-200-801, 20-20-31-200-802 AND 20-20-31-200-805 TO INSPECT LANDING GEAR CONTROL LEVER CABLE.
322171 20000
23-jul-08
MPD FEB.08 ADDED TASK. TASK WAS ADDED AFTER REVIEWING THE MSG-3 ANALYSIS TO ADDRESS SERVICE RELATED ISSUE ON NOSE LANDING GEAR AXLE. TASK ADDITION WAS APPROVED BY THE ISC CHAIR AND FAA MRB CHAIR.
324500 70000
23-jul-08
MPD JUN.08 REVISED FROM INSPECTION - DETAILED TO VISUAL CHECK. TASK WAS REVISED FROM "E3" TO "E1" AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS TASK DESCRIPTION. THE ORIGINAL MSG-3 ANALYSIS IDENTIFIED THE TASK AS A VISUAL CHECK. REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED FROM DETAILED INSPECTION TO VISUALLY CHECK AFTER REVIEWING THE ORIGINAL MSG-3 ANALYSIS TASK DESCRIPTION. THE ORIGINAL MSG-3 ANALYSIS IDENTIFIED THE TASK AS A VISUAL CHECK.
345300 73000
23-jul-08
AMM REFERENCE CORRECTED.
346002 00001
23-jul-08
AMM REFERENCE CORRECTED.
491611 10000
23-jul-08
AMM REFERENCES UPDATED.
491611 11000
23-jul-08
AMM REFERENCE CORRECTED.
493011 40000
23-jul-08
INTERVAL IN NOTE (I) CORRECTED.
494151 20000
23-jul-08
ZONE ADDED.
496100 90000
23-jul-08
REFERENCE "SERVICE EXPERIENCE" ADDED.
Date: 23-jul-08
HIGHLIGHTS
Page 13 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
498111 20100
23-jul-08
AMM REFERENCE CORRECTED.
499111 00000
23-jul-08
AMM REFERENCE CORRECTED.
524800 02000
23-jul-08
ACCESS PANEL CORRECTED.
526000 00000
23-jul-08
NEW ITEM ADDED ON CUSTOMER REQUEST.
526000 01000
23-jul-08
NEW ITEM ADDED ON CUSTOMER REQUEST.
526050 21000
23-jul-08
NEW ITEM ADDED ON CUSTOMER REQUEST.
527000 05000
23-jul-08
MPD FEB.08 REVISED TASK DESCRIPTION. TASK DESCRIPTION WAS REVISED FROM "THE THREE POSITION ROTARY SWITCH IN THE P5 PANEL" TO "THE THREE POSITION ROTARY SWITCH IN THE P8 PANEL" TO INDICATE THE APPROPRIATE LOCATION OF THE THREE POSITION ROTARY SWITCH.
527000 07000
23-jul-08
AMM REFERENCE ADDED.
527001 00000
23-jul-08
DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.
527001 02000
23-jul-08
DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.
23-jul-08
MPD FEB.08 REVISED TASK PROCEDURE. REVISED TASK PROCEDURE BY ADDING AIRCRAFT MAINTENANCE MANUAL (AMM) PROCEDURE 51-05-01-210-803 (CORROSION PREVENTION CONTROL PROGRAM (CPCP) BASIC STEPS PROCEDURE), TO REFLECT CORRECT CPCP REQUIREMENTS FOR THIS TASK.
23-jul-08
DELETED INTERVAL 16000 CYC DUE TO NON-APPLICABILITY AND ADJUSTED DESCRIPTION NOTE.
23-jul-08
MPD FEB.08
527001 04000
Date: 23-jul-08
737-6
REVISION
HIGHLIGHTS
Page 14 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION REVISED TASK PROCEDURE. REVISED TASK PROCEDURE BY ADDING AIRCRAFT MAINTENANCE MANUAL (AMM) PROCEDURE 51-05-01-210-803 (CORROSION PREVENTION CONTROL PROGRAM (CPCP) BASIC STEPS PROCEDURE), TO REFLECT CORRECT CPCP REQUIREMENTS FOR THIS TASK.
530900 01000
23-jul-08
ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.
530900 05000
23-jul-08
DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
530900 08000
23-jul-08
ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.
530900 10000
23-jul-08
ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.
530900 11000
23-jul-08
ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.
530900 13000
23-jul-08
ACCESS NOTE REVISED ACCORDING TO MRB REV SEP 2007.
531500 01000
23-jul-08
AMM-REFERENCES ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
531500 02000
23-jul-08
AMM-REFERENCES ADDED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
531500 04000
23-jul-08
MPD OCT.07 AMM REFERENCE ADDED.
544000 00000
23-jul-08
INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
544000 06000
23-jul-08
ITEM SPLITTED TO LEFT SIDE AND RIGHT SIDE SEPERATELY. RIGHT SIDE IS COVERED BY NEW MS-ITEM 544000 06100 (MPD 54-020-02).
544000 06100
23-jul-08
SPLITTED MS ITEM 544000 06000 IN TWO SEPARATE ITEMS (LEFT STRUT AND RIGHT STRUT).
Date: 23-jul-08
HIGHLIGHTS
Page 15 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION THIS NEW ITEM COVERS THE RIGHT ENGINE STRUT. THE EXISTING ITEM COVERS THE LEFT STRUT. REASON: TASK TO BE PERFORMED AT ENGINE CHANGE, WHICH TYPICALLY OCCURS ONLY ON ONE SIDE AT THE SAME TIME.
552000 03000
23-jul-08
DELETED NOTE (E) DUE TO NON-APPLICABILITY.
553000 00000
23-jul-08
REFERENCES EDITORIALLY REVISED.
553000 02000
23-jul-08
REFERENCES EDITORIALLY REVISED.
561100 02000
23-jul-08
DESCRIPTION REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
561100 03000
23-jul-08
NEW ITEM ADDED DUE TO AD REQUIREMENT OF INSPECTIONS ACCORDING TO SB 737-56A1022.
571000 03000
23-jul-08
DESCRIPTION REVISED ACCORDING TO MPD.
571400 02000
23-jul-08
ACCESS PANELS REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
571400 04000
23-jul-08
ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)
23-jul-08
NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
23-jul-08
ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)
23-jul-08
NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
23-jul-08
ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-03. (ISSUED WITH TR001/07)
571400 05000
571400 05500
Date: 23-jul-08
HIGHLIGHTS
Page 16 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
REVISION
23-jul-08
NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
23-jul-08
ENTERED CALCULATED THRESHOLD/INTERVAL ACC. MPD SECTION 9 FLS AND DTR 57-20-09. (ISSUED WITH TR001/07)
23-jul-08
NOTE (E) DELETED AND NOTE (I) REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
572200 00000
23-jul-08
MPD OCT.07 OEM TASK 57-270-01: REVISED ACCESS PANEL TO ADD 572CB, 572CT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENTS FOR THIS TASK BY ADDING 572CB AND 572CT. OEM TASK 57-270-02: REVISED ACCESS PANEL TO ADD 651GB AND DELETE 653AT. ACCESS WAS REVISED TO REFLECT CORRECT ACCESS REQUIREMENTS FOR THIS TASK BY ADDING 651GB AND DELETING 653AT.
573100 00000
23-jul-08
ACCESS PANELS REVISED ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
23-jul-08
EDITORIAL CORRECTION OF ITEM DESCRIPTION AND REFERENCES.
573200 01000
23-jul-08
INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
573500 00000
23-jul-08
INTERVAL REVISED FROM 9000 CYC/30 MTH TO 9000 CYC/36 MTH AS AGREED AT THE OCT 2006 ISC MEETING ACCORDING TO MPD REV JUN 2007. (ISSUED WITH TR001/07)
711102 20000
23-jul-08
AMM REFERENCE ADDED.
717100 20000
23-jul-08
AMM REFERENCE ADDED.
571400 07000
Date: 23-jul-08
737-6
HIGHLIGHTS
Page 17 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
720000 20000
23-jul-08
AMM REFERENCE ADDED.
720000 20200
23-jul-08
AMM REFERENCE ADDED.
720000 20300
23-jul-08
AMM REFERENCE ADDED.
720000 20400
23-jul-08
AMM REFERENCES CORRECTED.
720011 01200
23-jul-08
AMM REFERENCE ADDED.
720021 00200
23-jul-08
AMM REFERENCE ADDED.
722000 21000
23-jul-08
AMM REFERENCE ADDED.
722304 20000
23-jul-08
AMM REFERENCE ADDED.
722304 21000
23-jul-08
AMM REFERENCE ADDED.
725000 20000
23-jul-08
AMM REFERENCE ADDED.
731102 00000
23-jul-08
AMM REFERENCES ADDED.
732100 74000
23-jul-08
AMM REFERENCE ADDED.
742101 20000
23-jul-08
AMM REFERENCE ADDED.
742102 20000
23-jul-08
AMM REFERENCE ADDED.
781100 21000
23-jul-08
AMM REFERENCE ADDED.
783100 70000
23-jul-08
AMM REFERENCE ADDED.
783100 71000
23-jul-08
AMM REFERENCE ADDED.
783106 20000
23-jul-08
AMM REFERENCE ADDED.
783107 90000
23-jul-08
AMM REFERENCE ADDED.
783112 20000
23-jul-08
AMM REFERENCE ADDED.
783112 21000
23-jul-08
AMM REFERENCE ADDED.
783123 20000
23-jul-08
AMM REFERENCE ADDED.
Date: 23-jul-08
737-6
REVISION
HIGHLIGHTS
Page 18 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
790000 20000
23-jul-08
AMM REFERENCE ADDED.
790000 20500
23-jul-08
AMM REFERENCE CORRECTED.
792103 00000
23-jul-08
AMM REFERENCES ADDED.
792106 00000
23-jul-08
AMM REFERENCES ADDED.
801101 20000
23-jul-08
AMM REFERENCE ADDED.
CM2132 00000
23-jul-08
MPD REFERENCES ADDED.
CM2324 00000
23-jul-08
DESCRIPTION AND TASK CODE REVISED AND NOTE ADDED TO COVER SHOP REQUIREMENTS.
CM2371 00010
23-jul-08
NOTE (M) ADDED.
CM2560 00020
23-jul-08
INTERVAL CORRECTED AND NOTE REVISED.
CM2560 00021
23-jul-08
INTERVAL CORRECTED AND NOTE REVISED.
CM2560 00030
23-jul-08
INTERVAL CORRECTED AND NOTE REVISED.
23-jul-08
MPD REFERENCE ADDED.
23-jul-08
PARTNUMBER FOR CHILD LIFE VEST CORRECTED.
CM2560 00031
23-jul-08
INTERVAL CORRECTED AND NOTE REVISED.
CM2566 00010
23-jul-08
REFERENCES ADDED.
CM2740 00020
23-jul-08
SB ADDED AS A REFERENCE. IN SB THERE IS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER TRIM ACTUATOR.
CM2900 00020
23-jul-08
MPD JUN.08 OEM TASK REFERENCE 29-290-00 ADDED.
CM2999 00030
23-jul-08
MPD REFERENCE ADDED.
CM3211 00010
23-jul-08
MPD JUN.08 OEM TASK 32-040-01:32-040-02
Date: 23-jul-08
737-6
REVISION
HIGHLIGHTS
Page 19 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00020
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00030
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00040
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00050
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02
Date: 23-jul-08
HIGHLIGHTS
Page 20 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00060
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00070
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00080
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00090
23-jul-08
MPD JUN.08 OEM TASK 32-040-01:
Date: 23-jul-08
HIGHLIGHTS
Page 21 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
737-6
REVISION REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3211 00100
23-jul-08
MPD JUN.08 OEM TASK 32-040-01: 32-040-02 REVISED INTERVAL. TASK INTERVAL WAS REVISED FROM 18000FC TO 21000FC. THE ESCALATION WAS CONCURRED BY BOEING ENGINEERING AFTER REVIEWING LANDING GEAR DIMENSIONAL DATA COLLECTED DURING LANDING GEAR OVERHAUL. THE INTERVAL ESCALATION WAS ALSO APPROVED BY MRB /CHAIRMAN AND ISC CHAIRPERSON.
CM3351 00010
23-jul-08
TASK CODE REVISED.
CM3453 00010
23-jul-08
NEW ITEM ADDED TO COVER NFL REQUIREMENT.
CM3531 00010
23-jul-08
DESCRIPTION TEXT CHANGED.
CM4900 01010
23-jul-08
MPD REFERENCE ADDED.
CM4900 01020
23-jul-08
MPD JUN.08 OEM TASK 49-062-00 REFERENCE ADDED.
CM4900 01030
23-jul-08
MPD JUN.08 OEM TASK 49-072-00 REFERENCE ADDED.
CM4900 01040
23-jul-08
MPD JUN.08 OEM TASK 49-082-00 REFERENCE ADDED.
CM7200 20010
23-jul-08
EDITORIAL CORRECTION OF INTERVAL.
CM7200 20060
23-jul-08
P/N ADDED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.
CM7200 20070
23-jul-08
P/N CORRECTED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.
Date: 23-jul-08
HIGHLIGHTS
Page 22 of 23
HHI
MAINTENANCE SCHEDULE ITEM
DATE
REVISION
CM7200 20080
23-jul-08
INTERVAL INFORMATION TRANSFERED FROM NOTE TO INTERVAL COLUMN. NOTE DELETED.
23-jul-08
P/N ADDED IN CORRESPONDENCE TO ESM 05-11-02 REVISION.
CM7200 20090
23-jul-08
P/N ADDED IN CORRESPONDENCE TO ESM 05-11-03 REVISION.
CM7200 20100
23-jul-08
P/N ADDED IN CORRESPONDENCE TO ESM 05-11-03 REVISION.
CM7200 20110
23-jul-08
INTERVAL CHANGED IN CORRESPONDANCE WITH ESM 05-11-03 REVISION TR 05-0091.
23-jul-08
INTERVAL INFORMATION TRANSFERED FROM NOTE TO INTERVAL COLUMN. NOTE DELETED.
23-jul-08
P/N ADDED IN ACCORDANCE WITH ESM 05-11-03.
CM7200 20120
23-jul-08
NOTE DELETED AND P/N CORRECTED. P/N 1498M45P07 COVERD WITH NEW MS ITEM.
CM7200 20210
23-jul-08
P/N ADDED IN ACCORDANCE WITH ESM 05-12-04.
CM7200 20230
23-jul-08
AAR REFERENCES UPDATED.
CM7200 20240
23-jul-08
NEW ITEM TO COVER P/N 1498M45P07.
Date: 23-jul-08
HIGHLIGHTS
737-6
Page 23 of 23
HHI
737-6
MAINTENANCE SCHEDULE ATA Break-Down
ATA
DEFINITION
ATA
DEFINITION
05 10
ZONE 100 FUSELAGE -LOWER HALF-
05 50
LEFT WING / RIGHT WING
05 11
BODY STA 130 TO STA 360
05 51
05 12
BODY STA 360 TO STA 540
05 13
BODY STA 540 TO STA 727
WING LEADING EDGE - FORWARD OF FRONT SPAR INBOARD OF NACELLE STRUT - INCLUDING NACELLE GAP COVER AREA
05 14
BODY STA 727 TO 1016
05 52
WING LEADING EDGE - FORWARD OF FRONT SPAR OUTBOARD OF NACELLE STRUT
05 19
WING TO BODY FAIRINGS
05 53
05 20
FUSELAGE - UPPER HALF -
WING INSPAR AREA (FUEL TANKS) - INBOARD OF WING RIB 22 - WS 643.50
05 21
FLIGHT COMPARTMENT BODY STA 178 TO STA 259.5
05 54
WING TRAILING EDGE FLAP TRACK FAIRINGS
05 22
PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360
05 55
WING TRAILING EDGE - AFT OF REAR SPAR - INBOARD OF OUTBOARD TRAILING EDGE FLAP
05 23
PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75
05 56
05 24
PASSENGER COMPARTMENT BODY STA 663.75 TO STA 1016
WING TRAILING EDGE - AFT OF REAR SPAR OUTBOARD OF INBOARD TRAILING EDGE FLAP INBOARD OF FIXED TRAILING EDGE
05 57
FIXED TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP - INBOARD OF WING TIP WBL 658.17
05 30
ZONE 300-EMPENNAGE AND SECTION 48
05 31
FUSELAGE STA 1016 TO 1217
05 70
LANDING GEAR
05 32
FIN AND RUDDER
05 71
NOSE LANDING GEAR & DOORS
05 33
HORIZONTAL STABILIZER & ELEVATOR LEFT
05 73
LEFT MAIN LANDING GEAR & L.G. DOORS
05 40
POWER PLANTS & NACELLE STRUTS
05 80
ZONE 800- PASSENGER AND CARGO DOORS
05 41
NO. 1 POWERPLANT+ L/H NACELLE STRUT
05 82
DOORS, LOWER HALF FUSELAGE, L/H
05 43
LEFT NACELLE STRUT -
05 83
DOORS, UPPER HALF FUSELAGE, L/H
05 84
DOORS, UPPER HALF FUSELAGE, R/H
Date: 23-jul-08
ATA Break-Down
Page 1 of 5
HHI
737-6
MAINTENANCE SCHEDULE
ATA
DEFINITION
ATA
DEFINITION
05 90
EZAP
25 40
LAVATORIES
08 10
WEIGHING
25 52
CARCO COMPARTMENT LINING
21 25
RECIRCULATION SYSTEM
25 61
21 27
EQUIPMENT COOLING SYSTEM
ESCAPE STRAPS AND LANYARDS AND ESCAPE SLIDES (DOOR MOUNTED)
21 31
CABIN PRESSURE CONTROL SYSTEM
25 62
OVER-WATER SURVIVAL EQUIPMENT (OPTIONAL)
21 32
CABIN PRESSURE RELIEF
25 64
DETACHABLE EMERGENCY EQUIPMENT
21 33
CABIN PRESSURE INDICATION AND WARNING SYSTEM
25 66
DOOR-MOUNTED ESCAPE SYSTEM
25 71
ACCESSORY COMPARTMENTS
21 51
AIR COOLING SYSTEM
26 00
FIRE EXTINGUISHING SYSTEM
21 61
ZONE TEMPERATURE CONTROL AND INDICATION
26 14
LAVATORY SMOKE DETECTION
23 24
EMERGENCY LOCATOR TRANSMITTER
26 15
APU FIRE DETECTION SYSTEM
23 30
PASSENGER ADDRESS (PA) AND ENTERTAINMENT SYSTEM
26 20
FIRE EXTINGUISHING SYSTEM
26 23
EXTINGUISHING SYSTEM - CARGO COMPARTMENT
23 60
STATIC DISCHARGER
26 24
23 71
VOICE RECORDING SYSTEM
LAVATORY WASTE COMPARTMENT FIRE EXTINGUISHING
24 00
GENERAL
26 25
PORTABLE FIRE EXTINGUISHER
24 11
AC GENERATOR DRIVE SYSTEM
27 00
GENERAL
24 31
DC GENERATION SYSTEM
27 11
AILERON AND FLAPERON CONTROL SYSTEM
24 34
STANDBY POWER SYSTEM
27 21
RUDDER CONTROL SYSTEM
25 00
EQUIPMENT / FURNISHINGS
27 31
ELEVATOR CONTROL SYSTEM
25 11
FLIGHT COMPARTMENT SEATS
27 32
STALL WARNING
25 22
PASSENGER COMPARTMENT SEATS
27 41
HORIZONTAL STABILIZER CONTROL SYSTEM
25 25
CABIN ATTENDANT SEATS
27 51
FLAP/SLAT SYSTEM
Date: 23-jul-08
ATA Break-Down
Page 2 of 5
HHI
737-6
MAINTENANCE SCHEDULE
ATA
DEFINITION
ATA
DEFINITION
27 61
SPOILER AND SPEEDBRAKE CONTROL SYSTEM
32 11
MAIN LANDING GEAR SHOCK STRUT
27 62
AUTO SPEEDBRAKE CONTROL
32 21
NOSE LANDING GEAR SHOCK STRUT
27 81
LEADING EDGE SLAT SYSTEM
32 31
LANDING GEAR CONTROL SYSTEM
27 83
LEADING EDGE AUTOSLAT SYSTEM
32 32
MAIN LANDING GEAR EXTENSION AND RETRACTION
28 00
FUEL
32 34
NOSE LANDING GEAR EXTENSION AND RETRACTION
28 11
FUEL TANKS
32 35
LANDING GEAR ALTERNATE EXTENSION SYSTEM
28 13
FUEL VENT SYSTEM
32 41
BRAKE CONTROL SYSTEM
28 21
PRESSURE FUELING SYSTEM
32 44
PARKING BRAKE SYSTEM
28 22
ENGINE FUEL FEED SYSTEM
32 45
WHEELS, BRAKES, AND TIRES
28 25
APU FUEL FEED SYSTEM
32 51
NOSE GEAR STEERING SYSTEM
28 41
FUEL QUANTITY INDICATING SYSTEM (FQIS)
32 61
LANDING GEAR POSITION INDICATING AND WARNING
29 00
HYDRAULIC POWER
33 51
EMERGENCY LIGHTS
29 11
MAIN HYDRAULIC POWER SYSTEM
34 11
STATIC AND TOTAL AIR PRESSURE SYSTEM
29 18
GROUND SERVICING SYSTEM
34 24
STANDBY MAGNETIC COMPASS
29 21
STANDBY HYDRAULIC SYSTEM
34 53
AIR TRAFFIC CONTROL SYSTEM
29 22
POWER TRANSFER SYSTEM
34 60
FLIGHT MANAGEMENT COMPUTING
29 32
HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM
35 00
GENERAL
35 12
FLIGHT CREW OXYGEN SYSTEM
31 31
FLIGHT DATA RECORDER SYSTEM
35 21
PASSENGER / LLAR OXYGEN SYSTEM-CHEMICAL
31 51
CENTRAL WARNING SYSTEMS
35 22
PASSENGER OXYGEN SYSTEM-GASEOUS
31 62
COMMON DISPLAY SYSTEM
35 31
PORTABLE OXYGEN EQUIPMENT
32 00
GENERAL
36 14
APU BLEED SYSTEM
Date: 23-jul-08
ATA Break-Down
Page 3 of 5
HHI
737-6
MAINTENANCE SCHEDULE
ATA
DEFINITION
ATA
DEFINITION
38 11
STORAGE AND DISTRIBUTION
52 49
ACCESS AND BLOWOUT DOOR
38 32
VACUUM WASTE SYSTEM
52 60
AIR STAIRS
38 33
WASTE TANK QUANTITY INDICATION
52 70
COCKPIT DOOR
38 42
WATER TANK PRESSURIZATION SYSTEM
52 71
DOOR WARNING SYSTEM
49 00
AUXILIARY POWER UNIT (APU) - GENERAL
53 09
BODY UPPER
49 11
APU - SYSTEM
53 13
TAIL SECTION
49 13
APU MOUNTS
53 15
NOSE AND MAIN LANDING GEAR WHEEL WELL
49 15
APU AIR INTAKE SYSTEM
53 30
FUSELAGE EXTERIOR
49 16
APU DRAINS
53 51
WING-TO-BODY FAIRING
49 17
APU INSULATION PANELS
53 81
49 30
APU FUEL SYSTEM
UNDERFLOOR NOSE COMPARTMENT AND ELECTRONIC EQUIPMENT COMPARTMENT
49 41
IGNITION / STARTING
53 82
FORWARD CARGO COMPARTMENT
49 61
APU CONTROLS
53 84
AIR CONDITIONING COMPARTMENT LH AND RH
49 81
EXHAUST
53 85
AFT CARGO COMPARTMENT
49 91
APU EDUCTOR SYSTEM
54 30
PYLON-SKIN
52 11
PASSENGER ENTRY DOOR
54 40
ATTACHMENT FITTINGS
52 12
FORWARD AND AFT SERVICE DOORS
55 10
STABILIZER- HORIZONTAL
52 13
AFT ENTRY DOOR
55 20
52 22
EMERGENCY EXIT DOOR
ELEVATOR, HINGE SUPPORT AND BALANCE MECHANISM
52 31
CARGO DOOR
55 30
VERTICAL STABILIZER
52 48
EQUIPMENT COMPARTMENT EXTERIOR DOORS
55 40
RUDDER
56 11
FLIGHT COMPARTMENT WINDOWS
57 10
INTERSPAR WING
Date: 23-jul-08
ATA Break-Down
Page 4 of 5
HHI
737-6
MAINTENANCE SCHEDULE
ATA
DEFINITION
ATA
DEFINITION
57 12
FRONT AND REAR SPAR
74 21
IGNITION LEADS
57 14
CENTER WING BOX
78 11
TURBINE EXHAUST SYSTEM
57 15
MAIN LANDING GEAR TRUNNION SUPPORT BEAM
78 31
THRUST REVERSER SYSTEM ( HARDWARE)
57 21
LEADING EDGE
79 00
ENGINE OIL GENERAL
57 22
TRAILING EDGE
79 21
ENGINE OIL FILTER
57 31
WING UPPER SURFACE
80 11
STARTER
57 32
WING LOWER SURFACE
CM 21
AIR CONDITIONING
57 35
WING FITTINGS
CM 23
COMMUNICATIONS
57 52
TRAILING EDGE FLAPS
CM 24
ELECTRICAL POWER
57 54
SLATS
CM 25
EQUIPMENT/ FURNISHING
57 55
SPOILER
CM 26
FIRE PROTECTION
71 11
INLET COWL
CM 27
FLIGHT CONTROLS
71 71
ENGINE DRAINS
CM 28
FUEL
72 00
ENGINE
CM 29
HYDRAULIC POWER
72 20
FAN SECTION
CM 31
INSTRUMENTS
72 21
SPINNER CONE
CM 32
LANDING GEAR
72 23
THRUST MOUNT FITTINGS
CM 33
AIRCRAFT LIGHTING SYSTEM
72 30
COMPRESSOR SECTION
CM 34
NAVIGATION
72 50
TURBINE SECTION
CM 35
OXYGEN
72 60
ACCESSORY DRIVE SECTION
CM 36
PNEUMATIC
73 11
FUEL FILTER
CM 49
AUXILIARY POWER
73 21
FUEL CONTROL SYSTEM
CM 72
ENGINE
Date: 23-jul-08
ATA Break-Down
Page 5 of 5
HHI
737-6
MAINTENANCE SCHEDULE LIST OF EFFECTIVE ITEMS
05100- 00000 05100- 01000 05110- 00000 05110- 01000 05110- 02000 05111- 00000 05112- 00000 05120- 00000 05120- 01000 05120- 02000 05120- 03000 05120- 04000 05122- 00000 05130- 00000 05130- 01000 05130- 02000 05139- 00000 05141- 00000 05141- 01000 05141- 02000 05141- 03000 05142- 00000 05143- 00000 05145- 00000 05190- 00000 05191- 00000 05192- 00000 05194- 00000 05194- 01000 05195- 00000 Date: 23-jul-08
03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 22-mar-07 18-mar-05 18-mar-05 18-mar-05 03-jun-04 22-mar-07 18-mar-05 18-mar-05 03-jun-04 22-mar-07 22-mar-07 03-jun-04 18-mar-05 18-mar-05 22-mar-07 18-mar-05 23-jul-08 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08
05200- 00000 05210- 00000 05210- 01000 05210- 02000 05220- 00000 05220- 01000 05220- 02000 05221- 00000 05222- 00000 05230- 00000 05230- 01000 05230- 02000 05230- 03000 05240- 00000 05240- 01000 05240- 02000 05240- 03000 05241- 00000 05242- 00000 05300- 00000 05300- 01000 05310- 00000 05310- 01000 05310- 02000 05310- 03000 05310- 04000 05321- 00000 05322- 00000 05322- 01000 05322- 02000
03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 22-mar-07 03-jun-04 22-mar-07 22-mar-07 03-jun-04 22-mar-07 05-sep-06 05-sep-06 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 22-mar-07 13-apr-00 22-mar-07 22-mar-07 22-mar-07 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04
05323- 00000 05323- 01000 05324- 00000 05324- 01000 05325- 00000 05326- 00000 05331- 00000 05332- 00000 05332- 01000 05333- 00000 05333- 01000 05334- 00000 05335- 00000 05400- 00000 05410- 00000 05410- 01000 05410- 02000 05410- 03000 05411- 00000 05431- 00000 05432- 00000 05433- 00000 05434- 00000 05500- 00000 05500- 01000 05511- 00000 05511- 01000 05512- 00000 05512- 01000 05520- 00000
LIST OF EFFECTIVE ITEMS
22-mar-07 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 22-mar-07 22-mar-07 22-mar-07 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 05-sep-06 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04
05521- 00000 05521- 01000 05526- 00000 05526- 01000 05531- 00000 05531- 01000 05532- 00000 05532- 01000 05533- 00000 05533- 01000 05534- 00000 05541- 00000 05542- 00000 05542- 01000 05543- 00000 05543- 01000 05544- 00000 05544- 01000 05551- 00000 05551- 01000 05552- 00000 05553- 00000 05553- 01000 05560- 00000 05561- 00000 05567- 00000 05571- 00000 05571- 01000 05571- 02000 05572- 00000
03-jun-04 03-jun-04 03-jun-04 25-apr-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 03-jun-04 25-apr-06 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 Page 1 of 8
HHI 05700- 00000 05710- 00000 05730- 00000 05730- 01000 05800- 00000 05800- 01000 05821- 00000 05821- 01000 05822- 00000 05822- 01000 05831- 00000 05831- 01000 05833- 00000 05833- 01000 05834- 00000 05834- 01000 05841- 00000 05841- 01000 05843- 00000 05843- 01000 05844- 00000 05844- 01000 05900- 20290 05900- 20300 05900- 20310 05900- 20320 05900- 20330 05900- 20340 05900- 20350 05900- 20360 05900- 20370 05900- 20380 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 03-jun-04 22-mar-07 22-mar-07 18-mar-05 22-mar-07 03-jun-04 22-mar-07 03-jun-04 22-mar-07 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 22-mar-07 23-jul-08 03-jun-04 03-jun-04 22-mar-07 22-mar-07 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08
05900- 20390 05900- 20400 05900- 20410 05900- 20420 05900- 20430 05900- 20440 05900- 20450 05900- 20460 05900- 20470 05900- 20480 05900- 20490 05900- 20500 05900- 20510 05900- 20520 05900- 20530 05900- 20540 05900- 20550 05900- 20560 05900- 20570 05900- 20580 05900- 20590 05900- 20600 05900- 20610 05900- 20620 081000 01000 212502 40000 212503 00000 212700 70000 212700 71000 212700 89000 212701 00000 213100 71000
23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 30-nov-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 18-mar-05
213203 70000 213300 00000 215103 00000 215105 40000 216106 10000 232400 00000 233011 00000 236000 76000 237100 71000 237100 73000 237121 00000 240000 01000 240000 02000 240000 03000 240000 04000 240000 05000 240000 06000 240000 07000 240000 08000 240000 09000 240000 09100 240000 10000 240000 11000 240000 13000 240000 14000 240000 15000 240000 16000 240000 18000 241141 00000 241161 20000 243141 72000 243400 71200
LIST OF EFFECTIVE ITEMS
03-jun-04 18-mar-05 03-jun-04 18-mar-05 25-apr-06 18-mar-05 23-jul-08 03-jun-04 18-mar-05 03-jun-04 03-jun-04 25-apr-06 18-mar-05 18-mar-05 05-sep-06 05-sep-06 22-mar-07 22-mar-07 05-sep-06 05-sep-06 22-mar-07 05-sep-06 05-sep-06 05-sep-06 18-mar-05 03-jun-04 05-sep-06 03-jun-04 25-apr-06 25-apr-06 03-jun-04 03-jun-04
250000 01000 250000 04001 250000 05001 250000 06001 250000 08001 250000 09001 250000 13001 250000 14001 250000 15001 250000 22000 251100 20000 251100 20100 251111 20000 252200 20000 252200 71000 252200 71100 252512 20000 252512 71000 252512 71200 254008 00000 255200 20000 255200 20100 255200 21000 256110 20000 256110 71000 256110 71100 256299 00001 256400 21000 256400 71100 256400 71200 256401 21000 256401 71000
23-jul-08 11-dec-01 11-dec-01 03-jun-04 11-dec-01 23-jul-08 11-dec-01 11-dec-01 11-dec-01 11-dec-01 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 18-mar-05 22-mar-07 05-sep-06 05-sep-06 03-jun-04 23-jul-08 03-jun-04 30-nov-05 30-nov-05 03-jun-04 23-jul-08 Page 2 of 8
HHI 256402 90000 256403 20000 256404 90000 256405 90000 256600 71000 256601 00000 256601 20000 256601 40000 257100 21000 260000 01000 261400 73000 261401 10000 261500 71000 262000 01000 262000 02000 262000 21000 262001 72000 262001 72100 262001 72200 262001 73000 262002 21000 262003 21000 262300 00650 262300 01000 262300 02000 262300 03000 262300 04000 262300 05000 262401 00000 262401 01000 262401 90000 262500 01000 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 30-nov-05 22-mar-07 23-jul-08 23-jul-08 30-nov-05 22-mar-07 03-jun-04 23-jul-08 03-jun-04 13-apr-00 18-mar-05 18-mar-05 22-mar-07 03-jun-04 03-jun-04 25-apr-06 18-mar-05 03-jun-04 03-jun-04 05-sep-06 03-jun-04 03-jun-04 05-sep-06 05-sep-06 05-sep-06 05-sep-06 22-mar-07 05-sep-06 25-apr-06 25-apr-06 03-jun-04 03-jun-04
270000 00000 270000 01000 270000 02000 270000 03000 270000 04000 270000 05000 270000 06000 270000 07000 270000 08000 270000 09000 270000 10000 270000 11000 270000 12000 270000 13000 270000 14000 270000 15000 270000 16000 270000 17000 270000 18000 270000 19000 270000 20000 270000 21000 270000 22000 270000 25000 270000 32000 270000 35000 271100 21000 271100 21100 271100 71000 271100 71100 271100 73000 271100 82000
23-jul-08 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 18-mar-05 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 18-mar-05 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 03-jun-04 18-mar-05 03-jun-04 22-mar-07 18-mar-05
271101 70000 271101 70100 271101 71000 271101 72000 271131 21000 271131 22000 271161 21000 272100 03000 272100 60000 272100 65000 272100 80000 272100 85000 272100 86000 272100 87000 272101 70000 272102 70000 272103 70000 272124 21000 272124 22000 272151 21000 272161 21000 272171 00000 272182 00000 273100 01000 273100 70000 273100 71000 273100 72000 273100 73000 273100 82000 273101 70000 273101 75000 273102 01000
LIST OF EFFECTIVE ITEMS
18-mar-05 03-jun-04 03-jun-04 30-nov-05 03-jun-04 29-apr-03 18-mar-05 23-jul-08 29-apr-03 18-mar-05 03-jun-04 25-apr-06 05-sep-06 05-sep-06 18-mar-05 18-mar-05 03-jun-04 03-jun-04 18-mar-05 18-mar-05 05-sep-06 03-jun-04 03-jun-04 18-mar-05 18-mar-05 18-mar-05 03-jun-04 18-mar-05 03-jun-04 18-mar-05 23-jul-08 03-jun-04
273111 00000 273114 21000 273114 21100 273114 22000 273117 20000 273120 00000 273134 21000 273134 21500 273161 21000 273164 90000 273200 71000 274100 70000 274101 70000 274102 70000 274103 70000 274141 21000 274181 00000 274181 01000 274181 21000 274191 70000 274197 70000 275100 21000 275100 71000 275100 72000 275100 73000 275100 74000 275100 74100 275101 21000 275101 74000 275106 21000 275132 22000 276100 21000
03-jun-04 18-mar-05 30-nov-05 03-jun-04 18-mar-05 18-mar-05 18-mar-05 23-jul-08 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 18-mar-05 05-sep-06 23-jul-08 23-jul-08 18-mar-05 18-mar-05 22-mar-07 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 23-jul-08 03-jun-04 23-jul-08 Page 3 of 8
HHI 276100 71000 276100 72000 276100 73000 276100 82000 276101 82000 276200 21000 276201 21000 276201 82000 276202 82000 278100 21000 278100 70000 278100 71000 278100 86000 278300 71000 280000 03000 280000 04000 280000 05000 280000 06000 280000 76000 281100 01000 281100 21000 281331 10000 281331 20000 281341 20000 281341 21000 282111 20000 282151 20000 282200 20000 282200 21000 282200 71000 282200 72000 282200 72100 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 22-mar-07 30-nov-05 30-nov-05 03-jun-04 03-jun-04 23-jul-08 18-mar-05 05-sep-06 18-mar-05 18-mar-05 25-apr-06 18-mar-05 18-mar-05 03-jun-04 11-dec-01 11-dec-01 11-dec-01 23-jul-08 23-jul-08 23-jul-08 03-jun-04 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 05-sep-06 03-jun-04 18-mar-05
282211 20000 282211 72000 282213 20000 282214 00000 282502 20000 282505 79000 284100 01000 284100 28000 284100 29000 284100 71000 290000 01000 290000 01100 290000 06000 290011 01000 291100 20000 291100 30000 291102 00000 291103 00000 291104 20000 291121 00000 291141 00000 291151 00000 291161 00000 291171 40000 291811 00000 292100 60000 292100 61000 292100 70000 292141 00000 292151 00000 292200 73000 292201 71000
23-jul-08 23-jul-08 18-mar-05 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 03-jun-04 11-dec-01 11-dec-01 03-jun-04 18-mar-05 25-apr-06 22-mar-07 30-nov-05 25-apr-06 23-jul-08 03-jun-04 18-mar-05 25-apr-06 18-mar-05 03-jun-04 03-jun-04 22-mar-07 30-nov-05 23-jul-08 22-mar-07 22-mar-07 03-jun-04 22-mar-07
292221 02000 293200 73000 313100 97000 313109 70000 315100 73000 315100 74000 315101 73000 315102 73000 316200 00000 320000 01000 320000 03000 320000 04000 320000 05000 320000 08000 320000 09000 320000 11000 320000 21000 320000 31000 320000 41000 320000 60000 320000 61000 320000 62000 320000 63000 320000 64000 320000 65000 320000 66000 320000 67000 320000 68000 320010 00000 321100 01000 321100 40000 321100 50000
LIST OF EFFECTIVE ITEMS
22-mar-07 03-jun-04 18-mar-05 03-jun-04 18-mar-05 18-mar-05 18-mar-05 18-mar-05 22-mar-07 22-mar-07 22-mar-07 25-apr-06 22-mar-07 03-jun-04 22-mar-07 24-mar-99 24-mar-99 23-jul-08 24-mar-99 22-mar-07 22-mar-07 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 22-mar-07 22-mar-07 05-sep-06
322100 00000 322100 21000 322100 22000 322100 60000 322110 00100 322110 00200 322110 10000 322171 20000 323100 00000 323151 20000 323171 40000 323221 00000 323400 70000 323500 73000 324100 71000 324100 72000 324131 00000 324141 70000 324181 00000 324400 79000 324411 00000 324500 70000 324511 40000 324521 00000 325121 00000 326100 71000 335100 72000 335103 96000 335105 96000 341100 17000 341100 79000 341101 17000
22-mar-07 22-mar-07 22-mar-07 03-jun-04 22-mar-07 05-sep-06 03-jun-04 23-jul-08 25-apr-06 22-mar-07 03-jun-04 05-sep-06 25-apr-06 25-apr-06 18-mar-05 03-jun-04 22-mar-07 03-jun-04 22-mar-07 22-mar-07 22-mar-07 23-jul-08 03-jun-04 03-jun-04 22-mar-07 30-nov-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 22-mar-07 Page 4 of 8
HHI 341101 20000 341102 20000 342400 02000 345300 73000 346002 00001 350000 01000 350000 02000 350000 04000 350000 05000 350000 06000 350000 09000 351200 70000 351200 70001 351200 71000 352101 00000 352101 01000 352200 70000 352231 21000 353100 71000 361400 00000 381106 00000 381106 10000 381106 20000 383200 10000 383202 00100 383203 00000 383205 96000 383300 74000 384210 96000 490011 10000 491111 40000 491311 20000 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 18-mar-05 18-mar-05 29-apr-03 23-jul-08 23-jul-08 11-dec-01 11-dec-01 03-jun-04 11-dec-01 11-dec-01 18-dec-02 05-sep-06 03-jun-04 25-apr-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 18-mar-05 22-mar-07 05-sep-06 18-mar-05 22-mar-07 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04
491511 20000 491522 00000 491611 10000 491611 11000 491611 19900 491711 20000 493011 40000 493021 00000 494151 20000 496100 70000 496100 90000 498111 20000 498111 20100 498111 20200 499111 00000 499113 20000 499141 20000 499171 20000 499171 21000 521100 00000 521100 01000 521100 02000 521100 03000 521100 04000 521100 05000 521100 06000 521100 09000 521100 09100 521100 09200 521200 00000 521200 00500 521200 01000
03-jun-04 03-jun-04 23-jul-08 23-jul-08 18-mar-05 03-jun-04 23-jul-08 03-jun-04 23-jul-08 30-nov-05 23-jul-08 03-jun-04 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 30-nov-05
521200 01500 521200 02000 521200 02500 521200 03000 521200 03500 521200 04000 521200 05000 521200 06000 521300 00000 521300 01000 521300 02000 521300 03000 521300 04000 521300 05000 521300 06000 522200 00000 522200 01000 522200 02000 522200 03000 522200 04000 522200 05000 522200 06000 522200 07000 522200 07500 523100 00000 523100 00500 523100 01000 523100 01500 523100 02000 523100 03000 523100 05000 523100 06000
LIST OF EFFECTIVE ITEMS
30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 03-jun-04 18-mar-05 18-mar-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04
524800 00000 524800 02000 524800 03000 524800 04000 524800 07000 524900 00000 524900 01000 524900 02000 526000 00000 526000 01000 526050 21000 527000 00000 527000 01000 527000 02000 527000 03000 527000 04000 527000 05000 527000 07000 527001 00000 527001 01000 527001 02000 527001 04000 527100 00000 530900 00000 530900 01000 530900 02000 530900 03000 530900 04000 530900 05000 530900 06000 530900 07000 530900 08000
03-jun-04 23-jul-08 05-sep-06 05-sep-06 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 23-jul-08 30-nov-05 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 23-jul-08 03-jun-04 23-jul-08 23-jul-08 03-jun-04 18-mar-05 23-jul-08 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 23-jul-08 Page 5 of 8
HHI 530900 09000 530900 10000 530900 11000 530900 12000 530900 13000 530900 14000 530900 15000 530900 16000 531300 00000 531300 01000 531300 02000 531500 00000 531500 01000 531500 02000 531500 03000 531500 04000 533000 00000 533000 01000 533000 02000 533000 03000 533000 04000 533000 05000 533000 06000 535100 00000 538100 00000 538100 01000 538100 02000 538200 00000 538200 01000 538200 02000 538200 03000 538200 04000 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 22-mar-07 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 05-sep-06 18-mar-05 05-sep-06 03-jun-04 03-jun-04 18-mar-05 03-jun-04 03-jun-04 18-mar-05 03-jun-04 05-sep-06 03-jun-04 03-jun-04
538400 00000 538500 00000 538500 01000 538500 02000 538500 03000 538500 04000 543000 00000 543000 01000 543001 00000 543002 00000 544000 00000 544000 01000 544000 02000 544000 03000 544000 04000 544000 05000 544000 06000 544000 06100 551000 00000 551000 01000 551000 02000 551000 03000 551000 05000 551000 06000 551000 07000 552000 00000 552000 01000 552000 03000 553000 00000 553000 01000 553000 02000 554000 00000
03-jun-04 18-mar-05 03-jun-04 05-sep-06 03-jun-04 03-jun-04 25-apr-06 25-apr-06 30-nov-05 30-nov-05 23-jul-08 03-jun-04 25-apr-06 05-sep-06 25-apr-06 03-jun-04 23-jul-08 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 23-jul-08 03-jun-04 23-jul-08 03-jun-04
561100 00000 561100 01000 561100 02000 561100 03000 571000 00000 571000 01000 571000 02000 571000 03000 571000 04000 571000 05000 571200 00000 571400 00000 571400 01000 571400 02000 571400 03000 571400 04000 571400 05000 571400 05500 571400 07000 571500 00000 572100 00000 572200 00000 573100 00000 573100 02000 573200 01000 573200 02000 573200 03000 573200 04000 573200 05000 573500 00000 575200 00000 575200 01000
LIST OF EFFECTIVE ITEMS
03-jun-04 03-jun-04 23-jul-08 23-jul-08 25-apr-06 25-apr-06 25-apr-06 23-jul-08 03-jun-04 03-jun-04 03-jun-04 25-apr-06 05-sep-06 23-jul-08 05-sep-06 23-jul-08 23-jul-08 23-jul-08 23-jul-08 25-apr-06 03-jun-04 23-jul-08 23-jul-08 25-apr-06 23-jul-08 25-apr-06 25-apr-06 25-apr-06 25-apr-06 23-jul-08 25-apr-06 25-apr-06
575200 02000 575200 06000 575200 07000 575400 00000 575500 00000 711101 20000 711102 20000 711103 20000 711104 20000 717100 20000 717100 70000 720000 20000 720000 20200 720000 20300 720000 20400 720011 01200 720021 00200 722000 21000 722100 20000 722100 22000 722304 20000 722304 21000 723000 31000 725000 20000 726000 20000 731102 00000 732100 74000 742101 20000 742102 20000 781100 21000 783100 70000 783100 71000
25-apr-06 03-jun-04 03-jun-04 25-apr-06 25-apr-06 03-jun-04 23-jul-08 02-aug-99 03-jun-04 23-jul-08 25-apr-06 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 25-apr-06 23-jul-08 23-jul-08 18-mar-05 23-jul-08 30-nov-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 Page 6 of 8
HHI 783100 73000 783106 20000 783107 90000 783112 20000 783112 21000 783114 20000 783123 20000 790000 20000 790000 20500 790000 80000 792103 00000 792106 00000 801101 20000 CM2132 00000 CM2324 00000 CM2371 00010 CM2430 00010 CM2560 00020 CM2560 00021 CM2560 00030 CM2560 00031 CM2564 00020 CM2564 00090 CM2566 00010 CM2566 00020 CM2566 00030 CM2566 00040 CM2600 00010 CM2621 00010 CM2621 00020 CM2622 00010 CM2622 00020 Date: 23-jul-08
737-6
MAINTENANCE SCHEDULE 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 23-jul-08 23-jul-08 23-jul-08 18-mar-05 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 25-apr-06 23-jul-08 03-jun-04 22-mar-07 26-jun-02 22-mar-07 30-nov-05 03-jun-04 30-nov-05 03-jun-04
CM2623 00010 CM2626 00010 CM2626 00020 CM2721 00010 CM2740 00020 CM2822 00010 CM2900 00010 CM2900 00020 CM2900 00030 CM2911 00010 CM2921 00010 CM2921 00020 CM2999 00010 CM2999 00020 CM2999 00030 CM3131 00010 CM3211 00010 CM3211 00020 CM3211 00030 CM3211 00040 CM3211 00050 CM3211 00060 CM3211 00070 CM3211 00080 CM3211 00090 CM3211 00100 CM3211 02000 CM3211 03000 CM3211 04000 CM3211 05000 CM3211 06000 CM3211 07000
03-jun-04 30-nov-05 30-nov-05 30-nov-05 23-jul-08 03-jun-04 03-jun-04 23-jul-08 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 03-jun-04 23-jul-08 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02
CM3211 08000 CM3211 09000 CM3211 10000 CM3211 11000 CM3211 12000 CM3211 13000 CM3211 14000 CM3211 15000 CM3211 16000 CM3211 17000 CM3211 18000 CM3211 19000 CM3211 20000 CM3211 21000 CM3211 22000 CM3211 23000 CM3211 24000 CM3211 25000 CM3211 26000 CM3211 27000 CM3211 28000 CM3211 29000 CM3211 30000 CM3211 31000 CM3211 32000 CM3211 33000 CM3211 34000 CM3211 35000 CM3211 36000 CM3211 37000 CM3211 38000 CM3211 39000
LIST OF EFFECTIVE ITEMS
17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02
CM3211 40000 CM3221 00010 CM3221 00020 CM3221 00030 CM3221 01040 CM3221 02000 CM3221 03000 CM3221 04000 CM3221 05000 CM3221 06000 CM3221 07000 CM3221 08000 CM3221 09000 CM3221 10000 CM3221 11000 CM3221 12000 CM3221 13000 CM3221 14000 CM3221 15000 CM3221 16000 CM3221 17000 CM3221 18000 CM3221 19000 CM3221 20000 CM3221 21000 CM3232 00010 CM3241 00020 CM3241 00030 CM3351 00010 CM3410 00010 CM3453 00010 CM3510 00010
17-oct-02 03-jun-04 03-jun-04 03-jun-04 12-jun-01 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 17-oct-02 03-jun-04 17-oct-02 17-oct-02 17-oct-02 17-oct-02 22-mar-07 03-jun-04 03-jun-04 23-jul-08 29-apr-03 23-jul-08 03-jun-04 Page 7 of 8
HHI CM3512 00010 CM3512 01010 CM3522 00110 CM3531 00010 CM3610 00010 CM3610 00020 CM4900 01010 CM4900 01020 CM4900 01030 CM4900 01040 CM7200 20010 CM7200 20020 CM7200 20030 CM7200 20040 CM7200 20050 CM7200 20051 CM7200 20060 CM7200 20070 CM7200 20080 CM7200 20090 CM7200 20100 CM7200 20110 CM7200 20120 CM7200 20130 CM7200 20140 CM7200 20150 CM7200 20160 CM7200 20170 CM7200 20180 CM7200 20200 CM7200 20210 CM7200 20230 Date: 23-jul-08
MAINTENANCE SCHEDULE 30-nov-05 03-jun-04 03-jun-04 23-jul-08 18-mar-05 03-jun-04 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 22-mar-07 22-mar-07 18-mar-05 22-mar-07 22-mar-07 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 23-jul-08 18-mar-05 18-mar-05 18-mar-05 18-mar-05 22-mar-07 18-mar-05 11-jan-01 23-jul-08 23-jul-08
CM7200 20240
737-6
23-jul-08
LIST OF EFFECTIVE ITEMS
Page 8 of 8
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1
737-6
GENERAL
This Maintenance Schedule constitutes the maintenance program for the systems, power plant and structure of the B737-700 aircraft as defined/required by Regulation (EC) 2042/2003 Part M. It includes scheduled maintenance tasks and frequencies required by the B737-6/-7/-8 MAINTENANCE REVIEW BOARD REPORT (MRB Document) and other mandatory requirements, complemented by additional maintenance tasks considered for their economical effectiveness, reliability improvement as well as for passenger comfort and appearance reasons. The Maintenance Schedule is part of the approved maintenance system. Other part of the maintenance system is the Component Maintenance Section.
1.1
Validity
This Maintenance Schedule is valid for all Boeing B737-700 aircraft equipped with CFM56-7B22 / -7B24 Engine and GTCP131-9B APU operated by: Hamburg International Luftverkehrsgesellschaft mbH Hindenburgstr. 171 D-22297 Hamburg Germany For aircraft basic data information, see chapter 5.
Date: 23-Jul-2008
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1.2
737-6
Responsibilities
This Maintenance Schedule is prepared under the responsibility of Hamburg International by: Lufthansa Technik Aktiengesellschaft Department FRA WE Rhein-Main Airport 60546 Frankfurt/Main Germany This Maintenance Schedule is owned and released by : Hamburg International Luftverkehrsgesellschaft mbH Hindenburgstr. 171 D-22297 Hamburg Germany
1.3
Average Utilization
The application of this maintenance program assumes an average utilization of 3000 + 10% FH per year. Some items are sensitive to flight length and require both flight hours and flight cycles to determine the implementation threshold. For those items the threshold is determined by the Flight Length Sensitive (FLS) Threshold Curve (MPD Section 9 Figure 1 and 2). In addition, for supplemental structural inspection items the Damage Tolerance Rating (DTR) system is used to determine the inspections and repeat intervals necessary to provide adequate fatigue damage detection . All Items depending on Flight Length Sensitive (FLS) Threshold Curve and DTR Check Forms are determined based on an average FC to FH ratio of 0.46. The thresholds/intervals will be recalculated if a major change to the HHI flight profile occurs. Items depending on FLS/DTR are identified in the Interval Note NOTE(I), e.g. MS57.14.00.05500
Date: 23-Jul-2008
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1.4
737-6
Operator’s Statement
With reference to Appendix 1 to AMC M.A.302 Para. 1.1.4, Hamburg International confirms, that aircraft mentioned under section 1.1 will be maintained to this program, which will be reviewed and updated as required by AMC M.A.302 and as outlined in MM & OE Part 3, Chapter 3.2.
With reference to Appendix 1 to AMC M.A.302, Para. 1.1.18, Hamburg International confirms, that the practices and procedures to satisfy this program are to the standards specified in the Type Certificate Holder’s Maintenance Instructions.
-------------------------------------------------------------------Hamburg International Luftverkehrsgesellschaft mbH the Operator
Date: 23-Jul-2008
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1.5
737-6
Authority Approval
According to M.A.302 (a) & (b), this document and any subsequent amendment must be approved by the German Airworthiness Authority „Luftfahrt Bundesamt (LBA)“. Details about approval requirement are described in para. 2.14.1. For signature, see Document Approval Sheet.
1.6 A.
B. C.
D.
Explanation of Regulation Due to practical considerations, splitting of maintenance checks or packages and performance together with lower maintenance events may be possible as long as it is assured that each check item mentioned in the interval column of the Maintenance Schedule will be repeated at the required maintenance interval. Flight hour and cycle limited items can also be treated in accordance with this paragraph. If necessary, a check to be performed on parts/components located in several positions at the aircraft (e.g. at engine 1 and 2) may be performed together with other, lower maintenance events as long as the time between the check does not exceed the inspection interval. The maintenance intervals specified in the Maintenance Schedule must not exceed the end of a scheduled flight program (see Flight Program). If a flight program should exceed the normal standard flight time (see Normal Standard Flight Time) respectively the scheduled layover time due to events that are beyond the control of the Aircraft Routing Department. (e.g. alternate landings, strong headwinds, holding, delays, cancellations) the maintenance interval (flight hours or calendar time) may be exceeded as far as it is necessary for the aircraft to complete its flight program until reaching the maintenance station (see Maintenance Station) determined for this particular flight program. Continuing Airworthiness and other Service Information must be continuously evaluated by the operator and, where necessary, appropriate action must be taken to amend the Maintenance Schedule.
1.6.1 Flight Program Is a flight of a certain aircraft from a certain predetermined maintenance station, via several line stations, back to that maintenance station or to another predetermined maintenance station.
Date: 23-Jul-2008
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1.6.2 Normal Standard Flight Time Is the time, which has been pre calculated and will serve as a basis for aircraft routing and operational control.
1.6.3 Maintenance Station In this context is a station, where Daily-Checks and higher checks are performed
1.7
Revision Procedure
Revisions of this Maintenance Schedule will be prepared under the responsibility of Hamburg International by Lufthansa Technik AG, Engineering Dept. FRA WE and released by Hamburg International Luftverkehrsgesellschaft mbH and approved by the German Airworthiness Authority „Luftfahrt Bundesamt (LBA). MS pages amendments will be issued with a new effectivity date. Every amendments issue will include a list of highlights indicating significant changes. Each revision should be signed off in the Record Sheet of Revision. Following chapters of the MS are reissued completely with every MS revision : • • • • • •
Table of Contents Highlights ATA Break Down List of Effective Items Introduction Aircraft Zones
Only those pages with issue date of the latest revision (according to Record of Revision page) shall be used.
Date: 23-Jul-2008
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Temporary Revisions Changes to the Maintenance Schedule with high importance and/or high urgency may be incorporated between the regular revision periods by issue of a Temporary Revision (TR). The TR is edited including the following parts: • List of Effective Pages (LEP) • Approval Sheet • Record of Eff. Temporary Revisions • Introduction Page(s) (if necessary) and /or MS Page(s), where tasks have been changed/added/deleted. The TR must be filed into the Maintenance Schedule document, which should be confirmed in the “Record of Revision“ Sheet 2 (“Page 2 of 2”). If a subsequent regular MS Revision includes or supersedes a TR, this will be stated in the Highlights of that respective Revision. The “Record of Eff. Temporary Revisions“ Sheet lists only those TRs which are still effective.
1.8
Reliability Monitoring Program
A Reliability Monitoring Program acc. to M.A.301 (4) is necessary to ensure the effectiveness of the maintenance program. Review of the reliability data will be used to adjust the maintenance program as required. Accordance. to Appendix 1 to AMC M.A.302 Item 5.2.the Operator will review the detailed requirements for the Maintenance Program annually for continued validity in the light of operating experience. See also CAMOE Part 3 Chapter 3.10.
1.8.1 Aircraft Reliability Monitoring Aircraft and engine reliability data can be retrieved from the HHI Reliability Report, issued on a monthly basis. The report contains data regarding operational parameters such as aircraft in service, total flight hours, total take off, daily utilization, etc... including data regarding incidents, maintenance- and pilot-reports and delays/cancellations.
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1.8.2 Engine Condition Monitoring Engine parameters like EGT, Fuel Flow, N2 and N1 will be recorded on the Engine and Cruise Report and sent to Engineering. The parameters are continuously analyzed by engineering and, if necessary, will result in a corrective maintenance action.
1.8.3 Component Reliability Monitoring Component reliability data such as MTBR, MTBUR and MTBF will be retrieved from Lufthansa Technik EDP system with „CORIS“.
1.9
Reference Documents
This Maintenance Schedule is developed from the following documents : - B737-6/-7/-8 Maintenance Review Board Report, issued by the FAA // Revision March 2007 // incl. TR 02-003 and TR02-004 - B737-6/-7/-8 Maintenance Planning Document (Boeing-Document No.: D626A001), issued by Boeing // Revision June 2008 // - B737 Airworthiness Limitation (AWLs) and Certification Maintenance Requirements CMR (Boeing-Doc No. D626A001-CMR) dated // March 2008 // - CFM56-7B Engine Manual Revision 37 issued by SNECMA, dated 15 May 2008. - APU Manual 49-00-00, Revision 4, dated 05. Oct. 2007.
Date: 23-Jul-2008
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2
MAINTENANCE PROGRAM
2.1
Line Maintenance
737-6
The responsibility for accomplishing the task may be indicated in the "Performed-by"-column (FC = Flight Crew incl. Cabin Crew / SM = Station Mechanic). If this column is blank, the task is the duty of the maintenance personal. T = Trip Check Tasks to be performed by flight crew are to be accomplished prior to each flight. Tasks may also be performed by station mechanics. Trip Check has to be performed at ramp position not earlier than two hours before take-off. The Trip Check covers the requirements from Appendix 1 to AMC M.A.302, Item 1.1.9 Pre-Flight-Inspection Note: Before training - and test-flights - before the first takeoff of a training period and after each flight training period a walk around check has to be performed. The trip check has to be repeated if the training /test flight is interrupted for more than 2 hours. Z = Daily Check Tasks to be accomplished every 48 hours elapsed time. All other items in this Maintenance Schedule issue are listed in usage parameters (days, month, flight hours, cycles), as given in the manufacturer documentation. Where intervals are given in two dimensions (e.g. 75 days / 400 cycles), the rule "Which ever comes first" applies. HHI together with LHT production planning may find it useful to group the items from this Maintenance Schedule to packages which will be performed together. Eventually, these groups may be given check abbreviations as monthly, annual or letter checks. However, the maximum interval given in this Maintenance Schedule must not be exceeded. These groups may be handled independent from this Maintenance Schedule, or if deemed useful, be introduced in this Maintenance Schedule.
Date: 23-Jul-2008
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2.2
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Base Maintenance
All tasks included within the Annual Visit inspections and higher are considered to be Base Maintenance.
2.3
Time Controlled Maintenance
In addition to the intervals expressed in letter-codes, usage parameters such as • flight hours: FLH • flight cycles: CYC • calendar time • days: DAY • months: MTH • years: YRS • Engine/APU change : EC/AC • S. N (see Note): Indicated that check-interval is described in an interval (I) note. are called for where appropriate.
2.4
Zonal Inspection Program
The Zonal Inspection Program is contained in the ATA Chapter 05. It requires a General Visual Inspection (i.e. task code E1 or E2) of the specified aircraft zone in order to check system and power plant installation and structure for security and general condition. The extent of the inspection is defined by the access (identification of access doors, positioning of surfaces, removal of linings) and the whole of the zone is to be inspected as visible with the relevant access open. No inspection aid is required for accomplishment of inspections, however an additional lighting source may be used as deemed necessary. According AOM, VOL II, chapter 6.10, the flight crew shall perform an airplane's inspection of general condition which must include a check for obvious wear and damage of engines in/outlets, nose/main gear wheels, tires and brakes. This inspection is required due to the flight crew's obligation to assess the airworthiness of the airplane before each flight. As a result general visual inspection of airplane's condition and for obvious wear and damage of engines in/outlets, nose/main gear wheels, tires and brakes before each flight may be considered as crew tasks and therefore be excluded from the scheduled maintenance program. Date: 23-Jul-2008
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2.4.1 Enhanced Zonal Analysis Procedure (EZAP) An enhanced zonal analysis was performed for the interior of fuel tanks which contain electrical wiring and have a potential for combustible materials being present. This enhanced zonal analysis provided a means to identify applicable and effective tasks to minimize wiring contamination and to detect significant wiring installation discrepancies that may not be reliably detected through a standard zonal inspection. These dedicated tasks, containing (EZAP) in parenthesis as an identifier, are included in this MS under ATA 20. They are not system specific and do not have a failure effect category. Unless otherwise specified in the task, the disassembly of the bundle, connections, or clamps is not required. Wiring that is undisturbed will have less degradation than wiring that is disturbed during maintenance. The enhanced zonal analysis uses the existing Zonal requirements for a basis. All Zonal inspection requirements constitute Electrical Wiring Interconnection System (EWIS) Instructions for Continued Airworthiness (ICA). Electrical Wiring Interconnection System (EWIS) is used to describe inspection criteria. The term EWIS means any wire, wiring device, or combination of these, including termination devices, installed in the airplane for transmitting electrical energy between two of more termination points.
2.5
Structure Program
The Structure Program provides tasks and frequencies applicable to the aircraft structure with respect to fatigue damage, environment deterioration (corrosion) and accidental damage. For fatigue, flight cycles are used as the parameter for inspection thresholds and repeat intervals. (Threshold figures are identified by the abbreviation "T" in the intervals column). For environmental deterioration, as corrosion is mainly age dependent, inspection thresholds and repeat intervals are expressed in letter codes IL or D, which is a calendar time limit. For accidental damage, the repeat intervals are expressed in letter codes or flight cycles according to the damage consequence considered. Due to the random characteristics of accidental damage an inspection threshold is not introduced.
2.6
(Not used)
2.7
Corrosion Prevention and Control Program (CPCP)
The B737-600/-700/-800 Corrosion Prevention and Control Program (CPCP) is an integral part of the Structural Maintenance Program.
Date: 23-Jul-2008
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2.8
737-6
Identification of Type Certification and MRB Requirements
2.8.1 MSI, SSI, AWL and CMR Maintenance Significant Items (MSI) and Structural Significant Items (SSI) arise from the B737-6/-7/-8 MRB-Document. Airworthiness Limitation Items (AWLs) arise from the B737-6/-7/-8/-9 AWL and CMR-Document D626A001-CMR. One section of the Airworthiness Limitations contains an FAA approved program of scheduled inspections for operators to incorporate into their maintenance program for this type design to meet the new standards and assumptions introduced by FAA AC 25.981 and Special Federal Aviation Regulation SFAR No. 88. An AWL may be: an Airworthiness Limitation Instruction (ALI) or a Critical Design Configuration Control Limitation (CDCCL). ALIs identify inspection tasks related to fuel tank ignition source prevention which must be done to maintain the design level of safety for the operational life of the airplane. These ALIs are mandatory and cannot be changed or deleted without the approval of the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency. Strict adherence to methods, techniques and practices as prescribed is required to ensure the ALI is complied with. Any use of methods, techniques or practices not contained in these ALIs must be approved by the FAA office that is responsible for the airplane model Type Certificate, or applicable regulatory agency. Certification Maintenance Requirements (CMR) for system tasks arise from systems safety assessment. They are described in Section 9 of the B737-6/-7/-8 Maintenance Planning Document. These requirements are allocated to two categories (identified as "one star" and "two star") according to the failure condition consequence and the sensitivity of the safety objective to an interval increase. The identification of these items in the Maintenance Schedule is provided as follows: • MSIs are identified by quoting the MSI-number from the MRB-Document together with the MSG 3-Route (named MSG-Cat in the Maintenance Schedule) selected for this MSI. - Route 5 = Evident Safety Effects - Route 6 = Evident Economic (Operational) Effects - Route 7 = Evident Economic (Non-Operational) Effects - Route 8 = Hidden Function Safety Effects - Route 9 = Hidden Function Non-Safety Effects - Route 0 = Task Generated by MRB Determination Example: MRB 25-020-00 RTE:8 Date: 23-Jul-2008
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SSIs All SSI’s identified by the Manufacturer have been subjected to the MSG-3 analysis. This process has resulted in the identification of maintenance inspection tasks which are contained in the MRBR. SSIs are identified by quoting “MRB XX-3XX”. • AWLs are identified by quoting “AAR XX-AWL-XX“. The first and the second digits are the ATA Chapter Number. Example: AAR 28-AWL-01 • CMRs are identified by quoting “AAR CMR“. Example: CMR (525199 00002) All these references are located in the References column of the Maintenance Schedule.
2.9
Component Maintenance Program
The Component Maintenance Section ( Chapter CMS) reflects specific component maintenance tasks mandated by Airworthiness Authority Requirements. The storage requirements and limitations of Components are processed and controlled by Lufthansa Technik Component Tracking department.
2.10 Inspection Techniques Whenever the term "inspect" or "check" for satisfactory conditions is specified in this schedule, the term is defined as follows: • That the Zone / System / Item inspection is sufficient to establish at the time of inspection it is free of any defects likely to affect airworthiness and is expected to remain airworthy until the next scheduled inspection is due. • The inspection must comply with the minimum standards set out hereunder having regard to the environment and to the materials of construction of the Zone / System / Item. • Unless otherwise stated in the schedule, all the inspection requirements are to be applied without removing an item from the aircraft or dismantling the item in-situ unless this is considered essential, in which case this is specified. This, however, does not preclude removal or dismantling, or such other inspection activity as is considered essential. • Where a particular area or item is highlighted in the item it is considered as significant and should be given special attention during inspection.
Date: 23-Jul-2008
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Metal Parts All structural members, honeycomb bonded structure, bodies or casings of units in systems and in instrument, electrical and radio installations, metal pipes ducting, tubes, rods, levers, etc., inspect for: • Cleanliness, evidence of external damage, leaks, overheating or discharge, bulging, obstructions of drainage or vent holes, security of attachments, fasteners and visible connections, locking and bonding. • Freedom of cracks (visual) distortion, dents, bolts, screws. • Separation of bond, failure of welds and spot welds. Deterioration of protective treatment and corrosion. Correct sealing of fairings, fluid ingress. Rubber, Fabric, Fiber Glass and Plastic Parts Honeycomb bonded structure, ducting, flexible pipes, flexible mountings, seals, insulation of electrical cables, windows etc. Inspect for: • Separation of bond, cleanliness, cracks, cuts, chafing, kinking, twisting, crushing, sufficient free length for movement, deterioration, crazing, loss of flexibility, overheating, fluid spillage. • Security of attachment (supports, packings and electrical bonding correctly positioned, serviceable). Fuel Airworthiness Limitations CDCCLs • The purpose of the CDCCL is to provide instructions to retain critical ignition source prevention feature during configuration change that may be caused by alterations, repairs, or maintenance actions. For details refer to Boeing CMR (Boeing-Doc No. D626A001-CMR), latest revision (see chapter 1.9). All applicable manufacturer documents have been revised accordingly. (e.g. AMM,CMM,…) Control System Components Inspect for: • Correct alignment, no fouling. Free movement, distortion, evidence of bowing, scores, chafing, fraying, kinking, evidence of wear, fretting, cracks, loose rivets, deterioration of protective treatment, corrosion. Electrical bonding correctly positioned, undamaged and secure. Attachments, connections and locking secure. Electrical Motors, Alternators, Generators and Actuators Inspect for: • Cleanliness, obvious damage, corrosion, evidence of overheating, security of attachments and connections. • If protective covers are required to be removed: check for cleanliness, scoring, pitting, brushes free in holders, not excessively worn and correct bedding. Adequate spring tension, overheating and fluid ingress. Date: 23-Jul-2008
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Relays, Solenoids and Contactors Inspect for: • Cleanliness, obvious damage, corrosion, evidence of overheating, security of attachments and connections. • If protective covers are required to be removed: check for cleanliness, pitting or burning of contactors, evidence of overheating and security of contacts exposed. Electrical looms For the purpose of electrical inspections, it is understood that the stripping of looms is not normally contemplated, though in particular instances it may be required and will be called for at the discretion of the supervisor. Check for: • The condition of external cables within a loom or duct will be taken to indicate the condition of inner cables. • The condition of cables entering and leaving a conduit will be taken to indicate the condition of the cables within the conduit, unless otherwise suspect. Special precautionary checks All flight, engine, fuel and landing gear control systems: • Whenever inspections are made or work is undertaken on any part of above systems, detailed investigation must be made after completion to verify that distortion, tools, rags or any other loose articles or foreign objects cannot impede free movement and safe operation of the system(s). • Fuel systems: If, as a result of the application of this Maintenance Schedule, any part of the fuel system is dismantled, adjusted, repaired or renewed, affected parts of the system shall be checked for free movement and correct operation after completion of the work. Panel opening charts • Panel opening charts provide panel identification. • For the purpose of physical inspection, panel removal requirements shall not limit the degree of inspection required. Removal of other panels shall be at the discretion of inspection personnel.
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2.11 Task Codes E1 EXAMINATION 1 GENERAL VISUAL examination of the exposed structure or systems accomplished from the ground or from inside the control cabin, passenger cabin or cargo compartments. This examination does not require any access means or manual action to be performed except landing gear door opening and flap deflection, if required. E2 EXAMINATION 2 VISUAL examination using access means: it may require, for example, the use of stands, docks, "snorkel" crane, and if necessary, opening of specific panels. A mirror and/or suitable light may be necessary to ensure visual access to all surfaces. For cables, check for broken wire and corrosion. E3 EXAMINATION 3 THOROUGH/DETAILED VISUAL examination which may necessitate the use of access means, access door opening, and removal of fairings, linings, etc. and any other action to be performed in order to clear the inspection area. Visual thorough/detailed examination is including all usual normal work as required to check for proper attachment, play, loosening, interference, etc. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. E4 EXAMINATION 4 SPECIAL DETAILED examination using the following techniques: • Ultrasonic • Radiographic • Low Frequency Eddy Current • High Frequency Eddy Current • Dye penetrant • Resonance (by tapping). This method, used for detecting any panel bond separation, consists in slightly tapping the surface of bonded sheet metal and honeycomb panels, at spots approximately 10 cm apart. • Magnifying glass These various inspection methods are defined in specific documents. The use of any of these methods has to be clearly stated. S SERVICING This task can involve one of the following actions: a) Regular lubricant using grease, gun-squirt-can, brush or spray Date: 23-Jul-2008
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b) Fluid level check with refilling to proper level as required c) Cleaning d) Periodical software update (e.g. FMS data-base). F1 OPERATIONAL CHECK (OP/C) A qualitative check to determine that a system or component is operating in a normal or intended manner. Does not require quantitative tolerances. F2 FUNCTIONAL CHECK (F/C) A quantitative check to determine if one or more functions of a system or component perform within specified limits. M1 MEASUREMENT WITHOUT RECORDING Is a measurement of play, travel, torque, pressure level, cable tension, etc... to ensure that an item is within tolerance. M2 MEASUREMENT WITH RECORDING As above but actual figures shall be noted and entered into the record book or cards. W1 EXAMINATION OF WIRING AND COAXIAL-CABLES Check external condition or wire bundles, coaxial cables and attachments for physical condition, cleanliness, proper appearance (aging, weathering, overheating, chafing, distortion possible detrimental to characteristics), without systemically opening out harness or bundles. W2 THOROUGH EXAMINATION OF WIRING AND COAXIAL CABLES In addition to the above outlined inspection open all access doors and remove all readily detachable panels, shields or system units concealing wire bundles and coaxial cables. Check identification sleeves or tags, coatings, padding and protective devices. Wire bundles and coaxial cables concealed by floor or lining panels, unit of structural members which cannot be removed without extensive work, are checked by sampling inspections, whose extent and intervals are specified in each case. I1 EXAMINATION OF INTERCONNECTIONS (connectors, splices, pressurized bulkhead connectors terminal strips, clamps) Externally check that connectors are clean, corrosion free, and properly tightened, safetied and locked. Checking the connection tightness does not necessarily imply the use of a tool. The check may be visual - when, for instance, index mark dots where painted on the screw head and the component body or on the bolt head and its mating nut - or manual by pressing with the finger so as to detect any looseness of terminal lugs. I2 THOROUGH EXAMINATION OF CONNECTORS Date: 23-Jul-2008
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In addition to the above outlined inspection disconnect connectors and pressurized bulkhead connectors and check physical and electrical condition, inspect for oxidation traces: replace seals, gaskets, grommets, ferrules or other parts if necessary. Check tightness of connections on all electrical system accessories, bonding and grounding jumpers, bus bars, terminal strips, check all connectors not provided with safety wires. R1 EXAMINATION OF RACKS, SUPPORTING FRAMES AND SHELVES Without removing any system units, externally check that wire bundles, connectors, extractors, ducts, attachments, shock mounts, bonding jumpers are in proper physical condition, properly tightened, safetied and locked and their aspect is satisfactory. Externally check condition of all parts exposed when- ever system units are removed for testing or replacement. R2 THOROUGH EXAMINATION OF RACKS; SUPPORTING FRAMES AND SHELVES In addition to the above outlined inspection remove all system units. Clean and blow out dust from panels, shelves, slide channels, air valve ports, seals and ventilation ducts. Safety as applicable system unit attachment upon reinstallation. Check placards and nameplates. P1 EXAMINATION OF PANELS, JUNCTION BOXES, ACCESSORIES Without removal, externally check that panels, junction boxes, accessories and system units are in physical condition, clean, properly attached and locked and their aspect is satisfactory. P2 THOROUGH EXAMINATION OF PANELS, JUNCTION BOXES AND ACCESSORIES Open panels and protective boxes and externally check physical condition cleanliness, appearance, tightness, locking and safetying of the above components. Blow out dust and clean if necessary. Check placards and nameplates. Check physical condition of fuse-holders and inspect for evidence of overheating. Check that fuses (installed and spares) are in proper condition and conformance with nominal value.
2.12 (Not used) 2.13 Parking, Storage and Return to Service 2.13.1 Parking For normal parking procedures: see AMM 10-11-01.
2.13.2 Storage For prolonged parking (storage) procedures: see AMM 10-12-02.
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2.13.3 Return to Service For the return to service procedure: see AMM 10-12-02.
2.13.4 Special Regulations for Parked or Stored Aircraft An aircraft which has been taken out of operation and is parked or stored for more than 24 hours has to be maintained according the following rules: • All maintenance requirements and checks defined in this Maintenance Schedule, which become due during the parking/storage period, may be postponed until the end of the parking period (unless required by AMM 10-00). • All deferred complaints and open items, which are scheduled for rectification during the parking period, may be postponed until the end of the parking period (unless required by AMM 10-00). • All changes of components, which become due during the parking period according the CMS, may be postponed until the end of the parking period (unless required by AMM 10-00). • ALL EO´s, SB´s, SL´s, SIL´s, AD´s, CDN´s and national Airworthiness Requirements, which become due during the parking period, may be postponed until the end of the parking period, provided there is no specific requirement for the parking/storage period. • Provisioning related component, APU or engine removals during the parking/storage period are possible in general. The reinstallation of a component, APU or engine can be postponed until the end of the parking/storage period, but has to be performed in accordance with all relevant procedures. All outstanding work and component replacements must be completed before return of the aircraft back into service. For appropriate handling of a removed component, APU or engine before installation in another aircraft, refer to the relevant procedures. • For maintenance requirements and maintenance checks which are limited in Maintenance Schedule or in the CMS with calendar time, an interval credit may be used in principle. The amount of the interval credit depends on the duration and the condition of the parking/storage and is subject to LBA-approval. • Before the aircraft is returned to service, all open defects need to be rectified, and all relevant maintenance program tasks required to return the aircraft to airworthiness standards need to be complied with.
2.14 Authority Requirements 2.14.1 Approval of Maintenance Schedule by Authority All changes to the Maintenance Schedule revising the task interval and/or the task code of an item require authority approval. Tasks from the MRB Report can be developed or escalated in compliance with para. 2.14.2 and require authority approval. The responsible national authority for approvals is the Luftfahrt Bundesamt (LBA). Date: 23-Jul-2008
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2.14.2 Interval Escalation Procedure Generally, intervals defined in this Maintenance Schedule may be increased based on engineering judgment under consideration of operational, service or industry experience/standards. A minimum of 90% usage of the valid interval is required for escalation. MPD or MRB originated task intervals shall not be escalated more than 25% of the valid, presently applied interval. The following procedures for task escalation have to be followed : • For Line Maintenance tasks : - Qualitative assessment of findings from the existing interval. The number of tasks accomplished which will be investigated is the percentage of the intended escalation step applied to the number of aircraft in the fleet. The resulting figure is used for each task. - Request for approval by the responsible authority for use of the new interval on a trial basis. - Detailed assessment of findings from tasks accomplished under the new interval. The number of tasks which will be investigated is the percentage of the intended escalation step applied to the number of aircraft in the fleet. The resulting figure is used for each task. - Presentation of the assessment results to the responsible authority and request for final approval of the new interval. • For Base Maintenance tasks : - Detailed assessment of findings from the existing interval. - The number of tasks that will be investigated depends on fleet size and is subject to approval by the responsible authority. - Request for approval by the responsible authority for use of the new interval on a "trial" base. - Detailed assessment of findings from tasks accomplished under the new interval. - The number of tasks under trial that will be investigated depends on fleet size and is subject to approval by the responsible authority. - Presentation of the assessment results to the responsible authority and request for final approval of the new interval.
2.14.3 Permitted Variations to Task Frequencies Corrosion Prevention and Control Program ( CPCP): To accommodate unanticipated scheduling requirements, Repeat Intervals of CPCP Items may, occasionally, be increased by up to ten percent (10%), with a maximum of 6 months ( requires regulatory notification and regulatory approval in writing ).
Date: 23-Jul-2008
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2.15 (Not used) 2.16 (Not used) 2.17 (Not used) 2.18 Maintenance Requirements for Specific Aircraft Operations 2.18.1 MNPS Maintenance Procedures In accordance with EU OPS 1.870, no scheduled maintenance tasks nor specific recommendations on MNPS involved systems/tasks are needed on B737 aircraft to hold their MNPS capability.
2.18.2 RVSM (Reduced Vertical Separation Minimum) Capability The goal of RVSM is to reduce the vertical separation above flight level 290 from the current 2000- ft minimum to 1000-ft minimum. This will allow the aircraft to safely fly more optimum profiles, gain fuel savings and increase airspace capacity. This requires that the mean altimetry system error does not exceed specified values. In accordance with Boeing Service Letter 737-SL-02-017-G all required scheduled maintenance tasks are defined in the Boeing B737-6/7/8/9 MPD.
2.18.3 CAT II / CAT III Operation Specific Maintenance Tasks for Automatic Approach and Landing CAT II / CAT III Operation should be reflected in the Maintenance Schedule if applicable. On all Boeing B737-700 aircraft CAT II / CAT III are inherent functions of the basic aircraft design standard. Therefore related tasks are covered by the respective Maintenance Program without special recommendation for scheduled Maintenance Tasks. Consequently all Boeing B737-700 do not require scheduled periodic tests / functional checks / calibrations to assure CAT II / CAT III certification. However, HHI will comply with supplemental national requirements if applicable.
Date: 23-Jul-2008
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3
FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS
3.1
Revision Column
737-6
A letter code gives the status of the item at the date of publication shown in the page header: "N" : New "R" : Revised "D" : Deleted Blank : No change
3.2
ITEM Column
It lists in numerical sequence for each separate ATA 100 chapter and subchapter, all the items leading to a periodic maintenance or overhaul task. The item number is split into three figures groups: • group 1 : 6 digits giving the ATA Spec. 100 reference, • group 2 : 3 digits giving a sequence number (all sequence numbers from 001 to 999 can be used) • group 3 : 2 digits giving a "sub-sequence" number allowing grouping of items of same nature, but applying with different parameters. If only one item is used, this sequence number is "00". In principle each item corresponds to one task (which may cover several "tasks codes") and one interval (and possibly one threshold). If several intervals do appear, they are always in different units (FLH, CYC,...) and in that case the meaning of such a situation is: to apply the interval "what ever comes first".
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3.3
737-6
DESCRIPTION Column
It gives a brief but accurate description of the task to be accomplished. In addition in that column may appear some notes when necessary. These notes are of 3 categories: Note: General notes affecting some of the parameters produced in the layout (INTERVAL, TASK CODE, etc.). In any case a highlight "NOTE" appear, with, in front of it, a note mark identifying the affected parameters. These possible note marks are: • Z : zone • E : effectivity • T : threshold • I : interval • J : task code • R : reference • M : miscellaneous Access Note: Specific note when special access (other than those mentioned in ACCESS column) has to be made to perform the task (i.e.: landing gear doors closed, flaps extended ...). In that case a highlight "ACCESS" appears. Condition Note: Specific note when the task to be performed depends on the embodiment of such modifications which are then indicated in that note. In that case a highlight "CONDITION" appears.
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3.4
737-6
ZONE Column
Shows the zones concerned with the task, using the Boeing zone system for the B737-700 aircraft.
3.5
ACCESS Column
It lists all the access panels, corresponding to each zone of the ZONE column, to be opened to perform the task.
3.6
STRUCTURE Column
If applicable, shows the sampling fraction corresponding to that portion of the operators fleet which must be inspected (see Sampling Inspections for details).
Date: 23-Jul-2008
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3.7
737-6
REFERENCES Column
It shows each document or manual necessary to be consulted to produce a clear understanding of the requested task, as well as references covering the origin of the item. For items which are affected by Directive from Airworthiness Authorities, the letter's reference will be mentioned in this column, and the maximum allowable limit shown in a NOTE preceded by the note mark "I" (for interval). Such references are indicated by means of their alphabetical code and their number. Examples of references types: Indicates an Airworthiness Requirement • AAR (FAA) Airworthiness Directive • AD Aircraft Maintenance Manual • AMM Aircraft Maintenance Task Oriented Support System • AMTOSS Corrosion Prevention and Control Program • CPCP Maintenance Planning Document • MPD Task of the Maintenance Review Board Report • MRB MS item number related to this task • MS Non-Destructive Testing Manual • NTM Service Bulletin • SB Structural Significant Item of the MRB • SSI Service Information. Indicates if source of task is experience of Lufthansa Technik (LHT) or a customer request. • SI Standard Practices Manual • SPM
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3.8
737-6
THRESHOLD/INTERVAL Column
It shows the maximum allowed interval for each task to be performed. This interval is preceded by the letter "I:". Should the task become effective only after expiration of a certain limit, this limit appears (as a THRESHOLD) preceded by the letter "T:". The units in which intervals/ thresholds are expressed are as follows: • • • • • •
FLH CYC MTH YRS T Z
3.9
flight hours flight cycles months years trip check (preflight) daily additional items
TASK Column
The task code indicated in this column gives a more extensive definition of the task than that described in the column "DESCRIPTION". In the coding layout it has been considered that: − the access and degree of disassembly (if required) should be stated in the columns "ACCESS" and "DESCRIPTION", the object to be examined must be cleaned if the normal degree of operation contamination is exceeded and a perfect check of performance is not ensured.
3.10 EFFECTIVITY Column It describes the Aircraft model, or Engine type, or specific individual a/c to which the concerned task applies. "ALL" appears when the task applies to all aircraft
3.11 BY Column The indication FC (flight crew) or SM (station mechanic) appears each time the specific task is of "line maintenance" nature, neither "T" or "Z" checks.
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3.12 REP Column Information for Lufthansa Technik internal purposes only.
3.13 LEV Column It shows, for each time, the revision level of this item (00 for the first issue, 01 to 99 for revisions).
3.14 ITEM REVISION DATE Column Shows, for each item, the latest revision date. This date is always lower or equal to the date of revision of the whole Maintenance
Date: 23-Jul-2008
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4
WEIGHING
4.1
Weighing Periods
737-6
A. Each aircraft will be weighed and the C of G location established prior to being placed into service. New production aircraft delivered to operators and weighed by the manufacturer are eligible to be placed into operations without re weighing if only minor change and equipment installation are accomplished by the operator. B. Each aircraft will be weighed at overhaul. C. Each aircraft will be weighed after major repair or after major alteration unless reliable data allowing analytical calculation of weight and balance change are available. D. Every 4 years each aircraft within a fleet have to be weighed to allow correct assessment of the weight and C.G. position variation. E. The aircraft weighing schedule is published in Chapter 5.
4.2
Weighing Procedure
The weighing procedure will be carried out according to AMM 08-12-00.
4.3
Weighing Results
Before each weighing, the responsible weight and balance engineer or a qualified delegate, who must be familiar with the equipment of the aircraft will check the condition of the aircraft at the time of weighing against a standard equipment list. This standard equipment list must represent the actual condition of the aircraft in service. The responsible weight and balance engineer or qualified delegate carries out the weighing and reports the weighing results by documents as follows : One weighing record and a completed standard equipment list acc. to the actual configuration of the aircraft at time of weighing.
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5
737-6
AIRCRAFT
Aircraft Basic Data Table REGIST NEW D-AHIA
CUST ID HHI
D-AHIB D-AHIC
SERIES B737-73S
CON FIG PAX
ENGINE TYPE CFM56-7B22
APU TYPE 131-9(B)
HHI
B737-73S
PAX
CFM56-7B22
HHI
B737-7BK
PAX
CFM56-7B22
D-AHID
HHI
B737-73S
PAX
D-AHIE
HHI
B737-73S
D-AHIF
HHI
B737-73S
IPC EFF
LINE NO 229
PROD. NO YA 577
SERIAL NO 29082
131-9(B)
392
YA 578
131-9(B)
812
YB 276
CFM56-7B22
131-9(B)
211
PAX
CFM56-7B24
131-9(B)
PAX
CFM56-7B24
131-9(B)
AIR FRAME
DATE OF FIRST FLIGHT 05-mar-1999
REGIST OLD D-ASKH
REMARKS
29083
01-oct-1999
D-AWOH
30617
23-mar-2001
N/A
YA575
29080
04-feb-1999
EI-CRQ
Phased out
215
YA576
29081
01-mar-1999
TC-SUF
Phased out
194
YA574
29079
17-jan-1999
TC-SUE
Phased out
Phased out
Aircraft Additional Data Table
REGIST NEW D-AHIA
NEXT WEIGHING 16-Feb-2011
SAMPLING A/C NO
ETOPS A/C NO
REMARKS Last weighing date 16-Feb-2007
D-AHIB
07-mar-2011
NO
NO
Last weighing date 07-Mar-2007
D-AHIC
22-feb-2009
NO
NO
Last weighing date 22-feb-2005
D-AHID
10-Mar-2011
NO
NO
Last weighing date 10-Mar-2007
D-AHIE
23-Dec-2010
NO
NO
Last weighing date 23-Dec -2006
D-AHIF
26-Mar-2011
NO
NO
Last weighing date 26-Mar-2007
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PARA
NATIONAL SPECIAL REQUIREMENTS
Comment
EASA PART M.A.710 EASA PART M.A.901 NfL II-23/03
CONTINUING AIRWORTHINESS REVIEW
CAMOE 6.2 – 6.7
LEAK TEST OF STBY ALTITUDE AND STBY AIRSPEED SYSTEM
acc. MS- and CMS -Items ATA 34
SEAT BELTS
see MS-Item 250000 01000
737-6
NfL II-56/01 NfL II-83/99 NfL II-96/79 NfL II-92/99 NfL II-56/01 NfL II-56/01 EASA-OPS 1.700-1.725
PORTABLE FIRE EXTINGUISHER
see MS-Item 260000 01000 and 262500 01000
FLEXIBLE HOSES 2.3.7 FLIGHT DATA RECORDER AND COCKPIT VOICE RECORDER
NfL II-56/01
2.3.6
EASA-OPS 1.870
2.3.9 MNPS (Minimum Navigation Performance Specification Airspace) Maintenance Procedures 2.3.10 CAT II/III Maintenance Procedure
Vendor Rec. see MS 237100 73000 see MS 313100 97000 Functional Check of “FLIGHT DATA RECORDER” and VOICE RECORDER SYSTEM” must be performed according to NfL II-56/01 every 12 MTH (with exception of 24 MTHS for SSFDR) STANDBY COMPASS COMPENSATION must be performed according to NfL II-56/01every 12 MTH. see MS-Item 342400 02000 N/A
EASA-OPS 1.460 OR 3.460 EASA-OPS 1.872
Date: 23-Jul-2008
COMPENSATION OF MAGNETIC STBY COMPASS
2.3.11 RVSM Maintenance Procedure
CAMOE 2.26 See MS Items 05230 00000, 341102 20000 and 530900 12000
NATIONAL AND INTERNATIONAL SPECIAL REQUIREMENTS
Page: 1 of 1
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones
Description / Boundaries
100
LOWER HALF OF FUSELAGE
200
UPPER HALF OF FUSELAGE
300
EMPENNAGE AND BODY SECTION 48
400
POWER PLANTS AND NACELLE STRUTS
500
LEFT WING
600
RIGHT WING
700
LANDING GEAR AND LANDING GEAR DOORS
800
PASSENGER AND CARGO DOORS
800*
ONLY ON 737-800/900
800**
737-700 ONLY
MAJOR AIRCRAFT ZONES
Date: 23-jul-08
AIRCRAFT ZONES
Page: 1 Z
HHI
MAINTENANCE SCHEDULE
737-700
MAJOR ZONE 100 - LOWER HALF OF FUSELAGE
Date: 23-jul-08
AIRCRAFT ZONES
Page: 2 Z
MAINTENANCE SCHEDULE
HHI Major Zones
Description / Boundaries
Major Zones
110
STA 130 TO STA 360
111
RADOM
141/142
AFT CARGO COMPARTMENT
112
AREA FWD OF NOSE WHEEL WELL
143/144
AREA BELOW AFT CARGO COMPARTMENT
113/114
AREA ABOVE NOSE WHEEL WELL AREA OUTBD OF NOSE WHEEL WELL
145/146
AFT CARGO COMPARTMENT EQUIPMENT BAY
115/116
NOSE WHEEL WELL
117/118
ELECTRICAL AND ELECTRONICS COMPARTMENT
120
140
Description / Boundaries
Description / Boundaries
Major Zones
Description / Boundaries
BODY STA 727 TO STA 1016
149
KEEL BEAM (PART) STA 727 TO STA 743.95
190
FAIRING BODY STA 500B+15 TO STA 727D+8
191
LOWER WING, WING TO BODY FAIRING FWD OF WING BOX
BODY STA 360 TO STA 540
121/122
FWD CARGO COMPARTMENT
123/124
AREA BELOW FWD CARGO COMPARTMENT
192
LOWER WING, WING TO BODY FAIRING UNDER WING BOX
125/126
AIR CONDITIONING DISTRIBUTION BAY
193
LOWER WING, WING TO BODY FAIRING WHEEL WELL
129
KEEL BEAM (PART) STA 501.70 TO STA 540
194
LOWER WING, WING TO BODY FAIRING AFT OF WHEEL WELL
195 130
BODY STA 540 TO STA 727
ABOVE RIGHT WING, WING TO BODY FAIRING
196
ABOVE LEFT WING, WING TO BODY FAIRING
131/132
CENTER SECTION WING BOX (STA540 TO STA 663.75)
133/134
MAIN LANDING GEAR WELL (STA 633.75 TO STA 727)
135/136
AREA ABOVE WING CENTER SECTION (STA 540 TO STA 663.75)
137/138
AREA ABOVE MAIN LANDING GEAR WELL (STA 633.75 TO STA 727)
139
Major Zones
737-700
KEEL BEAM (PART) STA 540 TO STA 727
Date: 23-jul-08
AIRCRAFT ZONES
Page: 3 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones 210 211/212 220 221/222
230 231/232 240 241/242
Description / Boundaries FLIGHT COMPARTMENT BODY STA 178 TO STA 259.2 FLIGHT COMPARTMENT PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360 PASSENGER COMPARTMENT - AFT OF CONTROL COMPARTMENT TO FWD ENTRY DOOR PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75 FWD PASSENGER COMPARTMENT FWD ENTRY DOOR TO STA 663.75 PASSENGER COMPARTMENT AFT PASSENGER COMPARTMENT STA 633.75 TO AFT PRESSURE BULKHEAD
MAJOR ZONE 200 - UPPER HALF OF FUSELAGE
Date: 23-jul-08
AIRCRAFT ZONES
Page: 4 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones 310
Description / Boundaries FUSELAGE STA 1016 TO STA 1217
311/312
AREA AFT OF PRESSURE BULKHEAD
313/314
STABILIZER TORSION BOX COMPARTMENT
315/316
APU COMPARTMENT
317/318
TAIL CONE
320
FIN AND RUDDER
321
DORSAL FIN
322
FIN REMOVABLE LEADING EDGE
323
FIN FRONT SPAR TO REAR SPAR
324
FIN REAR SPAR TO TRAILING EDGE
325
RUDDER
326
FIN TIP
MAJOR ZONE 300 - FUSELAGE 310 - FIN AND RUDDER 320
Date: 23-jul-08
AIRCRAFT ZONES
Page: 5 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones
Description / Boundaries
330
HORIZONTAL STABILIZER AND ELEVATOR LEFT
331
REMOVABLE LEADING EDGE
332
FRONT SPAR TO REAR SPAR, STAB. STA 57.93 TO STAB. BL 249.81
333
REAR SPAR TO TRAILING EDGE
334
ELEVATOR
335
TIP
340
HORIZONTAL STABILIZER AND ELEVATOR RIGHT
341
REMOVABLE LEADING EDGE
342
FRONT SPAR TO REAR SPAR, STAB. STA 57.93 TO STAB. BL 249.81
343
REAR SPAR TO TRAILING EDGE
344
ELEVATOR
345
TIP
MAJOR ZONE 300 - HORIZONTAL STABILIZER
Date: 23-jul-08
AIRCRAFT ZONES
Page: 6 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones
Description / Boundaries
410
NO.1 POWER PLANT
411
ENGINE
412
NOSE INLET COWL
413
FAN COWL - LEFT
414
FAN COWL - RIGHT
415
THRUST REVERSER - LEFT
416
THRUST REVERSER - RIGHT
417
PRIMARY EXHAUST NOZZLE AND PLUG
420
NO.2 POWER PLANT
421
ENGINE
422
NOSE INLET COWL
423
FAN COWL - LEFT
424
FAN COWL - RIGHT
425
THRUST REVERSER - LEFT
426
THRUST REVERSER - RIGHT
427
PRIMARY EXHAUST NOZZLE AND PLUG
430/440
LEFT/RIGHT NACELLE STRUT
431/441
FORWDRD STRUT FAIRING
432/442
FAN COWL SUPPORT BEAM
433/443
STRUT TORQUE BOX
434/444
AFT STRUT FAIRING
MAJOR ZONE 400 - CFM56-7 POWERPLANT AND NACELLE
Date: 23-jul-08
AIRCRAFT ZONES
Page: 7 Z
HHI
MAINTENANCE SCHEDULE
737-700
MAJOR ZONE 500 - LEFT WING (SHOWN), MAJOR ZONE 600 - RIGHT WING (OPPOSITE)
Date: 23-jul-08
AIRCRAFT ZONES
Page: 8 Z
MAINTENANCE SCHEDULE
HHI Major Zones 510/610
Description / Boundaries WING LEADING EDGE - FORWARD OF FRONT SPAR, INBOARD OF NACELLE STRUT, INCLUDING NACELLE GAB COVER AREA
511/611
LEADING EDGE TO FRONT SPAR
512/612
KRUEGER FLAP NO. 2 AND NO. 3
513/613 520/620
Major Zones
Description / Boundaries
Major Zones
Description / Boundaries
540/640
WING TRAILING EDGE FLAP TRACK FAIRINGS
570/670
WING TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP, INBOARD OF WING TIP, WING BL 658. 17
541/641
FAIRING FLAP SUPPORT NO. 4 AND NO. 5
571/671
FIXED TRAILING EDGE
572/672
AILERON
542/642
FAIRING FLAP SUPPORT NO. 3 AND NO. 6
KRUEGER FLAP NO. 1 AND NO. 4
543/643
FAIRING FLAP SUPPORT NO. 2 AND NO. 7
WING LEADING EDGE - FORWARD OF FRONT SPAR, OUTBOARD OF NACELLE STRUT
544/644
FAIRING FLAP SUPPORT NO. 1 AND NO. 8
521/621
LEADING EDGE TO FRONT SPAR
550/560
522/622
SLATS NO. 4 AND NO. 5
WING TRAILING EDGE - AFT OF REAR SPAR, INBOARD OF OUTBOARD TRAILING EDGE FLAP
523/623
SLATS NO. 3 AND NO. 6
551/651
REAR SPAR TO LANDING GEAR SUPPORT BEAM
524/624
SLATS NO. 2 AND NO. 7
552/652
SPOILER NO. 6 AND NO. 7
525/625
SLATS NO. 1 AND NO. 8
553/653
INBOARD FLAP
526/626
WING TIP
560/660
530/630
WING INSPAR AREA (FUEL TANKS) INBOARD OF WING RIB 22, WING STA 643.50
WING TRAILING EDGE - AFT OF REAR SPAR, OUTBOARD OF INBOARD FLAP, INBOARD OF FIXED TRAILING EDGE
531/631
CENTER FUEL TANK RIB 1 TO RIB 5
561/661
532/632
MAIN TANK, RIB 5 TO RIB 25, WING STA 204.25 TO WING STA 643.50
REAR SPAR TO TRAILING EDGE, OUTBOARD OF INBOARD FLAP, INBOARD OF FIXED TRAILING EDGE
562/662
SPOILER NO. 5 AND NO. 8
533/633
SURGE TANK, RIB 22 TO RIB 25, WING STA 616.75 TO WING BL 643. 50
563/663
SPOILER NO. 4 AND NO. 9
564/664
SPOILER NO. 3 AND NO. 10
534/634
DRY BAY
565/665
SPOILER NO. 2 AND NO. 11
566/666
SPOILER NO. 1 AND NO. 12
567/667
OUTBOARD FLAP
Date: 23-jul-08
AIRCRAFT ZONES
737-700 Major Zones
Description / Boundaries
Page: 9 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones
Description / Boundaries
710
NOSE LANDING GEAR AND L. G. DOORS
711
NOSE LANDING GEAR DOOR, LEFT
712
NOSE LANDING GEAR DOOR, RIGHT
713
NOSE LANDING GEAR
730
LEFT MAIN LANDING GEAR AND L. G. DOORS
731
OUTBOARD DOOR, LEFT
732
CENTER DOOR, LEFT
733
INBOARD DOOR, LEFT
734
LEFT MAIN LANDING GEAR
740
RIGHT MAIN LANDING GEAR AND L. G. DOORS
741
OUTBOARD DOOR, RIGHT
742
CENTER DOOR, RIGHT
743
INBOARD DOOR, RIGHT
744
RIGHT MAIN LANDING GEAR
MAJOR ZONE 700 - LANDING GEAR AND LANDING GEAR DOORS
Date: 23-jul-08
AIRCRAFT ZONES
Page: 10 Z
HHI
MAINTENANCE SCHEDULE
737-700 Major Zones
Description / Boundaries
820
LOWER HALF OF FUSELAGE RIGHT SIDE
821
FORWARD CARGO DOOR
822
AFT CARGO DOOR
830
UPPER HALF OF FUSELAGE LEFT SIDE
831
FORWARD ENTRY DOOR
832
AUTOMATIC OVERWING EXIT (-800/900)
833
AUTOMATIC OVERWING EXIT
834
AFT ENTRY DOOR
835
MAIN DECK CARGO DOOR (-700C ONLY)
840
UPPER HALF OF FUSELAGE RIGHT SIDE
841
FORWARD ENTRY DOOR
842
AUTOMATIC OVERWING EXIT (-800/900)
843
AUTOMATIC OVERWING EXIT
844
AFT ENTRY DOOR
MAJOR ZONE 800 - PASSENGER AND CARGO DOORS
Date: 23-jul-08
AIRCRAFT ZONES
Page: 11 Y
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 05 - 10
05100- 00000
05100- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ZONAL ZONE 100 FUSELAGE -LOWER HALFVISUALLY INSPECT LOWER HALF OF FUSELAGE E X T E R N A L
100
GENERAL VISUAL INSPECTION OF THE LOWER FUSELAGE. THE NLG WHEEL WELL AND MLG WHEEL WELL ARE ALSO INCLUDED. E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS
110 120 130 140
emp
empty
SERVICE EXPERIENCE emp emp emp emp
ITEMS
MPD MRB
I: 1 T
E1 HHI 737-700
I: 560 CYC I: 90 DAY
E2 HHI 737-700
FC SM
1 03-jun-04
53-800-00 MSI 53-800-00
ATA: 05 - 10
5 22-mar-07
Page 1 of 1
HHI R E V
ITEM 05 - 11 05110- 00000
05110- 01000
05110- 02000
R
737-6
MAINTENANCE SCHEDULE
05111- 00000
R
05112- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
BODY STA 130 TO STA 360 GENERAL VISUAL INSPECTION OF THE AREA ABOVE AND OUTBOARD OF 113 THE NOSE WHEEL WELL. emp I N T E R N A L emp 114 emp emp
113AC 113AW 113BW 114AC 114AW 114BW
MPD MRB
GENERAL VISUAL INSPECTION OF THE ELECTRICAL AND ELECTRONICS 117 COMPARTMENT. emp I N T E R N A L 118 ACCESS FORWARD AIRSTAIR DRIP PAN ACCESS PANEL MUST BE REMOVED IF AIRSTAIR INSTALLED. ACCESS PANEL 117BL ONLY AT A/C WITH AIRSTAIR INSTALLED OR PROVISIONS.
117A 117BL emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE ELECTRICAL AND ELECTRONICS 117 COMPARTMENT ACCESS DOOR. 118 I N T E R N A L
117AW emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE RADOME I N T E R N A L NOTE( Z ) ZONE 111 INTERNAL INSPECTION INCLUDES THE BS 178 STRUCTURE AND INSTALLATIONS AND THE INTERNAL SIDE OF THE RADOME.
111
111
GENERAL VISUAL INSPECTION OF THE AREA FORWARD OF THE NOSE 112 WHEEL WELL - SECTION 41, STA 178 TO 224.8. I N T E R N A L
112A
ITEMS
MPD MRB
MPD MRB
53-806-00 MSI 53-806-00 I: 24 MTH I: 5500 CYC
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 24 MTH I: 5500 CYC
E2 HHI 737-700
3 23-jul-08
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
53-808-00 MSI 53-808-00
53-810-00 MSI 53-810-00
53-802-00 MSI 53-802-00
53-804-00 MSI 53-804-00
ATA: 05 - 11
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 12
05120- 00000
05120- 01000
05120- 02000
05120- 03000
05120- 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
BODY STA 360 TO STA 540 GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD. 122 I N T E R N A L ACCESS NO CARGO LINERS REMOVED.
821 emp
GENERAL VISUAL INSPECTION OF THE AIR CONDITIONING DISTRIBUTION 125 BAY - SECTION 43, FWD CARGO COMPARTMENT BULKHEAD TO STA 540. 126 I N T E R N A L ACCESS FORWARD CARGO COMPARTMENT AFT BULKHEAD CENTER PANEL REMOVAL REQUIRED.
821 emp
GENERAL VISUAL INSPECTION OF THE AREA ABOVE THE FORWARD CARGO COMPARTMENT - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD I N T E R N A L ACCESS CEILING PANELS REMOVAL REQUIRED
821 emp
121 122
GENERAL VISUAL INSPECTION OF THE AREA BELOW THE FORWARD 123 CARGO COMPARTMENT - SECTION 43, STA 396 TO FWD CARGO 124 COMPARTMENT BULKHEAD I N T E R N A L ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.
821 emp
GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 - SECTION 43, STA 396 TO FWD CARGO COMPARTMENT AFT BULKHEAD 122 I N T E R N A L ACCESS SIDEWALL PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.
821 emp
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-812-00 MSI 53-812-00 I: 560 CYC I: 90 DAY
E2 HHI 737-700
6 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
5 18-mar-05
I: 13000 CYC I: 60 MTH
E2 HHI 737-700
3 18-mar-05
I: 13000 CYC I: 60 MTH
E2 HHI 737-700
3 18-mar-05
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
2 03-jun-04
53-822-00 MSI 53-822-00
53-814-00 MSI 53-814-00
53-820-00 MSI 53-820-00
53-816-00 MSI 53-816-00
ATA: 05 - 12
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05122- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR 122 SURROUND STRUCTURE FITTINGS AND STOPS - SECTION 43, STA 460. E X T E R N A L
STRUCTURE
821
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
53-818-00 MSI 53-818-00 I: 1500 CYC I: 180 DAY
ITEMS
TSK
ATA: 05 - 12
E2 HHI 737-700
5 22-mar-07
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 13
05130- 00000
05130- 01000
05130- 02000
05139- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
BODY STA 540 TO STA 727 GENERAL VISUAL INSPECTION OF THE PRESSURE DECK ABOVE THE 137 MAIN LANDING GEAR WHEEL WELL - SECTION 44, STA 663.75 TO STA 727. 138 I N T E R N A L ACCESS FLOOR PANELS REMOVAL REQUIRED. INSULATION AS REQUIRED.
emp emp
GENERAL VISUAL INSPECTION OF THE CENTER SECTION WING BOX SECTION 44, STA 540 TO STA 663.75. I N T E R N A L
131 132
131AB 192CL
GENERAL VISUAL INSPECTION OF THE AREA ABOVE THE CENTER SECTION WING BOX - SECTION 44, STA 540 TO 663.75. I N T E R N A L ACCESS FLOOR PANELS REMOVAL REQUIRED. INSULATION AS REQUIRED.
135 136
GENERAL VISUAL INSPECTION OF THE KEEL BEAM (PART) - SECTION 44, 139 STA 540 TO 727. emp I N T E R N A L
emp emp
192CL 192CR
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-826-00 MSI 53-826-00 I: 13000 CYC I: 60 MTH
E2 HHI 737-700
2 18-mar-05
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
2 18-mar-05
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
2 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
57-800-00 MSI 57-800-00
53-824-01 MSI 53-824-01
53-828-00 MSI 53-828-00
ATA: 05 - 13
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 14
05141- 00000
05141- 01000
05141- 02000
05141- 03000
05142- 00000
05143- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
BODY STA 727 TO 1016 GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT SECTION 46 AND 47 (PART), STA 727 TO STA 947.5. ACCESS NO CARGO LINERS REMOVED.
141 142
GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT VACUUM WASTE COMPARTMENT I N T E R N A L ACCESS VACUUM WASTE COMPARTMENT PANELS REMOVAL REQUIRED
141
822 emp
822
GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT - 141 SECTION 46 AND 47 (PART), STA 727 TO STA 947.5 142 I N T E R N A L ACCESS UPPER ANGLED SIDEWALL AND CEILING PANELS REMOVAL REQUIRED
822 emp
GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT SECTION 46 AND 47 (PART), STA 727 TO STA 947.5 I N T E R N A L ACCESS SIDEWALL PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.
822 emp
141 142
GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR SURROUND 142 STRUCTURE FITTINGS AND STOPS -SECTION 46, STA 827. E X T E R N A L
822
GENERAL VISUAL INSPECTION OF THE AREA BELOW THE AFT CARGO 143 COMPARTMENT - SECTION 46 AND 47 (PART), STA 727 TO STA 947.5. 144 I N T E R N A L ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. INSULATION BLANKETS REMOVED OR DISPLACED.
emp 822
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-830-00 MSI 53-830-00 I: 560 CYC I: 90 DAY
E2 HHI 737-700
6 22-mar-07
I: 24 MTH I: 5500 CYC
E2 HHI 737-700
2 03-jun-04
I: 13000 CYC I: 60 MTH
E2 HHI 737-700
2 18-mar-05
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
2 18-mar-05
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
6 22-mar-07
I: 13000 CYC I: 60 MTH
E2 HHI 737-700
2 18-mar-05
53-838-00 MSI 53-838-00
53-832-00 MSI 53-832-00
53-834-00 MSI 53-834-00
53-836-00 MSI 53-836-00
53-840-00 MSI 53-840-00
ATA: 05 - 14
Page 1 of 2
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
05145- 00000
R
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT EQUIPMENT BAY - SECTION 47, STA 947.5 TO STA 1016. I N T E R N A L ACCESS AFT CARGO PANELS AT 947 BULKHEAD REMOVAL REQUIRED
ZONE ACCESS 145 146
STRUCTURE
822 emp
ITEMS
REFERENCES MPD MRB MPD MRB
53-842-00 MSI 53-842-00 53-842-00 MSI 53-842-00
AMM
05-41-01-210
THRESHOLD INTERVAL
I: 5500 CYC I: 24 MTH
ATA: 05 - 14
TSK
EFF
E2 HHI 737-700
R L ITEM BY E E REVISION P V DATE
4 23-jul-08
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 19
05190- 00000
05191- 00000
05192- 00000
05194- 00000
05194- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING TO BODY FAIRINGS GENERAL VISUAL INSPECTION OF THE WING TO BODY FAIRING. 190 E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS
emp
GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING - FORWARD OF WING BOX. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED
191 emp emp emp
191GL 191GR 192CL 192CR
MPD MRB
GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING - UNDER THE WING BOX. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED
192 emp emp emp emp
192BL 192BR 192CL 192CR 192DR
MPD MRB
GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING 194 - AFT OF WHEEL WELL. I N T E R N A L ACCESS THROUGH ACCESS PROVIDED
194DR
MPD MRB
GENERAL VISUAL INSPECTION OF THE LOWER WING TO BODY FAIRING 194 - AFT OF WHEEL WELL. emp I N T E R N A L emp emp emp emp emp emp emp emp emp emp emp emp emp
194AL 194AR 194BL 194BR 194CL 194CR 194DL 194DR 194E 194FL 194FR 194GL 194GR 194HL 194HR
ITEMS
MPD MRB
MPD MRB
53-844-00 MSI 53-844-00 I: 560 CYC I: 90 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 24 MTH I: 5500 CYC
E2 HHI 737-700
2 03-jun-04
I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
53-846-00 MSI 53-846-00
53-848-00 MSI 53-848-00
53-852-00 MSI 53-852-00
53-850-00 MSI 53-850-00
ATA: 05 - 19
Page 1 of 2
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
05195- 00000
R
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE ABOVE WING, WING TO BODY FAIRING - RIGHT AND LEFT SIDE. I N T E R N A L
ZONE ACCESS 195 emp emp emp emp emp 196 emp emp emp emp emp
STRUCTURE
195AL 195AR 195BL 195BR 195CL 195CR 196AL 196AR 196BL 196BR 196CL 196CR
ITEMS
REFERENCES MPD MPD MRB MRB MPD MPD MRB MRB
53-854-02 53-856-01 MSI 53-854-02 MSI 53-856-01 53-854-02 53-856-01 MSI 53-854-01 MSI 53-856-02
AMM
05-41-01-210
THRESHOLD INTERVAL
I: 24000 CYC I: 8 YRS
ATA: 05 - 19
TSK
EFF
E2 HHI 737-700
R L ITEM BY E E REVISION P V DATE
2 23-jul-08
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 20
05200- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUSELAGE - UPPER HALF VISUALLY INSPECT THE UPPER HALF OF FUSELAGE AS FAR AS VISIBLE 200 FROM GROUND E X T E R N A L
emp
empty
SERVICE EXPERIENCE
ITEMS
I: 1 T
ATA: 05 - 20
E1 HHI 737-700
FC SM
1 03-jun-04
Page 1 of 1
HHI R E V
ITEM 05 - 21 05210- 00000
R
737-6
MAINTENANCE SCHEDULE
05210- 01000
R
05210- 02000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLIGHT COMPARTMENT BODY STA 178 TO STA 259.5 GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 E X T E R N A L
emp emp
GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 I N T E R N A L ACCESS CONTROL STAND ACCESS PANELS 211A AND 212A REMOVAL REQUIRED
211A 212A
GENERAL VISUAL INSPECTION OF THE FLIGHT CONTROL COMPARTMENT 211 - SECTION 41, STA 178 TO STA 259.5. 212 I N T E R N A L ACCESS WITH ACCESS PROVIDED. SEATS REMOVED. CONTROL STAND ACCESS PANELS, OVERHEAD AND SIDEWALL PANELS AND FLOOR PANEL REMOVAL REQUIRED
emp emp
ITEMS
MPD MRB
53-858-00 MSI 53-858-00
MPD MRB
53-860-00 MSI 53-860-00
AMM
05-41-02-210
MPD MRB
53-862-00 MSI 53-862-00
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
4 23-jul-08
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
2 03-jun-04
ATA: 05 - 21
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 22
05220- 00000
05220- 01000
05220- 02000
05221- 00000
05222- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER COMPARTMENT BODY STA 259.5 TO STA 360 GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT AFT OF THE CONTROL COMPARTMENT TO FORWARD ENTRY DOOR LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. E X T E R N A L
221 222
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. I N T E R N A L
221 222
emp emp
emp emp
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT - 221 AFT OF THE CONTROL COMPARTMENT TO FORWARD ENTRY DOOR - 222 LEFT AND RIGHT - SECTION 41, STA 259.5 TO STA 360. I N T E R N A L ACCESS WITH ACCESS PROVIDED. GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED
emp emp
GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER ENTRY 221 DOOR STOPS, LATCHES AND HINGES -SECTION 41, STA 345. E X T E R N A L
831
GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR STOPS, LATCHES AND HINGES - SECTION 41, STA 340. E X T E R N A L
841
222
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-864-00 MSI 53-864-00 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
3 22-mar-07
I: 8 YRS I: 36000 CYC
E2 HHI 737-700
1 03-jun-04
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
53-866-00 MSI 53-866-00
53-868-00 MSI 53-868-00
53-870-00 MSI 53-870-00
53-872-00 MSI 53-872-00
ATA: 05 - 22
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 23
05230- 00000
05230- 01000
05230- 02000
05230- 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER COMPARTMENT BODY STA 360 TO STA 663.75 GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75. ATTENTION TO SKIN DAMAGE AROUND CRITICAL AREODYNAMIC AREAS OF THE FUSELAGE AT A/C OPERATING WITH RVSM (PITOT AND FLUSH STATIC PROBES AREA). E X T E R N A L
emp emp
GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75. I N T E R N A L
emp emp
GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75 WET AREAS (WITHIN APPROXIMATELY 20 INCHES FROM GALLEY OR LAV). I N T E R N A L ACCESS GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED IN WET AREAS
emp emp
GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER 231 COMPARTMENT - LEFT AND RIGHT - SECTION 43 AND 44 (PART), STA 360 232 TO STA 663.75 DRY AREA (AWAY FROM DOORS, GALLEYS AND LAVS). I N T E R N A L ACCESS FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED
emp emp
ITEMS
MPD MRB
53-874-00 MSI 53-874-00
SIL
737-SL-02-017-B
MPD MRB
53-876-00 MSI 53-876-00
MPD MRB
53-878-00 MSI 53-878-00
AMM
05-41-02-210
MPD MRB
53-880-00 MSI 53-880-00
AMM
05-41-02-210
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 8 YRS I: 36000 CYC
E2 HHI 737-700
3 05-sep-06
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
3 05-sep-06
ATA: 05 - 23
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 24
05240- 00000
05240- 01000
05240- 02000
05240- 03000
05241- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER COMPARTMENT BODY STA 663.75 TO STA 1016 GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD - LEFT AND RIGHT 242 SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. E X T E R N A L
emp emp
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD - LEFT AND RIGHT 242 SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L
emp emp
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD WET AREA (WITHIN 242 APPROXIMATELY 20 INCHES FROM GALLEY SERVICE DOOR, PASSENGER DOOR, GALLEY OR LAV) - LEFT AND RIGHT - SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L ACCESS GALLEYS AND LAVS REMOVED. FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED IN WET AREAS.
emp emp
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER COMPARTMENT 241 -STA 663.75 TO THE AFT PRESSURE BULKHEAD DRY AREA (AWAY FROM 242 DOORS, GALLEYS OR LAVS) - LEFT AND RIGHT - SECTION 44 (PART), 46 AND 47, STA 663.75 TO THE AFT PRESSURE BULKHEAD. I N T E R N A L ACCESS FLOOR PANELS, SIDEWALL PANELS AND CEILING PANELS REMOVAL REQUIRED.
emp emp
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER ENTRY DOOR 241 STOPS, LATCHES AND HINGES - SECTION 47, STA 980. E X T E R N A L
834
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-882-00 MSI 53-882-00 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 22-mar-07
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 8 YRS I: 36000 CYC
E2 HHI 737-700
2 22-mar-07
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
3 22-mar-07
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
53-884-00 MSI 53-884-00
53-886-00 MSI 53-886-00
53-888-00 MSI 53-888-00
53-890-00 MSI 53-890-00
ATA: 05 - 24
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05242- 00000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR STOPS, LATCHES AND HINGES- SECTION 47, STA 980. E X T E R N A L
ZONE ACCESS 242
STRUCTURE
844
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
53-892-00 MSI 53-892-00 I: 1500 CYC I: 180 DAY
ITEMS
TSK
ATA: 05 - 24
E2 HHI 737-700
5 22-mar-07
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 30
05300- 00000
05300- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ZONE 300-EMPENNAGE AND SECTION 48 GENERAL VISUAL INSPECTION OF THE VERTICAL FIN AND HORIZONTAL 320 STABILIZER. 330 E X T E R N A L 340 NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS
emp emp emp
MPD MRB
VISUALLY CHECK VERTICAL FIN AND RUDDER, HORIZONTAL STABILIZERS 300 AND ELEVATORS FOR OBVIOUS DAMAGE, EVIDENCE OF FLUID LEAKAGE 330 AND MISSING OR DAMAGED DISCHARGERS 340 E X T E R N A L
emp emp emp
empty
ITEMS
55-800-00 MSI 55-800-00
SERVICE EXPERIENCE
I: 560 CYC I: 90 DAY
E2 HHI 737-700
I: 1 T
E1 HHI 737-700
ATA: 05 - 30
5 22-mar-07
FC SM
1 13-apr-00
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 31
05310- 00000
05310- 01000
05310- 02000
05310- 03000
05310- 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUSELAGE STA 1016 TO 1217 GENERAL VISUAL INSPECTION OF THE AREA AFT OF PRESSURE 310 BULKHEAD - SECTION 48, STA 1016 TO STA 1088. E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.
emp
GENERAL VISUAL INSPECTION OF THE AREA AFT OF PRESSURE BULKHEAD - SECTION 48, AFT OF PRESSURE BULKHEAD TO STA 1088. I N T E R N A L
311BL emp
311 312
GENERAL VISUAL INSPECTION OF THE STABILIZER TORSION BOX 313 COMPARTMENT - SECTION 48, STA 1088 TO STA 1156. 314 I N T E R N A L ACCESS TORSION BOX COMPARTMENT VISIBLE THROUGH BS 1088 PENETRATION FOR THE HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING.
311BL emp
GENERAL VISUAL INSPECTION OF THE APU COMPARTMENT - SECTION 315 48, STA 1088 TO STA 1156. 316 I N T E R N A L
315A emp
GENERAL VISUAL INSPECTION OF THE TAIL CONE - SECTION 48, STA 1156 TO STA 1217. I N T E R N A L
emp 318BR
317 318
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-894-00 MSI 53-894-00 I: 560 CYC I: 90 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 22-mar-07
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 24 MTH I: 5500 CYC
E2 HHI 737-700
2 03-jun-04
53-896-00 MSI 53-896-00
53-898-00 MSI 53-898-00
53-900-00 MSI 53-900-00
53-902-00 MSI 53-902-00
ATA: 05 - 31
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 32
05321- 00000
05322- 00000
05322- 01000
05322- 02000
05323- 00000
05323- 01000
05324- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FIN AND RUDDER GENERAL VISUAL INSPECTION OF THE VERTICAL FIN DORSAL FIN E X T E R N A L
321
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 I N T E R N A L
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 E X T E R N A L
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - LEADING EDGE 322 I N T E R N A L
emp
322AL
emp
322B
MPD MRB
MPD MRB
MPD MRB
MPD MRB
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - FRONT SPAR TO 323 REAR SPAR emp I N T E R N A L emp emp emp emp emp
323AL 323BL 323CL 323DL 323EL 323FL 323GL
MPD MRB
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - FRONT SPAR TO 323 REAR SPAR E X T E R N A L
emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - REAR SPAR TO TRAILING EDGE I N T E R N A L
324AL 324BL 324DL 324HL
324 emp emp emp
ITEMS
MPD MRB
55-802-00 MSI 55-802-00 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
3 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 36000 CYC I: 12 YRS
E2 HHI 737-700
1 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
55-804-00 MSI 55-804-00
55-806-00 MSI 55-806-00
55-808-00 MSI 55-808-00
55-810-00 MSI 55-810-00
55-812-00 MSI 55-812-00
55-814-00 MSI 55-814-00
ATA: 05 - 32
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
05324- 01000
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN - REAR SPAR TO TRAILING EDGE E X T E R N A L
324
GENERAL VISUAL INSPECTION OF THE RUDDER E X T E R N A L
325
05325- 00000
05326- 00000
Date: 23-jul-08
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN TIP E X T E R N A L
ZONE ACCESS
326
STRUCTURE
emp
emp
emp
ITEMS
REFERENCES MPD MRB
MPD MRB
MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
55-816-00 MSI 55-816-00 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
55-818-00 MSI 55-818-00
55-820-00 MSI 55-820-00
ATA: 05 - 32
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 33
05331- 00000
05332- 00000
05332- 01000
05333- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
HORIZONTAL STABILIZER & ELEVATOR LEFT GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER LEADING EDGE - LEFT AND RIGHT E X T E R N A L
331 341
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - FRONT 332 SPAR TO REAR SPAR - LEFT AND RIGHT 342 E X T E R N A L
emp emp
emp emp
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - FRONT 332 SPAR TO REAR SPAR - LEFT AND RIGHT 342 I N T E R N A L ACCESS WITH ACCESS PROVIDED. AS AN ALTERNATE ACCESS PANEL 332AB AND 342AB CAN BE REMOVED FOR INSPECTION FROM LOWER SIDE OF STABILIZER.
332AT 342AT
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - REAR 333 SPAR TO TRAILING EDGE - LEFT AND RIGHT emp I N T E R N A L emp emp emp emp emp 343 emp emp emp emp emp emp emp
333AB 333AT 333AZ 333BB 333CB 333DB 333EB 343AB 343AT 343AZ 343BB 343CB 343DB 343EB 343FB
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
55-822-01 55-836-02 MSI 55-822-01 MSI 55-836-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 4000 CYC I: 18 MTH
E2 HHI 737-700
1 03-jun-04
I: 4000 CYC I: 18 MTH
E2 HHI 737-700
2 18-mar-05
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
55-824-01 55-838-02 MSI 55-824-01 MSI 55-838-02
55-826-01 55-840-02 MSI 55-826-01 MSI 55-840-02
55-828-01 55-842-02 MSI 55-828-01 MSI 55-842-02
ATA: 05 - 33
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05333- 01000
05334- 00000
05335- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER - REAR 333 SPAR TO TRAILING EDGE - LEFT AND RIGHT 343 E X T E R N A L
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER ELEVATOR - LEFT AND RIGHT E X T E R N A L
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER STABILIZER TIP - LEFT AND RIGHT E X T E R N A L
334 344
335 345
STRUCTURE
emp emp
emp emp
emp emp
ITEMS
REFERENCES MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
55-830-01 55-844-02 MSI 55-830-01 MSI 55-844-02 I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
55-832-01 55-846-02 MSI 55-832-01 MSI 55-846-02
55-834-01 55-848-02 MSI 55-834-01 MSI 55-848-02
ATA: 05 - 33
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 40
05400- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
POWER PLANTS & NACELLE STRUTS VISUALLY INSPECT POWERPLANTS, NACELLES AND PYLONS E X T E R N A L
400
emp
empty
SERVICE EXPERIENCE
ITEMS
I: 1 T
ATA: 05 - 40
E1 HHI 737-700
FC SM
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 41
05410- 00000
05410- 01000
05410- 02000
05410- 03000
05411- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NO. 1 POWERPLANT+ L/H NACELLE STRUT GENERAL VISUAL INSPECTION OF THE ENGINE NO.1 AND NO.2, AND ENGINE NO.1 AND NO.2 STRUT FAIRINGS. E X T E R N A L
410 420 430 440
GENERAL VISUAL INSPECTION OF THE THRUST REVERSER - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS THRUST REVERSER IN STOWED AND DEPLOYED POSITION
415 416 425 426
GENERAL VISUAL INSPECTION OF THE THRUST REVERSER - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS INNER AND OUTER EXTERIOR SURFACES
415 416 425 426
GENERAL VISUAL INSPECTION OF THE FAN COWL - ENGINE NO.1 AND NO.2 E X T E R N A L ACCESS INNER AND OUTER EXTERIOR SURFACE
413 414 423 424
GENERAL VISUAL INSPECTION OF THE ENGINE NO.1 AND NO.2 E X T E R N A L
411 emp emp emp 421 emp emp emp
emp emp emp emp
emp emp emp emp
415 416 425 426
413 414 423 424
413 414 415 416 423 424 425 426
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
70-800-01 70-810-02 MSI 70-800-01 MSI 70-810-02 I: 560 CYC I: 90 DAY
E2 HHI 737-700
5 22-mar-07
I: 2000 CYC
E2 HHI 737-700
1 03-jun-04
I: 2000 CYC
E2 HHI 737-700
1 03-jun-04
I: 4000 CYC
E2 HHI 737-700
1 03-jun-04
I: 2000 CYC
E2 HHI 737-700
1 03-jun-04
70-806-01 70-816-02 MSI 70-806-01 MSI 70-816-02
70-808-01 70-818-02 MSI 70-808-01 MSI 70-818-02
70-804-01 70-814-02 MSI 70-804-01 MSI 70-814-02
70-802-01 70-812-02 MSI 70-802-01 MSI 70-812-02
ATA: 05 - 41
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 43
05431- 00000
05432- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEFT NACELLE STRUT GENERAL VISUAL INSPECTION OF THE FORWARD STRUT FAIRING ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L
GENERAL VISUAL INSPECTION OF THE FAN COWL SUPPORT BEAM ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L
431 emp emp emp emp emp emp emp emp emp emp 441 emp emp emp emp emp emp emp emp emp emp
431AL 431AR 431AT 431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER 441AL 441AR 441AT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER
MPD MPD MRB MRB
432 442
431AT 441AT
MPD MPD MRB MRB
ITEMS
54-800-01 54-808-02 MSI 54-800-01 MSI 54-808-02 I: 9000 CYC I: 30 MTH
E2 HHI 737-700
1 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 05-sep-06
54-802-01 54-810-02 MSI 54-802-01 MSI 54-810-02
ATA: 05 - 43
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05433- 00000
05434- 00000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE STRUT TORQUE BOX - ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L
GENERAL VISUAL INSPECTION OF THE AFT STRUT FAIRING - ENGINE NO.1 AND ENGINE NO.2 I N T E R N A L
ZONE ACCESS
STRUCTURE
REFERENCES
433 emp emp emp emp emp 443 emp emp emp emp emp
433AL 433AR 433AT 433BT 433CT 433DT 443AL 443AR 443AT 443BT 443CT 443DT
MPD MPD MRB MRB
434 emp emp emp 444 emp emp emp
434AL 434AR 434BL 434CL 444AL 444AR 444BR 444CR
MPD MPD MRB MRB
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
54-804-01 54-812-02 MSI 54-804-01 MSI 54-812-02 I: 9000 CYC I: 30 MTH
E2 HHI 737-700
1 03-jun-04
I: 9000 CYC I: 30 MTH
E2 HHI 737-700
1 03-jun-04
54-806-01 54-814-02 MSI 54-806-01 MSI 54-814-02
ATA: 05 - 43
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 50
05500- 00000
05500- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEFT WING / RIGHT WING GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING E X T E R N A L NOTE( J ) INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS. ACCESS EXTEND CONTROL SURFACES
510 520 530 540 550 560 570 610 620 630 640 650 660 670
emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB MRB
VISUALLY CHECK LOWER WING SURFACE AND WING TIP OR WINGLETS 500 (IF INSTALLED) FOR OBVIOUS DAMAGE AND FUEL LEAKAGE 600 E X T E R N A L
emp emp
empty
ITEMS
57-802-01 57-872-02 MSI 57-802-01 MSI 57-872-02
SERVICE EXPERIENCE
I: 560 CYC I: 90 DAY
E2 HHI 737-700
I: 1 T
E1 HHI 737-700
ATA: 05 - 50
5 22-mar-07
FC SM
3 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 51
05511- 00000
05511- 01000
05512- 00000
05512- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING LEADING EDGE - FORWARD OF FRONT SPAR - INBOARD OF NACELLE STRUT - INCLUDING NACELLE GAP COVER AREA GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR 511 - INBOARD OF NACELLE STRUT - LEFT AND RIGHT WING. 611 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING
emp emp
GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR - INBOARD OF NACELLE STRUT - LEFT AND RIGHT WING. I N T E R N A L ACCESS FLAPS DEPLOYED
511AB 511AT 511BT 611AB 611AT 611BT
MPD MPD MRB MRB
emp emp emp emp
MPD MPD MRB MRB
511 emp emp 611 emp emp
GENERAL VISUAL INSPECTION OF THE KRUEGER FLAPS NO.1 AND NO.2 512 - LEFT WING, AND NO.3 AND NO.4 - RIGHT WING. 513 E X T E R N A L 612 613
GENERAL VISUAL INSPECTION OF THE KRUEGER FLAPS NO.1 AND NO.2 - LEFT WING, AND NO.3 AND NO.4 - RIGHT WING. I N T E R N A L ACCESS FLAPS DEPLOYED
512 513 612 613
emp emp emp emp
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
57-804-01 57-874-02 MSI 57-804-01 MSI 57-874-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-806-01 57-876-02 MSI 57-806-01 MSI 57-876-02
57-808-01 57-878-02 MSI 57-808-01 MSI 57-878-02
57-810-01 57-880-02 MSI 57-810-01 MSI 57-880-02
ATA: 05 - 51
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 52
05520- 00000
05521- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING LEADING EDGE - FORWARD OF FRONT SPAR - OUTBOARD OF NACELLE STRUT GENERAL VISUAL INSPECTION OF THE SLATS NO. 1, NO.2, NO.3 AND NO.4 - LEFT WING AND, SLATS NO.5, NO.6, NO.7 AND NO.8 - RIGHT WING. E X T E R N A L ACCESS SLATS IN FULL EXTEND POSITION
522 523 524 525 622 623 624 625
emp emp emp emp emp emp emp emp
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR 521 - OUTBOARD OF THE NACELLE STRUT - LEFT AND RIGHT WING. 621 E X T E R N A L ACCESS SLATS DEPLOYED
emp emp
MPD MPD MRB MRB
ITEMS
57-816-01 57-886-02 MSI 57-816-01 MSI 57-886-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-812-01 57-882-02 MSI 57-812-01 MSI 57-882-02
ATA: 05 - 52
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
05521- 01000
GENERAL VISUAL INSPECTION OF THE LEADING EDGE TO FRONT SPAR - OUTBOARD OF THE NACELLE STRUT - LEFT AND RIGHT WING. I N T E R N A L ACCESS SLATS DEPLOYED 521AAB, 521ABB, 621AAB
Date: 23-jul-08
ZONE ACCESS 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 621 emp emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-814-01 57-884-02 MSI 57-814-01 MSI 57-884-02 I: 5500 CYC I: 24 MTH
ATA: 05 - 52
E2 HHI 737-700
3 03-jun-04
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS emp emp emp emp emp emp emp emp emp
05526- 00000
05526- 01000
Date: 23-jul-08
GENERAL VISUAL INSPECTION OF THE WING TIP - LEFT AND RIGHT WING 526 E X T E R N A L 626
GENERAL VISUAL INSPECTION OF THE WING TIP - LEFT AND RIGHT WING 526 I N T E R N A L emp emp 626 emp emp
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB emp emp
526AB 526BB 526CB 626AB 626BB 626CB
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
57-818-01 57-888-02 MSI 57-818-01 MSI 57-888-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 21600 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
57-820-01 57-890-02 MSI 57-820-01 MSI 57-890-02
ATA: 05 - 52
Page 3 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
05 - 53
WING INSPAR AREA (FUEL TANKS) - INBOARD OF WING RIB 22 - WS 643.50
05531- 00000
05531- 01000
05532- 00000
Date: 23-jul-08
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE CENTER FUEL TANK - LEFT AND 531 RIGHT WING 631 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING
emp emp
GENERAL VISUAL INSPECTION OF THE CENTER FUEL TANK - LEFT AND 531 RIGHT WING emp I N T E R N A L 631 emp
531AB 531BB 631AB 631BB
GENERAL VISUAL INSPECTION OF THE MAIN FUEL TANK - LEFT AND RIGHT WING E X T E R N A L
532 632
STRUCTURE
emp emp
ITEMS
REFERENCES
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-824-01 57-894-02 MSI 57-824-01 MSI 57-894-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
1 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-822-01 57-892-02 MSI 57-822-01 MSI 57-892-02
57-828-01 57-898-02 MSI 57-828-01 MSI 57-898-02
ATA: 05 - 53
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05532- 01000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE MAIN FUEL TANK - LEFT AND RIGHT WING I N T E R N A L ACCESS ZONE 532: DO NOT REMOVE 532AZ AND 532BZ AT THE SAME TIME ZONE 632: DO NOT REMOVE 632AZ AND 632BZ AT THE SAME TIME
ZONE ACCESS 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-826-01 57-896-02 MSI 57-826-01 MSI 57-896-02 I: 36000 CYC I: 10 YRS
ATA: 05 - 53
E2 HHI 737-700
1 03-jun-04
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05533- 00000
05533- 01000
05534- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE SURGE TANK - LEFT AND RIGHT 533 WING 633 E X T E R N A L
STRUCTURE
emp emp
REFERENCES MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE SURGE TANK - LEFT AND RIGHT 533 WING emp I N T E R N A L emp 633 emp emp
533AB 533BB 533CB 633AB 633BB 633CB
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE DRY BAY - LEFT AND RIGHT WING 534 E X T E R N A L 634
emp emp
MPD MPD MRB MRB
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-832-01 57-902-02 MSI 57-832-01 MSI 57-902-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
1 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-830-01 57-900-02 MSI 57-830-01 MSI 57-900-02
57-834-01 57-904-02 MSI 57-834-01 MSI 57-904-02
ATA: 05 - 53
Page 3 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 54
05541- 00000
05542- 00000
05542- 01000
05543- 00000
05543- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING TRAILING EDGE FLAP TRACK FAIRINGS GENERAL VISUAL INSPECTION OF THE FLAP SUPPORT NO. 4 - LEFT WING , AND FLAP SUPPORT NO.5 - RIGHT WING - SECTION 46, STA 727. I N T E R N A L ACCESS FLAPS EXTENDED
133 134 194 541 641 emp
emp emp emp emp 194BL 194BR
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.3 - 542 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.6 - RIGHT WING 642 E X T E R N A L ACCESS FLAPS EXTENDED
emp emp
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.3 - 542 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.6 - RIGHT WING 642 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING
emp emp
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.2 - 543 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.7 - RIGHT WING 643 E X T E R N A L ACCESS FLAPS EXTENDED
emp emp
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.2 - 543 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.7 - RIGHT WING 643 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING
emp emp
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MPD MRB MRB
53-904-01 53-906-02 MSI 53-904-01 MSI 53-906-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
5 18-mar-05
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 18-mar-05
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 18-mar-05
57-836-01 57-906-02 MSI 57-836-01 MSI 57-906-02
57-838-01 57-908-02 MSI 57-838-01 MSI 57-908-02
57-840-01 57-910-02 MSI 57-840-01 MSI 57-910-02
57-842-01 57-912-02 MSI 57-842-01 MSI 57-912-02
ATA: 05 - 54
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05544- 00000
05544- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.1 - 544 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.8 - RIGHT WING 644 E X T E R N A L ACCESS FLAPS EXTENDED
emp emp
GENERAL VISUAL INSPECTION OF THE FAIRING FLAP SUPPORT NO.1 - 544 LEFT WING, AND THE FAIRING FLAP SUPPORT NO.8 - RIGHT WING 644 I N T E R N A L ACCESS FLAPS EXTENDED, INSIDE OF FAIRING
emp emp
STRUCTURE
ITEMS
REFERENCES MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-844-01 57-914-02 MSI 57-844-01 MSI 57-914-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 18-mar-05
57-846-01 57-916-02 MSI 57-846-01 MSI 57-916-02
ATA: 05 - 54
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
05 - 55
WING TRAILING EDGE - AFT OF REAR SPAR - INBOARD OF OUTBOARD TRAILING EDGE FLAP
05551- 00000
05551- 01000
05552- 00000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
REFERENCES
GENERAL VISUAL INSPECTION OF THE REAR SPAR TO LANDING GEAR 551 SUPPORT BEAM - LEFT AND RIGHT WING 651 E X T E R N A L ACCESS EXCLUDING SURFACE UNDER WING TO BODY FAIRING
emp emp
GENERAL VISUAL INSPECTION OF THE REAR SPAR TO LANDING GEAR 551 SUPPORT BEAM - LEFT AND RIGHT WING emp I N T E R N A L emp emp emp emp emp emp emp emp emp 651 emp emp emp emp emp emp emp emp emp emp
551AB 551AT 551BB 551BT 551CB 551CT 551DB 551DT 551EB 551ET 551FB 651AB 651AT 651BB 651BT 651CB 651CT 651DB 651DT 651EB 651ET 651FB
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE INBOARD SPOILER NO.6 - LEFT WING, AND THE INBOARD SPOILER NO.7 - RIGHT WING. E X T E R N A L ACCESS SPOILER RAISED
emp emp
MPD MPD MRB MRB
552 652
ITEMS
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-848-01 57-918-02 MSI 57-848-01 MSI 57-918-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 21600 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-850-01 57-920-02 MSI 57-850-01 MSI 57-920-02
57-852-01 57-922-02 MSI 57-852-01 MSI 57-922-02
ATA: 05 - 55
Page 1 of 2
HHI R E V
ITEM 05553- 00000
R
737-6
MAINTENANCE SCHEDULE
05553- 01000
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE INBOARD FLAPS - LEFT AND RIGHT 553 WING 653 E X T E R N A L ACCESS FLAPS EXTENDED
emp emp
GENERAL VISUAL INSPECTION OF THE INBOARD MAIN FLAPS - LEFT AND 553 RIGHT WING 653 I N T E R N A L ACCESS FLAPS EXTENDED
553BB 653BB
STRUCTURE
R
Date: 23-jul-08
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-854-01 57-924-02 MSI 57-854-01 MSI 57-924-02
MPD MPD MRB MRB MPD MPD MRB MRB
57-926-02 57-856-01 MSI 57-856-01 MSI 57-926-02 57-856-01 57-926-02 MSI 57-856-01 MSI 57-926-02
AMM AMM
05-41-05-210 05-41-06-210
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 21600 CYC I: 6 YRS
E2 HHI 737-700
3 23-jul-08
ATA: 05 - 55
Page 2 of 2
HHI R E V
R
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
05 - 56
WING TRAILING EDGE - AFT OF REAR SPAR - OUTBOARD OF INBOARD TRAILING EDGE FLAP - INBOARD OF FIXED TRAILING EDGE
05560- 00000
GENERAL VISUAL INSPECTION OF THE SPOILERS NO.1, 2, 3, 4, 5 - LEFT WING, AND SPOILERS NO.8, 9, 10, 11, 12 - RIGHT WING E X T E R N A L ACCESS SPOILERS RAISED
05567- 00000
Date: 23-jul-08
STRUCTURE
REFERENCES
562 563 564 565 566 662 663 664 665 666
emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB MRB MPD MPD MRB MRB
57-860-01 57-930-02 MSI 57-860-01 MSI 57-930-02 57-860-01 57-930-02 MSI 57-860-01 MSI 57-930-02
AMM AMM
05-41-05-210 05-41-06-210
GENERAL VISUAL INSPECTION OF THE REAR SPAR TO TRAILING EDGE 561 - OUTBOARD OF INBOARD FLAP - INBOARD OF FIXED TRAILING EDGE - 661 LEFT AND RIGHT WING E X T E R N A L ACCESS FLAPS DOWN, SPOILERS RAISED
emp emp
MPD MPD MRB MRB
57-858-01 57-928-02 MSI 57-858-01 MSI 57-928-02
GENERAL VISUAL INSPECTION OF THE OUTBOARD FLAPS - LEFT AND RIGHT WING E X T E R N A L ACCESS FLAPS EXTENDED
emp emp
R 05561- 00000
ZONE ACCESS
567 667
ITEMS
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 23-jul-08
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
57-862-01 57-932-02 MSI 57-862-01 MSI 57-932-02
ATA: 05 - 56
Page 1 of 1
HHI R E V
ITEM
DESCRIPTION
05 - 57
FIXED TRAILING EDGE - OUTBOARD OF OUTBOARD FLAP - INBOARD OF WING TIP WBL 658.17
05571- 00000
05571- 01000
R
737-6
MAINTENANCE SCHEDULE
05571- 02000
R
Date: 23-jul-08
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND 571 RIGHT WING 671 E X T E R N A L
GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND RIGHT WING I N T E R N A L ACCESS AILERON CONTROL AREA ONLY
571 emp 671 emp
GENERAL VISUAL INSPECTION OF THE FIXED TRAILING EDGE - LEFT AND 571 RIGHT WING emp I N T E R N A L emp emp emp emp emp emp 671 emp emp emp emp emp emp emp
STRUCTURE
emp emp
571AB 571BB 671AB 671BB
571AB 571AT 571BB 571BT 571CB 571DB 571EB 571FB 671AB 671AT 671BB 671BT 671CB 671DB 671EB 671FB
ITEMS
REFERENCES
MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-864-01 57-934-02 MSI 57-864-01 MSI 57-934-02 I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 10 YRS
E2 HHI 737-700
2 23-jul-08
57-868-01 57-938-02 MSI 57-868-01 MSI 57-938-02
MPD MPD MRB MRB MPD MPD MRB MRB
57-866-01 57-936-02 MSI 57-866-01 MSI 57-936-02 57-866-01 57-936-02 MSI 57-866-01 MSI 57-936-02
AMM AMM
05-41-05-210 05-41-06-210
ATA: 05 - 57
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
05572- 00000
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE AILERON - LEFT AND RIGHT WING 572 E X T E R N A L 672
STRUCTURE
emp emp
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
57-870-01 57-940-02 MSI 57-870-01 MSI 57-940-02 I: 5500 CYC I: 24 MTH
Date: 23-jul-08
TSK
ATA: 05 - 57
E2 HHI 737-700
2 03-jun-04
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 70
05700- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LANDING GEAR VISUALLY INSPECT LANDING GEARS, LANDING GEAR DOORS INCLUDING 700 WHEEL WELLS E X T E R N A L
emp
empty
SERVICE EXPERIENCE
ITEMS
I: 1 T
ATA: 05 - 70
E1 HHI 737-700
FC SM
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 71
05710- 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NOSE LANDING GEAR & DOORS GENERAL VISUAL INSPECTION OF THE NOSE LANDING GEAR AND 710 LANDING GEAR DOORS. E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.
emp
MPD MRB
32-800-00 MSI 32-800-00 I: 560 CYC I: 90 DAY
ITEMS
ATA: 05 - 71
E2 HHI 737-700
5 22-mar-07
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 73
05730- 00000
05730- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEFT MAIN LANDING GEAR & L.G. DOORS GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR AND LANDING 730 GEAR DOORS - LEFT AND RIGHT. 740 E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.
emp emp
GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR AND LANDING 730 GEAR DOORS - LEFT AND RIGHT. 740 E X T E R N A L
emp emp
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
32-804-01 32-808-02 MSI 32-804-01 MSI 32-808-02 I: 560 CYC I: 90 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
3 18-mar-05
32-806-01 32-810-02 MSI 32-806-01 MSI 32-810-02
ATA: 05 - 73
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 80
05800- 00000
05800- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ZONE 800- PASSENGER AND CARGO DOORS GENERAL VISUAL INSPECTION OF THE ENTRY DOORS, SERVICE DOORS, 820 AUTOMATIC OVERWING EXITS, AND CARGO DOORS. 830 E X T E R N A L 840 ACCESS DOORS CLOSED. INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS.
emp emp emp
MPD MRB
VISUALLY INSPECT ENTRY AND SERVICE DOORS, CARGO DOORS AND 800 EMERGENCY EXITS, INCLUDING DOOR SEALS E X T E R N A L ACCESS INSPECTION FROM GROUND WITHOUT THE USE OF STANDS OR LADDERS
emp
empty
52-800-00 MSI 52-800-00
SERVICE EXPERIENCE
ITEMS
I: 560 CYC I: 90 DAY
E2 HHI 737-700
I: 1 T
E1 HHI 737-700
ATA: 05 - 80
5 22-mar-07
FC SM
3 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 82
05821- 00000
05821- 01000
05822- 00000
05822- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOORS, LOWER HALF FUSELAGE, L/H GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR SECTION 43, STA 460. E X T E R N A L
821
GENERAL VISUAL INSPECTION OF THE FORWARD CARGO DOOR SECTION 43, STA 460. I N T E R N A L
821 emp emp emp
821
MPD MRB
821AR 821AZ 821BR 821BZ
MPD MRB
GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR - SECTION 46, 822 STA 827. E X T E R N A L
822
MPD MRB
GENERAL VISUAL INSPECTION OF THE AFT CARGO DOOR - SECTION 46, 822 STA 827. emp I N T E R N A L emp emp
822AR 822AZ 822BR 822BZ
ITEMS
MPD MRB
52-802-02 MSI 52-802-02 I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
52-804-02 MSI 52-804-02
52-806-02 MSI 52-806-02
52-808-02 MSI 52-808-02
ATA: 05 - 82
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 05 - 83
05831- 00000
05831- 01000
05833- 00000
05833- 01000
05834- 00000
05834- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOORS, UPPER HALF FUSELAGE, L/H GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER DOOR - 831 SECTION 41, STA 345. E X T E R N A L
831
GENERAL VISUAL INSPECTION OF THE FORWARD PASSENGER DOOR - 831 SECTION 41, STA 345. emp I N T E R N A L emp emp emp emp
831AW 831AZ 831BZ 831CZ 831DZ 831EZ
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. E X T E R N A L
833
833
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. I N T E R N A L ACCESS AUTOMATIC OVERWING EXIT DOOR LINER REMOVAL REQUIRED.
833
833AZ
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER DOOR - SECTION 834 47, STA 980. E X T E R N A L
834
GENERAL VISUAL INSPECTION OF THE AFT PASSENGER DOOR - SECTION 834 47, STA 980. emp I N T E R N A L emp emp emp emp
834AW 834AZ 834BZ 834CZ 834DZ 834EZ
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
52-810-01 MSI 52-810-01 I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 18000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
6 22-mar-07
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
52-812-01 MSI 52-812-01
52-818-01 MSI 52-818-01
52-820-01 MSI 52-820-01
52-822-01 MSI 52-822-01
52-824-01 MSI 52-824-01
ATA: 05 - 83
Page 1 of 1
HHI R E V
ITEM 05 - 84 05841- 00000
R
737-6
MAINTENANCE SCHEDULE
05841- 01000
R
05843- 00000
05843- 01000
05844- 00000
05844- 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOORS, UPPER HALF FUSELAGE, R/H GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR - SECTION 41, STA 340. E X T E R N A L
841
841
GENERAL VISUAL INSPECTION OF THE FORWARD GALLEY SERVICE DOOR - SECTION 41, STA 340. I N T E R N A L
841 emp emp emp emp emp
841AW 841AZ 841BZ 841CZ 841DZ 841EZ
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. E X T E R N A L
843
843
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT SECTION 44, STA 627. I N T E R N A L ACCESS AUTOMATIC OVERWING EXIT DOOR LINER REMOVAL REQUIRED
843
GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR SECTION 47, STA 980. E X T E R N A L
844
GENERAL VISUAL INSPECTION OF THE AFT GALLEY SERVICE DOOR SECTION 47, STA 980. I N T E R N A L
844 emp emp emp emp emp
843AZ
844
844AW 844AZ 844BZ 844CZ 844DZ 844EZ
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
52-826-02 MSI 52-826-02 I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 4000 CYC I: 18 MTH I: 24 MTH
E2 HHI 737-700
3 23-jul-08
I: 5500 CYC I: 24 MTH
E2 HHI 737-700
2 03-jun-04
I: 18000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
I: 1500 CYC I: 180 DAY
E2 HHI 737-700
5 22-mar-07
I: 4800 CYC I: 24 MTH
E2 HHI 737-700
2 22-mar-07
52-828-02 MSI 52-828-02
52-834-02 MSI 52-834-02
52-836-02 MSI 52-836-02
52-838-02 MSI 52-838-02
52-840-02 MSI 52-840-02
ATA: 05 - 84
Page 1 of 1
HHI R E V
ITEM 05 - 90
N
737-6
MAINTENANCE SCHEDULE
05900- 20290
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
05900- 20300
N
N
05900- 20310
N
N
05900- 20320
N
N
05900- 20330
N N
05900- 20340
N
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EZAP CLEAN AREA FORWARD OF NOSE WHEEL WELL. (EZAP)
112
112A
MPD MRB
20-290-00 MSI 20-290-00
N N
THRESHOLD INTERVAL
CLEAN THE AREA ABOVE AND OUTBOARD OF NOSE WHEEL WELL. (EZAP) LEFT AND RIGHT SIDE. ACCESS REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
113 emp emp 114 emp emp
113AC 113AW 113BW 114AC 114AW 114BW
MPD MRB
CLEAN THE AREA BEHIND THE ELECTRICAL AND ELECTRONICS RACK AND IN THE AIRSTAIR COMPARTMENT (IF INSTALLED). (EZAP) ACCESS ACCESS PANEL 117BL IS ONLY FOR AIRPLANES WITH AIRSTAIRS INSTALLED. ALTERNATE ACCESS BEHIND E2, E3, AND E4 ELECTRONICS RACK IS THROUGH 121JW, 121KW, 121LW AND 122HW PANELS.
117 emp 118 emp emp emp
117A 117BL 121JW 121KW 121LW 122HW
MPD MRB
INSPECT (DETAILED) THE POWER FEEDER AND EXPOSED EWIS BEHIND THE ELECTRICAL AND ELECTRONICS RACK. (EZAP) ACCESS ALTERNATE ACCESS BEHIND E2, E3, AND E4 ELECTRONICS RACK IS THROUGH 121JW, 121KW, 121LW AND 122HW PANELS.
117 118 emp emp emp
117A 121JW 121KW 121LW 122HW
MPD MRB
CLEAN AREAS BEHIND CEILING AND SIDEWALLS. (EZAP) ACCESS CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.
121 122
emp emp
MPD MRB
CLEAN AREAS BELOW FORWARD CARGO COMPARTMENT. (EZAP) 123 124 ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. CARGO LOADING SYSTEM REMOVED/DISPLACED AS REQUIRED.
emp emp
ITEMS
MPD MRB
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
20-300-00 MSI 20-300-00
20-310-00 MSI 20-310-00
20-320-00 MSI 20-320-00
20-330-00 MSI 20-330-00
20-340-00 MSI 20-340-00
ATA: 05 - 90
Page 1 of 8
HHI R E V
ITEM
N
05900- 20350
DESCRIPTION CLEAN AREA AFT OF FORWARD CARGO COMPARTMENT. (EZAP)
05900- 20360
N N
05900- 20370
N
N
05900- 20380
N N
05900- 20390
N N
05900- 20400
N N
05900- 20410
N
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
REFERENCES
125 emp 126
121EW 121HW 122GW
MPD MRB
INSPECT (GENERAL VISUAL) THE EWIS IN THE MAIN LANDING GEAR WHEEL WELL. (EZAP) ACCESS THROUGH MAIN LANDING GEAR OPENING.
133 134
emp emp
MPD MRB
CLEAN AREAS BEHIND THE AFT CARGO COMPARTMENT CEILING AND SIDEWALL PANELS. (EZAP) ACCESS CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.
141 142
N N
737-6
MAINTENANCE SCHEDULE
emp emp
CLEAN AREA BELOW AFT CARGO COMPARTMENT. (EZAP) 143 144 ACCESS CENTER FLOOR PANELS REMOVAL REQUIRED. CARGO LOADING SYSTEM REMOVED/DISPLACED AS REQUIRED.
emp emp
CLEAN AREA IN AFT CARGO COMPARTMENT EQUIPMENT BAY. (EZAP) ACCESS AFT CARGO PANELS AT 947 BULKHEAD REMOVAL REQUIRED.
emp emp
145 146
CLEAN FROM WATERLINE 208 TO 232 AND STA. 186 TO STA 211. (EZAP) 211 212 ACCESS ACCESSIBLE AREAS FORWARD OF AND ABOVE THE RUDDER PEDALS.
emp emp
INSPECT (DETAILED) THE EXPOSED EWIS IN THE FLIGHT COMPARTMENT. 211 (EZAP) 212 ACCESS WITH ACCESS PROVIDED. SEATS REMOVED. CONTROL STAND ACCESS PANELS, OVERHEAD AND SIDEWALL PANELS, GLARESHIELD, INSTRUMENT PANELS, P6, P18 FRONT PANELS, REMOVAL REQUIRED.
emp emp
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-350-00 MSI 20-350-00 I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 5500 CYC I: 30 MTH
E2 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS I: 1 s.N
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
S
HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
0 23-jul-08
20-360-00 MSI 20-360-00
20-370-00 MSI 20-370-00
20-380-00 MSI 20-380-00
20-390-00 MSI 20-390-00
20-400-00 MSI 20-400-00
20-410-00 MSI 20-410-00
ATA: 05 - 90
Page 2 of 8
HHI R E V
ITEM
N
05900- 20420
N
N
05900- 20430
N
N
05900- 20440
N
N
737-6
MAINTENANCE SCHEDULE
05900- 20450
DESCRIPTION
ZONE ACCESS
CLEAN AREAS ABOVE CEILING, SIDEWALLS AND UNDER THE RACEWAY 221 COVER PLATES ON BOTH SIDES OF THE PASSENGER COMPARTMENT. 222 (EZAP) ACCESS WITH ACCESS PROVIDED. GALLEYS AND LAVS REMOVED. CEILING AND SIDEWALL PANELS REMOVAL REQUIRED.
emp emp
CLEAN AREAS ABOVE CEILING, SIDEWALLS AND RETURN AIR GRILLES 231 IN FORWARD PASSENGER COMPARTMENT. (EZAP) 232 ACCESS GALLEYS AND LAVS REMOVED. SIDEWALL PANELS, CEILING PANELS AND AIR RETURN GRILLES REMOVAL REQUIRED.
emp emp
CLEAN AREAS ABOVE CEILING, SIDEWALLS AND RETURN AIR GRILLES 241 IN AFT PASSENGER COMPARTMENT. (EZAP) 242 ACCESS GALLEYS AND LAVS REMOVED. SIDEWALL PANELS, CEILING PANELS AND AIR RETURN GRILLES REMOVAL REQUIRED.
emp emp
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN THE 311 AREA AFT OF PRESSURE BULKHEAD. (EZAP) 312
311BL emp
STRUCTURE
REFERENCES MPD MRB
MPD MRB
MPD MRB
MPD MRB
05900- 20460
INSPECT (DETAILED) THE GENERATOR POWER FEEDERS, IGNITION LEADS AND ELECTRIC STARTER IN THE APU COMPARTMENT. (EZAP)
315 316
315A emp
MPD MRB
05900- 20470
INSPECT (DETAILED) THE GENERATOR POWER FEEDERS ON ENGINE NO. 1. (EZAP)
N N
05900- 20480
N
Date: 23-jul-08
INSPECT (DETAILED) THE GENERATOR POWER FEEDERS ON ENGINE NO. 2. (EZAP)
411 emp emp emp
413 414 415 416
MPD MRB
421 emp emp emp
423 424 425 426
MPD MRB
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
S
HHI 737-700
0 23-jul-08
I: 5500 CYC I: 30 MTH
E3 HHI 737-700
0 23-jul-08
I: 5500 CYC I: 30 MTH
E3 HHI 737-700
0 23-jul-08
I: 5500 CYC I: 30 MTH
E3 HHI 737-700
0 23-jul-08
20-430-00 MSI 20-430-00
20-440-00 MSI 20-440-00
20-450-00 MSI 20-450-00
20-460-00 MSI 20-460-00
N N
TSK
20-420-00 MSI 20-420-00
N N
THRESHOLD INTERVAL
20-470-00 MSI 20-470-00
20-480-00 MSI 20-480-00
ATA: 05 - 90
Page 3 of 8
HHI R E V
ITEM
DESCRIPTION
N
05900- 20490
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FWD STRUT FAIRING. (EZAP) NOTE( E ) ENGINE NO. 1
N
N
737-6
MAINTENANCE SCHEDULE
05900- 20500
ZONE ACCESS
STRUCTURE
REFERENCES
431 emp emp emp emp emp emp emp emp emp emp
431AL 431AR 431AT 431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER
MPD MRB
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FAN 432 COWL SUPPORT BEAM. (EZAP)
431AT
MPD MRB
05900- 20510
N
N
05900- 20520
N
Date: 23-jul-08
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN STRUT TORQUE BOX. (EZAP)
433 emp emp emp emp emp
433AL 433AR 433AT 433BT 433CT 433DT
MPD MRB
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FWD 441 STRUT FAIRING. (EZAP) emp emp emp emp emp emp emp emp emp emp
441AL 441AR 441AT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER
MPD MRB
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-490-00 MSI 20-490-00 I: 18000 CYC I: 6 YRS I: 1 s.N
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
20-500-00 MSI 20-500-00
N N
THRESHOLD INTERVAL
20-510-00 MSI 20-510-00
20-520-00 MSI 20-520-00
ATA: 05 - 90
Page 4 of 8
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
N
05900- 20530
DESCRIPTION
ZONE ACCESS
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN FAN 442 COWL SUPPORT BEAM. (EZAP)
STRUCTURE
441AT
REFERENCES MPD MRB
05900- 20540
INSPECT (DETAILED) THE POWER FEEDERS AND EXPOSED EWIS IN STRUT TORQUE BOX. (EZAP)
N
N
05900- 20550
N
Date: 23-jul-08
INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS FLAPS DEPLOYED.
443 emp emp emp emp emp
443AL 443AR 443AT 443BT 443CT 443DT
MPD MRB
511 emp emp
511AB 511AT 511BT
MPD MRB
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-530-00 MSI 20-530-00
N N
THRESHOLD INTERVAL
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
20-540-00 MSI 20-540-00
20-550-00 MSI 20-550-00
ATA: 05 - 90
Page 5 of 8
HHI R E V
ITEM
N
05900- 20560
N
N
737-6
MAINTENANCE SCHEDULE
05900- 20570
DESCRIPTION INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS SLATS DEPLOYED.
ZONE ACCESS 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO L.G. 551 SUPPORT BEAM. (EZAP)
STRUCTURE
REFERENCES
521AAB 521AB 521ABB 521AT 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB
MPD MRB
551DB
MPD MRB
05900- 20580
N
Date: 23-jul-08
INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO TRAILING EDGE. (EZAP) ACCESS FLAPS DOWN, SPOILERS RAISED.
561
emp
ITEMS
MPD MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-560-00 MSI 20-560-00 I: 36000 CYC I: 12 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
0 23-jul-08
20-570-00 MSI 20-570-00
N N
THRESHOLD INTERVAL
20-580-00 MSI 20-580-00
ATA: 05 - 90
Page 6 of 8
HHI R E V
ITEM
N
05900- 20590
N N
05900- 20600
N
N
737-6
MAINTENANCE SCHEDULE
05900- 20610
DESCRIPTION
ZONE ACCESS
STRUCTURE
INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS FLAPS DEPLOYED.
611 emp emp
611AB 611AT 611BT
MPD MRB
INSPECT (DETAILED) THE EXPOSED EWIS IN THE LEADING EDGE TO FRONT SPAR. (EZAP) ACCESS SLATS DEPLOYED.
621 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
621AAB 621AB 621ABB 621AT 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB
MPD MRB
651DB
MPD MRB
INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO L.G. 651 SUPPORT BEAM. (EZAP)
N
Date: 23-jul-08
REFERENCES
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-590-00 MSI 20-590-00 I: 36000 CYC I: 12 YRS
E3 HHI 737-700
0 23-jul-08
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
0 23-jul-08
I: 18000 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
20-600-00 MSI 20-600-00
20-610-00 MSI 20-610-00
ATA: 05 - 90
Page 7 of 8
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
N
05900- 20620
N
Date: 23-jul-08
DESCRIPTION INSPECT (DETAILED) THE EXPOSED EWIS FROM THE REAR SPAR TO TRAILING EDGE. (EZAP) ACCESS FLAPS DOWN, SPOILERS RAISED.
ZONE ACCESS 661
STRUCTURE
emp
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
20-620-00 MSI 20-620-00 I: 36000 CYC I: 12 YRS
ITEMS
TSK
ATA: 05 - 90
E3 HHI 737-700
0 23-jul-08
Page 8 of 8
HHI R E V
ITEM 08 08 - 10
R
737-6
MAINTENANCE SCHEDULE
081000 01000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEVELING AND WEIGHING WEIGHING PERFORM AIRCRAFT WEIGHING. REFER TO WEIGHING PROCEDURE IN MS INTRODUCTION. NOTE( I ) FOR WEIGHING DATES REFER TO MS INTRODUCTION CHAPTER 5.
000
emp
empty
AMM AAR
ITEMS
08-11-00-580-801 EU-OPS 1.605 B
I: 1 s.N
ATA: 08 - 10
M2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 21 - 25
212502 40000
212503 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIR CONDITIONING RECIRCULATION SYSTEM REPLACE THE RECIRCULATION FAN HEPA FILTER (S).
121
PERFORM A DETAILED INSPECTION OF THE RECIRCULATION FAN CHECK 121 VALVE(S) FOR CONDITION, SECURITY AND PROPER OPERATION. emp
emp
1201S 821
ITEMS
MPD MRB
21-010-00 MSI 21-010-00 RTE:7
AMTOSS AMTOSS
21-25-02-40 21-25-02-00
MPD MRB
21-015-00 MSI 21-015-00 RTE:8
AMTOSS
21-25-03-200
I: 6000 FLH
S
HHI 737-700
2 18-mar-05
I: 6000 FLH
E3 HHI 737-700
0 30-nov-05
ATA: 21 - 25
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 27
212700 70000
212700 71000
212700 89000
212701 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EQUIPMENT COOLING SYSTEM OPERATIONALLY CHECK THE ALTERNATE E/E COOLING EXHAUST FAN. 211 212 NOTE( J ) THIS TASK ALSO CHECKS THE NORMAL E/E COOLING EXHAUST FAN CHECK VALVE.
emp emp
OPERATIONALLY CHECK THE OVERBOARD EXHAUST VALVE IN SMOKE 211 CLEARANCE MODE. 212
emp emp
OPERATIONALLY CHECK THE ALTERNATE E/E COOLING SUPPLY FAN. 211 212 NOTE( J ) THIS TASK ALSO CHECKS THE NORMAL E/E COOLING SUPPLY FAN CHECK VALVE.
emp emp
REPLACE THE E/E COOLING SUPPLY FAN FILTER
emp
118
MPD MRB
21-030-00 MSI 21-030-00 RTE:9
AMTOSS
21-27-00-70
MPD MRB
21-050-00 MSI 21-050-00 RTE:9
AMTOSS
21-27-00-70
MPD MRB
21-020-00 MSI 21-020-00 RTE:9
AMTOSS
21-27-00-89
MPD MRB
21-040-00 MSI 21-040-00 RTE:6 MSI 21-040-00 RTE:9
MRB AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
21-27-01-40 21-27-01-00
I: 4000 FLH
F1 HHI 737-700
1 03-jun-04
I: 6000 FLH
F1 HHI 737-700
2 18-mar-05
I: 4000 FLH
F1 HHI 737-700
1 03-jun-04
I: 6000 FLH
S
2 18-mar-05
ATA: 21 - 27
HHI 737-700
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 31
213100 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CABIN PRESSURE CONTROL SYSTEM OPERATIONALLY CHECK THE OUTFLOW VALVE MANUAL MODE (MOTOR), 211 SELECTOR PANEL, INDICATOR, INDICATOR FEEDBACK MODULE. 212
emp emp
ITEMS
MPD MRB
21-060-00 MSI 21-060-00 RTE:9
AMTOSS
21-31-00-71
I: 6000 FLH
ATA: 21 - 31
F1 HHI 737-700
2 18-mar-05
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 32
213203 70000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CABIN PRESSURE RELIEF FUNCTIONALLY CHECK THE NEGATIVE PRESSURE RELIEF DOOR.
146
emp
ITEMS
MPD MRB
21-090-00 MSI 21-090-00 RTE:9
AMTOSS
21-32-03-700-801
I: 10 YRS
ATA: 21 - 32
F2 HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 33
213300 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CABIN PRESSURE INDICATION AND WARNING SYSTEM FUNCTIONAL CHECK OF THE CABIN PRESSURE SWITCH.
112
112A
ITEMS
MPD MRB
31-020-00 MSI 31-020-00 RTE:8
AMTOSS
21-33-00-00
I: 6000 FLH
ATA: 21 - 33
F2 HHI 737-700
3 18-mar-05
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 51
215103 00000
215105 40000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIR COOLING SYSTEM CLEAN THE PRIMARY AND SECONDARY HEAT EXCHANGERS.
CHECK THE LEFT AND RIGHT WATER SEPARATOR INDICATION DISK (WITH THE AIRCONDITIONING SYSTEM OPERATING).
131 132 emp emp emp emp
emp 192BL 192BR 192CL 192CR 192DR
MPD MRB
21-100-00 MSI 21-100-00 RTE:6
AMTOSS
21-51-03-000-801
123 124 emp
192CL 192CR 192DR
MPD MPD MRB
21-140-01 21-140-02 MSI 21-140-01 RTE:9 MSI 21-140-02 RTE:9
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
21-51-05-40
I: 2000 CYC
S
I: 600 FLH
E2 HHI 737-700
ATA: 21 - 51
HHI 737-700
2 03-jun-04
2 18-mar-05
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 21 - 61
216106 10000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ZONE TEMPERATURE CONTROL AND INDICATION CLEAN OR REPLACE THE CABIN TEMPERATURE SENSOR FILTERS (737-700 211 HAS ONE EACH IN THE CONTROL AND PASSENGER CABINS) 222
emp emp
ITEMS
MPD MRB
21-150-00 MSI 21-150-00 RTE:6
AMTOSS AMTOSS AMTOSS
21-61-06-10 21-61-06-40 21-61-06-00
I: 1200 FLH
ATA: 21 - 61
S
HHI 737-700
3 25-apr-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 23 23 - 24
232400 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COMMUNICATION EMERGENCY LOCATOR TRANSMITTER OPERATIONALLY CHECK THE EMERGENCY LOCATOR TRANSMITTER (AUTOMATIC/FIXED TYPE). NOTE( I ) AT VENDOR'S RECOMMENDATION
242
emp
MPD MRB
AMM
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
23-100-00 MSI 23-100-00 RTE:8 ARTEX I: 18 MTH INSTALLATION AND OPS. MANUAL DOC. NO.570-5004, CHAPTER 4 23-24-00
ATA: 23 - 24
F1 HHI 737-700 only: D-AHIC
0 18-mar-05
Page 1 of 1
HHI R E V
ITEM 23 - 30
R
737-6
MAINTENANCE SCHEDULE
233011 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER ADDRESS (PA) AND ENTERTAINMENT SYSTEM OPERATIONAL CHECK OF THE PASSENGER ADDRESS SPEAKERS, ATTENDANT AND LAVATORY SPEAKERS
200
emp
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
MPD MRB
23-090-00 MSI 23-090-00 RTE:9
AMTOSS AMM
23-31-00-74 23-31-00-740-801
I: 15000 FLH
ATA: 23 - 30
F1 HHI 737-700
6 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 23 - 60
236000 76000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STATIC DISCHARGER CHECK OF RESISTANCE OF STATIC DISCHARGERS.
325 326 330 340 526 570 572 626 670 672
emp emp emp emp emp emp emp emp emp emp
ITEMS
MPD MRB
23-030-00 MSI 23-030-00 RTE:9
AMTOSS
23-61-00-760-801
I: 4 YRS
ATA: 23 - 60
S HHI M1 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 23 - 71
237100 71000
237100 73000
237121 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
VOICE RECORDING SYSTEM OPERATIONAL CHECK OF THE VOICE RECORDER.
FUNCTIONAL CHECK OF THE VOICE RECORDER FOR AUDIO FIDELITY. NOTE( I ) MRB INTERVAL IS 2 YRS
OPERATIONAL CHECK OF THE ULB AT BATTERY REPLACEMENT. NOTE( I ) AT BATTERY REPLACEMENT
211
210
142
emp
emp
822
MPD MRB
23-040-00 MSI 23-040-00 RTE:9
AMTOSS
23-71-00-71
MPD MRB
23-050-00 MSI 23-050-00 RTE:9
AAR AMTOSS
NFL II-56/01 2.3.7 23-71-00-73
MPD MPD MRB
23-060-00 23-070-00 MSI 23-060-00 RTE:9 MSI 23-070-00 RTE:9
MRB AMTOSS AMTOSS AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
23-71-21-70 23-71-21-96 23-71-21-40 23-71-21-00
I: 300 FLH I: 40 DAY
F1 HHI 737-700
2 18-mar-05
I: 12 MTH I: 1 s.N
F2 HHI 737-700
1 03-jun-04
I: 1 s.N
F1 HHI 737-700
2 03-jun-04
ATA: 23 - 71
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 24 24 - 00
240000 01000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
CHANGE LEFT AND RIGHT IDG OIL.
411 421
413 423
MPD MPD MRB
R L ITEM BY E E REVISION P V DATE
DETAILED INSPECTION OF LEFT AND RIGHT IDG DELTA P INDICATOR
411 421
413AL 423AL
DETAILED INSPECTION OF LEFT AND RIGHT IDG OIL LEVEL. SERVICE IF 411 NECESSARY. 421
413AL 423AL
12-13-21-60
MPD MPD MRB
24-020-01 24-020-02 MSI 24-020-01 RTE:6 MSI 24-020-02 RTE:6
AMTOSS
12-13-21-20
MPD MPD MRB
24-030-01 24-030-02 MSI 24-030-01 RTE:6 MSI 24-030-02 RTE:6
AMTOSS
ITEMS
24-010-01 24-010-02 MSI 24-010-01 RTE:6 MSI 24-010-02 RTE:6
AMTOSS
MRB
Date: 23-jul-08
EFF
GENERAL
MRB
240000 03000
TSK
ELECTRICAL POWER
MRB
240000 02000
THRESHOLD INTERVAL
12-13-21-20
I: 1800 FLH
S
HHI 737-700
2 25-apr-06
I: 400 FLH
E3 HHI 737-700
2 18-mar-05
I: 400 FLH
S HHI E3 737-700
2 18-mar-05
ATA: 24 - 00
Page 1 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
240000 04000
GENERAL VISUAL INSPECTION OF HIRF/L SENSITIVE WIRE RUNS OUTSIDE THE PRESSURE VESSEL ON LEFT AND RIGHT SIDE OF THE AIRPLANE. LOOK FOR OBVIOUS SIGNS OF DAMAGE AND LACK OF SECURITY OF WIRE RUNS.
240000 05000
Date: 23-jul-08
GENERAL VISUAL INSPECTION OF HIRF/L SENSITIVE WIRE RUNS INSIDE THE PRESSURE VESSEL. LOOK FOR OBVIOUS SIGNS OF DAMAGE AND LACK OF SECURITY OF WIRE RUNS.
ZONE ACCESS
STRUCTURE
REFERENCES
131 133 191 emp 415 416 425 426 441 emp emp emp emp emp emp emp 510 520 550 560 610 620 650 660 730 740
emp emp 191FL 191FR emp emp emp emp 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp
MPD MPD MRB
AMTOSS AMTOSS
05-55-26-20 05-55-25-20
117 emp emp 118 emp emp emp emp
112A 113BW 117A 121EW 121JW 121KW 122GW 122HW
MPD MRB
20-020-00 MSI 20-020-00 RTE:8
AMTOSS
05-55-15-20
ITEMS
MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-010-01 20-010-02 MSI 20-010-01 RTE:8 MSI 20-010-02 RTE:8 I: 15000 FLH
E2 HHI 737-700
3 05-sep-06
I: 30000 FLH
E2 HHI 737-700
2 05-sep-06
ATA: 24 - 00
Page 2 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
240000 06000
PERFORM A DETAILED VISUAL INSPECTION OF HIRF/L SENSITIVE CONNECTORS OUTSIDE THE PRESSURE VESSEL ON LEFT AND RIGHT SIDE OF THE AIRPLANE.
Date: 23-jul-08
ZONE ACCESS 133 134 191 emp 440 emp emp emp emp emp emp emp emp emp emp emp emp emp 510 520 550 560 610 620 640 730 740
STRUCTURE
emp emp 191FL 191FR 416AR 431AL 431AR 431AT 431BL 431BR 431CL 431CR 441AL 441AR 441AT 441BL 441BR 441CL 511AB emp emp emp 611AB 621GB emp emp emp
ITEMS
REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-030-01 20-030-02 MSI 20-030-01 RTE:8 MSI 20-030-02 RTE:8 05-55-24-20 05-55-23-20
I: 12000 FLH
ATA: 24 - 00
E3 HHI 737-700
3 22-mar-07
Page 3 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
240000 07000
PERFORM A FUNCTIONAL CHECK OF THE HIRF/L SENSITIVE CONNECTORS OUTSIDE THE PRESSURE VESSEL ON THE LEFT AND RIGHT SIDE OF THE AIRPLANE. CHECK DC RESISTANCE FROM THE BACKSHELL TO GROUND.
240000 08000
Date: 23-jul-08
PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE CONNECTORS INSIDE THE PRESSURE VESSEL. DURING THE INSPECTION DO NOT DISCONNECT CONNECTORS. LOOK FOR CONDITION, SECURITY AND SIGNS OF CORROSION.
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
133 134 191 emp 431 emp emp emp 441 emp emp emp 510 520 550 560 610 emp 650 660 730 740
emp emp 191FL 191FR 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp
MPD MPD MRB
AMM AMM AMTOSS AMTOSS
05-55-44-200 05-55-45-200 05-55-41-20 05-55-40-20
117 emp emp 118 emp emp emp emp 211 212
112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp
MPD MRB
20-050-00 MSI 20-050-00 RTE:8
AMTOSS AMTOSS
20-10-37-12 05-55-15-200-801
ITEMS
MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-040-01 20-040-02 MSI 20-040-01 RTE:8 MSI 20-040-02 RTE:8 I: 15000 FLH
F2 HHI 737-700
3 22-mar-07
I: 20000 FLH
E3 HHI 737-700
3 05-sep-06
ATA: 24 - 00
Page 4 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
240000 09000
240000 09100
240000 10000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
FUNCTIONAL CHECK OF HIRF/L SENSITIVE CONNECTORS INSIDE THE 112 PRESSURE VESSEL BY DC RESISTANCE CHECK FROM BACKSHELL TO 113 GROUND. 117 118 emp emp emp emp 121 122 211 212 230
112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp emp emp emp
MPD MRB
20-060-00 MSI 20-060-00 RTE:8
AMTOSS
20-40-11-760-802
PERFORM A FUNCTIONAL CHECK OF THE HIRF/L SENSITIVE CONNECTORS 310 INSIDE THE EMPENNAGE.
311BL
MPD MRB
20-140-00 MSI 20-140-00 RTE:8
AMM AMM
05-55-42-200 05-55-46-200
MPD MRB
20-070-00 MSI 20-070-00 RTE:8
AMTOSS
05-55-15-200-803
PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE PIG TAILS INSIDE THE PRESSURE VESSEL. LOOK FOR CONDITION OF SECURITY AND SIGNS OF CORROSION.
117 emp emp 118 emp emp emp emp 211 212
112A 113BW 117A 121EW 121JW 121KW 122GW 122HW emp emp
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 30000 FLH
F2 HHI 737-700
3 05-sep-06
I: 15000 FLH
F2 HHI 737-700
0 22-mar-07
I: 30000 FLH
E3 HHI 737-700
3 05-sep-06
ATA: 24 - 00
Page 5 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
240000 11000
PERFORM A DETAILED VISUAL INSPECTION OF THE HIRF/L SENSITIVE PIG TAILS OUTSIDE THE PRESSURE VESSEL ON THE LEFT AND RIGHT SIDE OF THE AIRPLANE. INSPECT FOR CONDITION OF SECURITY AND SIGNS OF CORROSION.
Date: 23-jul-08
ZONE ACCESS 133 134 191 emp 415 416 431 emp emp emp emp emp emp emp 510 520 550 560 610 620 650 660 730 740
STRUCTURE
emp emp 191FL 191FR emp emp 431AL 431AR 431AT 431CR 441AL 441AR 441AT 441CL 511AB emp emp emp 611AB 621GB emp emp emp emp
ITEMS
REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-080-01 20-080-02 MSI 20-080-01 RTE:8 MSI 20-080-02 RTE:8 05-55-23-20 05-55-24-20
I: 15000 FLH
ATA: 24 - 00
E3 HHI 737-700
5 05-sep-06
Page 6 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
240000 13000
PERFORM A GENERAL VISUAL INSPECTION OF THE BONDING STRAPS AT THE FOLLOWING LOCATIONS: - 1 STRAP EACH ON THE RUDDER - 2 STRAPS PER AILERON, LEADING EDGE FLAP, SPOILER AND EACH ELEVATOR SURFACE. - STRUT TO WING BONDING USES 1 STRAP PER WING. - EACH AIR CONDITIONING PACK COMPARTMENT DOOR, MAIN LANDING GEAR DOOR, EACH ENGINE COWLING AND EACH STRUT TO ENGINE INSTALLATION USES 2 BONDING STRAPS.
Date: 23-jul-08
ZONE ACCESS 192 emp 325 334 emp 344 emp 431 441 emp 512 513 562 563 564 565 571 emp emp 612 613 662 663 664 665 671 emp emp 731 732 733 741 742 743
STRUCTURE
192CL 192CR 324ABL 334GB 334NB 344GB 344NB emp 431CL 441CR emp emp emp emp emp emp 571BB 571CB 571DB emp emp emp emp emp emp 671BB 671CB 671DB emp emp emp emp emp emp
ITEMS
REFERENCES MPD MRB
20-100-00 MSI 20-100-00 RTE:8
AMTOSS
05-55-08-20
THRESHOLD INTERVAL
I: 15000 FLH
ATA: 24 - 00
TSK
EFF
E2 HHI 737-700
R L ITEM BY E E REVISION P V DATE
4 05-sep-06
Page 7 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
240000 14000
240000 15000
240000 16000
DESCRIPTION
ZONE ACCESS
STRUCTURE
GENERAL VISUAL INSPECTION OF EXTERNAL (COWL OPEN) HARNESS 411 CONDITION AND SECURITY OF LEFT AND RIGHT ENGINE emp emp emp 421 emp emp emp
413 414 415 416 423 424 425 426
MPD MPD MRB
AMTOSS
05-55-10-20
DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE CONNECTORS 411 FOR TIGHTNESS (ALL CONNECTORS ON HARNESS J5, J6, J7, J8, J9, J10, emp CJ9, CJ10, MW0301, MW0302, MW0303, MW0304). emp emp 421 emp emp emp
413 414 415 416 423 424 425 426
MPD MPD MRB
20-120-01 20-120-02 MSI 20-120-01 RTE:8 MSI 20-120-02 RTE:8
AMTOSS
05-55-10-22
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ENGINE BONDING 415 STRAPS RELATED TO HIRF / LIGHTNING FOR CONDITION AND SECURITY. 416 425 426 433 443
415AL 416AR 425AL 426AR emp emp
MPD MPD MRB
20-130-01 20-130-02 MSI 20-130-01 RTE:8 MSI 20-130-02 RTE:8
MRB
MRB
MRB AMTOSS
240000 18000
Date: 23-jul-08
MEASURE THE AIRPLANE EXTERNAL POWER RECEPTACLE NEUTRAL PIN CONTINUITY TO AIRFRAME GROUND. MEASURE THE AIRPLANE ELECTRICAL RESISTANCE TO GROUND.
118 734 744
emp emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
20-110-01 20-110-02 MSI 20-110-01 RTE:8 MSI 20-110-02 RTE:8 I: 6000 FLH
E1 HHI 737-700
2 18-mar-05
I: 15000 FLH
E3 HHI 737-700
3 03-jun-04
05-55-11-200-801
I: 6000 FLH
E1 HHI 737-700
5 05-sep-06
737-SL-20-029-B
I: 4000 FLH
M2 HHI 737-700
2 03-jun-04
empty
SIL
ATA: 24 - 00
Page 8 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 24 - 11
241141 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
REPLACE LEFT AND RIGHT IDG CHARGE AND SCAVENGE FILTERS.
411 421
413 423
MPD MPD MRB
EFF
R L ITEM BY E E REVISION P V DATE
TORQUE CHECK LEFT AND RIGHT ENGINE IDG QUICK ATTACH/DETACH 411 (QAD) COUPLING. 421
413 423
24-11-41-00
MPD MPD MRB
24-050-01 24-050-02 MSI 24-050-01 RTE:6 MSI 24-050-02 RTE:6
AMTOSS
ITEMS
24-040-01 24-040-02 MSI 24-040-01 RTE:6 MSI 24-040-02 RTE:6
AMTOSS
MRB
Date: 23-jul-08
TSK
AC GENERATOR DRIVE SYSTEM
MRB
241161 20000
THRESHOLD INTERVAL
24-11-61-20
I: 1800 FLH
S
HHI 737-700
2 25-apr-06
I: 1800 FLH
M1 HHI 737-700
2 25-apr-06
ATA: 24 - 11
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 24 - 31
243141 72000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DC GENERATION SYSTEM CHECK REMOTE CONTROL CIRCUIT BREAKER NOTE( E ) FOR DUAL BATTERY INSTALLATION ONLY!
117 118
emp emp
ITEMS
MPD MRB
24-110-00 MSI 24-110-00 RTE:8
AMTOSS
24-31-41-71
I: 10000 CYC
ATA: 24 - 31
F1 HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 24 - 34
243400 71200
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STANDBY POWER SYSTEM OPERATIONAL TEST STANDBY POWER CONTROL UNIT NOTE( E ) FOR DUAL BATTERY INSTALLATION ONLY!
210
emp
ITEMS
MPD MRB
24-100-00 MSI 24-100-00 RTE:8
AMTOSS
24-34-00-710-802
I: 15 DAY
ATA: 24 - 34
F1 HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
ITEM
DESCRIPTION
25
EQUIPMENT & FURNISHINGS
25 - 00
EQUIPMENT / FURNISHINGS
250000 01000
250000 04001
250000 05001
250000 06001
250000 08001
D
737-6
MAINTENANCE SCHEDULE
250000 09001
ZONE ACCESS
STRUCTURE
emp
REFERENCES
CHECK THE EXPIRATION DATE OF THE FLIGHT CREW SEAT BELTS, PASSENGER SEAT BELTS, CREW REST BUNKS/SEAT BELTS, SPECIAL EQUIPMENT USING SEAT BELT WEBBING. IF THE EXPIRATION DATE IS LESS THAN 12 MONTH INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE( I ) EXPIRATION DATE IS MANUFACTURING DATE PLUS 12 YEARS
200
AAR
INTERIOR CLEANING DURING NIGHT STOP. NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS MAX.
220 240
emp emp
empty
FLOOR COVERING IN ENTRY AND GALLEY AREAS FOR OBVIOUS DAMAGE 220 AND CONTAMINATION 240 NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
emp emp
empty
GALLEYS FOR GENERAL CONDITION, OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
222
emp
empty
CARPET IN ENTIRE CABIN AREA FOR OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
220 240
emp emp
empty
emp emp
empty
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NFL II 83/99 I: 12 MTH
E2 HHI 737-700
1 23-jul-08
SERVICE EXPERIENCE
I: 1 Z
S
HHI 737-700
SM
2 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
SM
2 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
E2 HHI 737-700
SM
3 03-jun-04
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
SM
2 11-dec-01
ITEM DELETED.
D
3 23-jul-08 250000 13001
Date: 23-jul-08
SIDEWALL - AND CEILING PANELS, BINS: PARTITIONS AND CURTAINS FOR OBVIOUS DAMAGE AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
220 240
ITEMS
SERVICE EXPERIENCE
I: 1 Z
ATA: 25 - 00
E2 HHI 737-700
SM
2 11-dec-01
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
250000 14001
250000 15001
250000 22000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
CEILING PANELS FOR PROPER INSTALLATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
220 240
emp emp
empty
TOILETS FOR OBVIOUS DAMAGES AND CONTAMINATION NOTE( I ) EXCEPTIONALLY, THE INTERVAL MAY BE EXTENDED TO 7 DAYS
220 240
emp emp
empty
DIVIDER NET AND COVER, SEPARATION NET, DOOR PROTECTION NET 120 (NETS INCLUDING TENSION BUCKLE, TIE DOWN FITTINGS, ATTACHMENT 140 POINTS)
emp emp
empty
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
SM
2 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
E2 HHI 737-700
SM
2 11-dec-01
SERVICE EXPERIENCE
I: 7 DAY
E2 HHI 737-700
SM
2 11-dec-01
ATA: 25 - 00
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 11
251100 20000
251100 20100
251111 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLIGHT COMPARTMENT SEATS INSPECT (DETAILED) THE CAPTAIN, FIRST OFFICER, FIRST OBSERVER, 210 AND SECOND OBSERVER (IF INSTALLED) SEAT HARNESSES, CROTCH STRAPS, AND SHOULDER BELTS (AS APPLICABLE) FOR WEAR, CONDITION, AND SECURITY.
emp
OPERATIONALLY CHECK THE CAPTAIN, FIRST OFFICER, AND THE FIRST 210 OBSERVER SEAT HARNESS INERTIA REELS.
emp
FUNCTIONALLY CHECK THE HORIZONTAL ADJUSTMENT HOLES IN THE 211 CAPTAIN AND FIRST OFFICERS SEAT TRACKS FOR ELONGATION AND 212 VERIFY THE CAPTAIN AND FIRST OFFICER SEAT TRACKS FOR WEAR, CONDITION, AND SECURITY.
emp emp
MPD MRB
25-020-00 MSI 25-020-00 RTE:8
AMTOSS
25-11-00-200-801
MPD MRB
25-030-00 MSI 25-030-00 RTE: 8
AMTOSS
25-11-00-200-801
MPD MPD MRB
25-010-01 25-010-02 MSI 25-010-01 RTE:5 MSI 25-010-02 RTE:5
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
25-11-11-200-801
I: 600 FLH
E3 HHI 737-700
4 22-mar-07
I: 3500 FLH
F1 HHI 737-700
2 03-jun-04
I: 4000 FLH
F2 HHI 737-700
1 03-jun-04
ATA: 25 - 11
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 22
252200 20000
252200 71000
252200 71100
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER COMPARTMENT SEATS INSPECT (DETAILED) THE PASSENGER SEAT BELTS W/O REMOVAL FOR WEAR, CONDITION, AND SECURITY.
220 230 240
OPERATIONALLY CHECK THE PASSENGER SEAT BREAK-OVER FEATURE 230 ON ALL SEATS ADJACENT (FORWARD AND AFT) TO ALL OF EMERGENCY 240 EXITS..
INSPECT (DETAILED) THE PASSENGER SEAT BACK RECLINE AND RECLINE 220 RESTRICTION MECHANISMS FOR CONDITION, SECURITY, AND PROPER 230 OPERATION. 240
emp emp emp
emp emp
emp emp emp
MPD MRB
25-040-00 MSI 25-040-00 RTE:8
AMTOSS
25-22-00-20
MPD MRB
25-050-00 MSI 25-050-00 RTE:8
AMTOSS
25-22-00-71
MPD MPD MRB
25-060-00 25-070-00 MSI 25-060-00 RTE:5 MSI 25-070-00 RTE:5
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
25-22-00-71
I: 4000 FLH
E3 HHI 737-700
1 03-jun-04
I: 4000 FLH
F1 HHI 737-700
2 03-jun-04
I: 4000 FLH
E3 HHI 737-700
2 03-jun-04
ATA: 25 - 22
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 25
252512 20000
252512 71000
252512 71200
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CABIN ATTENDANT SEATS INSPECT (DETAILED) THE ATTENDANT SEAT HARNESS W/O REMOVAL FOR WEAR, CONDITION, AND SECURITY.
INSPECT (DETAILED) THE ATTENDANT SEAT BOTTOMS FOR PROPER RETRACTION, CONDITION, AND SECURITY.
221 241
221 241
OPERATIONALLY CHECK THE ATTENDANT SEAT HARNESS INERTIA REEL 221 LOCK FEATURE AND THE INERTIA REEL. 241
emp emp
emp emp
emp emp
MPD MRB
25-090-00 MSI 25-090-00 RTE:8
AMTOSS
25-25-12-200-801
MPD MRB
25-080-00 MSI 25-080-00 RTE:5
AMTOSS
25-25-12-710-801
MPD MPD MRB
25-100-00 25-110-00 MSI 25-100-00 RTE:8 MSI 25-110-00 RTE:8
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
25-25-12-710-802
I: 4000 FLH
E3 HHI 737-700
2 03-jun-04
I: 4000 FLH
E3 HHI F1 737-700
1 03-jun-04
I: 4000 FLH
F1 HHI 737-700
3 03-jun-04
ATA: 25 - 25
Page 1 of 1
HHI R E V
ITEM 25 - 40
R
737-6
MAINTENANCE SCHEDULE
254008 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LAVATORIES OPERATIONALLY CHECK THE LAVATORY WASTE COMPARTMENT 221 FLAPPER DOOR SPRING. INSPECT (DETAILED) THE LAVATORY WASTE 241 COMPARTMENT FLAPPER DOOR AND THE LAVATORY WASTE 242 COMPARTMENT ACCESS DOOR LATCHING MECHANISM FOR WEAR, CONDITION AND SECURITY. NOTE( I ) INSPECT THE WASTE RECEPTACLES PER AD 74-08-09 AT AN INTERVAL NOT TO EXCEED 1000 HOURS
emp emp emp
AAR MPD MPD MRB MRB
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
AMTOSS
ITEMS
AD 74-08-09 REV. 02 25-120-00 25-130-00 MSI 25-120-00 RTE:8 MSI 25-130-00 RTE:8 25-40-08-20
I: 1000 FLH
ATA: 25 - 40
E3 HHI F1 737-700
4 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 52
255200 20000
255200 20100
255200 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CARCO COMPARTMENT LINING INSPECT THE STA 396 BULKHEAD PANELS FOR CONDITION AND SECURITY.
121 122
emp emp
MPD MRB
25-140-00 MSI 25-140-00 RTE:8
AMTOSS
25-52-00-20
INSPECT (GENERAL VISUAL) THE CARGO COMPARTMENT FLOOR, CEILING 121 AND SIDEWALL PANELS / LINERS FOR HOLES / TEARS, CONDITION AND 122 SECURITY. 141 142 822
821 emp emp emp emp
MPD MRB
25-160-00 MSI 25-160-00 RTE:8
AMTOSS
25-52-00-20
INSPECT THE CARGO DOOR RESTRAINT SYSTEM FOR CONDITION AND 121 SECURITY. 122 141 142
emp 821 emp 822
MPD MRB
25-170-00 MSI 25-170-00 RTE:9
AMTOSS
25-52-00-21
ITEMS
I: 450 CYC
E2 HHI 737-700
2 03-jun-04
I: 300 CYC
E2 HHI 737-700
3 18-mar-05
I: 4000 CYC
E1 HHI 737-700
2 22-mar-07
ATA: 25 - 52
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
25 - 61
ESCAPE STRAPS AND LANYARDS AND ESCAPE SLIDES (DOOR MOUNTED)
256110 20000
ZONE ACCESS
OPERATIONALLY CHECK THE LEFT AND RIGHT EMERGENCY EXIT HATCH 231 ESCAPE STRAP. 232 emp
STRUCTURE
emp 833 843
REFERENCES
MPD MPD MRB MRB
256110 71000
INSPECT (DETAILED) THE LEFT AND RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP FOR CONDITION AND SECURITY.
231 232 emp
emp 833 843
256110 71100
Date: 23-jul-08
INSPECT (DETAILED) THE FLIGHT COMPARTMENT ESCAPE LANYARDS 211 (2) FOR CONDITION AND SECURITY. 212
emp emp
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
25-180-01 25-180-02 MSI 25-180-01 RTE:8 MSI 25-180-02 RTE:8
AMTOSS AMTOSS
25-61-10-71 25-61-10-20
MPD MPD MRB
25-190-01 25-190-02 MSI 25-190-01 RTE:8 MSI 25-190-02 RTE:8
MRB
THRESHOLD INTERVAL
AMTOSS AMTOSS
25-61-10-20 25-61-10-71
MPD MRB
25-210-00 MSI 25-210-00 RTE:8
AMTOSS AMTOSS
25-61-10-21 25-61-10-20
I: 10 YRS
F1 HHI 737-700
3 05-sep-06
I: 10 YRS
E3 HHI 737-700
3 05-sep-06
I: 10 YRS
E3 HHI 737-700
1 03-jun-04
ATA: 25 - 61
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 62
256299 00001
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
OVER-WATER SURVIVAL EQUIPMENT (OPTIONAL) CHECK THE EXPIRATION DATE OF THE FLIGHT CREW LIFE VEST (P/N 200 63600-505) AND PASSENGER LIFE VESTS (ADULT: P/N 63600-105, P/N 0723E105P, CHILD: P/N 216200-0, P/N 208511-1). IF THE EXPIRATION DATE IS LESS THAN 12 MONTH INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE: EXPIRATION DATE FOR VACUUM SEALED LIFE VESTS IS MANUFACTURING DATE PLUS 120 MTH , EXPIRATION DATE FOR NON-VACUUM SEALED LIFE VESTS IS MANUFACTURING DATE PLUS 60 MONTH.
emp
empty
MS MS
ITEMS
CM2560 00020 CM2560 00030 SERVICE EXPERIENCE
I: 12 MTH
ATA: 25 - 62
S
HHI 737-700
0 23-jul-08
Page 1 of 1
HHI R E V
ITEM 25 - 64 256400 21000
256400 71100
256400 71200
256401 21000
R
737-6
MAINTENANCE SCHEDULE
256401 71000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DETACHABLE EMERGENCY EQUIPMENT VISUALLY CHECK THE LIFE RAFT PRESSURE BOTTLE FOR PROPER PRESSURE.
OPERATIONALLY CHECK THE POWER MEGAPHONES.
REPLACE THE POWER MEGAPHONE BATTERIES AT THE MANUFACTURER'S RECOMMENDED INTERVAL.
221 241
221 241
221 241
VISUALLY CHECK ALL DETACHABLE EMERGENCY EQUIPMENT (GLOVES, 221 SMOKE GOGGLES, CRASH AXE, FLASH LIGHTS, FIRST AID KITS, AND 241 MEDICAL KITS AS APPLICABLE) FOR CONDITION AND PRESENCE.
OPERATIONALLY CHECK THE EMERGENCY FLASH LIGHTS. NOTE( I ) AT VENDOR RECOMMENDATION
221 241
emp emp
emp emp
emp emp
emp emp
emp emp
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
MPD MRB
25-310-00 MSI 25-310-00 RTE:8
AMTOSS
25-64-00-21
MPD MRB
25-330-00 MSI 25-330-00 RTE:9
AMTOSS
25-64-00-71
MPD MRB
25-340-00 MSI 25-340-00 RTE:9
AMTOSS
25-64-00-900
MPD MRB
25-370-00 MSI 25-370-00 RTE:8
AMTOSS
25-64-00-21
MPD MRB
25-380-00 MSI 25-380-00 RTE:9
AMTOSS AMTOSS AMM AMM
25-64-00-20 25-64-00-71 25-64-00-200-802 25-64-00-200-803
I: 15 MTH
E2 HHI 737-700
1 03-jun-04
I: 18 MTH
F1 HHI 737-700
2 30-nov-05
I: 18 MTH
S
HHI 737-700
0 30-nov-05
I: 2 YRS
E2 HHI 737-700
1 03-jun-04
I: 18 MTH
F1 HHI 737-700
2 23-jul-08
ATA: 25 - 64
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
256402 90000
256403 20000
256404 90000
256405 90000
Date: 23-jul-08
DESCRIPTION REPLACE THE EMERGENCY FLASH LIGHT BATTERIES. NOTE( I ) VENDOR RECOMMENDATION
ZONE ACCESS 200
STRUCTURE
emp
PROTECTIVE BREATHING EQUIPMENT (SMOKE HOODS) - VENDOR: SCOTT. 221 CHECK FOR CONDITION OF BOX AND ATTACHMENTS. REPLACE IF 241 DAMAGED, CLEAN IF NECESSARY. CHECK FOR EXPIRATION DATE. EXPIRATION DATE IS MANUFACTURE DATE + 10 YEARS. NOTE( M ) IF EXPIRATION DATE IS REACHED DURING NEXT 20 MONTHS, INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION!
emp emp
CHECK THE FIRST AID KITS FOR COMPLETENESS AND THE EXPIRY DATES 221 OF ITS CONTENT. IF ANY EXPIRATION DATE IS LESS THAN 6 MONTHS, 241 INFORM HHI-ENGINEERING FOR REPLACEMENT DISPOSITION. NOTE( I ) VENDOR RECOMMENDATION
emp emp
CHECK DOCTOR'S KIT (VENDOR MEDIFAN) EXPIRY DATE NOTED ON SEAL. 221 IF THE EXPIRATION DATE IS LESS THAN 6 MONTH INFORM 241 HHI-ENGINEERING FOR DISPLACEMENT DISPOSITION. NOTE( I ) VENDOR RECOMMENDATION (IF INSTALLED)
emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MRB
25-390-00 MSI 25-390-00 RTE:9
AMTOSS
25-64-00-90
MPD MRB
25-400-00 MSI 25-400-00 RTE:8
AMTOSS
25-64-00-200-801
MPD MRB
25-420-00 MSI 25-420-00 RTE:8
AMTOSS
25-64-00-90
MPD MRB
25-430-00 MSI 25-430-00 RTE:8
AMTOSS
25-64-00-90
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 2 YRS
S
HHI 737-700
2 30-nov-05
I: 24 MTH
S
HHI 737-700
4 22-mar-07
I: 6 MTH
S
HHI 737-700
2 23-jul-08
I: 6 MTH
S
HHI 737-700
2 23-jul-08
ATA: 25 - 64
Page 2 of 2
HHI R E V
ITEM 25 - 66 256600 71000
256601 00000
256601 20000
D
737-6
MAINTENANCE SCHEDULE
256601 40000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
DOOR-MOUNTED ESCAPE SYSTEM OPERATIONALLY CHECK, ON A SAMPLING BASIS, ONE DIFFERENT ESCAPE SLIDE DOOR UNTIL 10% OF ALL THE DOORS IN THE FLEET ARE COMPLETE WITHIN 12 YEARS. NO PARTICULAR DOOR CAN BE TESTED MORE THAN ONCE WITHIN THIS 12 YEAR PERIOD. CONTINUING MAINTENANCE REQUIREMENTS ARE TO BE DETERMINED BY EACH OPERATOR AND REGULATORY AGENCY.
221 222 241 242
831 834 841 844
MPD MRB
25-220-00 MSI 25-220-00 RTE:8
AMTOSS
25-66-00-71
VISUALLY CHECK THE EMERGENCY ESCAPE SLIDE PRESSURE BOTTLES 231 FOR PROPER PRESSURE 232 241 242
emp emp emp emp
MPD MRB
25-250-00 MSI 25-250-00 RTE:8
AMTOSS
25-66-01-20
INSPECT (DETAILED) THE ENTRY AND SERVICE DOOR EMERGENCY ESCAPE SYSTEM (AT ALL 4 DOORS) INCLUDING THE DOOR OPENINGS, THE EMERGENCY ESCAPE SLIDE COMPARTMENTS AND THE ESCAPE SLIDE COMPONENTS WITHOUT REMOVING THE ESCAPE SLIDE FOR CONDITION AND SECURITY.
831 834 841 844
MPD MRB
25-230-00 MSI 25-230-00 RTE:8
AMTOSS
25-66-01-20
221 222 241 242
I: 3 YRS
F1 HHI 737-700
3 30-nov-05
I: 90 DAY
E1 HHI 737-700
4 22-mar-07
I: 2 YRS
E3 HHI 737-700
1 03-jun-04
ITEM DELETED.
D
Date: 23-jul-08
TSK
2 23-jul-08
ITEMS
ATA: 25 - 66
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 25 - 71
257100 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ACCESSORY COMPARTMENTS INSPECT THE ELECTRONIC COMPARTMENT MOISTURE SHROUDS FOR 117 OBVIOUS CRACKS/TEARS, CLOGGED DRAINS, CONDITION AND SECURITY. 118
emp emp
ITEMS
MPD MRB
25-150-00 MSI 25-150-00 RTE:9
AMTOSS
25-71-00-21
I: 2 YRS
ATA: 25 - 71
E1 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 26 - 00
260000 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FIRE PROTECTION FIRE EXTINGUISHING SYSTEM VISUALLY CHECK THAT ALL PORTABLE FIRE EXTINGUISHERS, HALON 200 AND WATER ARE ON BOARD, PROPERLY STOWED, HANDLES SAFETIED AND THE POINTER OF THE PRESSURE GOUGE, IF INSTALLED, IS WITHIN THE GREEN RANGE.
emp
empty
AAR AAR AAR
ITEMS
NFL II 139/99 NFL II 96/79 NFL II 92/99
I: 1 Z
ATA: 26 - 00
E1 HHI 737-700
FC
1 13-apr-00
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 14
261400 73000
261401 10000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LAVATORY SMOKE DETECTION OPERATIONAL CHECK OF THE LAVATORY SMOKE DETECTORS.
RESTORE LAVATORY SMOKE DETECTOR GRILL BY CLEANING.
221 241 242
221 241 242
emp emp emp
emp emp emp
ITEMS
MPD MRB
26-010-00 MSI 26-010-00 RTE:8
AMTOSS
26-14-00-73
MPD MRB
26-020-00 MSI 26-020-00 RTE:9
AMTOSS
26-14-01-10
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
I: 6000 FLH
S
3 18-mar-05
ATA: 26 - 14
HHI 737-700
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 15
261500 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU FIRE DETECTION SYSTEM OPERATIONAL CHECK OF THE APU REMOTE FIRE DETECTION SYSTEM 117 (M279 FIRE DETECTION CONTROL MODULE AND P28 REMOTE APU 134 CONTROL PANEL). 210
117A emp emp
ITEMS
MPD MRB
26-030-00 MSI 26-030-00 RTE:8
AMTOSS
26-15-00-71
I: 12000 FLH
ATA: 26 - 15
F1 HHI 737-700
6 22-mar-07
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 20
262000 01000
262000 02000
262000 21000
262001 72000
262001 72100
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FIRE EXTINGUISHING SYSTEM CHECK ENGINE FIRE EXTINGUISHER SQUIBS FOR EXPIRATION DATE IS 133 REACHED DURING THE NEXT 6 MONTH, REPLACE THE SQUIB. THE EXPIRATION DATE IS THE MANUFACTURING DATE PLUS THE LIFE LIMIT. THE MANUFACTURING DATE IS STAMPED ON THE HEXHEAD OF THE SQUIB. THE LIFE LIMIT IS SHOWN IN THE CMS.
emp
CHECK APU FIRE EXTINGUISHER SQUIBS FOR EXPIRATION DATE. IF THE 311 EXPIRATION DATE IS REACHED DURING THE NEXT 6 MONTH, REPLACE THE SQUIB. THE EXPIRATION DATE IS THE MANUFACTURING DATE PLUS THE LIFE LIMIT. THE MANUFACTURING DATE IS STAMPED ON THE HEXHEAD OF THE SQUIB. THE LIFE LIMIT IS SHOWN IN THE CMS.
311BL
VISUALLY CHECK ENGINE FIRE BOTTLES PRESSURE GAUGE FOR CORRECT PRESSURE (AND APU FIRE BOTTLE PRESSURE GAUGE IF INSTALLED).
emp 311BL
133 311
OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER SYSTEM CHECK 133 VALVES FOR FREEDOM OF MOVEMENT. NOTE( I ) AT BOTTLE CHANGE
emp
FUNCTIONAL CHECK THE ENGINE FIRE EXTINGUISHER DISTRIBUTION SYSTEM (PRESSURE CHECK).
emp 413 414 415 416 423 424 425 426
133 411 emp emp emp 421 emp emp emp
ITEMS
MPD MRB
26-070-00 MSI 26-070-00 RTE:8
AMTOSS AMTOSS MS AMM
26-21-02-40 26-21-02-00 CM2621 00020 26-21-00
MPD MRB
26-210-00 MSI 26-210-00 RTE:8
AMTOSS AMTOSS MS AMM
26-22-02-40 26-22-02-00 CM2622 00020 26-22-00
MPD MRB
26-050-00 MSI 26-050-00 RTE:8
AMTOSS
26-20-00-21
MPD MRB
26-090-00 MSI 26-090-00 RTE:8
AMTOSS
26-21-00-720-801
MPD MRB
26-150-00 MSI 26-150-00 RTE:8
AMTOSS
26-21-00-730-803
I: 6 MTH
E1 HHI 737-700
3 03-jun-04
I: 6 MTH
E1 HHI 737-700
4 03-jun-04
I: 1800 FLH
E1 HHI 737-700
5 25-apr-06
I: 6000 FLH
F1 HHI 737-700
5 18-mar-05
I: 6000 FLH
F2 HHI 737-700
3 03-jun-04
ATA: 26 - 20
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
262001 72200
262001 73000
262002 21000
262003 21000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF ENGINE FIRE EXTINGUISHER DISTRIBUTION SYSTEM.
ZONE ACCESS
STRUCTURE
133 411 emp emp emp 421 emp emp emp
emp 413 414 415 416 423 424 425 426
MPD MRB
26-170-00 MSI 26-170-00 RTE:8
AMTOSS
26-21-01-21
FUNCTIONALLY TEST THE ENGINE AND APU FIRE CONTROL MODULE. THE FUNCTIONAL CHECK INCLUDES CHECKOUT OF THE FOLLOWING: ENGINE: - FUEL SHUTOFF VALVE - HYDRAULIC SUPPLY SHUTOFF VALVE - BLEED AIR VALVE - GENERATOR CONTROL RELAY - THRUST REVERSER VALVE, SQUIB FIRING CIRCUITS - FIRE HANDLE LOCK OVERRIDE APU: - FUEL SHUTOFF VALVE - GENERATOR CONTROL RELAY - SQUIB FIRING CIRCUITS - FIRE HANDLE LOCK OVERRIDE - P28 REMOTE APU CONTROL PANEL
133 134 210 212 311 emp 411 421
emp emp emp emp 311BL 315A 415 425
MPD MPD MPD MPD MRB
26-080-00 26-110-00 26-220-00 26-230-00 MSI 26-080-00 RTE:8 MSI 26-110-00 RTE:8 MSI 26-220-00 RTE:8 MSI 26-230-00 RTE:8
PERFORM A GENERAL VISUAL INSPECTION OF THE APU REMOTE CONTROL PANEL. CHECK FOR CONDITION AND SECURITY OF INSTALLATION.
134
MRB MRB MRB
PERFORM A DETAILED VISUAL INSPECTION OF THE APU FIRE 311 EXTINGUISHER DISTRIBUTION SYSTEM AND APU FIRE BOTTLE. 315 CHECK FOR CONDITION, SECURITY OF INSTALLATION, KINKED, CRACKED AND OBSTRUCTED TUBING.
emp
311BL 315A
ITEMS
THRESHOLD INTERVAL
REFERENCES
AMTOSS AMTOSS AMTOSS AMTOSS
26-21-00-730-801 25-21-00-720-802 26-22-00-730-801 26-22-00-720-801
MPD MRB
26-250-00 MSI 26-250-00 RTE:8
AMTOSS
26-22-03-21
MPD MRB
26-280-00 MSI 26-280-00 RTE:8
AMTOSS
26-22-01-21
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 6000 FLH
E2 HHI 737-700
2 03-jun-04
I: 6000 FLH
F2 HHI 737-700
7 05-sep-06
I: 6000 FLH
E2 HHI 737-700
2 03-jun-04
I: 6000 FLH
E3 HHI 737-700
4 03-jun-04
ATA: 26 - 20
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 23
262300 00650
262300 01000
262300 02000
262300 03000
262300 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EXTINGUISHING SYSTEM - CARGO COMPARTMENT CHECK THE EXPIRATION DATE OF THE FIRE EXTINGUISHER SQUIBS. 125 EXPIRATION DATE IS THE MANUFACTURING DATE PLUS 10 YEARS. 126 MANUFACTURING DATE IS STAMPED ON THE HEX FLAT OF THE SQUIB. IF THE EXPIRATION TIME IS LESS THAN 6 MONTH, REPLACE SQUIB. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
121HW emp
OPERATIONALLY CHECK THE CARGO FIRE EXTINGUISHING ARM AND DISCHARGE SWITCHES TO VERIFY CIRCUITRY. ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
125 126 210
121HW emp emp
FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHING 60-MINUTE TIMER. NOTE( J ) IF SECOND HALON BOTTLE INSTALLED ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
125 126 210
REPLACE THE CARGO COMPARTMENT FIRE EXTINGUISHER SYSTEM (FILTER/DRYER) NOTE( I ) AT FIRE EXTINGUISHER BOTTLE DISCHARGE ACCESS SPECIAL ACCESS REQUIRED REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
121 125 126
FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHER DISTRIBUTION SYSTEM (PRESSURE CHECK). ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED
121 122 125 141 142 145 146
121HW emp emp
121HW emp emp
121HW emp emp emp emp emp emp
ITEMS
MPD MRB
26-330-00 MSI 26-330-00 RTE:8
AMTOSS AMTOSS
26-23-02-000-801 26-23-02-400-801
MPD MRB
26-370-00 MSI 26-370-00 RTE:8
AMTOSS AMTOSS
26-23-00-730-801 26-23-00-730-802
MPD MRB
26-400-00 MSI 26-400-00 RTE:8
AMTOSS
26-23-00-730-801
MPD MRB
26-390-00 MSI 26-390-00 RTE:8
AMTOSS AMTOSS
26-23-04-40 26-23-04-00
MPD MRB
26-340-00 MSI 26-340-00 RTE:8
AMTOSS AMTOSS
26-23-00-73 26-23-00-72
I: 6 MTH
E1 HHI 737-700
2 05-sep-06
I: 6000 FLH
F1 HHI 737-700
6 05-sep-06
I: 6000 FLH
F2 HHI 737-700
6 05-sep-06
I: 1 s.N
S
HHI 737-700
5 05-sep-06
I: 12000 FLH
F2 HHI 737-700
4 22-mar-07
ATA: 26 - 23
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
262300 05000
Date: 23-jul-08
DESCRIPTION FUNCTIONALLY CHECK THE CARGO FIRE EXTINGUISHER BOTTLE PRESSURE SWITCH. NOTE( I ) AT HYDROSTATIC TEST. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
ZONE ACCESS 125 126
STRUCTURE
121HW emp
ITEMS
REFERENCES MPD MRB
26-360-00 MSI 26-360-00 RTE:9
AMTOSS
26-23-00-73
THRESHOLD INTERVAL
I: 1 s.N
ATA: 26 - 23
TSK
EFF
F2 HHI 737-700
R L ITEM BY E E REVISION P V DATE
3 05-sep-06
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 24
262401 00000
262401 01000
262401 90000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LAVATORY WASTE COMPARTMENT FIRE EXTINGUISHING DETAILED VISUAL INSPECTION OF THE LAVATORY FIRE BOTTLE FUSIBLE 221 TIPS AND DISCHARGE TUBES 241 242
VISUAL CHECK OF LAVATORY WASTE COMPARTMENT TEMPERATURE 221 INDICATOR STRIP FOR HEAT EXPOSURE. 241 242
REMOVE LAVATORY FIRE BOTTLE FOR WEIGHT CHECK. NOTE( I ) VENDOR RECOMMENDATION
221 241 242
emp emp emp
emp emp emp
emp emp emp
ITEMS
MPD MRB
26-300-00 MSI 26-300-00 RTE:9
AMTOSS
26-24-01-20
MPD MRB
26-320-00 MSI 26-320-00 RTE:9
AMTOSS
26-24-01-21
MPD MRB
26-290-00 MSI 26-290-00 RTE:9
AMTOSS
26-24-01-90
I: 3600 FLH
E3 HHI 737-700
4 25-apr-06
I: 1200 FLH
E1 HHI 737-700
4 25-apr-06
I: 5 YRS
S
3 03-jun-04
ATA: 26 - 24
HHI 737-700
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 26 - 25
262500 01000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PORTABLE FIRE EXTINGUISHER CHECK THAT ALL PORTABLE FIRE EXTINGUISHERS ARE PROPERLY 200 STOWED, HANDLES SAFETIED, PRESSURE GAUGE (IF INSTALLED) IS IN GREEN RANGE AND THE INSCRIBTION IS LEGIBLE. VISUALLY INSPECT THE STOWAGE BRACKET FOR CONDITION AND SECURITY OF INSTALLATION. REMOVE THE CONTROL AND PASSENGER CABIN FIRE EXTINGUISHERS FOR WEIGHT CHECK. NOTE( J ) THIS INCLUDES ALL TYPES OF PORTABLE FIRE EXTINGUISHERS.
emp
MPD MPD MPD MPD MRB MRB MRB MRB AAR AAR AAR AMM
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
26-450-00 26-470-00 26-490-00 26-510-00 MSI 26-450-00 RTE:8 MSI 26-470-00 RTE:8 MSI 26-490-00 RTE:8 MSI 26-510-00 RTE:8 NFL II 139/99 NFL II 96/79 NFL II 92/99 26-26-01
I: 12 MTH
ATA: 26 - 25
E3 HHI 737-700
4 03-jun-04
Page 1 of 1
HHI R E V
ITEM 27 27 - 00
R
737-6
MAINTENANCE SCHEDULE
270000 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
LUBRICATE THE STABILIZER TRIM ACTUATOR AND ACTUATOR GIMBAL 311 PINS AND BALLNUT. 312
311BL emp
MPD MRB
R L ITEM BY E E REVISION P V DATE
LUBRICATE THE LEFT AND RIGHT WING FLAP TRANSMISSION UNIVERSAL JOINTS AND BALLSCREW ACTUATORS. ACCESS FLAPS DEPLOYED
27-102-00 MSI 27-102-00 RTE:6 MSI 27-102-00 RTE:8
SB AMTOSS
737-27A1277 R1 12-22-41-600-801 27-144-00 27-146-00 MSI 27-144-00 RTE:6 MSI 27-146-00 RTE:6
133 134 210 541 542 543 544 553 641 642 643 644 653
emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS AMTOSS AMTOSS AMTOSS
12-22-51-640-805 12-22-51-640-804 12-22-51-640-803 12-22-51-640-802
LUBRICATE THE #4 AND #5 FLAP TRANSMISSION ANGLE/TEE GEARBOX 133 UNIVERSAL JOINTS. 134 553 653
emp emp emp emp
MPD MPD MRB
27-152-01 27-152-02 MSI 27-152-01 RTE:6 MSI 27-152-02 RTE:6
MRB
MRB AMTOSS
Date: 23-jul-08
EFF
GENERAL
R
270000 02000
TSK
FLIGHT CONTROL
MRB
270000 01000
THRESHOLD INTERVAL
REFERENCES
ITEMS
12-22-51-640-806
I: 1600 FLH I: 8 MTH
S
HHI 737-700
8 23-jul-08
I: 1000 CYC
S
HHI 737-700
4 03-jun-04
I: 12 MTH I: 2000 CYC
S
HHI 737-700
4 03-jun-04
ATA: 27 - 00
Page 1 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 03000
270000 04000
Date: 23-jul-08
DESCRIPTION LUBRICATE THE LEFT AND RIGHT TRAILING EDGE FLAP ACTUATION MECHANISM. ACCESS FLAPS DEPLOYED
LUBRICATE THE RIGHT AND LEFT WING AILERON MECHANICAL CONTROL PATH AND AILERON POWER CONTROL UNITS. NOTE( R ) ACCOMPLISH THE LUBRICATION OF THE AILERON TAB HINGES IN ACCORDANCE WITH AD 2006-21-01 AND SB 737-27-1273 (EO 154339).
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
133 134 emp 541 542 543 544 553 561 567 641 642 643 644 653 661 667
emp 194BL 194BR emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS
12-22-51-640-811 12-22-51-640-812 12-22-51-640-813 12-22-51-640-814 12-22-51-640-815 12-22-51-640-816
133 134 572 emp emp emp emp emp 672 emp emp emp emp emp
571BB 671BB 572AB 572CB 572DB 572FB 572GB 572HB 672AB 672CB 672DB 672FB 672GB 672HB
MPD MPD MRB
27-026-01 27-026-02 MSI 27-026-01 RTE:6 MSI 27-026-01 RTE:8 MSI 27-026-02 RTE:6
ITEMS
MRB
MRB MRB AAR EO SB AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-170-01 27-170-02 MSI 27-170-01 RTE:6 MSI 27-170-02 RTE:6
AD 2006-21-01 154339 737-27-1273 12-22-11-640-804 12-22-11-640-803 12-22-11-640-802 12-22-11-600-801 12-22-11-640-801
I: 8 MTH I: 1250 CYC
S
HHI 737-700
6 03-jun-04
I: 4000 FLH I: 12 MTH
S
HHI 737-700
6 22-mar-07
ATA: 27 - 00
Page 2 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 05000
270000 06000
DESCRIPTION
ZONE ACCESS
LUBRICATE THE LEFT WING #S 1, 2 AND 3 AND THE RIGHT WING #S 6, 7 542 AND 8 TRAILING EDGE FLAP TRACK FORWARD ATTACHMENT POINT PINS. 543 544 642 643 644
LUBRICATE THE LEFT WING #4 AND THE RIGHT WING #5 INBOARD FLAP 553 TRACK ATTACHMENT FITTINGS. 653
STRUCTURE
542AB 543AB 544AB 642AB 643AB 644AB
emp emp
MPD MPD MRB MRB
Date: 23-jul-08
LUBRICATE THE SPOILER MIXER, THE LEFT WING AND RIGHT WING SPOILER MECHANICAL CONTROL PATH. ACCESS FLAPS DEPLOYED
134 552 562 563 564 565 566 652 662 663 664 665 666
emp emp emp emp emp emp emp emp emp emp emp emp emp
12-22-51-640-816 12-22-51-640-815 12-22-51-640-814
MPD MPD MRB
27-176-01 27-176-02 MSI 27-176-01 RTE:5 MSI 27-176-02 RTE:5
ITEMS
AMTOSS
12-22-51-640-813
MPD MPD MPD MRB
27-182-00 27-182-01 27-182-02 MSI 27-182-00 RTE:6 MSI 27-182-01 RTE:6 MSI 27-182-02 RTE:6
MRB MRB AMTOSS AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-174-01 27-174-02 MSI 27-174-01 RTE:6 MSI 27-174-02 RTE:6
AMTOSS AMTOSS AMTOSS
MRB
270000 07000
THRESHOLD INTERVAL
REFERENCES
12-22-61-600-802 12-22-61-640-801 12-22-61-600-801
I: 4000 CYC
S
HHI 737-700
3 03-jun-04
I: 1000 CYC
S
HHI 737-700
3 03-jun-04
I: 4000 FLH
S
HHI 737-700
3 03-jun-04
ATA: 27 - 00
Page 3 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 08000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
LUBRICATE THE LEFT AND RIGHT WING LEADING EDGE SLAT ROLLERS. 522 523 ACCESS 524 LEADING EDGES EXTENDED 525 emp emp emp emp emp emp emp 622 623 624 625 emp emp emp emp emp emp emp
STRUCTURE
emp emp emp 521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621HB 621LB 621PB 621SB 621VB 621YB
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MPD MRB MRB AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-220-01 27-220-02 MSI 27-220-01 RTE:6 MSI 27-220-02 RTE:6 12-22-71-600-801
I: 1250 CYC I: 8 MTH
ATA: 27 - 00
S
HHI 737-700
5 03-jun-04
Page 4 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 09000
270000 10000
270000 11000
DESCRIPTION
ZONE ACCESS
STRUCTURE
LUBRICATE THE LEFT AND RIGHT WING LEADING EDGE SLAT TRACKS. 522 523 ACCESS 524 LEADING EDGES EXTENDED 525 emp emp emp emp emp emp emp 622 623 624 625 emp emp emp emp emp emp emp
emp emp emp 521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621HB 621LB 621PB 621SB 621VB 621YB
MPD MPD MRB
AMTOSS
12-22-71-640-801
LUBRICATE THE RUDDER FEEL AND CENTERING UNIT SPRING SLIDER. 211 212 324
emp emp 324CL
MPD MRB
27-040-00 MSI 27-040-00 RTE:5
AMTOSS
12-22-21-600-802
MPD MRB
27-046-00 MSI 27-046-00 RTE:8 MSI 27-046-00 RTE:9
LUBRICATE THE MAIN AND STANDBY RUDDER POWER CONTROL UNIT 324 ROD ENDS AND RUDDER HINGES.
324DL
MRB
MRB AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-222-01 27-222-02 MSI 27-222-01 RTE:6 MSI 27-222-02 RTE:6
12-22-21-640-801 12-22-21-600-801
I: 2500 CYC I: 16 MTH
S
HHI 737-700
6 03-jun-04
I: 6000 FLH
S
HHI 737-700
3 18-mar-05
I: 6000 FLH
S
HHI 737-700
4 18-mar-05
ATA: 27 - 00
Page 5 of 10
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
270000 12000
R
270000 13000
DESCRIPTION LUBRICATE THE ELEVATOR MECHANICAL CONTROL PATH.
ZONE ACCESS 334 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 344
LUBRICATE THE FORWARD STABILIZER TRIM MECHANISM (STABILIZER 112 CHAIN AND FLEXIBLE SHAFT).
STRUCTURE
315A 333AT 333BB 333CB 333DB 333EB 334AB 334BB 334GB 334HB 334JB 334KB 334MB 334NB 343AT 343BB 343CB 343DB 343EB 344AB 344BB 344GB 344HB 344KB 344MB 344NB 344JB
MPD MRB
AMTOSS AMTOSS AMTOSS
12-22-31-640-802 12-22-31-640-801 12-22-31-600-801
112A
MPD MRB
27-104-00 MSI 27-104-00 RTE:6 MSI 27-104-00 RTE:9
MPD MRB
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-070-00 MSI 27-070-00 RTE:6 27-070-00 MSI 27-070-00 RTE:6
12-22-41-600-802
I: 6000 FLH
S
HHI 737-700
5 23-jul-08
I: 25000 FLH
S
HHI 737-700
2 03-jun-04
ATA: 27 - 00
Page 6 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 14000
270000 15000
270000 16000
DESCRIPTION
ZONE ACCESS
CHECK FLAP POWER DRIVE UNIT OIL LEVEL AND SERVICE AS REQUIRED. 133 134
REPLACE THE FLAP POWER DRIVE UNIT OIL.
LUBRICATE LEFT AND RIGHT WING FLAP SKEW SENSOR MECHANISM. ACCESS FLAPS DEPLOYED
133 134
553 567 653 667
STRUCTURE
emp emp
emp emp
emp emp emp emp
MPD MRB
27-132-00 MSI 27-132-00 RTE:6
AMTOSS
12-22-51-610-801
MPD MRB
27-134-00 MSI 27-134-00 RTE:6
AMTOSS
12-22-51-610-802
MPD MPD MRB
27-136-01 27-136-02 MSI 27-136-01 RTE:6 MSI 27-136-02 RTE:6
MRB
270000 17000
LUBRICATE THE FLAP DRIVE TORQUE TUBES COUPLINGS AND TORQUE TUBE SUPPORTS. ACCESS FLAPS DEPLOYED
133 134 553 567 653 667
emp emp emp emp emp emp
AMTOSS AMTOSS AMTOSS AMTOSS
12-22-51-640-810 12-22-51-640-809 12-22-51-640-808 12-22-51-640-807
MPD MPD MRB
27-138-00 27-150-00 MSI 27-138-00 RTE:6 MSI 27-150-00 RTE:6
MRB AMTOSS
Date: 23-jul-08
ITEMS
THRESHOLD INTERVAL
REFERENCES
12-22-51-640-801
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 5000 CYC
S
HHI 737-700
2 03-jun-04
I: 25000 CYC
S
HHI 737-700
2 03-jun-04
I: 24 MTH I: 4000 FLH
S
HHI 737-700
2 03-jun-04
I: 24 MTH I: 4800 CYC
S
HHI 737-700
5 22-mar-07
ATA: 27 - 00
Page 7 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
270000 18000
270000 19000
270000 20000
270000 21000
Date: 23-jul-08
DESCRIPTION CHECK THE LEFT AND RIGHT WING FLAP DRIVE TRANSMISSION OIL LEVEL AND SERVICE AS REQUIRED. ACCESS FLAPS DEPLOYED
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
133 134 210 541 542 543 544 641 642 643 644
emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS
12-22-51-610-803
REPLACE THE LEFT AND RIGHT WING FLAP DRIVE TRANSMISSION OIL. 133 134 ACCESS 211 FLAPS DEPLOYED 212 541 542 543 544 553 641 642 643 644 653
emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
27-142-01 27-142-02 MSI 27-142-01 RTE:6 MSI 27-142-01 RTE:8 MSI 27-142-02 RTE:6 MSI 27-142-02 RTE:8
AMTOSS
12-22-51-610-804
CHECK ALTERNATE FLAP DRIVE GEARBOX OIL LEVEL AND SERVICE AS 133 REQUIRED. 134
emp emp
MPD MRB
27-178-00 MSI 27-178-00 RTE:9
AMTOSS
12-22-51-610-805
MPD MRB
27-186-00 MSI 27-186-00 RTE:6
AMTOSS
12-22-81-600-801
LUBRICATE THE SPEEDBRAKE LEVER NO-BACK BRAKE.
112
112A
ITEMS
MRB MRB MRB
MRB MRB MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-140-01 27-140-02 MSI 27-140-01 RTE:6 MSI 27-140-01 RTE:8 MSI 27-140-02 RTE:6 MSI 27-140-02 RTE:8 I: 5000 CYC
S
HHI 737-700
3 03-jun-04
I: 25000 CYC
S
HHI 737-700
2 03-jun-04
I: 6000 FLH
S
HHI 737-700
3 18-mar-05
I: 6000 FLH
S
HHI 737-700
3 18-mar-05
ATA: 27 - 00
Page 8 of 10
HHI R E V
R
737-6
MAINTENANCE SCHEDULE DESCRIPTION
270000 22000
PERFORM A DETAIL VISUAL INSPECTION OF ALL EXPOSED PORTIONS OF THE FLIGHT CONTROL CABLES RUNS. ACCESS EXTEND FLAPS
133 134 210 550 emp 561 571 660 emp 661 671
emp emp emp 551CT 551DB emp 571BB 651CT 651DB emp 671BB
MPD MRB
27-226-00 MSI 27-226-00 RTE:6
AMTOSS AMTOSS AMTOSS
20-20-31-200-805 20-20-31-200-802 20-20-31-200-801
PERFORM A DETAIL VISUAL INSPECTION OF ALL INTERNAL PORTIONS OF THE FLIGHT CONTROL CABLE RUNS. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD. FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540. AFT CARGO COMPARTMENT CEILING PANELS AFT CARGO COMPARTMENT AFT BULKHEAD PANELS AND WATER TANK, OR THE PRESSURIZATION AFT OUTFLOW VALVE ASSEMBLY.
112 113 emp emp 114 emp emp 117 118 121 122 125 126 137 138 141 142 145 146 300 311 312 313 314 317 318 323
112A 113AC 113AW 113BW 114AC 114AW 114BW 117A emp 821 emp emp emp emp emp 822 emp emp emp emp 311BL emp emp emp 317AL 318BR 323FL
MPD MRB
27-228-00 MSI 27-228-00 RTE:6
AMTOSS AMTOSS AMTOSS
20-20-31-200-802 20-20-31-200-805 20-20-31-200-801
270000 25000
R
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
ITEM
ITEMS
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 4800 CYC I: 24 MTH
E3 HHI 737-700
6 23-jul-08
I: 21600 CYC I: 6 YRS
E3 HHI 737-700
5 23-jul-08
ATA: 27 - 00
Page 9 of 10
HHI R E V
ITEM
DESCRIPTION
R
270000 32000
PERFORM A DETAIL VISUAL INSPECTION OF ALL FLIGHT CONTROL CABLES THAT ARE OVER THE CENTER WING SECTION B.S. 540 TO B.S. 663.75 AND CABLES WITHIN PILOT'S CONTROL QUADRANT. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 540 TO B.S. 663.75.
ZONE ACCESS 135 136 211 emp 212
STRUCTURE
emp emp 211A 211B emp
R
N
737-6
MAINTENANCE SCHEDULE
270000 35000
INSPECT (DETAILED) INBOARD TRAILING EDGE AFT FLAP DRIVE CABLE. 553 653
553BB 653BB
N
Date: 23-jul-08
ITEMS
THRESHOLD INTERVAL
REFERENCES MRB MPD MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MSI 27-230-00 RTE:6 27-230-00 MSI 27-230-00 RTE:6
AMTOSS AMTOSS AMTOSS
20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
MPD MRB
27-229-00 MSI 27-229-00 FEC:6
AMM AMM AMM
20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
6 23-jul-08
T: 21600 CYC T: 6 YRS I: 21600 CYC I: 6 YRS
E3 HHI 737-700
0 23-jul-08
ATA: 27 - 00
Page 10 of 10
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 11
271100 21000
271100 21100
DESCRIPTION
ZONE ACCESS
STRUCTURE
271100 71100
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AILERON AND FLAPERON CONTROL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE FORWARD AILERON 112 MECHANICAL COMPONENTS FROM CONTROL WHEEL TO AILERON BUS 211 DRUMS. 212
PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING AILERON MECHANICAL COMPONENTS FROM THE AILERON PCU'S TO THE AILERON AND THE FLIGHT SPOILER MECHANICAL CONTROL PATH.
133 134 572 672
112A emp emp
emp emp 572BB 672BB
MPD MRB
27-011-00 MSI 27-011-00 RTE:6
AMTOSS
27-11-00-210-801
MPD MPD MRB
27-013-01 27-013-02 MSI 27-013-01 RTE:6 MSI 27-013-02 RTE:6
MRB
271100 71000
THRESHOLD INTERVAL
REFERENCES
OPERATIONALLY CHECK THE AILERON SPRING CARTRIDGE AND TRANSFER MECHANISM.
130 211 212
FUNCTIONALLY CHECK THE AILERON SPRING CARTRIDGE AND TRANSFER 133 MECHANISM. 134 211 212
emp emp emp
emp emp emp emp
ITEMS
AMTOSS
27-11-00-210-802
MPD MRB
27-016-00 MSI 27-016-00 RTE:8
AMTOSS
27-11-00-710-802
MPD MRB
27-018-00 MSI 27-018-00 RTE:8
AMTOSS
27-11-00-700-806
I: 4000 FLH
E1 HHI 737-700
4 03-jun-04
I: 4000 FLH
E1 HHI 737-700
5 03-jun-04
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 25000 FLH
F2 HHI 737-700
3 03-jun-04
ATA: 27 - 11
Page 1 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
271100 73000
271100 82000
271101 70000
271101 70100
271101 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
FUNCTIONALLY CHECK THE LEFT AND RIGHT WING AILERON SURFACE 210 AND AILERON TAB FREEPLAY. 572 672 NOTE( R ) ACCOMPLISH THE AILERON TAB FREEPLAY CHECK IN ACCORDANCE WITH AD 2006-21-01 AND SB 737-27-1273 (EO 154339).
PERFORM A DETAILED VISUAL INSPECTION OF THE AILERON FEEL AND 133 CENTERING SPRINGS.
STRUCTURE
emp emp emp
MPD MPD MRB MRB
emp
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
27-033-00 27-035-00 MSI 27-033-00 RTE:8 MSI 27-035-00 RTE:8
AAR EO SB AMTOSS
AD 2006-21-01 154339 737-27-1273 27-09-91-200-801
MPD MRB
27-028-00 MSI 27-028-00 RTE:6
AMTOSS
27-11-81-210-801
OPERATIONALLY CHECK (HYDRAULIC POWER OFF) THE AILERON 133 CONTROL SURFACES FOR FULL RANGE OF TRAVEL AND FREEDOM OF 134 MOVEMENT. 211 212
emp emp emp emp
MPD MRB
27-030-00 MSI 27-030-00 RTE:8
AMTOSS
27-11-00-700-807
FUNCTIONALLY CHECK THE AILERON SYSTEM CONTROL WHEEL FORCES. 133 134 211 212
emp emp emp emp
MPD MRB
27-032-00 MSI 27-032-00 RTE:8
AMTOSS
27-11-00-700-803
FUNCTIONALLY CHECK THE FORCE REQUIRED TO EXTEND AND 133 COLLAPSE THE A AND B SYSTEM AILERON POWER CONTROL UNIT INPUT 134 POGO'S. 211 212
emp emp emp emp
MPD MRB
27-022-00 MSI 27-022-00 RTE:8
AMTOSS
27-11-00-720-801
ITEMS
TSK
I: 8000 FLH I: 24 MTH
F2 HHI 737-700
3 22-mar-07
I: 6000 FLH
E3 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
I: 25000 FLH
F2 HHI 737-700
2 03-jun-04
I: 12500 FLH
F2 HHI 737-700
3 03-jun-04
ATA: 27 - 11
Page 2 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
271101 72000
271131 21000
DESCRIPTION
ZONE ACCESS
FUNCTIONALLY CHECK THE A AND B SYSTEM AILERON POWER CONTROL 133 UNIT INTERNAL LEAKAGE IN A LOADED CONDITION. 134 211 212
PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING AILERON BALANCE BAY SEALS.
572 emp emp 672 emp emp
STRUCTURE
emp emp emp emp
571BB 571CB 571DB 671BB 671CB 671DB
MPD MRB MRB
29-00-00-790-804
MPD MPD MRB
27-034-01 27-034-02 MSI 27-034-01 RTE:8 MSI 27-034-02 RTE:8
MRB
Date: 23-jul-08
CHECK UPPER AND LOWER SIDE OF LEFT AND RIGHT AILERON BALANCE PANELS FOR DEICING / ANTI-ICING FLUID RESIDUE AND CLEAN IF NECESSARY. METHOD 1 USE A SUITABLE FLEXISCOPE AND CHECK UPPER AND LOWER SIDE OF ALL BALANCE PANELS AND AFT PANEL HINGE AREA THROUGH GAPS BETWEEN AILERON AND FIXED TRAILING EDGE AS FAR AS POSSIBLE; OR METHOD 2 OPEN LOWER ACCESS PANELS 571BB/671BB TO BALANCE BAY 4, DISCONNECT AFT END OF BALANCE PANEL AND CHECK UPPER AND LOWER SIDE OF BALANCE PANEL. IF NO CONTAMINATION IS FOUND NO OTHER BALANCE PANELS HAVE TO BE CHECKED. IF CONTAMINATION IS EVIDENT OPEN OTHER ACCESS PANELS TO REMAINING BALANCE BAYS FOR INSPECTION. NOTE( J ) THIS ITEM IS EFFECTIVE FROM OCT01 UNTIL MAR 31.
572 emp emp 672 emp emp
571BB 571CB 571DB 671BB 671CB 671DB
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-024-00 MSI 27-024-00 RTE:6 MSI 27-024-00 RTE:9
AMM
AMTOSS 271131 22000
THRESHOLD INTERVAL
REFERENCES
I: 12500 FLH
F2 HHI 737-700
0 30-nov-05
27-11-31-210-801
I: 8000 FLH I: 3 YRS
E3 HHI 737-700
3 03-jun-04
737-SL-12-014
I: 450 FLH
E3 HHI S 737-700
2 29-apr-03
empty
SIL
ATA: 27 - 11
Page 3 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
271161 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A GENERAL VISUAL INSPECTION OF THE AILERON TRANSFER 112 MECHANISM.
STRUCTURE
112A
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MRB
27-012-00 MSI 27-012-00 RTE:8
AMTOSS
27-11-61-210-801
I: 6000 FLH
ATA: 27 - 11
TSK
EFF
E1 HHI 737-700
R L ITEM BY E E REVISION P V DATE
3 18-mar-05
Page 4 of 4
HHI R E V
ITEM 27 - 21
R
737-6
MAINTENANCE SCHEDULE
272100 03000
R
272100 60000
272100 65000
272100 80000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
RUDDER CONTROL SYSTEM FUNCTIONALLY CHECK THE RUDDER POWER CONTROL UNIT INTERNAL LEAKAGE IN A LOADED CONDITION. NOTE( I, R, E ) NOTE (R): THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT TASK 27-CMR-03. NOTE (E): APPLICABLE TO AIRPLANE LINE NUMBERS 1-595 AND 597-1267 THAT HAVE NOT INCORPORATED SB 737-27-1253. NOTE (I): MSG-3 ANALYSIS FOR THIS ATSK IS 12500 FLH. CMR INTERVAL FOR THIS TASK IS 8000 FLH (SEE MPD SECTION9).
117 133 134 211 212 325
emp emp emp 117A emp 324DR
AAR
AMTOSS AMTOSS
27-21-00-700-822-001 I: 8000 FLH 27-21-00-700-821-001
REMOVE RUDDER PCU AND TEST PCU ACCORDING PARKER SB 381500-27-01. NOTE( J ) ITEM FOR COMPLETENESS ONLY COVERED BY COSL. P/N S251A301-1 P/N S251A301-2
324
emp
AAR
AD 99-11-05
AAR SB
LTA 1999-278 737-27A1222
OPERATIONAL CHECK OF THE MAIN RUDDER PCU FORCE FIGHT 210 MONITOR. 325 emp NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBERS 596, 1268 AND ON AND LINE NUMBERS 1 -595 AND 597 - 1267 THAT HAVE INCORPORATED SB 737-27-1253.
emp 324CL 324EL
OPERATIONAL CHECK OF THE RUDDER PCU OVERRIDES. 210 325 NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBERS 596, 1268 AND ON AND LINE emp NUMBERS 1 - 595 AND 597 - 1267 THAT HAVE INCORPORATED SB 737-27-1253.
emp 324BL 324DL
ITEMS
MPD MRB
27-CMR-03 ONE STAR 27-044-00 MSI 27-044-00 RTE:8 F2 HHI 737-700
7 23-jul-08
I: 24000 FLH
M1 HHI 737-700
1 29-apr-03
MPD MRB
27-041-00 MSI 27-041-00 RTE:9
AMTOSS
27-21-00-700-824-002 I: 10000 FLH
F1 HHI 737-700
2 18-mar-05
MPD MRB
27-043-00 MSI 27-043-00 RTE:8
AMTOSS
27-21-00-700-823-002 I: 12500 FLH
F1 HHI 737-700
1 03-jun-04
ATA: 27 - 21
Page 1 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
272100 85000
272100 86000
272100 87000
272101 70000
272102 70000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
FUNCTIONAL CHECK OF THE RUDDER POWER CONTROL UNIT INTERNAL 133 LEAKAGE IN A LOADED CONDITION. 134 325 NOTE( I, E ) NOTE (E): APPLICABLE TO AIRPLANES LINE NUMBER 596 AND 1268 AND ON AND LINE NUMBERS 1-595 AND 597-1267 THAT HAVE INCORPORATED SB 737-27-1253. NOTE (I): MSG-3 ANALYSIS FOR THIS TASK IS 12500 FLH. CMR INTERVAL FOR THIS TASK IS 10000 FLH (SEE MPD SECTION 9).
emp emp 324DL
OPERATIONALLY CHECK THE RUDDER PCU PRESSURE REDUCING VALVE. 134 AIRPLANE NOTE: APPLICABLE TO AIRPLANES L/N 1-595 AND 597-1267 135 THAT HAVE NOT INCORPORATED SB737-27-1253. 325 NOTE( E ) APPLICABLE TO AIRPLANES L/N 1-595 AND 597-1267 THAT HAVE NOT INCORPORATED SB737-27-1253.
emp emp emp
FUNCTIONALLY CHECK THE RUDDER PCU RELIEF VALVE (AUTHORITY 131 LIMITER) DURING RUDDER PCU INTERNAL LEAKAGE. 134 325 NOTE( R, E ) NOTE: (R) THIS TASK IS SATISFIED BY ACCOMPLISHMENT OF TASK 27-047-00. NOTE: (E) APPLICABLE TO AIRPLANES LINE NUMBER 596; AND 1268 AND ON; AND L/N 1-595 AND 597-1267 WITH INCORPORATION OF SB 737-27-1253.
emp emp 324DL
OPERATIONALLY CHECK THE WHEEL TO RUDDER INTERCONNECT SYSTEM (WTRIS).
emp emp
211 212
OPERATIONALLY CHECK THE RUDDER TRIM THROUGH THE FULL RANGE 211 OF MOVEMENT.
STRUCTURE
THRESHOLD INTERVAL
REFERENCES AAR MPD MRB
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
27-CMR-10 ONE STAR 27-047-00 MSI 27-047-00 RTE:8
AMTOSS
27-21-00-700-822-002 I: 10000 FLH
MPD MRB
27-050-00 MSI 27-050-00 RTE:8
AMM
27-21-00-700-821-001 I: 8000 FLH
MPD MRB
27-048-00 MSI 27-048-00 RTE:8 I: 10000 FLH
emp
TSK
MPD MRB
27-060-00 MSI 27-060-00 RTE:8
AMTOSS AMTOSS
27-21-00-700-820-002 I: 6000 FLH 27-21-00-700-820-001
MPD MRB
27-062-00 MSI 27-062-00 RTE:9
AMTOSS AMTOSS
27-21-00-700-819-002 I: 6000 FLH 27-21-00-700-819-001
ATA: 27 - 21
F2 HHI 737-700
4 25-apr-06
F1 HHI 737-700
3 05-sep-06
F2 HHI 737-700
0 05-sep-06
F1 HHI 737-700
4 18-mar-05
F1 HHI 737-700
4 18-mar-05
Page 2 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
272103 70000
272124 21000
272124 22000
272151 21000
272161 21000
Date: 23-jul-08
DESCRIPTION FUNCTIONALLY CHECK THE RUDDER SURFACE FREEPLAY.
ZONE ACCESS 325
PERFORM A GENERAL VISUAL INSPECTION OF THE STANDBY RUDDER 211 POWER CONTROL UNIT WITH HYDRAULIC POWER ON. 325
PERFORM A DETAILED VISUAL INSPECTION OF THE STANDBY RUDDER 325 POWER CONTROL UNIT FORE AND AFT ATTACHMENT POINTS (STRUCTURE TO PCU TO RUDDER SURFACE).
GENERAL VISUAL INSPECTION OF THE RUDDER FORWARD MECHANICAL 112 CONTROL PATH.
DETAILED INSPECTION OF AFT RUDDER QUADRANT, TORQUE TUBE 320 ASSEMBLY, FEEL AND CENTERING UNIT AND ASSOCIATED INPUT/OUTPUT 325 RODS. emp - AFT QUADRANT - AFT QUADRANT OUTPUT ROD - AFT QUADRANT BEARINGS - AFT QUADRANT SHAFT - RUDDER TORQUE TUBE - RUDDER TORQUE TUBE BEARINGS - RUDDER TORQUE TUBE CRANKS - RUDDER TORQUE TUBE INPUT RODS - FEEL AND CENTERING UNIT - FEEL AND CENTERING UNIT OUTPUT ROD
STRUCTURE
emp
emp 324DL
emp
112A
324CL 323FL 324DL
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MRB
27-064-00 MSI 27-064-00 RTE:8
AMTOSS
27-21-00-700-814
MPD MRB
27-056-00 MSI 27-056-00 RTE:8
AMTOSS
27-21-24-210-801
MPD MRB
27-058-00 MSI 27-058-00 RTE:8
AMTOSS
27-21-24-210-802
MPD MRB
27-038-00 MSI 27-038-00 RTE:5
AMTOSS
27-21-51-210-801
MPD MRB
27-036-00 MSI 27-036-00 RTE:8
AMTOSS
27-21-61-210-801
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 8000 FLH
F2 HHI 737-700
3 03-jun-04
I: 5000 FLH
E1 HHI 737-700
2 03-jun-04
I: 6000 FLH
E3 HHI 737-700
4 18-mar-05
I: 6000 FLH
E1 HHI 737-700
3 18-mar-05
I: 6000 FLH
E3 HHI 737-700
6 05-sep-06
ATA: 27 - 21
Page 3 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
272171 00000
272182 00000
Date: 23-jul-08
DESCRIPTION PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER SINGLE ELEMENT DUAL LOAD PATH RUDDER PCU INPUT COMPONENTS.
PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER SINGLE ELEMENT DUAL LOAD PATH FEEL AND CENTERING COMMAND AND GROUND PATH COMPONENTS.
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
324 emp emp emp
323CL 323FL 324BL 324DL
MPD MRB
27-066-00 MSI 27-066-00 RTE:8
AMTOSS
27-21-61-210-801
324 emp emp 325
323CL 323FL 324DL emp
MPD MRB
27-065-00 MSI 27-065-00 RTE:8
AMTOSS
27-21-61-210-801
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 6 YRS
E3 HHI 737-700
5 03-jun-04
I: 6 YRS
E3 HHI 737-700
5 03-jun-04
ATA: 27 - 21
Page 4 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 31
273100 01000
273100 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
273100 72000
273100 73000
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ELEVATOR CONTROL SYSTEM PERFORM A BITE CHECK OF THE ELEVATOR AUTOPILOT SERVO PRESSURE REGULATOR.
211 212
OPERATIONALLY CHECK, HYDRAULIC POWER OFF, THE ELEVATOR 211 CONTROL SURFACES FOR FULL RANGE OF TRAVEL AND FREEDOM OF 212 MOVEMENT.
emp emp
311BL emp
MPD MRB
27-094-00 MSI 27-094-00 RTE:9
AMTOSS
22-11-26-710-801
MPD MRB
27-074-00 MSI 27-074-00 RTE:6 MSI 27-074-00 RTE:9
MRB
273100 71000
THRESHOLD INTERVAL
REFERENCES
FUNCTIONALLY CHECK THE ELEVATOR SURFACE FREEPLAY.
FUNCTIONALLY CHECK THE FORCE NECESSARY TO BREAKOUT THE ELEVATOR CONTROL COLUMN OVERRIDE ASSEMBLY.
334 344
211 212
FUNCTIONALLY CHECK THE ELEVATOR FREEPLAY AND THE ELEVATOR 334 TAB FREEPLAY. 344 NOTE( E ) APPLICABLE TO AIRPLANE LINE NUMBER 1-595 AND 597-1174 THAT HAVE NOT INCORPORATED SB 737-55A1080.
311BL emp
emp emp
311BL emp
ITEMS
AMTOSS
27-31-00-700-807
MPD MRB
27-098-01 MSI 27-098-01 RTE:9
MPD MRB
27-084-00 MSI 27-084-00 RTE:8
AMTOSS
27-31-00-720-801
MPD MRB
27-096-00 MSI 27-096-00 RTE:9
AMTOSS
27-09-91-200-803
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
T: 8000 FLH I: 8000 FLH
F2 HHI 737-700
0 18-mar-05
I: 25000 FLH
F2 HHI 737-700
2 03-jun-04
I: 8000 FLH
F2 HHI 737-700
2 18-mar-05
ATA: 27 - 31
Page 1 of 4
HHI R E V
ITEM 273100 82000
273101 70000
R
737-6
MAINTENANCE SCHEDULE
273101 75000
DESCRIPTION FUNCTIONALLY CHECK THE FORCE NECESSARY TO COLLAPSE AND EXTEND THE ELEVATOR INPUT ROD POGO'S.
ZONE ACCESS
STRUCTURE
211 212 317 318
311BL emp emp emp
MPD MRB
27-092-00 MSI 27-092-00 RTE:8
AMTOSS
27-31-00-820-809
211 212 334 344
emp emp emp emp
MPD MRB
27-086-00 MSI 27-086-00 RTE:9
AMTOSS
27-31-00-700-815
PERFORM A FUNCTIONAL CHECK OF THE ELEVATOR TAB FREEPLAY. 334 344 NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBERS 596, 1175 AND ON AND LINE NUMBERS 1 - 595 AND 597 - 1174 THAT HAVE INCORPORATED SB 737-55A1080.
emp emp
AAR
OPERATIONALLY CHECK THE ELEVATOR TAB CONTROL SYSTEM.
MPD MRB
R
Date: 23-jul-08
CHECK UPPER AND LOWER SIDE OF LEFT AND RIGHT ELEVATOR BALANCE PANELS FOR DEICING / ANTI-ICING FLUID RESIDUE AND CLEAN IF NECESSARY. METHOD 1 USE A SUITABLE FLEXISCOPE AND CHECK UPPER AND LOWER SIDE OF ALL BALANCE PANELS AND AFT PANEL HINGE AREA THROUGH GAPS BETWEEN ELEVATOR AND FIXED TRAILING EDGE AS FAR AS POSSIBLE; OR METHOD 2 OPEN LOWER ACCESS PANELS 333CB/343CB TO BALANCE BAY 5, DISCONNECT AFT END OF BALANCE PANEL AND CHECK UPPER AND LOWER SIDE OF BALANCE PANEL. IF NO CONTAMINATION IS FOUND NO OTHER BALANCE PANELS HAVE TO BE CHECKED. IF CONTAMINATION IS EVIDENT OPEN OTHER ACCESS PANELS TO REMAINING BALANCE BAYS FOR INSPECTION. NOTE( J ) THIS ITEM IS EFFECTIVE FROM OCT01 UNTIL MAR 31.
334 emp emp emp 344 emp emp emp
333BB 333CB 333DB 333EB 343BB 343CB 343DB 343EB
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 12500 FLH
F2 HHI 737-700
3 03-jun-04
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
27-31-32-200-802
I: 2000 CYC I: 4000 FLH
F2 HHI 737-700
3 23-jul-08
737-SL-12-014
I: 450 FLH
E3 HHI S 737-700
0 03-jun-04
27-CMR-08 ONE STAR 27-099-00 MSI 27-099-00 RTE:9
AMTOSS 273102 01000
THRESHOLD INTERVAL
REFERENCES
empty
SIL
ATA: 27 - 31
Page 2 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
273111 00000
273114 21000
273114 21100
273114 22000
273117 20000
273120 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE ELEVATOR PUSH 334 RODS (BETWEEN OUTPUT TORQUE TUBE AND CONTROL SURFACE) AND 344 ATTACHMENT BOLTS.
PERFORM A GENERAL VISUAL INSPECTION OF THE ELEVATOR POWER 317 CONTROL UNIT WITH HYDRAULIC POWER ON. 318
FUNCTIONALLY CHECK THE A AND B SYSTEM ELEVATOR POWER CONTROL UNIT FOR INTERNAL LEAKAGE IN A LOADED CONDITION.
STRUCTURE
318BR emp
emp 318BR
THRESHOLD INTERVAL
REFERENCES MPD MRB
27-100-00 MSI 27-100-00 RTE:8
AMTOSS
27-31-00-200-801
MPD MRB
27-076-00 MSI 27-076-00 RTE:8
AMTOSS
27-31-14-210-801
133 134 211 212
emp emp emp emp
MPD MRB
27-078-00 MSI 27-078-00 RTE:8
AMTOSS
29-00-00-790-804
OPERATIONALLY CHECK THE ELEVATOR CONTROL COLUMN OVERRIDE 211 ASSEMBLY. 212
emp emp
MPD MRB
27-082-00 MSI 27-082-00 RTE:8
AMTOSS
27-31-00-710-802
MPD MRB
27-080-00 MSI 27-080-00 RTE:6
AMTOSS AMTOSS
27-31-17-790-801 27-31-17-200-801
MPD MRB
27-068-00 MSI 27-068-00 RTE: 9
AMTOSS
27-31-20-740-801
DRAIN AND LEAK CHECK THE ELEVATOR PITOT-STATIC SYSTEM.
OPERATIONALLY CHECK THE ELEVATOR FEEL SHIFT FUNCTION. (IF INSTALLED)
311 312 320
117 118 211 212
311BL emp 323FL
117A emp emp emp
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 6 YRS
E3 HHI 737-700
3 03-jun-04
I: 6000 FLH
E1 HHI 737-700
3 18-mar-05
I: 12500 FLH
F2 HHI 737-700
0 30-nov-05
I: 12500 FLH
F1 HHI 737-700
2 03-jun-04
I: 6000 FLH
F2 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
ATA: 27 - 31
Page 3 of 4
HHI R E V
ITEM 273134 21000
R
737-6
MAINTENANCE SCHEDULE
273134 21500
R
273161 21000
273164 90000
Date: 23-jul-08
DESCRIPTION PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ELEVATOR BALANCE WEIGHT INSTALLATION AND ELEVATOR TAB CONTROL MECHANISM.
ZONE ACCESS
STRUCTURE
334 emp emp emp 344 emp emp emp
333BB 333CB 333DB 334PT 343BB 343CB 343DB 344PT
MPD MPD MRB
PERFORM A DETAILED VISUAL INSPECTION OF THE ELEVATOR TAB RODS AND TAB MECHANISM FOR CONDITION AND SECURITY OF INSTALLATION. THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT TASK 27-CMR-07. NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBER 596 AND 1175 AND ON AND LINE NUMBERS 1-595 AND 597-1174 THAT HAVE INCORPORATED SB 737-55A1080.
333 334 343 344
333BB 334PT 343BB 344PT
AAR
PERFORM A GENERAL VISUAL INSPECTION OF THE ELEVATOR MECHANICAL CONTROL PATH.
112 334 344
PERFORM A DETAILED VISUAL INSPECTION OF THE SINGLE ELEMENT DUAL LOAD PATH FEEL AND CENTERING UNIT OUTPUT ROD.
313 314
112A 318BR emp
emp 318BR
ITEMS
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
27-075-01 27-075-02 MSI 27-075-01 RTE:9 MSI 27-075-02 RTE:9
MRB AMTOSS
MPD MRB
TSK
27-31-34-210-801
I: 6000 FLH
E1 HHI 737-700
3 18-mar-05
I: 2000 CYC I: 4000 FLH
E3 HHI 737-700
3 23-jul-08
I: 6000 FLH
E1 HHI 737-700
4 18-mar-05
I: 6 YRS
E3 HHI 737-700
4 18-mar-05
27-CMR-07 ONE STAR 27-093-00 MSI 27-093-00 RTE:8
AMTOSS
27-31-00-220-802
MPD MRB
27-073-00 MSI 27-073-00 RTE:6
AMTOSS
27-31-61-210-801
MPD MRB
27-101-00 MSI 27-101-00 RTE:8
AMTOSS
27-31-00-200-802
ATA: 27 - 31
Page 4 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 32
273200 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STALL WARNING FUNCTIONALLY CHECK THE STALL WARNING SYSTEM.
117 118 211 212
117A emp emp emp
ITEMS
MPD MRB
27-088-00 MSI 27-088-00 RTE:9
AMTOSS AMTOSS
27-32-00-740-803 27-32-00-710-801
I: 6000 FLH
ATA: 27 - 32
F2 HHI 737-700
4 18-mar-05
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 41
274100 70000
274101 70000
274102 70000
274103 70000
274141 21000
274181 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
HORIZONTAL STABILIZER CONTROL SYSTEM FUNCTIONALLY CHECK THE SECONDARY STABILIZER TRIM BRAKE. NOTE( E ) APPLICABLE TO 251A4510-6 AND ON ACTUATORS.
211 212 311 312
emp emp 311BL emp
MPD MRB
27-106-00 MSI 27-106-00 RTE:8
AMTOSS
27-41-00-700-808
OPERATIONALLY CHECK THE STABILIZER TRIM LIMIT SWITCHES (FLAPS 211 UP AND FLAPS DOWN). 311 312
emp 311BL emp
MPD MRB
27-112-00 MSI 27-112-00 RTE:9
AMTOSS
27-41-00-700-805
MPD MRB
27-114-00 MSI 27-114-00 RTE:9
AMTOSS
27-41-00-700-810
MPD MRB
27-118-00 MSI 27-118-00 RTE:8
AMTOSS
27-41-00-700-807
MPD MRB
27-120-00 MSI 27-120-00 RTE:8
AMTOSS
27-41-41-210-801
MPD MRB
27-107-00 MSI 27-107-00 RTE:8
AMTOSS
12-22-41-610-802
OPERATIONALLY CHECK THE STABILIZER TRIM CONTROL COLUMN SWITCHING MODULE.
112 210
OPERATIONALLY CHECK THE AISLE STAND STABILIZER TRIM OVERRIDE 211 SWITCH. 212
DETAILED VISUAL INSPECTION OF THE UPPER AND LOWER STABILIZER 112 TRIM FORWARD MECHANISM RETENTION TURNBUCKLES AND TURNBUCKLE ATTACHMENT POINTS.
SERVICE THE HORIZONTAL TRIM ACTUATOR BRAKE. 311 312 NOTE( E ) APPLICABLE TO LINE NUMBER 350 AND ON. APPLICABLE TO AIRPLANES LINE NUMBER 1 TO 349 THAT HAVE INCORPORATED SB 737-27-1210.
112A emp
emp emp
112A
emp emp
ITEMS
I: 6000 FLH
F2 HHI 737-700
6 18-mar-05
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
I: 6000 FLH
E3 HHI 737-700
4 18-mar-05
I: 6000 FLH
S
2 05-sep-06
ATA: 27 - 41
HHI 737-700
Page 1 of 2
HHI R E V
ITEM
R
274181 01000
R
R
737-6
MAINTENANCE SCHEDULE
274181 21000
DESCRIPTION
ZONE ACCESS
REMOVE THE STABILIZER TRIM ACTUATOR FOR RESTORATION. NOTE( J, E ) NOTE (J): TASK IS A TIME CONTROLLED ITEM, IT IS INCLUDED IN MS FOR COMPLETENESS. NOTE (E): FOR 251A4510-6 AND ON ACTUATORS ONLY.
311 emp 312
PERFORM A DETAILED VISUAL INSPECTION OF THE STABILIZER TRIM JACKSCREW, BALLNUT, BALLNUT RETURN TUBES AND UPPER AND LOWER GIMBAL PINS.
311 312
STRUCTURE
112A 311BL emp
274197 70000
Date: 23-jul-08
OPERATIONALLY CHECK THE MAIN CONTROL COLUMN CUTOUT SWITCHES.
MPD MRB MRB
311BL emp
211 212
OPERATIONALLY CHECK THE CONTROL COLUMN STABILIZER TRIM ARM 211 AND DIRECTIONAL SWITCHES FOR MOVEMENT OF A SINGLE SWITCH TO 212 CAUSE STABILIZER MOVEMENT.
emp emp
emp emp
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-108-00 MSI 27-108-00 RTE:8 MSI 27-108-00 RTE:9
MS CM2740 00020 AMTOSS 27-41-81-400-801 AMTOSS 27-41-81-000-801 SB 737-27A1277 R1 SB CONTAINS A REQUIREMENT FOR OVERHAUL OF THE HORIZONTAL STABILIZER.
R
274191 70000
THRESHOLD INTERVAL
REFERENCES
MPD MRB
27-110-00 MSI 27-110-00 RTE:8
SB AMTOSS
737-27A1277 R1 27-41-81-210-801
MPD MRB
27-116-00 MSI 27-116-00 RTE:8
AMTOSS
27-41-91-700-801
MPD MRB
27-122-00 MSI 27-122-00 RTE:9
AMTOSS
27-41-97-700-801
I: 25000 FLH
S
HHI 737-700
4 23-jul-08
I: 1 YRS I: 1600 FLH I: 8 MTH
E3 HHI 737-700
8 23-jul-08
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
ATA: 27 - 41
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 51
275100 21000
275100 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLAP/SLAT SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING FLAP DRIVE SEAL RIB ANGLE GEAR BOX, FLAP DRIVE TORQUE TUBES, TORQUE TUBE COUPLINGS AND SUPPORTS AND FLAP TRANSMISSIONS. ACCESS FLAPS DEPLOYED
OPERATIONALLY CHECK THE LEFT AND RIGHT WING TRAILING EDGE FLAP TRANSMISSION NO-BACK BRAKES. ACCESS FLAPS DEPLOYED
133 134 541 542 543 544 550 553 560 561 562 565 641 642 643 644 650 653 660 661 662 665
emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS
27-51-00-210-801
133 134 210 541 542 543 544 553 641 642 643 644 653
emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
27-168-01 27-168-02 MSI 27-168-01 RTE:8 MSI 27-168-02 RTE:8
ITEMS
MRB
MRB AMTOSS
27-171-01 27-171-02 MSI 27-171-01 RTE:6 MSI 27-171-02 RTE:6
27-51-00-710-802
I: 6000 FLH
E1 HHI 737-700
5 22-mar-07
I: 25000 CYC
F1 HHI 737-700
4 03-jun-04
ATA: 27 - 51
Page 1 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
275100 72000
275100 73000
275100 74000
275100 74100
DESCRIPTION FUNCTIONALLY CHECK THE FLAP LOAD RELIEF SYSTEM.
FUNCTIONALLY CHECK THE ALTERNATE FLAP DRIVE SYSTEM.
OPERATIONALLY CHECK THE FLAP LOAD RELIEF SYSTEM.
ZONE ACCESS 117 118
133 134 212
117 118 210
OPERATIONALLY CHECK THE FLAP SKEW AND ASYMMETRY SYSTEM BY 117 INITIATING A BITE CHECK AT THE FLAP/SLAT ELECTRONICS UNIT (FSEU). 118 211 212
STRUCTURE
117A emp
emp emp emp
117A emp emp
117A emp emp emp
MPD MRB
27-156-00 MSI 27-156-00 RTE:9
AMTOSS
27-51-00-720-804
MPD MRB
27-158-00 MSI 27-158-00 RTE:9
AMTOSS
27-51-00-720-803
MPD MRB
27-154-00 MSI 27-154-00 RTE:9
AMTOSS
27-51-00-740-803
MPD MPD MRB
27-160-00 27-162-00 MSI 27-160-00 RTE:8 MSI 27-162-00 RTE:8
MRB AMTOSS
Date: 23-jul-08
ITEMS
THRESHOLD INTERVAL
REFERENCES
27-51-00-740-802
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 10000 FLH
F2 HHI 737-700
2 03-jun-04
I: 6000 FLH
F2 HHI 737-700
3 18-mar-05
I: 2500 FLH
F1 HHI 737-700
2 03-jun-04
I: 750 FLH
F1 HHI 737-700
3 03-jun-04
ATA: 27 - 51
Page 2 of 4
HHI R E V
ITEM 275101 21000
275101 74000
R
737-6
MAINTENANCE SCHEDULE
275106 21000
DESCRIPTION PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING TRAILING EDGE FLAP ACTUATION MECHANISM TO INCLUDE: - AFT FLAP DRIVE RODS - AFT FLAP PUSH RODS - INBOARD CARRIAGE ROLLERS - OUTBOARD CARRIAGE ROLLERS - BELLCRANKS - INBOARD CARRIAGE FORWARD ATTACH FITTING - INBOARD CARRIAGE ATTACH LINK - OUTBOARD CARRIAGE FWD ATTACH FITTING - OUTBOARD CARRIAGE ATTACH LINK - INBOARD FLAP PROGRAMMING ROLLERS - AFT FLAP TRACK ATTACH FITTING - AFT FLAP PROGRAMMING ROLLER - OUTBOARD FLAP PROGRAMMING ROLLERS ACCESS FLAPS DEPLOYED
ZONE ACCESS 542 543 544 553 561 562 564 567 642 643 644 653 661 667
STRUCTURE
emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS
27-51-00-210-802
OPERATIONALLY CHECK THE FLAP UNCOMMANDED MOTION PROTECTION 117 SYSTEM BY INITIATING A BITE CHECK OF THE FLAP SLAT ELECTRONICS 118 UNIT. 211 212
117A emp emp emp
MPD MRB
27-164-00 MSI 27-164-00 RTE:8
AMTOSS
27-51-00-740-801
PERFORM A DETAILED VISUAL INSPECTION OF THE TRAILING EDGE FLAP 112 LEVER SENSOR, LINKAGE, ROD AND ROD ENDS. 117 118 211 emp 212
emp emp emp 211A 211B emp
MPD MRB
27-166-00 MSI 27-166-00 RTE:8 27-166-00 MSI 27-166-00 RTE:8
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
MRB
MPD MRB AMTOSS
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-172-01 27-172-02 MSI 27-172-01 RTE:6 MSI 27-172-02 RTE:6
27-51-06-210-801
I: 12000 CYC
E3 HHI 737-700
3 03-jun-04
I: 6000 FLH
F1 HHI 737-700
2 18-mar-05
I: 25000 FLH
E3 HHI 737-700
4 23-jul-08
ATA: 27 - 51
Page 3 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
275132 22000
Date: 23-jul-08
DESCRIPTION FUNCTIONALLY CHECK THE LEFT AND RIGHT WING TRAILING EDGE FLAPS BALLSCREW ACTUATOR BACKLASH. ACCESS FLAPS DEPLOYED
ZONE ACCESS 133 134 210 541 542 543 544 553 641 642 643 644 653
STRUCTURE
emp emp emp emp emp emp emp emp emp emp emp emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MPD MRB MRB AMTOSS AMTOSS AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-148-01 27-148-02 MSI 27-148-01 RTE:6 MSI 27-148-02 RTE:6 27-51-42-220-801 27-51-32-220-801 27-51-42-220-802 27-51-32-220-802
I: 25000 CYC
ATA: 27 - 51
F2 HHI 737-700
3 03-jun-04
Page 4 of 4
HHI R E V
ITEM 27 - 61
N
737-6
MAINTENANCE SCHEDULE
276100 21000
DESCRIPTION
ZONE ACCESS
STRUCTURE
276100 72000
276100 73000
276100 82000
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
SPOILER AND SPEEDBRAKE CONTROL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE SPOILER MECHANICAL 134 CONTROL PATH.
emp
N 276100 71000
THRESHOLD INTERVAL
REFERENCES
MPD MRB
27-215-03 MSI 27-215-03 FEC:6
AMM
27-61-00-210-801
OPERATIONALLY CHECK THE SPOILER MIXER CENTERING MECHANISM. 133 134 NOTE( I ) 210 CMR-INTERVAL 20000 FLH 550 562 563 564 565 650 662 663 664 665
emp emp emp emp emp emp emp emp emp emp emp emp emp
AAR MPD MRB
27-CMR-04 27-194-00 MSI 27-194-00 RTE:8
AMTOSS
27-61-00-710-802
FUNCTIONALLY CHECK THE INTERNAL LEAKAGE OF LEADING EDGE SLAT 133 ACTUATORS. 134 211 212
emp emp emp emp
MPD MRB
27-210-00 MSI 27-210-00 RTE:6
AMM
29-00-00-790-804
FUNCTIONALLY CHECK THE INTERNAL LEAKAGE OF LEADING EDGE FLAP 133 ACTUATORS. 134 211 212
emp emp emp emp
MPD MRB
27-212-00 MSI 27-212-00 RTE:6
AMM
29-00-00-790-804
FUNCTIONALLY CHECK THE TORQUE OF THE SPOILER MIXER NO-BACK 133 ASSEMBLY. 134
112A emp
MPD MRB
27-184-00 MSI 27-184-00 RTE:8
AMTOSS
27-61-00-820-809
ITEMS
T: 4000 FLH I: 4000 FLH
E2 HHI 737-700
0 23-jul-08
I: 12000 FLH
F1 HHI 737-700
4 22-mar-07
I: 12500 FLH
F2 HHI 737-700
0 30-nov-05
I: 12500 FLH
F2 HHI 737-700
0 30-nov-05
I: 22400 FLH
F2 HHI 737-700
3 03-jun-04
ATA: 27 - 61
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
276101 82000
Date: 23-jul-08
DESCRIPTION PERFORM AN OPERATIONAL CHECK OF EACH LEFT AND RIGHT WING FLIGHT SPOILER ACTUATOR OVERRIDE QUADRANT. ACCESS FLAPS DEPLOYED
ZONE ACCESS 562 563 564 565 566 662 663 664 665 666
STRUCTURE
emp emp emp emp emp emp emp emp emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MPD MRB MRB AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
27-192-01 27-192-02 MSI 27-192-01 RTE:8 MSI 27-192-02 RTE:8 27-61-00-820-810
I: 25000 FLH
ATA: 27 - 61
F1 HHI 737-700
2 03-jun-04
Page 2 of 2
HHI R E V
ITEM 27 - 62
R
737-6
MAINTENANCE SCHEDULE
276200 21000
DESCRIPTION
276201 82000
276202 82000
Date: 23-jul-08
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AUTO SPEEDBRAKE CONTROL PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING FLIGHT SPOILER AND SPEEDBRAKE ACTUATORS.
emp emp emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS
27-62-00-210-802
PERFORM A GENERAL VISUAL INSPECTION OF THE FORWARD STABILIZER 112 TRIM MECHANISM AND THE SPEEDBRAKE LEVER ASSEMBLY AND AUTO SPEEDBRAKE ELECTRIC ACTUATOR, ACTUATOR ROD END, AND FORWARD ATTACHMENT POINTS.
112A
MPD MRB
27-121-00 MSI 27-121-00 RTE:6
AMTOSS
27-62-00-210-801
OPERATIONALLY CHECK THE SPEEDBRAKE REFUSED TAKEOFF (RTO) 117 SYSTEM. 118 210 211 212
117A emp emp emp emp
MPD MRB
27-188-00 MSI 27-188-00 RTE:9
AMTOSS AMTOSS
27-61-00-820-809 27-62-00-820-809
OPERATIONALLY CHECK THE SPEEDBRAKES EXTENDED LIGHT.
117A emp emp
MPD MRB
27-190-00 MSI 27-190-00 RTE:8
AMTOSS
27-62-00-820-810
R
276201 21000
ZONE ACCESS
210 552 562 563 564 565 566 652 653 662 663 664 665 666
117 118 210
ITEMS
MRB MPD MPD MRB
27-215-01 27-215-02 MSI 27-215-01 RTE:6 MSI 27-215-02 RTE:6 27-215-01 27-215-02 MSI 27-215-01 RTE:6 I: 4000 FLH
E1 HHI 737-700
6 23-jul-08
I: 6000 FLH
E1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F1 HHI 737-700
5 05-sep-06
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
ATA: 27 - 62
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 81
278100 21000
278100 70000
278100 71000
278100 86000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEADING EDGE SLAT SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LEADING EDGE FLAP AND SLAT ACTUATORS AND THE LEFT AND RIGHT WING LEADING EDGE FLAP SLAT ACTUATION MECHANISMS. ACCESS LEADING EDGES EXTENDED
512 513 522 523 524 525 612 613 622 623 624 625
OPERATIONALLY CHECK THE LEADING EDGE UNCOMMANDED MOTION 211 PROTECTION SYSTEM. 212
OPERATIONALLY CHECK THE LEADING EDGE DEVICES UNCOMMANDED 211 MOTION PROTECTION USING THE STANDBY HYDRAULIC SYSTEM. 212
OPERATIONALLY CHECK THE LEADING EDGE STANDBY ACTUATION SYSTEM.
211 212 510 610
emp emp emp emp emp emp emp emp emp emp emp emp
MPD MPD MRB
AMTOSS
27-81-00-210-801
117A emp
MPD MRB
27-218-00 MSI 27-218-00 RTE:8
AMTOSS
27-81-00-700-804
MPD MRB
27-224-00 MSI 27-224-00 RTE:8
AMTOSS
27-81-00-710-802
MPD MPD MRB
27-214-00 29-240-00 MSI 27-214-00 RTE:9 MSI 29-240-00 RTE:9
emp emp
emp emp emp emp
MRB
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
27-225-01 27-225-02 MSI 27-225-01 RTE:6 MSI 27-225-02 RTE:6
27-81-00-710-801
I: 6000 FLH
E1 HHI 737-700
3 18-mar-05
I: 3600 FLH
F1 HHI 737-700
4 25-apr-06
I: 1250 FLH
F1 HHI 737-700
5 18-mar-05
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
ATA: 27 - 81
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 27 - 83
278300 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEADING EDGE AUTOSLAT SYSTEM FUNCTIONALLY CHECK THE AUTOSLAT SYSTEM TO INCLUDE A BITE 117 CHECK OF THE STALL MANAGEMENT/YAW DAMPER (SMYD) COMPUTER. 118 211 212
117A emp emp emp
ITEMS
MPD MRB
27-216-00 MSI 27-216-00 RTE:8
AMTOSS
27-83-00-710-801
I: 1250 FLH
ATA: 27 - 83
F2 HHI 737-700
5 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
28
FUEL
28 - 00
FUEL
280000 03000
280000 04000
280000 05000
Date: 23-jul-08
DRAIN ALL TANKS (EXCEPT SURGE TANKS)
CHECK THAT FUELING STATION DOOR IS SECURED
VISUALLY CHECK DRAIN MAST AREAS AND DRAINS FOR LEAKAGE OF FUEL AND/OR HYDRAULIC FLUID
ZONE ACCESS
STRUCTURE
REFERENCES
530 630
emp emp
empty
630
emp
empty
100 434 444 500 600
emp emp emp emp emp
ITEMS
AMM
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
12-11-00 SERVICE EXPERIENCE
I: 4 Z
S
HHI 737-700
SM
2 11-dec-01
SERVICE EXPERIENCE
I: 1 T
S
HHI 737-700
SM
3 11-dec-01
SERVICE EXPERIENCE
I: 1 T
E1 HHI 737-700
SM
1 11-dec-01
empty
ATA: 28 - 00
Page 1 of 3
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
280000 06000
INSPECT (DETAILED) IN-TANK TUBING AND EQUIPMENT STATIC GROUND STRAPS AND CLAMPS FOR CONDITION, SECURITY AND OTHER DEGRADATION. (SFAR 88) NOTE( I ) PERFORM TASK CONCURRENTLY WITH OTHER FUEL TANK INSPECTION TASKS TO MINIMIZE TANK ENTRIES AND POSSIBLE ACCIDENTAL DAMAGE.
R
Date: 23-jul-08
ZONE ACCESS 131 emp 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 533 emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp
STRUCTURE
131AB 434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 533AB 533BB 533CB 534AB 534BB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB
ITEMS
THRESHOLD INTERVAL
REFERENCES MRB MPD MRB AMTOSS AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MSI 28-140-00 RTE:9 28-140-00 MSI 28-140-00 RTE:8 28-00-00-280-803 28-00-00-280-802 28-00-00-280-801
I: 10 YRS
ATA: 28 - 00
E3 HHI 737-700
4 23-jul-08
Page 2 of 3
HHI R E V
R
737-6
MAINTENANCE SCHEDULE ITEM
280000 76000
DESCRIPTION
FUNCTIONAL CHECK (RESISTANCE MEASUREMENT) OF THE EQUIPMENT FAULT CURRENT GROUND STRAP (S). (SFAR 88) NOTE( J, E ) NOTE (J): PUMP FAULT CURRENT GROUND STRAPS ARE EXTERNAL OF FUEL TANK. NOTE (E): IF THE APU FUEL BOOST PUMP IS INSTALLED
ZONE ACCESS emp emp emp emp emp emp emp emp emp 633 emp emp emp emp
632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB 633AB 633BB 633CB 634AB 634BB
131 132 531 551 631
emp emp emp 551DB emp
STRUCTURE
REFERENCES
MRB MRB MPD MPD MRB MRB
R
Date: 23-jul-08
AMM
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MSI 28-150-00 RTE:9 MSI 28-160-00 RTE:9 28-150-00 28-160-00 MSI 28-150-00 RTE:8 MSI 28-160-00 RTE:8 28-00-00-76
I: 5 YRS I: 6 YRS
ATA: 28 - 00
F2 HHI 737-700
3 23-jul-08
Page 3 of 3
HHI R E V
ITEM 28 - 11
R
737-6
MAINTENANCE SCHEDULE
281100 01000
R
281100 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUEL TANKS EXTERNAL WIRES OVER CENTER FUEL TANK 211 (DETAILED INSPECTION) CONCERN: POTENTIAL FOR WIRE CHAFING AND ARCING TO CENTER FUEL TANK UPPER PANEL. PERFORM A DETAILED INSPECTION OF THE WIRE BUNDLES ROUTED ON MAIN DECK OVER THE CENTER FUEL TANK AND UNDER THE MAIN DECK FLOOR BOARDS PER AMM 28-11-00 TO DETECT DAMAGED CLAMPS, WIRE CHAFING, AND THAT THE WIRE BUNDLE IS NOT IN CONTACT WITH SURFACE OF THE CENTER FUEL TANK. IF DISCREPANCIES ARE FOUND, REPAIR PER THE STANDARD WIRING PRACTICES MANUAL D6-54446. NOTE( )
emp
INSPECT THE MAIN AND CENTER FUEL TANK (WING) EXTERNAL LOWER 531 SURFACES INCLUDING TANK VENTS, SUMP DRAIN VALVES, SKIN LAP 532 JOINTS FOR OBVIOUS LEAKS, CONDITION AND SECURITY. 533 631 632 633
emp emp emp emp emp emp
ITEMS
AAR AAR
28-AWL-01 ALI 28-AWL-01
AMM AMM
28-11-00-211-801 28-11-00-211-801
MPD MRB
28-010-00 MSI 28-010-00 RTE:9
AMTOSS
28-11-00-21
T: 10 YRS I: 10 YRS I: 36000 CYC
E3 HHI 737-700
1 23-jul-08
I: 4000 FLH
E1 HHI 737-700
1 03-jun-04
ATA: 28 - 11
Page 1 of 1
HHI R E V
ITEM 28 - 13 281331 10000
DESCRIPTION
ZONE ACCESS
STRUCTURE
281331 20000
DETAILED INSPECTION OF THE LEFT AND RIGHT SURGE TANK VENT FLAME ARRESTOR FOR CLOGGING, CONDITION AND SECURITY.
533 633
emp emp
MPD MPD MRB
281341 21000
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING BETWEEN THE LOWER AIR VENT STACK AND THE DOOR STRUCTURE. (SFAR 88)
533 633
533BB 633BB
OPERATIONALLY CHECK THE LEFT AND RIGHT SURGE TANK RELIEF VALVES.
533 633
emp emp
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING 533 BETWEEN THE PRESSURE RELIEF VALVE AND THE STRUCTURE. (SFAR 633 88)
533BB 633BB
N
Date: 23-jul-08
EFF
R L ITEM BY E E REVISION P V DATE
ITEMS
28-030-01 28-030-02 MSI 28-030-01 RTE:8 MSI 28-030-02 RTE:8
AMTOSS
28-13-31-100-801
MPD MRB
28-204-00 MSI 28-204-00 RTE:9
AMM
28-13-31-200
MPD MPD MRB
28-020-01 28-020-02 MSI 28-020-01 RTE:9 MSI 28-020-02 RTE:9
MRB
N
TSK
FUEL VENT SYSTEM
N 281341 20000
THRESHOLD INTERVAL
REFERENCES
MRB
N
737-6
MAINTENANCE SCHEDULE
AMTOSS
28-13-41-20
MPD MRB
28-205-00 MSI 28-205-00 RTE:9
AMM
28-13-41-200
I: 3 YRS
E3 HHI 737-700
2 03-jun-04
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
I: 3 YRS
F1 HHI 737-700
1 03-jun-04
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
ATA: 28 - 13
Page 1 of 1
HHI R E V
ITEM 28 - 21
N
282111 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
282151 20000
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING 621 BETWEEN THE FUELING RECEPTACLE (MANIFOLD) AND THE STRUCTURE. (SFAR 88)
621GB
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING OF THE FUELING SHUTOFF VALVE ACTUATOR (SOLENOID) TO THE ADJOINING STRUCTURE. (SFAR 88)
621
621GB
N
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PRESSURE FUELING SYSTEM
N N
737-6
MAINTENANCE SCHEDULE
ITEMS
MPD MRB
28-208-00 MSI 28-208-00 RTE:9
AMM
28-21-11-200
MPD MRB
28-207-00 MSI 28-207-00 RTE:9
AMM
28-21-51-200-801
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
ATA: 28 - 21
Page 1 of 1
HHI R E V
ITEM 28 - 22
R
282200 20000
R
R
737-6
MAINTENANCE SCHEDULE
282200 21000
R
282200 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ENGINE FUEL FEED SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE FOLLOWING ITEMS ON ALL THE FUEL PUMPS FOR SIGNS OF FUEL LEAKS, HEAT DISCOLORATION OR DAMAGE: - WIRE TERMINAL ASSEMBLY - ELECTRICAL CONNECTOR - WIRE INSULATION NOTE: THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT 28-CMR-01. IF ANY DISCREPANCY IS DETECTED, PRIOR TO FURTHER FLIGHT, REPLACE THE FUEL PUMP WITH A NEW OR SERVICEABLE FUEL PUMP AND PERFORM AN INSULATION RESISTANCE TEST PER 28-CMR-02 NOTE( E ) THIS CMR TASK IS ONLY APPLICABLE TO THE FOLLOWING 737NG MAIN TANK FUEL BOOST PUMPS PARTNUMBERS: 60B92404-6 AND 60B92404-7, AND CENTER WING TANK OVERRIDE FUEL PUMPS PARTNUMBERS: 60B89004-10 AND 60B89004-12.
131 132 531 631
emp emp emp emp
AAR
PERFORM AN INSULATION RESISTANCE TEST ON ALL OF THE FUEL PUMPS. NOTE : THIS TASK ACCOMPLISHES CERTIFICATION MAINTENANCE REQUIREMENT 28-CMR-02. IF ANY RESISTANCE MEASUREMENT IS LESS THAN 5 MEGAOHM, PRIOR TO FURTHER FLIGHT, REPLACE THE FUEL PUMP WITH A NEW OR SERVICEABLE FUEL PUMP AND REPEAT INSULATION RESISTANCE TEST. NOTE( E ) THIS CMR TASK IS ONLY APPLICABLE TO THE FOLLOWING 737NG MAIN TANK FUEL BOOST PUMP PARTNUMBERS: 60B92404-6 AND 60B92404-7, AND CENTER WING TANK OVERRIDE FUEL PUMP PARTNUMBERS: 60B89004-10 AND 60B89004-12
131 132 531 631
emp emp emp emp
AAR
AMTOSS
28-22-00-200-801
OPERATIONALLY CHECK ENGINE FUEL SUCTION FEED SYSTEM
211 212
emp emp
MPD MRB
28-050-00 MSI 28-050-00 RTE:8
AMM AMM
28-22-15-710-801 28-22-00-710
ITEMS
MPD
28-CMR-01 ONE STAR 28-100-00
AMTOSS
MPD
28-22-00-210-801
I: 5000 FLH I: 18 MTH
E3 HHI I1 737-700 W1
8 23-jul-08
I: 5000 FLH I: 18 MTH
M2 HHI 737-700
6 23-jul-08
I: 7500 FLH
F1 HHI 737-700
1 05-sep-06
28-CMR-02 ONE STAR 28-110-00
ATA: 28 - 22
Page 1 of 4
HHI R E V
ITEM 282200 72000
282200 72100
N
737-6
MAINTENANCE SCHEDULE
282211 20000
N
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
OPERATIONALLY CHECK THE CENTER TANK FUEL SCAVENGE SYSTEM 211 (JET PUMP, INDUCED PORT CHECK VALVE, FLOAT VALVE AND LINE). 212
OPERATIONALLY CHECK THE FUEL SHUTOFF VALVE BATTERY
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING BETWEEN MOTOR OPERATED VALVE ACTUATOR AND ADJOINING STRUCTURE. (SFAR 88) NOTE( J ) THIS TASK IS PERFORMED FROM OUTSIDE OF TANK.
212 551 651
132 521 621
STRUCTURE
emp emp
emp emp emp
emp 521BB 621BB
ITEMS
REFERENCES MPD MRB
28-040-00 MSI 28-040-00 RTE:9
AMTOSS
28-22-00-72
MPD MRB
28-125-00 MSI 28-125-00 RTE:9
AMTOSS
28-22-00-72
MPD MRB
28-211-00 MSI 28-211-00 RTE:9
AMM AMM
28-22-11-200 28-22-21-200
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 10000 FLH
F1 HHI 737-700
1 03-jun-04
I: 6000 FLH
F1 HHI 737-700
2 18-mar-05
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
ATA: 28 - 22
Page 2 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
N
282211 72000
N
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
LIGHTNING AND FAULT CURRENT PROTECTION - MOTOR OPERATED 521 VALVE (MOV) ACTUATOR 621 CONCERN: POTENTIAL FOR ARCING OR SPARKING INSIDE THE FUEL TANK AT A CONDUCTIVE METAL-TO-GROUND STRUCTURE INTERFACE AS A RESULT OF LIGHTNING OR ELECTRICAL FAULT CURRENT EVENT. PERFORM THE FOLLOWING FUNCTIONAL CHECK (PER BOEING AMM 28-22-11) TO ENSURE THE INTEGRITY OF THE SPAR VALVE ACTUATOR ELECTRICAL BONDING PATH: 1. DISCONNECT THE ELECTRICAL CONNECTOR. 2. DISCONNECT THE BONDING JUMPER. 3. WITH THE ACTUATOR ELECTRICAL CONNECTOR AND THE BONDING JUMPER DISCONNECTED, VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE CONNECTOR FLANGE AND THE SPAR WEB IS 0.010 OHMS (10 MILLIOHMS) OR LESS. 4. ATTACH THE BONDING JUMPER TO THE ACTUATOR UPPER HOUSING USING A SEALED ELECTRICAL FAY SURFACE BOND AND VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE HOUSING AND THE ATTACHED BONDING JUMPER TERMINAL IS 0.001 OHMS (1 MILLIOHM) OR LESS. 5. WITH THE ACTUATOR ELECTRICAL CONNECTOR DISCONNECTED, VERIFY ELECTRICAL BONDING RESISTANCE BETWEEN THE OUTERMOST FQIS SHIELD GROUND TERMINAL AND THE SPAR WEB IS 0.014 OHMS (14 MILLIOHMS) OR LESS. NOTE( E, T ) NOTE(E) ALL AIRPLANES LINE NUMBER 1877-1980, 1982, AND AIRPLANES THAT HAVE INC. SB 737-28A1207. NOTE(T) T: DATE OF EMBODIMENT SB 737-28A1207.
STRUCTURE
emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES AAR AAR
28-AWL-24 FAA AD 2008-06-03
AMM AMM EO
28-22-11-720-801 28-00-00-910-801 155334
T: 1 s.N I: 6 YRS
ATA: 28 - 22
TSK
EFF
FC HHI 737-700
R L ITEM BY E E REVISION P V DATE
0 23-jul-08
Page 3 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
282213 20000
DESCRIPTION RESTORE (CLEAN) THE LEFT AND RIGHT MAIN FUEL TANK AND BOTH CENTER WING FUEL TANK WATER SCAVENGE JET PUMPS (WITHOUT DEFUELING THE TANK).
ZONE ACCESS 133 134 532 632
STRUCTURE
emp emp emp emp
REFERENCES MPD MPD MPD MRB MRB MRB
282214 00000
Date: 23-jul-08
REPLACE THE FUEL SHUT-OFF VALVE BATTERY NOTE( R ) FOR COMPLETENESS ONLY, COVERED BY CMS
212
emp
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
28-060-01 28-060-02 28-060-03 MSI 28-060-01 RTE:9 MSI 28-060-02 RTE:9 MSI 28-060-03 RTE:9
AMTOSS
28-22-13-20
MPD MRB
28-130-00 MSI 28-130-00 RTE:9
AMTOSS AMTOSS
28-22-14-40 28-22-14-00
I: 4000 FLH
S
HHI 737-700
5 18-mar-05
I: 7 YRS
S
HHI 737-700
2 03-jun-04
ATA: 28 - 22
Page 4 of 4
HHI R E V
ITEM 28 - 25
N
737-6
MAINTENANCE SCHEDULE
282502 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
Date: 23-jul-08
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU FUEL FEED SYSTEM FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING RESISTANCE BETWEEN THE APU SHUTOFF VALVE ACTUATOR AND ADJOINING STRUCTURE. (SFAR 88)
133
emp
N 282505 79000
REFERENCES
FUNCTIONALLY (PRESSURE DECAY) CHECK THE APU FUEL LINE SHROUD. 145
emp
ITEMS
MPD MRB
28-213-00 MSI 28-213-00 RTE:9
AMM
28-25-02-200
MPD MRB
28-070-00 MSI 28-070-00 RTE:8
AMTOSS
28-25-05-79
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
I: 12000 FLH
F2 HHI 737-700
1 03-jun-04
ATA: 28 - 25
Page 1 of 1
HHI R E V
ITEM 28 - 41
R
737-6
MAINTENANCE SCHEDULE
284100 01000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUEL QUANTITY INDICATING SYSTEM (FQIS) DETAILED INSPECTION (VISUAL) OF THE FQIS IN TANK WIRE HARNESS, COMPENSATOR AND TANK UNITS FOR SIGNS OF CHAFING OR RUBBING. (SFAR 88) (EZAP) NOTE( I ) PERFORM TASK CONCURRENTLY WITH OTHER FUEL TANK INSPECTION TASKS TO MINIMIZE TANK ENTRIES AND POSSIBLE ACCIDENTAL DAMAGE.
131 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp
434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB
ITEMS
MPD MRB
28-170-00 MSI 28-170-00 RTE:8
AMTOSS AMTOSS AMTOSS
28-41-44-280-803 28-41-44-280-802 28-41-44-280-801
I: 10 YRS
ATA: 28 - 41
E3 HHI 737-700
5 23-jul-08
Page 1 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS emp emp emp emp emp
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
632MB 632NB 632PB 632QB 632RB
ITEMS
ATA: 28 - 41
Page 2 of 6
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
N
284100 28000
N
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
INSPECT (DETAILED) THE IN-TANK FQIS COMPONENTS FOR CHAFING, 131 RUBBING, ADEQUATE SEPARATION FROM STRUCTURE AND CONDITION emp FOR SECURITY. (SFAR 88) 132 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
131AB 434CL 444CR 531AB 531BB 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 631AB 631BB 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB
ITEMS
REFERENCES MPD MRB
28-171-00 MSI 28-171-00 RTE:8
AMM
28-41-44-280
THRESHOLD INTERVAL
T: 10 YRS I: 10 YRS
ATA: 28 - 41
TSK
EFF
E3 HHI 737-700
R L ITEM BY E E REVISION P V DATE
0 23-jul-08
Page 3 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS emp emp emp emp
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
632NB 632PB 632QB 632RB
ITEMS
ATA: 28 - 41
Page 4 of 6
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
N
284100 29000
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) OUT TANK FQIS WIRE BUNDLE LIGHTNING SHIELD TO GROUND TERMINATION. (SFAR 88) CONCERN: POTENTIAL FOR LIGHTNING INDUCED VOLTAGES ON THE FQIS WIRING TO ENTER THE FUEL TANK. PERFORM THE FOLLOWING FUNCTIONAL CHECK TO ENSURE THE INTEGRITY OF THE FQIS WIRING SHIELD TO GROUND TERMINATION: 1. VERIFY THE RESISTANCE OF THE SHIELD TO GROUND TERMINATIONS AT SIDE OF BODY, AND AT THE SPAR PENETRATION IN THE UNPRESSURIZED AREA BY MAKING THE FOLLOWING MEASUREMENTS USING A LOOP RESISTANCE TESTER P/N 906-10246-2 OR 906-10246-3 PER BOEING AMM 05-55-54. RESTORE THE BONDS PER THE BOEING AMM IF REQUIRED. PERFORM A LOOP RESISTANCE MEASUREMENT WHERE THE WIRE BUNDLE ENTERS THE FUEL TANK: 1. THE LOOP RESISTANCE SHALL NOT EXCEED 138 MILLIOHMS FOR CONNECTOR D11312 (LEFT MAIN TANK WITHOUT DENSITOMETER) WIRE BUNDLE W1140. 2. THE LOOP RESISTANCE SHALL NOT EXCEED 63 MILLIOHMS FOR CONNECTOR D11312 (LEFT MAIN TANK WITH DENSITOMETER) WIRE BUNDLE W1140. 3. THE LOOP RESISTANCE SHALL NOT EXCEED 138 MILLIOHMS FOR CONNECTOR D11314 (RIGHT MAIN TANK WITHOUT DENSITOMETER) WIRE BUNDLE W1138. 4. THE LOOP RESISTANCE SHALL NOT EXCEED 63 MILLIOHMS FOR CONNECTOR D11314 (RIGHT MAIN TANK WITH DENSITOMETER) WIRE BUNDLE W1138. 5. THE LOOP RESISTANCE SHALL NOT EXCEED 40 MILLIOHMS FOR CONNECTOR D11316 (CENTER TANK WITHOUT DENSITOMETER) WIRE BUNDLE W7580. 6. THE LOOP RESISTANCE SHALL NOT EXCEED 40 MILLIOHMS FOR CONNECTOR D11316 (CENTER TANK WITH DENSITOMETER) WIRE BUNDLE W7580. NOTE( T ) (1)WITHIN 120 MONTHS SINCE THE DATE OF ISSUANCE OF THE ORIGINAL STANDARD AIRWORTHINESS CERTIFICATION OR THE DATE OF ISSUANCE OF THE ORIGINAL EXPORT CERTIFICATION OF AIRWORTHINESS. (2) WITHIN 24 MONTHS AFTER THE EFFECTIVE DATE OF AD 2008-10-09 (12-JUN-08), THEREFORE 12-JUN-10. WHICHEVER OCCURS LATER!
N
Date: 23-jul-08
ZONE ACCESS 133 510 emp 610 emp
STRUCTURE
emp 511AT 521BB 611AT 621BB
ITEMS
REFERENCES AAR MPD MRB
ALI 28-AWL-03 28-173-00 MSI 28-173-00 RTE:8
AMM
05-55-54-200
THRESHOLD INTERVAL
T: 1 s.N I: 10 YRS
ATA: 28 - 41
TSK
EFF
F2 HHI 737-700
R L ITEM BY E E REVISION P V DATE
0 23-jul-08
Page 5 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
284100 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
OPERATIONALLY (BITE) CHECK THE FUEL QUANTITY INDICATING SYSTEM. 210 632
STRUCTURE
emp 621GB
ITEMS
REFERENCES MPD MRB
28-080-00 MSI 28-080-00 RTE:9
AMTOSS
28-41-00-71
THRESHOLD INTERVAL
I: 6000 FLH
ATA: 28 - 41
TSK
EFF
F1 HHI 737-700
R L ITEM BY E E REVISION P V DATE
1 03-jun-04
Page 6 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
29
HYDRAULIC POWER
29 - 00
HYDRAULIC POWER
290000 01000
290000 01100
290000 06000
290011 01000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
113 134
emp emp
empty
113 134
emp emp
empty
OPERATIONALLY CHECK THE STANDBY HYDRAULIC ELECTRIC MOTOR 211 DRIVEN PUMP TO INCLUDE OBSERVING LOW PRESSURE LIGHT 212 ILLUMINATION AND THEN GOING OUT.
emp emp
HYDRAULIC FLUID SAMPLING A- AND B-SYSTEM
HYDRAULIC FLUID SAMPLING STANDBY-SYSTEM
PTU OPERATIONAL CHECK. 139 PERFORM AN OPERATIONALLY CHECK OF THE POWER TRANSFER UNIT 211 CONTROL SYSTEM TO INCLUDE A VISUAL CHECK OF THE CONTROL 212 VALVE FOR PROPER POSITION.
emp emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES
AMM
TSK
EFF
R L ITEM BY E E REVISION P V DATE
29-11-00-200-801
I: 25000 FLH
S
HHI 737-700
0 11-dec-01
AMM
29-11-00-200-801
I: 25000 FLH
S
HHI 737-700
0 11-dec-01
MPD MRB
29-200-00 MSI 29-200-00 RTE:8
AMTOSS
29-34-31-400-801PAR.E I: 5000 FLH
F1 HHI 737-700
5 03-jun-04
MPD MRB
29-250-00 MSI 29-250-00 RTE:8
AMTOSS
29-22-00-710-801
F1 HHI E1 737-700
5 18-mar-05
I: 6000 FLH
ATA: 29 - 00
Page 1 of 1
HHI R E V
ITEM 29 - 11 291100 20000
291100 30000
291102 00000
291103 00000
N
737-6
MAINTENANCE SCHEDULE
291104 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MAIN HYDRAULIC POWER SYSTEM GROSS HYDRAULIC SYSTEM LEAKAGE CHECK.
133 134 211 212
emp emp emp emp
MPD MRB
29-010-00 MSI 29-010-00 RTE:6
AMM AMM AMM AMM
29-00-00-790-802 29-00-00-790-803 29-00-00-790-804 29-00-00-790-808
OPERATIONALLY CHECK THE A & B SYSTEM ENGINE DRIVEN PUMP (EDP) 133 SHUTOFF VALVES. 134 210
emp emp emp
MPD MRB
29-100-00 MSI 29-100-00 RTE:8
AMM
29-11-81-710-801
emp emp 192CL 192CR
MPD MRB
29-070-00 MSI 29-070-00 RTE:6
AMTOSS AMTOSS AMTOSS AMTOSS
29-11-02-400-802 29-11-02-000-802 29-09-01-000-801 29-09-01-400-801
DETAILED INSPECTION AND CHECK FOR CLOGGED CONDITION OF THE 133 RESERVOIR PRESSURIZATION MODULE VENT CAP 134 NOTE( E ) APPLICABLE TO AIRPLANES THAT HAVE NOT INCORPORATED SB 737-29-1106
emp emp
MPD MRB
29-060-00 MSI 29-060-00 RTE:6
AMTOSS
29-11-03-220-801
FUNCTIONALLY CHECK (RESISTANCE MEASUREMENT) THE BONDING RESISTANCE BETWEEN THE HYDRAULIC LINE FITTING AT FUEL TANK WALL PENETRATIONS AND THE ADJOINING STRUCTURE. (SFAR 88)
551DB
MPD MRB
28-201-00 MSI 28-201-00 RTE:9
AMM
29-11-04-200
CLEAN THE RESERVOIR PRESSURIZATION MODULE FILTER
133 134 192 emp
532
N
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
I: 12000 FLH
F2 HHI 737-700
5 25-apr-06
I: 6000 FLH
F1 HHI 737-700
4 22-mar-07
I: 4000 FLH
S
HHI 737-700
3 30-nov-05
I: 4000 FLH
E3 HHI 737-700
4 25-apr-06
T: 12 YRS I: 12 YRS
F2 HHI 737-700
0 23-jul-08
ATA: 29 - 11
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
291121 00000
291141 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
OPERATIONAL CHECK OF EMDP GROUND FAULT PROTECTION SYSTEM 133 134 211 212
emp emp 117A emp
MPD MRB
29-080-00 MSI 29-080-00 RTE:6
AMTOSS
29-11-21-700-802
REPLACE THE "A" AND "B" HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN 133 PUMP (EMDP) CASE DRAIN FILTER 134
emp emp
MPD MPD MRB
29-030-01 29-030-02 MSI 29-030-01 RTE:6 MSI 29-030-02 RTE:6
MRB
291151 00000
REPLACE "A" AND "B" SYSTEM EDP CASE DRAIN FILTERS
411 421
413 423
AMTOSS AMTOSS
29-11-41-400-801 29-11-41-000-801
MPD MPD MRB
29-050-01 29-050-02 MSI 29-050-01 RTE:6 MSI 29-050-02 RTE:6
MRB
291161 00000
291171 40000
INSPECT (GENERAL VISUAL) THE DELTA "P" INDICATION OF A & B SYSTEM 133 RETURN FILTER MODULE. 134
REPLACE A & B SYSTEM ENGINE DRIVEN PUMP (EDP) AND ELECTRIC MOTOR DRIVEN PUMP (EMDP) PRESSURE FILTERS.
133 134
emp emp
emp emp
AMTOSS AMTOSS
29-11-51-400-801 29-11-51-000-801
MPD MRB
29-090-00 MSI 29-090-00 RTE:9
AMTOSS
29-11-61-210-801
MPD MPD MRB
29-020-00 29-040-00 MSI 29-020-00 RTE:6 MSI 29-040-00 RTE:6
MRB AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
29-11-71-000-802 29-11-71-400-802
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 4000 FLH
F1 HHI 737-700
1 03-jun-04
I: 600 FLH
S
HHI 737-700
4 18-mar-05
I: 2400 FLH
S
HHI 737-700
4 25-apr-06
I: 600 FLH
E2 HHI 737-700
2 18-mar-05
I: 8000 FLH
S
3 03-jun-04
ATA: 29 - 11
HHI 737-700
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 29 - 18
291811 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
GROUND SERVICING SYSTEM REPLACE THE GROUND HYDRAULIC RESERVOIR FILL FILTER.
133 134
emp emp
ITEMS
MPD MRB
29-180-00 MSI 29-180-00 RTE:9
AMTOSS AMTOSS
29-18-11-400-802 29-18-11-000-802
I: 16000 FLH
ATA: 29 - 18
S
HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
ITEM 29 - 21 292100 60000
292100 61000
R
737-6
MAINTENANCE SCHEDULE
292100 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
FUNCTIONALLY CHECK STANDBY HYDRAULIC SYSTEM FOR INTERNAL 133 LEAKAGE. NOTE: THIS TASK IS SATISFIED BY ACCOMPLISHMENT OF TASK 134 27-054-00. 211 212
emp emp emp emp
MPD MRB
29-190-00 MSI 29-190-00 RTE:8
AMM
29-00-00-790-808
FUNCTIONALLY CHECK THE STANDBY RUDDER POWER CONTROL UNIT 133 FOR INTERNAL LEAKAGE IN A LOADED CONDITION. 134 211 212
emp emp emp emp
MPD MRB
27-054-00 MSI 27-054-00 RTE:8
AMM
29-00-00-790-808
OPERATIONALLY CHECK THE STANDBY RUDDER SYSTEM. TO INCLUDE OBSERVING LOW PRESSURE LIGHT ILLUMINATION AND THEN EXTINGUISHING. NOTE( )
emp emp emp emp
MPD MPD MPD MRB
27-052-00 29-200-00 29-230-00 MSI 27-052-00 RTE:8 MSI 29-200-00 RTE:8 MSI 29-230-00 RTE:8
133 134 211 212
MRB R
292151 00000
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STANDBY HYDRAULIC SYSTEM
MRB
292141 00000
THRESHOLD INTERVAL
REFERENCES
REPLACE THE STANDBY HYDRAULIC SYSTEM CASE DRAIN FILTER.
REPLACE THE STANDBY HYDRAULIC SYSTEM PRESSURE FILTER
139
139
emp
emp
ITEMS
AMTOSS
29-21-00-700-803
MPD MRB
29-220-00 MSI 29-220-00 RTE:8
AMTOSS AMTOSS
29-21-41-400-801 29-21-41-000-801
MPD MRB
29-210-00 MSI 29-210-00 RTE:8
AMTOSS AMTOSS
29-21-51-400-802 29-21-51-000-802
I: 25000 FLH
F2 HHI 737-700
1 22-mar-07
I: 12500 FLH
F2 HHI 737-700
0 30-nov-05
I: 1 s.N I: 180 DAY I: 1200 FLH
F1 HHI 737-700
7 23-jul-08
I: 12000 FLH
S
HHI 737-700
4 22-mar-07
I: 12000 FLH
S
HHI 737-700
4 22-mar-07
ATA: 29 - 21
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 29 - 22
292200 73000
292201 71000
292221 02000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
POWER TRANSFER SYSTEM FUNCTIONALLY CHECK THE POWER TRANSFER UNIT.
211 212
OPERATIONALLY CHECK THE POWER TRANSFER UNIT ISOLATION CHECK 139 VALVE. 211 212
REPLACE THE POWER TRANSFER UNIT PRESSURE FILTER.
133 134
emp emp
emp emp emp
emp emp
ITEMS
MPD MRB
29-260-00 MSI 29-260-00 RTE:8
AMTOSS
29-22-00-730-801
MPD MRB
29-280-00 MSI 29-280-00 RTE:8
AMTOSS
29-22-00-710-801
MPD MRB
29-270-00 MSI 29-270-00 RTE:8
AMTOSS AMTOSS
29-22-21-400-802 29-22-21-020-801
I: 25000 FLH
F2 HHI 737-700
1 03-jun-04
I: 25000 FLH
F1 HHI 737-700
2 22-mar-07
I: 12000 FLH
S
5 22-mar-07
ATA: 29 - 22
HHI 737-700
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 29 - 32
293200 73000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
HYDRAULIC FLUID TEMPERATURE INDICATING SYSTEM FUNCTIONALLY CHECK THE A & B HYDRAULIC SYSTEM CASE DRAIN WARNING SWITCHES.
133 134 210
emp emp emp
ITEMS
MPD MRB
29-310-00 MSI 29-310-00 RTE:9
AMTOSS
29-32-00-730-802
I: 25000 FLH
ATA: 29 - 32
F2 HHI 737-700
3 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 31 31 - 31
313100 97000
313109 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
INDICATING & RECORDING SYSTEMS FLIGHT DATA RECORDER SYSTEM FUNCTIONAL CHECK OF REQUIRED PARAMETERS (FDR, DFDAU OUTPUT, 118 INTERFACING SYSTEMS) BY 242 DOWNLOADING FDR DATA. (CHECK OF DATA IS DONE OFF AIRCRAFT) NOTE( I ) MRB INTERVAL IS 6000 FLH
OPERATIONAL CHECK OF THE ULB AT BATTERY REPLACEMENT. NOTE( I ) AT BATTERY REPLACEMENT
242
emp emp
MPD MPD MRB MRB
emp
NFL II-56/01 2.3.7 31-31-00-97
MPD MPD MRB
31-140-00 31-150-00 MSI 31-140-00 RTE:9 MSI 31-150-00 RTE:9
MS AMTOSS AMTOSS AMTOSS AMTOSS
ITEMS
31-120-00 31-130-00 MSI 31-120-00 RTE:7 MSI 31-130-00 RTE:7
AAR AMTOSS
MRB
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
CM3131 00010 31-31-09-00 31-31-09-96 31-31-09-40 31-31-09-70
I: 24 MTH I: 1 s.N
F2 HHI 737-700
3 18-mar-05
I: 1 s.N
F1 HHI 737-700
2 03-jun-04
ATA: 31 - 31
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 31 - 51
315100 73000
315100 74000
315101 73000
315102 73000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CENTRAL WARNING SYSTEMS OPERATIONAL CHECK OF MACH / AIRSPEED SYSTEMS 1 AND 2 DISCRETE 210 OUTPUTS FOR AURAL WARNING SYSTEM.
FUNCTIONAL CHECK OF THE AURAL WARNING MODULE (AWM) USING BITE CHECK.
211 212
OPERATIONAL CHECK OF LANDING GEAR LOGIC MODULE OUTPUT TO 211 THE AWM SYSTEMS 1 & 2. 212
FUNCTIONAL CHECK OF THE TRAILING EDGE AND LEADING EDGE FLAP, 211 THRUST LEVER, UPPER AND LOWER STABILIZER TRIM LIMIT, GROUND 212 SPOILER PRESSURE, SPEED BRAKE, PARK BRAKE AND GROUND SPOILER BYPASS VALVE SWITCHES FOR THE AURAL WARNING MODULE (AWM).
emp
emp emp
emp emp
emp emp
ITEMS
MPD MRB
31-030-00 MSI 31-030-00 RTE:9
AMTOSS
34-16-00-730-802
MPD MRB
31-010-00 MSI 31-010-00 RTE:6
AMTOSS
31-51-00-740-801
MPD MRB
31-040-00 MSI 31-040-00 RTE:8
AMTOSS
31-51-00-730-802
MPD MRB
31-050-00 MSI 31-050-00 RTE:8
AMTOSS
31-51-00-730-803
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F2 HHI 737-700
3 18-mar-05
I: 6000 FLH
F1 HHI 737-700
4 18-mar-05
I: 6000 FLH
F2 HHI 737-700
3 18-mar-05
ATA: 31 - 51
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 31 - 62
316200 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COMMON DISPLAY SYSTEM COMMON DISPLAY SYSTEMS INSPECT AND CLEAN THE F/O AND CENTER UPPER DISPLAY UNIT AIR INLET SCREEN ACCORDING AMM SECTION 31-62-11
211 212
emp emp
ITEMS
MPD MRB
31-160-00 MSI 31-160-00 RTE:6
AMM
31-62-11-100
I: 12 MTH
ATA: 31 - 62
S HHI E2 737-700 F1
2 22-mar-07
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 32 - 00
320000 01000
DESCRIPTION
ZONE ACCESS
STRUCTURE
LUBRICATE THE LEFT AND RIGHT MAIN LANDING GEAR ASSEMBLY.
734 744
551DB 651DB
MPD MPD MRB
MRB
Date: 23-jul-08
R L ITEM BY E E REVISION P V DATE
LUBRICATE THE NOSE LANDING GEAR ASSEMBLY.
713
emp
CHECK BRAKE ACCUMULATOR PRECHARGE PRESSURE, SERVICE AS REQUIRED.
133 211 212
CHECK NOSE AND MAIN LANDING GEAR TIRES FOR PROPER INFLATION. 713 SERVICE AS REQUIRED. 733 744 NOTE( I ) 48 ELAPSED CLOCK HOURS
emp emp emp
emp emp emp
ITEMS
32-030-01 32-030-02 MSI 32-030-01 RTE:6 MSI 32-030-01 RTE:8 MSI 32-030-02 RTE:6 MSI 32-030-02 RTE:8
AMTOSS AMTOSS
12-25-07-06 12-21-11-64
MPD MRB
32-080-00 MSI 32-080-00 RTE:6 MSI 32-080-00 RTE:8
MRB
320000 05000
EFF
GENERAL
MRB
320000 04000
TSK
LANDING GEAR
MRB
320000 03000
THRESHOLD INTERVAL
REFERENCES
AMTOSS
12-21-21-64
MPD MRB
32-300-00 MSI 32-300-00 RTE:9
AMTOSS AMTOSS
12-15-11-420-801 12-15-11-610-801
MPD MRB
32-350-00 MSI 32-350-00 RTE:9
AMTOSS AMTOSS AMTOSS
12-15-51-42 12-15-51-78 12-15-51-61
I: 560 CYC I: 90 DAY
S
HHI 737-700
4 22-mar-07
I: 560 CYC I: 90 DAY
S
HHI 737-700
3 22-mar-07
I: 1200 FLH
S
HHI 737-700
4 25-apr-06
I: 1 Z
S
HHI 737-700
4 22-mar-07
ATA: 32 - 00
Page 1 of 8
HHI R E V
ITEM 320000 08000
320000 09000
DESCRIPTION SERVICE THE NOSE LANDING GEAR SHOCK STRUT.
SERVICE THE LEFT AND RIGHT MLG SHOCK STRUT.
ZONE ACCESS 115 116
734 744
STRUCTURE
emp emp
emp emp
REFERENCES MPD MRB
32-070-00 MSI 32-070-00 RTE:9
AMTOSS
12-15-41-61
MPD MPD MRB
32-020-01 32-020-02 MSI 32-020-01 RTE:9 MSI 32-020-02 RTE:9
MRB AMTOSS 320000 11000
320000 21000
R
737-6
MAINTENANCE SCHEDULE
320000 31000
713 734 744
emp emp emp
empty
BRAKES FOR WEAR, DAMAGE AND LEAKAGE (PARKING BRAKE NOT SET)
734 744
emp emp
empty
INSPECT TIRES FOR WEAR AND DAMAGE
713 734 744
emp emp emp
empty
713 734 744
emp emp emp
empty
NLG AND MLG STRUCTURE AND COMPONENTS
R 320000 41000
Date: 23-jul-08
WHEELS FOR DAMAGE AND PARTICULAR FOR MISSING OR DEFECT TIEBOLTS
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 3000 CYC
S
HHI 737-700
1 03-jun-04
12-15-31-61
I: 4000 CYC
S
HHI 737-700
2 22-mar-07
SERVICE EXPERIENCE
I: 1 T
E1 HHI 737-700
FC
0 24-mar-99
SERVICE EXPERIENCE
I: 1 T
E1 HHI 737-700
FC
0 24-mar-99
SERVICE EXPERIENCE
I: 1 T
E1 HHI 737-700
FC
1 23-jul-08
SERVICE EXPERIENCE
I: 1 T
E1 HHI 737-700
FC
0 24-mar-99
ATA: 32 - 00
Page 2 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
320000 60000
320000 61000
320000 62000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 115 IN THE NLG WHEEL WELL FOR BROKEN WIRES. CHECK ASSOCIATED 116 PULLEYS AND BRACKETS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE NLG WHEEL WELL: - NLG MANUAL EXTENSION CABLES - NLG STEERING CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD AREAS. ACCESS COVERS P/N 273A4520-1 OR -2 NEED TO BE REMOVED TO PERFORM THIS TASK.
emp emp
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 133 IN THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL FOR BROKEN 134 WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE LEFT AND RIGHT MLG WHEEL WELL: - MLG MANUAL EXTENSION CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. MLG MANUAL EXTENSION CABLES DO NOT REQUIRE DISPLACEMENT FOR COMPLETE INSPECTION.
emp emp
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 210 WITHIN THE CONTROL CABIN FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED IN THE CONTROL CABIN: - LANDING GEAR CONTROL LEVER CABLES - NOSE WHEEL STEERING CABLES NOTE( J ) THE CONTROL CABLES MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD.
S2113
STRUCTURE
REFERENCES MPD MRB MRB
20-20-31-20
MPD MRB
32-440-00 MSI 32-440-00 RTE:6 MSI 32-440-00 RTE:8
AMTOSS
20-20-31-20
MPD MRB
32-460-00 MSI 32-460-00 RTE:6 MSI 32-460-00 RTE:8
MRB AMTOSS
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-440-00 MSI 32-440-00 RTE:6 MSI 32-440-00 RTE:8
AMTOSS
MRB
THRESHOLD INTERVAL
20-20-31-20
I: 4800 CYC I: 24 MTH
E3 HHI 737-700
3 22-mar-07
I: 4800 CYC I: 24 MTH
E3 HHI 737-700
3 22-mar-07
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
3 18-mar-05
ATA: 32 - 00
Page 3 of 8
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
320000 63000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 137 WITHIN THE OVERWING CENTER SECTION AND WHEEL WELLS FROM BS 138 663 TO BS 727 FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE AFT PASSENGER CABIN OVERWING CENTER SECTION: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.
STRUCTURE
emp emp
MPD MRB MRB AMTOSS AMTOSS AMTOSS
ITEMS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
I: 21600 CYC I: 6 YRS
ATA: 32 - 00
E3 HHI 737-700
5 23-jul-08
Page 4 of 8
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
320000 64000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 112 WITHIN THE LOWER NOSE COMPARTMENT FOR BROKEN WIRES. CHECK 113 ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION 114 AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE LOWER NOSE COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES - NLG MANUAL EXTENSION CABLES - NLG STEERING CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.
STRUCTURE
112A emp emp
MPD MRB MRB AMTOSS AMTOSS AMTOSS
ITEMS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
I: 21600 CYC I: 6 YRS
ATA: 32 - 00
E3 HHI 737-700
5 23-jul-08
Page 5 of 8
HHI R E V
ITEM
R
320000 65000
R
R
737-6
MAINTENANCE SCHEDULE
320000 66000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 117 WITHIN THE ELECTRONICS COMPARTMENT FOR BROKEN WIRES. CHECK 118 ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE ELECTRONICS COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.
117A emp
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 125 WITHIN THE AIR CONDITIONING DISTRIBUTION BAY FOR BROKEN WIRES. 126 CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE AIR CONDTIONING DISTRIBUTION BAY: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.
emp 821
STRUCTURE MPD MRB MRB
20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
MPD MRB
32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8
AMTOSS AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8
AMTOSS AMTOSS AMTOSS
MRB
ITEMS
THRESHOLD INTERVAL
REFERENCES
20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
I: 21600 CYC I: 6 YRS
E3 HHI 737-700
5 23-jul-08
I: 21600 CYC I: 6 YRS
E3 HHI 737-700
5 23-jul-08
ATA: 32 - 00
Page 6 of 8
HHI R E V
ITEM
R
320000 67000
R
R
737-6
MAINTENANCE SCHEDULE
320000 68000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 121 WITHIN THE FORWARD CARGO COMPARTMENT FOR BROKEN WIRES. 122 CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE FORWARD CARGO COMPARTMENT: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD. ACCESS PASSENGER CABIN FLOOR PANELS BETWEEN B.S. 663.75 AND B.S. 727 FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS FORWARD CARGO COMPARTMENT CEILING PANELS OR FLOOR PANELS BETWEEN B.S.396 TO B.S. 540.
821 emp
PERFORM A DETAILED VISUAL INSPECTION OF THE CONTROL CABLES 135 WITHIN THE PASSENGER COMPARTMENT OVER THE WING CENTER 136 SECTION FROM BS 540 TO BS 663.75 FOR BROKEN WIRES. CHECK ASSOCIATED PULLEYS, BRACKETS AND MECHANISMS FOR CONDITION AND SECURITY OF INSTALLATION. THE FOLLOWING CABLES ARE LOCATED WITHIN THE PASSENGER COMPARTMENT ABOVE THE WING CENTER SECTION: - MLG CONTROL CABLES - MLG MANUAL EXTENSION CABLES - MLG BRAKE CONTROL CABLES NOTE( J ) THE CONTROL CABLE SYSTEM MUST BE DISPLACED FULL TRAVEL IN EACH DIRECTION FOR COMPLETE INSPECTION AT SEALS, PULLEYS AND FAIRLEAD.
131AB emp
STRUCTURE MPD MRB MRB
20-20-31-200-801 20-20-31-200-802
MPD MRB
32-460-00 MSI 32-460-00 RTE:6 MSI 32-460-00 RTE:8
AMTOSS AMM AMM AMM AMM
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-450-00 MSI 32-450-00 RTE:6 MSI 32-450-00 RTE:8
AMTOSS AMTOSS
MRB
ITEMS
THRESHOLD INTERVAL
REFERENCES
20-20-31-20 32-31-22-211-801 20-20-31-200-801 20-20-31-200-802 20-20-31-200-805
I: 21600 CYC I: 6 YRS
E3 HHI 737-700
5 23-jul-08
I: 36000 CYC I: 12 YRS
E3 HHI 737-700
4 23-jul-08
ATA: 32 - 00
Page 7 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
320010 00000
DESCRIPTION CLEAN EXPOSED SURFACE OF THE LEFT AND RIGHT MAIN LANDING GEAR SHOCK STRUT
ZONE ACCESS 734 744
STRUCTURE
emp emp
MPD MPD MRB MRB AMTOSS
Date: 23-jul-08
ITEMS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-010-01 32-010-02 MSI 32-010-01 RTE:9 MSI 32-010-02 RTE:9 32-00-10-100-801
I: 50 CYC
ATA: 32 - 00
S
HHI 737-700
3 03-jun-04
Page 8 of 8
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 11
321100 01000
321100 40000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MAIN LANDING GEAR SHOCK STRUT PERFORM A DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT 734 MAIN LANDING GEAR EXTENSION AND RETRACTION MECHANISM ( 744 INCLUDING RETRACT ACTUATORS, UPLOCK ACTUATORS AND DOWNLOCK ACTUATORS, UPLOCK MECHANISM AND DOWNLOCK MECHANISM).
551DB 651DB
RESTORE THE LEFT AND RIGHT MAIN LANDING GEAR ASSEMBLY. NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.
551BB 551BT 551DB 551DT 551EB 551ET 551FB 651BB 651BT 651DB 651DT 651EB 651ET 651FB
734 emp emp emp emp emp emp 744 emp emp emp emp emp emp
ITEMS
MPD MRB
32-150-00 MSI 32-150-00 RTE:6
AMTOSS
32-11-00-20
MPD MPD MPD MPD MRB
MRB MRB
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM MS
32-11-00-000 32-11-00-400 32-11-61-000 32-11-61-400 32-11-71-000 32-11-71-420 32-11-83-000 32-11-83-400 32-11-89-000 32-11-89-420 32-32-11-000 32-32-11-400 32-32-31-000 32-32-31-400 57-16-02-000 57-16-02-400 CM3211 .....
MRB
I: 4000 CYC
E3 HHI 737-700
5 22-mar-07
I: 10 YRS I: 18000 CYC
S
5 22-mar-07
ATA: 32 - 11
HHI 737-700
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
321100 50000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
DISCARD THE LEFT AND RIGHT MAIN LANDING GEAR LIFE LIMITED PARTS 734 emp NOTE( J ) emp FOR COMPLETENESS ONLY SEE CMS FOR AFFECTED PARTS. emp emp emp emp 744
STRUCTURE
551BB 551BT 551DB 551DT 551EB 551ET 551FB emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MRB MRB AMTOSS AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
32-050-01 32-050-02 CMR PAGE 9.0-50 MSI 32-050-01 RTE:8 MSI 32-050-02 RTE:8 32-11-00-00 32-11-00-40
I: 45000 CYC
ATA: 32 - 11
S
HHI 737-700
6 05-sep-06
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 21
322100 00000
322100 21000
322100 22000
322100 60000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NOSE LANDING GEAR SHOCK STRUT PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE LANDING GEAR 713 EXTENSION AND RETRACTION MECHANISM (INCLUDING RETRACT ACTUATOR, LOCK ACTUATOR AND LOCK MECHANISM).
PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE WHEEL STEERING MECHANICAL CONTROL PATH.
PERFORM A DETAILED VISUAL INSPECTION OF THE NOSE WHEEL STEERING ACTUATOR ROD ENDS AND ASSOCIATED HARDWARE.
REPLACE NLG AFT LOCK LINK (162A2115-2) NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.
115
713
713
emp
emp
emp
emp
MPD MRB
32-120-00 MSI 32-120-00 RTE:6
AMTOSS
32-11-00-00
MPD MRB
32-390-00 MSI 32-390-00 RTE:6
AMTOSS
32-51-00-200-801
MPD MRB
32-400-00 MSI 32-400-00 RTE:6
AMTOSS
32-21-00-20
MPD MPD
MRB
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
I: 4000 CYC
E3 HHI 737-700
4 22-mar-07
I: 4000 CYC
E3 HHI 737-700
7 22-mar-07
I: 4000 CYC
E3 HHI 737-700
4 22-mar-07
I: 4200 CYC
S
2 03-jun-04
32-100-00 PAGE 9.0-17 STRUCTURAL SAFE LIFE PARTS MSI 32-100-00 RTE:8
ATA: 32 - 21
HHI 737-700
Page 1 of 2
HHI R E V
ITEM 322110 00100
322110 00200
322110 10000
N
737-6
MAINTENANCE SCHEDULE
322171 20000
DESCRIPTION RESTORE THE NOSE LANDING GEAR ASSEMBLY. NOTE( J ) FOR COMPLETENESS ONLY COVERED BY CMS.
DISCARD THE NOSE LANDING GEAR LIFE LIMITED PARTS NOTE( J ) FOR COMPLETENESS ONLY SEE CMS FOR AFFECTED PARTS
ZONE ACCESS emp emp 113AC 113AW 113BW 114AC 114AW 114BW 711AL 712AR
MPD MPD MRB
115 116 713 emp emp emp emp emp emp emp
713
MRB
32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00
AMM AMM AMM AMM AMM AMM MS
32-21-00-000 32-21-00-400 32-21-21-000 32-21-21-400 32-33-51-000 32-33-51-400 CM3221 000..
emp emp 113AC 113AW 113BW 114AC 114AW 114BW 711AL 712AR
MPD MRB
32-100-00 MSI 32-100-00 RTE:8
AMTOSS AMTOSS
32-21-00-40 32-21-00-00
emp
MPD MRB
32-060-00 MSI 32-060-00 RTE:9
AMTOSS
32-00-10-10
MPD MRB
32-085-00 MSI 32-085-00 FEC:8
AMM TC
32-21-71-200-803 32-085-00-01
emp
N
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
115 116 713 emp emp emp emp emp emp emp
CLEAN EXPOSED SURFACE OF THE NOSE LANDING GEAR SHOCK STRUT. 713
INSPECT (DETAILED) NOSE LANDING GEAR AXLE.
STRUCTURE
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 18000 CYC I: 10 YRS
S
HHI 737-700
5 22-mar-07
I: 75000 CYC
S
HHI 737-700
4 05-sep-06
I: 50 CYC
S
HHI 737-700
1 03-jun-04
T: 30 MTH I: 30 MTH
E3 HHI 737-700
0 23-jul-08
ATA: 32 - 21
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 31
323100 00000
323151 20000
323171 40000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LANDING GEAR CONTROL SYSTEM FUNCTIONAL CHECK / ADJUSTMENT OF CONTROL CABLE TENSION
PERFORM A DETAILED VISUAL INSPECTION OF THE LANDING GEAR SELECTOR VALVE.
OPERATIONALLY CHECK THE LANDING GEAR TRANSFER VALVE
112
133
133 134 211 212
112A
emp
112A emp emp emp
ITEMS
empty
AMM
32-31-00-820-801
MPD MRB
32-110-00 MSI 32-110-00 RTE:8
AMTOSS
32-31-51-20
MPD MRB
32-240-00 MSI 32-240-00 RTE:8
AMTOSS
32-31-71-40
I: 18000 CYC I: 5 YRS
F2 HHI 737-700
2 25-apr-06
I: 4000 CYC
E3 HHI 737-700
4 22-mar-07
I: 8000 FLH
F1 HHI 737-700
1 03-jun-04
ATA: 32 - 31
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 32
323221 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MAIN LANDING GEAR EXTENSION AND RETRACTION REMOVE THE MAIN LANDING GEAR WHEEL WELL PROTECTION RETRACT 133 PRESSURE FUSE FOR FUNCTIONAL TEST 134 NOTE( J ) FOR COMPLETENESS ONLY, COVERED BY COSL.
emp emp
ITEMS
MPD MRB
32-230-00 MSI 32-230-00 RTE:6
AMM AMM AMTOSS
32-32-21-400 32-32-21-000 32-32-21-00
I: 25000 FLH
ATA: 32 - 32
S
HHI 737-700
4 05-sep-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 34
323400 70000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NOSE LANDING GEAR EXTENSION AND RETRACTION PERFORM A FUNCTIONAL CHECK OF THE LEFT AND RIGHT MAIN LANDING 212 GEAR MANUAL EXTENSION SYSTEM AND ALTERNATE EXTENSION BYPASS 734 VALVE. 744
S2122 emp emp
ITEMS
MPD MRB
32-220-00 MSI 32-220-00 RTE:8
AMTOSS
32-34-00-730-801
I: 30 MTH
ATA: 32 - 34
F1 HHI F2 737-700
4 25-apr-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 35
323500 73000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LANDING GEAR ALTERNATE EXTENSION SYSTEM PERFORM A FUNCTIONAL CHECK OF THE NOSE LANDING GEAR MANUAL 211 EXTENSION SYSTEM. 212 713
emp S2122 emp
ITEMS
MPD MRB
32-200-00 MSI 32-200-00 RTE:8
AMTOSS
32-35-00-730-801
I: 30 MTH
ATA: 32 - 35
F2 HHI 737-700
4 25-apr-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 41
324100 71000
324100 72000
324131 00000
324141 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
BRAKE CONTROL SYSTEM PERFORM AN OPERATIONAL CHECK OF THE ALTERNATE BRAKE SYSTEM 133 AND ALTERNATE BRAKE SELECTOR VALVE. 134 211 212
emp emp emp emp
MPD MRB
32-290-00 MSI 32-290-00 RTE:8
AMTOSS
32-41-00-71
OPERATIONALLY CHECK THE BRAKE ACCUMULATOR ISOLATION VALVE 133 134 211 212
emp emp emp emp
MPD MRB
32-310-00 MSI 32-310-00 RTE:9
AMTOSS
32-41-00-72
PERFORM A DETAILED VISUAL INSPECTION OF THE BRAKE METERING 133 VALVES.
emp
MPD MRB
32-260-00 MSI 32-260-00 RTE:6
AMTOSS
32-41-31-00
MPD MPD MRB
32-270-01 32-270-02 MSI 32-270-01 RTE:6 MSI 32-270-02 RTE:6
VISUALLY CHECK THE LEFT AND RIGHT BRAKE WEAR PINS FOR MINIMUM 211 EXTENSION. 734 (PARKING BRAKE SET) 744
emp emp emp
MRB
324181 00000
THRESHOLD INTERVAL
PERFORM A DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT 133 BRAKE CONTROL LINKAGES AND CABLES QUADRANTS. 134 210
112A emp emp
ITEMS
AMTOSS AMM
32-41-41-70 32-41-41
MPD MRB
32-250-00 MSI 32-250-00 RTE:6
AMTOSS
32-41-81-00
I: 15000 CYC
F1 HHI 737-700
2 18-mar-05
I: 12500 CYC
F1 HHI 737-700
1 03-jun-04
I: 4000 CYC
E3 HHI 737-700
4 22-mar-07
I: 50 CYC
E2 HHI 737-700
1 03-jun-04
I: 4000 CYC
E3 HHI 737-700
5 22-mar-07
ATA: 32 - 41
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 44
324400 79000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PARKING BRAKE SYSTEM PERFORM A FUNCTIONAL BLEED DOWN CHECK OF THE PARKING BRAKE 134 SYSTEM AND BRAKE ACCUMULATOR PRECHARGE PRESSURE. 211 212
emp emp emp
MPD MRB MRB
324411 00000
THRESHOLD INTERVAL
PERFORM A DETAILED VISUAL INSPECTION OF THE PARKING BRAKE MECHANICAL CONTROL PATH.
112 emp 211 212
112A 2111S emp emp
ITEMS
32-340-00 MSI 32-340-00 RTE:6 MSI 32-340-00 RTE:9
AMTOSS
32-44-00-79
MPD MRB
32-330-00 MSI 32-330-00 RTE:6
AMTOSS
32-44-11-00
I: 4000 CYC
F2 HHI 737-700
3 22-mar-07
I: 4000 CYC
E3 HHI 737-700
4 22-mar-07
ATA: 32 - 44
Page 1 of 1
HHI R E V
ITEM 32 - 45
R
737-6
MAINTENANCE SCHEDULE
324500 70000
R 324511 40000
324521 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WHEELS, BRAKES, AND TIRES VISUALLY CHECK NOSE AND MAIN LANDING GEAR TIRES AND WHEELS 713 FOR CONDITION AND WEAR. 734 744 NOTE( I ) 48 ELAPSED CLOCK HOURS
emp emp emp
MPD MRB
32-360-00 MSI 32-360 RTE:9
AMTOSS
32-45-00-70
RESTORE THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL ASSEMBLY 734 (IES) 744 NOTE( I, J ) NOTE (I): TIRE CHANGE NOTE (J): FOR COMPLETENESS ONLY COVERED BY CMS.
emp emp
MPD MPD MRB
32-380-01 32-380-02 MSI 32-380-01 RTE:9 MSI 32-380-02 RTE:9
RESTORE THE NOSE LANDING GEAR WHEEL ASSEMBLY (IES). NOTE( I, J ) NOTE (I): TIRE CHANGE NOTE (J): FOR COMPLETENESS ONLY COVERED BY CMS.
emp
713
MRB
ITEMS
AMTOSS AMTOSS
32-45-11-40 32-45-11-00
MPD MRB
32-380-00 MSI 32-380-00 RTE:9
AMTOSS AMTOSS
32-45-21-40 32-45-21-00
I: 48 HRS
VC HHI E1 737-700
5 23-jul-08
I: 1 s.N
S
HHI 737-700
2 03-jun-04
I: 1 s.N
S
HHI 737-700
2 03-jun-04
ATA: 32 - 45
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 51
325121 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NOSE GEAR STEERING SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE RUDDER PEDAL STEERING INTERCONNECT MECHANICAL CONTROL PATH.
112 113 emp emp emp
emp 113AC 113AW 113BW 114AC
ITEMS
MPD MRB
32-410-00 MSI 32-410-00 RTE:6
AMTOSS
32-51-21-00
I: 4000 CYC
ATA: 32 - 51
E3 HHI 737-700
3 22-mar-07
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 32 - 61
326100 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LANDING GEAR POSITION INDICATING AND WARNING PERFORM AN OPERATIONAL CHECK ( BITE CHECK ) THE PROXIMITY SWITCH ELECTRONICS UNIT
112
emp
ITEMS
MPD MRB
32-420-00 MSI 32-420-00 RTE:8
AMM
32-09-10-710-801
I: 25000 FLH
ATA: 32 - 61
F1 HHI 737-700
2 30-nov-05
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 33 33 - 51
335100 72000
335103 96000
335105 96000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LIGHTS EMERGENCY LIGHTS FUNCTIONAL CHECK OF THE FLIGHT DECK EMERGENCY LIGHTING SWITCH "ON" AND "ARMED" POSITION AND THE ATTENDANT PANEL EMERGENCY LIGHTING SWITCH "ON" POSITION.
OPERATIONAL CHECK OF THE EMERGENCY LIGHTS.
210 220 230 240
emp emp emp emp
MPD MRB
33-020-00 MSI 33-020-00 RTE:8
AMTOSS
33-51-00-720-801
200
emp
MPD MRB
33-010-00 MSI 33-010-00 RTE:8
AMTOSS
33-51-00-710-801
MPD MRB
33-055-00 MSI 33-055-00 RTE:8
AMTOSS
33-51-06-200-801
FUNCTIONAL CHECK OF THE EMERGENCY LIGHTS BATTERY PACKS FOR 220 CAPACITY (15MIN. MINIMUM) AND ONE COMPLETE DEEP CYCLE. 230 240 NOTE( J ) PERFORM THIS TEST NOT LESS THAN 120MIN. BEFORE DEPARTURE.
emp emp emp
ITEMS
I: 2 YRS
F2 HHI 737-700
6 03-jun-04
I: 300 FLH
F1 HHI 737-700
3 03-jun-04
I: 1 YRS
F2 HHI 737-700
5 03-jun-04
ATA: 33 - 51
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 34 34 - 11
341100 17000
341100 79000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NAVIGATION STATIC AND TOTAL AIR PRESSURE SYSTEM DETAILED INSPECTION FOR MOISTURE IN THE PITOT SYSTEMS
PERFORM A FUNCTIONAL PITOT STATIC SYSTEM LEAK CHECK
112
113 114 121 122 211 212 221 222
112A
emp emp emp emp emp emp emp emp
MPD MRB
34-090-00 MSI 34-090-00 RTE:6
AMTOSS
34-11-00-21
MPD MPD MPD MPD MPD MPD MRB
34-010-00 34-020-00 34-030-00 34-040-00 34-050-00 34-060-00 MSI 34-010-00 RTE:6 MSI 34-020-00 RTE:6 MSI 34-030-00 RTE:6 MSI 34-040-00 RTE:6 MSI 34-050-00 RTE:6 MSI 34-060-00 RTE:6
MRB MRB MRB MRB MRB AAR AAR AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
I: 6000 FLH
NFL II - 2/00, PAGE I: 24 MTH 82 NFL II - 23/03 34-11-00-790-815 34-11-00-790-814 34-11-00-790-813 34-11-00-790-812 34-11-00-790-811 34-11-00-790-810
ATA: 34 - 11
E3 HHI 737-700
3 18-mar-05
F2 HHI 737-700
4 03-jun-04
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
341101 17000
341101 20000
341102 20000
Date: 23-jul-08
DESCRIPTION DETAILED INSPECTION FOR MOISTURE IN THE STATIC SYSTEMS
DETAILED VISUAL INSPECTION OF THE PITOT PROBES
DETAILED VISUAL INSPECTION OF THE STATIC PROBES
ZONE ACCESS 112 118 122
113 114
113 114
STRUCTURE
112A 117A 821
emp emp
emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MRB
34-100-00 MSI 34-100-00 RTE:6
AMTOSS
34-11-00-210-802
MPD MRB
34-070-00 MSI 34-070-00 RTE:6
AMTOSS
34-11-01-200-803
MPD MRB
34-080-00 MSI 34-080-00 RTE:6
AMTOSS
34-11-02-200-801
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 12000 FLH
E3 HHI 737-700
3 22-mar-07
I: 6000 FLH
E3 HHI 737-700
3 18-mar-05
I: 6000 FLH
E3 HHI 737-700
3 18-mar-05
ATA: 34 - 11
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 34 - 24
342400 02000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STANDBY MAGNETIC COMPASS STANDBY MAGNETIC COMPASS SWING.
200
emp
ITEMS
AAR
NFL II 56/01
AMM
34-23-00-820-802
I: 12 MTH
ATA: 34 - 24
F2 HHI 737-700
2 29-apr-03
Page 1 of 1
HHI R E V
ITEM 34 - 53
R
737-6
MAINTENANCE SCHEDULE
345300 73000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIR TRAFFIC CONTROL SYSTEM PERFORM A FUNCTIONAL CHECK OF THE AIRCRAFT´S ATC SYSTEM
210
emp
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
MPD MRB AAR
34-110-00 MSI 34-110-00 RTE:7
AAR FAR 91.413 PART 43 APPENDIX F AMTOSS 34-53-00-73 AMM 34-53-00-730-803
ITEMS
I: 24 MTH
ATA: 34 - 53
F2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
ITEM 34 - 60
R
737-6
MAINTENANCE SCHEDULE
346002 00001
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLIGHT MANAGEMENT COMPUTING FMS NAVIGATION DATA BASE (NDB) REVISE NDB
205
emp
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
empty
AMM AMM
ITEMS
34-61-00-470-803 34-61-00-470-805
I: 28 DAY
ATA: 34 - 60
S
HHI 737-700
1 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
35
OXYGEN
35 - 00
GENERAL
350000 01000
350000 02000
350000 04000
350000 05000
350000 06000
350000 09000
Date: 23-jul-08
CREW OXYGEN SYSTEM FOR MINIMUM DISPATCH PRESSURE
MASK ASSY, OPERATIONAL CHECK IN "SITU"
DISCHARGE DISC FOR DAMAGE
ZONE ACCESS
210
210
122
CHECK FOR PRESENCE AND PROPER STORAGE OF SMOKE GOGGLES 212
PORTABLE OXYGEN UNITS FOR MINIMUM DISPATCH PRESSURE
212
PROTECTIVE BREATHING EQUIPMENT, VENDOR SCOTT: IF INSTALLED 212 CHECK FOR HUMIDITY INDICATOR COLOR: IF COLOR HAS CHANGED FROM BLUE TO PINK, DISCARD UNIT
STRUCTURE
emp
emp
emp
emp
emp
emp
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
empty
SERVICE EXPERIENCE
I: 1 Z
M1 HHI 737-700
FC
1 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
M1 HHI 737-700
FC
1 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
SM
3 03-jun-04
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
FC
1 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
M1 HHI 737-700
1 11-dec-01
SERVICE EXPERIENCE
I: 1 Z
E1 HHI 737-700
3 18-dec-02
empty
empty
empty
empty
empty
ATA: 35 - 00
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 35 - 12
351200 70000
351200 70001
351200 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLIGHT CREW OXYGEN SYSTEM OPERATIONALLY CHECK EACH FLIGHT CREW OXYGEN MASK/MICROPHONE.
210
OPERATIONALLY CHECK EACH FLIGHT CREW OXYGEN MASK/REGULATOR 122 (OUT OF THE BOX ASSEMBLY). 210
VISUALLY (CROSS) CHECK THE FLIGHT CREW OXYGEN CYLINDER 122 PRESSURE INDICATOR AND THE CONTROL COMPARTMENT FLIGHT CREW 210 OXYGEN INDICATOR.
821
821 emp
117A emp
ITEMS
MPD MRB
23-080-00 MSI 23-080-00 RTE:9
AMTOSS
35-12-00-70
MPD MRB
35-010-00 MSI 35-010-00 RTE:8
MPD MRB
35-050-00 MSI 35-050-00 RTE:8
AMTOSS
35-12-00-71
I: 4000 FLH
F1 HHI 737-700
3 05-sep-06
I: 4000 FLH
F1 HHI 737-700
0 03-jun-04
I: 2400 FLH
E2 HHI 737-700
3 25-apr-06
ATA: 35 - 12
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 35 - 21
352101 00000
352101 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER / LLAR OXYGEN SYSTEM-CHEMICAL CHEMICAL OXYGEN GENERATOR CHECK EXPIRATION DATE, IF AGE LIMIT 220 WILL BE REACHED DURING NEXT 15 MTH, CHANGE GENERATOR. 230 240
VISUALLY CHECK THE TEMPERATURE SENSITIVE TAPE AND POSITION 220 OF FIRING PINS ON EACH PASSENGER CABIN CHEMICAL OXYGEN 230 GENERATOR (INCLUDING EACH LAVATORY AND CABIN ATTENDANT'S 240 SERVICE UNIT).
emp emp emp
emp emp emp
ITEMS
MPD MRB
35-070-00 MSI 35-070-00 RTE:9
AMTOSS AMTOSS
35-22-11-40 35-22-11-00
MPD MRB
35-060-00 MSI 35-060-00 RTE:9
AMTOSS
35-22-00-21
I: 15 MTH
E2 HHI 737-700
1 03-jun-04
I: 4 YRS
E2 HHI 737-700
3 03-jun-04
ATA: 35 - 21
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 35 - 22
352200 70000
352231 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PASSENGER OXYGEN SYSTEM-GASEOUS OPERATIONALLY CHECK THE PASSENGER OXYGEN SYSTEM AUTOMATIC 220 AND MANUAL MODES, ( THIS CHECK INCLUDES THE DOOR LATCH 230 ACTUATORS / SOLENOIDS ) 240
VISUALLY CHECK 10% ( ROTATIONAL INSPECTION ) OF THE PASSENGER, 220 LAVATORY, AND ATTENDANT OXYGEN MASKS FOR CONDITION AND 230 SECURITY. 240
emp emp emp
emp emp emp
ITEMS
MPD MRB
35-080-00 MSI 35-080-00 RTE: 9
AMTOSS
35-22-00-70
MPD MRB
35-090-00 MSI 35-090-00 RTE:9
AMTOSS
35-22-31-21
I: 8000 FLH
F1 HHI 737-700
1 03-jun-04
I: 8000 FLH
E2 HHI 737-700
1 03-jun-04
ATA: 35 - 22
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 35 - 31
353100 71000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PORTABLE OXYGEN EQUIPMENT VISUALLY CHECK ALL THE PORTABLE OXYGEN CYLINDERS FOR PRESENCE, CONDITION AND SECURITY
221 241
emp emp
ITEMS
MPD MRB
35-100-00 MSI 35-100-00 RTE:9
AMTOSS
35-31-00-71
I: 8000 FLH
ATA: 35 - 31
E2 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 36 36 - 14
361400 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PNEUMATIC APU BLEED SYSTEM DISCARD APU BLEED AIR DUCT FLEXIBLE PRESSURE SEAL.
133 emp 141 143 145
193D 311BL emp emp emp
ITEMS
MPD MRB
21-190-00 MSI 21-190-00 RTE:6
AMM AMM
36-13-01-020 36-13-01-420
I: 6 YRS
ATA: 36 - 14
S
HHI 737-700
0 22-mar-07
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 38 38 - 11
381106 00000
381106 10000
381106 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WATER & WASTE STORAGE AND DISTRIBUTION OPERATIONALLY CHECK THE FORWARD LAVATORY POTABLE WATER DRAIN VALVE FOR EVIDENCE OF LEAKAGE.
221
emp
ANNUAL INSPECTION AND CERTIFICATION OF POTABLE WATER SYSTEM. 146 IN CASE OF FINDINGS PERFORM CLEANING WITH HERISIL. NOTE( R ) TRINKWASSERVERORDNUNG § 18 UND 19 VOM 21.05.2001
146AR
PERFORM CLEANING OF POTABLE WATER SYSTEM.
146AR
146
MPD MRB
38-010-00 MSI 38-010-00 RTE:9
AMTOSS
38-11-06-00
AAR
SEE NOTE
ITEMS
I: 6500 FLH
F1 HHI 737-700
1 03-jun-04
I: 12 MTH
S
HHI 737-700
0 18-mar-05
I: 4 MTH
S
HHI 737-700
1 22-mar-07
empty
AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
38-10-00-600-801
ATA: 38 - 11
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 38 - 32
383200 10000
383202 00100
383203 00000
383205 96000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
VACUUM WASTE SYSTEM SERVICE THE TOILET WASTE LINES.
REPLACE THE WASTE TANK WATER SEPARATOR. NOTE( E ) APPLICABLE FOR L/N 138 AND ON, OR WITH SUPPLIER (EDO FIBER SCIENCE) S/B 01930-38-1 INSTALLED.
117 221 241
141 145 emp
RESTORE THE WASTE DRAIN BALL-VALVE BY REPLACING THE SEALS (2) 141 (OFF AIRCRAFT).
RESTORE (CLEAN) OR REPLACE THE VACUUM BLOWER FILTER.
141 145 emp
117A emp emp
emp 1401S 822
822
emp 1401S 822
ITEMS
MPD MRB
38-020-00 MSI 38-020-00 RTE:7
AMTOSS AMTOSS
38-32-00-100-802 38-32-00-100-801
MPD MRB
38-100-00 MSI 38-100-00 RTE:9
AMTOSS AMTOSS
38-32-02-40 38-32-02-00
MPD MRB
38-040-00 MSI 38-040-00 RTE:9
AMTOSS AMTOSS
38-32-03-40 38-32-03-00
MPD MRB
38-030-00 MSI 38-030-00 RTE:7
AMTOSS
38-32-05-96
I: 2400 FLH
S
HHI 737-700
6 05-sep-06
I: 6000 FLH
S
HHI 737-700
5 18-mar-05
I: 60 MTH
S
HHI 737-700
4 22-mar-07
I: 2500 FLH
S
HHI 737-700
2 03-jun-04
ATA: 38 - 32
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 38 - 33
383300 74000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WASTE TANK QUANTITY INDICATION OPERATIONALLY ( BITE ) CHECK THE WASTE TANK QUANTITY INDICATION 241 SYSTEM FROM THE FLIGHT ATTENDANT´S PANEL.
emp
ITEMS
MPD MRB
38-050-00 MSI 38-050-00 RTE:9
AMTOSS
38-33-00-74
I: 6500 FLH
ATA: 38 - 33
F1 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 38 - 42
384210 96000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WATER TANK PRESSURIZATION SYSTEM DISCARD AND REPLACE THE BLEED AIR IN-LINE FILTER.
146 emp
1401S 822
ITEMS
MPD MRB
38-060-00 MSI 38-060-00 RTE:9
AMTOSS
38-42-10-96
I: 6500 FLH
ATA: 38 - 42
S
HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 49 49 - 00
490011 10000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIRBORNE AUXILIARY POWER AUXILIARY POWER UNIT (APU) - GENERAL CHECK THE OIL LEVEL AND SERVICE THE APU WITH OIL AS REQUIRED 316
315A
empty
SERVICE EXPERIENCE
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
I: 7 DAY
ATA: 49 - 00
S
HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 49 - 11
491111 40000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU - SYSTEM PERFORM A DETAILED VISUAL INSPECTION OF THE APU MOUNTS, STRUTS AND BRACKETS FOR CRACKS, FATIGUE OR CORROSION.
315 316
315A emp
ITEMS
MPD MRB
49-020-00 MSI 49-020-00 RTE:8
AMTOSS
49-13-11-20
I: 8 YRS I: 1 AC
ATA: 49 - 11
E3 HHI 737-700
5 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 49 - 13
491311 20000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU MOUNTS PERFORM A GENERAL VISUAL INSPECTION OF THE APU MOUNTS FOR 315 GENERAL CONDITION AND SECURITY OF INSTALLATION 316
315A emp
ITEMS
MPD MRB
49-010-00 MSI 49-010-00 RTE:8
AMTOSS
49-13-11-20
I: 2 YRS
ATA: 49 - 13
E1 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 49 - 15
491511 20000
491522 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU AIR INTAKE SYSTEM PERFORM A DETAILED INSPECTION OF THE SIGMA SEAL. (AFTER APU REMOVAL). NOTE( I ) APU CHANGE
316
LUBRICATE THE VORTEX GENERATOR HINGE PIN
312
315A
emp
ITEMS
MPD MRB
49-030-00 MSI 49-030-00 RTE:8
AMTOSS
49-15-11-20
MPD MRB
49-240-00 MSI 49-240-00 RTE:9
AMTOSS
49-15-22-60
I: 1 s.N
E3 HHI 737-700
3 03-jun-04
I: 16000 FLH
S
2 03-jun-04
ATA: 49 - 15
HHI 737-700
Page 1 of 1
HHI R E V
ITEM 49 - 16
R
491611 10000
R
R
737-6
MAINTENANCE SCHEDULE
491611 11000
R
491611 19900
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU DRAINS CLEAN THE COMBUSTOR DRAIN AND EXAMINE THE THREAD FOR CRACKS. PERFORM AN OPERATIONAL CHECK. NOTE( I ) INTERVAL 4000 APU HRS
315 316
315A emp
CLEAN AND EXAMINE THE DRAIN FITTING ON EXHAUST DUCT MUFFLER 315 EDUCTOR HOUSING. 316 NOTE( I ) INTERVAL 5000 APU-HRS
315A emp
PERFORM A GENERAL VISUAL INSPECTION OF THE APU DRAIN MAST FOR FLUID LEAKAGE. NOTE( I ) INTERVAL 1600 APU HRS
315A emp
315 316
ITEMS
MPD MRB
49-120-00 MSI 49-120-00 RTE:8
AMM AMM AMTOSS AMM AMM
49-16-12 49-16-11 49-16-11-10 49-16-11-100-801 49-16-12-100-801
MPD MRB
49-180-00 MSI 49-180-00 RTE:9
AMTOSS AMTOSS AMM
49-81-12-10 49-81-12-801 49-81-12-100-801
MPD MRB
49-090-00 MSI 49-090-00 RTE:8
AMTOSS
49-16-11-20
I: 1 s.N
S HHI F1 737-700 E3
5 23-jul-08
I: 1 s.N
E3 HHI S 737-700
8 23-jul-08
I: 1 s.N
E1 HHI 737-700
2 18-mar-05
ATA: 49 - 16
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 49 - 17
491711 20000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU INSULATION PANELS PERFORM A DETAILED INSPECTION OF THE APU INSULATION PANELS. 315 (AFTER APU REMOVAL). 316 NOTE( I ) APU CHANGE
315A emp
ITEMS
MPD MRB
49-040-00 MSI 49-040-00 RTE:8
AMTOSS
49-17-11-20
I: 1 s.N
ATA: 49 - 17
E3 HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
ITEM 49 - 30
R
737-6
MAINTENANCE SCHEDULE
493011 40000
R 493021 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU FUEL SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE FCU, SEALS, FUEL 315 LINES, AND INTERFACING CONNECTIONS FOR LEAKAGE, GENERAL 316 CONDITION, AND SECURITY OF INSTALLATION NOTE( I ) INTERVAL 1600 APU HRS
315A emp
DISCARD THE FUEL INLET FILTER ELEMENT ON THE FUEL CONTROL UNIT 315 (FCU). 316 NOTE( I ) INTERVAL 4000 APU HRS
315A emp
MPD MRB
49-110-00 MSI 49-110-00 RTE:9
AMTOSS
49-31-11-200-801
MPD MRB
49-102-00 MSI 49-102-00 RTE:7 MSI 49-102-00 RTE:9
MRB AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
49-31-21-40 49-31-21-00
I: 1 s.N
E1 HHI 737-700
4 23-jul-08
I: 1 s.N
S
2 03-jun-04
ATA: 49 - 30
HHI 737-700
Page 1 of 1
HHI R E V
ITEM 49 - 41
R
737-6
MAINTENANCE SCHEDULE
494151 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
IGNITION / STARTING PERFORM A DETAILED INSPECTION OF THE IGNITOR PLUG NOTE( I ) INTERVAL 2000 APU HRS
315 316
315A emp
R
Date: 23-jul-08
REFERENCES
ITEMS
MPD MRB
49-132-00 MSI 49-132-00 RTE:7
AMTOSS
49-41-51-20
I: 1 s.N
ATA: 49 - 41
E3 HHI 737-700
2 23-jul-08
Page 1 of 1
HHI R E V
ITEM 49 - 61 496100 70000
R
737-6
MAINTENANCE SCHEDULE
496100 90000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU CONTROLS PERFORM AN OPERATIONAL CHECK OF THE FOLLOWING BY INTERROGATING THE CDU´S APU MAINTENANCE PAGES. -APU DATA MEMORY MODULE ( DMM ) - ELECTRONICS CONTROL UNIT ( ECU ) - SPEED SENSOR - EGT RAKE NOTE( I ) INTERVAL 1600 APU HRS
211
RECORD APU HOURS AND CYCLES VIA THE CDU NOTE( M ) RECORDING IS ALSO REQUIRED AT ECU OR APU CHANGE
210
emp
emp
MPD MRB
49-140-00 MSI 49-140-00 RTE:9
AMTOSS
49-61-00-710-801
I: 1 s.N
F1 HHI 737-700
4 30-nov-05
49-70-00 SERVICE EXPERIENCE
I: 500 FLH
M2 HHI 737-700
2 23-jul-08
empty
AMM
ITEMS
ATA: 49 - 61
Page 1 of 1
HHI R E V
ITEM 49 - 81 498111 20000
R
737-6
MAINTENANCE SCHEDULE
498111 20100
DESCRIPTION
ZONE ACCESS
STRUCTURE
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EXHAUST PERFORM A GENERAL VISUAL INSPECTION INSIDE THE EXHAUST DUCT 315 MUFFLER ( GAS FLOW PATH ) FOR OBVIOUS DAMAGE AND OBSTRUCTION. 316 NOTE( I ) APU CHANGE
315A emp
PERFORM A GENERAL VISUAL INSPECTION OF THE INSULATION BLANKET 317 ON THE EXHAUST DUCT MUFFLER FOR GENERAL CONDITION AND 318 SECURITY OF INSTALLATION
315A 318BR
R 498111 20200
THRESHOLD INTERVAL
REFERENCES
PERFORM A DETAILED INSPECTION OF THE EXHAUST DUCT MUFFLER 317 318 NOTE( I ) INTERVAL 10000 APU HRS
315A 318BR
ITEMS
MPD MRB
49-152-00 MSI 49-152-00 RTE:7
AMTOSS
49-81-11-20
MPD MRB
49-162-00 MSI 49-162-00 RTE:7
AMTOSS AMM
49-81-11-20 49-81-13-200-801
MPD MRB
49-172-00 MSI 49-172-00 RTE:7
AMTOSS
49-81-11-20
I: 1 s.N
E1 HHI 737-700
1 03-jun-04
I: 10000 FLH
E1 HHI 737-700
3 23-jul-08
I: 1 s.N
E3 HHI 737-700
2 03-jun-04
ATA: 49 - 81
Page 1 of 1
HHI R E V
ITEM 49 - 91
R
737-6
MAINTENANCE SCHEDULE
499111 00000
R
499113 20000
499141 20000
499171 20000
499171 21000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
APU EDUCTOR SYSTEM PERFORM A GENERAL VISUAL INSPECTION OF THE LUBE MODULE AND 315 LINES FOR LEAKAGE, GENERAL CONDITION, AND SECURITY OF 316 INSTALLATION. NOTE( I ) INTERVAL 1000 APU HRS
315A emp
PERFORM A DETAILED INSPECTION OF THE OIL FILTER DELTA-P INDICATOR. NOTE( I ) INTERVAL 1000 APU HRS
emp 315A
315 316
PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR ( ON THE 315 APU ) FOR GENERAL CONDITION 316 NOTE( I ) INTERVAL 5000 APU HRS
PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR INLET DUCT (AIR FLOW PATH) FOR OBVIOUS DAMAGE AND OBSTRUCTION (AFTER APU REMOVAL) NOTE( I ) APU CHANGE
315 emp
PERFORM A GENERAL VISUAL INSPECTION OF THE EDUCTOR INLET 317 DUCT (INSIDE THE AIRPLANE TAIL CONE COMPARTMENT) FOR FLUID 318 ACCUMULATION, GENERAL CONDITION, AND SECURITY OF INSTALLATION
315A emp
MPD MRB
49-190-00 MSI 49-190-00 RTE: 9
AMTOSS AMTOSS AMM
49-91-11-40 49-91-11-00 49-91-11-200-801
MPD MRB
49-200-00 MSI 49-200-00 RTE:9
AMTOSS
49-91-13-20
MPD MRB
49-212-00 MSI 49-212-00 RTE:7 MSI 49-212-00 RTE:8
MRB
315A 318BR
315A 318BR
ITEMS
AMTOSS
49-81-41-20
MPD MRB
49-230-00 MSI 49-230-00 RTE:8
AMTOSS
49-91-71-20
MPD MRB
49-220-00 MSI 49-220-00 RTE:8
AMTOSS
49-91-71-20
I: 1 s.N
E1 HHI 737-700
3 23-jul-08
I: 1 s.N
E3 HHI 737-700
2 03-jun-04
I: 1 s.N
E1 HHI 737-700
1 03-jun-04
I: 1 s.N
E1 HHI 737-700
3 03-jun-04
I: 12000 FLH
E1 HHI 737-700
4 22-mar-07
ATA: 49 - 91
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 52 - 11
521100 00000
521100 01000
521100 02000
521100 03000
521100 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOORS PASSENGER ENTRY DOOR GENERAL VISUAL INSPECTION OF THE FORWARD ENTRY DOOR PRESSURE SEAL AND FLAPPER SEALS FOR DEGRADATION.
831
831
MPD MRB
52-050-00 MSI 52-050-00 RTE:6
AMTOSS
52-11-00-20
MPD MRB
52-020-00 MSI 52-020-00 RTE: 9
AMTOSS
12-25-11-64
MPD MRB
52-030-00 MSI 52-030-00 RTE: 9
AMTOSS
52-11-00-20
831 831AW 831AZ 831BZ 831CZ 831DZ 831EZ
MPD MRB
52-010-00 MSI 52-010-00 RTE:9
AMTOSS
12-25-11-64
831
MPD MRB
52-610-00 MSI 52-610-00
LUBRICATE THE FORWARD ENTRY DOOR GUIDE PLATE TRACKS AND 831 ARM ASSEMBLIES (ROD END BEARINGS AND THREADS), THE UPPER AND LOWER HINGE ARM BUSHINGS, GATE HINGES AND THE FUSELAGE HINGE TORQUE TUBE BEARING.
831
DETAILED VISUAL INSPECTION OF THE FORWARD ENTRY DOOR CENTERING GUIDE STUD AND NYLON TRACK PADS CONDITION
831
LUBRICATE THE FORWARD ENTRY DOOR HANDLE, LATCH MECHANISMS, (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS), THE BEARINGS ON THE DOOR HINGE TORQUE TUBE AND THE FWD ENTRY DOOR CONTROL RODS AND STOP RODS.
831
831 emp emp emp emp emp emp
DETAILED VISUAL INSPECTION OF THE FORWARD ENTRY DOOR STOP 831 FITTING AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.
ITEMS
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 1 YRS
S
HHI 737-700
3 30-nov-05
I: 1 YRS
E3 HHI 737-700
3 03-jun-04
I: 2 YRS
S
HHI 737-700
2 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
1 03-jun-04
ATA: 52 - 11
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
521100 05000
521100 06000
521100 09000
521100 09100
521100 09200
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
DETAILED VISUAL INPECTION OF THE FORWARD ENTRY DOOR STOP FITTING AND PINS. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.
831 emp
GENERAL VISUAL INSPECTION OF THE FORWARD ENTRY DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.
831 emp emp emp emp emp emp
831 8311S 831AZ 831BZ 831CZ 831DZ 831EZ
MPD MRB
DETAILED VISUAL INSPECTION OF THE FORWARD AIRSTAIRS DOOR STOP 117 FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR OPENED
1172S 117BL
MPD MRB
GENERAL VISUAL INSPECTION OF THE FORWARD AIRSTAIRS ACCESS DOOR SKIN AND STRUCTURE. E X T E R N A L ACCESS INSPECT WITH DOOR BOTH OPENED AND CLOSED.
117BL
117
GENERAL VISUAL INSPECTION OF THE FORWARD AIRSTAIRS DOOR SKIN 117 AND STRUCTURE. emp I N T E R N A L ACCESS REMOVE INSULATION BLANKET
831 831AW
REFERENCES
1172S 117BL
ITEMS
MPD MRB
MPD MRB
MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
52-620-00 MSI 52-620-00 I: 8 YRS I: 18000 CYC
E3 HHI 737-700
1 03-jun-04
I: 8 YRS I: 18000 CYC
E2 HHI 737-700
2 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
2 03-jun-04
I: 4000 CYC I: 24 MTH
E2 HHI 737-700
1 03-jun-04
I: 18000 CYC I: 8 YRS
E2 HHI 737-700
2 03-jun-04
52-650-00 MSI 52-650-00
52-580-00 MSI 52-580-00
52-590-00 MSI 52-590-00
52-600-00 MSI 52-600-00
ATA: 52 - 11
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 12
521200 00000
521200 00500
521200 01000
521200 01500
521200 02000
521200 02500
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FORWARD AND AFT SERVICE DOORS GENERAL VISUAL INSPECTION OF THE FORWARD SERVICE DOOR PRESSURE SEAL FOR DEGRADATION.
841
GENERAL VISUAL INSPECTION OF THE AFT SERVICE DOOR PRESSURE 844 SEAL FOR DEGRADATION.
841
844
LUBRICATE THE FORWARD SERVICE DOOR GUIDE PLATE TRACKS AND 841 ARM ASSEMBLIES (ROD END BEARINGS AND THREADS), TORQUE TUBE BUSHINGS, THE UPPER AND LOWER HINGE ARM BUSHINGS AND GATE HINGES
841
LUBRICATE THE AFT SERVICE DOOR GUIDE PLATE AND ARM ASSEMBLIES 844 (ROD END BEARINGS AND THREADS), TORQUE TUBE BUSHINGS, THE UPPER AND LOWER HINGE ARM BUSHINGS AND GATE HINGES
844
DETAILED VISUAL INSPECTION OF THE FORWARD SERVICE DOOR CENTERING GUIDE BEARINGS FOR CONDITION
841
DETAILED VISUAL INSPECTION AFT SERVICE DOOR CENTERING GUIDE 844 BEARINGS FOR CONDITION
841
844
ITEMS
MPD MRB
52-050-00 MSI 52-050-00 RTE:6
AMTOSS
52-41-00-20
MPD MRB
52-050-00 MSI 52-050-00 RTE:6
AMTOSS
52-41-00-20
MPD MRB
52-020-00 MSI 52-020-00 RTE: 9
AMTOSS
12-25-13-64
MPD MRB
52-020-00 MSI 52-020-00 RTE: 9
AMTOSS
12-25-13-64
MPD MRB
52-040-00 MSI 52-040-00 RTE: 9
AMTOSS
52-41-00-20
MPD MRB
52-040-00 MSI 52-040-00 RTE: 9
AMTOSS
52-41-00-20
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 1 YRS
S
HHI 737-700
3 30-nov-05
I: 1 YRS
S
HHI 737-700
3 30-nov-05
I: 1 YRS
E3 HHI 737-700
3 03-jun-04
I: 1 YRS
E3 HHI 737-700
3 03-jun-04
ATA: 52 - 12
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
521200 03000
521200 03500
521200 04000
521200 05000
521200 06000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
LUBRICATE THE FORWARD SERVICE DOOR HANDLE, LATCH MECHANISMS 841 (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE. emp emp emp
841 841AW 841AZ 841BZ 841CZ
MPD MRB
52-010-00 MSI 52-010-00 RTE:9
AMTOSS
12-25-13-64
LUBRICATE THE AFT SERVICE DOOR HANDLE, LATCH MECHANISMS 844 (LATCH TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE. emp emp emp
844 844AW 844AZ 844BZ 844CZ
MPD MRB
52-010-00 MSI 52-010-00 RTE:9
AMTOSS
12-25-13-64
DETAILED VISUAL INSPECTIONN OF THE FORWARD AND AFT SERVICE 841 DOOR STOP FITTING AND PINS. 844 E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.
841 844
MPD MRB
52-610-00 MSI 52-610-00
DETAILED VISUAL INSPECTION OF THE AFT AND FORWARD SERVICE DOORS STOP FITTING AND PINS. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINES AND ACCESS PANELS, AS REQUIRED.
841 emp 844 emp
841 841AW 844 844AW
MPD MRB
GENERAL VISUAL INSPECTION OF THE SERVICE DOORSSKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS, AS REQUIRED.
841 emp emp emp emp emp emp 844 emp emp emp emp emp
841 8411S 841AZ 841BZ 841CZ 841DZ 841EZ 8441S 844AZ 844BZ 844CZ 844DZ 844EZ
MPD MRB
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 2 YRS
S
HHI 737-700
2 03-jun-04
I: 2 YRS
S
HHI 737-700
0 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
1 03-jun-04
I: 8 YRS I: 18000 CYC
E3 HHI 737-700
1 03-jun-04
I: 18000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
52-620-00 MSI 52-620-00
52-650-00 MSI 52-650-00
ATA: 52 - 12
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 13
521300 00000
521300 01000
521300 02000
521300 03000
521300 04000
521300 05000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AFT ENTRY DOOR GENERAL VISUAL INSPECTION OF THE AFT ENTRY DOOR PRESSURE SEAL FOR DEGRADATION.
834
834
LUBRICATE THE AFT ENTRY DOOR GUIDE PLATE TRACKS AND ARM 834 ASSEMBLIES (ROD END BEARINGS AND THREADS), THE UPPER AND LOWER HINGE ARM BUSHINGS, GATE HINGES AND THE FUSELAGE HINGE TORQUE TUBE BEARING.
834
DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR CENTERING GUIDE BEARINGS FOR CONDITION
834
834
MPD MRB
52-050-00 MSI 52-050-00 RTE:6
AMTOSS
52-13-00-20
MPD MRB
52-020-00 MSI 52-020-00 RTE: 9
AMTOSS
12-25-12-64
MPD MRB
52-040-00 MSI 52-040-00 RTE: 9
AMTOSS
52-13-00-20
LUBRICATE THE AFT ENTRY DOOR HANDLE, LATCH MECHANISMS (LATCH 834 TORQUE TUBE BEARINGS AND LATCH CONTROL RODS) AND THE emp BEARINGS ON THE DOOR HINGE TORQUE TUBE.. emp emp emp
834 834AW 834AZ 834BZ 834CZ
MPD MRB
52-010-00 MSI 52-010-00 RTE:9
AMTOSS
12-25-12-64
DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR STOP FITTING 834 AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.
834
MPD MRB
52-610-00 MSI 52-610-00
DETAILED VISUAL INSPECTION OF THE AFT ENTRY DOOR STOP FITTING 834 AND PINS. emp I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS AS REQUIRED.
834 834AW
ITEMS
MPD MRB
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 1 YRS
S
HHI 737-700
3 30-nov-05
I: 1 YRS
E3 HHI 737-700
3 03-jun-04
I: 2 YRS
S
HHI 737-700
3 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
1 03-jun-04
I: 18000 CYC I: 8 YRS
E3 HHI 737-700
1 03-jun-04
52-620-00 MSI 52-620-00
ATA: 52 - 13
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
521300 06000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE AFT ENTRY DOOR SKIN AND STRUCTURES. I N T E R N A L ACCESS REMOVE INSULATION, INTERIOR LINERS AND ACCESS PANELS, AS REQUIRED.
ZONE ACCESS 834 emp emp emp emp emp emp
STRUCTURE
834 8341S 834AZ 834BZ 834CZ 834DZ 834EZ
ITEMS
REFERENCES MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
52-650-00 MSI 52-650-00 I: 8 YRS I: 18000 CYC
ATA: 52 - 13
E2 HHI 737-700
1 03-jun-04
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 22
522200 00000
522200 01000
522200 02000
522200 03000
522200 04000
522200 05000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EMERGENCY EXIT DOOR OPERATIONALLY CHECK THE FLIGHT LOCK MECHANICAL SWITCHES FOR 833 THE AUTOMATIC OVERWING EXIT DOORS 843
OPERATIONALLY CHECK THE AUTOMATIC OVERWING EXIT DOORS.
DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR LATCH ROLLERS, LINKS AND PIVOT FITTINGS/JOINTS.
833 843
833 843
833 843
MPD MRB
52-210-00 MSI 52-210-00 RTE:7
AMTOSS
52-22-00-71
MPD MRB
52-220-00 MSI 52-220-00 RTE:8
AMTOSS
52-22-00-71
833 emp 843 emp
833 833AZ 843 843AZ
MPD MRB
52-230-00 MSI 52-230-00 RTE:8
AMTOSS
52-22-00-21
DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR STOP FITTINGS AND PINS. E X T E R N A L ACCESS INSPECT WITH DOORS OPENED AND LINING NOT REMOVED.
833 843
833 843
MPD MRB
52-730-00 MSI 52-730-00
OPERATIONALLY CHECK THE FLIGHT LOCK ENGAGEMENT AND DISENGAGEMENT.
833 843
DETAILED VISUAL INSPECTION OF THE AUTOMATIC EMERGENCY DOOR 833 FLIGHT LOCKS FOR CORROSION AND CONDITION. emp 843 emp
833 843
833 833AZ 843 843AZ
ITEMS
MPD MRB
52-240-00 MSI 52-240-00 RTE:8
AMTOSS
52-22-00-71
MPD MRB
52-250-00 MSI 52-250-00 RTE:8
AMTOSS
52-22-00-21
I: 4000 FLH
F1 HHI 737-700
3 03-jun-04
I: 2 YRS
F1 HHI 737-700
2 03-jun-04
I: 2 YRS
E3 HHI 737-700
2 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
3 18-mar-05
I: 2 YRS
F1 HHI 737-700
2 03-jun-04
I: 2 YRS
E3 HHI 737-700
2 03-jun-04
ATA: 52 - 22
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
522200 06000
GENERAL VISUAL INSPECTION OF THE AUTOMATIC EMERGENCY EXIT DOOR PRESSURE SEALS FOR DEGRADATION.
522200 07000
522200 07500
Date: 23-jul-08
ZONE ACCESS 833 843
STRUCTURE
833 843
REFERENCES MPD MRB
52-260-00 MSI 52-260-00 RTE:6
AMTOSS
52-22-00-20 52-740-00 MSI 52-740-00
DETAILED VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS INSPECT WITH HATCHES REMOVED, THE DOOR OPENED OR REMOVED. REMOVE LININGS AND INSULATIONS.
833 emp 843 emp
833 8331S 843 8431S
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS INSPECT WITH HATCHES REMOVED, THE DOOR REMOVED OR OPENED. REMOVE LININGS AND INSULATIONS.
833 emp 843 emp
833 8331S 843 8431S
MPD MRB
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 2 YRS
E2 HHI 737-700
2 03-jun-04
I: 8 YRS I: 18000 CYC
E3 HHI 737-700
2 18-mar-05
I: 8 YRS I: 18000 CYC
E2 HHI 737-700
3 18-mar-05
52-760-00 MSI 52-760-00
ATA: 52 - 22
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 31
523100 00000
523100 00500
523100 01000
523100 01500
523100 02000
523100 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CARGO DOOR GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 821 DOOR PRESSURE SEAL FOR DEGRADATION.
GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT DOOR 822 PRESSURE SEAL FOR DEGRADATION.
LUBRICATE THE FORWARD CARGO COMPARTMENT DOOR LATCH 821 TORQUE TUBE BEARINGS AND THE COUNTER BALANCE IDLER CRANK.
LUBRICATE THE AFT CARGO COMPARTMENT DOOR LATCH TORQUE TUBE BEARINGS AND THE COUNTER BALANCE IDLER CRANK.
822
821
822
821
822
DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR 821 STOP FITTINGS AND PINS. 822 E X T E R N A L ACCESS INSPECT WITH DOORS OPENED. LINING NOT REMOVED.
821 822
OPERATIONALLY CHECK THE FORWARD AND AFT CARGO COMPARTMENT 821 DOOR SNUBBER. 822
821 822
ITEMS
MPD MRB
52-100-00 MSI 52-100-00 RTE:6
AMTOSS
52-31-00-20
MPD MRB
52-100-00 MSI 52-100-00 RTE:6
AMTOSS
52-31-00-20
MPD MRB
52-090-00 MSI 52-090-00 RTE: 9
AMTOSS
12-25-31-64
MPD MRB
52-090-00 MSI 52-090-00 RTE: 9
AMTOSS
12-25-31-64
MPD MRB
52-670-00 MSI 52-670-00
MPD MRB
52-110-00 MSI 52-110-00 RTE:9
AMTOSS
52-31-13-710-802
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 4000 FLH
E2 HHI 737-700
3 03-jun-04
I: 1 YRS
S
HHI 737-700
2 03-jun-04
I: 1 YRS
S
HHI 737-700
2 03-jun-04
I: 4000 CYC I: 24 MTH
E3 HHI 737-700
2 03-jun-04
I: 8000 FLH
F1 HHI 737-700
4 03-jun-04
ATA: 52 - 31
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
523100 05000
DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS REMOVE INSULATION BLANKET
821 emp 822 emp
821 8211S 822 8221S
MPD MRB
DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT CARGO DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS REMOVE INSULATION BLANKET
821 emp 822 emp
821 8211S 822 8221S
MPD MRB
523100 06000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
52-680-00 MSI 52-680-00 I: 8 YRS I: 18000 CYC
E3 HHI 737-700
1 03-jun-04
I: 18000 CYC I: 8 YRS
E3 HHI 737-700
1 03-jun-04
52-710-00 MSI 52-710-00
ATA: 52 - 31
Page 2 of 2
HHI R E V
ITEM 52 - 48 524800 00000
R
737-6
MAINTENANCE SCHEDULE
524800 02000
R
524800 03000
524800 04000
524800 07000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EQUIPMENT COMPARTMENT EXTERIOR DOORS GENERAL VISUAL INSPECTION OF THE E / E ACCESS DOOR PRESSURE 117 SEAL FOR DEGRADATION. 118
117A emp
DETAILED VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 ACCESS DOOR STOP FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR REMOVED
117 117A
DETAILED VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 ACCESS DOOR STOP FITTINGS AND PINS. I N T E R N A L ACCESS INSPECT WITH DOOR AND ACCESS PANEL REMOVED. REMOVE DAGGER PINS AS REQUIRED.
117A
GENERAL VISUAL INSPECTION OF THE E/E EQUIPMENT COMPARTMENT 117 DOOR SKIN AND STRUCTURE. I N T E R N A L ACCESS INSPECT WITH DOOR AND ACCESS PANEL REMOVED. REMOVE DAGGER PINS AS REQUIRED.
117A
LUBRICATE THE E/E ACCESS DOOR HANDLE LATCHING MECHANISM (RACK AND PINION GEAR AND THE LOCK PINS).
117A emp
117 118
ITEMS
MPD MRB
52-130-00 MSI 52-130-00 RTE:6
AMTOSS
52-48-41-20
MPD MRB
52-540-00 MSI 52-540-00
MPD MRB
MPD MRB
I: 4000 FLH
E2 HHI 737-700
2 03-jun-04
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
3 23-jul-08
I: 8 YRS I: 18000 CYC
E3 HHI 737-700
2 05-sep-06
I: 8 YRS I: 18000 CYC
E2 HHI 737-700
2 05-sep-06
I: 2 YRS
S
2 03-jun-04
52-550-00 MSI 52-550-00
52-570-00 MSI 52-570-00
MPD MRB
52-120-00 MSI 52-120-00 RTE:9
AMTOSS
12-25-41-64
ATA: 52 - 48
HHI 737-700
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 49
524900 00000
524900 01000
524900 02000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ACCESS AND BLOWOUT DOOR DETAILED VISUAL INSPECTION OF THE FORWARD ACCESS DOOR STOP 112 FITTINGS AND PINS. emp E X T E R N A L ACCESS INSPECT WITH DOOR OPENED. LINING NOT REMOVED.
1121S 112A
GENERAL VISUAL INSPECTION OF THE FORWARD ACCESS DOOR PRESSURE SEAL FOR DEGRADATION.
112A
112
GENERAL VISUAL INSPECTION OF THE FORWARD ACCESS DOOR SKIN 112 AND STRUCTURE. emp I N T E R N A L ACCESS INSPECT WITH DOOR REMOVED.
1121S 112A
ITEMS
MPD MRB
52-510-00 MSI 52-510-00
MPD MRB
52-140-00 MSI 52-140-00 RTE:6
AMTOSS
52-48-31-20
MPD MRB
52-530-00 MSI 52-530-00
I: 24 MTH I: 4000 CYC
E3 HHI 737-700
2 03-jun-04
I: 8000 FLH
E2 HHI 737-700
1 03-jun-04
I: 18000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
ATA: 52 - 49
Page 1 of 1
HHI R E V
ITEM 52 52 - 60
N
526000 00000
N
N
526000 01000
N
N
737-6
MAINTENANCE SCHEDULE
526050 21000
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOORS AIR STAIRS LUBRICATE THE AIRSTAIR DOOR SYSTEM, (INCLUDES TWO ROLLERS, 117 THE CARRIAGE DRIVE BALL BEARING, DRIVE NUT IN JACKSCREW, LOCK emp PIN GREASE FITTING AND FOUR BEARINGS IN THE CARRIAGE ROLLERS). (APPLICABLE IF AIRSTAIR SYSTEM OR PARTIAL AIRSTAIR SYSTEM WITH ROLLER AND CARRIAGE DRIVE IS INSTALLED.)
117A 117BL
LUBRICATE THE AIRSTAIR SYSTEM PER THE MANUFACTURER'S 117 RECOMMENDATIONS (IF INSTALLED). NOTE( I ) STANDARD MAINTENANCE IS TO APPLY LUBRICANT PER MIL-G-23827 EVERY 300 COMPLETE CYCLES OR 1000 FLIGHT HOURS OR 6 MONTHS TIME, WHICHEVER OCCURS FIRST, AT ALL LUBRICATION POINTS (REF: MONOGRAM SYSTEMS (FORMERLY WEBER AIRCRAFT)-COMPONENT MAINTENANCE MANUAL 52-60-10; AIRSTAIR LUBRICATION DIAGRAM-FIGURE701).
117BL
INSPECT (GENERAL VISUAL) THE AIRSTAIR DOOR PRESSURE SEAL FOR 117 DEGRADATION (IF INSTALLED). emp
117A 117BL
N
Date: 30-jul-08
REFERENCES
ITEMS
MPD MRB
52-150-00 MSI 52-150-00 RTE:7
AMM
12-25-14-600
MPD MRB
52-160-00 MSI 52-160-00 RTE:7
AMM
12-25-71-600
MPD MRB
52-180-00 MSI 52-180-00 RTE:6
AMM
52-61-50-210
I: 1 YRS
LU HHI 737-700 only: D-AHIB
0 23-jul-08
I: 1 s.N
LU HHI 737-700 only: D-AHIB
0 23-jul-08
I: 4000 FLH
GV HHI 737-700 only: D-AHIB
0 23-jul-08
ATA: 52 - 60
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 70
527000 00000
527000 01000
527000 02000
527000 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COCKPIT DOOR PERFORM A FUNCTIONAL CHECK OF THE LOCKING AND UNLOCKING 221 LATCH BOLT MECHANISM ON THE FLIGHT DECK DOOR DECOMPRESSION 222 PANEL. NOTE( E, I ) NOTE (E): APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. NOTE (I): THE EQUIVALENT CMR TASK (52-CMR-01) IS PERFORMED AT 3000 HOURS, WHICH HAS PRECEDENCE OVER THE MRB INTERVAL OF 30000 HOURS. REFER TO MS 527000 07000.
emp emp
OPERATIONALLY CHECK THE FLIGHT DECK DOOR DECOMPRESSION 221 PANEL HINGES. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.
emp emp
GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR 221 DECOMPRESSION PANEL HINGES FOR CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.
emp emp
GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR SEALS FOR 221 CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.
emp emp
ITEMS
MPD MRB
52-360-00 MSI 52-360-00 RTE:8
SB AMTOSS
CDRB 22-1-18 52-51-00-71
MPD MRB
52-370-00 MSI 52-370-00 RTE:8
SB AMTOSS
CDRB 22-1-18 52-51-00-71
MPD MRB
52-380-00 MSI 52-380-00 RTE:8
SB AMTOSS
CDRB 22-1-18 52-51-00-71
MPD MRB
52-390-00 MSI 52-390-00 RTE:8
SB AMTOSS
CDRB 22-1-18 52-51-00-71
I: 30000 FLH
F2 HHI 737-700
4 30-nov-05
I: 30000 FLH
F1 HHI 737-700
2 03-jun-04
I: 30000 FLH
E2 HHI 737-700
2 03-jun-04
I: 6000 FLH
E2 HHI 737-700
2 03-jun-04
ATA: 52 - 70
Page 1 of 4
HHI R E V
ITEM 527000 04000
R
527000 05000
R
R
737-6
MAINTENANCE SCHEDULE
527000 07000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FLIGHT DECK DOOR 221 DECOMPRESSION PANEL SEALS FOR CONDITION AND SECURITY. 222 NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.
emp emp
FUNCTIONALLY CHECK THE DENY TIME DELAY FUNCTION OF THE FLIGHT 221 DECK SECURITY DOOR ACCESS SYSTEM TO VERIFY OPERATION OF THE 222 THREE POSITION ROTARY SWITCH IN THE P8 PANEL, THE DENY FUNCTION, AND REVERSION TO THE DEFAULT MODE. NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS.
emp emp
PERFORM A FUNCTIONAL CHECK OF THE LOCKING AND UNLOCKING 221 LATCH BOLT MECHANISM ON THE FLIGHT DECK DOOR DECOMPRESSION 222 PANEL. NOTE( E, R ) NOTE (E): APPLICABLE TO AIRPLANES L/N 1221 AND ON, AND L/N 1-1220 THAT HAVE INCORPORATED ENHANCED FLIGHT DECK SECURITY PHASE II COCKPIT DOOR NOTE (R): CMR B22-69-1 IS INCLUDED IN C&D AEROSPACE REPORT CDRB 22-69 REV. E, DATED NOVEMBER 8, 2002.
emp emp
STRUCTURE
REFERENCES MPD MRB
52-400-00 MSI 52-400-00 RTE:8
SB AMTOSS
CDRB 22-1-18 52-51-00-71
MPD MRB
52-410-00 MSI 52-410-00 RTE:6
SB AMTOSS
CDRB 22-1-18 52-51-00-70
AAR AAR SB AMM
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 30000 FLH
E2 HHI 737-700
2 03-jun-04
I: 6000 FLH
F2 HHI 737-700
4 23-jul-08
I: 3000 FLH
F2 HHI 737-700
3 23-jul-08
52-CMR-01 ONE STAR CMR B22-69-1 ONE STAR CDRB 22-1-18 52-51-08
ATA: 52 - 70
Page 2 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
527001 00000
R
527001 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
INTERNAL - DETAILED: FLIGHT DECK SECURITY DOOR PANEL ASSEMBLY. 221 INSPECT FLIGHT DECK SECURITY DOOR ASSEMBLY, INCLUDING MAIN 222 DOOR PANEL ASSY., MAIN DOOR PANEL BOND ASSY., AND ARMOR LAMINATE ASSY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISASSEMBLE DOOR ONLY IF EVIDENCE OF DAMAGE, FATIGUE, DELAMINATION, AND OR BULGING IS FOUND
emp emp
EXTERNAL - GENERAL VISUAL: FLIGHT DECK SECURITY DOOR SURROUND 221 ASSEMBLY. 222 INSPECT FLIGHT DECK SECURITY DOOR SURROUND ASSEMBLY, INCLUDING HEADER ASSEMBLY, POST ASSEMBLY (RIGHT HAND POST), LATCH AND DEADBOLT RECEIVER ASSEMBLY, SUPPORT STRUCTURE, POST COVER ARMOR ASSEMBLY AND HINGE ASSEMBLY. E X T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS AS VISIBLE WITH CARPET, TAPESTRIES (IF EQUIPPED) AND KICK STRIPS DISPLACED.
emp emp
STRUCTURE
ITEMS
REFERENCES MPD MRB
52-450-00 MSI 52-450-00
SB
CDRB 22-1-18
MPD MRB
52-460-00 MSI 52-460-00
SB
CDRB 22-1-18
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 16000 CYC I: 3000 DAY
E3 HHI 737-700
4 23-jul-08
I: 8000 CYC I: 1500 DAY
E2 HHI 737-700
2 03-jun-04
ATA: 52 - 70
Page 3 of 4
HHI R E V
ITEM
R
527001 02000
R
R
737-6
MAINTENANCE SCHEDULE
527001 04000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
INTERNAL - DETAILED: FLIGHT DECK SECURITY DOOR SURROUND 221 ASSEMBLY. 222 INSPECT FLIGHT DECK SECURITY DOOR SURROUND ASSEMBLY, INCLUDING HEADER ASSEMBLY, POST ASSEMBLY (RIGHT HAND POST), LATCH AND DEADBOLT RECEIVER ASSEMBLY, SUPPORT STRUCTURE, POST COVER ARMOR ASSEMBLY AND HINGE ASSEMBLY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISPLACE INTERIOR FURNISHINGS INCLUDING CLOSETS, LAVS, GALLEYS (IF EQUIPPED) ADJACENT TO DOOR FRAME, AND CEILING PANELS ABOVE DOOR. REMOVE ARMOR FROM DOOR FRAME.
emp emp
INTERNAL - DETAILED: FLIGHT DECK DOOR LATCH AND HINGE SUPPORT 221 ASSEMBLIES. 222 I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANE L/N 1221 AND ON AND TO THOSE AIRPLANES WITH THE NEW FLIGHT DECK SECURITY DOOR INSTALLED BY THE CUSTOMER SPECIFIC BOEING SERVICE BULLETINS. ACCESS DISASSEMBLE DOOR ONLY IF EVIDENCE OF DAMAGE, FATIGUE, DELAMINTION, AND OR BULGING IS FOUND
emp emp
STRUCTURE
ITEMS
REFERENCES MPD MRB
52-470-00 MSI 52-470-00
SB AMM AMM
CDRB 22-1-18 51-05-01-210 52-05-03-211
MPD MRB
52-490-00 MSI 52-490-00
SB AMM AMM
CDRB 22-1-18 51-05-01-210 52-05-03-211
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
I: 16000 CYC I: 3000 DAY
E3 HHI 737-700
3 23-jul-08
I: 16000 CYC I: 3000 DAY
E3 HHI 737-700
4 23-jul-08
ATA: 52 - 70
Page 4 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 52 - 71
527100 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
DOOR WARNING SYSTEM OPERATIONALLY CHECK THE DOOR SENSORS (PROXIMITY OR MECHANICAL SWITCHES AS APPLICABLE) FOR THE PASSENGER CABIN ENTRY / SERVICE, E / E ACCESS, AUTOMATIC OVERWING EXIT, FORWARD ACCESS, CARGO DOORS AND AIRSTAIR DOOR PROXIMITY SENSOR (AS APPLICABLE, IF AIRSTAIRS SYSTEM INCLUDING STAIRS INSTALLED).
112 117 emp 211 212 800 emp emp emp emp emp emp emp
112A 117A 117BL emp emp 821 822 831 833 834 841 843 844
ITEMS
MPD MRB
52-200-00 MSI 52-200-00 RTE:9
AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS AMTOSS
52-71-11-71 52-71-42-71 52-71-41-71 52-71-31-71 52-71-21-71 52-71-61-71
I: 4000 FLH
ATA: 52 - 71
F1 HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
ITEM 53 53 - 09 530900 00000
R
737-6
MAINTENANCE SCHEDULE
530900 01000
R
530900 02000
530900 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUSELAGE BODY UPPER DETAILED VISUAL INSPECTION OF THE DOOR FRAMES, STOPS, LATCHES AND HINGES ON FORWARD AND AFT ENTRY AND GALLLEY DOOR CUTOUT SURROUND STRUCTURES. E X T E R N A L ACCESS OPEN FWD AND AFT ENTRY AND GALLEY DOORS
221 222 emp emp emp 241 242
emp 831 834 841 844 emp emp
MPD MRB
DETAILED VISUAL INSPECTION OF THE FORWARD AND AFT ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE (THE DOOR CUTOUT TO, AND INCLUDING THE DOOR SIDE FIRST FRAME OF THE DOOR). I N T E R N A L ACCESS REMOVE GALLEYS/LAVS. REMOVE CABIN INTERIOR AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
221 222 emp 241 242
emp 2001S 222AR emp emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE AUTOMATIC OVERWING EXIT CUTOUT STRUCTURE, FITTINGS AND STOPS. E X T E R N A L ACCESS OPEN AUTOMATIC OVERWING EXITS.
231 232 emp
emp 833 843
MPD MRB
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREAS ( WITHIN APPROXIMATELY 20 INCHES FROM DOORS, GALLEYS AND LAVS) FROM LOWER LOBE. I N T E R N A L ACCESS REMOVE CEILING, SIDEWALL PANELS, INSULATION BLANKETS OF FWD AND AFT CARGO COMPARTMENT AS REQUIRED. REMOVE FORWARD AIRSTAIRS AND AIRSTAIRS COMPARTMENT (IF INSTALLED).
113 114 117 118 121 122 125 126 141 142 145 146
S1002 emp 117BL emp emp emp emp emp emp emp emp emp
MPD MRB
ITEMS
53-310-00 MSI 53-310-00 I: 4000 CYC I: 24 MTH
E3 HHI 737-700
2 18-mar-05
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E3 HHI 737-700
2 23-jul-08
I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 03-jun-04
T: 8 YRS I: 6 YRS
E2 HHI 737-700
1 03-jun-04
53-360-00 MSI 53-360-00
53-290-00 MSI 53-290-00
53-110-00 MSI 53-110-00
ATA: 53 - 09
Page 1 of 6
HHI R E V
R
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
530900 04000
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREA (WITHIN APPROXIMATELY 20 INCHES FROM DOORS, GALLEYS AND LAVS, AND THE FLOOR STRUCTURE BELOW THE DOOR TO AND INCLUDING THE DOORSIDE OF THE FIRST FRAME OF THE DOOR). I N T E R N A L ACCESS REMOVE GALLEYS, LAVS, FLOOR PANELS, SIDEWALLS AND INSULATION BLANKETS AS REQUIRED.
221 222 231 232 241 242
2003S emp emp emp emp emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREA INSPECT GALLEY AND LAV ATTACH FITTINGS AND ANY OTHER EASILY VISIBLE PORTIONS OF THE FLOOR STRUCTURE IN WET AREA (WITHIN APPROXIMATELY 20 INCHES FROM GALLEYS AND LAVS, AND THE FLOOR STRUCTURE BELOW THE DOOR TO AND INCLUDING THE DOORSIDE OF THE FIRST FRAME FROM THE DOOR). I N T E R N A L ACCESS GALLEYS AND LAVS REMOVAL IS NOT REQUIRED. REMOVE GALLEY KICK-PLATES AND ANY OTHER EASILY REMOVABLE PANELS FOR INSPECTION.
221 222 231 232 241 242
2004S emp emp emp emp emp
MPD MRB
GENERAL VISUAL INSPECTION OF FORWARD AND AFT CARGO COMPARTMENT FLOOR STRUCTURE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS.
121 122 141 142
1003S emp emp emp
MPD MRB
112A
MPD MRB
530900 05000
R
530900 06000
530900 07000
Date: 23-jul-08
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT FLOOR 112 STRUCTURE FROM LOWER LOBE. I N T E R N A L
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-380-00 MSI 53-380-00 T: 8 YRS I: 6 YRS
E2 HHI 737-700
1 03-jun-04
T: 8 YRS I: 3 YRS
E2 HHI 737-700
2 23-jul-08
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E2 HHI 737-700
1 03-jun-04
I: 10 YRS
E2 HHI 737-700
1 03-jun-04
53-390-00 MSI 53-390-00
53-140-00 MSI 53-140-00
53-080-00 MSI 53-080-00
ATA: 53 - 09
Page 2 of 6
HHI R E V
ITEM
R
530900 08000
R
530900 09000
R
530900 10000
R
R
737-6
MAINTENANCE SCHEDULE
530900 11000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT FLOOR 211 STRUCTURE. 212 I N T E R N A L ACCESS REMOVE SIDEWALLS AND FLOOR PANELS AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
2102S emp
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN DRY AREAS ( AWAY FROM DOORS, GALLEYS AND LAVS) FROM LOWER LOBE. I N T E R N A L ACCESS REMOVE CEILING, SIDEWALL PANELS, INSULATION BLANKETS. REMOVE FORWARD AIRSTAIRS AND AIRSTAIRS COMPARTMENT (IF INSTALLED).
113 114 117 emp 118 121 122 125 126 141 142 145 146
emp emp 1001S 117BL emp emp emp emp emp emp emp emp emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE FLIGHT COMPARTMENT, 211 INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), 212 CIRCUMFERENTIAL SKIN AND STRINGER SPLICE, CREW CABIN WINDOW CUTOUT STRUCTURE, AND FORWARD PRESSURE BULKHEAD. I N T E R N A L ACCESS REMOVE GLARE SHIELD, LINERS, OVERHEAD UNITS AND PANELS. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
2101S emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT 221 FROM STA 259.5 TO 360 (EXCEPT AREAS AROUND DOOR CUTOUTS), 222 INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES. I N T E R N A L ACCESS REMOVE GALLEYS/LAVS. REMOVE CABIN INTERIOR AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
2201S emp
ITEMS
MPD MRB
MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-340-00 MSI 53-340-00 I: 10 YRS
E2 HHI 737-700
2 23-jul-08
I: 12 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 23-jul-08
T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
E2 HHI 737-700
2 23-jul-08
53-100-00 MSI 53-100-00
53-330-00 MSI 53-330-00
53-350-00 MSI 53-350-00
ATA: 53 - 09
Page 3 of 6
HHI R E V
ITEM 530900 12000
R
737-6
MAINTENANCE SCHEDULE
530900 13000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
GENERAL VISUAL INSPECTION OF PASSENGER COMPARTMENT FROM 231 STA 360 TO 663.75, INCLUDING: 232 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), emp LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.WINDOW BELT STRUCTURE; 3.OVERWING EMERGENCY EXIT CUTOUT STRUCTURE; 4.FORWARD CARGO DOOR CUTOUT SURROUND STRUCTURE (PORTION IN UPPER LOBE); 5.STA 540 AND 663 BULKHEADS AND SPLICES; 6.OVERWING FRAMES AND STUB BEAMS. ATTENTION TO SKIN DAMAGE AROUND CRITICAL AERODYNAMIC AREAS OF THE FUSELAGE AT A/C OPERATING WITH RVSM (PITOT AND FLUSH STATIC PROBES AREA). I N T E R N A L ACCESS REMOVE CABIN INTERIOR AND INSULATION BLANKETS. OPEN AUTOMATIC OVERWING EXIT DOORS.
S2301 833 843
MPD MRB
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT FLOOR STRUCTURE IN DRY AREA (AWAY FROM DOORS, GALLEYS AND LAVS). EXCLUDE FLOOR STRUCTURE FROM STA 540 TO 727. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND SIDEWALLS AS REQUIRED. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
2002S emp emp emp emp emp
MPD MRB
221 222 231 232 241 242
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-400-00 MSI 53-400-00 T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
E2 HHI 737-700
4 03-jun-04
I: 12 YRS
E2 HHI 737-700
2 23-jul-08
53-370-00 MSI 53-370-00
ATA: 53 - 09
Page 4 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
530900 14000
530900 15000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE PASSENGER COMPARTMENT 241 FROM STA 663.75 TO 1016 (EXCEPT AREAS AROUND DOOR CUTOUTS), 242 INCLUDING: 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.WINDOW BELT STRUCTURE; 3.STA 663 BULKHEAD AND SPLICES; 4.STA 727 BULKHEAD; 5.SIDE STRUT SUPPORT FRAME AT STA 706; 6.MAIN LANDING GEAR SUPPORT FRAMES AT STA 695 AND 716; 7.WHEEL WELL FRAME AT STA 685; 8.AFT CARGO DOOR CUTOUT SURROUND STRUCTURE (PORTION IN UPPER LOBE); 9.FORWARD SIDE OF STA 1016 BULKHEAD (CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS), INCLUDING VERTICAL FIN FRONT SPAR FITTINGS; 10.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. I N T E R N A L ACCESS REMOVE GALLEYS/LAVS, CABIN INTERIOR AND INSULATION BLANKETS.
2401S emp
GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE ABOVE 135 WING BOX CENTER SECTION UPPER PANEL, INCLUDING SIDE SKIN 136 PANELS (SKINS, FRAMES AND STRINGERS), STA 540 BULKHEAD, AND OVERWING FRAMES AND STUB BEAMS. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION BLANKETS.
S1301 emp
STRUCTURE
ITEMS
REFERENCES MPD MRB
MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-410-00 MSI 53-410-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS
E2 HHI 737-700
1 03-jun-04
53-190-00 MSI 53-190-00
ATA: 53 - 09
Page 5 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
530900 16000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE ABOVE 137 MAIN LANDING GEAR WHEEL WELL, INCLUDING: 138 1.PRESSURE DECK WEB TO STIFFENERS, STIFFENER ATTACHMENT TO FLOOR BEAM AT STA 727; 2.SIDE SKIN PANELS, CIRCUMFERENTIAL SKIN AND STRINGER SPLICE; 3.BULKHEADS AT STA 663 AND 727; 4.SIDE STRUT SUPPORT FRAME AT STA 706; 5.MAIN LANDING GEAR SUPPORT FRAME AT STA 695 AND 716; 6.WHEEL WELL FRAME AT STA 685. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION BLANKETS.
STRUCTURE
S1302 emp
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
53-200-00 MSI 53-200-00 T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS
ITEMS
TSK
ATA: 53 - 09
E2 HHI 737-700
1 03-jun-04
Page 6 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 13
531300 00000
531300 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
TAIL SECTION GENERAL VISUAL INSPECTION OF THE AREA AFT OF STA 1016 PRESSURE 311 BULKHEAD TO STA 1088, INCLUDING: 312 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.AFT SIDE OF STA 1016 BULKHEAD (CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS) 3.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. 4.STA 1088 BULKHEAD, INCLUDING VERTICAL FIN REAR SPAR FITTINGS AND HORIZONTAL STABILIZER CENTER SECTION JACKSREW FITTING LUGS AND BOLTS. I N T E R N A L
311BL emp
GENERAL VISUAL INSPECTION OF THE STABILIZER TORSION BOX COMPARTMENT AND APU COMPARTMENT, INCLUDING: 1.SKIN PANELS (SKINS, FRAMES AND STRINGERS), LONGITUDINAL LAP SPLICES 2.STA 1088 BULKHEAD, INCLUDING VERTICAL FIN REAR SPAR FITTINGS; 3.FORWARD SIDE OF STA 1156 BULKHEAD, INCLUDING HORIZONTAL STABILIZER HINGE FITTINGS AND BOLTS; 4.UPPER HORIZONTAL DECK (AT STRINGER 6) AND LOWER HORIZONTAL DECK (AT STRINGER 12). I N T E R N A L ACCESS FOR AREA BELOW STRINGER 12, REMOVE APU FIREWALLS AND APU PLENUM. FOR AREA ABOVE STRINGER 12, ADJUST STABILIZER TRIM AS REQUIRED. FOR ACCESS TO STA 1156 HORIZONTAL STABILIZER HINGE FITTING LUGS AND BOLTS, REMOVE HORIZONTAL STABILIZER REAR SPAR SLIDING SEAL AS REQUIRED. ACCESS PANELS 333BT AND 343 BT NOT ON ALL A/C'S.
311BL emp 315A 3101S 331A 332AB 332AT 333AB 333AT 333BT 341A 342AB 342AT 343AB 343AT
313 314 315 316 emp emp emp emp emp emp emp emp emp emp emp
ITEMS
MPD MRB
MPD MRB
53-420-00 MSI 53-420-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 22-mar-07
53-430-00 MSI 53-430-00
ATA: 53 - 13
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
531300 02000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE AFT SIDE OF STA 1156 BULKHEAD. 317 I N T E R N A L 318 ACCESS
STRUCTURE
318BR emp
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
53-440-00 MSI 53-440-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ITEMS
TSK
ATA: 53 - 13
E2 HHI 737-700
1 03-jun-04
Page 2 of 2
HHI R E V
ITEM 53 - 15 531500 00000
R
531500 01000
R
R
737-6
MAINTENANCE SCHEDULE
531500 02000
R
531500 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NOSE AND MAIN LANDING GEAR WHEEL WELL GENERAL VISUAL INSPECTION OF THE KEEL BEAM IN WHEEL WELL 139 (STA663.75 TO 727), INCLUDING KEEL BEAM CHORDS, WEBS, STIFFENERS, 193 SPLICE, KEEL BEAM/REAR SPAR ATTACHMENT ANGLES. emp I N T E R N A L
emp 193B 193D
MPD MRB
GENERAL VISUAL INSPECTION OF THE NOSE LANDING GEAR WHEEL WELL, INCLUDING CANTED BULKHEAD (STA 224.8 TO 227.8), STA 294.5 BULKHEAD, SIDE AND TOP PANELS, TRUNNION SUPPORT FITTING, ACTUATOR SUPPORT FITTING, AND DRAG BRACE FITTING. E X T E R N A L
115 116
emp emp
MPD MRB
53-020-00 MSI 53-020-00
AMM AMM
51-05-01-210 53-05-03-210
GENERAL VISUAL INSPECTION OF THE MAIN LANDING GEAR WHEEL WELL, INCLUDING: 1. PRESSURE DECK WEB AND STIFFENERS, INCLUDING ATTACHMENT TO WING CENTER SECTION REAR SPAR AT STA 663; 2. BULKHEAD AT STA 663; 3. BULKHEAD AND PRESSURE WEB AT STA 727; 4. KEEL BEAM CHORDS, WEBS, STIFFENERS AND SPLICE, KEEL BEAM/ REAR SPAR ATTACHMENT ANGLES; 5. STRINGER 18A WEB, CHORD AND LINKS; 6. SIDE STRUT SUPPORT FRAME AT STA 706; 7. MAIN LANDING GEAR SUPPORT FRAME AT STA 695 AND716; 8. WHEEL WELL FRAME AT STA 685; 9. FLAP TRACK SUPPORT FITTINGS. E X T E R N A L
133 134 139 193
emp emp emp emp
MPD MRB
53-050-00 MSI 53-050-00
AMM AMM
51-05-01-210 53-05-03-210
1122S 112A
MPD MRB
53-070-00 MSI 53-070-00
GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE FROM 112 STA 178 BULKHEAD TO CANTED BULKHEAD (STA 224.8 TO 227.8), emp INCLUDING BULKHEADS, SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, FORWARD ACCESS DOOR CUTOUT, AND NOSE WHEEL WELL CUTOUT. I N T E R N A L ACCESS REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED. REMOVE WEATHER RADAR RT SHELF.
ITEMS
53-220-00 MSI 53-220-00 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 03-jun-04
T: 9 YRS I: 3 YRS
E2 HHI 737-700
2 23-jul-08
T: 9 YRS I: 3 YRS
E2 HHI 737-700
3 23-jul-08
T: 36000 CYC T: 12 YRS I: 8 YRS I: 24000 CYC
E2 HHI 737-700
2 03-jun-04
ATA: 53 - 15
Page 1 of 2
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
531500 04000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
SPECIAL DETAILED INSPECTION OF THE WHEEL WELL AFT BULKHEAD 141 INSPECT (ULTRASONIC) THE AFT SIDE OF 727 BULKHEAD AT THE FRAME 142 AROUND THE SIX FASTENERS THROUGH THE INNER CHORD AND WEB AT WL 201. (PSE 53-40-16-2) I N T E R N A L NOTE( E, I ) FOR 737-600 L/N #1-766 THRESHOLD IS 34,000 FC, REPEAT IS 7,000 FC. FOR 737-600 L/N #767-1192 THRESHOLD IS 56,000 FC, REPEAT IS 7,000 FC. FOR737-700 L/N #1-766 THRESHOLD IS 27,000 FC, REPEAT IS 7,000 FC. FOR 737-700 L/N #767-1192 THRESHOLD IS 56,000 FC, REPEAT IS 7,000 FC. FOR 737-600 AND 737-700 AIRPLANES SEE INTERVAL NOTE FOR AIRPLANE SPECIFIC THRESHOLD, REPEAT AND SAMPLING INTERVALS. ACCESS REMOVE AND/OR DISPLACE THE FORWARD BULKHEAD, SIDEWALL CEILING PANELS AND INSULATION BLANKETS AS REQUIRED.
STRUCTURE
emp emp
ITEMS
THRESHOLD INTERVAL
REFERENCES MPD MRB
53-668-00 MSI 57-05-02-200
AMM AMM
53-668-00 53-05-02-010-801
T: 27000 CYC I: 7000 CYC
ATA: 53 - 15
TSK
EFF
E4 HHI 737-700
R L ITEM BY E E REVISION P V DATE
2 23-jul-08
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 30
533000 00000
533000 01000
533000 02000
533000 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUSELAGE EXTERIOR GENERAL VISUAL INSPECTION OF THE DOOR CUTOUTS AT FORWARD ACCESS DOOR, FORWARD AIRSTAIRS DOOR AND FORWARD E/E BAY DOOR. E X T E R N A L ACCESS OPEN FORWARD ACCESS DOOR, AIRSTAIRS DOOR AND E/E COMPARTMENT DOOR.
112 117 emp
112A 117A 117BL
MPD MRB
GENERAL VISUAL INSPECTION OF THE FUSELAGE SKIN UNDER DORSAL 321 FIN AND AFT TO STA 1016, INCLUDING CIRCUMFERENTIAL SPLICE. I N T E R N A L
321A
MPD MRB
GENERAL VISUAL INSPECTION OF THE AREA UNDER LOWER WING-TO-BODY FAIRING (AFT OF WHEEL WELL), INCLUDING SKIN PANELS, LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN SPLICE, STRINGER 18 STRAP AT SIDE OF BODY, STRINGER 18A (WEB, CHORDS AND LINKS), AND KEEL BEAM EXTENSION. I N T E R N A L
149 194 emp emp emp emp emp emp emp emp emp emp emp emp emp emp
emp 194AL 194AR 194BL 194BR 194CL 194CR 194DL 194DR 194E 194FL 194FR 194GL 194GR 194HL 194HR
MPD MRB
GENERAL VISUAL INSPECTION OF THE AREA UNDER WING-TO-BODY FAIRING (ABOVE WING), INCLUDING SKIN PANELS, CIRCUMFERENTIAL SKIN SPLICES, AND STRINGER 18 STRAP AT SIDE OF BODY. I N T E R N A L
195 emp emp 196 emp emp
195AL 195BL 195CL 196AR 196BR 196CR
MPD MRB
ITEMS
53-010-00 MSI 53-010-00 I: 24 MTH I: 4000 CYC
E2 HHI 737-700
3 03-jun-04
I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 05-sep-06
53-450-00 MSI 53-450-00
53-270-00 MSI 53-270-00
53-280-00 MSI 53-280-00
ATA: 53 - 30
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
533000 04000
533000 05000
533000 06000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FRONT SPAR FITTING LUGS AND BOLTS (STA 1016) I N T E R N A L ACCESS PIN REMOVAL IS NOT REQUIRED.
322 emp emp emp
323AL 323AR 323BL 323BR
MPD MRB
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN REAR SPAR FITTING LUGS AND BOLTS STA 1088. INSPECT FUSELAGE SKIN UNDER VERTICAL FIN FROM STA 1016 TO 1088. I N T E R N A L
323 emp emp emp emp emp
323AL 323AR 323BL 323BR 323CL 323CR
MPD MRB
53-480-00 MSI 53-480-00
AMM AMM
51-05-01-210 53-05-03-210
GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FRONT SPAR FITTING LUGS AND BOLTS (STA 1016) I N T E R N A L ACCESS PIN REMOVAL IS REQUIRED. REMOVE ONLY ONE PIN AT A TIME.
322 emp emp emp
323AL 323AR 323BL 323BR
MPD MRB
53-470-00 MSI 53-470-00
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-460-00 MSI 53-460-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 18-mar-05
T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
E2 HHI 737-700
2 05-sep-06
T: 20 YRS I: 8 YRS
E2 HHI 737-700
1 03-jun-04
ATA: 53 - 30
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 51
535100 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING-TO-BODY FAIRING GENERAL VISUAL INSPECTION OF THE AREA UNDER LOWER WING-TO-BODY FAIRING (FORWARD OF WING BOX), INCLUDING SKIN PANELS, LONGITUDINAL LAP SPLICES, KEEL BEAM EXTENSION, WING-TO-BODY DRAG ANGLES, AND STA 540 BULKHEAD. I N T E R N A L
129 191 emp emp emp emp emp emp emp emp emp emp emp emp
emp 191AL 191AR 191BL 191BR 191CL 191CR 191D 191FL 191FR 191GL 191GR 191HL 191HR
ITEMS
MPD MRB
53-180-00 MSI 53-180-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ATA: 53 - 51
E2 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 81
538100 00000
538100 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
UNDERFLOOR NOSE COMPARTMENT AND ELECTRONIC EQUIPMENT COMPARTMENT GENERAL VISUAL INSPECTION OF THE E/E COMPARTMENT (STA294.5 TO 117 396), INCLUDING: emp 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP 118 SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, BULKHEAD AT STA 294.5; 2.E/E COMPARTMENT DOOR AND AIRSTAIRS DOOR CUTOUT SURROUND STRUCTURE 3. FORWARD ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE (PORTION IN LOWER LOBE). I N T E R N A L ACCESS REMOVE LRU'S AND RACKS, DO NOT REMOVE PERMANENTLY INSTALLED STRUCTURE. REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED.
1102S 117A emp
MPD MRB
GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF STA 178 BULKHEAD. I N T E R N A L ACCESS OPEN RADOME
111
MPD MRB
111
ITEMS
53-120-00 MSI 53-120-00 T: 12 YRS T: 36000 CYC I: 24000 CYC I: 8 YRS
E2 HHI 737-700
2 18-mar-05
T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
E2 HHI 737-700
1 03-jun-04
53-060-00 MSI 53-060-00
ATA: 53 - 81
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
538100 02000
GENERAL VISUAL INSPECTION OF THE FUSELAGE LOWER LOBE FROM CANTED BULKHEAD (STA 224.8 TO 227.8) TO STA 294, INCLUDING: 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, BULKHEAD AT STA 259.5; 2.NOSE WHEEL WELL CUTOUT SURROUND STRUCTURE, NOSE WHEEL WELL SIDE AND TOP PANELS; 3.TRUNNION SUPPORT FITTING, ACTUATOR SUPPORT FITTING AND DRAG BRACE FITTING. I N T E R N A L ACCESS ACCESS THROUGH NOSE WHEEL WELL SIDE AND TOP ACCESS PANELS, AND THROUGH ACCESS PANEL IN CREW FLOOR. REMOVE/ DISPLACE INSULATION BLANKETS AS REQUIRED.
Date: 23-jul-08
ZONE ACCESS 113 emp emp 114 emp emp emp
STRUCTURE
113AC 113AW 113BW 1101S 114AC 114AW 114BW
ITEMS
REFERENCES MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
53-090-00 MSI 53-090-00 T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
ATA: 53 - 81
E2 HHI 737-700
1 03-jun-04
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 82
538200 00000
538200 01000
538200 02000
538200 03000
538200 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FORWARD CARGO COMPARTMENT DETAILED VISUAL INSPECTION OF THE FORWARD CARGO DOOR SURROUND STRUCTURE, FITTINGS AND STOPS. E X T E R N A L
122
821
DETAILED VISUAL INSPECTION OF THE FORWARD CARGO DOOR CUTOUT 122 SURROUND STRUCTURE. I N T E R N A L ACCESS REMOVE DOOR REVEALS, SIDEWALLS AS REQUIRED AND INSULATION BLANKETS AS REQUIRED.
1221S
GENERAL VISUAL INSPECTION OF THE FORWARD BILGE SKIN PANELS 123 INCLUDING SKINS, FRAMES, STRINGERS, LONGITUDINAL LAP SPLICES, 124 AND CARGO DOOR CUTOUT SURROUND STRUCTURE IN BILGE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS AND SCUFF PLATES. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
1202S emp
GENERAL VISUAL INSPECTION OF THE FORWARD CARGO COMPARTMENT 121 SKIN PANELS (SKINS, FRAMES AND STRINGERS). 122 I N T E R N A L ACCESS REMOVE SIDEWALL, CEILING PANELS, INSULATION BLANKETS AS REQUIRED.
1201S emp
GENERAL VISUAL INSPECTION OF THE AREA AFT OF FORWARD CARGO 125 COMPARTMENT, INCLUDING SKIN PANELS (SKINS, FRAMES, STRINGERS), 126 LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES, AND FORWARD SIDE OF STA 540 BULKHEAD AND BULKHEAD SPLICES. I N T E R N A L ACCESS REMOVE/DISPLACE FORWARD CARGO COMPARTMENT AFT BULKHEAD PANELS, INSULATION BLANKETS AND DUCTING AS REQUIRED.
1203S emp
ITEMS
MPD MRB
MPD MRB
MPD MRB
MPD MRB
MPD MRB
53-030-00 MSI 53-030-00 I: 24 MTH I: 4000 CYC
E3 HHI 737-700
2 18-mar-05
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E3 HHI 737-700
1 03-jun-04
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E2 HHI 737-700
3 05-sep-06
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 36000 CYC I: 10 YRS
E2 HHI 737-700
2 03-jun-04
53-150-00 MSI 53-150-00
53-160-00 MSI 53-160-00
53-130-00 MSI 53-130-00
53-170-00 MSI 53-170-00
ATA: 53 - 82
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 84
538400 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIR CONDITIONING COMPARTMENT LH AND RH GENERAL VISUAL INSPECTION OF THE KEEL BEAM UNDER WING-TO-BODY FAIRING (UNDER WING BOX, STA 540 TO 663.75), INCLUDING KEEL BEAM CHORDS, WEBS, STIFFENERS, SPLICE, KEEL BEAM/ REAR SPAR ATTACHMENT ANGLES. I N T E R N A L ACCESS OPTION 1: REMOVE CENTER WING-TO-BODY FAIRING (192CL, 192CR, 192E, 192F) AND OPEN AC BAY ACCESS DOOR. OPTION 2: OPEN AC BAY DOOR AND REMOVE AC PACK TO GAIN ACCESS TO ACCESS HOLES.
139 192 emp emp emp
1004S 192CL 192CR 192E 192F
ITEMS
MPD MRB
53-210-00 MSI 53-210-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ATA: 53 - 84
E2 HHI 737-700
3 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 53 - 85
538500 00000
538500 01000
538500 02000
538500 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AFT CARGO COMPARTMENT DETAILED VISUAL INSPECTION OF THE AFT CARGO DOOR SURROUND 142 STRUCTURE, FITTINGS AND STOPS. E X T E R N A L
822
DETAILED VISUAL INSPECTION OF THE AFT CARGO DOOR CUTOUT SURROUND STRUCTURE. I N T E R N A L ACCESS REMOVE DOOR REVEALS, SIDEWALLS AND INSULATION BLANKETS.
1421S
142
GENERAL VISUAL INSPECTION OF THE AFT BILGE SKIN PANELS (SKINS, 143 FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL 144 SKIN AND STRINGER SPLICES, STA 727 BULKHEAD AND PRESSURE WEB, AND CARGO DOOR CUTOUT SURROUND STRUCTURE IN BILGE. I N T E R N A L ACCESS REMOVE CARGO FLOOR PANELS AND SCUFF PLATES. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
1402S emp
GENERAL VISUAL INSPECTION OF THE AFT CARGO COMPARTMENT, 141 INCLUDING: 142 1.SIDE SKIN PANELS ( SKIN, FRAMES, STRINGERS), CIRCUMFERENTIAL SKIN AND STRINGER SPLICE; 2.STRINGER 18 STRAP AT SIDE OF BODY; 3.STRINGER 18A WEB, CHORD AND LINKS; 4.AFT SIDE OF STA 727 BULKHEAD AND PRESSURE WEB. I N T E R N A L ACCESS REMOVE AFT CARGO COMPARTMENT AFT BULKHEAD PANEL AND POTABLE WATER TANK. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
S1401 emp
ITEMS
MPD MRB
MPD MRB
53-030-00 MSI 53-030-00 I: 4000 CYC I: 24 MTH
E3 HHI 737-700
2 18-mar-05
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E3 HHI 737-700
1 03-jun-04
T: 24000 CYC T: 8 YRS I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 05-sep-06
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
53-240-00 MSI 53-240-00
MPD MRB
53-250-00 MSI 53-250-00
AMM AMM
51-05-01-210 53-05-03-210
MPD MRB
53-230-00 MSI 53-230-00
ATA: 53 - 85
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
538500 04000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE AREA AFT CARGO COMPARTMENT, 145 INCLUDING: 146 1.SKIN PANELS (SKINS, FRAMES, STRINGERS), LONGITUDINAL LAP SPLICES, CIRCUMFERENTIAL SKIN AND STRINGER SPLICES; 2.AFT ENTRY AND GALLEY DOOR CUTOUT SURROUND STRUCTURE IN LOWER LOBE; 3.STA 1016 BULKHEAD, INCLUDING CHORDS, PRESSURE WEB, STIFFENERS, CHORD/WEB ATTACHMENTS; 4.STRINGER SPLICE FITTINGS AND TENSION BOLTS AT STA 1016. I N T E R N A L ACCESS REMOVE AFT CARGO COMPARTMENT AFT BULKHEAD PANEL AND POTABLE WATER TANK. REMOVE/DISPLACE INSULATION BLANKETS AS REQUIRED.
STRUCTURE
1403S emp
REFERENCES MPD MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
53-260-00 MSI 53-260-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ITEMS
TSK
ATA: 53 - 85
E2 HHI 737-700
1 03-jun-04
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 54 54 - 30
543000 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NACELLES/ PYLONS PYLON-SKIN GENERAL VISUAL INSPECTION OF THE EXTERNAL AREAS OF L/H AND R/H STRUT BOX, INCLUDING UPPER AND LOWER SPARS, FORWARD ENGINE MOUNT BULKHEAD, AFT BULKHEAD, AND SIDE SKINS. I N T E R N A L ACCESS REMOVE INSULATION BLANKETS/HEAT SHIELDS AND FAN COWLS. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.
433 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp
413 414 415 416 423 424 425 426 431AT 431BL 431BR 431CL 431CR 431EL 431ER S4331 441AT 441BL 441BR 441CL 441CR 441EL 441ER S4431
ITEMS
MPD MPD MRB MRB
54-070-01 54-070-02 MSI 54-070-01 MSI 54-070-02 I: 18000 CYC I: 6 YRS
ATA: 54 - 30
E2 HHI 737-700
3 25-apr-06
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
543000 01000
GENERAL VISUAL INSPECTION OF THE INTERNAL AREAS OF STRUT BOX L/H AND R/H, INCLUDING UPPER AND LOWER SPARS, FORWARD AND AFT ENGINE MOUNT BULKHEAD, AFT AND MID BULKHEADS, AND SIDE SKINS. I N T E R N A L ACCESS DISASSEMBLE PNEUMATIC DUCTS AS REQUIRED. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.
433 emp emp emp emp emp emp emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp emp emp emp emp emp emp emp
431BL 431BR 431CL 431CR 431DL 431DR 431EL 431ER 4332S 433AL 433AR 433AT 433BT 433CT 433DT 441BL 441BR 441CL 441CR 441DL 441DR 441EL 441ER 4432S 443AL 443AR 443AT 443BT 443CT 443DT
MPD MPD MRB MRB
FUNCTIONALLY CHECK THE LEFT ENGINE FORWARD STRUT AND AFT STRUT FAIRING DRAINS.
410 430 emp
emp 434AR 434BL
MPD MRB
543001 00000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
54-080-01 54-080-02 MSI 54-080-01 MSI 54-080-02 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
3 25-apr-06
T: 9000 CYC T: 30 MTH I: 9000 CYC I: 30 MTH
F2 HHI 737-700
1 30-nov-05
54-090-01 MSI 54-090-01 RTE:9
ATA: 54 - 30
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
543002 00000
DESCRIPTION
ZONE ACCESS
FUNCTIONALLY CHECK THE RIGHT ENGINE FORWARD STRUT AND AFT 420 STRUT FAIRING DRAINS. 440 emp
STRUCTURE
emp 444AL 444BR
REFERENCES MPD MRB
THRESHOLD INTERVAL
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
54-090-02 MSI 54-090-02 RTE:9 T: 9000 CYC T: 30 MTH I: 30 MTH I: 9000 CYC
Date: 23-jul-08
TSK
ATA: 54 - 30
F2 HHI 737-700
1 30-nov-05
Page 3 of 3
HHI R E V
ITEM 54 - 40
R
737-6
MAINTENANCE SCHEDULE
544000 00000
R
544000 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ATTACHMENT FITTINGS GENERAL VISUAL INSPECTION OF THE L/H AND R/H STRUTS TO WING UPPER LINK, DIAGONAL BRACE, SIDE LINKS, AND STRUT ATTACHMENT FITTINGS. I N T E R N A L ACCESS REMOVE UPPER AND LOWER WING JUNCTION FAIRINGS. REMOVE THRUST REVERSER STRUT FAIRING AND AFT STRUT FAIRING. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.
431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp
431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR
MPD MPD MRB MRB
DETAILED VISUAL INSPECTION OF L/H AND R/H PINS AND FUSE PINS ON UPPER LINK, MIDSPAR, DIAGONAL BRACE, AND SIDE LINKS. PIN REMOVAL IS NOT REQUIRED. I N T E R N A L ACCESS REMOVE UPPER AND LOWER WING JUNCTION FAIRINGS. REMOVE THRUST REVERSER STRUT FAIRING AND AFT STRUT FAIRING PANELS, AS REQUIRED. TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.
431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp
431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR
MPD MPD MRB MRB
ITEMS
54-040-01 54-040-02 MSI 54-040-01 MSI 54-040-02 I: 9000 CYC I: 30 MTH I: 36 MTH
E2 HHI 737-700
4 23-jul-08
I: 9000 CYC I: 30 MTH
E3 HHI 737-700
3 03-jun-04
54-050-01 54-050-02 MSI 54-050-01 MSI 54-050-02
ATA: 54 - 40
Page 1 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
544000 02000
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT FORWARD ENGINE MOUNT ASSEMBLY, INCLUDING FAN CASE FITTING, SIDE LINKS, HANGER AND LINK PINS. E X T E R N A L ACCESS OPEN FAN COWL.
413 414 423 424
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT STRUT ATTACH BOLTS AT FORWARD ENGINE MOUNT. I N T E R N A L ACCESS REMOVE FAN COWL.
413 414 emp emp 423 424
413 414 431AT 441AT 423 424
MPD MPD MRB MRB
54-015-01 54-015-02 MSI 54-015-01 MSI 54-015-02
AMM AMM
54-05-03-210 51-05-01-210
GENERAL VISUAL INSPECTION OF THE L/H AND R/H AFT ENGINE MOUNT ASSEMBLY, INCLUDING THRUST LINKS AND THRUST LINK PINS; MOUNT TO ENGINE LEFT, CENTER AND RIGHT LINKS, INCLUDING LINK PINS; HANGER AND EVENER BAR; ATTACH BOLTS. E X T E R N A L
415 416 425 426
415 416 425 426
MPD MPD MRB MRB
54-030-01 54-030-02 MSI 54-030-01 MSI 54-030-02
DETAILED VISUAL INSPECTION OF THE L/H AND R/H BORES OF PINS AND FUSE PINS ON UPPER LINK, MIDSPAR, DIAGONAL BRACE, AND SIDE LINKS. PIN REMOVAL IS NOT REQUIRED. I N T E R N A L ACCESS TR'S MUST BE OPEN TO REMOVE ACCESS PANELS 431EL, 431ER, 441EL AND 441ER.
431 emp emp emp emp emp 434 emp emp 441 emp emp emp emp emp 444 emp emp
544000 03000
544000 04000
544000 05000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
413 414 423 424
431CL 431CR 431DL 431DR 431EL 431ER 434AL 434AR 434BL 441CL 441CR 441DL 441DR 441EL 441ER 444AL 444AR 444BR
ITEMS
REFERENCES MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
54-010-01 54-010-02 MSI 54-010-01 MSI 54-010-02 I: 6 YRS I: 18000 CYC
E2 HHI 737-700
3 25-apr-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
4 05-sep-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
I: 36000 CYC I: 10 YRS
E3 HHI 737-700
3 03-jun-04
54-060-01 54-060-02 MSI 54-060-01 MSI 54-060-02
ATA: 54 - 40
Page 2 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
R
544000 06000
R
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE FORWARD AND AFT ENGINE MOUNT TO STRUT SHEAR PINS. I N T E R N A L NOTE( I ) AT ENGINE REMOVAL. ACCESS ENGINE REMOVAL REQUIRED.
ZONE ACCESS 413 emp 414 emp emp emp 423 emp 424 emp emp emp 433 emp emp emp emp emp emp emp emp 443 emp emp emp emp emp emp emp emp
STRUCTURE
4001S 413 414 415 416 416CR 423 S4002 424 425 425CL 426 431AL 431AT 431BL 431BR 431CL 431DL 431DR 431EL 431ER 441AL 441AT 441BL 441BR 441CL 441DL 441DR 441EL 441ER
ITEMS
REFERENCES MPD MRB MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
54-020-01 MSI 54-020-01 54-020-01 54-020-02 MSI 54-020-01 MSI 54-020-02 I: 1 EC
ATA: 54 - 40
E2 HHI 737-700
4 23-jul-08
Page 3 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
N
544000 06100
N
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE FORWARD AND AFT ENGINE MOUNT TO STRUT SHEAR PINS. I N T E R N A L NOTE( I ) AT ENGINE REMOVAL. ACCESS ENGINE REMOVAL REQUIRED.
ZONE ACCESS 423 emp 424 emp emp emp 443 emp emp emp emp emp emp emp emp
STRUCTURE
423 S4002 424 425 425CL 426 441AL 441AT 441BL 441BR 441CL 441DL 441DR 441EL 441ER
ITEMS
REFERENCES MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
54-020-02 MSI 54-020-02 I: 1 EC
ATA: 54 - 40
E2 HHI 737-700
0 23-jul-08
Page 4 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 55 55 - 10
551000 00000
551000 01000
551000 02000
551000 03000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
STABILIZERS STABILIZER- HORIZONTAL GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER FRONT SPAR TERMINAL FITTINGS AND CENTER SECTION FRONT SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS NOT REQUIRED.
331 341
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER REAR SPAR TERMINAL FITTINGS AND CENTER SECTION REAR SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS NOT REQUIRED .
333 emp 343 emp
331A 341A
333AB 333AT 343AB 343AT
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER CENTER 311 SECTION JACKSCREW FITTING. 312 I N T E R N A L
311BL emp
GENERAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER CENTER 313 SECTION FRONT SPAR, REAR SPAR, PIVOT FITTINGS, AND PRIMARY AND emp SECONDARY THRUST BEAMS. 314 I N T E R N A L ACCESS ADJUST STABILIZER TRIM AS REQUIRED. REMOVE GAP SEAL AND REAR SPAR SLIDING SEAL TO INSPECT PIVOT FITTINGS.
3102S 311BL emp
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
MPD MRB
MPD MRB
55-080-01 55-080-02 MSI 55-080-01 MSI 55-080-02 T: 8 YRS I: 4 YRS
E2 HHI 737-700
1 03-jun-04
T: 8 YRS I: 4 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
55-120-01 55-120-02 MSI 55-120-01 MSI 55-120-02
55-010-00 MSI 55-010-00
55-020-00 MSI 55-020-00
ATA: 55 - 10
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
551000 05000
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT HORIZONTAL STABILIZER FROM FRONT SPAR TO REAR SPAR INCLUDING SPAR CHORDS, WEBS, TERMINAL FITTINGS, UPPER AND LOWER INSPAR SKINS. I N T E R N A L
Date: 23-jul-08
ZONE ACCESS 332 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 342 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
331B 331BZ 331CZ 331DZ 332AB 332AT 332BB 332CB 332DB 332EB 332FB 332GB 332HB 332JB 332KB 332LB 332MB 332NB 335A 341B 341BZ 341CZ 341DZ 342AB 342AT 342BB 342CB 342DB 342EB 342FB 342GB 342HB 342JB 342KB 342LB 342MB 342NB 345A
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
55-100-01 55-100-02 MSI 55-100-01 MSI 55-100-02 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ATA: 55 - 10
E2 HHI 737-700
1 03-jun-04
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
551000 06000
GENERAL VISUAL INSPECTION OF THE L/H AND R/H FORWARD SIDE OF FRONT SPAR, INCLUDING FRONT SPAR CHORDS AND WEBS, TERMINAL FITTINGS, AND CENTER SECTION FRONT SPAR LUGS. I N T E R N A L ACCESS BOLT REMOVAL IS REQUIRED TO INSPECT TERMINAL FITTINGS AND CENTER SECTION FRONT SPAR LUGS.
331 emp emp emp 341 emp emp emp
3311S 331A 331AZ 331B 3411S 341A 341AZ 341B
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE AFT SIDE OF LEFT AND RIGHT HORIZONTAL STABILIZER REAR SPAR INCLUDING SPAR CHORDS, WEBS, TERMINAL FITTINGS, ELEVATOR TAB ACTUATOR SUPPORT FITTING, CENTER SECTION REAR SPAR LUGS, ELEVATOR HINGE RIBS AND ELEVATOR TAB LEADING EDGE. I N T E R N A L ACCESS DISCONNECT BALANCE PANELS IN BALANCE BAYS. BOLT REMOVAL IS REQUIRED TO INSPECT TERMINAL FITTINGS AND CENTER SECTION REAR SPAR LUGS, EXCEPT AT REAR SPAR UPPER LUGS AND CLEVIS. REMOVE TAB HINGE COVERS TO INSPECT ELEVATOR TAB LEADING EDGE.
333 emp emp emp emp emp emp emp emp emp emp emp emp emp emp 343 emp emp emp emp emp emp emp emp emp emp emp emp emp emp
3331S 333AB 333AT 333BB 333CB 333DB 333EB 333FB 334AB 334BB 334CB 334DB 334EB 334FB 335A 3431S 343AB 343AT 343BB 343CB 343DB 343EB 343FB 344AB 344BB 344CB 344DB 344EB 344FB 345A
MPD MPD MRB MRB
551000 07000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
55-070-01 55-070-02 MSI 55-070-01 MSI 55-070-02 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
4 03-jun-04
55-110-01 55-110-02 MSI 55-110-01 MSI 55-110-02
ATA: 55 - 10
Page 3 of 3
HHI R E V
ITEM 55 - 20 552000 00000
552000 01000
R
737-6
MAINTENANCE SCHEDULE
552000 03000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ELEVATOR, HINGE SUPPORT AND BALANCE MECHANISM GENERAL VISUAL INSPECTION OF THE ELEVATOR AND ELEVATOR TAB SKIN PANELS, ELEVATOR SPARS, INSPAR RIBS, LEADING EDGE SKINS AND LEADING EDGE RIBS AND LEADING EDGE SPARS. I N T E R N A L
334 emp emp emp emp emp 344 emp emp emp emp emp emp
333AB 333BB 333EB 333FB 334AB 334PT 3001S 343BB 343CB 343DB 343EB 343FB 344PT
MPD MRB
DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT ELEVATOR TAB 334 MECHANISM SUPPORT FITTINGS ON ELEVATOR FRONT SPAR AND 344 ELEVATOR TAB SPAR AT LEADING EDGE CUTOUTS. I N T E R N A L ACCESS REMOVE UPPER OR LOWER HORIZONTAL STABILIZER TRAILING EDGE SEAL AND ELEVATOR INBOARD HINGE COVER PANEL TO INSPECT SUPPORT FITTINGS. REMOVE TAB HINGE COVERS TO LOCALLY INSPECT FORWARD FACE OF SPAR.
emp emp
MPD MPD MRB MRB
INSPECT DETAILED THE ELEVATOR HINGE FITTINGS, ELEVATOR 334 ACTUATOR FITTINGS, ELEVATOR BALANCE WEIGHT SUPPORT 344 STRUCTURE, ELEVATOR TAB MAST ARM FITTING AND ELEVATOR TAB HINGE FITTINGS. I N T E R N A L NOTE( ) ACCESS REMOVE LOWER TRAILING EDGE PANELS AND DISCONNECT BALANCE BAYS. REMOVE ELEVATOR HINGE COVER PLATES. ALTERNATIVE REMOVE ELEVATOR FROM HORIZONTAL STABILIZER. FOR ELEVATOR TAB MAST ARM FITTINGS, REMOVE FAIRING ON UPPER SURFACE OF ELEVATOR TO GAIN ACCESS.
emp emp
ITEMS
MPD MPD MRB MRB
55-130-00 MSI 55-130-00 T: 36000 CYC T: 12 YRS I: 10 YRS I: 30000 CYC
E2 HHI 737-700
4 03-jun-04
T: 12 YRS T: 36000 CYC I: 8 YRS I: 24000 CYC
E3 HHI 737-700
2 03-jun-04
T: 18000 CYC T: 8 YRS I: 18000 CYC I: 8 YRS
E3 HHI 737-700
5 23-jul-08
55-115-01 55-115-02 MSI 55-115-01 MSI 55-115-02
55-135-01 55-135-02 MSI 55-135-01 MSI 55-135-02
ATA: 55 - 20
Page 1 of 1
HHI R E V
ITEM 55 - 30
R
737-6
MAINTENANCE SCHEDULE
553000 00000
R
553000 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
VERTICAL STABILIZER GENERAL VISUAL INSPECTION OF THE VERTICAL FIN FROM FRONT SPAR TO REAR SPAR, INCLUDING SPAR CHORDS AND WEBS, INSPAR SKINS, LOWER CLOSURE RIB, AND REAR SPAR TERMINAL FITTINGS. I N T E R N A L ACCESS REMOVE UPPER REMOVABLE WEB. PIN REMOVAL IS NOT REQUIRED FOR TERMINAL FITTING INSPECTION.
323 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
322A 322AL 322AR 322B 322C 323AL 323AR 323BL 323BR 323CL 323CR 323DL 323EL 323FL 323GL 324AL 324AR 324BL 324BR 324DL 324DR 324JL 324KL 324LL 324ML 324NL S3232
MPD MRB MPD MRB
GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF THE VERTICAL FIN FRONT SPAR, INCLUDING FRONT SPAR CHORDS, WEBS, AND TERMINAL FITTINGS. I N T E R N A L
322 emp emp emp emp emp
322B 322C 323AL 323AR 323BL 323BR
MPD MRB
ITEMS
55-050-00 MSI 55-050-00 55-050-00 MSI 55-050-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
3 23-jul-08
T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
E2 HHI 737-700
1 03-jun-04
55-030-00 MSI 55-030-00
ATA: 55 - 30
Page 1 of 2
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
553000 02000
GENERAL VISUAL INSPECTION OF THE AFT SIDE OF VERTICAL FIN REAR SPAR,INCLUDING REAR SPAR CHORDS AND WEBS, AND RUDDER HINGE RIBS. I N T E R N A L
R
Date: 23-jul-08
ZONE ACCESS 324 emp emp emp emp emp emp emp
STRUCTURE
323CL 324BL 324DL 324GL 324KL 324LL 324ML 324NL
ITEMS
REFERENCES MPD MRB MPD MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
55-060-00 MSI 55-060-00 55-060-00 MSI 55-060-00 T: 36000 CYC T: 12 YRS I: 24000 CYC I: 8 YRS
ATA: 55 - 30
E2 HHI 737-700
3 23-jul-08
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 55 - 40
554000 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
RUDDER GENERAL VISUAL INSPECTION OF THE RUDDER SKIN PANELS, SPARS, 325 INSPAR RIBS, LEADING EDGE SKINS AND LEADING EDGE RIBS AND LEADING EDGE SPARS. I N T E R N A L
3001S
MPD MRB
55-130-00 MSI 55-130-00 T: 36000 CYC T: 12 YRS I: 10 YRS I: 30000 CYC
ITEMS
ATA: 55 - 40
E2 HHI 737-700
4 03-jun-04
Page 1 of 1
HHI R E V
ITEM 56 56 - 11 561100 00000
561100 01000
R
561100 02000
R
N
737-6
MAINTENANCE SCHEDULE
561100 03000
N
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WINDOWS FLIGHT COMPARTMENT WINDOWS LUBRICATE THE INSIDE RELEASE MECHANISMS FOR THE PILOTS AND CO-PILOTS #2 SLIDING WINDOWS. LUBRICATE THE OUTSIDE RELEASE MECHANISM FOR THE CO-PILOTS #2 SLIDING WINDOW.
211 212
emp emp
OPERATIONALLY CHECK THE INSIDE RELEASE MECHANISMS FOR THE 211 PILOTS AND CO-PILOTS #2 SLIDING WINDOWS. 212 OPERATIONALLY CHECK THE CO-PILOTS #2 SLIDING WINDOW FROM THE OUTSIDE.
emp emp
PERFORM A GENERAL VISUAL INSPECTION OF THE PILOTS AND 211 CO-PILOTS #2 SLIDING WINDOW SILL DRAIN FOR OBVIOUS DAMAGE, 212 CLOGGING, CONDITION AND SECURITY. I N T E R N A L NOTE( E ) APPLICABLE TO AIRPLANES LINE NUMBER 145 AND ON. APPLICABLE TO AIRPLANES LINE NUMBER 1 TO 144 INCORPORATING SB 737-56-1011.
emp emp
DO AN INTERNAL AND EXTERNAL DETAILED INSPECTION OF THE LEFT 211 SIDE AND RIGHT SIDE FLIGHT DECK WINDOWS NUMBER 2, 4 AND 5 FOR 212 CRACKING AND DAMAGE IN THE VINYL INTERLAYER AND GLASS PANES. NOTE( T ) THE INITIAL INSPECTION ON D-AHIB MUST BE DONE PRIOR TO JANUARY 3, 2009. THE INITIAL INSPECTION ON D-AHIC MUST BE DONE PRIOR TO JULY 3, 2009.
emp emp
ITEMS
MPD MRB
56-010-00 MSI 56-010-00 RTE:9
AMTOSS
12-25-81-60
MPD MRB
56-030-00 MSI 56-030-00 RTE:9
AMTOSS
56-12-11-71
MPD MRB
56-050-00 MSI 56-050-00 RTE:9
AMTOSS
56-12-11-20
AAR AAR EO SB
AD 2008-11-08 LTA D-2008-235 160169 737-56A1022
I: 2 YRS
S
HHI 737-700
2 03-jun-04
I: 2 YRS
F1 HHI 737-700
2 03-jun-04
I: 2 YRS
E2 HHI 737-700
4 23-jul-08
T: 1 s.N I: 6000 FLH I: 24 MTH
E3 HHI 737-700
0 23-jul-08
ATA: 56 - 11
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 57 - 10
571000 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WINGS INTERSPAR WING GENERAL VISUAL INSPECTION OF THE OUTBOARD WING FRONT SPAR. INSPECT LEFT AND RIGHT FRONT SPAR CHORDS, WEBS AND STIFFENERS, INCLUDING AT SIDE OF BODY JOINT AND AT NACELLE FITTING ATTACHMENT. I N T E R N A L ACCESS EXTEND KRUEGER FLAPS. ACCESS PANEL: 521AAB, 521ABB, 621AAB
511 emp 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 611 emp 621 emp emp emp emp emp emp emp
511AT 511BT 521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB 611AT 611BT 621AB 621AT 621BB 621CB 621DB 621EB 621FB 621GB
ITEMS
MPD MPD MRB MRB
57-120-01 57-120-02 MSI 57-120-01 MSI 57-120-02 I: 18000 CYC I: 6 YRS
ATA: 57 - 10
E2 HHI 737-700
2 25-apr-06
Page 1 of 5
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
571000 01000
571000 02000
Date: 23-jul-08
DESCRIPTION
GENERAL VISUAL INSPECTION OF THE L/H AND R/H AFT SIDE OF REAR SPAR (CHORDS, WEBS AND STIFFENERS), INCLUDING FLAP 1&2 AND 7&8 SUPPORT FITTINGS. I N T E R N A L
GENERAL VISUAL INSPECTION OF THE L/H AND R/H WING AFT SIDE OF REAR SPAR (CHORDS, WEBS AND STIFFENERS), INCLUDING AT MAIN LANDING GEAR OUTBOARD SUPPORT ATTACHMENT, AND AT TRUNNION ATTACHMENT. I N T E R N A L
ZONE ACCESS
STRUCTURE
REFERENCES
emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB
561 571 emp emp emp emp 661 emp emp emp emp 671
emp 561AB 561BB 561CB 571CB 571DB 661AB 661BB 661CB 671CB 671DB emp
MPD MPD MRB MRB
551 emp emp 651 emp emp
551BT 551CT 551EB 651BT 651CT 651EB
MPD MPD MRB MRB
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-310-01 57-310-02 MSI 57-310-01 MSI 57-310-02 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
57-260-01 57-260-02 MSI 57-260-01 MSI 57-260-02
ATA: 57 - 10
Page 2 of 5
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
571000 03000
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING FROM SIDE OF BODY RIB TO RIB 5: 1.SIDE OF BODY RIB (INCLUDING WEBS AND STIFFENERS, UPPER RIB CHORD, LOWER TEE CHORD, SPLICE FITTINGS, TERMINAL FITTINGS AT FRONT AND REAR SPARS); 2.UPPER AND LOWER SURFACES (INCLUDING SKINS; TYPICAL SPLICE, VENT AND RAIL STRINGERS; AT DRAIN INSTALLATION; AT ATTACHMENTS TO FRONT AND REAR SPARS; AT ATTACHMENTS TO SHEAR TIED RIBS AND SUPPORT FITTINGS); 3.FRONT AND REAR SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS; 4.SHEAR TIED AND NON-SHEAR TIED RIBS. I N T E R N A L
R
Date: 23-jul-08
ZONE ACCESS 531 emp 631 emp
STRUCTURE
531AB 531BB 631AB 631BB
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
EFF
R L ITEM BY E E REVISION P V DATE
57-170-01 57-170-02 MSI 57-170-01 MSI 57-170-02 I: 36000 CYC I: 10 YRS
ITEMS
TSK
ATA: 57 - 10
E2 HHI 737-700
2 23-jul-08
Page 3 of 5
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
571000 04000
Date: 23-jul-08
DESCRIPTION GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING FROM RIB5 TO RIB 22: 1.UPPER AND LOWER SURFACES (INCLUDING SKINS; TYPICAL SPLICE, VENT AND RAIL STRINGERS; AT ATTACHMENTS TO FRONT AND REAR SPARS; AT ATTACHMENTS TO SHEAR TIED RIBS AND SUPPORT FITTINGS; AT ATTACHMENT TO NACELLE FITTINGS; AT DRAIN INSTALLATIONS); 2.FRONT SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS, INCLUDING AT NACELLE FITTING ATTACHMENTS; 3.REAR SPAR CHORDS, WEBS, STIFFENERS AND RIB POSTS, FLAP TRACK SUPPORT FITTINGS, INCLUDING REAR SPAR AT MAJOR FITTING ATTACHMENTS; 4.SHEAR TIED AND NON-SHEAR TIED RIBS (INCLUDING RIB 6 STRUCTURAL DOORS, RIBS 6 AND 7 AT NACELLE SUPPORT FITTINGS, RIBS 10 AND 14 AT FLAP TRACK SUPPORT FITTINGS); 5.NACELLE SUPPORT FITTINGS (R2 BACKUP LINK, R4 BACK UP LINK, R7/8 BACKUP FITTING). I N T E R N A L ACCESS DO NOT REMOVE THE 532AZ AND THE 532BZ ACCESS DOORS AT THE SAME TIME.
ZONE ACCESS 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
5321S 532AB 532AZ 532BB 532BZ 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 6321S 632AB 632AZ 632BB 632BZ 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB 632QB 632RB
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-180-01 57-180-02 MSI 57-180-01 MSI 57-180-02 I: 36000 CYC I: 10 YRS
ATA: 57 - 10
E2 HHI 737-700
1 03-jun-04
Page 4 of 5
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
571000 05000
GENERAL VISUAL INPECTION OF THE LEFT AND RIGHT OUTBOARD WING SURGE TANK AND DRY BAY (FROM RIB 22 TO RIB 27), INCLUDING UPPER AND LOWER SKINS, STRINGERS, FRONT AND REAR SPARS, RIB POSTS "WBL 656.17 CLOSURE RIB (LN 778 AND ON)", SHEAR TIED AND NON-SHEAR TIED RIBS, AND ACCESS HOLES. I N T E R N A L
Date: 23-jul-08
ZONE ACCESS 533 emp emp 534 emp 633 emp emp 634 emp
STRUCTURE
533AB 533BB 533CB 534AB 534BB 633AB 633BB 633CB 634AB 634BB
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-190-01 57-190-02 MSI 57-190-01 MSI 57-190-02 I: 36000 CYC I: 10 YRS
ATA: 57 - 10
E2 HHI 737-700
2 03-jun-04
Page 5 of 5
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 12
571200 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FRONT AND REAR SPAR GENERAL VISUAL INSPECTION OF THE WING CENTER SECTION AFT SIDE OF REAR SPAR, INCLUDING KEEL BEAM STIFFENERS AT BL 6.2., AND SIDE OF BODY REAR SPAR TERMINAL FITTING. E X T E R N A L
133 134 192 emp emp emp emp emp
emp 1007S 192BL 192BR 192CL 192CR 192E 192F
ITEMS
MPD MRB
57-030-00 MSI 57-030-00 T: 9 YRS I: 3 YRS
ATA: 57 - 12
E2 HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 14
571400 00000
571400 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
CENTER WING BOX GENERAL VISUAL INSPECTION OF THE LOWER SIDE OF LOWER SURFACE OF WING CENTER SECTION: 1.SKINS, TYPICAL STRINGERS, SPLICE STRINGERS, FRONT AND REAR SPAR LOWER CHORDS; 2.SIDE OF BODY LOWER TEE CHORD AND SPLICE PLATES; 3.LOWER BEAMS AT BL 41; 4.AT ATTACHMENTS TO KEEL BEAM, TO LOWER BEAMS AT BL 41, TO FUSELAGE DRAG ANGLES; AT DRAIN INSTALLATION AND ACCESS HOLES. I N T E R N A L ACCESS REMOVE ECS HEAT EXCHANGER ACCESS PANEL.
131 132 192 emp emp emp emp emp emp emp emp emp emp
emp emp 1008S 192AL 192AR 192BL 192BR 192CL 192CR 192E 192F 192HL 192HR
MPD MRB
GENERAL VISUAL INSPECTION OF THE WING CENTER SECTION FORWARD SIDE OF FRONT SPAR, INCLUDING SIDE OF BODY/TERMINAL FITTING ATTACHMENTS. I N T E R N A L
125 emp 126 192 emp emp emp emp emp emp emp
121EW 121HW 122GW 191FL 191FR 192AL 192AR 192BL 192BR 192HL 192HR
MPD MRB
57-050-00 MSI 57-050-00
AMM AMM
51-05-01-210 57-05-03-210
ITEMS
57-040-00 MSI 57-040-00 I: 6 YRS I: 18000 CYC
E2 HHI 737-700
2 25-apr-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
3 05-sep-06
ATA: 57 - 14
Page 1 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
571400 02000
GENERAL VISUAL INSPECTION OF THE FORWARD SIDE OF WING CENTER SECTION FRONT SPAR, INCLUDING THE SIDE OF BODY/TERMINAL FITTING. I N T E R N A L ACCESS REMOVE AFT PANELS IN FORWARD CARGO COMPARTMENT.
125 126 191 emp emp emp emp emp emp 195 emp 196 emp
emp S1006 191AL 191AR 191CL 191CR 191D 191FL 191FR 195AL 195AR 196AL 196AR
MPD MRB
GENERAL VISUAL INSPECTION OF THE INSIDE WING CENTER SECTION: 1.UPPER SURFACE (INCLUDING SKINS, TYPICAL AND VENT STRINGERS, SPLICE STRINGER, AT ATTACHMENT TO FLOOR BEAMS); 2.LOWER SURFACE (INCLUDING SKINS, TYPICAL STRINGERS, SPLICE STRINGERS, AT ATTACHMENT TO KEEL BEAM, AT DRAIN INSTALLATION, AT ACCESS HOLE, AT ATTACHMENT TO FUSELAGE DRAG ANGLE, AT ATTACHMENT TO LOWER BEAM AT BL 41); 3.FRONT AND REAR SPARS (INCLUDING WEBS AND STIFFENERS, UPPER AND LOWER SPAR CHORDS, ATTACHMENTS TO SKIN); 4.SIDE OF BODY RIB (INCLUDING WEBS AND STIFFENERS, UPPER RIB CHORD, LOWER TEE CHORD, FRONT AND REAR SPAR TERMINAL FITTINGS, SPLICE FITTINGS); 5.SPANWISE BEAMS. I N T E R N A L
131 emp 132 emp emp emp 231 232
131AB S1303 192CL 192CR 192E 192F emp emp
MPD MRB
57-020-00 MSI 57-020-00
AMM AMM
51-05-01-210 57-05-03-210
R
571400 03000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-010-00 MSI 57-010-00 I: 10 YRS I: 36000 CYC
E2 HHI 737-700
2 23-jul-08
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
3 05-sep-06
ATA: 57 - 14
Page 2 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
571400 04000
DETAILED INSPECTION OF LOWER WING PANEL, RAIL STRINGERS; INTERNAL SURFACE OF STRINGERS 6 & 8, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE 57-20-02) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-02.
532 emp emp emp emp emp 632 emp emp emp emp emp
532AB 532BB 532DB 532EB 532HB 532JB 632AB 632BB 632DB 632EB 632HB 632JB
MPD MRB
57-616-00 MSI 57-616-00
AMM
57-05-02-200
DETAILED INSPECTION OF LOWER WING PANEL, SPLICE STRINGERS; STRINGERS 5 & 9, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE57-20-03) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-03.
434 444 532 emp emp emp emp emp 543 544 632 emp emp emp emp emp 643 644
emp emp 532AB 532BB 532DB 532EB 532HB 532JB emp emp 632AB 632BB 632DB 632EB 632HB 632JB emp emp
MPD MRB
57-618-00 MSI 57-618-00
AMM
57-05-02-200
R
R
571400 05000
R
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
T: 40000 CYC T: 88000 FLH I: 1 s.N I: 36000 CYC
E3 HHI 737-700
1 23-jul-08
T: 30000 CYC T: 64000 FLH I: 1 s.N I: 36000 CYC
E3 HHI 737-700
1 23-jul-08
ATA: 57 - 14
Page 3 of 4
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
571400 05500
SPECIAL DETAILED INSPECTION OF LOWER WING PANEL, SPLICE STRINGERS; INSPECT (HIGH FREQUENCY EDDY CURRENT) THE INTERNAL SURFACE OF STRINGERS 5 & 9, ALL LOCATIONS AT EXTERNAL FAIRINGS/FITTINGS WHERE STRINGER IS VISIBLE IN VICINITY OF RIBS 6, 7, 10, & 14. (PSE57-20-03) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-03.
434 444 532 emp emp emp emp emp 543 544 632 emp emp emp emp emp 643 644
emp emp 532AB 532BB 532DB 532EB 532HB 532JB emp emp 632AB 632BB 632DB 632EB 632HB 632JB emp emp
MPD MRB
57-618-01 MSI 57-618-01
AMM
57-05-02-200
SPECIAL DETAILED INSPECTION OF LOWER WING PANEL, UNDER THE NACELLE FITTING; INSPECT (ULTRASONIC) THE SKIN PANEL UNDER R2, R3 AND R4 NACELLE FITTINGS BETWEEN THE FRONT SPAR CHORD AND SPLICE STRINGER 5. (PSE 57-20-09) I N T E R N A L NOTE( I ) SEE MPD SECTION 9, FIGURE 1, FLIGHT LENGTH SENSITIVE (FLS) TO DETERMINE THRESHOLD INTERVAL. FOR REPEAT INTERVAL AND SAMPLING SEE DTR 57-20-09.
434 emp emp 444 emp emp 532 632
434AL 434AR 434BL 444AL 444AR 444BL emp emp
MPD MRB
57-643-00 MSI 57-643-00
AMM
57-05-02-200
R
R
571400 07000
R
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
T: 40000 CYC T: 88000 FLH I: 1 s.N I: 36000 CYC
E4 HHI 737-700
1 23-jul-08
T: 40000 CYC T: 88000 FLH I: 18000 CYC I: 1 s.N
E4 HHI 737-700
1 23-jul-08
ATA: 57 - 14
Page 4 of 4
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 15
571500 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MAIN LANDING GEAR TRUNNION SUPPORT BEAM GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT MAIN LANDING GEAR SUPPORT STRUCTURE: 1.MAIN LANDING GEAR BEAM ASSEMBLY; 2.OUTBOARD SUPPORT (DOG HOUSE) ASSEMBLY; 3.INBOARD SUPPORT (HANGER LINK) ASSEMBLY; 4.TRUNNION SUPPORT ASSEMBLY; 5.STABILIZER LINKS, INCLUDING ATTACH FITTINGS AND FUSE PINS. I N T E R N A L
551 emp 651 emp
551DT 551ET 651DT 651ET
MPD MPD MRB MRB
57-250-01 57-250-02 MSI 57-250-01 MSI 57-250-02 I: 18000 CYC I: 6 YRS
ITEMS
ATA: 57 - 15
E2 HHI 737-700
2 25-apr-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 21
572100 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
LEADING EDGE GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LEADING EDGE CAVITY, INCLUDING FLAPS AND SLATS. I N T E R N A L ACCESS EXTEND KRUEGER FLAPS AND SLATS. ACCESS PANEL: 521AAB , 521ABB, 621AAB
511 512 513 521 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 522 523 524 525 611 612 613 621 emp emp
emp emp emp 521AB 521BB 521CB 521DB 521EB 521FB 521GB 521HB 521JB 521KB 521LB 521MB 521NB 521PB 521QB 521RB 521SB 521TB 521UB 521VB 521WB 521XB 521YB 521ZB emp emp emp emp emp emp emp 621AB 621BB 621CB
ITEMS
MPD MPD MRB MRB
57-130-01 57-130-02 MSI 57-130-01 MSI 57-130-02 I: 10 YRS
ATA: 57 - 21
E2 HHI 737-700
1 03-jun-04
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 622 623 624 625
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
621DB 621EB 621FB 621GB 621HB 621JB 621KB 621LB 621MB 621NB 621PB 621QB 621RB 621SB 621TB 621UB 621VB 621WB 621XB 621YB 621ZB emp emp emp emp
ITEMS
ATA: 57 - 21
Page 2 of 2
HHI R E V
ITEM 57 - 22
R
737-6
MAINTENANCE SCHEDULE
572200 00000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
TRAILING EDGE GENERAL VISUAL INSPECTION OF THE INTERIOR OF LEFT AND RIGHT WING TRAILING EDGE CAVITY, INCLUDING SKINS, RIBS, AILERONS AND SPOILERS. I N T E R N A L ACCESS FLAP EXTENSION REQUIRED FOR INSPECTION.
551 emp emp emp emp emp emp 552 553 561 emp emp 562 563 564 565 566 567 571 emp emp emp emp emp 572 emp emp emp emp emp emp emp emp emp emp emp emp
551AB 551BB 551CB 551DB 551EB 551FB 551GB emp emp 561AB 561BB 561CB emp emp emp emp emp emp 571AB 571BB 571CB 571DB 571EB 571FB 572AB 572BB 572CB 572CT 572DB 572DT 572EB 572FB 572FT 572GB 572GT 572HB S5001
ITEMS
MPD MPD MRB MRB
57-270-01 57-270-02 MSI 57-270-01 MSI 57-270-02 T: 10 YRS I: 5 YRS
ATA: 57 - 22
E2 HHI 737-700
3 23-jul-08
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS 651 emp emp emp emp emp emp 652 653 661 emp emp 662 663 664 665 666 667 671 emp emp emp emp emp 672 emp emp emp emp emp emp emp emp emp emp emp emp
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
651AB 651BB 651CB 651DB 651EB 651FB 651GB emp 653AT 661AB 661BB 661CB emp emp emp emp emp emp 671AB 671BB 671CB 671DB 671EB 671FB 672AB 672BB 672CB 672CT 672DB 672DT 672EB 672FB 672FT 672GB 672GT 672HB S6002
ITEMS
ATA: 57 - 22
Page 2 of 2
HHI R E V
ITEM 57 - 31
R
737-6
MAINTENANCE SCHEDULE
573100 00000
DESCRIPTION
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING UPPER SURFACE GENERAL VISUAL INSPECTION OF THE UPPER SIDE OF LEFT AND RIGHT OUTBOARD WING UPPER SURFACE (UNDER SIDE-OF-BODY FAIRING), INCLUDING: 1.WING UPPER SURFACE AT SIDE-OF-BODY SPLICE, INCLUDING UPPER RIB CHORD; 2.WING UPPER SURFACE AT ATTACHMENT LOCATIONS. I N T E R N A L
R
573100 02000
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE UPPER SIDE OF UPPER WING SURFACE: 1.UPPER PANEL, INCLUDING AT ATTACHMENTS, FRONT AND REAR SPAR UPPER CHORDS, AND SIDE OF BODY UPPER RIB CHORD; 2.FLOOR BEAMS FROM STA 540 TO STA 727, INCLUDING AT FLOOR BEAM ATTACHMENTS; 3.INSPECT FOR CONDITION OF SECONDARY VAPOR BARRIER. I N T E R N A L ACCESS REMOVE FLOOR PANELS AND INSULATION AS REQUIRED IN PASSENGER COMPARTMENT AS REQUIRED FOR ACCESS.
195 emp emp emp emp emp emp 196 emp emp emp emp emp emp 511 531 551 611 631 651
191AR 195AL 195AR 195BL 195BR 195CL 195CR 191AL 196AL 196AR 196BL 196BR 196CL 196CR emp emp emp emp emp emp
MPD MPD MRB MRB MPD MPD MRB
135 136 231 232
emp emp emp emp
MPD MRB
ITEMS
57-070-01 57-070-02 MSI 57-070-01 MSI 57-070-02 57-070-01 57-070-02 MSI 57-070-01 I: 6 YRS I: 18000 CYC
E2 HHI 737-700
3 23-jul-08
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
2 25-apr-06
57-090-00 MSI 57-090-00
ATA: 57 - 31
Page 1 of 1
HHI R E V
ITEM 57 - 32
R
737-6
MAINTENANCE SCHEDULE
573200 01000
DESCRIPTION
Date: 23-jul-08
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING LOWER SURFACE GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT WING LOWER SURFACE UNDER STRUT FAIRING, INCLUDING ALL ATTACHMENT LOCATIONS. I N T E R N A L
R
573200 02000
ZONE ACCESS
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD WING LOWER SURFACE (UNDER LOWER SIDE OF BODY FAIRING), INCLUDING ATTACHMENT LOCATIONS. I N T E R N A L
434 emp emp 444 emp emp 531 532 631 632
434AL 434AR 434BL 444AL 444AR 444BR emp emp emp emp
MPD MPD MRB MRB
192 emp emp emp emp emp emp emp emp emp emp emp emp emp 511 531 551 611 631 651
191AL 191AR 191FL 191FR 192AL 192AR 192BL 192BR 192HL 192HR 193AL 193AR 193CL 193CR emp emp emp emp emp emp
MPD MPD MRB MRB
ITEMS
57-110-01 57-110-02 MSI 57-110-01 MSI 57-110-02 I: 9000 CYC I: 30 MTH I: 36 MTH
E2 HHI 737-700
3 23-jul-08
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
57-060-01 57-060-02 MSI 57-060-01 MSI 57-060-02
ATA: 57 - 32
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
573200 03000
GENERAL VISUAL INSPECTION OF THE FUEL ACCESS HOLES IN LEFT AND RIGHT OUTBOARD WING LOWER SURFACE. ( TANK ENTRY IS NOT REQUIRED.) I N T E R N A L
Date: 23-jul-08
ZONE ACCESS 531 emp 532 emp emp emp emp emp emp emp emp emp emp emp emp emp emp emp 533 emp emp 534 emp 631 emp 632 emp emp emp emp emp emp emp emp emp emp emp emp emp
STRUCTURE
531AB 531BB 532AB 532BB 532CB 532DB 532EB 532FB 532GB 532HB 532JB 532KB 532LB 532MB 532NB 532PB 532QB 532RB 533AB 533BB 533CB 534AB 534BB 631AB 631BB 632AB 632BB 632CB 632DB 632EB 632FB 632GB 632HB 632JB 632KB 632LB 632MB 632NB 632PB
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-160-01 57-160-02 MSI 57-160-01 MSI 57-160-02 I: 18000 CYC I: 6 YRS
ATA: 57 - 32
E2 HHI 737-700
2 25-apr-06
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
573200 04000
573200 05000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS emp emp 633 emp emp 634 emp
632QB 632RB 633AB 633BB 633CB 634AB 634BB
GENERAL VISUAL INSPECTION OF THE L/H AND R/H LOWER SIDE OF 542 LOWER SURFACE (UNDER FLAP SUPPORT NO.3 AND NO. 6 642 FAIRING),INCLUDING ALL ATTACHMENT LOCATIONS AND ACCESS HOLES. I N T E R N A L ACCESS EXTEND FLAPS
542AB 642AB
GENERAL VISUAL INSPECTION OF THE L/H AND R/H LOWER SIDE OF LOWER SURFACE (UNDER FLAP SUPPORT NO.1&2 AND 7&8 FAIRINGS), INCLUDING ALL ATTACHMENT LOCATIONS AND ACCESS HOLES. I N T E R N A L ACCESS EXTEND FLAPS
543AB 544AB 643AB 644AB
543 544 643 644
STRUCTURE
ITEMS
REFERENCES
MPD MPD MRB MRB
MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-220-01 57-220-02 MSI 57-220-01 MSI 57-220-02 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
57-240-01 57-240-02 MSI 57-240-01 MSI 57-240-02
ATA: 57 - 32
Page 3 of 3
HHI R E V
ITEM 57 - 35
R
737-6
MAINTENANCE SCHEDULE
573500 00000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
WING FITTINGS GENERAL VISUAL INSPECTION OF THE FOLLOWING FITTINGS L/H AND R/H: 1. FRONT SPAR PITCH LOAD FITTING (R1); 2. AFT DRAG LOAD FITTING (R2); 3.OUTBOARD SIDE LOAD FITTING (R3); 4.INBOARD SIDE LOAD FITTING (R4); 5.SIDE BRACE SUPPORT FITTINGS (R7 AND R8); 6.R3 FORWARD BACKUP FITTING. INSPECT UPPER WING SKIN AT ATTACHMENT TO NACELLE FITTING R1. I N T E R N A L ACCESS REMOVE UPPER WING JUNCTION FAIRING AND AFT STRUT FAIRING PANEL.
431 emp emp emp emp 434 441 emp 444 emp emp emp
431CL 431CR 434AL 434AR 434BL emp 441CL 441CR 444AL 444AR 444BL 444BR
ITEMS
MPD MPD MRB MRB
57-100-01 57-100-02 MSI 57-100-01 MSI 57-100-02 I: 9000 CYC I: 30 MTH I: 36 MTH
ATA: 57 - 35
E2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 52
575200 00000
575200 01000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
TRAILING EDGE FLAPS GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD FLAP INBOARD AND OUTBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING ASSEMBLY,AND AFT LINKS. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS REMOVE FLAP FORWARD FAIRINGS AND DEPLOY FLAPS.
543 544 643 644
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP 542 OUTBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING 642 ASSEMBLY,AND AFT ATTACH FITTING. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS REMOVE FLAP SUPPORT FORWARD FAIRING AND DEPLOY FLAPS.
543AB 544AB 643AB 644AB
542AB 642AB
ITEMS
MPD MPD MRB MRB
MPD MPD MRB MRB
57-230-01 57-230-02 MSI 57-230-01 MSI 57-230-02 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
I: 18000 CYC I: 6 YRS
E2 HHI 737-700
2 25-apr-06
57-210-01 57-210-02 MSI 57-210-01 MSI 57-210-02
ATA: 57 - 52
Page 1 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
575200 02000
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP INBOARD TRACK ASSEMBLY, CARRIAGE ASSEMBLY, FORWARD FITTING ASSEMBLY, AFT LINK AND AFT LINK PINS. NORMAL OVERHAUL PROCEDURES, APPLIED WITH THE FLAP TRACK ASSEMBLIES, CARRIAGE ASSEMBLIES AND FORWARD FITTING ASSEMBLIES REMOVED, AT INTERVALS NOT EXCEEDING 10 YEARS, ARE ADEQUATE TO MAINTAIN CORROSION AT SAFE LEVELS ON THESE COMPONENTS. THEREFORE APPLICATION OF THE BASIC TASKS AND REPORTING ARE NOT REQUIRED ON THESE COMPONENTS I N T E R N A L ACCESS TO INBOARD SIDE OF TRACK ASSEMBLY THROUGH THE MLG WHEEL WELL.
541 emp emp emp emp 641
193CL 193CR 194BL 194CL 194CR 194BR
MPD MPD MRB MRB
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD FLAP INTERNALLY: 1.FRONT SPAR (AFT SIDE), REAR SPAR (FORWARD SIDE), INSPAR RIBS, TORQUE TUBE, TORQUE TUBE RIBS; 2.AFT FLAP TRACK SUPPORT ASSEMBLY ATTACHMENT ON MAIN FLAP REAR SPAR. I N T E R N A L
553 emp emp emp emp 653 emp emp emp emp
553AT 553BB 553CT 553DT 553ET 653AT 653BB 653CT 653DT 653ET
MPD MPD MRB MRB
575200 06000
Date: 23-jul-08
ZONE ACCESS
STRUCTURE
ITEMS
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-200-01 57-200-02 MSI 57-200-01 MSI 57-200-02 I: 18000 CYC I: 6 YRS
E2 HHI 737-700
3 25-apr-06
I: 36000 CYC I: 10 YRS
E2 HHI 737-700
1 03-jun-04
57-300-01 57-300-02 MSI 57-300-01 MSI 57-300-02
ATA: 57 - 52
Page 2 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
575200 07000
GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT OUTBOARD FLAP INTERNALLY: 1.FRONT SPAR (AFT SIDE), INCLUDING SUPPORT FITTINGS AT WBL 254 AND 358; 2.REAR SPAR (FORWARD SIDE); 3.INSPAR RIBS AND AFT FLAP TRACK SUPPORT RIBS. I N T E R N A L ACCESS DEPLOY AFT FLAP SO THAT AFT FLAP TRACKS DO NOT BLOCK VIEW OF REAR SPAR LOWER CHORD.
Date: 23-jul-08
ZONE ACCESS 567 emp emp emp emp emp emp emp 667 emp emp emp emp emp emp emp
STRUCTURE
567AT 567BT 567CT 567DT 567ET 567FT 567GT 567HT 667AT 667BT 667CT 667DT 667ET 667FT 667GT 667HT
ITEMS
REFERENCES MPD MPD MRB MRB
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
57-330-01 57-330-02 MSI 57-330-01 MSI 57-330-02 I: 36000 CYC I: 10 YRS
ATA: 57 - 52
E2 HHI 737-700
1 03-jun-04
Page 3 of 3
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 54
575400 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
SLATS DETAILED VISUAL INSPECTION OF THE LEFT AND RIGHT WING SLAT TRACKS. I N T E R N A L ACCESS EXTEND SLATS.
522 emp emp emp emp emp emp emp 523 524 525 622 emp emp emp emp emp emp emp 623 624 625
521CB 521FB 521JB 521MB 521QB 521TB 521WB 521ZB emp emp emp 621CB 621FB 621JB 621MB 621QB 621TB 621WB 621ZB emp emp emp
ITEMS
MPD MPD MRB MRB
57-140-01 57-140-02 MSI 57-140-01 MSI 57-140-02 I: 6 YRS
ATA: 57 - 54
E3 HHI 737-700
2 25-apr-06
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 57 - 55
575500 00000
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
SPOILER GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT INBOARD GROUND SPOILER ACTUATOR FITTINGS. I N T E R N A L ACCESS EXTEND FLAPS AND GROUND SPOILERS.
552 652
5521S 6521S
MPD MPD MRB MRB
57-280-01 57-280-02 MSI 57-280-01 MSI 57-280-02 I: 6 YRS I: 18000 CYC
ITEMS
ATA: 57 - 55
E2 HHI 737-700
2 25-apr-06
Page 1 of 1
HHI R E V
ITEM 71 71 - 11 711101 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
711102 20000
VISUALLY CHECK THE LEFT AND RIGHT INLET COWL (INNER SIDE AND 412 OUTER SKIN). 422
emp emp
VISUALLY CHECK THE LEFT AND RIGHT ENGINE FAN COWL FOR CONDITION AND SECURITY OF INSTALLATION.
413 414 423 424
emp emp emp emp
R
MPD MPD MRB
Date: 23-jul-08
EFF
R L ITEM BY E E REVISION P V DATE
71-11-01-200-801-F00 I: 800 FLH
MPD MPD MRB
71-020-01 71-020-02 MSI 71-020-01 RTE:9 MSI 71-020-02 RTE:9
CHECK THRUST REVERSER, EXHAUST PLUG, EXHAUST CASE STRUTS 410 AND VISIBLE TURBINE BLADES ON LPT FOR OBVIOUS DAMAGE AND 420 EVIDENCE OF METAL / OIL ACCUMULATION
emp emp
empty
CHECK ENGINE COWLING, INLET COWL, NOSE DOME AND VISIBLE FAN 410 BLADES FOR OBVIOUS DAMAGE. 420 CHECK ACCESS PANELS AND BLOW OUT DOORS FOR CONDITION AND SECURITY ALSO CHECK FOR OPEN LATCHES AND SIGNS OF FLUID LEAKAGE.
emp emp
empty
AMM
AMM AMM AMM
ITEMS
71-010-01 71-010-02 MSI 71-010-01 RTE:9 MSI 71-010-02 RTE:9
AMTOSS
AMTOSS AMM
711104 20000
TSK
INLET COWL
MRB
711103 20000
THRESHOLD INTERVAL
POWER PLANT
MRB
R
737-6
MAINTENANCE SCHEDULE
E2 HHI 737-700
3 03-jun-04
71-11-02-20 I: 4000 FLH 71-11-02-200-801-F00
E2 HHI 737-700
3 23-jul-08
71-00-00 SERVICE EXPERIENCE
I: 1 T
E2 HHI 737-700
1 02-aug-99
SERVICE I: 1 T EXPERIENCE 71-11-00 71-11-01-200-801-F00 71-11-02-200-802-F00
E2 HHI 737-700
3 03-jun-04
ATA: 71 - 11
Page 1 of 1
HHI R E V
ITEM 71 - 71
R
737-6
MAINTENANCE SCHEDULE
717100 20000
R
717100 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ENGINE DRAINS GENERAL VISUAL INSPECTION OF THE LEFT AND RIGHT ENGINE DRAIN 411 LINES. emp 415 416 417 421 emp 425 426 427
413 414 415 416 emp 423 424 425 426 emp
MPD MPD MRB
AMTOSS AMM
71-71-00-20 I: 6000 FLH 71-71-00-200-802-F00
OPERATIONALLY CHECK ALL LEFT AND RIGHT ENGINE DRAIN LINES.
emp emp
MPD MPD MRB
71-040-01 71-040-02 MSI 71-040-01 RTE:9 MSI 71-040-02 RTE:9
411 421
MRB
MRB AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
71-050-01 71-050-02 MSI 71-050-01 RTE:9 MSI 71-050-02 RTE:9
71-71-00-700-801-F00 I: 6 YRS
ATA: 71 - 71
E1 HHI 737-700
5 23-jul-08
F1 HHI 737-700
3 25-apr-06
Page 1 of 1
HHI R E V
R
ITEM
DESCRIPTION
72
ENGINE
72 - 00
ENGINE
720000 20000
R R
720000 20200
ZONE ACCESS
STRUCTURE
REFERENCES
413 414 415 416 423 424 425 426
MPD MPD MRB
AMTOSS AMM
72-00-00-20 I: 1600 CYC 72-00-00-200-805-F00
BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE HPT NOZZLE. 411 emp 421 emp
415 416 425 426
MPD MPD MRB
72-200-01 72-200-02 MSI 72-200-01 RTE:6 MSI 72-200-02 RTE:6
R 720000 20300
MRB
BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE HPT BLADES. 411 emp 421 emp
415 416 425 426
R
72-00-00-20 I: 1600 CYC 72-00-00-200-806-F00
MPD MPD MRB
72-210-01 72-210-02 MSI 72-210-01 RTE:6 MSI 72-210-02 RTE:6
AMTOSS AMM
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
72-180-01 72-180-02 MSI 72-180-01 RTE:9 MSI 72-180-02 RTE:9
AMTOSS AMM
MRB
Date: 23-jul-08
THRESHOLD INTERVAL
BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE COMBUSTION 411 CHAMBER. emp emp emp 421 emp emp emp
MRB
R
737-6
MAINTENANCE SCHEDULE
72-00-00-20 I: 1600 CYC 72-00-00-200-807-F00
ATA: 72 - 00
E4 HHI 737-700
2 23-jul-08
E4 HHI 737-700
2 23-jul-08
E4 HHI 737-700
2 23-jul-08
Page 1 of 2
HHI R E V
ITEM
R
720000 20400
R
R
720011 01200
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
413 414 415 416 423 424 425 426
MPD MPD MRB
AMTOSS AMM AMM AMM
72-00-00-200-814-F00 I: 6000 FLH 72-00-00-200-804-F00 I: 6000 CYC 72-00-00-200-802-F00 72-00-00-200-817-F00
VISUAL CHECK OF THE LEFT AND RIGHT ENGINE FAN INLET ATTACHMENT 411 BOLTS. emp 421 emp
413 414 423 424
MPD MPD MRB
72-080-01 72-080-02 MSI 72-080-01 RTE:9 MSI 72-080-02 RTE:9
R 720021 00200
MRB
VISUAL CHECK OF THE ATTACHMENT BOLTS FOR THE LEFT AND RIGHT 411 FORWARD ENGINE MOUNT. emp 421 emp
413 414 423 424
R
71-11-01-20 I: 6000 FLH 71-11-01-200-802-F00
MPD MPD MRB
72-090-01 72-090-02 MSI 72-090-01 RTE:9 MSI 72-090-02 RTE:9
AMM AMTOSS
ITEMS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
72-120-01 72-120-02 MSI 72-120-01 RTE:6 MSI 72-120-02 RTE:6
AMTOSS AMM
MRB
Date: 23-jul-08
THRESHOLD INTERVAL
BORESCOPE INSPECTION OF THE LEFT AND RIGHT ENGINE STAGES 2, 411 4, 6 & 8 HPC BLADES emp emp emp 421 emp emp emp
MRB
R
737-6
MAINTENANCE SCHEDULE
71-21-00-200-801-F00 I: 6000 FLH 71-21-00-20
ATA: 72 - 00
E4 HHI 737-700
4 23-jul-08
E2 HHI 737-700
3 23-jul-08
E2 HHI 737-700
3 23-jul-08
Page 2 of 2
HHI R E V
ITEM 72 - 20
R
737-6
MAINTENANCE SCHEDULE
722000 21000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FAN SECTION VISUALLY CHECK OF THE LEFT AND RIGHT ENGINE TRANSFER AND /OR 411 ACCESSORY GEARBOX MOUNT FLANGES. emp 421 emp
413 414 423 424
MPD MPD MRB MRB
R
Date: 23-jul-08
THRESHOLD INTERVAL
AMM AMTOSS
ITEMS
72-070-01 72-070-02 MSI 72-070-01 RTE:9 MSI 72-070-02 RTE:9 72-20-00-210-801-F00 I: 6000 FLH 72-20-00-21 I: 6000 CYC
ATA: 72 - 20
E2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 72 - 21
722100 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
VISUALLY CHECK THE LEFT AND RIGHT ENGINE INLET AND FAN BLADES. 411 421
emp emp
MPD MPD MRB
EFF
R L ITEM BY E E REVISION P V DATE
DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE INLET AND FAN 411 BLADES. 421
emp emp
72-21-00-200-801-F00 I: 50 FLH
MPD MPD MRB
72-020-01 72-020-02 MSI 72-020-01 RTE:6 MSI 72-020-02 RTE:6
AMTOSS
ITEMS
72-010-01 72-010-02 MSI 72-010-01 RTE:6 MSI 72-010-02 RTE:6
AMTOSS
MRB
Date: 23-jul-08
TSK
SPINNER CONE
MRB
722100 22000
THRESHOLD INTERVAL
72-21-00-220-801-F00 I: 1200 FLH
ATA: 72 - 21
E2 HHI 737-700
3 03-jun-04
E3 HHI 737-700
4 25-apr-06
Page 1 of 1
HHI R E V
ITEM 72 - 23
R
722304 20000
R R
737-6
MAINTENANCE SCHEDULE
722304 21000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
THRUST MOUNT FITTINGS VISUAL CHECK OF THE LEFT AND RIGHT ENGINE ATTACHMENT BOLTS 411 FOR THE THRUST MOUNT FITTINGS. emp emp emp 421 emp emp emp
413 414 415 416 423 424 425 426
MPD MPD MRB
AMM AMTOSS
72-23-04-200-802-F00 I: 5000 CYC 72-23-04-20
VISUAL CHECK OF THE LEFT AND RIGHT ENGINE THRUST MOUNT FITTINGS.
413 414 415 416 423 424 425 426
MPD MPD MRB
72-110-01 72-110-02 MSI 72-110-01 RTE:8 MSI 72-110-02 RTE:8
411 emp emp emp 421 emp emp emp
ITEMS
MRB
MRB AMM AMTOSS
72-100-01 72-100-02 MSI 72-100-01 RTE:9 MSI 72-100-02 RTE:9
72-23-04-200-801-F00 I: 6000 FLH 72-23-04-20
ATA: 72 - 23
E2 HHI 737-700
2 23-jul-08
E2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 72 - 30
723000 31000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COMPRESSOR SECTION DETAILED INSPECTION AND LUBRICATION OF THE ENGINES FAN BLADE 411 PRESSURE FACES AND FAN DISK DOVETAIL SLOTS. 421
emp emp
empty
AMM
AMM
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
ESM 005 72-21-02 REMOVAL/ INSTALLATION 72-21-01 REMOVAL/ INSTALLATION
I: 3000 CYC I: 5000 FLH
ATA: 72 - 30
E3 HHI S 737-700
3 18-mar-05
Page 1 of 1
HHI R E V
ITEM 72 - 50
R
737-6
MAINTENANCE SCHEDULE
725000 20000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
TURBINE SECTION VISUAL CHECK OF THE LEFT AND RIGHT ENGINE AFT MOUNTS CLEVIS 411 FOR STRUCTURAL INTEGRITY FAILURE. emp emp emp 421 emp emp emp
413 414 415 416 423 424 425 426
ITEMS
MPD MPD MRB MRB AMTOSS AMM
72-300-01 72-300-02 MSI 72-300-01 RTE:9 MSI 72-300-02 RTE:9 72-56-00-20 I: 6000 FLH 72-56-00-200-802-F00
ATA: 72 - 50
E2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM 72 - 60
726000 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ACCESSORY DRIVE SECTION VISUAL CHECK OF THE LEFT AND RIGHT ENGINE AGB AND TGB ATTACHMENT FLANGES.
411 emp 421 emp
413 414 423 424
MPD MPD MRB MRB AMTOSS AMTOSS
Date: 23-jul-08
THRESHOLD INTERVAL
ITEMS
72-340-01 72-340-02 MSI 72-340-01 RTE:9 MSI 72-340-02 RTE:9 72-60-00-200-801-F00 I: 6000 FLH 72-63-00-200-801-F00
ATA: 72 - 60
E2 HHI 737-700
3 30-nov-05
Page 1 of 1
HHI R E V
ITEM 73 73 - 11
R
737-6
MAINTENANCE SCHEDULE
731102 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ENGINE FUEL AND CONTROL FUEL FILTER REPLACE THE LEFT AND RIGHT ENGINE FUEL FILTER.
411 emp 421 emp
413 414 423 424
MPD MPD MRB MRB
R
Date: 23-jul-08
THRESHOLD INTERVAL
AMTOSS AMM AMM
ITEMS
73-010-01 73-010-02 MSI 73-010-01 RTE:6 MSI 73-010-02 RTE:6 73-11-02-00 I: 6000 FLH 73-11-02-000-801-F00 73-11-02-400-801-F00
ATA: 73 - 11
S
HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
ITEM 73 - 21
R
737-6
MAINTENANCE SCHEDULE
732100 74000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FUEL CONTROL SYSTEM INTERROGATE THE FMC CDU FOR LEFT AND RIGHT ENGINE FAULTS.
211 212
emp emp
MPD MPD MRB MRB
R
Date: 23-jul-08
THRESHOLD INTERVAL
AMTOSS AMM
ITEMS
73-020-01 73-020-02 MSI 73-020-01 RTE:9 MSI 73-020-02 RTE:9 73-21-00-74 I: 150 FLH 73-21-00-740-803-F00
ATA: 73 - 21
F1 HHI 737-700
2 23-jul-08
Page 1 of 1
HHI R E V
ITEM 74 74 - 21
R
742101 20000
R R
737-6
MAINTENANCE SCHEDULE
742102 20000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
IGNITION IGNITION LEADS DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE IGNITOR LEAD. 411 emp emp emp 421 emp emp emp
413 414 415 416 423 424 425 426
MPD MPD MRB
AMTOSS AMM
74-21-01-20 I: 4000 CYC 74-21-01-200-801-F00
DETAILED INSPECTION OF THE ENGINE IGNITOR PLUGS.
413 414 415 416 423 424 425 426
MPD MPD MRB
74-010-01 74-010-02 MSI 74-010-01 RTE:6 MSI 74-010-02 RTE:6
411 emp emp emp 421 emp emp emp
ITEMS
MRB
MRB AMTOSS AMM
74-020-01 74-020-02 MSI 74-020-01 RTE:6 MSI 74-020-02 RTE:6
74-21-02-20 I: 1600 CYC 74-21-02-200-801-F00
ATA: 74 - 21
E3 HHI 737-700
3 23-jul-08
E3 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
ITEM 78 78 - 11
R
737-6
MAINTENANCE SCHEDULE
781100 21000
R
Date: 23-jul-08
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EXHAUST TURBINE EXHAUST SYSTEM VISUAL CHECK OF LEFT AND RIGHT ENGINE LABYRINTH SEALS.
417 emp emp emp 427 emp emp emp
413 414 415 416 423 424 425 426
ITEMS
MPD MPD MRB MRB AMTOSS AMM
78-020-01 78-020-02 MSI 78-020-01 RTE:9 MSI 78-020-02 RTE:9 78-11-00-21 I: 6000 FLH 78-11-00-210-801-F00
ATA: 78 - 11
E2 HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
ITEM 78 - 31
R
783100 70000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
PERFORM OPERATIONAL CHECK (BITE) ON THE LEFT AND RIGHT ENGINE 117 EAU. 118
117A emp
R 783100 71000
PERFORM AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ENGINE 117 T/R SYNC LOCK 118 415 416 425 426
117A emp emp emp emp emp
R 783100 73000
MPD MPD MRB
783106 20000
R
Date: 23-jul-08
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PERFORM AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ENGINE 211 "REVERSER" LIGHT INDICATION SYSTEM. 212
emp emp
VISUALLY CHECK THE LEFT AND RIGHT ENGINE BLOCKER DOORS.
415 emp emp 416 425 emp emp 426
413 414 415 416 423 424 425 426
ITEMS
78-120-01 78-120-02 MSI 78-120-01 RTE:9 MSI 78-120-02 RTE:9
AMTOSS AMM
78-31-00-70 I: 1200 FLH 78-31-00-700-804-F00
AAR MPD MPD MRB
78-CMR-01 78-110-01 78-110-02 MSI 78-110-01 RTE:9 MSI 78-110-02 RTE:9
MRB
F1 HHI 737-700
3 23-jul-08
F1 HHI 737-700
2 23-jul-08
I: 6000 FLH
F1 HHI 737-700
3 18-mar-05
78-31-06-20 I: 6000 FLH 78-31-06-200-801-F00
E2 HHI 737-700
4 23-jul-08
AMTOSS AMM
78-31-00-70 I: 5000 FLH 78-31-00-700-803-F00
MPD MPD MRB
78-130-01 78-130-02 MSI 78-130-01 RTE:9 MSI 78-130-02 RTE:9
MRB
R
THRESHOLD INTERVAL
THRUST REVERSER SYSTEM ( HARDWARE)
MRB
R
737-6
MAINTENANCE SCHEDULE
AMTOSS AMTOSS
78-31-00-71 78-31-00-70
MPD MPD MRB
78-070-01 78-070-02 MSI 78-070-01 RTE:9 MSI 78-070-02 RTE:9
MRB AMTOSS AMM
ATA: 78 - 31
Page 1 of 3
HHI R E V
ITEM
R
783107 90000
DESCRIPTION DETAILED INSPECTION OF THE THRUST REVERSER DRAG LINK SPHERICAL BEARINGS
R R
783112 20000
VISUALLY CHECK THE RIGHT AND LEFT ENGINE T / R FIRE SEAL.
R R
737-6
MAINTENANCE SCHEDULE
783112 21000
DETAILED INSPECT THE LEFT AND RIGHT ENGINE T/R FIRE SEAL.
R 783114 20000
Date: 23-jul-08
VISUALLY CHECK THE LEFT AND RIGHT ENGINE T/R'S INNER WALL.
ZONE ACCESS
STRUCTURE
REFERENCES
THRESHOLD INTERVAL
415 emp emp 416 425 emp emp 426
413 414 415 416 423 424 425 426
MPD MPD MRB
AMTOSS AMM
78-31-07-90 I: 6000 FLH 78-31-07-900-801-F00
415 emp emp 416 425 emp emp 426
413 414 415 416 423 424 425 426
MPD MPD MRB
78-090-01 78-090-02 MSI 78-090-01 RTE:8 MSI 78-090-02 RTE:8
AMTOSS AMM
78-31-12-20 I: 3600 FLH 78-31-12-200-801-F00
415 emp emp 416 425 emp emp 426
413 414 415 416 423 424 425 426
MPD MPD MRB
78-100-01 78-100-02 MSI 78-100-01 RTE:8 MSI 78-100-02 RTE:8
AMTOSS AMM
78-31-12-20 I: 6000 FLH 78-31-12-200-802-F00
415 emp emp 416 425 emp emp 426
413 414 415 416 423 424 425 426
MPD MPD MRB
78-050-01 78-050-02 MSI 78-050-01 RTE:9 MSI 78-050-02 RTE:9
ITEMS
MRB
MRB
MRB
MRB AMTOSS
TSK
EFF
R L ITEM BY E E REVISION P V DATE
78-060-01 78-060-02 MSI 78-060-01 RTE:9 MSI 78-060-02 RTE:9
78-31-14-20
I: 6000 FLH
ATA: 78 - 31
E3 HHI 737-700
7 23-jul-08
E2 HHI 737-700
6 23-jul-08
E3 HHI 737-700
3 23-jul-08
E2 HHI 737-700
3 18-mar-05
Page 2 of 3
HHI
737-6
MAINTENANCE SCHEDULE
R E V
ITEM
DESCRIPTION
R
783123 20000
VISUALLY CHECK THE LEFT AND RIGHT ENGINE BULLNOSE SEAL AND RETAINER.
R
Date: 23-jul-08
ZONE ACCESS 415 emp emp 416 425 emp emp 426
STRUCTURE
413 414 415 416 423 424 425 426
ITEMS
REFERENCES MPD MPD MRB MRB AMTOSS AMM
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
78-080-01 78-080-02 MSI 78-080-01 RTE:9 MSI 78-080-02 RTE:9 78-31-23-20 I: 6000 FLH 78-31-23-200-801-F00
ATA: 78 - 31
E2 HHI 737-700
4 23-jul-08
Page 3 of 3
HHI R E V
ITEM 79 79 - 00
R
790000 20000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE OIL SUPPLY FILTER POP-OUT INDICATOR.
411 421
413BL 423BL
MPD MPD MRB
DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE AGB/ TGB AND AFT AND FWD SUMP MAGNETIC CHIP DETECTOR FOR PARTICLES (FOR ENGINES WITH MCD) OR INTERROGATE DMS FOR CHIP DETECTOR STATUS (FOR ENGINES WITH DEBRIS MONITORING SYSTEM).
211 212 411 421
emp emp 413BL 423BL
R
79-00-00-20 I: 1200 FLH 79-00-00-200-805-F00
MPD MPD MRB
72-320-01 72-320-02 MSI 72-320-01 RTE:6 MSI 72-320-02 RTE:6
AMTOSS AMM
Date: 23-jul-08
EFF
R L ITEM BY E E REVISION P V DATE
TOP OFF ENGINE OIL ON BOTH ENGINES AFTER 5 MINUTES FROM ENGINE 410 SHUT DOWN, BUT NOT GREATER THAN 30 MINUTES AND RECORD 420 CONSUMPTION. CHECK OIL TANK CAP FOR PROPER INSTALLATION.
emp emp
E3 HHI 737-700
3 23-jul-08
79-00-00-20 I: 500 FLH 79-00-00-200-804-F00
E3 HHI 737-700
3 23-jul-08
SERVICE EXPERIENCE 12-13-11
S HHI E1 737-700
2 18-mar-05
empty
AMM
ITEMS
79-020-01 79-020-02 MSI 79-020-01 RTE:9 MSI 79-020-02 RTE:9
AMTOSS AMM
MRB
790000 80000
TSK
ENGINE OIL GENERAL
R 790000 20500
THRESHOLD INTERVAL
OIL
MRB
R
737-6
MAINTENANCE SCHEDULE
I: 1 Z
ATA: 79 - 00
Page 1 of 1
HHI R E V
ITEM 79 - 21
R
792103 00000
DESCRIPTION
ZONE ACCESS
STRUCTURE
REFERENCES
REMOVE AND REPLACE THE LEFT AND RIGHT ENGINE OIL SUPPLY FILTER 411 ELEMENT. 421
413 423
R
792106 00000
MPD MPD MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
REMOVE AND REPLACE THE LEFT AND RIGHT ENGINE OIL SCAVENGE FILTER ELEMENT.
411 421
413 423
R
79-21-03-40 I: 6000 FLH 79-21-03-00 79-21-03-000-802-F00 79-21-03-400-801-F00
MPD MPD MRB
79-040-01 79-040-02 MSI 79-040-01 RTE:9 MSI 79-040-02 RTE:9
AMTOSS AMTOSS AMM AMM
ITEMS
79-010-01 79-010-02 MSI 79-010-01 RTE:9 MSI 79-010-02 RTE:9
AMTOSS AMTOSS AMM AMM
MRB
Date: 23-jul-08
THRESHOLD INTERVAL
ENGINE OIL FILTER
MRB
R
737-6
MAINTENANCE SCHEDULE
79-21-06-40 I: 6000 FLH 79-21-06-00 79-21-06-000-801-F00 79-21-06-400-801-F00
ATA: 79 - 21
S
HHI 737-700
3 23-jul-08
S
HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
R
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
80
STARTING
80 - 11
STARTER
801101 20000
DETAILED INSPECTION OF THE LEFT AND RIGHT ENGINE STARTER MAGNETIC CHIP DETECTOR FOR METAL CHIPS.
ZONE ACCESS
411 421
STRUCTURE
413 423
REFERENCES
MPD MPD MRB MRB
R
Date: 23-jul-08
AMTOSS AMM
ITEMS
THRESHOLD INTERVAL
TSK
EFF
R L ITEM BY E E REVISION P V DATE
80-010-01 80-010-02 MSI 80-010-01 RTE:6 MSI 80-010-02 RTE:6 80-11-01-20 I: 1600 CYC 80-11-01-200-801-F00
ATA: 80 - 11
E3 HHI 737-700
2 23-jul-08
Page 1 of 1
HHI
1
MAINTENANCE SCHEDULE
737-6/-7/-8
GENERAL
This Component Maintenance Section is an integrated part of the 737 Maintenance Schedule. Component Maintenance Section reflects specific component maintenance tasks under consideration of Airworthiness Authority Requirements as like: - Life Limits from Service Letters - Life Limits from Engine Manual - Requirements from Type Certification Data Sheets - National Requirements - MRBR component requirements All common statements from Maintenance Schedule Introduction are also effective for Component Maintenance Section. Explanation of deviations from Maintenance Schedule Introduction to Component Maintenance Section are given in the following.
2
FORMAT LAYOUT DESCRIPTION AND DEFINITION OF TERMS
2.1
Revision Column
A letter code gives the status of the item at the date of publication shown in the page header: "N" : New "R" : Revised "D" : Deleted Blank : No change
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 1 of 6
HHI
2.2
MAINTENANCE SCHEDULE
737-6/-7/-8
ITEM Column
The item number is split into four figure groups: • group 1 : 2 digits (CM) indicating that this item is part of the Component Maintenance Section • group 2 : 4 digits giving ATA / sub ATA specification as per IPC • group 3 : 2 digits giving ATA-unit specification as per IPC • group 4 : 3 digits giving item number identification In principle each item corresponds to one task (which may cover several "tasks codes") and one interval (and possibly one threshold). If several intervals do appear, they are always in different units (FLH, CYC,...) and in that case the meaning of such a situation is: to apply the interval "what ever comes first".
2.3
Description Column
It gives an accurate part description according to manufacturer nomenclature with a specified part number reference. The part number reference gives a clear statement of considered part numbers approved for installation by IPC or equivalent documents. - P/N all - P/N only - except P/N
i.e. all part numbers with this part description are effected i.e. only specified part numbers with this part description are effected i.e. all part numbers with this part description except for specified part numbers are effected
In addition in that column may appear some notes when necessary. These notes are of 2 categories:
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 2 of 6
HHI
MAINTENANCE SCHEDULE
737-6/-7/-8
Note: General notes affecting some of the parameters produced in the layout (INTERVAL, TASK CODE, etc.). In any case a highlight "NOTE" appear, with, in front of it, a note mark identifying the affected parameters. These possible note marks are: • E : effectivity • T : threshold • I : interval • J : task code • R : reference • M : miscellaneous Condition Note: Specific note when the task to be performed depends on the embodiment of such modifications which are then indicated in that note. In that case a highlight "CONDITION" appears.
2.4
ZONE Column (not used)
NOTE: Due to EDP requirements this field has an initial setting „000“.
2.5
ACCESS Column (not used)
2.6
Structure Column (not used)
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 3 of 6
HHI
2.7
MAINTENANCE SCHEDULE
737-6/-7/-8
REFERENCES Column
It shows each document or manual necessary to be consulted to produce a clear understanding of the requested task, as well as references covering the origin of the item. For items which are affected by Directive from Airworthiness Authorities, the letter's reference will be mentioned in this column, and the maximum allowable limit shown in a NOTE preceded by the note mark "I" (for interval). Such references are indicated by means of their alphabetical code and their number. Examples of references types: Indicates an Airworthiness Requirement • AAR......AD number: Aircraft Maintenance Manual • AMM...........number: Certification Maintenance Requirements • CMR........................: Requirement of US Department of Transportation • DOT........................: Maintenance Significant Item of the MRBR • MSI.............number: Structural Significant Item of the MRBR • SSI..............number: Cross Reference to MS task • MS .............number: Service Information. Indicates if source of task is experience of Lufthansa Technik (LHT) or a customer request. • SI ...........................:
2.8
THRESHOLD / INTERVAL Column
It shows the maximum allowed interval for each task to be performed. This interval is preceded by the letter "I:". Should the task become effective only after expiration of a certain limit, this limit appears (as a THRESHOLD) preceded by the letter "T:". The units in which intervals/ thresholds are expressed are as follows:
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 4 of 6
HHI
• • • • • • • • • • •
MAINTENANCE SCHEDULE
FLH CYC OPM OSM STM C CR IL D EC AC
2.9
737-6/-7/-8
flight hours flight cycles Operational Month Operational & Storage Month Storage Month C-check Cabin Refurbishment Intermediate Layover D-Check Engine Change APU Change
TASK Column
The task code indicated in this column gives a definition of the required task. Task Codes in accordance with JAA Form One are used as follows: Inspection / Test • F Overhaul • O Discard • Y
2.10 EFFECTIVITY Column It describes the Airline, or Aircraft model, or Engine type, or specific individual a/c to which the concerned task applies. "ALL" appears when the task applies to all aircraft.
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 5 of 6
HHI
MAINTENANCE SCHEDULE
737-6/-7/-8
2.11 BY Column (not used) 2.12 REP Column Information for LHT internal purposes only.
2.13 LEV Column It shows, for each time, the revision level of this item (00 for the first issue, 01 to 99 for revisions).
2.14 ITEM REVISION DATE Column It shows, for each item, the last revision date of this item. This date is always lower or equal to the date of revision of the whole Maintenance Schedule.
Date: 23-Jul-2008
EXPLANATION COMPONENT MAINTENANCE SECTION
Page: 6 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM CM - 21
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COMPONENT MAINTENANCE SECTION AIR CONDITIONING
R CM2132 00000 FUNCTIONAL CHECK OF THE POSITIVE PRESSURE RELIEF VALVES AND 000 REPLACEMENT OF THE POSITIVE PRESSURE RELIEF VALVE FILTERS
emp
MPD MPD MRB MRB
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
21-070-00 21-080-00 MSI 21-070-00 RTE:9 MSI 21-080-00 RTE:9 I: 10000 FLH
ITEMS
ATA: CM - 21
O
HHI 737-700
2 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 23
DESCRIPTION
ZONE ACCESS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
COMMUNICATIONS
R CM2324 00000 EMERGENCY LOCATOR TRANSMITTER (AUTOMATIC/FIXED). P/N 453-5004 NOTE( J ) R TASK TO INCLUDE BATTERY REPLACEMENT.
000
R CM2371 00010 UNDERWATER LOCATOR BEACON 000 P/N "ALL" NOTE( M, I ) R NOTE:(I) INTERVAL LIMIT TO BE CALCULATED FROM BATTERY FABRICATION DATE. NOTE: (M) TASK TO INCLUDE BATTERY REPLACEMENT.
Date: 23-jul-08
STRUCTURE
emp
emp
ITEMS
MRB
MSI 23-110-00 RTE:8
AMM
23-24-00-900-801-001 I: 60 OSM
MRB
MSI 23-070-00 RTE:9
MS
237121 00000
I: 72 OSM
ATA: CM - 23
Y F
HHI 737-700 only: D-AHIC
2 23-jul-08
O
HHI 737-700
3 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 24
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
ELECTRICAL POWER
CM2430 00010 BATTERY, MAIN AND AUXILIARY P/N "ALL"
000
emp
MRB MRB
MSI 24-090-00 RTE:8 MSI 24-120-00 RTE:8 I: 2000 FLH
Date: 23-jul-08
TSK
ITEMS
ATA: CM - 24
O
HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 25
DESCRIPTION
ZONE ACCESS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
EQUIPMENT/ FURNISHING
R CM2560 00020 LIFE VEST CREW P/N 63600-505 NOTE( E ) R VACUUM SEALED LIFE VESTS
000
R CM2560 00021 LIFE VEST CREW P/N 63600-505 NOTE( E ) R NON-VACUUM SEALED LIFE VESTS
000
R CM2560 00030 LIFE VEST ADULT/CHILD ADULT: P/N 63600-105 P/N 0723E105P CHILD: P/N 216200-0 R P/N 208511-1 NOTE( E ) VACUUM SEALED LIFE VESTS
000
R CM2560 00031 LIFE VEST ADULT/CHILD ADULT: P/N 63600-105 P/N 0723E105P R CHILD: P/N 21600-0 P/N 208511-1 NOTE( E ) NON-VACUUM SEALED LIFE VESTS
000
CM2564 00020 EMERGENCY LOCATOR TRANSMITTER (PORTABLE) P/N 1151324-1 NOTE( J ) TASK TO INCLUDE BATTERY REPLACEMENT
000
CM2564 00090 SMOKE HOODS P/N "ALL" NOTE( I ) VENDOR RECOMMENDATION
000
Date: 23-jul-08
STRUCTURE
emp
emp
emp
emp
emp
emp
ITEMS
MRB
MRB
MPD MRB
MRB
MSI 25-290-00 RTE:8 I: 120 OSM I: 1 s.N
O
HHI 737-700
3 23-jul-08
I: 1 s.N I: 60 OSM
O
HHI 737-700
1 23-jul-08
I: 120 OSM I: 1 s.N
O
HHI 737-700
3 23-jul-08
I: 60 OSM I: 1 s.N
O
HHI 737-700
1 23-jul-08
I: 60 OSM
F
HHI 737-700
5 18-mar-05
I: 120 OSM
Y
HHI 737-700
0 25-apr-06
MSI 25-290-00 RTE:8
25-290-00 MSI 25-290-00 RTE:8
MSI 25-290-00 RTE:8
MRB
MSI 25-350-00 RTE:8
CMM
25-60-10
MPD MRB
25-410-00 MSI 25-410-00 RTE:8
ATA: CM - 25
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS
R CM2566 00010 ESCAPE SLIDE 1L/R 000 P/N "ALL" NOTE( I ) INFLATABLES FIFTEEN YEARS AND OLDER SHOULD BE INSPECTED AT 12 MTH INTERVAL (BFG SNL 25-163 OF NOV 12/99).
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MRB MPD MRB MRB MRB
emp
MPD MRB MRB MRB
CM2566 00030 RESERVOIR AND VALVE ASSY, ESCAPE SLIDE 1 L/R, 3L/R P/N "ALL"
CM2566 00040 RESERVOIR ASSY, ESCAPE SLIDE 1 L/R, 3L/R P/N "ALL" NOTE( I ) LIFE LIMIT 180 MTH REQUIRED BY DOT
Date: 23-jul-08
000
000
emp
emp
ITEMS
MPD MRB
AAR
EFF
R L ITEM BY E E REVISION P V DATE
25-260-00 25-270-00 25-280-00 MSI 25-280-00 RTE:8 25-240-00 MSI 25-240-00 RTE:8 MSI 25-260-00 RTE:8 MSI 25-270-00 RTE:8
R CM2566 00020 ESCAPE SLIDE 3L/R 000 P/N "ALL" NOTE( I ) INFLATABLES FIFTEEN YEARS AND OLDER SHOULD BE INSPECTED AT 12 MTH INTERVAL (BFG SNL 25-163 OF NOV 12/99)
TSK
I: 36 OSM
O
HHI 737-700
2 23-jul-08
I: 36 OSM
O
HHI 737-700
1 03-jun-04
I: 36 OSM
O
HHI 737-700
3 22-mar-07
I: 180 OSM
Y
HHI 737-700
1 26-jun-02
25-240-00 MSI 25-240-00 RTE:8 MSI 25-260-00 RTE:8 MSI 25-270-00 RTE:8
25-240-00 MSI 25-240-00 RTE:8
DOT
ATA: CM - 25
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 26
DESCRIPTION
ZONE ACCESS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FIRE PROTECTION
CM2600 00010 LOWER CARGO COMPARTMENT FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MTH SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH. ACCESS REMOVAL OF AIR CONDITIONING DUCTING MAY BE REQUIRED.
emp
CM2621 00010 ENGINE FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MONTHS SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH, REMOVAL FOR FUNCTIONAL TEST OF THE FIRE BOTTLE PRESSURE GAUGE AND REPLACEMENT OF THE ENGINE FIRE BOTTLE OVERPRESSURE RELIEF DISC.
emp
CM2621 00020 CARTRIDGE, ENGINE FIRE EXTINGUISHER 000 P/N "ALL" NOTE( I ) FOR CARTRIDGES MANUFACTURED PRIOR TO 07/1991 THE TOTAL LIFE IS REDUCED TO 78 MONTH.
emp
Date: 23-jul-08
STRUCTURE
MRB MRB
MRB MRB MRB MRB
ITEMS
MRB
MSI 26-351-00 MSI 26-360-00 RTE:9 I: 120 OSM
O
HHI 737-700
6 22-mar-07
I: 120 OSM
O
HHI 737-700
4 30-nov-05
I: 132 OSM
Y
HHI 737-700
1 03-jun-04
MSI 26-061-00 MSI 26-100-00 RTE:8 MSI 26-120-00 RTE:8 MSI 26-130-00 RTE:8
MSI 26-070-00 RTE:8
ATA: CM - 26
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS
CM2622 00010 APU FIRE EXTINGUISHING BOTTLE 000 P/N "ALL" NOTE( I, J ) NOTE (I): HYDROSTATIC TEST PRIOR TO ITS NEXT REFILL AFTER 60 MONTHS SINCE PREVIOUS HYDROSTATIC TEST NOTE (J): HYDROSTATIC TEST INCLUDES THE FUNCTIONAL CHECK OF THE FIRE BOTTLE PRESSURE SWITCH.
emp
CM2622 00020 CARTRIDGE, APU FIRE EXTINGUISHER 000 P/N "ALL" NOTE( I ) FOR CARTRIDGES MANUFACTURED PRIOR TO 07/1991 THE TOTAL LIFE IS REDUCED TO 78 MONTH.
emp
CM2623 00010 CARTRIDGE, CARGO FIRE EXTINGUISHER P/N "ALL"
emp
000
CM2626 00010 WATER FIRE EXTINGUISHER, PORTABLE P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST
000
CM2626 00020 HALON FIRE EXTINGUISHER 1.1KG, PORTABLE P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST.
000
Date: 23-jul-08
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MRB MRB
MRB
MRB
MRB
MRB
R L ITEM BY E E REVISION P V DATE
I: 120 OSM
O
HHI 737-700
5 30-nov-05
I: 132 OSM
Y
HHI 737-700
1 03-jun-04
I: 120 OSM
Y
HHI 737-700
2 03-jun-04
O
HHI 737-700
4 30-nov-05
O
HHI 737-700
4 30-nov-05
MSI 26-210-00 RTE:8
MSI 26-330-00 RTE:8
MSI 26-481-00
MSI 26-461-00 VENDOR I: 144 OSM RECOMMENDATION
ITEMS
EFF
MSI 26-181-0 MSI 26-260-00 RTE:8
VENDOR I: 60 OSM RECOMMENDATION emp
TSK
ATA: CM - 26
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 27
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
FLIGHT CONTROLS
CM2721 00010 RUDDER POWER CONTROL UNIT P/N 381500-1001 P/N 381500-1003 P/N S251A301-1 P/N S251A301-2 R CM2740 00020 STABILIZER TRIM ACTUATOR P/N 251A4510-6 AND ON
000
000
emp
emp
AAR
AD 99-11-05
AAR
LTA 1999-278
MRB
MSI 27-108-00 RTE:8 MSI 27-108-00 RTE:9
MRB R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
MS SB
ITEMS
274181 01000 737-27A1277 R1 SB CONTAINS THE REQUIREMENT FOR OVERHAUL
I: 24000 FLH
F
HHI 737-700
2 30-nov-05
I: 25000 FLH
O
HHI 737-700
2 23-jul-08
ATA: CM - 27
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 28
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
FUEL
CM2822 00010 BATTERY ASSY, FUEL SHUTOFF P/N "ALL"
000
emp
MRB
MSI 28-130-00 RTE:9 I: 84 OPM
Date: 23-jul-08
TSK
ITEMS
ATA: CM - 28
O
HHI 737-700
1 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 29
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
HYDRAULIC POWER
CM2900 00010 FUSE ASSY, HYDRAULIC B-SYSTEM RUDDER P/N "ALL"
R CM2900 00020 FUSE ASSY , LEADING EDGE STAND BY P/N "ALL"
000
000
emp
emp
MRB
MPD MRB
MSI 29-170-00 RTE:8
CM2900 00030 FUSE ASSY, A SYSTEM BRAKE P/N "ALL"
CM2911 00010 FUSE ASSY, B SYSTEM BRAKE P/N "ALL"
CM2921 00010 FUSE ASSY, EM DP - THRUST REVERSER A-SYSTEM P/N "ALL"
CM2921 00020 FUSE ASSY, STAND BY THRUST REVERSER P/N "ALL"
CM2999 00010 FUSE ASSY, NLG UP LINE P/N "ALL"
000
000
000
000
000
emp
emp
emp
emp
emp
ITEMS
MRB
MRB
MRB
MRB
MRB
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
I: 25000 FLH
F
HHI 737-700
2 23-jul-08
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
I: 25000 FLH
F
HHI 737-700
1 03-jun-04
29-290-00 MSI 29-290-00 RTE:8
R
Date: 23-jul-08
TSK
MSI 29-160-00 RTE:8
MSI 29-150-00 RTE:8
MSI 29-130-00 RTE:8
MSI 29-300-00 RTE:8
MSI 29-120-00 RTE:8
ATA: CM - 29
Page 1 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM2999 00020 FUSE ASSY, NLG DOWN LINE P/N "ALL"
R CM2999 00030 FUSE ASSY, LEADING EDGE B-SYSTEM P/N "ALL"
ZONE ACCESS 000
000
STRUCTURE
emp
emp
R
Date: 23-jul-08
ITEMS
THRESHOLD INTERVAL
REFERENCES MRB
MPD MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MSI 29-110-00 RTE:8 I: 25000 FLH
F
HHI 737-700
0 03-jun-04
I: 25000 FLH
F
HHI 737-700
1 23-jul-08
29-140-00 MSI 29-140-00 RTE:8
ATA: CM - 29
Page 2 of 2
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 31
DESCRIPTION
ZONE ACCESS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
INSTRUMENTS
CM3131 00010 UNDERWATER LOCATOR BEACON 000 P/N "ALL" NOTE( I, J ) NOTE (I): INTERVAL LIMIT ARE TO BE COMPUTED FROM BATTERY FABRICATION DATE. NOTE (J): TASK TO INCLUDE BATTERY REPLACEMENT.
Date: 23-jul-08
STRUCTURE
emp
MPD MPD MRB MRB MS
ITEMS
31-140-00 31-150-00 MSI 31-140-00 RTE:9 MSI 31-150-00 RTE:9 313109 70000
I: 72 OSM
ATA: CM - 31
O
HHI 737-700
2 03-jun-04
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 32
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
LANDING GEAR
R CM3211 00010 MAIN LANDING GEAR MAIN LANDING GEAR ASSY LH/RH P/N "ALL"
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
R CM3211 00020 MAIN LANDING GEAR STRUT ASSY - SIDE LH / RH P/N "ALL"
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
R
Date: 23-jul-08
TSK
ITEMS
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
ATA: CM - 32
Page 1 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
R CM3211 00030 MAIN LANDING GEAR STRUT ASSY - UPPER AND LOWER P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
R
Date: 23-jul-08
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
R CM3211 00040 MAIN LANDING GEAR LINK ASSY - UPPER LH / RH P/N "ALL"
TSK
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
3 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
ATA: CM - 32
Page 2 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
R CM3211 00050 MAIN LANDING GEAR LINK ASSY - LOWER P/N "ALL"
DESCRIPTION
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
R
Date: 23-jul-08
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
R CM3211 00060 MAIN LANDING GEAR LINK ASSY - REACTION P/N "ALL"
TSK
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
ATA: CM - 32
Page 3 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
R CM3211 00070 MAIN LANDING GEAR LINK ASSY - HANGER P/N "ALL"
DESCRIPTION
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
R
Date: 23-jul-08
ITEMS
EFF
R L ITEM BY E E REVISION P V DATE
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
R CM3211 00080 MAIN LANDING GEAR LINK ASSY - RETRACTION P/N "ALL"
TSK
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
ATA: CM - 32
Page 4 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
R CM3211 00090 MAIN LANDING GEAR BEAM ASSY - WALK. P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES MPD MPD MPD MPD MRB MRB MRB MRB
000
emp
MPD MPD MPD MPD MRB MRB MRB MRB
000
emp
CMR
000
emp
CMR
ITEMS
O
HHI 737-700
2 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
O
HHI 737-700
2 23-jul-08
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
I: 18000 CYC I: 120 OPM I: 21000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 03000 MLG INNER CYLINDER ASSY-SHOCK STRUT P/N "ALL"
R L ITEM BY E E REVISION P V DATE
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
CM3211 02000 MLG OUTER CYLINDER ASSY-SHOCK STRUT P/N "ALL"
EFF
32-040-01 32-040-02 32-720-01 32-720-02 MSI 32-040-01 RTE:8 MSI 32-040-02 RTE:8 MSI 32-720-01 MSI 32-720-02
R
R CM3211 00100 MAIN LANDING GEAR HOUSING ASSY P/N "ALL"
TSK
ATA: CM - 32
Page 5 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 04000 MLG PIN - AXLE RETENTION P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 10000 MLG PIN - LWR TORSION LINK, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 09000 MLG PIN - UPPER TORSION LINK, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 08000 MLG PIN - TORSION LINK APEX, P/N "ALL"
I: 45000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 07000 MLG LOWER TORSION LINK ASSY, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 06000 MLG UPPER TORSION LINK ASSY, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 05000 MLG AXLE ASSY, P/N "ALL"
TSK
ATA: CM - 32
Page 6 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 11000 MLG NUT - TORSION LINK APEX, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 17000 MLG NUT - DAMPER, TORSION LINK APEX, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 16000 MLG PIN - DAMPER, TORSION LINK APEX, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 15000 MLG PIN ASSY - AFT TRUNNION BEARING, P/N "ALL"
I: 45000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 14000 MLG PIN - AFT TRUNNION CROSSBOLT, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 13000 MLG PIN - FWD TRUNNION CROSSBOLT, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 12000 MLG PIN ASSY - FWD TRUNNION BEARING, P/N "ALL"
TSK
ATA: CM - 32
Page 7 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 18000 MLG UPPER SIDE STRUT ASSY, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 24000 MLG PIN - SIDE STRUT TO REACTION LINK, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 23000 MLG PIN - LOWER DOWN LOCK, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 22000 MLG PIN - SIDE STRUT ASSY APEX, P/N "ALL"
I: 45000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 21000 MLG UPPER LOCK LINK ASSY, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 20000 MLG LOWER DOWN LOCK LINK ASSY, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 19000 MLG LOWER SIDE STRUT ASSY, P/N "ALL"
TSK
ATA: CM - 32
Page 8 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 25000 MLG PIN - DOWNLOCK TO REACTION LINK, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 31000 MLG PIN - REACTION LINK TO TRUNNION, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 30000 MLG PIN - OUTER CYLINDER SIDE STRUT, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 29000 MLG PIN - SIDE OF BODY JOINT, P/N "ALL"
I: 45000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 28000 MLG PIN - OUTBOARD DOWNLOCK SPRING ASSY, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 27000 MLG PIN - DOWNLOCK ACTUATOR, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 26000 MLG PIN - DOWNLOCK APEX, P/N "ALL"
TSK
ATA: CM - 32
Page 9 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 32000 MLG REACTION LINK ASSY, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 38000 MLG PIN - LINK ASSY ATTACHMENT, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 37000 MLG PIN - WALKING BEAM ASSY, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 36000 MLG RETRACTION LINK ASSY, P/N "ALL"
I: 45000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 35000 MLG RETRACTION WALKING BEAM, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 34000 MLG PIN - HANGER LINK TO REACTION LINK, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 33000 MLG HANGER LINK ASSY, P/N "ALL"
TSK
ATA: CM - 32
Page 10 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3211 39000 MLG PIN - RETRACT ACTUATOR ATTACHMENT, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
MPD MPD MRB MRB
CM3221 00020 NOSE LANDING GEAR STRUT ASSY LOWER P/N "ALL"
000
emp
MPD MPD MRB MRB
CM3221 00030 NOSE LANDING GEAR LINK ASSY LOCK P/N "ALL"
000
emp
MPD MPD MRB MRB
CM3221 01040 AFT LOCK LINK P/N 162A2115-2 (NEXT HIGHER ASSY P/N 162A2115-3)
Date: 23-jul-08
000
emp
ITEMS
AAR
R L ITEM BY E E REVISION P V DATE
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 45000 CYC
Y
HHI 737-700
0 17-oct-02
I: 18000 CYC I: 120 OPM
O
HHI 737-700
1 03-jun-04
I: 18000 CYC I: 120 OPM
O
HHI 737-700
1 03-jun-04
I: 18000 CYC I: 120 OPM
O
HHI 737-700
1 03-jun-04
I: 4200 CYC
Y
HHI 737-700
1 12-jun-01
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3221 00010 NOSE LANDING GEAR NOSE GEAR COMPONENT P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 161A0002
CM3211 40000 MLG PIN - WALKING BEAM ATTACHMENT, P/N "ALL"
TSK
32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00
32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00
32-090-00 32-750-00 MSI 32-090-00 RTE:8 MSI 32-750-00
CMR MPD PAGE 9.0-50
ATA: CM - 32
Page 11 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3221 02000 NLG PIN - LEFT TRUNNION, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 08000 NLG UPPER TORSION LINK ASSY, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 07000 NLG PIN - TORSION LINK APEX, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 06000 NLG PIN - UPPER AND LOWER TORSION LINK, P/N "ALL"
I: 75000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 05000 NLG INNER CYLINDER, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 04000 NLG OUTER CYLINDER, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 03000 NLG PIN - RIGHT TRUNNION, P/N "ALL"
TSK
ATA: CM - 32
Page 12 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3221 09000 NLG LOWER TORSION LINK ASSY, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
ITEMS
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
Date: 23-jul-08
0 17-oct-02
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 15000 NLG LOWER DRAG STRUT, P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 14000 NLG UPPER DRAG STRUT, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 13000 NLG STEERING PLATE, P/N "ALL"
I: 75000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 12000 NLG PIN STRG COLLAR ATTACH, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 11000 NLG STEERING SLEEVE, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 10000 NLG STEERING COLLAR, P/N "ALL"
TSK
ATA: CM - 32
Page 13 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3221 16000 NLG FWD LOCK LINK, P/N "ALL"
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
000
emp
CMR
Date: 23-jul-08
000
emp
ITEMS
MRB
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
1 03-jun-04
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 75000 CYC
Y
HHI 737-700
0 17-oct-02
I: 25000 FLH
F
HHI 737-700
1 22-mar-07
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3232 00010 MLG WHEEL WELL PROTECTION FUSE P/N "ALL"
HHI 737-700
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 21000 NLG PIN - DRAG STRUT ASSY, P/N "ALL"
Y
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 20000 NLG PIN - DRAG STRUT TRUNNION, P/N "ALL"
I: 75000 CYC
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 19000 NLG PIN - LOCK LINK APEX, P/N "ALL"
R L ITEM BY E E REVISION P V DATE
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 18000 NLG LOCK LINK SHAFT, P/N "ALL"
EFF
STRUCTURAL SAFE LIFE PARTS DRW 162A0002
CM3221 17000 NLG AFT LOCK LINK, P/N "ALL EXCEPT 162A2115-2
TSK
MSI 32-230-00 RTE:6
ATA: CM - 32
Page 14 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM3241 00020 WHEEL MAIN LANDING GEAR P/N "ALL" NOTE( I ) OVERHAUL AT EACH TIRECHANGE
CM3241 00030 WHEEL NOSE LANDING GEAR P/N "ALL" NOTE( I ) OVERHAUL AT EACH TIRECHANGE
Date: 23-jul-08
ZONE ACCESS 000
STRUCTURE
emp
MRB MRB
000
emp
ITEMS
THRESHOLD INTERVAL
REFERENCES
MRB
TSK
EFF
R L ITEM BY E E REVISION P V DATE
MSI 32-380-01 RTE:9 MSI 32-380-02 RTE:9 I: 1 s.N
O
HHI 737-700
1 03-jun-04
I: 1 s.N
O
HHI 737-700
1 03-jun-04
MSI 32-380-00 RTE:9
ATA: CM - 32
Page 15 of 15
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 33
DESCRIPTION
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AIRCRAFT LIGHTING SYSTEM
R CM3351 00010 BATTERY PACK, EMERGENCY LIGHTS P/N AD-D717-01-100 P/N D 717-01-100 R
Date: 23-jul-08
ZONE ACCESS
000
emp
MRB
MSI 33-060-00 RTE:8 I: 24 OPM
ITEMS
ATA: CM - 33
O F
HHI 737-700
5 23-jul-08
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 34
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
NAVIGATION
CM3410 00010 ALTIMETER, STAND-BY AND AIRSPEED P/N "ALL" N CM3453 00010 TRANSPONDER ATC, TPR-900 P/N "ALL"
000
000
emp
emp
N
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ITEMS
empty
AAR
NFL II - 23/03
AAR
FAR 91.413 PART 43, APPEND. F
AAR
NFL II - 23/03
I: 24 OSM
F
HHI 737-700
2 29-apr-03
I: 12 MTH
F
HHI 737-700
0 23-jul-08
ATA: CM - 34
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 35
DESCRIPTION
ZONE ACCESS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
OXYGEN
CM3510 00010 FF/QD MASK WITH REGULATOR P/N "ALL"
000
CM3512 00010 CYLINDER ASSY, OXYGEN, 115 CU/FT P/N "ALL" NOTE( J ) TASK TO INCLUDE HYDROSTATIC TEST
000
CM3512 01010 CYLINDER ASSY, OXYGEN, 115 CU/FT P/N "ALL" NOTE( I ) LIFE LIMIT 288 MTH REQUIRED BY DOT
000
CM3522 00110 GENERATOR, OXYGEN P/N "ALL"
000
R CM3531 00010 RESTORE PORTABLE OXYGEN CYLINDER ASSY P/N "ALL" NOTE( J ) R TASK TO INCLUDE HYDROSTATIC TEST
Date: 23-jul-08
STRUCTURE
000
emp
emp
emp
emp
emp
ITEMS
MPD MRB
AAR MRB
AAR MRB
MRB
AAR MRB
35-020-00 MSI 35-020-00 RTE:8 I: 16000 FLH
F
HHI 737-700
1 03-jun-04
I: 36 OSM
O
HHI 737-700
4 30-nov-05
I: 288 OSM
Y
HHI 737-700
1 03-jun-04
I: 144 OSM
Y
HHI 737-700
1 03-jun-04
I: 60 OSM
O
HHI 737-700
4 23-jul-08
49 CFR § 180.205 MSI 35-031-00
DOT MSI 35-040-00 RTE:8
MSI 35-070-00 RTE:9
49 CFR § 180.205 MSI 35-111-00
ATA: CM - 35
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 36
DESCRIPTION
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
PNEUMATIC
CM3610 00010 FUNCTIONALLY CHECK THE RIGHT AND LEFT PRECOOLER VALVE SENSOR. P/N "ALL"
CM3610 00020 FUNCTIONALLY CHECK THE PRECOOLER CONTROL VALVE AND SOLENOID P/N "ALL"
Date: 23-jul-08
ZONE ACCESS
000
emp
MRB MRB
000
emp
MRB MRB
ITEMS
MSI 36-030-01 RTE:8 MSI 36-030-02 RTE:8 I: 16000 FLH
F
HHI 737-700
2 18-mar-05
I: 16000 FLH
F
HHI 737-700
2 03-jun-04
MSI 36-020-01 RTE:8 MSI 36-020-02 RTE:8
ATA: CM - 36
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 49
DESCRIPTION
ZONE ACCESS
STRUCTURE
TSK
EFF
R L ITEM BY E E REVISION P V DATE
AUXILIARY POWER
R CM4900 01010 ENGINE COMPRESSOR IMPELLER NOTE( I ) INTERVAL IS 30000 APU CYCLES
000
emp
MPD MRB
R R CM4900 01020 FIRST STAGE TURBINE DISK NOTE( I ) INTERVAL IS 30000 APU CYCLES
R CM4900 01030 SECOND STAGE TURBINE ROTOR NOTE( I ) INTERVAL IS 30000 APU CYCLES
000
emp
MPD MRB
000
emp
MPD MRB
emp
R
MPD MRB
HHI 737-700
4 23-jul-08
I: 1 s.N
Y
HHI 737-700
3 23-jul-08
I: 1 s.N
Y
HHI 737-700
3 23-jul-08
I: 1 s.N
Y
HHI 737-700
3 23-jul-08
49-082-00 MSI 49-082-00 RTE:7 EM 49-00-00
ITEMS
Y
49-072-00 MSI 49-072-00 RTE:7 EM 49-00-00
000
I: 1 s.N
49-062-00 MSI 49-062-00 RTE:7 EM 49-00-00
R R CM4900 01040 TURBINE SHAFT NOTE( I ) INTERVAL IS 30000 APU CYCLES
49-052-00 MSI 49-052-00 RTE:7 EM 49-00-00
R
Date: 23-jul-08
THRESHOLD INTERVAL
REFERENCES
ATA: CM - 49
Page 1 of 1
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM CM - 72
DESCRIPTION
ZONE ACCESS
STRUCTURE
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
ENGINE
R CM7200 20010 CFM56-7B22 & B24 FAN ROTOR PARTS FAN DISK P/N 340-000-410-0 NOTE( )
000
emp
AAR MRB MRB
ESM 05-11-01 MSI 72-030-01 RTE:5 MSI 72-030-02 RTE:5
R CM7200 20020 CFM56-7B22 & B24 FAN ROTOR PARTS BOOSTER SPOOL P/N 340-000-816-0
CM7200 20030 CFM56-7B22 & B24 FAN ROTOR PARTS FAN SHAFT P/N 335-006-414-0
CM7200 20040 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS FORWARD SHAFT P/N 1386M56P03
Date: 23-jul-08
TSK
000
emp
AAR MRB MRB
000
emp
AAR MRB MRB
000
emp
AAR MRB MRB
ITEMS
I: 1 s.N I: 17900 CYC
Y
HHI 737-700
4 23-jul-08
I: 23600 CYC
Y
HHI 737-700
3 22-mar-07
I: 30000 CYC
Y
HHI 737-700
3 22-mar-07
I: 20000 CYC
Y
HHI 737-700
2 18-mar-05
ESM 05-11-01 MSI 72-040-01 RTE:5 MSI 72-040-02 RTE:5
ESM 05-11-01 MSI 72-050-01 RTE:5 MSI 72-050-02 RTE:5
ESM 05-11-02 MSI 72-160-01 RTE:5 MSI 72-160-02 RTE:5
ATA: CM - 72
Page 1 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM7200 20050 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 1 - 2 SPOOL P/N 1558M31G04
ZONE ACCESS 000
STRUCTURE
emp
AAR MRB MRB
CM7200 20051 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 1-2 SPOOL P/N 1558M31G07
000
R CM7200 20060 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 3 DISK P/N 1590M59P01 P/N 2116M23P01
000
emp
emp
THRESHOLD INTERVAL
REFERENCES
emp
CMM
05-11-02
AAR MRB
ESM 05-11-02 MSI 72-140-01 RTE:5 MSI 72-140-02 RTE:5
AAR MRB MRB
Date: 23-jul-08
000
emp
AAR MRB MRB
ITEMS
I: 20000 CYC
Y
HHI 737-700
3 22-mar-07
I: 20000 CYC
Y
HHI 737-700
0 22-mar-07
I: 20000 CYC
Y
HHI 737-700
3 23-jul-08
I: 20000 CYC
Y
HHI 737-700
4 23-jul-08
I: 1 s.N I: 20000 CYC
Y
HHI 737-700
5 23-jul-08
ESM 05-11-02 MSI 72-150-01 RTE:5 MSI 72-150-02 RTE:5
R R CM7200 20080 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS COMP REAR (CDP) AIR SEAL P/N 1523M35P01 P/N 2116M25P01 NOTE( ) R
R L ITEM BY E E REVISION P V DATE
empty
MRB
000
EFF
ESM 05-11-02 MSI 72-130-01 RTE:5 MSI 72-130-02 RTE:5
R R CM7200 20070 CFM56-7B22 & B24 COMPRESSOR ROTOR PARTS STAGE 4 - 9 SPOOL P/N 1588M89G03 P/N 2048M20G03
TSK
ESM 05-11-02 MSI 72-170-01 RTE:5 MSI 72-170-02 RTE:5
ATA: CM - 72
Page 2 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
R CM7200 20090 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS FRONT SHAFT P/N 1873M73P01 P/N 2048M21P03
ZONE ACCESS 000
STRUCTURE
emp
THRESHOLD INTERVAL
REFERENCES AAR MRB MRB
000
emp
AAR MRB MRB
000
R CM7200 20120 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS REAR SHAFT P/N 1498M45P06 P/N 1498M90P04 NOTE( ) R
000
Date: 23-jul-08
emp
AAR MRB MRB
emp
AAR MRB MRB
ITEMS
R L ITEM BY E E REVISION P V DATE
I: 20000 CYC
Y
HHI 737-700
4 23-jul-08
I: 20000 CYC
Y
HHI 737-700
4 23-jul-08
I: 1 s.N I: 20000 CYC
Y
HHI 737-700
5 23-jul-08
I: 1 s.N I: 20000 CYC
Y
HHI 737-700
4 23-jul-08
ESM 05-11-03 MSI 72-230-01 RTE:5 MSI 72-230-02 RTE:5
R R CM7200 20110 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS DISK P/N 1498M43P04 P/N 1498M43P06 P/N 1498M43P07 R NOTE( )
EFF
ESM 05-11-03 MSI 72-220-01 RTE:5 MSI 72-220-02 RTE:5
R R CM7200 20100 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS FRONT AIR SEAL P/N 1795M36P02 P/N 2116M20P02
TSK
ESM 05-11-03 MSI 72-240-01 RTE:5 MSI 72-240-02 RTE:5
ESM 05-11-03 MSI 72-250-01 RTE:5 MSI 72-250-02 RTE:5
ATA: CM - 72
Page 3 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
CM7200 20130 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 1 DISK P/N 336-001-804-0
CM7200 20140 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 2 DISK P/N 336-001-909-0
CM7200 20150 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 3 DISK P/N 336-002-006-0
CM7200 20160 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS STAGE 4 DISK P/N 336-002-105-0
Date: 23-jul-08
ZONE ACCESS 000
STRUCTURE
emp
AAR MRB MRB
000
emp
AAR MRB MRB
000
emp
AAR MRB MRB
000
emp
AAR MRB MRB
ITEMS
THRESHOLD INTERVAL
REFERENCES
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5 I: 25000 CYC
Y
HHI 737-700
2 18-mar-05
I: 25000 CYC
Y
HHI 737-700
2 18-mar-05
I: 25000 CYC
Y
HHI 737-700
2 18-mar-05
I: 25000 CYC
Y
HHI 737-700
2 18-mar-05
ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5
ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5
ESM 05-11-04 MSI 72-290-01 RTE:5 MSI 72-290-02 RTE:5
ATA: CM - 72
Page 4 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
ZONE ACCESS
CM7200 20170 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS LPT SHAFT P/N 340-074-705-0 P/N 340-074-720-0 P/N 340-074-722-0
000
CM7200 20180 CFM56-7B22 & B24 LOW PRESSURE TURBINE (LPT) ROTOR PARTS LPT ROTOR SUPPORT P/N 338-077-502-0
000
emp
emp
AAR MRB
AAR MRB MRB
000
R CM7200 20210 CFM56-7B22 LOW PRESSURE TURBINE (LPT) STATOR PARTS R LPT REAR FRAME P/N 340-027-115-0 P/N 340-027-121-0
000
R CM7200 20230 CFM56-7B LOW PRESSURE TURBINE (LPT) STATOR PARTS LPT REAR FRAME P/N 340-166-205-0 P/N 340-166-206-0 R P/N 340-166-207-0 P/N 340-166-208-0 P/N 340-166-209-0 P/N 340-166-210-0
000
emp
emp
emp
ITEMS
THRESHOLD INTERVAL
REFERENCES
MRB
CM7200 20200 CFM56-7B22 LOW PRESSURE TURBINE (LPT) STATOR PARTS LPT REAR FRAME P/N 340-027-113-0
Date: 23-jul-08
STRUCTURE
AAR
AAR
TSK
EFF
R L ITEM BY E E REVISION P V DATE
ESM 05-11-04 MSI 72-280-01 RTE:5 MSI 72-280-02 RTE:5 I: 20000 CYC
Y
HHI 737-700
3 22-mar-07
I: 25000 CYC
Y
HHI 737-700
2 18-mar-05
I: 25000 CYC
Y
HHI 737-700
0 11-jan-01
I: 24200 CYC
Y
HHI 737-700
2 23-jul-08
T: 25000 CYC I: 4700 CYC
Y
HHI 737-700
1 23-jul-08
ESM 05-11-04 MSI 72-270-01 RTE:5 MSI 72-270-02 RTE:5
ESM 05-12-04
ESM 05-12-04
AAR AAR AAR AAR
2008-03-09 EAD 2007-0104 ESM 05-12-04 05-12-04
SB
72-0579
ATA: CM - 72
Page 5 of 6
HHI R E V
737-6
MAINTENANCE SCHEDULE ITEM
DESCRIPTION
N CM7200 20240 CFM56-7B22 & B24 HIGH PRESSURE TURBINE (HPT) ROTOR PARTS REAR SHAFT P/N 1498M45P07
ZONE ACCESS 000
STRUCTURE
emp
Date: 23-jul-08
AAR MRB MRB
N
THRESHOLD INTERVAL
REFERENCES
EFF
R L ITEM BY E E REVISION P V DATE
ESM 05-11-03 MSI 72-250-01 RTE:5 MSI 72-250-02 RTE:5 I: 11500 CYC
ITEMS
TSK
ATA: CM - 72
Y
HHI 737-700
0 23-jul-08
Page 6 of 6