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E.O. Nº: Revision: Rev. date: Page:

ENGINEERING ORDER

GERENCIA DE SOPORTE TECNICO SUBGERENCIA DE INGENIERIA

Subject: FUEL - GENERAL - REVISE THE ELECTRICAL BONDING OF THE EQUIPMENT IN THE FUEL TANKS – ADDITIONAL WORK

SB-28-0124-LA 00 15/Nov//2010 1 de 2

Accomplish On:

This E. O. fully embodies SB A340-28-4097 REV. 05

A340

Reg. CC-CQA CC-CQG

Remarks

See Remarks

Applicability

VN / MSN Reg. 359 CC-CQC 167

VN / MSN 363

Reg. CC-CQE

Component Description:

P/Nº:

Seq.

All All

Skill MECH INSP

Reg. CC-CQF

Open 16.0

8.0

Insp.

Test 2.0 2.0

Mod/Rework 2.0 2.0

8.0

VN / MSN 442

S/N:

Procedure (M/H / Elapsed Time)

Estimated Man Hour: EO Item

VN / MSN 429

Manuf.

8.0

Estimated Close 16.0

8.0

per Item

42 M/H 2 M/H

44 Hrs

Total Estimated Man Hour to Accomplish this E.O. Comply with EO : SB-28-0124 as follows PART I PART II (Not applicable) Due Date (D/M/Y): See Note 2 Due Cycles/Hours: -Repeat: No Ground Time: 26 Hrs

PART III (Not applicable)

Notes: 1.

2. 3.

This EO complements the required actions embodied on the fleet as per EO AD-28-0086 and EO AD-28-0087 as applicable to A/C registration. Comply with this EO within 24 months after 26/Nov/10 If you are going to use the pressure defueling method make sure that there is enough capacity on the center tank for the fuel coming from the trim tank. At least 10874 lb (4890 Kgs) or 1646 USgal (6230 lts) of tank capacity are required for this. Refer to AMM 28-11-00 PB 001 for A/C tank capacities information. Refer to EO Paragraph B, Step 1.c).

Quality Control Follow-Up Action/Part Accomplished:

Inspector Name & License, Signature:

Next Action/Part: Next due :

Accomp. Verification and Record Signature dd/mm/yy Sign Off / / Engineering / / Record Keep / /

After Application Return E.O. to Engineering? (Yes / No) : Yes Accomplishment Data (Aircraft or Component): Accp. On Date Hours Cycles Used M/H (S/Nº/Reg.)

MANDATORY DOCUMENT Lan Engineering Services This document and attachment are Lan property and can not be used, copied o given to any other party without the written authorization of the Engineering Director

ENGINEERING ORDER

GERENCIA DE SOPORTE TECNICO SUBGERENCIA DE INGENIERIA

E.O. Nยบ: Revision: Rev. date: Page:

SB-28-0124-LA 00 15/Nov//2010 2 de 2

Affected Manuals Manual M.M. I.P.C. W.D. OVERHAUL MANUAL OPERATION MANUAL M.E.L. WEIGHT AND BALANCE OTHER

Action/document generated ---------

APPROVAL THE MODIFICATION AS SPECIFIED BY THIS ENGINEERING ORDER WAS BASED IN AD 2010-0232 AND SB A340-28-4097 REV. 05 EASA APPROVED DATA AND APPROVED BY CHILEAN DGAC ACCORDING TO DAR PART 39. Remarks: At the moment of release of this Engineering Order, SB A340-28-4097 Rev. 03, was embodied on LAN Aircraft MSN 363 and MSN 429 thru the application of both EO SB-280064 and EO AD-28-0087; and embodied on LAN Aircraft MSN 167, MSN 359 and MSN 442 thru the application of EO AD-28-0086 This EO complies with the requirements of EASA SB A340-28-4097 Rev. 05, Config 03 Additional Work as per SBIT SEMB/914.0701/09 recommendations.

Prepared by:

Reviewed by:

Approved by:

Constantino Restrepo P Aircraft Systems Engineer

Alejandro Mancinelli Base Engineering Chief

Carlos Durรกn V. Engineering Manager