MEL

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

TABLE OF CONTENTS ATA SYS NO. SYSTEM -Record of revisions -Bulletin control -List of effective pages -Table of contents -Applicability list -Preamble -Definitions 21 Air Conditioning 22 Autopilot 23 Communications 24 Electrical Power 25 Equipment/Furnishings 26 Fire Protection 27 Flight Controls 28 Fuel 29 Hydraulic Power 30 Ice and Rain Protection 31 Indicating/Recording Systems 32 Landing Gear 33 Lights 34 Navigation 35 Oxygen 37 Vacuum/Pressure 46 Information Systems 52 Doors 61 Propellers 71 Power Plant 73 Engine Fuel & Control 74 Ignition 77 Engine Indicating 80 Starting 82 Water Injection MAINTENANCE & OPERATOINS PROCEDURES

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PAGE RR-1 CB-1 LEP-1 CONT-1 APL-1 PRE-1 thru PRE-2 DEF-1 thru DEF-4 21-1 thru 21-2 22-1 23-1 thru 23-2 24-1 thru 24-2 25-1 thru 25-3 26-1 27-1 28-1 29-1 30-1 thru 30-2 31-1 32-1 33-1 thru 33-2 34-1 thru 34-8 35-1 37-1 46-1 52-1 thru 52-2 61-1 71-1 73-1 74-1 77-1 80-1 82-1 MO-1 thru MO-8

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 APPLICABILITY LIST This MANUAL contains the FAIRCHILD SA-226 & SA-227 Minimum Equipment List (MEL) under which the Aeronaves TSM, S.A. de C.V., FAIRCHILD SA-226 & SA227 Airplane must be operated and was developed from the F.A.A. SA-226 & SA-227 Master Minimum Equipment List through revision 16A dated 01/25/2010 approved by the F.A.A. The Fairchild Airplane that Aeronaves TSM, S.A. de C.V., operates is model SA-226 and SA-227 and the present MANUAL is only for the use in the following airplanes.

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MANUFACTURER

MODEL

FAIRCHILD

SA-226

FAIRCHILD

SA-227

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 PREAMBLE The following is applicable for authorized certificate holders operating under DGAC regulations. The DGAC regulations require that equipment installed on an aircraft in compliance with the Airworthiness and the Operating Rules must be operative. However, the rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has show that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. This MEL is developed from a Master Minimum Equipment List (MMEL) developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The Aeronaves TSM, S.A. de C.V., MEL is not less restrictive that the MMEL and does not differ in format form level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders.

Equipment not required by the operation being conducted and equipment in excess of DGAC requirements are included in the MEL with appropriate conditions and limitations. This MEL does not deviate form the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed in this MEL must be operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in this MEL to ensure that an acceptable level of safety is maintained.

This MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability this MEL establishes limitations on the duration of and conditions for operation with inoperative equipment. This MEL provide for release of the aircraft for light with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported but marking an entry in the Aircraft Maintenance Logbook as prescribed by DGAC and Aeronaves TSM, S.A de .C.V, procedures. The item is then either repaired or may be deferred per this MEL. MEL conditions and limitations do not relieve the Captain and Maintenance personnel form determining that the aircraft is in condition for safe operation with items of equipment inoperative.

When these requirements are met, an Airworthiness Release, Maintenance Aircraft Logbook entry is issued as prescribed by DGAC and Aeronaves TSM, S.A. de C.V., procedures. Such documentation is required prior to operation with an item of equipment inoperative.

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 Preamble (Cont.)

Aeronaves TSM, S.A. de C.V., is responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the affect on aircraft operation and crew workload will be considered. All this evaluation is made by the Captain in charge and Maintenance personnel.

Aeronaves TSM, S.A. de C.V., has established in their General Maintenance Manual, a controlled and sound repair program including the parts, personnel, facilities, procedures and schedules to ensure timely repair.

“WHEN USING THIS MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THIS MEL IS REQUIRED”

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 DEFINITIONS 1. System Definitions System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially. a. “Item” (Column 1) Means the equipment, system, component, or function listed in the “Item” column. b. “Number Installed” (Column 2) Is the number (quantity) of items normally installed in the aircraft? These numbers represent the aircraft configuration considered in developing this MEL, Should the number be a variable (e.g., passenger cabin items) number is not required c. “Number Required for Dispatch” (Column 3) Is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met. d. “Remarks or Exceptions” (Column 4) In this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate note. e. A vertical bar (change bar) In the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page 2. “Airplane Flight Manual” (AFM) Is the document required for type certification and approved by the responsible FAA Aircraft Certification and DGAC office.

3. “As required by DGAC” means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules.

The number of items required by DGAC must be operative. When the listed item is not required by DGAC to may be inoperative for time specified by repair category (Continued) Revision: Reedición

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment.

Note - To the extent practical, placards should be located adjacent to the control or indicator for the item affected however, unless otherwise specified, placard wording and location will be determined by Maintenance personnel.

5. Not Applicable 6. “Deleted” in the remark column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

7. Not Applicable 8. “DIRECCION GENERAL DE AERONAUTICA CIVIL” (DGAC) means the aplicable portions of SECRETARIA DE COMUNICACIONES Y TRANSPORTES Regulations.

9. “Flight Day” means a 24 hours period (from midnight to midnight) either Universal Coordinated Time (UTC) or local time, as established by the Aeronaves TSM, S.A. de C.V., during which at least one flight is initiated for the affected aircraft.

10. “Icing Conditions” means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s) 11. Alphabetical symbol in columns 4 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

12. “Inoperative” means a system and/or components malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit (s) or tolerance (s).

13. “Notes” in column 4 provides additional information for crewmember or maintenance consideration. Notes are used to compliance, but no not relieve the operator of the responsibility for compliance with all applicable requirements. Note are not a part of the provisos 14. Inoperative components of an inoperative system: Inoperative items, which are components of a system, which is inoperative, are usually considered components directly associated with and having no other function than to support that system.

(Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MEL).

(Continued)

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 15. “(M)” symbol indicates a requirement for a specific maintenance procedure, which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions (See Aeronaves TSM, S.A. de C.V., General Maintenance Manual). Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the Aeronaves TSM, S.A. de C.V., maintenance. Appropriate procedures among with the operating procedures are published as part of the Aeronaves TSM, S.A. de C.V., General Maintenance Manual or MEL. 16. “(O)” symbol indicates a requirement for a specific operations procedure, which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the Aeronaves TSM, S.A. de C.V.; appropriate procedures are required to be published as a part of the Aeronaves TSM, S.A. de C.V. Appropriate procedures are required to be published as part of the MEL. 17. “Deactivated” and “Secured” means that the specified component must be pun into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by Aeronaves TSM, S.A. de C.V. 18. “Visual Flight Rules” VFR is as defined in the Ley de Aviación Civil.

19. “Visual meteorological Conditions” (VMC) means the atmospheric environment is such would allow a flight to proceed under the visual flight rules applicable to the flight.

20. “Visible Moisture” means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

21. “Passenger Convenience Item” means those items related to passenger convenience, comfort or entertainment such as, but not limit to, galley equipment, movie equipment, ashtrays, stereo equipment, overhead reading lamps, etc.

22. Repair Intervals: All users of an MEL approved by D.G.A.C, must affected repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators.

Category A. Items in this category shall be repaired within the item interval specified in the remark column of the Aeronaves TSM, S.A. de C.V., approved MEL. (Continued)

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 Repair interval (Cont) Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the mal the malfunction was recorded in the aircraft maintenance record/logbook For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29tn Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the mal the malfunction was recorded in the aircraft maintenance record/logbook For example, if it were recorded at 10 a.m. on January 26th, the three day interval would begin at midnight the 26th and end at midnight February 5Th. Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours); excluding the mal the malfunction was recorded in the aircraft maintenance log and/or record.

The letter designators are inserted adjacent to Column 2 23.

Not applicable

24.

Not applicable

25.

“Not Installed” means an item that is included in the MMEL but is not installed in the Aeronaves TSM, S.A. de C.V., airplane FAIRCHILD SA226 & SA227

26.

“Not applicable” means an item that is included in the MMEL but is not applicable for FAIRCHILD SA226 & SA227

27.

“Day of Discovery” is the calendar day an equipment/instruments malfunction recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MEL for the repair of an inoperative item of equipment. This provision is applicable to all MEL item, i.e. categories “A, B, C, and D”.

Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

21 AIR CONDITIONING 1. Cabin Altitude Warning System.

2. Cabin Altitude/Differential Pressure Indicator.

A) ALTITUDE Indication.

C

1

0 (O) May be inoperative for unpressurized flight, (AFM. III 8-9)

C

1

0 May be inoperative for pressurized flight below 10,000 feet MSL.

C

1

0 (O) May be inoperative for unpressurized flight, (AFM. III 8-9)

C

1

0 (O) May be inoperative provided: a) Cabin DIFFERENTIAL PRESSURE portion of the Indicator is operative, and b) A chart is provided to the crew to convert Cabin Differential Pressure to Cabin Altitude.

B) DIFFERENTIAL PRESSURE Indication.

C

1

0 (O) May be inoperative provided: a) Cabin ALTITUDE portion of the Indicator is operative, and b) A chart is provided to the crew to convert Cabin Altitude to Cabin Differential Pressure.

3 Cabin Rate Of Climb Indicator.

C

1

0

4 Flow Control Valves.

C

2

1 (M) May be inoperative in the CLOSED position provided: a) Cockpit Fresh Air Fan is operable with Gear retracted, b) Oxygen and Masks are provided for all occupants, and c) Other Air Conditioning System is operative.

5 Automatic Pressurization Controller.

Revision: Reediciรณn

C

1

0 (O) May be inoperative for unpressurized flight.

C

1

0 (O) May be inoperative for pressurized flight provided Manual Pressurization Controller is operative

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

21 AIR CONDITIONING 6 Manual Pressurization Controller.

C

1

0 (O) May be inoperative for unpressurized flight, (AFM. III 8-9)

C

1

0 (O) May be inoperative for pressurized flight provided Automatic Pressurization Controller is operative.

7 Automatic Temperature Control System.

C

1

0 Automatic System may be inoperative provided Manual System is operative.

8 Manual Temperature Control System.

C

1

0 Manual System may be inoperative provided Automatic System is operative.

9 Air Conditioning System.

C

2

1 (O) One may be inoperative provided: a) Cockpit Fresh Air Fan is operable with Landing Gear retracted, b) Oxygen and Masks are provided for all occupants, as required by DGAC, and c) The other Flow Control Valve and Air Conditioning System are operative.

10 Cabin Dump Valve.

C

1

0 (O) May be inoperative provided the Cabin Dump Valve is secured in OPEN position and aircraft remains VMC. NOTE: Alternate Static System will be unusable.

11 Windshield De-Fog Fan.

C

1

0

12 Supplemental Air Conditioning System.

Not Applicable

13 Cabin Supplemental (Auxiliary) Heater.

Not Applicable

14 Cabin Temperature Indicator.

Revision: Reediciรณn

C

1

FECHA: 21 Febrero 2011

0

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

22 AUTOPILOT 1 Autopilot System.

Not Installed

2 Yaw Damper.

Not Installed

3 Autopilot Disconnect Functions (Quick Release Controls).

Not Installed

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INTENCIONALMENTE EN BLANCO

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

23 COMMUNICATIONS 1 Communications System.

A UHF.

Not Installed.

B VHF XA-ADQ, XA-ADS.

D

3

1

May be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or DC Transfer Bus (as appropriate to aircraft configuration) and not required for emergency procedures.

Two transmitters and receivers are required for IFR. One is required for VFR operations.

XA–DCX, XA–EEE, XA–EGC, XA– MIO, XA–PNG, XA-SLW, XA–TSM, XA–TYX, XA–UFO , XA-UGJ, XA– UKJ, XA–UKP, XA–UMW, XA–UNQ, XA-UOS, XA-USB, XA-USG.

D

2

1

May be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or DC Transfer Bus (as appropriate to aircraft configuration) and not required for emergency procedures.

Two transmitters and receivers are required for IFR. One is required for VFR operations.

2 Cockpit Speaker.

C

2

0

May be inoperative provided two operative Headsets are available to flight crew.

3 Audio Amplifier.

C

2

0

May be inoperative provided two operative Headsets are available to flight crew.

4 Passenger Address System (PA).

A) Passenger Configuration.

Not Applicable

B) Cargo Configuration.

D

1

0

5 Auxiliary Public Address System.

6 Cockpit Voice Recorder (CVR), XAUSG only.

Revision: 03

May be inoperative provided procedures do not require its use.

Not Applicable

A

1

0 May be inoperative provided: a) Flight Data Recorder (FDR) operates normally, and b) Repairs are made within three flight days.

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

23 COMMUNICATIONS 7 Cockpit Voice Recorder (CVR) Underwater Locating Device (ULD).

Not installed.

8 Boom Microphones.

Not installed

A) Cockpit Voice Recorder With Flight Data Recorder Installed.

Not applicable

9 Boom Mikes (Flight Data Recorder Not Required By DGAC.

COMBINED WITH ATA 23-8, REVISION 16.

10 Avionics Master Switch.

11 Radio Master Switch.

C

3

0

May be inoperative provided Both Left and Right Auxiliary Avionics Master Switches are operative.

C

1

0

May be inoperative provided Both Left and Right Auxiliary Avionics Master Switches are operative.

C

1

0

May be inoperative provided the Emergency Radio Master Switches are operative.

12 Prerecorded Passenger Announcement System.

Not Applicable

13 Push To Talk Switch.

C

2

1

May be inoperative provided an operable Hand Mike is available on the affected side.

14 Service Interphone System (Flight Deck To Cabin) (Cabin To Cabin) (Flight Deck To Ground).

C

1

0

(O)

15 Static Discharge Wicks.

XA-ADQ, XA-ADS, XA-DCX, XAEEE, XA-TSM, XA-UFO, XA-UGJ, XA-UKJ, XA-UKP

C

13

5

(O) The wick on the rudder and the outboard wick on each wing and elevator must be installed. Any one of the remaining wicks may be missing

Revision: Reediciรณn

FECHA: 21 Febrero 2011

May be inoperative provided procedures are not dependent upon its use

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

23 COMMUNICATIONS 15 Static Discharge Wicks.

XA-EGC, XA-MIO, XA-PNG, XASLW, XA-TYX, XA-UMW, XA-UNQ, XA-UOS, XA-USB, XA-USG

C

18

5

16 High Frequency (HF) Communication System.

(O) The wick on the rudder and the outboard wick on each wing and elevator must be installed. Any one of the remaining wicks may be missing.

Not Installed.

17 Emergency Locator Transmitter (ELT).

Fixed ELTs.

1

1

18 Selective Call Systems (SELCAL).

Revision: 03

FECHA: 11 Febrero 2013

Always operative, as required by DGAC, in the NOM-008-SCT3-2002, num. 6.7.12 (b) (9) and NOM-12-SCT3 2001, num.4.1.14 (f).

Not Installed.

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INTENCIONALMENTE EN BLANCO

Revision: 01

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

24 ELECTRICAL 1 Batteries.

A) (SA226T And AT), XA/UGJ.

B

2

1 (M) Left Battery may be inoperative provided: a) Associated Battery Cable is disconnected from the Battery and SECURED, and b) A GPU is used for starting, c) Battery Overheat Switch remains grounded.

B) Batteries (SA226TC Effectivity 355 Thru 419).

XA-ADQ, XA-ADS, XA-UKP, XATSM,

B

2

1 (M) Right Battery may be inoperative provided: a) The associated Battery Cable is disconnected from the Battery and SECURED, and b) A GPU is used for starting, c) Battery Overheat Switch remains grounded.

C) Batteries (SA226TC Effectivity 201 Thru 354).

XA-UFO.

B

2

1

(M) One Battery may be inoperative provided: a) The associated Battery Cable is disconnected from the Battery and SECURED, and b) A GPU is used for starting, c) Battery Overheat Switch remains grounded.

D) Batteries (SA227 Aircraft).

XA-DCX, XA-EEE, XA-EGC, XAMIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XAUOS, XA-USB, XA-USG

B

2

1 (M) Right Battery may be inoperative provided: a) Associated Battery Cable is disconnected from the Battery and SECURED, b) A GPU is used for starting, and c) Battery Overheat Switch remains grounded.

Revision: 03

FECHA: 11 Febrero 2013

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

24 ELECTRICAL 2 DC Voltmeter (Combination Indicator).

C

2

1 (O) May be inoperative for day VMC provided opposite Battery and DC Voltmeter are operative.

3 DC Voltmeter (Applicable For Aircraft Without Combination Indicator).

C

1

1 (O) Any Selector position may be inoperative provided an alternate position or means remains on the Meter for determining the function of the failed position.

4 Inverters (All Aircraft Except SA226-T SN’s 201-248 And SA226-AT, SN-002 Unless Modified To A DC Generator / Inverter System.

C

2

1 One may be inoperative for day VMC. NOTE: With third Inverter modification, two may be inoperative provided operative Inverter powers AC Bus.

5 Alternator (AC System) (SA226T SN’s 201-248 And SA226AT, SN-002 Only).

Not applicable

6 AC Warning Lights.

C

2

1 One may be inoperative provided AC Voltmeter is operative.

7 AC Voltmeter.

C

1

0 AC Voltmeter may be inoperative provided both AC Warning Lights are operative.

8 Battery Disconnect Warning Lights.

B

2

1 (M) One may be inoperative provided: a) The associated Battery Switch is in the OFF position, b) The associated Battery Cable is disconnected from the Battery and SECURED, and c) A GPU is used for starting.

Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

24 ELECTRICAL 9 Battery Overheat Warning Lights.

B

2

1 (M) One may be inoperative provided: a) The associated Battery Cable is disconnected from the Battery and SECURED, b) A GPU is used for starting, and c) Battery Overheat Switch Wire is grounded to keep Battery Overheat Warning Lights OFF.

XA-UKJ, XA-UKP, XA-UMW, XAUNQ, XA-USB, XA-USG.

10 Battery Temperature Indicating And Warning Lights System (Temperature Indications).

It is not installed because of the use of two Lead-acid Batteries N/P RG390E/S, according STC SA09111AC, and Aircraft Type certificate.

B

2

1 (M) One Temperature Indication may be inoperative provided: a) The associated Battery Cable is disconnected from the Battery and SECURED, b) A GPU is used for starting, and c) Associated temperature indication is operative.

XA-UKJ XA-UKP, XA-UMW, XAUNQ, XA-USB, XA-USG.

It is not installed because of the use of two Lead-acid Batteries N/P RG390E/S, according STC SA09111AC, and Aircraft Type certificate.

11 Auxiliary Battery Warning Lights.

12 DC Generator Warning Lights

Revision: 03

DELETED, REVISION 13c.

C

2

0 May be inoperative provided Ammeters are monitored throughout the flight.

FECHA: 11 Febrero 2013

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

25 EQUIPMENT/FURNISHING 1 Cockpit Seat.

B

2

1 Right side may be inoperative for single pilot operations provided right Seat remains unoccupied.

NOTE: A Seat with an inoperative Seat Belt or Shoulder Harness is considered to be inoperative.

2 Passenger Seat(s).

XA-EGC, Only.

D

15

0 May be inoperative provided: A) Seat does not block an Emergency Exit, B) Seat does not restrict any passenger from access to the Main Aircraft Aisle, and C) Affected Seat(s) are blocked and placarded “DO NOT OCCUPY”.

NOTE 1: A Seat with an inoperative Seat Belt is considered inoperative.

NOTE 2: Inoperative Seats do not affect the required number of Flight Attendants.

NOTE 3: Affected Seat(s) may include the Seat(s) behind and/or adjacent outboard Seats.

Not installed

A) Recline Mechanism.

B) Underseat Baggage Restraining Bars.

XA-EGC, Only

C

15

0 (O) May be inoperative provided: a) Baggage is not stowed under Seat with inoperative Restraining Bar, b) Associated Seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and c) Procedures are established to alert Cabin Crew of inoperative Restraining Bar.

Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

25 EQUIPMENT/FURNISHING C) Armrest.

XA-EGC, Only

C

15

0 May be inoperative or missing and Seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the Main Aircraft Aisle, and c) For an Armrest with a Recline Mechanism, Seat is secured in the UPRIGHT position.

3 Approved Flotation.

XA-EGC, Only.

C

18

0

Except XA-EGC.

C

3

0

4 ELT.

RELOCATED TO ATA 23-17, REVISION 16.

5 Non-Essential Equipment & Furnishings (NEF).

Not applicable

6 Baggage Restraint Bars (Under Passenger Seats).

COMBINED WITH PASSENGER SEAT(S), REVISION 15.

7 Crew Arm Rests.

C

4

0 May be inoperative provided Arm Rest(s) can be secured in the DOWN position.

8 Closet Restraining Net.

Not applicable

9 Aft Cargo Tie-Down Net.

C

1

0 May be inoperative if cargo is not to be carried.

10 Aft Cargo Tie-Down Rings.

XA-ADQ, XA-ADS, XA-TSM, XAUFO XA-UGJ. XA-UKP

C

24

0 Adequate number must be operative to properly secure cargo.

XA-DCX, XA-EEE, XA-EGC, XAMIO, XA-PNG. XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XAUOS, XA-USB, XA-USG.

C

36

0 Adequate number must be operative to properly secure cargo.

11 Aft Cargo Blanket Liner Assembly.

C

1

0 May be inoperative if cargo is not to be carried.

Revision: 03

FECHA: 11 Febrero 2013

Pรกg: 25-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

25 EQUIPMENT/FURNISHING 12 Nose Cargo Blanket Liner Assembly.

C

1

13 EMS Equipment.

0 May be inoperative if cargo is not to be carried.

Not installed

14. Emergency Medical Equipment.

A) Automatic External Defibrillator (AED) And/Or Associated Equipment.

C) First Aid Kit (FAK) And/Or Associated Equipment.

Not applicable

A

1

1 (O) The First Aid Kits may be incomplete, missing or inoperative provided: a) FAK is resealed in a manner that will identify it as a Unit that can not be mistaken for a fully serviceable Unit, and b) Repairs or replacements are made within three flight cycles.

15 “Fasten Seat Belt While Seated” Sign Or Placard.

XA-EGC, Only

C

1

0 One or more Signs or Placards may be illegible or missing provided a legible Sign or Placard is visible from each occupied Passenger Seat.

16 Exterior Lavatory Door Ashtrays.

Not applicable

17 Galley Waste Receptacles Access Doors/Covers.

Not applicable

18 Cargo Restraint Systems.

C

10

0 (M) May be inoperative or missing provided acceptable cargo loading limits from an approved source, i.e., an Approved Cargo Loading Manual, Cargo Handling Manual, or Weight and Balance Document are observed.

C

10

0 May be inoperative or missing provided Cargo Compartment remains EMPTY.

19 Overhead Storage Bin(s)/Cabin And Galley Storage Compartments/ Closets.

A) Storage Compartment Key Locks.

Revision: Reedición

FECHA: 21 Febrero 2011

Not applicable

Not applicable

Pág: 25-3

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

25 EQUIPMENT/FURNISHING 20 Observer Seat(s).

A) Primary Observer Seat (Including Associated Equipment).

A

1

0 May be inoperative provided: a) The seat is NOT REQUIRED for official authority duties, and b) Repairs are made within two flight days.

A

1

0 May be inoperative provided: a) Required minimum safety equipment (Safety Belt and Oxygen) is available, b)Seat is acceptable to the DGAC inspector for performance of official duties, and b) Repairs are made within two flight days.

NOTE 1: These provisos are intended to provide for occupancy of the above Seat by an FAA Inspector when the minimum safety equipment (Oxygen and Safety Belt) is functional and the inspector determines the conditions to be acceptable.

NOTE 2: The Pilot-in-Command will determine if the minimum safety equipment is functional for other persons authorized to occupy any Observer Seat(s).

21 Flight Attendant Seat Assembly (Aircraft With Only One Flight Attendant Seat).

22 Crash Axe.

Revision: 02

Not applicable

D

1

FECHA: 19 Enero 2012

0

Pรกg: 25-4

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

26 FIRE PROTECTION 1 Engine Fire Extinguishing System.

DELETED, REVISION 12.

2 Portable Fire Extinguisher(s).

D XA-ADQ, XA-ADS, XA-TSM, XA-UFO, XA-UGJ, XA-UKP.

3

2 Any in excess of those required by FAR may be inoperative or missing provided: a) The inoperative Fire Extinguisher is tagged INOPERATIVE, removed from the installed location and placed out of sight so it cannot be mistaken for a functional Unit, and b) Required distribution is maintained.

XA-DCX, XA-EEE, XA-EGC, XAMIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XAUOS, XA-USB, XA-USG.

D

2

1 Any in excess of those required by authority be inoperative or missing provided: a) The inoperative Fire Extinguisher is tagged INOPERATIVE, removed from the installed location and placed out of sight so it cannot be mistaken for a functional Unit, and b) Required distribution is maintained.

3 “E” (Empty) Light(s) On Engine Fire Extinguisher Control Panel.

C

2

0 (O) May be inoperative provided Bottle Pressure is visually checked and determined to be within the required range prior to each departure.

XA-UGJ, Only

Not installed

4 Lavatory Smoke Detection System.

Not applicable

5 Lavatory Fire Extinguisher System.

Not applicable

Revision: 03

FECHA: 11 Febrero 2013

Pág: 26-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 26-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

27 FLIGHT CONTROLS 1 Trim-In-Motion Sonalerts.

C

2

1 One may be inoperative provided Stabilizer Position Indicator is operative.

2 Stabilizer Position Indicator System.

C

1

0 May be inoperative provided: a) Both Trim-In-Motion Sonalerts are operative, b) Stabilizer Check is accomplished, c) Stabilizer Takeoff Position is set and visually checked prior to each departure, d) Stabilizer is not moved after being set until the aircraft is airborne, and e) Pitch Trim Out-Of-Trim (Takeoff Position Aural Warning is operative.

3 Flap Position Indicator System.

C

1

0 May be inoperative provided a Flap Preselect System is installed.

4 Gust Lock System.

C

1

0 (O)(M) May be inoperative provided: a) Maintenance assures that Flight Control Locking Pins are secured in the UNLOCKED positions, and b) Flight Controls must not be left unattended unless gust protection can be provided.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 27-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 27-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

28 FUEL 1 Fuel Quantity System.

C

2

1 (O) One Fuel Tank Indicator may be inoperative provided: a) Either the Fuel Crossflow Switch Annunciator or Crossflow Valve Position Light is installed and operative, b) A reliable means is established to determine that the fuel quantity on board meets the regulatory requirement for the flight, and c) Both Fuel Flowmeters are operative.

NOTE: MAGNASTICK READINGS ARE INVALID ABOVE 155 GALLONS AND BELOW 30 GALLONS.

2 Fuel Boost Pumps.

C

4

2 One Boost Pump per side may be inoperative.

3 Fuel Magna-Sticks.

C

2

0 NOTE: See Fuel Quantity System and Fuel Quantity Push-To-Test System.

4 Fuel Crossflow Switch Annunciator.

C

1

0 May be inoperative provided Crossflow Valve Position Light is operative.

C

1

0 May be inoperative provided Crossflow Valve Switch is checked CLOSED prior to takeoff and landing.

5 Crossflow Valve Position Light.

C

1

0 May be inoperative provided Fuel Crossflow Switch Annunciator is operative.

6 Fuel Totalizer System.

C

1

0

7 Fuel Quantity Push-To-Test System.

C

1

0 May be inoperative provided fuel quantity indications are verified by use of the Fuel Magna-Sticks.

A) Fuel Crossflow Switch Annunciator (Aircraft incorporating SB226-28005).

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 28-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 28-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

ITEM

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

29 HYDRAULIC POWER 1 Hydraulic Pressure Gauge.

C

1

0 May be inoperative provided both Low Hydraulic Pressure Warning Lights are operative.

2 Low Hydraulic Pressure Warning Light C System.

2

1 One Light may be inoperative provided the Engine with the inoperative Light is started first.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 29-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 29-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

30 ICE & RAIN PROTECTION 1 Propeller Deicing Systems.

C

2

1 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

2 Propeller Heat Ammeter.

C

1

0 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

3 SAS Heat System.

C

1

0 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

4 Pitot Heaters.

B

2

0 May be inoperative provided: a) Passengers are not carried under IFR, and b) Aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

5 Pitot Heater Loadmeter/Ammeter.

B

1

0 May be inoperative provided: a) Passengers are not carried under IFR, and b) Aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

6 Heated Windshield Systems.

XA-ADQ, XA-ADS.

C

1

O May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

XA-DCX, XA-EEE, XA-EGC, XA-MIO, C XA-PNG, XA-SLW, XA-TSM, XA-TYX, XA-UFO, XA-UGJ, XA-UKJ, XA-UKP, XA-UMW, XA-UNQ, XA-UOS, XAUSB, XA-USG.

2

0 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

7 Wing And Tail Deicing System.

C

1

0 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

8 Wing And Tail Deicing Automatic Control.

C

1

0 May be inoperative provided Manual Control is operative.

Revision: 03

FECHA: 11 Febrero 2013

Pรกg: 30-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

30 ICE & RAIN PROTECTION 9 Wing And Tail Deicing Manual Control.

C

1

0 May be inoperative provided Automatic Control is operative.

10 Deice Pressure Indicator.

C

1

0 (O)

11 Engine Inlet Anti-Icing Systems.

C

2

1 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade and not otherwise required by the AFM; AFM REFER TO SPECIAL SYSTEMS OPERATIONS AND CHECKS pages II-14, II-15 AND AFM limitations page 1-21, 1-22

12 Windshield Wipers.

C

2

0 May be inoperative provided flight is not conducted in precipitation within 5 nautical miles of the airport of takeoff or intended landing.

13 Windshield Wiper Park Mode.

C

2

1 (O) May be inoperative provided Circuit Breaker is pulled to manually park the Wiper Blade in a position providing a field of vision satisfactory to the flight crew.

14 Windshield Wiper Slow Mode.

C

2

0 May be inoperative provided Windshield Wipers are operative in Fast Mode.

15 Oil Cooler Inlet Lip DC Thermal AntiIce Heater.

C

2

0 May be inoperative provided aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade and not otherwise required by the AFM; AFM REFER TO SPECIAL SYSTEMS OPERATIONS AND CHECKS pages II-14, II-15

16 Oil Cooler Inlet Lip DC Thermal AntiIce Heater Cycle Lights.

Revision: Reediciรณn

C

2

FECHA: 21 Febrero 2011

0 May be inoperative provided the applicable Generator Ammeter indicates a minimum of 7.5 ampere increase when activating each Lip Anti-Ice Heater.

Pรกg: 30-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

30 ICE & RAIN PROTECTION 17 Pitot Heat Indicating Systems (Required By The Certification Or Operating Rules).

B

2

0 May be inoperative provided: a) All other Elements of the Pitot Heat System operate normally, and b) The airplane is not operated into known or forecast icing conditions.

18 Pitot Heat Indicating Systems (Not Required By The Certification Or Operating Rules).

C

2

0 May be inoperative provided: a) All other Elements of the Pitot Heat System operate normally, and b The airplane is not operated into known or forecast icing conditions.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 30-3

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 30-4

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

31 INDICATING / RECORDING SYSTEMS 1 Clock With Sweep Hand Or Digital Clock.

C

2

1

2 Flight Hour Recorder.

Not installed

3 Flight Data Recorder (FDR) System, XA-USB, XA-USG.

A

1

0 May be inoperative provided: a) Cockpit Voice Recorder (CVR) is operative, b) Airplane is not dispatched from a designated airport: 1. The FDR failure occurs after pushback but before takeoff, or 2. FDR repair was attempted but was not successful. c) In those cases where repair is attempted but not successful, the aircraft may be dispatched on a flight or series of flight until the next designated airport where repair must be accomplished before dispatch, and d) Repairs are made within three flight day

Except XA-USB, XA-USG.

It is not installed in the airplane, according 4.1.314.-IA-0840-1 DGAC authorization, Accomplishing BT-02-ACAS, obligatory bulletin.

4 Flight Data Recorder (FDR) Underwater Locating Device (ULD) (FDR Required By the Authority.

Revision: 03

FECHA: 11 Febrero 2013

Not applicable

Pรกg: 31-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 31-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

32 LANDING GEAR 1 Nose Wheel Steering System (SA227 Aircraft Built Per ECP 603 Or Modified

By SB 227-32-030).

A) Nose Wheel Steering System (All Other Aircraft).

Not Applicable

C

1

0 (O) (M) May be inoperative provided the System is deactivated by: a) Disconnect the Tube Assembly from the Nose Wheel Steering filter to the Restrictor, b) Cap both the Filter Fitting, and Restrictor, c) Turn OFF the NWS ARM Switch, d) Pull the Circuit Breaker, and e) Verify the Steering Casters left and right.

2 Nose Wheel Steering Speed Lever Microswitch.

C

1

0 (O)

3 Nose Wheel Steering Power Lever Microswitch.

DELETED, REVISION 13.

4 Wheel Brake Anti-Skid System.

Not Installed

5 Parking Brake.

C

1

0 (O)

6 Gear Door Warning System.

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, XAUSB, XA-USG. Only.

C

1

0 May be inoperative provided a flight crew member confirms by visual inspection that Main Gear Doors are CLOSED prior to each departure.

7 Landing Gear Control Latch Solenoid.

C

1

0 (O) May be inoperative in the LATCHED position provided the Manual Over-Ride Mechanism operates normally and the aircraft is operated with a crew of two.

Revision: 03

FECHA: 11 Febrero 2013

Pรกg: 32-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 32-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

33 LIGHTS 1 Cockpit/ Flight Deck/ Flight Compartment And Instrument Lighting System.

C

1

0 Individual Lights may be inoperative provided remaining Lights are: a) Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided, b) Positioned so that direct rays are shielded from flight crewmembers eyes, and c) Lighting configuration and intensity is acceptable to the flight crew.

XA-SLW, XA-TYX, XA-UFO.

C

8

2

C

4

0 May be inoperative provided lighting configuration is acceptable to the flight crew.

XA-PNG.

C

8

2

XA-SLW, XA-TYX, XA-UFO.

C

6

2

XA-DCX, XA-UKJ, XA-UKP, XAUMW, XA-UNQ, XA-UOS XA-USB, XA-USG.

C

1

0

C

1

0 (O) May be inoperative provided appropriate verbal briefings are given to the passengers.

2 Cabin Light Systems.

XA-ADQ, XA-ADS.

3 Passenger Notice System (Fasten Seat Belt / No Smoking).

XA-EGC, Only.

Except XA-EGC.

Not applicable

4 Anti-Collision Beacon Light System.

5 Strobe Lights.

Revision: 03

B

1

0 May be inoperative for day operations.

B

1

0 May be inoperative provided Strobe Light System is operative (SA226-AT and TC models only).

C

3

0

FECHA: 11 Febrero 2013

Pรกg: 33-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

ITEM

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

33 LIGHTS 6 Landing Lights.

C

2

0 May be inoperative for day operations. One may be inoperative for night operations.

When Wing mounted Landing/Recognition Lights are installed, both Landing Lights may be inoperative for night flights if both Recognition Lights and the Taxi Light are operative.

XA-ADQ, XA-ADS, XA-DCX, XA-TSM, C

3

0

XA-TYX,

C

1

0

C

3

0 May be inoperative for day operations.

C

6

3 For night operations, individual Bulbs may be inoperative provided at least one Bulb is operative in each Position Light Assembly.

8 Taxi Light.

C

1

0

9 Recognition Lights.

C

2

0

7 Position Light(s).

10 Logo Lights.

11Wing Ice Lights.

Not installed C

2

0 May be inoperative provided aircraft is not operated in known or forecast icing conditions at night.

C

2

0 May be inoperative provided a portable lamp/light of adequate capacity for wing and/or control surface inspection is available for night operations in icing conditions.

C

2

0 May be inoperative provided: a) Aircraft is equipped with an approved Ice Detection System, and b) Ground deicing procedures do not require use of Wing Ice Lights.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 33-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

ITEM

33 LIGHTS 11Wing Ice Lights, (Cont) C

2

1 One may be inoperative provided: a) Left Light is operative for single pilot operations, and b) Ground deicing procedures do not require use of Wing Ice Lights.

12 Baggage Compartment Lights.

C

1

0

XA-MIO, XA-PNG, XA-SLW, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, Only.

C

4

0

13 Normal Annunciator Dim Switch System.

C

1

0 May be inoperative. Bright position must be available for day.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 33-3

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227

INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: 33-4

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 1 Gyroscopic Rate Of Turn / Slip Skid Indicator.

B

2

1 Must be operative on left side for IFR, passenger carrying VFR over-the-top, and passenger carrying VFR night flights.

2 Vertical Speed Indicator.

B

2

1 Must be operative on left side for IFR passenger carrying operations.

NOTE: One rapid response Vertical Indicator is required to be operative in all operations for the Metro IIA (SA226 TC/SFAR 41) airplane.

3 ATC Transponders And Automatic Altitude Reporting Systems.

B

2

0 May be inoperative provided: a) Operations do not require its use, and b) Prior to flight, approval is obtained from ATC facilities having jurisdiction over the planned route of flight.

XA-ADS, Only.

1

1

A) Elementary And Enhanced Downlink Aircraft Reportable Parameters Not Required By 14 CFR.

Not Installed.

B) ADS-B Squitter Transmissions.

Not installed.

4 Navigation Equipment.

A) (VOR / ILS).

C

2

B) (LORAN, OMEGA / VLF, INS, DOPPLER, Global Positioning System, Flight Management Systems).

Revision: Reediciรณn

FECHA: 21 Febrero 2011

0

Two required for IFR operations in IMC conditions.

One may be inoperative for VMC conditions.

One localizer required for IFR in IMC conditions if any approach to be used is predicated upon its use.

Not Installed.

Pรกg: 34-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION A) Navigation Databases.

RELOCATED TO ITEMS ATA 34-22 AND 34-23, REVISION 16.

5 Weather Radar/Thunderstorm Detection Equipment.

C

1

0 May be inoperative provided Wheatear minimums does not require its usage.

C

1

0

6 Marker Beacon.

C XA-ADQ, XA-ADS, XA-DCX, XA-EEE, XA-TSM, XA-UFO, XA-UGJ, XA-UOS,

1

0 May be inoperative provided approach procedure does not require its usage.

XA-EGC, XA-MIO, XA-PNG, XA-SLW, C XA-TYX, XA-UKJ, XA-UKP, XA-UMW, XA-UNQ, XA-USB, XA-USG.

2

0

C 7 Flight Director.

XA-DCX, XA-EGC, XA-MIO, XA-PNG. XA-SLW, XA-TYX, XA-UFO, XA-UKJ, XA-UKP, XA-UOS,

1

0 May be inoperative provided landing minimums are not based on its use.

A) Radar Stabilization.

XA–ADQ, XA–ADS, XA–EEE, XA– TSM, XA-UGJ, XA–UMW, XA–UNQ, XA-USB, XA-USG. 8 Radar Altimeter.

Not Installed.

C

1

0 May be inoperative provided landing minimums are not based on its use.

NOTE: Deferral may affect GPWS operation.

9 Altitude Encoder.

COMBINED WITH ATC TRANSPONDER, REVISION 15.

10 Distance Measuring Equipment (DME) Systems.

XA-ADQ, XA-ADS, XA-EEE, XATSM, XA-UGJ. XA-DCX, XA-EGC, XA-MIO, XAPNG, XA-SLW, XA-TYX, XA-UFO, XA-UKJ, XA-UKP, XA-UMW, XAUNQ, XA-UOS, XA-USB, XA-USG. Revision: 03

D

2

0 May be inoperative provided: The flight is not conducted above 24,000 FT. MSL without prior ATC approval.

Approach is not predicated upon its use.

D

1

0

FECHA: 11 Febrero 2013

Pág: 34-2

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 11 Standby Attitude Indicator XA-MIO, XA-PNG, XA-TYX, XAUFO, XA-UKJ, XA-USB, XA-USG.

C

1

0 May be inoperative provided aircraft does not have an Electronic Attitude Direction Indicator (EADI) installed.

B

1

0 May be inoperative provided: a) Operations are conducted in day VMC only, and

XA–ADQ, XA–ADS, XA–DCX, XA– EEE, XA–EGC, XA-SLW, XA–TSM, XA-UGJ, XA–UKP, XA–UMW, XA– UNQ, XA-UOS. 12 Altitude Alerting System.

b) Operations are not conducted into known or forecast over-the-top conditions.

Not installed

A

1

0 (O) May be inoperative provided: a) Autopilot with Altitude Hold is operative, b) Enroute operations do not require its use, and c) Repairs are made within three flight days.

A

1

0 (O) May be inoperative provided: a) Aircraft is operated with a Second in Command, b) Enroute operations do not require its use, and c) Repairs are made within three flight days.

C 13 Automatic Direction Finder (ADF).

XA.ADQ, XA.ADS, XA-DCX, XAEEE, XA-EGC, XA-MIO, XA-SLW, XA-TSM, XA-TYX, XA-UGJ, XA-UKJ, XA-UKP, XA-UMW, XA-UNQ, XAUOS. XA-PNG, XA-UFO, XA-USB, XAUSG.

Revision: 03

C

2

0

1

0

FECHA: 11 Febrero 2013

Pág: 34-3

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 14 Radio Magnetic Indicator (RMI).

XA-DCX, XA-EEE, XA-EGC, XAUKJ, XA-UKP, XA-UMW, XA-UNQ, XA-UOS, XA-USB, XA-USG.

C

2

0

XA-ADQ, XA-ADS, XA-MIO, XAPNG, XA-SLW, XA-TSM, XA-TYX, XA-UFO XA-UFO, XA-UGJ.

C

1

0

B

1

0 (O) May be inoperative provided any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

B

1

0 (O) May be inoperative provided:

15 Non-Stabilized Magnetic Compass System.

a) Any combination of two Gyro or INS (IRU) Stabilized Compass Systems operate normally, and b) Airplane is operated with Dual Independent Navigation Capability and under Positive Radar Control by ATC on the enroute portion of the flight.

16 Traffic Alert Collision Avoidance System (TCAS I), XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG XASLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS,

B

1

0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are installed, operate normally, and used in conjunction with approved Free Gyro Navigation Techniques.

B

1

0 (M) May be inoperative provided: a) System is deactivated and SECURED, and b) Enroute or approach procedures do not require its use.

C

Revision: 03

1

0 (M) May be inoperative provided: a) Not required by the authority b) System is deactivated and SECURED, and c) Enroute or approach procedures do not require its use.

FECHA: 11 Febrero 2013

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SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION A) Traffic Alert Collision Avoidance B System (TCAS II), XA-USG, Only.

1

C

1

0 (M) May be inoperative provided: a) System is deactivated and SECURED, and b) Enroute or approach procedures do not require its use.

0 (M) May be inoperative provided: a) Not required by the authority b) System is deactivated and SECURED, and c) Enroute or approach procedures do not require its use.

1 One may be inoperative on the non-flying pilot side provided: a) TA and RA visual display is operative on flying pilot side, and b) TA and RA audio function is operative on flying pilot side.

1 May be inoperative on non-flying pilot side.

1) Combined Traffic Alert (TA) And Resolution Advisory (RA) Dual Display.

C

2

2) Resolution Advisory (RA) Display System(s).

C

2

C

2

3) Traffic Alert Display System(s). C

2

4) Audio Functions.

B

1

0 May be inoperative provided enroute or approach procedures do not require use of TCAS.

5) Airspace Selection Function.

C

1

0

Revision: 03

0 (O) May be inoperative provided: a) Traffic Alert (TA) visual display and audio functions are operative, b) TA ONLY Mode is selected by the crew, and c)Enroute or approach procedures do not require its use.

0 (O) May be inoperative provided: a) RA visual display and audio functions are operative, and b) Enroute or approach procedures do not require its use.

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SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 17 Terrain Awareness And Warning System (TAWS).

C

1

0

A) Class A TAWS Equipment Required.

Not applicable

B) Class B TAWS Equipment Required.

1) Ground Proximity Warning System (GPWS), XA-DCX, XAEEE, XA-EGC, XA-MIO, XAPNG, XA-SLW, XA-TYX, XAUKJ, XA-UMW, XA-UNQ, XAUOS, XA-USB, XA-USG, XAUSB, XA-USG. XA-ADS, XA-ADQ, XA-TSM, XA-UFO, XA-UGJ, XA-UKP,

1

0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days.

NOT INSTALLED Accomplishing Alternate procedure described in BT-01-GPWS.Obligatory bulletin, approved by the DGAC.

a) Modes 1 & 3.

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS,

A

XA-EGC, XA-MIO, XA-SLW, XA-TYX, XA-USB, XA-USG.

A

1

1

b) Test Mode.

A XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, XA-USB, XA-USG. c) Modes 2, 4 & 5.

C XA-DCX, XA-EEE, XA-PNG, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, XA-USB, XA-USG.

1

0 May be inoperative provided:

XA-EGC, XA-MIO, XA-SLW, XA-TYX, Revision: 03

A

2

0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within two flight days.

a) GPWS is considered inoperative, and b) Repairs are made within two flight days.

3

0

2

0

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SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION d) Advisory Callouts.

XA-DCX, XA-EEE, XA-EGC, XA-PNG, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS,

B

4

0 (O) May be inoperative provided alternate procedures are established and used.

C

4

0 (O) May be inoperative provided: a) Advisory Callouts not required by 14 CFR, and b) Alternate procedures are established and used.

XA-MIO, XA-SLW, XA-TYX, XA-USB, XA-USG.

B

1

0

e) Windshear Mode (Reactive).

Not installed.

2) Terrain System-Forward Looking Terrain Avoidance (FLTA) And Premature Descent Alert (PDA) Functions.

3) Terrain Displays.

Not installed.

4) Runway Awareness & Advisory System (RAAS).

Not installed.

Not installed.

C) Class C TAWS Equipment.

Not installed.

18 Gyroscopic Direction Indicator Slaved Mode.

C

2

0 (O) May be inoperative provided DG Mode is operative.

19 Overspeed Warning Sensor.

XA-ADQ, XA-ADS, XA-DCX, XAEEE, XA-TSM, XA-TYX, XA-UGJ, XA-UOS, XA-USB, XA-USG.

B

1

0 May be inoperative provided AFM speed limitations are observed.

XA-MIO, XA-PNG, XA-SLW, XAUFO, XA-UKJ, XA-UKP, XA-UMW, XA-UNQ.

B

2

0 May be inoperative provided AFM speed limitations are observed.

20 Outside Air Temperature (OAT) Indicating System.

XA-ADS XA-ADQ, XA-DCX, XAUGJ, XA-UOS, XA-USB, XA-USG.

C

1

1 May be inoperative provided OAT is provided by another calibrated System that allows determination of true OAT.

Revision: 03

FECHA: 11 Febrero 2013

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SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 20 Outside Air Temperature (OAT) Indicating System, (Cont).

XA-EEE, XA-MIO, XA-PNG, XASLW, XA-TSM, XA-TYX, XA-UFO, XA-UKJ, XA-UKP, XA-UMW, XAUNQ. 21 Externally Mounted Airspeed Bugs.

C

2

1

C

4

0 May be inoperative, broken, or missing except for CC/DC single pilot operations. In that case left side Bugs must be installed.

Not installed.

22 Flight Management System.

A) Navigation Databases.

Not applicable.

23 Navigation Management System.

Not installed.

A) Navigation Databases.

Not applicable.

24 Windshear Detection, Guidance And Avoidance System.

Not installed.

25 Automatic Dependent Surveillance Broadcast (ADS-B) System.

Not installed.

CARGO OPERATIONS ONLY-SECOND IN COMMAND IS REQUIRED. 1 Airspeed Indicator CARGO OPERATIONS ONLY-SECOND IN COMMAND IS REQUIRED.

B

2

1 May be inoperative on right side provided: a) Copilot’s Pitot System is functioning normally, and b)A functioning Pneumatic Indicator is installed and available to the pilot.

2 Gyroscopic Bank and Pitch Indicator CARGO OPERATIONS ONLYSECOND IN COMMAND IS REQUIRED.

B

2

1 May be inoperative on right side provided: a) Two independent power sources are available to drive the left side instruments, and b) Aircraft does not have an Electronic Attitude Direction Indicator (EADI) installed on left side.

Revision: 03

FECHA: 11 Febrero 2013

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SYSTEM & SEQUENCE ITEM NUMBERS

34 NAVIGATION 3 Gyroscopic Direction Indicator CARGO OPERATIONS ONLYSECOND IN COMMAND IS REQUIRED.

B

2

1 May be inoperative on right side provided: a) Magnetic Compass is operative, b) Two independent power sources are available to drive the left side instruments, and c) Aircraft does not have an Electronic Horizontal Situation Indicator (EHSI) installed on the left side.

4 Altimeter, Barometric Pressure, Adjustable CARGO OPERATIONS ONLY-SECOND IN COMMAND IS REQUIRED.

Revision: 03

B

2

1 May be inoperative on right side provided a functioning Pneumatic Altimeter, adjustable for barometric pressure, is installed and available to the pilot.

FECHA: 11 Febrero 2013

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INTENCIONALMENTE EN BLANCO

Revision: 03

FECHA: 11 Febrero 2013

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SYSTEM & SEQUENCE ITEM NUMBERS

35 OXYGEN 1 Passenger Oxygen System.

DELETED, REVISION 14.

2 Crew Oxygen System.

C

1

3 Protective Breathing Equipment (PBE).

Revision: Reediciรณn

FECHA: 21 Febrero 2011

1 A two hour oxygen supply required for each pilot or greater, required by DGAC Not Installed.

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

37 VACUUM 1 Low Suction Warning Light.

Revision: Reediciรณn

C

1

FECHA: 21 Febrero 2011

0 May be inoperative provided the Suction Gauge is operative.

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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SYSTEM & SEQUENCE ITEM NUMBERS

46 INFORMATION SYSTEMS 1 Electronic Flight Bag Systems (EFBs).

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Not Installed

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Revision: Reediciรณn

FECHA: 21 Febrero 2011

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SYSTEM & SEQUENCE ITEM NUMBERS

52 DOORS 1 CABIN DOOR CLOSED Warning Light System.

C

1

0 (O) May be inoperative provided: a) All Latches are visually checked in the CLOSED and LATCHED position, and Door is not reopened prior to departure, b) Fasten Seat Belt Sign remains on, or passengers are briefed to remain seated with their Seat Belts FASTENED, and c) The aircraft remains unpressurized.

NOTE: Removing one Latch is acceptable as in Item 52-5.

2 AFT CARGO DOOR CLOSED Warning Light System.

C

1

0 (O) May be inoperative provided: a) All Latches are visually checked in the CLOSED and LATCHED position, and the Door is not reopened prior to departure, b) FASTEN SEAT BELT Sign remains ON, or passengers are briefed to remain seated with their Seat Belts FASTENED, and c) The airplane remains unpressurized.

3 Aft Cargo Door Test Light (Cabin Door C Entryway, SA226 Series).

XA-ADQ, XA-ADS, XA-TSM, XA-UFO

1

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UFO, XA-UGJ, XA-UKJ, XA-UKP, XA-UMW.

0 (O) May be inoperative provided AFT CARGO DOOR CLOSED Warning Light System (Item 52-2) is operative.

Not installed.

C

1

0 (O) May be inoperative provided: a) All Latches are visually checked in the CLOSED and LATCHED position, and Door is not reopened prior to departure, b) FASTEN SEAT BELT Sign remains ON, or passengers are briefed to remain seated with their Seat Belts FASTENED, and c) The aircraft remains unpressurized.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

52 DOORS 4 Aft Cargo Door Secondary Warning And Test System.

C

1

0 Switches NORMAL (Green Light). May be inoperative provided all Aft Cargo Door Switches are visually checked to insure they have extended to their relaxed (Door Open) positions prior to departure.

The DOOR UNSAFE Light may be inoperative provided all Latches are visually checked in the CLOSED and LATCHED position, and not reopened prior to departure, or the AFT CARGO DOOR CLOSED Warning Light (Annunciator Panel) is operative.

5 Cabin Door Latches.

C

7

6 (O) (M) One may be removed provided aircraft is operated unpressurized and the Latches are visually checked in the CLOSED and LATCHED position and not reopened prior to departure.

6 AFT Cargo Door Latches.

C

8

7 (O) (M) One may be removed provided aircraft is operated unpressurized and the remaining Latches are visually checked in the CLOSED and LATCHED position, and not reopened prior to departure.

C

8

7 (O) (M) One may be removed provided aircraft is operated unpressurized and the AFT CARGO DOOR CLOSED Warning System is operative for the remaining Door Latches.

C

2

0 (M) May be inoperative provided the FASTEN SEAT BELT Sign remains ON, or the passengers are orally briefed to remain seated with their Seat Belts FASTENED.

7 Door Seals Systems (Passenger And Cargo Doors).

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

SYSTEM & SEQUENCE ITEM NUMBERS

52 DOORS 8 Passenger Door/Gas Springs.

C XA-ADQ, XA-ADS, XA-TSM, XA-UFO, XA-UGJ, XA-UKP, XA-USB, XA-USG.

2

0 May be inoperative provided Door is manually restrained by the crew and inoperative Snubber/Gas Spring does not interfere with Door operation. Placard Door Area both inside and outside: SNUBBER/GAS SPRING CLOSERS NOT INSTALLED. DO NOT DROP DOOR. NOTE: Second Snubber is an option. No placard is required when one Snubber is operative.

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS

Revision: 03

C

1

0

FECHA: 11 Febrero 2013

Pรกg: 52-3

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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SYSTEM & SEQUENCE ITEM NUMBERS

61 PROPELLERS 1 NTS Systems (SA226-T Only).

Not Applicable

2 NTS Check Systems (SA226-T Only).

Not Applicable

3 Propeller Synchronizing/ Synchrophaser System.

Revision: Reediciรณn

C

1

FECHA: 21 Febrero 2011

0

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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SYSTEM & SEQUENCE ITEM NUMBERS

71 POWER PLANT 1 Engine Case Ground Heating System (Tanis Type).

2 Reserve Power Systems.

XA-MIO, XA-PNG, XA-SLW, XA-TYX, XA-UFO.

Not installed.

D

2

0 May be inoperative provided aircraft performance (i. e. takeoff, enroute drift down, or approach climb) are not predicated on its use.

XA–ADQ, XA–ADS, XA–DCX, XA– EEE, XA–EGC, XA–TSM, XA-UGJ, XA–UKJ, XA–UKP, XA–UMW, XA– UNQ, XA-UOS, XA-USB, XA-USG.

Revision: 03

FECHA: 11 Febrero 2013

Not installed.

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Revision: Reediciรณn

FECHA: 21 Febrero 2011

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REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

73 ENGINE FUEL AND CONTROL 1 Fuel Flowmeters.

B

2

1 (O) One may be inoperative.

Place a placard on the dash to advise the crew that there will be inaccuracies in the fuel totalize

2 Fuel Consumed Totalizer.

Revision: Reediciรณn

DELETED, REVISION 12 (Item moved to ATA Section 28).

FECHA: 21 Febrero 2011

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 SYSTEM & SEQUENCE ITEM NUMBERS

REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

74 IGNITION 1 Ignition Lights.

C

2

0 Both may be inoperative provided: a) Continuous and Override Ignition Systems are audibly checked prior to each Engine Start, and b) Aircraft is not operated in visible moisture and OAT less than +5 degrees Centigrade.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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INTENCIONALMENTE EN BLANCO

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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SYSTEM & SEQUENCE ITEM NUMBERS

77 ENGINE INDICATING 1 SRL Computer System (SA226-T(B) And SA227-TT Only).

2 SRL Computer System (SA-227 Aircraft With SRL Inoperative AFM Supplements Only).

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG. XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, XAUSB, XA-USG. 3 Temperature Limiter And Indicator Light (SA 227 Series Only).

XA-DCX, XA-EEE, XA-EGC, XA-MIO, XA-PNG. XA-SLW, XA-TYX, XA-UKJ, XA-UMW, XA-UNQ, XA-UOS, XAUSB, XA-USG.

DELETED, REVISION 13. SEE ATA 80, STARTING. C

2

0 May be inoperative provided operations are conducted in accordance with SRL Inoperative Supplement Data contained in AFM/POH.

C

2

0 May be inoperative in accordance with AFM.

4 ITT Indicator, Digital Readout.

Not Applicable

5 ITT Compensator (SA226 Series With TPE-331-3 Engines).

Not Applicable.

6 EGT Compensator (SA-226-TC Series With TPE-331-10UA-551G Engines).

Not Applicable

7 ET Indicator, Digital Readout (SA226T(B) Only).

Not Applicable.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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FECHA: 21 Febrero 2011

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REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

80 STARTING 1 Auto-Start System.

C

2

XA-UFO.

Revision: Reediciรณn

0 (O) May be inoperative provided AFM manual start procedures are used.

NOT APPLICABLE

FECHA: 21 Febrero 2011

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Revision: Reediciรณn

FECHA: 21 Febrero 2011

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REPAIR INTERVAL NUMBER INSTALLED NUMBER REQUIRED FOR DISPATCH REMARKS OR EXCEPTIONS

82 WATER INJECTION 1 AWI System.

Not applicable

2 CAWI System.

C

1

0 May be inoperative provided AFM performance does not require its use.

3 AWI/CAWI Quantity Indicator.

C

1

0 May be inoperative provided: a) Visual check of the quantity is made prior to departure, and b) Landing performance is not predicated upon its use.

4 Standby Rocket System.

Revision: Reediciรณn

Not applicable

FECHA: 21 Febrero 2011

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Revision: Reediciรณn

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MAINTENANCE & OPERATIONS

PROCEDURES

Revision: Reediciรณn

FECHA: 21 Febrero 2011

Pรกg: MO-1

MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

21.1 Cabin Altitude Warning System.

(O) For unpressurized flight consider the topographic and meteorological conditions for the flight level the pilot choice the airspeed for altitudes above 10,000 feet the oxygen will be enough for the estimated time enroute. Refer to AFM, procedure 3A-32.

21.2 Cabin Altitude/Differential Pressure Indicator.

(O) For unpressurized flight consider the topographic and meteorological conditions for the flight level and the airspeed is choice by the pilot for altitudes above 10,000 feet the oxygen will be enough for the estimated time enroute. Refer to AFM, procedures 3-3, 3-15

21.4 Flow Control Valves (M) Determine position of failed valve by starting applicable engine and run at ground idle with bleed air switch in open position, if no airflow from vents, valve is closed.

(O) Bleed air switch OFF, fan switch to OVERRIDE. Hold taxi light/fresh air fan switch in nose wheel well. Fan should continue to operate. Verify oxygen masks available to all occupants.

21.5 Automatic Pressurization Controller (O) For unpressurized flight consider the topographic and meteorological conditions for the flight level and the airspeed is choice by the pilot for altitudes above 10,000 feet the oxygen will be enough for the estimated time enroute. Refer to AFM, procedure 3A-32.

21.6 Manual Pressurization Controller (O) For unpressurized flight consider the topographic and meteorological conditions for the flight level and the airspeed is choice by the pilot for altitudes above 10,000 feet the oxygen will be enough for the estimated time enroute. Refer to AFM, procedure 3A-32.

21.9 Air Conditioning System.

(O) Operations procedure to identify, isolate, and operate with one system inoperative and to determine cockpit fan is operative. AFM Abnormal procedures 3A-4, Warning and monitoring systems 6-56.

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

21.10 Cabin Dump Valve.

(O) Place cabin dump switch to “DUMP” position. Refer to oxygen chart in AFM EMERGENCY PROCEDURES 3-15, 8A. Operations procedure to operate the aircraft in unpressurized flight. AFM Manufacturer´s data 6-52, emergency systems 3-15 a 3-17.

Maintenance note: Have a mechanic to deactivate and secure the dump valve in the open position.

Pull the dump valve circuit breaker and secure it with a tie wrap. Maintenance Manual Cap. 21-30-20

23.14 (O) When the system is inoperative the crew must to coordinate with the maintenance and operations the signals to be used during starting and departure.

23.15 Static Discharge Wicks.

(O) Verify the required wicks are installed.

24.1 Batteries.

(M) Maintenance procedures to disconnect and secure the Battery cable. Maintenance Manual 24-3013, 24-30-15

24.2 DC Voltmeter (Combination Indicator).

(O) Operations procedure to determine the opposite battery and DC voltmeter are Operative and monitored. AFM Abnormal procedures 3A4, 3A5.

24. 8 Battery Disconnect Warning Lights.

(M) Maintenance procedures to assure that no unsafe Condition exists and a procedure to disconnect and secure the battery cable. Maintenance manual cap. 24-30-13.

(O) Operations procedure to determine the opposite battery and DC voltmeter are Operative and monitored. AFM normal procedures 2-30.

24.9 Battery Overheat Warning Lights, (M) The mechanic disconnect the associated Battery Cable and SECURED, also grounded the Battery Overheat Switch Wire to keep the Warning Lights OFF-

24.10 Battery Temperature Indicating And Warning Lights System (Temperature Indications).

(M) The mechanic disconnect the associated Battery Cable and SECURED Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

25.2 Underseat Baggage Restraining Bars.

(O) When the Underseat Baggage Bar is inoperative the crew must placard the seat DO NOT STOW BAGGAGE UNDER THIS SEAT

25.14 C First Aid Kit (FAK) (O) The crew must to reseal the First aid kit, and request another as soon as practical.

25.18 Cargo Restraint Systems.

(M) Observe the correct limits when the cargo is loaded

26. 3 “E” (Empty) Light(s) On Engine Fire Extinguisher Control Panel.

(O) Operations procedure to determine the system is properly charged prior to each Departure. AFM normal procedures 2-41, 2-42

27.4 Gust Lock System.

(O) Operations procedure to secure controls. AFM manufacturer´s data 6B-22.

(M) Maintenance procedure to assure the flight control locking pins is secured in the unlocked position. Maintenance manual cap. 27-20-10, page 211

28.1 Fuel Quantity System.

(O) Ensure that either the fuel crossflow switch annunciator is operable or both flow meters are operable. Verify quantity by loading enough fuel for the required trip or topping off the tanks.

Operations procedure to determine fuel on board meets regulatory requirements. AFM manufacturer´s data 6B-28, normal procedures 2-6

30.10 Deice Pressure Indicator.

(O) Operations procedure to visually monitor the deice boots for inflation cycle. Normal procedures 249.

30.13 Windshield Wiper Park Mode.

(O) Crew will pull breaker and secure with a tie wrap. Refer to operations procedure to manually park windshield wipers. Manufacturer´s data 6B-39

Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

32.1 A) Nose Wheel Steering System (O) Ensure NWS switch is in the “OFF” position.

Check for free castering while taxing using brakes and differential power.

Note: If amber NWS fail light illuminates in flight with NWS inoperative, select emergency gear extension and perform a normal landing.

Procedure to operate the aircraft with the nose wheel steering deactivated. AFM emergency procedures 3-29.

(M) For the Procedure for deactivating the nose wheel steering and ensuring no unwanted Hydraulic commands will occur. Refer to Maintenance manual cap. 32-50-00

32.2 Nose Wheel Steering Speed Lever Microswitch (O) Place a placard on the power quadrant to advise the pilot they must depress the power lever micro switch to activate the steering. Refer to AFM emergency procedures 3-29, limitations 1-15 Takeoffs and landings must be performed without NWS system.

32. 5 Parking Brake.

(O) Operations procedure for preventing movement of aircraft when stopped or Parked. AFM manufacturer´s data 6B-37.

32. 7 Landing Gear Control Latch Solenoid.

(O) Procedure to advise flight crew of need to manually over-ride the locking Mechanism. Abnormal procedures 3A-8.

33.3 Passenger Notice System (Fasten Seat Belt / No Smoking).

(O) The crew must be aware for give the appropriate instructions to the passengers.

34.12 Altitude Alerting System.

(O) The crew must verify before departure the autopilot is operative with the altitude hold function operative.

34.15 Non-Stabilized Magnetic Compass System.

(O) the crew must verify the gyros are operative before departure.

Revision: Reedición

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

34.17 Terrain Awareness And Warning System (TAWS).

1) Ground Proximity Warning System (GPWS).

(O) Pilot not flying should monitor flight path during takeoff, approach, and landing, and alert the pilot flying if any of the following conditions exist: 1) Excessive descent rate.

2) Excessive terrain closure rate.

3) Altitude loss after takeoff or go-around.

4) Unsafe terrain clearance while not in the landing mode.

5) Deviation from glideslope

34.17 Terrain Awareness And Warning System (TAWS).

1) Ground Proximity Warning System (GPWS). a) Modes 1&3 (O) Pilot not flying should monitor flight path during takeoff, approach, and landing, and alert the pilot flying if any of the following conditions exist: 1) Excessive descent rate.

2) Excessive terrain closure rate.

3) Altitude loss after takeoff or go-around.

4) Unsafe terrain clearance while not in the landing mode.

5) Deviation from glide slope.

34.17 Terrain Awareness And Warning System (TAWS).

1) Ground Proximity Warning System (GPWS). d) Advisory Callouts.

(O) Pilot not flying should monitor flight path during takeoff, approach, and landing, and alert the pilot flying

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

34. 18 Gyroscopic Direction Indicator Slaved Mode.

(O) The crew must verify that the DG Mode is operative before departure, during flight check heading with compass and correct DG indicator each 10 minutes.

52.1 CABIN DOOR CLOSED Warning Light System.

(O) Procedure to advise flight crew how to operate aircraft unpressurized. AFM emergency procedure 3-18

52.2 AFT CARGO DOOR CLOSED Warning Light System.

(O) Procedure to advise flight crew how to operate aircraft unpressurized. AFM emergency procedure 3-18

52.3 Aft Cargo Door Test Light (Cabin Door Entryway, SA226 Series).

(O) The crew must be sure the AFT cargo door closed warning light system is operative, and visually check if the door is closed and latched.

52.5 Cabin Door Latches.

(O) The crew must be sure the door is closed and the other latches are in position.

(M) Maintenance procedure for removing the latch and restoring the "cabin door Open" warning light function. Maintenance manual cap. 52-10-10, 52-30-20

52.6 Aft Cargo Door Latches (O) Operations procedure to assure the "click clack latches" are in the latched Position and a procedure to operate the aircraft unpressurized. AFM emergency procedure 3-18.

(M) Maintenance procedure for removing the latch and restoring the "cabin door Open" warning light function. Maintenance manual cap. 52-10-10, 52-30-20

52.7 Door Seals Systems (Passenger and cargo door) (M) Maintenance procedure for removing the latch and restoring the "aft cargo door" Warning light function. Maintenance manual cap. 52-10-10, 52-30-20

Revision: Reediciรณn

FECHA: 21 Febrero 2011

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MINIMUM EQUIPMENT LIST FAIRCHILD SA226 & SA227 MAINTENANCE & OPERATIONS PROCEDURES

73.1 Fuel Flowmeters.

(O) Operations procedure to assure the crew is aware of the inaccuracy of the fuel totalize when the fuel flow meter is malfunctioning. AFM manufacturer´s data 6B-28

80.1 Auto-Start System.

(O) Refer to AFM manual start procedure.

Normal procedures 2-27.

Abnormal procedures 3A-17.

Revision: Reedición

FECHA: 21 Febrero 2011

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