# Maintenance Review Board

Report

Airbus A340

July 2010

This MRB Report is produced by Airbus on behalf of the A330/A340 Industry Steering Committee and is

available from AIRBUS SAS, Customer Services - Technical Data & Support Services, 1 rond-point Maurice

Bellonte, 31707 BLAGNAC Cedex, France.

# This page is intentionally left blank

# A340 MRB REPORT

Issue : 

# July 2010 R.O.R. 1 RECORD OF REVISIONS

REV.

NO. ISSUE

DATE DATE

INSERTED BY REV.

NO. ISSUE

DATE DATE

INSERTED BY

0 27 JAN 93

1 11 FEB 94

2 15 MAR 95

3 16 OCT 96

4 07 APR 97

5 31 DEC 98

6 31 DEC 99

7 21 MAR 02

8 28 NOV 03

9 15 SEP 05

10 15 DEC 06

11 18 JUN 08

12 01 JUL 10

RETAIN THIS RECORD IN THE FRONT OF THIS REPORT. UPON RECEIPT OF REVISION, INSERT

REVISED PAGES IN THE DOCUMENT AND ENTER REVISION NUMBER, DATE INSERTED AND INITIAL.

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 SOC Page : 1 

# SUMMARY OF CHANGES INCORPORATED INTO

A340 MRB REPORT REVISION 12

GENERAL

The A340 MRB REPORT revision 12 (Sep 2009) is issued to:

- Add EWIS compliance notes to Sections A, B, C INTRO & E INTRO.

- Add EWIS task identifiers in Section E and ATA 20 of Section C.

- Update abbreviated MSI title table in Section C INTRO

- WV GROUP 45A updated.

A full list of the individual changes is highlighted below:

COVER PAGE

Updated

ROR

Updated

TOC

No change

SOC

Updated.

LEP

Updated.

SECTION A

Page A2

Paragraph 5 “(including EWIS)” added

SECTION B

Page B1 Rule 8: “Damage Tolerant” added for clarification

Page B2 Rule 17: Reworded to add EWIS compliance notes.

SECTION C

Page C-INTRO-2 Paragraph 1 (j) Table updated. The following MSIs were added: 23.33.00,

34.48.00, 46.11.00, 52.36.00.

# A340 MRB REPORT

Issue : July 2010 SOC Page : 2 Page C-INTRO-3 Paragraph 1 (l) Reworded to add EWIS compliance notes.

SYSTEMS AND POWERPLANT SECTION

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.121/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AVIONICS COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE

AVIONICS COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.121/02 R DESCRIPTION CHANGED FROM: "(EZAP).", TO: "(EWIS)."

C-20 20.0.131/01 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

FORWARD CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE

FORWARD CARGO COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.131/02 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

FORWARD CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE

FORWARD CARGO COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.131/03 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE FORWARD CARGO COMPARTMENT,

(EZAP).", TO:

"ROUTES INSTALLED IN THE FORWARD CARGO

COMPARTMENT, (EWIS)."

C-20 20.0.131/04 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE FORWARD CARGO COMPARTMENT,

(EZAP).", TO:

"ROUTES INSTALLED IN THE FORWARD CARGO

COMPARTMENT, (EWIS)."

C-20 20.0.137/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE BAY BEHIND FWD CARGO COMPARTMENT (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE BAY BEHIND FWD CARGO

COMPARTMENT (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.141/01 R DESCRIPTION CHANGED FROM: "ALL THE WIRING

INSTALLED INSIDE THE FUEL TANK (AS FAR AS

VISIBLE), (EZAP).", TO: "EWIS INSTALLED INSIDE THE

FUEL TANK (AS FAR AS VISIBLE), (EWIS)."

C-20 20.0.145/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE ZONE UNDER CABIN FLOOR (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE ZONE

UNDER CABIN FLOOR (ONLY IF

CONTAMINATED), (EWIS)."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 3 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.151/01 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

AFT CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE AFT CARGO

COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.151/02 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

AFT CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE AFT CARGO

COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.151/03 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

AFT CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE AFT CARGO

COMPARTMENT (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.151/04 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

AFT CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING),(EZAP).", TO: "EWIS INSTALLED IN THE AFT CARGO

COMPARTMENT (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.151/05 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE AFT CARGO COMPARTMENT, (EZAP).",

TO:

"ROUTES INSTALLED IN THE AFT CARGO COMPARTMENT,

(EWIS)."

C-20 20.0.151/06 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE AFT CARGO COMPARTMENT, (EZAP).",

TO:

"ROUTES INSTALLED IN THE AFT CARGO COMPARTMENT,

(EWIS)."

C-20 20.0.151/07 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE AFT CARGO COMPARTMENT, (EZAP).",

TO:

"ROUTES INSTALLED IN THE AFT CARGO COMPARTMENT,

(EWIS)."

C-20 20.0.151/08 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED AT

THE ACT, EXTERNAL SURFACE ONLY.(EZAP)", TO: "EWIS

INSTALLED AT THE ACT, EXTERNAL SURFACE

ONLY.(EWIS)"

C-20 20.0.155/01 R DESCRIPTION CHANGED FROM: "ALL THE WIRING

INSTALLED INSIDE THE REAR CENTER TANK (AS FAR AS

VISIBLE), (EZAP).", TO: "EWIS INSTALLED INSIDE THE

REAR CENTER TANK (AS FAR AS VISIBLE),

(EWIS)."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 4 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.161/01 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

BULK CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE BULK CARGO

COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.161/02 R DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE

BULK CARGO COMPARTMENT (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE BULK

CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.161/03 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE BULK CARGO COMPARTMENT, (EZAP).",

TO:

"ROUTES INSTALLED IN THE BULK CARGO COMPARTMENT,

(EWIS)."

C-20 20.0.161/04 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE BULK CARGO COMPARTMENT, (EZAP).",

TO:

"ROUTES INSTALLED IN THE BULK CARGO COMPARTMENT,

(EWIS)."

C-20 20.0.211/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE COCKPIT (ONLY CONTAMINATED WIRING), (EZAP).",

TO: "EWIS INSTALLED IN THE COCKPIT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.211/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE COCKPIT AT LEVEL OF LATERAL FLOOR STRUCTURE

BETWEEN FR.1 TO FR.11, (EZAP).", TO: "EWIS

INSTALLED IN THE COCKPIT AT LEVEL OF LATERAL FLOOR

STRUCTURE BETWEEN FR.1 TO FR.11,

(EWIS)."

C-20 20.0.221/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS BETWEEN SEAT AND A/C INSTALLED IN THE

FWD CABIN

UTILITY AREA, (EZAP). NOTE: THIS TASK IS

APPLICABLE FOR A/C VERSIONS WITH SEATS

AND WITH WIRING CONNECTIONS BETWEEN SEAT AND

A/C,", TO: "EWIS CONNECTIONS, ATTACHMENT POINTS

AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION INSTALLED IN THE

FWD CABIN UTILITY AREA, (EWIS).

NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS

WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN

SEAT AND A/C AND/OR SEAT TO SEAT

CONNECTION,"

APPLICABILITY CHANGED FROM: "ALL", TO: "ALL NOTE"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 5 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.221/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE FWD CABIN UNTILITY AREA (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE FWD

CABIN UTILITY AREA (ONLY IFCONTAMINATED), (EWIS)."

C-20 20.0.221/03 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THIS AREA, (EZAP).", TO: "ROUTES INSTALLED

IN THIS AREA, (EWIS)."

C-20 20.0.223/01 R TASK TITLE CHANGED FROM: "COPMPARTMENT", TO:

"COMPARTMENT"

DESCRIPTION CHANGED FROM: "ALL WIRING AND CIRCUIT

BRAKERS "5001 VE" INSTALLED IN THE FWD CABIN

UTILITY AREA OVERHEAD COMPARTMENT (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS AND

CIRCUIT BRAKERS "5001 VE" INSTALLED IN THE FWD

CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.223/02 R TASK TITLE CHANGED FROM: "COPMPARTMENT", TO:

"COMPARTMENT"

DESCRIPTION CHANGED FROM: "INSTALLED IN THE FWD

CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "AND "G, AND

P" ROUTES INSTALLED IN THE FWD CABIN

UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.231/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS

BETWEEN SEAT AND A/C INSTALLED IN THE FWD CABIN

AREA, (EZAP). NOTE: THIS TASK IS APPLICABLE FOR

A/C VERSIONS WITH SEATS AND WITH

WIRING CONNECTIONS BETWEEN SEAT AND A/C ONLY,

(EZAP).", TO: "EWIS CONNECTIONS, ATTACHMENT POINTS

AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION

INSTALLED IN THE FWD CABIN AREA,(EWIS). NOTE: THIS

TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND

WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION,

ONLY."

C-20 20.0.231/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE FWD CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE FWD CABIN

AREA (ONLY IF CONTAMINATED),

(EWIS)."

C-20 20.0.231/03 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE FWD CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE FWD CABIN

AREA (ONLY IF CONTAMINATED),

(EWIS)."

C-20 20.0.233/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE FWD CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE FWD CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS)."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 6 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.233/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE FWD CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE FWD CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS)."

C-20 20.0.233/03 N NEW TASK ADDED

C-20 20.0.233/04 N NEW TASK ADDED

C-20 20.0.241/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS

BETWEEN SEAT AND A/C INSTALLED IN THE MID CABIN

UTILITY AREA, (EZAP). NOTE: THIS TASK IS

APPLICABLE FOR A/C VERSIONS WITH SEATS

AND WITH WIRING CONNECTIONS BETWEENSEAT AND

A/C", TO: "EWIS CONNECTIONS, ATTACHMENT POINTS AND

ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION INSTALLED

IN THE MID CABIN UTILITY AREA, (EWIS). NOTE: THIS

TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND

WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION,"

C-20 20.0.241/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN UTILITY AREA (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE MID

CABIN UTILITY AREA (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.241/03 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN UTILITY AREA (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE MID

CABIN UTILITY AREA (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.243/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN UTILITY AREA OVERHEAD COMPARTMENT

AREA (ONLY CONTAMINATED WIRING), (EZAP).", TO:

"EWIS INSTALLED IN THE MID CABIN

UTILITY OVERHEAD COMPARTMENT AREA (ONLY IF

CONTAMINATED). (EWIS)."

C-20 20.0.243/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN UTILITY AREA OVERHEAD COMPARTMENT

AREA (ONLY CONTAMINATED WIRING), (EZAP).", TO:

"EWIS INSTALLED IN THE MID CABIN

UTILITY OVERHEAD COMPARTMENT AREA (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.243/03 N NEW TASK ADDED

C-20 20.0.243/04 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 7 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.251/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS BETWEEN SEAT AND A/C INSTALLED IN THE

MID CABIN AREA, (EZAP). NOTE: THIS TASK IS APPLICABLE

FOR A/C VERSIONS WITH SEATS AND WITH

WIRING CONNECTIONS BETWEEN SEAT AND A/C ONLY,

(EZAP).", TO: "EWIS CONNECTIONS, ATTACHMENT POINTS

AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION

INSTALLED IN THE MID CABIN AREA, (EWIS). NOTE:

THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH

SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT

AND A/C AND/OR SEAT TO SEAT CONNECTION,

ONLY."

C-20 20.0.251/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE MID CABIN

AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.251/03 R DESCRIPTION CHANGED FROM: ""G" ROUTES INSTALLED IN

THIS AREA, (EZAP).", TO: ""G AND P" ROUTES

INSTALLED IN THIS AREA, RH ONLY, (EWIS)."

APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

OR A340-300"

C-20 20.0.251/04 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE MID CABIN

AREA (ONLY IF CONTAMINATED),

(EWIS)."

C-20 20.0.251/05 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE MID CABIN

OVERHEAD AREA (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.251/06 N NEW TASK ADDED

C-20 20.0.251/07 N NEW TASK ADDED

C-20 20.0.253/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE MID CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.253/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE MID CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.253/03 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE MID CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE MID CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.253/04 N NEW TASK ADDED

C-20 20.0.253/05 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 8 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.253/06 N NEW TASK ADDED

C-20 20.0.261/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS BETWEEN SEAT AND A/C INSTALLED IN THE

AFT CABIN AREA, (EZAP). NOTE: THIS TASK IS APPLICABLE

FOR A/C VERSIONS WITH SEATS AND WITH

WIRING CONNECTIONS BETWEEN SEAT AND A/C ONLY,

(EZAP).", TO: "EWIS CONNECTION, ATTACHMENT POINTS

AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION,

INSTALLED IN THE AFT CABIN AREA,(EWIS). NOTE: THIS

TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS AND

WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION,

ONLY."

C-20 20.0.261/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN AREA (ONLY CONTAMINATED WIRING),

(EZAP).", TO: "EWIS INSTALLED IN THE AFT CABIN

AREA (ONLY IF CONTAMINATED),

( EWIS ) ."

C-20 20.0.261/03 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN AREA (ONLY CONTAMINATED

WIRING),(EZAP).", TO: "EWIS INSTALLED IN THE AFT

CABIN AREA (ONLY IF ONTAMINATED), (EWIS)."

C-20 20.0.261/04 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN AREA (ONLY CONTAMINATED

WIRING),(EZAP).", TO: "EWIS INSTALLED IN THE AFT

CABIN AREA (ONLY IF CONTAMINATED),

(EWIS)."

C-20 20.0.263/01 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE AFT CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.263/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE AFT CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS)."

C-20 20.0.263/03 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN OVERHEAD COMPARTMENT AREA (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS

INSTALLED IN THE AFT CABIN OVERHEAD

COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS)."

C-20 20.0.263/04 N NEW TASK ADDED

C-20 20.0.263/05 N NEW TASK ADDED

C-20 20.0.263/06 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 9 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.271/01 R DESCRIPTION CHANGED FROM: "ALL WIRING

CONNECTIONS BETWEEN SEAT AND A/C INSTALLED IN THE

AFT CABIN UTILITY AREA. NOTE: THIS TASK IS APPLICABLE

FOR A/C VERSIONS WITH SEATS AND WITH

WIRING CONNECTIONS BETWEEN SEAT AND A/C, ONLY,

(EZAP).", TO: "EWIS CONNECTIONS, ATTACHMENT POINTS

AND ELECTRICAL CONNECTORS, BETWEEN SEAT AND A/C

AND/OR SEAT TO SEAT CONNECTION,

INSTALLED IN THE AFT CABIN UTILITY AREA, (EWIS).

NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS

WITH SEATS AND WITH EWIS CONNECTIONS BETWEEN

SEAT AND A/C AND/OR SEAT TO SEAT

CONNECTION ONLY."

C-20 20.0.271/02 R DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN

THE AFT CABIN UTILITY AREA (ONLY CONTAMINATED

WIRING), (EZAP).", TO: "EWIS INSTALLED IN THE AFT

CABIN UTILITY AREA (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.271/03 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THIS AREA, (EZAP).", TO: "ROUTES INSTALLED

IN THIS AREA, (EWIS)."

C-20 20.0.273/01 R DESCRIPTION CHANGED FROM: "ALL WIRING AND CIRCUIT

BRAKERS "5005 VE" INSTALLED IN THE AFT CABIN

UTILITY AREA OVERHEAD COMPARTMENT (ONLY

CONTAMINATED WIRING), (EZAP).", TO: "EWIS AND

CIRCUIT BRAKERS "5005 VE" INSTALLED IN THE AFT

CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF

CONTAMINATED), (EWIS)."

C-20 20.0.273/02 R DESCRIPTION CHANGED FROM: "INSTALLED IN THE AFT

CABIN UTILITY AREA OVERHEAD COMPARTMENT, (EZAP).",

TO: "AND "P" ROUTE INSTALLED IN THE AFT CABIN

UTILITY AREA OVERHEAD COMPARTMENT,

(EWIS)."

C-20 20.0.315/01 R DESCRIPTION CHANGED FROM: "WIRING ROUTES

INSTALLED IN THE TAIL CONE FIREWALL AND APU AREA,

(EZAP).", TO: "ROUTES INSTALLED IN THE TAIL CONE

FIREWALL AND APU AREA, (EWIS)."

C-20 20.0.319/01 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE), (EZAP).", TO: "EWIS (AS FAR AS VISIBLE),

(EWIS)."

C-20 20.0.319/02 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE), (EZAP).", TO: "EWIS (AS FAR AS VISIBLE),

(EWIS)."

C-20 20.0.319/03 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE), (EZAP).", TO: "EWIS (AS FAR AS VISIBLE),

(EWIS)."

C-20 20.0.333/01 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) FROM RIB 3 TO RIB 4 LH / RH (EZAP)", TO:

"EWIS (AS FAR AS VISIBLE) FROM RIB 3 TO RIB 4 LH /

RH (EWIS)"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 10 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.333/02 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) FROM RIB 4 TO RIB 19LH / 20RH (EZAP)",

TO: "EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO RIB

19LH / 20RH (EWIS)"

C-20 20.0.333/03 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) FROM RIB 4 TO RIB 13LH / 20RH (EZAP)",

TO: "EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO RIB

13LH / 20RH (EWIS)"

C-20 20.0.333/04 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) FROM RIB 13 TO RIB 20LH (EZAP)", TO:

"EWIS (AS FAR AS VISIBLE) FROM RIB 13 TO RIB 20LH

(EWIS)"

C-20 20.0.333/05 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) FROM RIB 4 TO RIB 20 LH/RH (EZAP)", TO:

"EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO RIB 20

LH/RH (EWIS)"

C-20 20.0.333/06 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) (EZAP)", TO: "EWIS (AS FAR AS VISIBLE)

(EWIS)"

C-20 20.0.333/07 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE) (EZAP)", TO: "EWIS (AS FAR AS VISIBLE)

(EWIS)"

C-20 20.0.346/01 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE)(EZAP)", TO: "EWIS (AS FAR AS VISIBLE)

(EWIS)"

C-20 20.0.346/02 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE)(EZAP)", TO: "EWIS (AS FAR AS VISIBLE)

(EWIS)"

C-20 20.0.541/01 R DESCRIPTION CHANGED FROM: "WIRING WITHIN THE INNER

FUEL TANK (AS FAR AS VISIBLE)(EZAP).", TO: "EWIS

WITHIN THE INNER FUEL TANK (AS FAR AS

VISIBLE)(EWIS)."

C-20 20.0.541/02 R DESCRIPTION CHANGED FROM: "WIRING WITHIN THE INNER

FUEL TANK (AS FAR AS VISIBLE)(EZAP).", TO: "EWIS

WITHIN THE INNER FUEL TANK (AS FAR AS

VISIBLE)(EWIS)."

C-20 20.0.542/01 R DESCRIPTION CHANGED FROM: "WIRING IN THE OUTER

FUEL TANK (RIB 23 TO RIB 33)(AS FAR AS

VISIBLE)(EZAP).", TO: "EWIS IN THE OUTER FUEL TANK

(RIB 23 TO RIB 33)(AS FAR AS

VISIBLE)(EWIS)."

C-20 20.0.542/02 R DESCRIPTION CHANGED FROM: "WIRING IN THE INNER

FUEL TANK NO. 1/4 (RIB 6 TO RIB 11 AFT OF CENTRE

SPAR TO RIB 23)(RIB 11 TO RIB 23)(AS FAR AS

VISIBLE)(EZAP).", TO: "EWIS IN THE INNER

FUEL TANK NO. 1/4 (RIB 6 TO RIB 11 AFT OF CENTRE

SPAR TO RIB 23)(RIB 11 TO RIB 23)(AS FAR AS

VISIBLE)(EWIS)."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 11 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-20 20.0.543/01 R DESCRIPTION CHANGED FROM: "WIRING WITHIN THE

OUTER FUEL TANK (AS FAR AS VISIBLE)(EZAP).", TO: "EWIS

WITHIN THE OUTER FUEL TANK (AS FAR AS

VISIBLE)(EWIS)."

C-20 20.0.550/01 R DESCRIPTION CHANGED FROM: "WIRING WITHIN THE VENT

SURGE TANK (AS FAR AS VISIBLE)(EZAP).", TO: "EWIS

WITHIN THE VENT SURGE TANK (AS FAR AS

VISIBLE)(EWIS)."

C-20 20.0.571/01 R DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS

VISIBLE)(EZAP).", TO: "EWIS (AS FAR AS

VISIBLE)(EWIS)."

C-21 21.21.00/09 R 100% INTERVAL CHANGED FROM: "2 C", TO: "2 C NOTE 24"

C-21 21.70.00/01 N NEW TASK ADDED

C-21 21.70.00/02 N NEW TASK ADDED

C-21 21.70.00/03 N NEW TASK ADDED

C-21 21.70.00/04 N NEW TASK ADDED

C-23 23.33.00/03 R IN DESCRIPTION: "(IF INSTALLED)" ADDED

C-23 23.39.01/01 R DESCRIPTION CHANGED FROM: "ELEMENTS.", TO:

"ELEMENTS ON TAILWIND SYSTEM."

APPLICABILITY CHANGED FROM: "POST 54128", TO: "IF

TAILWIND SYSTEM INSTALLED"

C-23 23.73.00/01 R APPLICABILITY CHANGED FROM: "PRE 44058 PRE 47057

PRE 48823 OR PRE 45556 PRE 47057 PRE 48823", TO:

"A340-200 PRE 44058 PRE 45556 OR A340-300 PRE

44058 PRE 45556 OR A340-300 PRE

48823 OR A340-500 PRE 47057 OR A340-600 PRE 47057"

C-23 23.73.00/03 R 100% INTERVAL CHANGED FROM: "2 C NOTE 26", TO: "2 C"

C-23 23.73.00/05 R 100% INTERVAL CHANGED FROM: "16000 FH", TO: "20000

FH"

APPLICABILITY CHANGED FROM: "POST 43319", TO:

"POST 43319 PRE 49314"

C-23 23.73.00/09 R DESCRIPTION CHANGED FROM: "CABIN/COCKPIT INCIDENT

ALERT SYSTEM", TO: "EMERGENCY CABIN ALERT SYSTEM

(ECAS)"

C-23 23.73.00/10 N NEW TASK ADDED

C-24 24.30.00/03 R DESCRIPTION CHANGED FROM: "RESTORATION", TO:

"OVERHAUL"

C-25 25.21.00/04 R 100% INTERVAL CHANGED FROM: "800 FH", TO: "VR"

C-25 25.27.00/01 R IN APPLICABILITY: "A340-300 POST 45670 PRE 56746"

ADDED

C-25 25.40.00/01 R 100% INTERVAL CHANGED FROM: "NR OR 1 C", TO: "1 C

OR NR"

C-25 25.40.00/02 R 100% INTERVAL CHANGED FROM: "NR OR 1 C", TO: "1 C

OR NR"

C-25 25.51.00/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 12 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-25 25.51.00/02 R DESCRIPTION CHANGED FROM: "XZ LATCHES", TO:

"XZ-LATCHES"

FEC CHANGED FROM: "9", TO: "8"

100% INTERVAL CHANGED FROM: "4 C", TO: "34000 FH"

APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/03 R DESCRIPTION CHANGED FROM: "FR53.7", TO: "C53.7"

FEC CHANGED FROM: "9", TO: "8"

100% INTERVAL CHANGED FROM: "4 C", TO: "34000 FH"

APPLICABILITY CHANGED FROM: "POST 40611", TO:

"A340-200 POST 40611"

C-25 25.51.00/04 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/05 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/06 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/07 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/08 R TASK CODE CHANGED FROM: "GVI", TO: "DI"

DESCRIPTION CHANGED FROM: "GENERAL VISUAL

INSPECTION OF POWER DRIVE UNITS", TO: "DETAILED

INSPECTION OF POWER DRIVE UNIT ROLLER FOR WEAR

AND DAMAGE."

APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/09 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/10 R FEC CHANGED FROM: "9", TO: "8"

100% INTERVAL CHANGED FROM: "4 A", TO: "3200 FH"

IN ZIP-REFERENCE(S): "ZL-151-01-1" REMOVED

APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/11 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/12 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/13 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 13 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-25 25.51.00/14 R FEC CHANGED FROM: "9", TO: "8"

100% INTERVAL CHANGED FROM: "4 C", TO: "34000 FH"

C-25 25.51.00/17 R APPLICABILITY CHANGED FROM: "ALL", TO: "A340-200

PRE 55380 OR A340-300 PRE 55380 OR A340-500 OR

A340-600"

C-25 25.51.00/19 N NEW TASK ADDED

C-25 25.51.00/20 N NEW ENTRY "TASK RESERVED"

C-25 25.51.01/01 N NEW TASK ADDED

C-25 25.51.01/02 N NEW TASK ADDED

C-25 25.51.01/03 N NEW ENTRY "TASK RESERVED"

C-25 25.51.01/04 N NEW TASK ADDED

C-25 25.51.01/05 N NEW TASK ADDED

C-25 25.51.01/06 N NEW TASK ADDED

C-25 25.51.01/07 N NEW TASK ADDED

C-25 25.51.01/08 N NEW TASK ADDED

C-25 25.51.01/09 N NEW TASK ADDED

C-25 25.51.01/10 N NEW TASK ADDED

C-25 25.51.01/11 N NEW TASK ADDED

C-25 25.51.01/12 N NEW TASK ADDED

C-25 25.51.01/13 N NEW TASK ADDED

C-25 25.51.01/14 N NEW TASK ADDED

C-25 25.51.01/15 N NEW TASK ADDED

C-25 25.52.00/03 R DESCRIPTION CHANGED FROM: "OUTLETS FOR EVIDENCE

OF DRAINAGE SYSTEM OBSTRUCTION AND CLEAN AS

NECESSARY. (NOTE:IF ACT'S INSTALLED, TASK TO BE

PERFORMED IN THE REMAINING AREA)", TO:

"FUNNELS AT THE END OF THE ROLLER TRACKS AND

BELOW THE PDUS FOR EVIDENCE OF CLOGGING OR

OBSTRUCTION AND CLEAN AS NECESSARY. (NOTE 11)"

C-25 25.52.00/04 N NEW TASK ADDED

C-25 25.52.00/05 N NEW TASK ADDED

C-25 25.52.00/06 N NEW TASK ADDED

C-25 25.54.00/04 R TASK CODE CHANGED FROM: "GVI", TO: "DI"

DESCRIPTION CHANGED FROM: "GENERAL VISUAL", TO:

"DETAILED"

IN ZIP-REFERENCE(S): "ZL-161-01-1" REMOVED

C-25 25.54.00/05 R TASK CODE CHANGED FROM: "GVI", TO: "DI"

DESCRIPTION CHANGED FROM: "GENERAL VISUAL", TO:

"DETAILED"

IN ZIP-REFERENCE(S): "ZL-161-01-1" REMOVED

C-25 25.54.00/06 R TASK CODE CHANGED FROM: "GVI", TO: "DI"

DESCRIPTION CHANGED FROM: "GENERAL VISUAL", TO:

"DETAILED"

IN ZIP-REFERENCE(S): "ZL-161-01-1" REMOVED

C-25 25.62.00/02 R DESCRIPTION CHANGED FROM: "REMOVE SLIDE/RAFT FOR

RESTORATION", TO: "RESTORATION OF LIFE RAFTS BY

REMOVAL AND REPLACEMENT WITH OVERHAULED."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 14 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-25 25.62.00/03 R 100% INTERVAL CHANGED FROM: "NOTE 10 NOTE 8", TO:

"OR VR NOTE 10"

C-25 25.65.32/01 R TASK CODE CHANGED FROM: "FC", TO: "RS"

DESCRIPTION CHANGED FROM: "EMERGENCY LOCATOR

TRANSMITTER FOR FUNCTIONAL CHECK", TO: "SURVIVAL

EMERGENCY LOCATOR TRANSMITTER (ELT(S)) FOR

WORKSHOP CHECK."

APPLICABILITY CHANGED FROM: "ALL", TO: "IF

SURVIVAL ELT INSTALLED"

C-25 25.65.35/01 R IN TASK TITLE: "SYSTEM" ADDED

DESCRIPTION CHANGED FROM: "ELT SYSTEM BY MANUAL

ACTIVATION", TO: "AUTOMATIC FIXED EMERGENCY

LOCATOR TRANSMITTER (ELT(AF)) SYSTEM BY MANUAL

ACTIVATION."

APPLICABILITY CHANGED FROM: "IF ELT INSTALLED",

TO: "IF AUTOMATIC FIXED ELT INSTALLED"

C-25 25.65.35/02 R TASK CODE CHANGED FROM: "FC", TO: "RS"

IN TASK TITLE: "SYSTEM" ADDED

DESCRIPTION CHANGED FROM: "ELT FOR BATTERY

REPLACEMENT AND DURING RE-INSTALLATION PERFORM

FUNCTIONAL CHECK OF ELT SYSTEM INCLUDING

AUTOMATIC ACTIVATION", TO: "AUTOMATIC FIXED

EMERGENCY LOCATOR TRANSMITTER (ELT(AF)) FOR

RESTORATION IN WORKSHOP INCLUDING BATTERY

REPLACEMENT AND CHECK OF AUTOMATIC ELT

ACTIVATION."

APPLICABILITY CHANGED FROM: "IF ELT INSTALLED",

TO: "IF AUTOMATIC FIXED ELT INSTALLED"

C-25 25.66.52/01 R IN DESCRIPTION: "BY REMOVAL AND REPLACEMENT WITH

OVERHAULED." ADDED

C-26 26.18.00/19 N NEW TASK ADDED

C-26 26.18.00/20 N NEW TASK ADDED

C-26 26.18.00/21 N NEW TASK ADDED

C-27 27.24.00/02 R IN DESCRIPTION: "(THIS TASK COVERS TASK

29.10.00/08)" ADDED

C-28 28.24.00/03 N NEW TASK ADDED

C-28 28.27.00/01 R IN TASK TITLE: "TANK" ADDED

C-28 28.27.00/02 R IN TASK TITLE: "TANK" ADDED

C-28 28.27.00/03 R IN TASK TITLE: "TANK" ADDED

C-29 29.10.00/08 R IN DESCRIPTION: "(COVERED BY MSI 27-24-00 TASK NO

2)" ADDED

C-29 29.20.00/11 N NEW TASK ADDED

C-29 29.20.00/12 N NEW TASK ADDED

C-31 31.33.00/01 R IN DESCRIPTION: "(THIS TASK COVERS TASK

31.36.01/01)" REMOVED

APPLICABILITY CHANGED FROM: "ALL", TO: "A340 PRE

47606 PRE 48904"

C-31 31.33.00/02 R IN DESCRIPTION: "(THIS TASK COVERS TASK

31.36.01/02)" REMOVED

APPLICABILITY CHANGED FROM: "ALL", TO: "A340 PRE

47606 PRE 48904"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 15 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-31 31.33.00/03 R IN DESCRIPTION: "(THIS TASK COVERS TASK

31.36.01/03)" REMOVED

APPLICABILITY CHANGED FROM: "ALL", TO: "A340 PRE

47606 PRE 48904"

C-31 31.36.01/01 R IN DESCRIPTION: "(COVERED BY MSI 31-33-00, TASK

NO1)" REMOVED

IN APPLICABILITY: "POST 48904" ADDED

C-31 31.36.01/02 R IN DESCRIPTION: "(COVERED BY MSI 31-33-00, TASK

NO2)" REMOVED

IN APPLICABILITY: "POST 48904" ADDED

C-31 31.36.01/03 R DESCRIPTION CHANGED FROM: "THE ULB (COVERED BY

MSI

31-33-00, TASK NO3)", TO: "ULB."

IN APPLICABILITY: "POST 48904" ADDED

C-31 31.36.01/04 N NEW TASK ADDED

C-34 34.13.00/05 N NEW TASK ADDED

C-34 34.48.00/01 R TASK TITLE CHANGED FROM: "GROUND PROXIMITY

WARNING

SYSTEM (GPWS)", TO: "TERRAIN AWARNESS AND WARNING

SYSTEM (INCLUDING (E)GPWS AND T2CAS-TAWS)"

C-34 34.48.00/02 R TASK TITLE CHANGED FROM: "GROUND PROXIMITY

WARNING SYSTEM (GPWS)", TO: "TERRAIN AWARNESS AND

WARNING SYSTEM (INCLUDING (E)GPWS AND T2CASTAWS)"

DESCRIPTION CHANGED FROM: "GPWC BY BITE", TO:

"GROUND SELF TEST SYSTEM"

C-34 34.53.00/01 R APPLICABILITY CHANGED FROM: "PRE 47245 POST 50453

PRE 53622 OR POST 47482 POST 50453 PRE 53622 OR

POST 50860 POST 50453 PRE 53622", TO: "PRE 50859

PRE 53622 OR PRE 50859 POST 54662

OR POST 50860 PRE 53622 OR POST 50860 POST 54662

OR PRE 47019 PRE 53622 OR PRE 47019 POST 54662 OR

POST 47482 PRE 53622 OR POST 47482 POST 54662"

C-34 34.55.00/01 R APPLICABILITY CHANGED FROM: "POST 50453 PRE

53622", TO: "PRE 53622 OR POST 54662"

C-35 35.10.00/01 R 100% INTERVAL CHANGED FROM: "1 C", TO: "18 MO"

C-35 35.10.00/02 R DESCRIPTION CHANGED FROM: "CLEAN", TO: "CLEANING

OF"

C-35 35.10.00/04 R IN DESCRIPTION: "AND FUNCTIONAL CHECK OF CYLINDER

PRESSURE GAUGE." ADDED

FEC CHANGED FROM: "6", TO: "6,9"

100% INTERVAL: "72 MO OR" ADDED

C-35 35.10.00/05 R 100% INTERVAL CHANGED FROM: "6 YE", TO: "72 MO"

C-35 35.10.00/06 N NEW TASK ADDED

C-35 35.10.00/07 N NEW TASK ADDED

C-35 35.20.02/04 R DESCRIPTION CHANGED FROM: "48635/48728)", TO:

"48635/48728/55606)"

C-35 35.20.02/06 R 100% INTERVAL CHANGED FROM: "2 A", TO: "1600 FH"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 16 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-35 35.20.02/07 R 100% INTERVAL CHANGED FROM: "30 MO NOTE 24A", TO:

"30 MO"

C-35 35.20.02/08 R 100% INTERVAL CHANGED FROM: "30 MO NOTE 24A", TO:

"30 MO"

C-35 35.20.02/10 R 100% INTERVAL CHANGED FROM: "6 YE NOTE 24A", TO:

"6 YE"

C-35 35.20.02/11 R APPLICABILITY CHANGED FROM: "POST 40257", TO:

"POST 40257 PRE 48635 OR PRE 48728 OR PRE 55606"

C-35 35.20.02/12 R 100% INTERVAL CHANGED FROM: "60 MO NOTE 24A", TO:

"60 MO"

C-35 35.20.02/13 R 100% INTERVAL CHANGED FROM: "60 MO NOTE 24", TO:

"60 MO"

C-35 35.20.02/15 R 100% INTERVAL CHANGED FROM: "60 MO NOTE 24B", TO:

"60 MO"

C-35 35.20.02/16 R 100% INTERVAL CHANGED FROM: "60 MO NOTE 24B", TO:

"60 MO"

C-35 35.30.00/03 R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE 55559"

C-35 35.30.00/04 R 100% INTERVAL: "NOTE 26" ADDED

C-35 35.30.00/05 R 100% INTERVAL CHANGED FROM: "4 C", TO: "72 MO"

C-35 35.30.00/06 N NEW TASK ADDED

C-35 35.30.00/07 N NEW TASK ADDED

C-36 36.00.00/07 R APPLICABILITY CHANGED FROM: "A340-200 OR

A340-300", TO: "A340-200 PRE 57418 OR A340-300 PRE

57418"

C-36 36.00.00/09 R 100% INTERVAL CHANGED FROM: "36 MO", TO: "72 MO"

C-36 36.00.00/12 N NEW TASK ADDED

C-36 36.00.00/13 N NEW TASK ADDED

C-38 38.10.00/01 R DESCRIPTION CHANGED FROM: "SYSTEM AND DISCARD OF

WATER FILTER CARTRIDGES (IF INSTALLED).", TO:

"SYSTEM."

FEC CHANGED FROM: "7,9", TO: "9"

C-38 38.10.00/02 N NEW TASK ADDED

C-38 38.10.00/03 N NEW TASK ADDED

C-38 38.31.00/05 D TASK DELETED

C-38 38.31.00/07 D TASK DELETED

C-38 38.31.00/08 N NEW TASK ADDED

C-38 38.31.00/09 N NEW TASK ADDED

C-38 38.31.00/10 N NEW TASK ADDED

C-38 38.31.00/11 N NEW TASK ADDED

C-38 38.31.00/12 N NEW TASK ADDED

C-38 38.31.00/13 N NEW ENTRY "TASK RESERVED"

C-46 46.11.00/01 N NEW TASK ADDED

C-46 46.21.01 R TASK TITLE CHANGED FROM: "'A' CONFIGURATION", TO:

"CONFIGURATIONS"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 17 SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

C-46 46.55.00 N NEW ENTRY "NO TASK SELECTED"

C-52 52.51.11/04 R APPLICABILITY CHANGED FROM: "POST 50014", TO:

"POST 50014 PRE 57371"

C-52 52.51.11/05 R APPLICABILITY CHANGED FROM: "POST 50014", TO:

"POST 50014 PRE 57371"

C-52 52.51.11/07 N NEW TASK ADDED

C-52 52.51.11/08 N NEW TASK ADDED

SECTION D

Page D-INTRO-17 8. NOTES FOR SECTION D . New note 8 added.

NOTE 8: The threshold is to be counted from 1st flight.

Page D-INTRO-18 Weight Variant Table updated to add WV 004 to Group 45A.

STRUCTURE SECTION

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-52 523101-01-2 R IN ZIP-REFERENCE(S): "ZL-821-01-1" ADDED

D-52 523121-01-2 N NEW TASK ADDED

D-52 523201-01-2 R IN ZIP-REFERENCE(S): "ZL-822-01-1" ADDED

D-52 523221-01-2 N NEW TASK ADDED

D-52 523301-01-1 R IN ZIP-REFERENCE(S): "ZL-823-01-1" ADDED

D-52 523321-01-2 N NEW TASK ADDED

D-53 531107-01-1 R 100% THRESHOLD CHANGED FROM: "6 YE", TO: "3 YE"

100% INTERVAL CHANGED FROM: "6 YE", TO: "3 YE"

D-53 531111-01-1 R 100% THRESHOLD CHANGED FROM: "12 YE", TO: "3 YE"

100% INTERVAL CHANGED FROM: "12 YE", TO: "3 YE"

D-53 531150-01-1 R SAMPLE THRESHOLD: "12 YE" REMOVED

SAMPLE INTERVAL: "12 YE" REMOVED

100% THRESHOLD CHANGED FROM: "20 YE", TO: "12 YE"

TPS: "APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE

3" ADDED

D-53 531850-01-1 R SAMPLE THRESHOLD: "12 YE" REMOVED

SAMPLE INTERVAL: "12 YE" REMOVED

100% THRESHOLD CHANGED FROM: "20 YE", TO: "12 YE"

TPS: "APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE

3" ADDED

D-53 532103-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

D-53 532104-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 18

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 532107-02-1 R DESCRIPTION CHANGED FROM: "FORWARD CARGO

COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B

AND FR 25 (10 PLACES)", TO: "ECCENTRIC BOLTS FOR

FWD CARGO COMPARTMENT DOOR AT 10 POSITIONS

BETWEEN FR 20B AND FR 25"

D-53 532117-01-2 R DESCRIPTION CHANGED FROM: "FR18 AND FR 38 FROM

STR 26 TO CROWN CENTERLINE", TO: "FR 18 AND FR 38

FROM STR 6 TO STR 26,"

D-53 532119-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

D-53 532122-01-1 R IN PREPARATION TASKS: "AIR CONDITION DUCTS" ADDED

AND "AIR CONDITIONING DUCTS" REMOVED

DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 532123-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 532134-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 532134-01-2 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 532135-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 532166-01-2 N NEW TASK ADDED

D-53 532217-01-1 R DESCRIPTION CHANGED FROM: "26 TO CROWN CENTER

LINE,", TO: "6 TO STR 26,"

D-53 532266-01-1 N NEW TASK ADDED

D-53 533005-01-1 R SAMPLE THRESHOLD: "OR 75000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "5000 FC", TO: "4750

FC OR 32300 FH"

APPLICABILITY CHANGED FROM: "A340-200 OR

A340-300", TO: "GROUP 42A OR GROUP 43A OR GROUP

42B OR GROUP 43B OR GROUP 43E"

D-53 533035-01-1 R IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.37.1 (FOR A340-300) OR FR.34 (FOR A340-200) AND

FR.47 FROM Y=-2390 TO Y=2390" ADDED AND "FAIRING

PANELS BETWEEN FR 37.1 (FOR

A340-300) OR FR 34 (FOR A340-200) AND FR 47"

REMOVED

DESCRIPTION CHANGED FROM: "BETWEEN FR 37.1 (FOR

A340-300) OR FR 34 (FOR A340-200) AND FR 47", TO:

"LOWER PART BETWEEN FR.37.1 (FOR A340-300) OR

FR.34 (FOR A340-200) AND FR.47 FROM

Y=-2390 TO Y=2390,"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 19

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 533035-01-2 R IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.37.1 (FOR A340-300) OR FR.34 (FOR A340-200) AND

FR.47 FROM Y=-2390 TO Y=2390" ADDED AND "FAIRING

PANELS BETWEEN FR 37.1 (FOR

A340-300) OR FR 34 (FOR A340-200) AND FR 47"

REMOVED

DESCRIPTION CHANGED FROM: "BETWEEN FR 37.1 (FOR

A340-300) OR FR 34 (FOR A340-200) AND FR 47", TO:

"LOWER PART BETWEEN FR.37.1 (FOR A340-300) OR

FR.34 (FOR A340-200) AND FR.47 FROM

Y=-2390 TO Y=2390,"

D-53 533036-01-1 R IN ACCESS: "147AT; 147BT; 148AT; 148BT; 197AB;

197AT; 197FB; 197GB; 197HB" REMOVED

IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.47 AND FR.56 FROM Y=-2390 TO Y=2390." ADDED

DESCRIPTION CHANGED FROM: "BETWEEN FR 47 AND FR

56", TO: "LOWER PART BETWEEN FR.47 AND FR.56 FROM

Y=-2390 TO Y=2390,"

D-53 533036-01-2 R IN ACCESS: "147AT; 147BT; 148AT; 148BT; 197AB;

197AT; 197FB; 197GB; 197HB" REMOVED

IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.47 AND FR.56 FROM Y=-2390 TO Y=2390." ADDED

DESCRIPTION CHANGED FROM: "BETWEEN FR 47 AND FR

56", TO: "LOWER PART BETWEEN FR.47 AND FR.56 FROM

Y=-2390 TO Y=2390,"

D-53 533037-01-1 N NEW TASK ADDED

D-53 533103-02-1 R SAMPLE THRESHOLD: "OR 75000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "7340 FC", TO: "7300

FC OR 49500 FH"

D-53 533104-01-2 R DESCRIPTION CHANGED FROM: "50MM AROUND - UPPER

BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 –

ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN

FR.48 AND FR.49 AND BETWEEN FR.52 AND FR.53,

BETWEEN STRINGER 1 LH AND STRINGER 1 RH - AFIS

ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND

FR.40.1 (IF INSTALLED)", TO: "BETWEEN STRINGER 1LH

AND 1RH 50 MM AROUND: - UPPER BEACON

LIGHT CUTOUT BETWEEN FR.42 AND FR.43 - ADF LOOP

AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 AND

FR.49 AND BETWEEN FR.52 AND FR.53 - AFIS ANTENNA

CUTOUT BETWEEN FR.40 AND FR.40.1 (IF

INSTALLED)."

SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 13800

FH", TO: "7200 FC OR 14400 FH"

D-53 533106-01-1 R SAMPLE INTERVAL CHANGED FROM: "8300 FC OR 16600

FH", TO: "8450 FC OR 16900 FH"

D-53 533107-01-1 R DESCRIPTION CHANGED FROM: "26)", TO: "28)"

SAMPLE THRESHOLD: "OR 60000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "10100 FC", TO:

"10400 FC OR 70600 FH"

D-53 533107-01-2 R DESCRIPTION CHANGED FROM: "26)", TO: "28)"

SAMPLE INTERVAL CHANGED FROM: "12400 FC OR 24800

FH", TO: "12700 FC OR 25400 FH"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 20

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 533113-01-1 R SAMPLE THRESHOLD: "OR 60000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "9100 FC", TO: "9200

FC OR 62300 FH"

D-53 533126-01-1 R DESCRIPTION CHANGED FROM: "AREA AROUND CENTER

LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO AN

EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE", TO:

"SKIN PANEL, AREA AROUND CENTER

LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO AN

EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE."

D-53 533132-02-2 R SAMPLE INTERVAL CHANGED FROM: "9900 FC OR 19800

FH", TO: "9550 FC OR 19100 FH"

D-53 533139-01-1 R SAMPLE THRESHOLD: "OR 75000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "5600 FC", TO: "5550

FC OR 37600 FH"

D-53 533139-01-3 R SAMPLE THRESHOLD: "OR 26000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "8100 FC", TO: "8050

FC OR 16100 FH"

D-53 533145-01-2 D TASK DELETED

D-53 533152-01-2 R SAMPLE THRESHOLD CHANGED FROM: "13000 FC", TO:

"13000 FC NOTE 8"

D-53 533152-01-4 R SAMPLE THRESHOLD CHANGED FROM: "13000 FC", TO:

"13000 FC NOTE 8"

D-53 533154-01-3 R SAMPLE THRESHOLD: "OR 26000 FH" ADDED

SAMPLE INTERVAL CHANGED FROM: "13000 FC", TO:

"13300 FC OR 26600 FH"

D-53 533162-01-1 R SAMPLE THRESHOLD: "OR 60000 FH" ADDED

SAMPLE INTERVAL: "OR 61000 FH" ADDED

D-53 533164-01-1 R DESCRIPTION CHANGED FROM: "FUSELAGE INTERNAL

STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION

AREA OF CANTED DIAPHRAGMS", TO: "MAIN LANDING

GEAR BAY,CANTED DIAPHRAGMS AND CANTED

DIAPHRAGMS JUNCTION"

SAMPLE INTERVAL CHANGED FROM: "7900 FC OR 56500

FH", TO: "8800 FC OR 59600 FH"

D-53 533164-01-2 R DESCRIPTION CHANGED FROM: "FUSELAGE INTERNAL

STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION

AREA OF CANTED DIAPHRAGMS", TO: "MAIN LANDING

GEAR BAY CANTED DIAPHRAGMS AND CANTED

DIAPHRAGMS JUNCTION"

SAMPLE INTERVAL CHANGED FROM: "11000 FC OR 22000

FH", TO: "9900 FC OR 19800 FH"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 21

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 533164-01-3 R DESCRIPTION CHANGED FROM: "FUSELAGE INTERNAL

STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION

AREA OF

CANTED DIAPHRAGMS ON FLOOR BEAMS BETWEENFR",

TO:

"MAIN LANDING GEAR BAY, CANTED

DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON

FLOOR

BEAMS BETWEEN FR"

D-53 533190-01-1 R DESCRIPTION CHANGED FROM:

"(EMERGENCY/PASSENGER/ CREW DOOR) CUT-OUT,

BETWEEN FR 53.4 AND 53.8 FROM CABIN", TO:

"(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,

BETWEEN FR 53.4 AND FR 53.8 FROM MAIN DECK"

D-53 533191-01-1 R DESCRIPTION CHANGED FROM:

"(EMERGENCY/PASSENGER/

CREW DOOR) CUT-OUT, BETWEEN FR 53.4 AND 53.8

FROM

CABIN", TO: "(EMERGENCY/PASSENGER/CREW DOOR)

CUT-OUT, BETWEEN FR 53.4 AND FR 53.8

FROM MAIN DECK"

D-53 533728-01-1 R IN DESCRIPTION: "SPECIAL" ADDED

D-53 533735-01-1 R IN ACCESS: "191AB; 191AT; 191BB; 191BT; 191CB;

191CT; 191FB; 192AT; 192BB; 192BT; 192CB; 192CT;

192GB; 192JB; 193AB; 193BB; 193DB; 195AB; 196AB"

REMOVED IN PREPARATION TASKS: "FAIRING PANELS

BETWEEN FR.37.1 AND FR.47 FROM Y=-2360 TO Y=2360"

ADDEDDESCRIPTION CHANGED FROM: "BETWEEN FR

37.11 AND FR 47", TO: "LOWER PART BETWEEN FR 37.1

AND FR 47 FROM Y=-2360 TO Y=2360,"

APPLICABILITY CHANGED FROM: "A340-500 PRE 51066

ORA340-600 PRE 51066", TO: "A340-500 PRE 51066 AND

PRE 56418 OR A340-600 PRE 51066 AND PRE 56418"

D-53 533735-01-2 R IN ACCESS: "191AB; 191AT; 191BB; 191BT; 191CB;

191CT; 191FB; 192AT; 192BB; 192BT; 192CB; 192CT;

192GB; 192JB; 193AB; 193BB; 193DB; 195AB; 196AB"

REMOVED IN PREPARATION TASKS: "FAIRING PANELS

BETWEEN FR.37.1 AND FR.47 FROM Y=-2360 TO Y=2360"

ADDEDDESCRIPTION CHANGED FROM: "BETWEEN FR

37.11 AND FR 47", TO: "LOWER PART BETWEEN FR 37.1

AND FR 47 FROM Y=-2360 TO Y=2360,"

IN APPLICABILITY: "POST 56418" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 22

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 533736-01-1 R IN ACCESS: "147AT; 147BT; 148AT; 148BT; 197AB;

197AT; 197FB; 197GB; 197HB" REMOVED

IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.47 AND FR.56 FROM Y=-2360 TO Y=2360." ADDED

DESCRIPTION CHANGED FROM: "BETWEEN FR 47 AND FR

56", TO: "LOWER PART BETWEEN FR.47 AND FR.56 FROM

Y=-2360 TO Y=2360,"

APPLICABILITY CHANGED FROM: "A340-500 PRE 51066 OR

A340-600 PRE 51066", TO: "A340-500 PRE 51066 AND

PRE 56418 OR A340-600 PRE 51066 AND PRE 56418"

D-53 533736-01-2 R IN ACCESS: "147AT; 147BT; 148AT; 148BT; 197AB;

197AT; 197FB; 197GB; 197HB" REMOVED

IN PREPARATION TASKS: "FAIRING PANELS BETWEEN

FR.47 AND FR.56 FROM Y=-2360 TO Y=2360." ADDED

DESCRIPTION CHANGED FROM: "BETWEEN FR 47 AND FR

56", TO: "LOWER PART BETWEEN FR.47 AND FR.56 FROM

Y=-2360 TO Y=2360,"

IN APPLICABILITY: "POST 56418" ADDED

D-53 533737-01-1 N NEW TASK ADDED

D-53 534124-01-2 R DESCRIPTION CHANGED FROM: "26 LH/RH TO CROWN

CENTER LINE EXCLUDING AREA UNDER VERTICAL

STABILIZER FAIRING, EXTERNAL SURFACE", TO: "6 TO

STR 26, LH/RH EXCLUDING AREA UNDER VERTICAL

STABILIZER FAIRING, EXTERNAL SURFACE."

D-53 534128-01-1 R DESCRIPTION CHANGED FROM: "CABIN FLOOR

INCLUDING CABIN", TO: "MAIN DECK FLOOR INCLUDING

MAIN DECK"

D-53 534133-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 534134-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 534140-02-1 R IN DESCRIPTION: "AND" ADDED

D-53 534157-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 534158-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN

FLOOR PANELS AND CARGO COMPARTMENT FLOOR

FROM FR 53.2 TO FR 73, INCLUDING PASSENGER CABIN",

TO: "MAIN DECK FLOOR PANELS AND CARGO

COMPARTMENT FLOOR FROM FR 53.2 TO FR 73,

INCLUDING MAIN DECK"

D-53 534159-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 534159-01-2 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 534161-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

D-53 534162-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 23

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 534177-01-2 N NEW TASK ADDED

D-53 534224-01-1 R DESCRIPTION CHANGED FROM: "26 TO CROWN CROWN

CENTER LINE,", TO: "6 TO STR 26,"

D-53 534261-02-1 R DESCRIPTION CHANGED FROM: "53.1", TO: "56.1"

D-53 534277-01-1 N NEW TASK ADDED

D-53 535101-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 535102-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

D-53 535103-01-1 R DESCRIPTION CHANGED FROM: "STRINGERS", TO: "STR"

D-53 535104-01-1 R DESCRIPTION CHANGED FROM: "STRINGERS", TO: "STR"

D-53 535111-01-1 R DESCRIPTION CHANGED FROM: "29", TO: "27"

D-53 535121-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE" IN

ZIP-REFERENCE(S): "ZL-271-02-1; ZL-273-01-1"

ADDED

D-53 535122-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

100% THRESHOLD CHANGED FROM: "5 YE", TO: "6 YE"

100% INTERVAL CHANGED FROM: "5 YE", TO: "6 YE"

IN ZIP-REFERENCE(S): "ZL-171-02-1" ADDED

D-53 535123-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

IN ZIP-REFERENCE(S): "ZL-311-01-1" ADDED

D-53 535124-01-1 R 100% THRESHOLD CHANGED FROM: "5 YE", TO: "6 YE"

100% INTERVAL CHANGED FROM: "5 YE", TO: "6 YE"

D-53 535129-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

D-53 535130-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN DECK"

100% THRESHOLD CHANGED FROM: "5 YE", TO: "6 YE"

100% INTERVAL CHANGED FROM: "5 YE", TO: "6 YE"

D-53 535131-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

D-53 535201-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

D-53 535203-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 24

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-53 535219-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

D-53 535220-01-1 R 100% THRESHOLD CHANGED FROM: "5 YE", TO: "6 YE"

100% INTERVAL CHANGED FROM: "5 YE", TO: "6 YE"

D-53 535221-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "12 YE"

100% INTERVAL CHANGED FROM: "10 YE", TO: "12 YE"

D-54 545104-01-7 R IN PREPARATION TASKS: "FASTENERS TO BE REMOVED"

REMOVED SAMPLE INTERVAL CHANGED FROM: "6000 FC

OR 29900 FH", TO: "4100 FC OR 27600 FH"

D-54 545104-01-8 R IN PREPARATION TASKS: "FASTENERS TO BE REMOVED"

REMOVED SAMPLE INTERVAL CHANGED FROM: "5460 FC

OR 36900 FH", TO: "4100 FC OR 27600 FH"

D-54 545146-01-1 D TASK DELETED

D-54 545146-01-2 D TASK DELETED

D-54 545174-01-1 D TASK DELETED

D-54 545174-01-2 D TASK DELETED

D-54 545174-01-4 D TASK DELETED

D-54 545174-01-5 D TASK DELETED

D-55 551018-01-2 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE

WATER SYSTEM PIPE" REMOVED

CPCP: "CPCP" REMOVED

IN ZIP-REFERENCE(S): "ZL-319-02-2" REMOVED

D-55 551029-01-2 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE

WATER SYSTEM PIPE" REMOVED

D-55 551029-02-2 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE

WATER SYSTEM PIPE" REMOVED

D-55 551035-01-1 R IN ACCESS: "332AB; 332AT" ADDED AND "334GB"

REMOVED IN PREPARATION TASKS: "PEELABLE HOLE

COVERS" ADDED APPLICABILITY CHANGED FROM: "A340-

200 PRE 43491 OR A340-300 PRE 43491", TO: "A340-200

POST 41471 PRE 43491 OR A340-300 POST 41471 PRE

43491"

D-55 551035-01-2 R IN PREPARATION TASKS: "PEELABLE HOLE COVERS"

ADDED

D-55 551035-01-3 R IN PREPARATION TASKS: "PEELABLE HOLE COVERS"

ADDED

D-55 551035-01-4 N NEW TASK ADDED

D-55 551035-02-1 R IN PREPARATION TASKS: "PEELABLE HOLE COVERS"

ADDED APPLICABILITY CHANGED FROM: "A340-200 POST

43491 PRE 44818 OR A340-300 POST 43491 PRE 44818",

TO: "A340-200 PRE 41471 OR POST 43491 PRE 44818 OR

A340-300 PRE 41471"

D-55 552001-01-1 R IN ZIP-REFERENCE(S): "ZL-300-01-1" ADDED

D-55 553074-01-1 R IN ACCESS: "323EL" ADDED AND "323CL" REMOVED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 25

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-55 554001-01-1 R IN DESCRIPTION: "INCLUDING TRAILING EDGE," REMOVED

IN ZIP-REFERENCE(S): "ZL-300-01-1" ADDED

D-55 554003-01-1 R IN PREPARATION TASKS: "PEELABLE HOLE COVERS"

ADDED DESCRIPTION CHANGED FROM: "DETAILED

INSPECTION OF RUDDER FRONT SPAR FORWARD FACE

AND INTERNAL STRUCTURE AS FAR AS VISIBLE", TO:

"SPECIAL DETAILED INSPECTION OF RUDDER FRONT

SPAR"

D-55 554003-01-2 R IN PREPARATION TASKS: "PEELABLE HOLE COVERS"

ADDED IN DESCRIPTION: "FORWARD FACE AND

INTERNAL STRUCTURE AS FAR AS VISIBLE" REMOVED

100% THRESHOLD CHANGED FROM: "6 YE", TO: "12 YE"

D-55 554005-01-1 D TASK DELETED

D-55 554005-02-1 D TASK DELETED

D-55 554009-01-1 N NEW TASK ADDED

D-55 554010-01-1 N NEW TASK ADDED

D-55 554010-01-2 N NEW TASK ADDED

D-55 554011-01-1 N NEW TASK ADDED

D-55 554012-01-1 N NEW TASK ADDED

D-55 554012-01-2 N NEW TASK ADDED

D-55 554013-01-1 N NEW TASK ADDED

D-55 554014-01-1 N NEW TASK ADDED

D-55 554070-01-1 R IN DESCRIPTION: "INCLUDING TRAILING EDGE," REMOVED

IN ZIP-REFERENCE(S): "ZL-300-01-2" ADDED

D-55 554071-01-1 R IN DESCRIPTION: "FORWARD FACE AND INTERNAL

STRUCTURE AS FAR AS VISIBLE" REMOVED

100% THRESHOLD CHANGED FROM: "6 YE", TO: "12 YE"

D-55 554072-01-1 D TASK DELETED

D-55 554073-01-1 R IN DESCRIPTION: "AND ACTUATOR ATTACHMENTS"

REMOVED

D-55 554074-01-1 N NEW TASK ADDED

D-55 554075-01-1 N NEW TASK ADDED

D-55 554076-01-1 N NEW TASK ADDED

D-55 554077-01-1 N NEW TASK ADDED

D-55 554078-01-1 N NEW TASK ADDED

D-55 554079-01-1 N NEW TASK ADDED

D-56 562101-01-1 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN", TO:

"MAIN DECK"

D-57 571103-01-2 D TASK DELETED

D-57 571103-02-2 D TASK DELETED

D-57 571107-01-3 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 12200

FH", TO: "4900 FC OR 9850 FH"

D-57 571108-01-3 R SAMPLE INTERVAL CHANGED FROM: "6000 FC OR 41900

FH", TO: "5900 FC OR 40000 FH"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 26

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 571108-01-4 R SAMPLE INTERVAL CHANGED FROM: "8400 FC OR 16800

FH", TO: "6700 FC OR 13400 FH"

D-57 571114-01-4 D TASK DELETED

D-57 571116-01-3 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 12200

FH", TO: "4900 FC OR 9850 FH"

D-57 571118-01-5 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 12200

FH", TO: "4900 FC OR 9850 FH"

D-57 571122-01-3 R SAMPLE INTERVAL CHANGED FROM: "5800 FC OR 11600

FH", TO: "4650 FC OR 9350 FH"

D-57 571125-01-1 R SAMPLE THRESHOLD CHANGED FROM: "60000 FH", TO:

"75000 FH"

SAMPLE INTERVAL CHANGED FROM: "4370 FC OR 21800

FH", TO: "3850 FC OR 26000 FH"

D-57 571125-01-2 R SAMPLE INTERVAL CHANGED FROM: "5200 FC OR 10400

FH", TO: "4200 FC OR 8400 FH"

D-57 571126-01-2 D TASK DELETED

D-57 571133-01-2 R SAMPLE THRESHOLD CHANGED FROM: "60000 FH", TO:

"75000 FH"

SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 42600

FH", TO: "4700 FC OR 31900 FH"

D-57 571133-01-3 R SAMPLE INTERVAL CHANGED FROM: "11300 FC OR 22600

FH", TO: "5450 FC OR 10900 FH"

D-57 571146-02-1 R SAMPLE INTERVAL CHANGED FROM: "9600 FC OR 60000

FH", TO: "9500 FC OR 64100 FH"

D-57 571146-02-3 D TASK DELETED

D-57 571149-01-3 R SAMPLE INTERVAL CHANGED FROM: "8000 FC OR 16000

FH", TO: "7200 FC OR 14400 FH"

D-57 571152-01-1 R SAMPLE THRESHOLD CHANGED FROM: "60000 FH", TO:

"75000 FH"

SAMPLE INTERVAL CHANGED FROM: "6700 FC OR 33600

FH", TO: "5900 FC OR 40000 FH"

D-57 571153-01-4 R SAMPLE INTERVAL CHANGED FROM: "13000 FC OR 26000

FH", TO: "6000 FC OR 12000 FH"

D-57 571153-01-6 R SAMPLE INTERVAL CHANGED FROM: "13000 FC OR 60000

FH", TO: "6000 FC OR 40700 FH"

D-57 572002-01-7 R SAMPLE THRESHOLD CHANGED FROM: "13000 FC OR

60000

FH", TO: "13000 FC OR 60000 FH NOTE 8"

D-57 572154-01-4 N NEW TASK ADDED

D-57 572617-01-1 N NEW TASK ADDED

D-57 574301-01-1 R DESCRIPTION CHANGED FROM: "AREA", TO: "AREA."

D-57 574301-01-2 R DESCRIPTION CHANGED FROM: "AREA", TO: "AREA."

D-57 574301-01-3 R DESCRIPTION CHANGED FROM: "AREA", TO: "AREA."

D-57 574303-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574303-02-1 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 27

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574304-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574304-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574304-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574304-02-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574304-02-2 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574304-02-3 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574304-03-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH NOTE:

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

AS TASK 574304-01-1", TO: "EXTERNAL,LH/RH. NOTE: THIS

TASK MAY BE PERFORMED AT THE

SAME TIME AS TASK 574304-01-1."

D-57 574305-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574306-02-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE"

D-57 574307-01-1 R IN PREPARATION TASKS: "REMOVAL OF THE BOLTS ONE

AT A TIME." ADDED AND "BOLTS SUCCESSIVELY"

REMOVED IN ZONE: "511; 611" ADDED AND "521; 621"

REMOVED DESCRIPTION CHANGED FROM: "LH/RH", TO:

"LH/RH."

D-57 574308-01-1 R TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574353-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574354-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574354-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574354-03-1."

D-57 574354-03-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH NOTE:

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

TASK 574354-01-1", TO: "EXTERNAL,LH/RH. NOTE: THIS

TASK MAY BE PERFORMED AT THE

SAME TIME AS TASK 574354-01-1."

D-57 574356-02-1 R DESCRIPTION CHANGED FROM: "1 TRAILING EDGE,

LOWER

FACE, 100 MM FORWARD OF AFT", TO: "1, TRAILING

EDGE LOWER FACE, 100 MM FROM LEFT"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 28

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574357-01-1 R IN ACCESS: "521CB; 521FB; 621CB; 621FB" ADDED AND

"521DB; 521GB; 621DB; 621GB" REMOVED

IN PREPARATION TASKS: "REMOVAL OF THE BOLTS ONE

AT A TIME." ADDED AND "BOLTS SUCCESSIVELY"

REMOVED DESCRIPTION CHANGED FROM: "BOLTS

LH/RH", TO:

"BOLTS, LH/RH."

D-57 574401-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574401-01-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574401-01-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574401-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574403-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574403-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574404-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574404-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574404-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574404-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574404-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574404-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574404-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574404-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574404-01-1."

D-57 574405-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574407-01-1 N NEW TASK ADDED

D-57 574451-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574453-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574454-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574454-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574454-03-1."

D-57 574454-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574454-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574454-01-1."

D-57 574455-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574456-01-1 R DESCRIPTION CHANGED FROM: "2 TRAILING EDGE

LOWER FACE, 100 MM FORWARD OF AFT EDGE", TO: "2,

TRAILING EDGE LOWER FACE, 100 MM FROM AFT EDGE,"

D-57 574457-01-1 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 29

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574501-01-1 R DESCRIPTION CHANGED FROM: "8 ; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: "8, VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

D-57 574501-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574501-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574501-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574501-02-4 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574503-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574504-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574504-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574504-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574504-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574504-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574504-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574504-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574504-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574504-01-1."

D-57 574505-01-1 R IN ZONE: "512; 612" ADDED AND "513; 613" REMOVED

DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574506-02-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE"

D-57 574507-01-2 N NEW TASK ADDED

D-57 574551-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574553-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574554-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574554-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574554-03-1."

D-57 574554-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574554-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574554-01-1."

D-57 574555-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574556-02-1 R DESCRIPTION CHANGED FROM: "EDGE, LOWER FACE, 100

MM FORWARD OF", TO: "EDGE LOWER FACE, 100 MM

FROM"

D-57 574557-01-1 N NEW TASK ADDED

D-57 574558-02-1 N NEW TASK ADDED

D-57 574601-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574601-01-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 30

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574601-01-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574601-02-1 R DESCRIPTION CHANGED FROM: "10 ; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: "10, VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

D-57 574603-01-1 R DESCRIPTION CHANGED FROM: "TO 10 ATTACHMENTS,

INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS

AND LINK PLATE, LH/RH", TO: "& 10 ATTACHMENTS

INCLUDING TRACK RIB LUGS, TRACK LUGS,

BOLTS, LINKS AND LINK PLATE, LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574604-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574604-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574604-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574604-02-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574604-02-2 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574604-02-3 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH."

D-57 574604-03-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH NOTE:

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

TASK 574604-01-1", TO: "EXTERNAL,LH/RH. NOTE: THIS

TASK MAY BE PERFORMED AT THE

SAME TIME AS TASK 574604-01-1."

D-57 574605-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574606-02-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE"

D-57 574607-01-1 N NEW TASK ADDED

D-57 574651-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574653-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574654-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574654-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574654-03-1."

D-57 574654-03-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH NOTE:

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

TASK 574654-01-1", TO: "EXTERNAL,LH/RH. NOTE: THIS

TASK MAY BE PERFORMED AT THE

SAME TIME AS TASK 574654-01-1."

D-57 574655-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 31

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574656-02-1 R DESCRIPTION CHANGED FROM: "4 TRAILING EDGE,

LOWER

FACE, 100 MM FORWARD OF AFT EDGE", TO: "4,

TRAILING EDGE LOWER FACE, 100 MM FROM AFT EDGE,"

D-57 574657-01-1 N NEW TASK ADDED

D-57 574701-01-1 R DESCRIPTION CHANGED FROM: "12 ; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: "12, VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

D-57 574701-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574701-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574701-02-4 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574703-01-1 R DESCRIPTION CHANGED FROM: "ATTACHMENTS,

INCLUDING

TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK

PLATE, LH/RH", TO: "ATTACHMENTS INCLUDING TRACK

RIB LUGS, TRACK LUGS, BOLTS,

LINKS AND LINK PLATE, LH/RH."

D-57 574704-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574704-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574704-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574704-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574704-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574704-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574704-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574704-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574704-01-1."

D-57 574705-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574707-01-1 N NEW TASK ADDED

D-57 574708-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574751-01-1 R DESCRIPTION CHANGED FROM: "; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: ", VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574753-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574754-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574754-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574754-03-1."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 32

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574754-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574754-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574754-01-1."

D-57 574755-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574756-02-1 R DESCRIPTION CHANGED FROM: "5 TRAILING EDGE,

LOWER

FACE, 100 MM FORWARD OF AFT EDGE", TO: "5,

TRAILING EDGE LOWER FACE, 100 MM FROM AFT EDGE,"

D-57 574757-01-1 N NEW TASK ADDED

D-57 574758-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574801-01-1 R DESCRIPTION CHANGED FROM: "14 ; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: "14, VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

D-57 574801-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574801-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574801-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574803-01-1 R DESCRIPTION CHANGED FROM: "ATTACHMENTS,

INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS

AND LINK PLATE, LH/RH", TO: "ATTACHMENTS INCLUDING

TRACK RIB LUGS, TRACK LUGS, BOLTS,

LINKS AND LINK PLATE, LH/RH."

D-57 574804-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574804-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574804-03-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574804-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574804-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574804-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574804-02-4 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574804-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574804-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574804-01-1."

D-57 574805-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574806-02-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE"

D-57 574807-01-1 N NEW TASK ADDED

D-57 574851-01-1 R DESCRIPTION CHANGED FROM: "; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: ", VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574853-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 33

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574854-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574854-03-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574854-03-1."

D-57 574854-03-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574854-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574854-01-1."

D-57 574855-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574856-02-1 R DESCRIPTION CHANGED FROM: "6 TRAILING EDGE,

LOWER

FACE, 100 MM FORWARD OF AFT EDGE", TO: "6,

TRAILING EDGE LOWER FACE, 100 MM FROM AFT EDGE,"

D-57 574857-01-1 N NEW TASK ADDED

D-57 574901-01-1 R DESCRIPTION CHANGED FROM: "; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: ";VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH."

D-57 574901-02-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574901-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574901-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574903-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574904-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574904-02-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574904-02-1."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574904-02-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574904-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574904-01-1."

D-57 574904-02-2 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574904-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574904-02-4 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574905-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

D-57 574906-02-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE"

D-57 574907-01-1 N NEW TASK ADDED

D-57 574951-01-1 R DESCRIPTION CHANGED FROM: "17; VISIBLE PART OF

ROLLER CONTACT AREA, LH/RH", TO: "17, VISIBLE PART

OF ROLLER CONTACT AREA, LH/RH."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 574953-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 34

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 574954-01-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574954-02-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574954-02-1."

D-57 574954-02-1 R DESCRIPTION CHANGED FROM: "LH/RH NOTE: THIS TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

574954-01-1", TO: "LH/RH. NOTE: THIS TASK MAY BE

PERFORMED AT THE SAME TIME AS TASK

574954-01-1."

D-57 574956-02-1 R DESCRIPTION CHANGED FROM: "7 TRAILING EDGE,

LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH.",

TO: "7, TRAILING EDGE, LOWER FACE, 100 MM FROM AFT

EDGE,H/RH."

D-57 574957-01-1 N NEW TASK ADDED

D-57 575054-01-1 R DESCRIPTION CHANGED FROM: "BOX SUPPORT, FORK

ASSY,

DRIVE STRUT AND CARRIAGE", TO: "BOX, FORK ASSY,

DRIVE STRUT AND CARRIAGE."

D-57 575059-01-1 R DESCRIPTION CHANGED FROM: "NO.4", TO: "NO.4."

D-57 575061-01-1 R DESCRIPTION CHANGED FROM: "ASSEMBLIES", TO:

"ASSEMBLIES."

APPLICABILITY CHANGED FROM: "GROUP 43A OR GROUP

43B OR GROUP 43C", TO: "A340-300"

D-57 575065-01-1 R DESCRIPTION CHANGED FROM: "STRUCTURE", TO:

"STRUCTURE."

D-57 575067-01-1 R IN PREPARATION TASKS: "FS BOLTS" REMOVED

DESCRIPTION CHANGED FROM: "NO.2, 3, 4 AND 5,

FORWARD ATTACHMENT SPIGOTS.", TO: "NO.2,3,4 AND 5,

FORWARD ATTACHMENT SPIGOTS,EXTERNAL

STRUCTURE."

D-57 575067-02-1 R DESCRIPTION CHANGED FROM: "SPIGOTS. INTERNAL

STRUCTURE", TO: "SPIGOTS, INTERNAL STRUCTURE."

D-57 575069-01-1 R TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 575074-01-1 R DESCRIPTION CHANGED FROM: "NO 1,", TO: "NO.1,"

D-57 575075-01-1 R DESCRIPTION CHANGED FROM: "NO 1, ATTACHMENTS",

TO:

"NO.1, ATTACHMENT"

D-57 575079-01-1 R DESCRIPTION CHANGED FROM: "NO 2, 3, 4 AND 5, DRIVE

ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE

ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND

TRAVELING BEAM AT TRACK NO 4.", TO:

"NO.2, 3, 4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE

ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT

SUPPORT LINK AND TRAVELING BEAM AT TRACK NO.4."

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 575081-01-1 R DESCRIPTION CHANGED FROM: "NO 2,", TO: "NO.2,"

# A340 MRB REPORT

Issue : July 2010 SOC Page : 35

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 575083-01-1 R DESCRIPTION CHANGED FROM: "NO 2,", TO: "NO.2,"

D-57 575085-01-1 R DESCRIPTION CHANGED FROM: "NO 2,", TO: "NO.2,"

D-57 575087-01-1 R DESCRIPTION CHANGED FROM: "NO 2,", TO: "NO.2,"

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 575087-02-1 R DESCRIPTION CHANGED FROM: "NO 2,", TO: "NO.2,"

D-57 575089-01-1 R DESCRIPTION CHANGED FROM: "NO 2, 3, 4 AND 5, AFT

ATTACHMENT SPIGOTS", TO: "NO.2, 3, 4 AND 5, AFT

ATTACHMENT SPIGOTS."

D-57 575403-01-1 R DESCRIPTION CHANGED FROM: "EXTERNAL NOTE : TASK

MUST BE PERFORMED AT THE SAME TIME AS TASK

575403-02-2", TO: "EXTERNAL."

D-57 575403-02-1 R DESCRIPTION CHANGED FROM: "INTERNAL", TO:

"INTERNAL."

D-57 575404-01-1 N NEW TASK ADDED

D-57 575404-03-1 N NEW TASK ADDED

D-57 575404-03-2 N NEW TASK ADDED

D-57 575405-01-1 R DESCRIPTION CHANGED FROM: "BRACKET", TO:

"BRACKET."

D-57 575405-01-3 R IN ACCESS: "531AT; 531CB; 631AT; 631CB" ADDED AND

"531SB; 531VT; 631SB; 631VT" REMOVED

DESCRIPTION CHANGED FROM: "BRACKET", TO:

"BRACKET."

D-57 575405-02-1 R DESCRIPTION CHANGED FROM: "NO.2", TO: "NO.2."

D-57 575405-02-2 R IN ACCESS: "531AT; 531CB; 631AT; 631CB" ADDED AND

"531SB; 531VT; 631SB; 631VT" REMOVED

DESCRIPTION CHANGED FROM: "NO.2", TO: "NO.2."

D-57 575407-01-1 R TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 575409-01-1 R DESCRIPTION CHANGED FROM: "STRUCTURE", TO:

"STRUCTURE."

D-57 575451-01-1 R DESCRIPTION CHANGED FROM: "SKIN", TO: "SKIN."

D-57 575453-01-1 R DESCRIPTION CHANGED FROM: "NO1", TO: "NO.1"

D-57 575453-02-1 R DESCRIPTION CHANGED FROM: "NO1 AND TRUNION,

INTERNAL", TO: "NO.1 AND TRUNION, INTERNAL."

D-57 575454-01-1 N NEW TASK ADDED

D-57 575454-03-1 N NEW TASK ADDED

D-57 575455-01-1 R DESCRIPTION CHANGED FROM: "NO2 AND EXTERNAL

DRIVE STRUT BRACKET, CARRIAGE ATTACHMENT

BRACKET AND GUIDE ARM ATTACHMENT BRACKET.", TO:

"NO.2 AND EXTERNAL DRIVE STRUT BRACKET,

CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM

ATTACHMENT BRACKET. NOTE: THIS TASK MUST BE

PERFORMED AT THE SAME TIME AS TASK 575455-02-01."

D-57 575455-02-1 R IN PREPARATION TASKS: "PLUGS" REMOVED

DESCRIPTION CHANGED FROM: "NO2", TO: "NO. 2."

D-57 575459-01-1 R DESCRIPTION CHANGED FROM: "STRUCTURE", TO:

"STRUCTURE."

D-57 575501-01-2 N NEW TASK ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 36

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 575503-01-1 R DESCRIPTION CHANGED FROM: "FITTING", TO:

"FITTING."

D-57 575503-02-1 R DESCRIPTION CHANGED FROM: "NO.3", TO: "NO.3."

D-57 575505-01-1 R DESCRIPTION CHANGED FROM: "FWD. SUPPORT LINK

AND AFT SUPPORT LINK ATTACH FITTING", TO: "FWD

SUPPORT LINK AND AFT SUPPORT LINK ATTACH

FITTING."

D-57 575505-02-1 R DESCRIPTION CHANGED FROM: "NO.4", TO: "NO.4."

D-57 575507-01-1 R IN ACCESS: "533AT; 533CB; 633AT; 633CB" ADDED AND

"534AT; 534CB; 634AT; 634CB" REMOVED

DESCRIPTION CHANGED FROM: "FITTING", TO:

"FITTING."

D-57 575507-02-1 R IN ACCESS: "533AT; 533CB; 633AT; 633CB" ADDED AND

"534AT; 534CB; 634AT; 634CB" REMOVED

DESCRIPTION CHANGED FROM: "NO.5", TO: "NO.5."

D-57 575551-01-1 R DESCRIPTION CHANGED FROM: "RH/LH", TO: "RH/LH."

D-57 575553-01-1 R DESCRIPTION CHANGED FROM: "NO3,", TO: "NO. 3,"

D-57 575553-02-1 R IN PREPARATION TASKS: "PLUGS" REMOVED

DESCRIPTION CHANGED FROM: "NO3", TO: "NO. 3."

D-57 575555-01-1 R DESCRIPTION CHANGED FROM: "FLAP INTERNAL

SUPPORT FITTING AT TRACK NO4,", TO: "FLAP, INTERNAL

SUPPORT FITTING AT TRACK NO. 4,"

TPS: "TPS MUST NOT BE APPLIED" ADDED

D-57 575555-02-1 R IN PREPARATION TASKS: "PLUGS" REMOVED

DESCRIPTION CHANGED FROM: "FLAP INTERNAL

SUPPORT FITTING AT TRACK NO4", TO: "FLAP, INTERNAL

SUPPORT FITTING AT TRACK NO. 4."

D-57 575557-01-1 R IN ACCESS: "533SB; 533VT; 633SB; 633VT" ADDED AND

"534SB; 534VT; 634SB; 634VT" REMOVED

DESCRIPTION CHANGED FROM: "NO5,", TO: "NO. 5,"

D-57 575557-02-1 R IN ACCESS: "533SB; 533VT; 633SB; 633VT" ADDED AND

"534SB; 534VT; 634SB; 634VT" REMOVED

IN PREPARATION TASKS: "PLUGS" REMOVED

DESCRIPTION CHANGED FROM: "NO5", TO: "NO. 5."

D-57 577001-01-1 R DESCRIPTION CHANGED FROM: "SURFACE. LH/RH", TO:

"SURFACE, LH/RH."

CPCP: "CPCP" REMOVED

D-57 577003-01-1 R DESCRIPTION CHANGED FROM: "FITTINGS (6 PLACES)",

TO: "FITTINGS."

D-57 577051-01-1 R IN PREPARATION TASKS: "SPOILERS DEPLOYED" ADDED

AND "SPOILERS EXTENDED" REMOVED

DESCRIPTION CHANGED FROM: "NO 1 TO 2, UPPER AND

LOWER SKIN, EXTERNAL SURFACE", TO: "NO. 1 AND 2,

UPPER AND LOWER SKIN, EXTERNAL SURFACE."

# A340 MRB REPORT

Issue : July 2010 SOC Page : 37

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGE

D-57 577053-01-1 R IN PREPARATION TASKS: "SPOILERS DEPLOYED" ADDED

AND "SPOILERS EXTENDED" REMOVED

DESCRIPTION CHANGED FROM: "NO.1AND NO.2, HINGE

AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES)", TO:

"NO.1 AND NO.2, HINGE AND ACTUATOR ATTACHMENT

FITTINGS (6 PLACES)."

SECTION E

Page E-INTRO-1 1 GENERAL : last paragraph, “wiring” changed to “EWIS”

Page E-INTRO-2 1 GENERAL : last paragraph “identified with “(EWIS)” after the task description”

text added.

"This practice overrides any requirement to identify each task individually with

(EZAP) in each task description.” text deleted

2. COMPATIBILITY WITH SYSTEMS AND STRUCTURES SECTIONS : second

paragraph reworded to refer to “(EWIS)” identifier after tasks.

ZONAL SECTION

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-100 ZL-110-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-121-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-121-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-121-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-121-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-121-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-123-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-123-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.51.01/05; 25.51.01/06;

25.51.01/07; 25.51.01/09; 25.51.01/11;

25.51.01/12; 25.51.01/13; 25.51.01/14;

25.51.01/15" ADDED

E-100 ZL-131-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-131-03-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-133-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.52.00/05" ADDED

E-100 ZL-133-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-137-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-137-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-137-01-3 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 38

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-100 ZL-141-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-141-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-143-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-145-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-147-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-147-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-149-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-149-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-149-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.51.01/05; 25.51.01/06;

25.51.01/07; 25.51.01/09; 25.51.01/11;

25.51.01/12; 25.51.01/13; 25.51.01/14;

25.51.01/15" ADDED AND "25.51.00/10" REMOVED

E-100 ZL-151-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-02-4 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-03-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-151-03-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-153-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.52.00/05" ADDED

E-100 ZL-153-01-2 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.52.00/05" ADDED

E-100 ZL-153-01-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-155-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-161-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.54.00/04; 25.54.00/05;

25.54.00/06" REMOVED

E-100 ZL-161-02-1 R UN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-161-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-161-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-161-03-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-163-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.52.00/05" ADDED

E-100 ZL-163-01-2 R IN TASK TITLE: "(EWIS)" ADDED

IN MSI-REFERENCE(S): "25.52.00/05" ADDED

E-100 ZL-171-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-171-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-171-01-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-171-02-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "535122-01-1" ADDED

E-100 ZL-171-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-171-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-191-01-1 R UN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-191-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-191-02-1 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 39

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-100 ZL-191-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-193-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-193-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-193-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-193-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-195-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-195-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-195-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-197-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-197-02-1 R UN TASK TITLE: "(EWIS)" ADDED

E-100 ZL-197-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-200-01-1 R IN SSI-REFERENCE(S): "532166-01-2; 534177-01-2"

ADDED

E-200 ZL-200-01-2 R IN SSI-REFERENCE(S): "532266-01-1; 534277-01-1"

ADDED

E-200 ZL-211-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-211-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-211-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-221-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-221-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-223-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-223-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-231-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-231-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-233-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-233-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-241-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-241-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-243-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-243-01-2 R TASK TITLE CHANGED FROM: "COMPARTMENT", TO:

"COMPARTMEN (EWIS)"

E-200 ZL-251-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-251-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-251-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-253-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-253-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-253-01-3 R TASK TITLE CHANGED FROM: "COMPARTMENT", TO:

"COMPARTMEN (EWIS)"

E-200 ZL-261-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-261-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-261-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-263-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-263-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-263-01-3 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 40

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-200 ZL-271-02-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "535121-01-1" ADDED

E-200 ZL-271-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-273-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "535121-01-1" ADDED

E-200 ZL-273-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-200 ZL-273-01-3 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-300-01-1 R IN SSI-REFERENCE(S): "552001-01-1; 554001-01-1;

554014-01-1" ADDED

E-300 ZL-300-01-2 R IN SSI-REFERENCE(S): "554070-01-1; 554079-01-1"

ADDED

E-300 ZL-311-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "535123-01-1" ADDED

E-300 ZL-311-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-313-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-313-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-315-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-317-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-317-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-319-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-319-02-2 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE

WATER SYSTEM PIPE" REMOVED

IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "551018-01-2" REMOVED

E-300 ZL-319-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-321-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-322-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-322-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-323-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-323-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-323-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-323-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-324-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-324-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-325-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-325-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-325-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-325-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-03-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-03-3 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-326-04-1 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 41

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-300 ZL-331-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-331-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-332-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-332-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-333-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-333-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-333-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-333-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-334-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-334-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-334-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-334-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-335-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-335-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-335-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-335-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-337-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-337-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-346-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-300 ZL-346-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-411-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-411-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-411-04-2 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-412-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-412-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-413-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-413-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-414-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-414-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-415-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-415-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-417-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-417-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-419-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-451-01-1 R IN ACCESS: "451AL; 461AL; 471AL; 481AL" REMOVED

IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-451-04-1 R IN ACCESS: "451AL; 461AL; 471AL; 481AL" REMOVED

IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-452-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-452-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-452-01-4 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-452-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-453-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-453-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-01-2 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 42

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-400 ZL-454-01-3 R IN ACCESS: "484KR" ADDED AND "484AR" REMOVED

IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-02-3 R IN ACCESS: "484KR" ADDED AND "484AR" REMOVED

IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-454-04-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-500-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-500-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-500-02-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "572138-01-1; 572139-01-1"

REMOVED

E-500 ZL-500-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-521-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-521-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-522-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-522-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-523-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-523-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-531-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-531-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-531-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-531-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-535-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-535-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-541-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-541-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-541-03-1 R IN ACCESS: "541CB; 541DB; 541DZ; 541EB; 541EZ;

541FB; 541FZ; 541GB; 541GZ; 541HB; 541JB; 541KB;

541LB; 541MB; 541NB; 541PB; 541QB; 541RB; 541SB;

641CB; 641DB; 641DZ; 641EB; 641EZ;

641FB; 641FZ; 641GB; 641GZ; 641HB; 641JB; 641KB;

641LB; 641MB; 641NB; 641PB; 641QB; 641RB; 641SB"

REMOVED

IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-542-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-542-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-543-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-550-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-550-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-571-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-571-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-572-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-572-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-573-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-573-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-574-01-1 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 43

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-500 ZL-574-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-575-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-575-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-591-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-500 ZL-592-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-711-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-713-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-713-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-715-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-715-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-731-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-732-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-732-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-733-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-733-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-734-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-734-01-2 R UN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-751-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-751-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-753-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-753-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-755-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-700 ZL-755-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-811-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-811-01-2 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-821-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523101-01-2" ADDED

E-800 ZL-821-01-2 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523121-01-2" ADDED

E-800 ZL-821-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-821-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-822-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523201-01-2" ADDED

E-800 ZL-822-01-2 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523221-01-2" ADDED

E-800 ZL-822-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-822-03-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-823-01-1 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523301-01-1" ADDED

E-800 ZL-823-01-2 R IN TASK TITLE: "(EWIS)" ADDED

IN SSI-REFERENCE(S): "523321-01-2" ADDED

E-800 ZL-823-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-823-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-831-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-831-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-832-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-832-02-1 R IN TASK TITLE: "(EWIS)" ADDED

# A340 MRB REPORT

Issue : July 2010 SOC Page : 44

SECTION TASK

NUMBER REV

CODE SUMMARY OF CHANGES

E-800 ZL-833-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-833-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-834-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-834-02-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-834-02-2 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-834-02-3 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-836-01-1 R IN TASK TITLE: "(EWIS)" ADDED

E-800 ZL-836-02-1 R IN TASK TITLE: "(EWIS)" ADDED

SECTION F

No change.

APPENDIX 1

Last sentence changed from

“Airbus advises the availability of new revisions of the ALS Parts by issuance of an Operator Information

Telex (OIT) that provides guidance on downloading the document from AirbusWorld.”

to

“The availability of new revisions of the ALS Parts is announced by an email, sent by the ALS tool, to those

AirbusWorld subscribers who have chosen to receive automatic notifications.”

APPENDIX 2

No change.

APPENDIX 3

No change.

APPENDIX 4

No change.

APPENDIX 5

To be updated for meetings leading up to MRBR rev 12.

APPENDIX 6

No change.

APPENDIX 7

New abbreviations added on pages APX 7.1, APX 7.2, APX 7.3, APX 7.4.

# A340 MRB REPORT

Issue : July 2010 SOC Page : 45 APPENDIX 8

No change.

APPENDIX 9

No change .

APPENDIX 10

The MODIFICATION REFERENCE LIST has been updated to include the following modifications:

41471 STABILIZERS-HORIZONTAL STABILIZER- MODIFY FRONT SPAR

43719 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - INSTALL

COMPARTMENT DRAINAGE

44001 FUEL - TANKS - DEFINE SINGLE ACT FULL PROVISIONS TO SUIT A340-200

44003 FUEL - TANKS - INSTALL FULL PROVISION FOR A THIRD ADDITIONAL CENTRE

TANK

44004 FUEL - TANKS - INSTALL FULL PROVISIONS FOR A SECOND ADDITIONAL

CENTRE TANK

44440 WINGS - CENTER WING - MODIFY LOWER KEEL FITTING AND FWD LOWER

SHELL CONNECTION

44818 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR OF LATERAL BOX -

PROVIDE AN INSPECTION ACCESS

47108 AIR CONDITIONING - BULK COMPARTMENT VENTILATION-INSTALL AN AIR

HUMIDIFIER SYSTEM FROM VENDOR LE BOZEC

47115 EQUIPMENT/FURNISHINGS-FWD AND AFT CARGOCOMPARTMENT-INSTALL

HEATED DRAINAGE FOR A340-600

47423 EQUIPMENT/FURNISHINGS - DOOR AREA FLOOR PANEL HEATING - REMOVE

HEATING ELEMENTS FOR PAX DOORS 1, 2, 3, 4

47606 INDICATING/RECORDING SYSTEMS - RECORDERS - INSTALL A SYSTEM

PROVISIONS FOR THE COMBINED FDIU/DMU (FDIMU)

47798 WINGS - INBOARD FLAP - OPTIMIZE INBOARD FLAP DESIGN

48904 INDICATING/RECORDING SYSTEM - ACMS - INSTALL SYSTEM PROVISIONS FOR

THE COMBINED FDIU/DMU ( FDIMU )

49059 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - INSTALL

HEATED DRAINAGE SYSTEM FOR A340-500

49314 ELECTICAL POWER - GENERAL - INSTALL EMERGENCY POWER CENTER 743 VU IN

SECT 11/12

49353 WINGS - TRAILING EDGE - INTRODUCE REVISED MAIN LANDING GEAR BUSHES AT

A FT ATTACHMENT FITTING

49639 AIR CONDITIONING-CABIN AIR DISTRIBUTION-INSTALL LE BOZEC HUMIDIFICATION

SYSTEMFOR FCRC

51617 EQUIPMENT/FURNISHINGS – ANCILLARY EQUIPMENT - INTRODUCE FLOOR

TEMPERATURE SETTING PANEL IN DOOR AREA

53234 PNEUMATIC - PYLON AIR BLEED SYSTEM - REPLACE THERMOSTAT DUCT

53368 NAVIGATION-ADIRS-INTRODUCE AIR DATA MONITORING FUNCTION

54173 STABILISERS-HORIZONTAL STABILISER - INCREASE CAPACITY OF FUEL TANK

55048 INDICATING/RECORDING SYSTEMS - ACMS - INSTALL A WIRELESS GROUND LINK

DAR, 8 GSM/GPRS, ARINC 600

55380 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL ADVANCED CARGO

LOADING SYSTEM ON BASIC LR

55559 OXYGEN-CABIN ATTENDANTS PORTABLE DEVICE- INTRODUCE NEW STD LAYOUT

LIGHT WEIGHT PORTABLE OXYGEN CYLINDER ASSEMBLY

# A340 MRB REPORT

Issue : July 2010 SOC Page : 46 55606 OXYGEN - PASSENGER OXYGEN - INSTALL A GASEOUS OXYGEN SYSTEM FOR

A 340-300 ENHANCED

56293 INDICATING / RECORDING SYSTEMS - ACMS -INSTALL A WIRELESS GRO UND LINK

DAR , 4GSM/GPRS , ARINC 600

56418 FUSELAGE - BELLY FAIRING - CHANGE PART MATERIAL (RETROFIT SOLUTION)

56746 EQUIPMENT/FURNISHINGS - ANCILLARY EQUIPMENT - REPLACE HEATED BY

STANDARD FLOOR PANELS ( BY SB )

56834 E/F - CARGO COMPARTMENTS - INSTALL HEATED DRAINAGE IN FWD AND AFT

CARGO COMPARTMENT - A DVANCED CLS

57371 EQUIPMENT/FURNISHING - CURTAINS AND PARTITIONS - INTRODUCE IMPROVED

DECOMPRESSION PANEL IN COCKPIT DOOR

57393 WATER/WASTE - TOILET SYSTEM - CHANGE S/W FOR WCU AND REMOVE THE

A BSOLUTE PRESSURE SENSORS ( APS )

57418 PNEUMATIC - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - INTRODUCE

NEW CRISSAIR APU CHECK VALVE 2S7138 AMDT A

57459 WATER/WASTE-POTABLE-INSTL WATER FILTER HOUSING AND CARTRIDGE 1

MICROMETER DECHLORINATING IN EACH LAVATOR Y

58640 CABIN SYSTEM - ON-BOARD MOBILE TELEPHONY SYSTEM - DEFINE OMTS PART

OF ALNA V2

APPENDIX 11

Page 11.12 20000 FC changed to 8500 FC.

Page 11.14 Following FC sampling note added:

Additionally, aircraft will also be nominated to sample Flight Cycle usage and validate the

target TBO, i.e. 8,500FC. For nominated sample aircraft refer to Table C, below. Each

sample will be the subject of a commercial agreement between Airbus/Messier-Dowty and

the relevant operator

Operator for MSN 436 updated in Table A.

Page 11.15 Table B title corrected to indicate Calendar TBO.

Table C added:

“A340-500/600 sample aircraft to perform MLG, NLG and CLG samples to validate target

Flight Cycle TBO”.

# A340 MRB REPORT

Issue : 

# July 2010 T.O.C. 1 TABLE OF CONTENTS

- Record of Revisions

- Summary of Changes

- List of Effective Pages

- Section A. INTRODUCTION

1. Scope and purpose

2. Basis for standards and procedures

3. Aircraft Utilisation Assumptions

4. Revision policy

5. Overall Document Description

6. Inspection intervals

Section B. GENERAL RULES THAT APPLY TO ALL A340 SECTIONS

Section C. SYSTEMS AND POWERPLANT SECTION

Section D. STRUCTURES SECTION

Section E. ZONAL INSPECTION SECTION

Section F. REQUIREMENTS FOR U.S. OPERATORS

Appendix 1 : Certification Maintenance Requirements and Airworthiness Limitation Items

Appendix 2 : Zone diagrams

Appendix 3 : - deleted –

Appendix 4 : - deleted –

Appendix 5 : Administration - composition of working bodies

Appendix 6 : Glossary of terms

Appendix 7 : Abbreviations

Appendix 8 : Structures Inspection Reporting System

Appendix 9 : HIRF / Lightning Protection

Appendix 10 : Modification reference list

Appendix 11 : Landing Gear Overhaul / Restoration Requirements”

# This page is intentionally left blank

# A340 MRB REPORT

LIST OF EFFECTIVE PAGES

SECTION PAGES SECTION PAGES



# Issue : July 2010 Page : L.E.P. 1

ROR 1 to 1

SOC 1 to 46

TOC 1 to 1

LEP 1 to 1

A 1 to 3

B 1 to 3

C-INTRO 1 to 8

C-20 1 to 11

C-21 1 to 7

C-22 1 to 1

C-23 1 to 4

C-24 1 to 3

C-25 1 to 11

C-26 1 to 13

C-27 1 to 12

C-28 1 to 9

C-29 1 to 4

C-30 1 to 2

C-31 1 to 2

C-32 1 to 8

C-33 1 to 1

C-34 1 to 4

C-35 1 to 5

C-36 1 to 1

C-38 1 to 3

C-45 1 to 1

C-46 1 to 1

C-H331-350-49 1 to 4

C-H331-600-49 1 to 4

C-52 1 to 5

C-53 1 to 2

C-54 1 to 1

C-55 1 to 1

C-56 1 to 1

C-57 1 to 1

C-CFM56-5-71 1 to 2

C-CFM56-5-72 1 to 3

C-CFM56-5-73 1 to 1

C-CFM56-5-74 1 to 1

C-CFM56-5-75 1 to 1

C-CFM56-5-76 1 to 1

C-CFM56-5-77 1 to 1

C-CFM56-5-78 1 to 2

C-CFM56-5-79 1 to 2

C-CFM56-5-80 1 to 1

C-RR T500-71 1 to 1

C-RR T500-72 1 to 4

C-RR T500-73 1 to 1

C-RR T500-74 1 to 1 C-RR T500-75 1 to 1

C-RR T500-76 1 to 1

C-RR T500-77 1 to 1

C-RR T500-78 1 to 2

C-RR T500-79 1 to 1

C-RR T500-80 1 to 1

D-INTRO 1 to 22

D-28 1 to 1

D-32 1 to 7

D-52 1 to 14

D-53 1 to 85

D-54 1 to 20

D-55 1 to 18

D-56 1 to 1

D-57 1 to 252

D-71 1 to 3

D-72 1 to 1

D-78 1 to 3

E-INTRO 1 to 5

E-100 1 to 13

E-200 1 to 10

E-300 1 to 9

E-400 1 to 10

E-500 1 to 11

E-600 1 to 1

E-700 1 to 3

E-800 1 to 6

F1 1 to 2

APX 1 1 to 1

APX 2 1 to 40

APX 3 1 to 1

APX 4 1 to 1

APX 5 1 to 39

APX 6 1 to 4

APX 7 1 to 4

APX 8 1 to 2

APX 9 1 to 9

APX 10 1 to 8

APX 11 1 to 15

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : A1 SECTION A

INTRODUCTION

1. SCOPE AND PURPOSE

This Report provides the initial minimum scheduled maintenance tasks and their frequencies for the

systems, powerplant and structure of the Airbus A340 aircraft. It is intended that this Report will be used

as a basis for each operator to develop his own maintenance program subject to the approval of his

Regulatory Authority.

This document is referenced in the EASA A340 Type Certificate Data Sheet (TCDS) under the

number 00F050A0002/C01.

The tasks and their frequencies given in this Report, together with the Certification Maintenance

Requirements and Airworthiness Limitations, form part of the instructions considered essential for

proper maintenance as required by certification requirements for JAR 25.1529 and JAR 25 Appendix

H, Instructions for Continued Airworthiness.

This Report has been approved by the following authorities and is proposed to other Authorities for

their endorsement:

- European Aviation Safety Agency (EASA).

- FAA (With the addition of Section F, Requirements for U.S. Operators)

- Transport Canada

The information and instructions included herein are applicable to the following A340 models and

powerplants as defined on the aircraft Type Certificate Data Sheet:

- A340-21x with CFM 56-5x engines

- A340-31x with CFM 56-5x engines

- A340-54x with TRENT553 engines

- A340-64x with TRENT556 engines or TRENT 560

The third digit of the hyphenated number is identified as "x" in order to indicate that all aircraft models

in this series are covered by this MRB Report. The final digit in the official aircraft designation is

associated with thrust levels and has no repercussion on the MRB Report.

For further clarification, the following table provides an example of the specific aircraft models included

in the above mentioned designations. The right hand list in this table may not be exhaustive.

Generic model designation Specific model designations

A340-21x

A340-31x

A340-54x

A340-64x A340-211, A340-212, A340-213

A340-311, A340-312, A340-313

A340-541, A340-542

A340-642, A340-643

Note: Within the MRB Report the Applicability of individual tasks is, where necessary, defined using

generic series i.e. A340-200, -300, -500, -600 since only one engine type can be fitted to each series.

2. BASIS FOR STANDARDS AND PROCEDURES

The scheduled maintenance tasks and frequencies contained in this MRB Report have been

developed by an Industry Steering Committee and joint Airline/Manufacturer Working Groups. The

procedures utilized have been based on the "Maintenance Program Development Document -MSG 3

Revision 2" dated September, 1993 and are fully detailed in the A330/A340 Scheduled Maintenance

Development Policy and Procedures Handbook - Reference AI/SE-M2 95A.0925/01, issue 15, dated

Mar 2007.

The composition of the various working bodies is given in Appendix 5 to this MRB Report.

# A340 MRB REPORT

Issue : July 2010 Page : A2 3. AIRCRAFT UTILISATION ASSUMPTIONS

The MRB Report for the A340 is based on the following aircraft utilisation assumptions:

With interval defined as 800FH: Flight cycle envelope = 44 FC to 267 FC

Calendar envelope = 44 days to 145 days

Annual utilisation (12 months): Flight hour envelope = 1667 FH to 5667 FH

Flight cycle envelope = 367 FC to 1100 FC

Operators whose aircraft utilisation differs significantly from these assumptions may need to make

adjustments to their program with their Regulatory Authority

4. REVISION POLICY

The need for revision will be considered on an annual basis following discussion between the ISC

Chairman, ISC Co-chairman and the MRB Chairman. An ISC meeting will be called if the revision is

significant. Minor changes will be handled by postal correspondence with ISC/MRB members.

5. OVERALL DOCUMENT DESCRIPTION

The maintenance tasks and their frequencies are presented in the Systems and Powerplant, Structure

and Zonal sections.

- The Systems and Powerplant section defines specific tasks at the level of each Maintenance

Significant Item (MSI) considering the failure effects and failure causes.

- The Structures section defines the necessary inspections for each Structural Significant Item (SSI)

developed through evaluation with respect to fatigue environmental and accidental damage. A

Corrosion Prevention and Control Program (CPCP) was integrated into the Structures section in

the Apr 97 MRB Report revision.

- The Zonal section defines General Visual Inspections of system installations (including EWIS) and

structure by aircraft zone.

- Certification requirements dictate that the critical systems installed in the A340 aircraft are provided

with protective measures against the effects of High Intensity Radiated Fields (HIRF). These were

not identified as MSIs or subjected to analysis by the MSG-3 process.

The manufacturer has identified an appropriate method by which to confirm that in-service

operation will not reduce the HIRF and lightning protection to a level which is inadequate to

maintain Type Certification objectives. This is explained in Appendix 9.

6. INSPECTION INTERVALS

For the Systems and Powerplant section C and the Zonal section E, the basic initial inspection check

intervals are:

A - Check and multiples 800 FH and multiples

C - Check 18 months

2C – Check 36 month

4C – Check 6 Yrs

8C – Check 12 Yrs

For safety related tasks, intervals are given in the appropriate usage parameter (e.g. flight hours, flight

cycles, calendar time). For non-safety tasks, intervals may be quoted in terms of letter check unless

# A340 MRB REPORT

Issue : July 2010 Page : A3 degradation is predominantly dependent on a particular usage parameter or in service experience did

not support escalation

The MRB Report is not intended to be the total maintenance program. There are items which are

typically performed by each operator in his maintenance program more frequent than "A"-check. The

routine content of checks occurring more frequently than the "A"-check shall be developed by the

operator and approved/accepted by their local Regulatory Authority. Maintenance/inspection tasks with

intervals more frequent than the "A"-check found in this MRB Report were developed through the

MSG-3 analysis process.

An operator may desire to perform "A" or "C" interval tasks as part of a continuous or a progressive

maintenance program system, i.e. "A" or "C" interval tasks would be phased into a number of individual

packages. This would be considered acceptable provided the maximum interval between successive

tasks does not exceed that listed in this MRB Report.

For the Structures section D, the basic initial thresholds and intervals for environmental deterioration

related items are as follows:

Thresholds: 6 Years and 12 Years

Intervals: 6 Years and 12 Years.

NOTE: Some calendar thresholds and intervals remain at 5 Years or 10 Years, pending further

evolution.

Thresholds and intervals for fatigue damage related items are given in Flight Cycles (and Flight

Hours for range sensitive items) .

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : B1 SECTION B

GENERAL RULES THAT APPLY TO ALL A340 SECTIONS

1. The operator's manuals shall contain the details and responsibilities for accomplishing the

maintenance identified by this MRB Report.

2. The overall reliability of the A340 will be monitored by each operator's system for continuous

analysis and surveillance as required by the operator's Regulatory Authority.

3. Task intervals may be changed in accordance with the operator's Regulatory Authority practices

and rules. In this respect, attention is drawn :

- For Systems and Powerplant section, to the Failure Effect Category (FEC) noted in

Sect.C, Systems and Powerplant section, para 3 Explanation, Column 4

- For Zonal Inspection section, to the validity of the General Visual Inspections of the

Structures Section.

- For Structures Program, to tasks derived from Damage Tolerance Evaluation as noted in

Sect. D, Structures , General.

In addition, CMRs, mandatory structural inspections and life limits are to be handled with specific

associated rules, as described in Rules 6, 7 and 8 below.

4. The individual maintenance task frequency shown in this MRB Report may be adjusted with the

assigned Regulatory Authority. However, tasks with Failure Effect Category 5 and 8 must not be

deleted from the operator's maintenance program.

5. Each operator should be aware of the various inspection techniques such as X-Ray, ultrasonic,

eddy current, radio isotope,... which are available and described in the Non-Destructive Testing

Manual (NTM). The use of such techniques can be developed to provide a valuable adjunct to the

prescribed inspections. For any substitution of such inspection technique, it must be ensured that

the same damage size will be detectable by the proposed technique with the same level of

confidence.

6. Items that are life limited will be discarded according to the life limits stated in the appropriate

section of the engine or aircraft manufacturer's manuals. These sections are referenced in the

aircraft and engine "Type Certificate Data Sheet".

7. Certification Maintenance Requirements tasks/intervals arising from analyses (eg Systems Safety

Assessments) performed as part of the Type Certification process are given in Airbus document

955.3019/92. The process by which CMRs are identified is independent of the MRB analysis

process. The CMR document is the controlling document for all tasks identified as CMRs. When

the interval for an MRB Report task is less (more conservative) than the applicable CMR task

interval, the MRB Report task interval will take precedence.

8. Mandatory structural inspection thresholds and intervals resulting from damage tolerance

evaluation are given in the Damage Tolerant Airworthiness Limitation Items document ref SEM4/95A.0051/97. This is the controlling document for all tasks identified as Damage Tolerant

Airworthiness Limitation Items.

# A340 MRB REPORT

Issue : July 2010 Page : B2 9. Within this MRB Report the terms "test", "check" and "inspection" are not intended to imply a level

of skill required to accomplish the task.

10. Tasks may be considered to conform to the requirements of the scheduled maintenance program

if accomplished as part of an equivalent check/test performed by the operators flight crew in

accordance with an approved/accepted flight crew normal check list and with Regulatory Authority

concurrence.

11. It is the responsibility of each operator to adjust their own maintenance program in accordance with

their National Requirements, and to comply with existing rules with respect to reporting to their

Regulatory Authority and to the manufacturer, events having effects on the continued airworthiness

of the aircraft.

12. The reapplication of all protective materials (e.g. Temporary Protection Systems (TPS), paints etc.)

shall be carried out following their removal to perform the inspection/maintenance task.

13. Revisions to this MRB Report may be considered as sufficient justification for Regulatory Authority

approval/acceptance.

14. When two or more intervals are assigned to a task, and when not otherwise stated, the interval

expiring first shall apply.

15. Any fairings, panels, doors or other items which are removed/opened to gain access for

maintenance tasks must also be inspected for general condition with a minimum level of GVI

before reassembly/refitting.

16. Tasks approved from Fuel Tank Safety (FTS) Requirements using the criteria established in

Special Federal Aviation Regulation (SFAR88) / EASA policy statement on the process for

developing instructions for maintenance and inspection of fuel tank system ignition source

prevention; are identified with (SFAR88) in parenthesis following the task description in the MRB

Report. This policy has been applied to Systems & Powerplant tasks listed under ATA 281800

in Section C.

For Operators under U.S. FAA Jurisdiction only:

Operators requesting revisions to the baseline FTS requirements for failure effect category

(FEC) 5 and 8 tasks, description or intervals, must submit their request through the cognizant

Flight Standards District Office, who may add comments and then forward it to the manager of

the appropriate FAA Aircraft Certification Office, or office of the Transport Airplane Directorate,

having cognizance over the type certificate for the affected airplane for concurrence prior to

approval. Tasks and intervals other than FEC 5 and 8 may be revised through normal operator

approval process.

For Operators Not under U.S. FAA Jurisdiction:

Operators requesting revisions to the baseline FTS requirements may revise these tasks and

intervals through their normal operator approval process.

17. Electrical Wiring Interconnection System (EWIS) tasks derived from the Enhanced Zonal

Analysis Procedure (EZAP) in ATA 20 of Section C and standard zonal tasks with EWIS

content are identified by (EWIS) in parenthesis following the task description in the MRB Report.

For Operators under U.S. FAA Jurisdiction only:

Operators requesting revisions to the baseline EWIS task or description must submit their

request through the cognizant Flight Standards District Office, who may add comments and

then forward it to the manager of the appropriate FAA Aircraft Certification Office, or office of

# A340 MRB REPORT

Issue : July 2010 Page : B3 the Transport Airplane Directorate, having cognizance over the type certificate for the affected

airplane for concurrence prior to approval. Task intervals may be revised through normal

operator approval process. Tasks indicated with “(EWIS)” after the task description must not be

deleted from the operator's maintenance program.

For Operators not under U.S. FAA Jurisdiction:

Operators requesting revisions to the EWIS requirements may revise these tasks and intervals

through their normal operator approval process. Tasks indicated with “(EWIS)” after the task

description must not be deleted from the operator's maintenance program.

# A340 MRB REPORT

This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : C-INTRO-1 SECTION C

SYSTEMS AND POWERPLANT

1. GENERAL

This section provides the initial minimum scheduled maintenance tasks and frequencies for all

systems including Powerplant and auxiliary power unit.

With respect to the evaluation procedures and the resulting tasks the following is noted:

(a) Operational checks were not considered as forming part of Normal Operating Crew

Duties when determining the evident or hidden aspects of functional failures

(ref. MSG3 para 2.3.4.1). As a result some tasks given in this section may be

considered as flight crew tasks in accordance with Note 5. See also Section B,

General Rule 9.

(b) Operators should take the opportunity of engine/APU removal and disassembly to

perform "off-wing" inspections and parts/assemblies restoration as per engine shop

manuals. No scheduled basis for these tasks is defined in this MRB Report.

(c) No threshold or opportunity inspection requirements are given for APU or Powerplant.

Manufacturers may recommend such inspections in the event that late development

or early in-service experience would indicate the desirability to examine specific

components of individual engines. If this is necessary, then direct negotiations

between applicable operators and the engine manufacturer will be arranged. Results

of these inspections are to be made available by the manufacturers to other customer

airlines as well as the Regulatory Authorities.

(d) As noted in Section B, General Rule 6, limitations of life limited parts are controlled by

the manufacturers and published in the following documents:

- Airbus A340 Airworthiness Limitation Section - Part 1

- CFM 56-5 Engine Shop Manual Chapter 5

- RR-TRENT500 Time Limits Manual

- GTCP 331-600 Component Maintenance Manual

(e) APU task intervals quoted in terms of APU HRS may be converted to another usage

parameter in accordance with an appropriate conversion factor based on an

operator's specific APU utilization.

(f) No recommendation is made for scheduled fuel analysis. Operators who suspect the

quality of their fuel supplies or who operate in an environment known to promote

microbiological growth are recommended to introduce fuel sampling and consider the

use of additives to minimize the potential for such growth.

(g) This section identifies some tasks with intervals less than A-check. These have been

developed using the MSG-3 process and should be included in routine checks. With

the exception of any task with CMR status, those tasks which are typical for all

aircraft types may be scheduled by the operator in accordance with Regulatory

Authority accepted standard practices, the quoted interval being given for the

guidance of operators who do not have appropriate standards. See also Section A

Para 5.

(h) Cat II/Cat III landing capabilities and RVSM capability are inherent functions of the

basic design standard of the aircraft. Scheduled tasks necessary for these operations

have been considered in the development of this section. Operators should comply

with National Requirements as applicable.

# A340 MRB REPORT

Issue : July 2010 Page : C-INTRO-2 (i) Lubrication requirements specified in this MRB Report arise from the MSG-3 analysis

process and do not represent the total lubrication provisions for the aeroplane.

Accordingly, operators should refer to th e manufacturer's appropriate maintenance

publications for additional lubrication information.

(j) In the Systems and Powerplant section, some MSI references and titles include two

or more ATA subchapters.

In this issue of MRB Report produced from a Data Base Management System, only

the first reference is printed and the title must have less than 120 characters. This

concerns the following items:

QUOTED REFERENCE- ABBREVIATED TITLE COMPLETE REFERENCE AND TITLE

21.28.00 LOWER DECK CARGO

COMPARTMENT HEATING, VENTILATION

AND COOLING (FWD, AFT AND BULK) 21.28.00 LOWER DECK CARGO

COMPARTMENT VENTILATION AND COOLING

(FWD, AFT AND BULK)

21.43.00 LOWER DECK CARGO

COMPARTMENT HEATING (FWD, AFT AND

BULK)

21.50.00 A IR COOLING, TEMPERATURE

CONTROL 21.50.00 A IR COOLING

21.60.00 TEMPERATURE CONTROL

23.33.00 IN FLIGHT ENTERTAINMENT

SYSTEM 23.33.00 IN FLIGHT ENTERTAINMENT

SYSTEM

23.36.00 PASSENGER VIDEO

ENTERTAINMENT

25.52.00 LOWER DECK FORWARD AND AFT

CARGO COMPARTMENT 25.52.00 LOWER DECK FORWARD CARGO

COMPARTMENT

25.53.00 LOWER DECK AFT CARGO

COMPARTMENT

32.30.00 EXTENSION AND RETRACTION,

POSITION AND WARNING 32.30.00 EXTENSION AND RETRACTION

32.60.00 POSITION AND WARNING

34.48.00 TERRAIN AWARENESS AND

WARNING SYSTEM (INCLUDING (E)GPWS

AND T2CAS-TAWS) 34.43.20 T2CAS - TERRAIN AWARENESS AND

WARNING SYSTEM

34.48.00 TERRAIN AWARENESS AND

WARNING SYSTEM (INCLUDING (E)GPWS

AND T2CAS-TAWS)

46.11.00 FLYSMART WITH AIRBUS 46.11.00 FLYSMART WITH AIRBUS

46.12.00 AIRCRAFT NETWORK SERVER UNIT

46.41.00 CABIN INFORMATION NETWORK

SYSTEM

46.42.00 INTERNAL WIRELESS DATA LINK

46.46.00 PASSENGER INFORMATION

NETWORK

46.51.00 MISCELLANEOUS INFORMATION

SYSTEMS - OPERATIONAL USE

46.52.00 MISCELLANEOUS INFORMATION

SYSTEMS - ACQUISITION AND INTERFACES

46.54.00 MASS MEMORY SYSTEM

52.31.00 FWD AND AFT CARGO

COMPARTMENT DOOR 52.31.00 FWD CARGO COMPARTMENT DOOR

52.32.00 AFT CARGO COMPARTMENT DOOR

52.36.00 CARGO COMPARTMENT DOOR

HYDRAULIC SYSTEM 52.35.00 CARGO COMPARTMENT DOOR

ELECTRICAL CONTROL SYSTEM

52.36.00 CARGO COMPARTMENT DOOR

HYDRAULIC SYSTEM

53.19.00 FUSELAGE DRAINS 53.19.00 FUSELAGE DRAINS

53.29.00

53.39.00

53.49.00

53.59.00

k) During the review of an aircraft system for the purpose of modifying or verifying the

# A340 MRB REPORT

Issue : July 2010 Page : C-INTRO-3 maintenance requirements, the reviewer must be aware that those functions

associated with the ignition prevention features of all systems are identified and

analysed in MSI 28-18-00 Ignition Prevention.

Any review of an existing MSI task must therefore consider that it may be necessary

to review MSI 28-18-00 in addition to the specific system MSI identified.

(l) Tasks arising from the Enhanced Zonal Analysis Procedure (EZAP), (comprised of

GVI tasks not fully covered by Zonal tasks and DI/RS tasks) are included within ATA

chapter 20 of the System and Powerplant section of the MRBR and have no Failure

Effect Category (FEC) quoted

. The tasks are identified with “EWIS” following the task

description (see Section B General rule 17 for further details). These tasks remain

under the responsibility of the Zonal Maintenance Working Group.

Note (i): The term “EWIS in the task description of ATA 20 tasks includes all

electrical wiring and interconnection systems installations (e.g. cables,

conduits, clamps, etc...)

Note (ii): ATA 20 tasks must not be deleted from the operators maintenance program

Note (iii): For advice on cleaning contaminated wiring, refer to the Airbus Electrical

Standard Practices Manual (ESPM) chapter 20-55-20 “CLEANING OF

WIRES (Airbus)”.

2. NOTES FOR SECTION C

NOTE 1: Depending on operating environment and the operator's experience, a less

frequent or more frequent initial interval may be used.

NOTE 2: -deletedNOTE 3: -deletedNOTE 4: For interval refer to Chapter 5 of Engine Shop Manual (ESM) for CFMI

engines, Time Limits Manual (TLM) for Rolls-Royce engines and to GTCP

331-600 CMM for Honeywell APU.

NOTE 5: Performance of task is not required by maintenance personnel if

accomplished as part of a Regulatory Authority accepted/approved flight crew

check list. See Section B, General Rules, para 10.

NOTE 6: -deleted-.

NOTE 7: Refer to MRBR Appendix 11 “LANDING GEAR OVERHAUL/

RESTORATION INTERVAL REQUIREMENTS”

NOTE 8: Interval or vendor recommendation quoted is only applicable if no National

requirement exists.

NOTE 9: -deleted-.

NOTE 10: Operationally check the slide/raft in accordance with the following schedule:

DOOR/EXIT QUANTITY CHECK

(RH OR LH SIDE) (PER OPERATOR FLEET) INTERVAL

FWD Passenger/ 1 36 MTHS

Crew Door

# A340 MRB REPORT

Issue : July 2010 Page : C-INTRO-4 MID Passenger/ 1 36 MTHS

Crew Door

AFT Passenger/ 1 36 MTHS

Crew Door

Over wing Door 1 36 MTHS

Emergency Exit 1 36 MTHS

Checks may be performed on either side and do not all have to be performed

on the same aircraft. As an ongoing continuous maintenance program the

operator should continue the operational check sequence until this schedule

has been revised by the MRB.

Inadvertent deployments may not be used to satisfy the above requirements.

A330/A340 fleets can be combined for common doors.

NOTE 11: Crew rest room (underfloor) and/or ACTs not to be removed if installed.

NOTE 12: - deleted - (transfered to Section B).

NOTE 13: - deleted -

NOTE 14: - deleted -

NOTE 15: Credit may be taken for monitoring filter condition through the CMS in order

to maximise service life.

NOTE 16: - reserved -

NOTE 17: - reserved -

NOTE 18: Task is included in manufacturer’s ACT removal/installation procedure.

Credit can be taken for performance of this task at this opportunity.

NOTE 19: - deleted -

NOTE 20: - reserved -

NOTE 21: If ACT not fitted when task becomes due it may be postponed until next ACT

installation.

NOTE 22: - reserved -

NOTE 23: ACT serial number to be tracked since task accomplishment is a function of

ACT age and not aircraft age.

NOTE 24: Refer to A340 Certification Maintenance Requirements (CMR) document

(Reference 955.3019/92) for identification of specific requirements regarding

handling of task interval. Instructions to locate the CMR document are given

in Appendix 1a of this MRB Report. Where the CMR interval for an MRB

Report task is more restrictive, the CMR interval takes precedence.

NOTE 24 is written in the Interval column when the CMR status is applicable

to all series, NOTE 24A when it is applicable only to A340-200/300 and

NOTE 24B when it is applicable only to A340-500 and A340-600.

NOTE 25 Task is included in manufacturer’s Crew Rest Room (underfloor)

removal/installation procedure. Credit can be taken for performance of this

task at this opportunity.

# A340 MRB REPORT

Issue : July 2010 Page : C-INTRO-5 NOTE 26 For CRR(u) users only:

CRR(u) part is included in this task. If CRR(u) is not fitted when task

becomes due, CRR(u) part should be performed when CRR(u) is next

installed.

NOTE 27 Task is also applicable for CRR(u). Interval 6 YE.A340MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-63. EXPLANATION OF SYSTEMS AND POWERPLANT SECTION FORMATMSIREFERENCETASK MSI AND TASK DESCRIPTION FEC INTERVALZIPREFERENCEAPPLICABILITY1 2 3 4 5 6 71- This column indicates the MSI reference number and is directly obtained from the Airbus ATA Breakdown and Nomenclature Reference document.Paragraph C1(j) identifies MSIs that address two or more systems / sub-systems.2- This column identifies the task type and thus enables the user to understand from which MSG-3 Level 2 logic question the task has been developed, ie :- LU Lubrication 5A, 6A, 7A, 8A, 9A- SV Servicing 5A, 6A, 7A, 8A, 9A- OP Operational Check 8B, 9B- VC Visual Check 8B, 9B- GVI, DI, SDI Inspection 5B, 6B, 7B, 8C, 9C- FC Functional Check 5B, 6B, 7B, 8C, 9C- RS Restoration 5C, 6C, 7C, 8D, 9D- DS Discard 5D, 6D, 7D, 8E, 9EThis information can be used to clarify whether the task is to detect a failure (8B, 9B) or to detect degradation (5B, 6B, 7B,8C, 9C).3- This column identifies the MSI title (which is in accordance with the Airbus ATA Breakdown) and the description of each taskidentified through the MRBReport development process.The term "No task selected" indicates that the MSI has been subjected to a full MSG-3 analysis but no applicable and effectivetasks were identified.The term "-task deleted-" indicates that during the development process a task had been proposed which was eventually deleted due to re analysis, taskamalgamation or ISC decision. Renumbering of tasks was avoided inorder to minimise impact on cross reference data in operatorsinitial maintenanceschedules.A340MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-7The term "-reserved-" indicates that the task number has been allocated to an A330 MRB Report task. This ensures that corresponding Systems sectiontasks have the same reference number in the A330 and A340 MRB Reports.4- This column identifies the Failure Effect Category (FEC). MSG-3 analysis allocates tasks against the following FECs depending on the consequence offailure :- FEC 5 : Evident Safety Effects- FEC 6 : Evident Operational Effects- FEC 7 : Evident Economic Effects- FEC 8 : Hidden Safety Effects- FEC 9 : Hidden Non-Safety Effects.The notation "-" (hyphen) in the FEC column indicates that the task has not been developed through the MSG-3 systems and powerplant logic process.Such tasks arise from either a specific MRB requirement (e.g. escape slide sampling) or have been determined as necessary to maintain compliance withType Certification requirements or are the results of the ATA 20 HIRF/EZAP analysis process.Multiple FECs are quoted only when the task is associated with both a hidden and an evident FEC. Where multiple hidden FECs (8,9) or multiple evidentFECs (5, 6, 7) are applicable only the most important one is quoted.5- This column identifies the interval between successive accomplishments of the task. Refer to Section A para 5 "Inspection Intervals" for definition of lettercheck. The "Note x." referred to in this column is detailed in Section C para 2.Some of the tasks necessary to maintain compliance with Type Certification requirements have been determined to warrant Certification MaintenanceRequirement (CMR) status. Such tasks are highlighted in this section by the notation "NOTE 24" in the interval column. The corresponding handlinginstructions are given in the approved document "A340 Certification Maintenance Requirements" reference 955.3019/92 which is located in Appendix 1 ofthis MRB Report.When the interval is not quoted in terms of letter check, the suitable usage parameter is provided. The usage parameters are:- Calendar time : day (DY), month (MO), year (YE)- Flight hours (FH)- Flight cycles (FC)- APU hours (AH) / APU cycles- ACT Hours / ACT Month (ACT MO)- CRR Hours (CRR FH) / CRR Month (CRR MO)A340MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-86- The scheduled maintenance task derived from MSG-3 analysis is considered adequately covered by the referenced Zonal tasks inthis column. It should benoted that the Zonal task interval may be more frequent than that required by the Systems and Powerplant task.These requirements are quoted for record purposes and do not lead to tasks additional to those given in Section E.7- This column indicates the aircraft configuration, model or engine type to which this requirement is applicable. Examples aregiven below:ALLTask applicable to all A340 aircraft.A340-200 Task applicable to all A340-200 only.PRE 49144 Task applicable to all A340 PRE 49144.i.e. Aircraft without modification 49144 embodied.POST 49144 Task applicable to: all A340 POST 49144.i.e. to Aircraft with modification 49144 embodied.IF CREW REST ROOMINSTALLEDSelf-explanatoryA340-300PRE 44051Task applicable to A340-300 without modification 44051embodied.A340-500POST 44051Task applicable to A340-500 with modification 44051 embodied.POST 44051POST 44061POST 44085Task applicable to all A340 with modification 44051 and 44061 and44085 embodied.i.e. only to Aircraft with all modifications embodied.POST 45040ORPOST 45056Task applicable to all A340 with modification 45040 or 45056embodied i.e. to Aircraft with one of the modification or bothmodifications embodied.PRE 45040PRE 45056Task applicable to all A340 without both modification 45051 and45085 embodied at the same timei.e. without any if these modifications embodiedA340-200ORA340-300PRE 49144Task applicable to all A340-300 without modification 49144embodied and all A340-200A340MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-9A340-300POST 49144ORA340-500ORA340-600Task applicable to all A340-300 with modification embodied and toall A340-500 and A340-600POST 44040PRE 44057Task applicable to all A340 with modification 44040 and withoutmodification 44057 embodied at the same time.APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.00.00 ENHANCED ZONAL20.0.121 AVIONICS COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AVIONICS - I: 72 MOALLCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF 710VU AND 740VU IN THE - I: 144 MOALLAVIONICS COMPARTMENT, (EWIS).20.0.131 FORWARD CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO - I: 72 MOA340-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 02 CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO - I: 72 MOA340-500COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).ORA340-600R GVI 03 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-200INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).ORA340-300R GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-500INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).ORA340-60020.0.137 BAY BEHIND FWD CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD - I: 72 MOALLCARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).20.0.141 CENTER WING BOXR GVI 01 GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE - I: 144 MOALLTHE FUEL TANK (AS FAR AS VISIBLE), (EWIS).20.0.145 ZONE UNDER CABIN FLOOR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.145 * * * * * C O N T I N U E * * * * *R RS 01 CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN - I: 144 MOALLFLOOR (ONLY IF CONTAMINATED), (EWIS).20.0.151 AFT CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA340-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).WITHOUT ACT(S)ORA340-300WITHOUT ACT(S)R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA340-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).WITH ACT(S)ORA340-300WITH ACT(S)R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA340-500COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R RS 04 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA340-600COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R GVI 05 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-200INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).ORA340-300R GVI 06 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-500INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).R GVI 07 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-600INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).R GVI 08 GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THE - I: 72 MOA340-300ACT, EXTERNAL SURFACE ONLY.(EWIS)POST 42612NOTE: TASK COULD BE PERFORMED AT THE OPPORTUNITY OFORACT R/IA340-200POST 44002POST 4400520.0.155 REAR CENTER TANK* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.155 * * * * * C O N T I N U E * * * * *R GVI 01 GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE - I: 144 MOA340-500THE REAR CENTER TANK (AS FAR AS VISIBLE), (EWIS).20.0.161 BULK CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MOAICRAFT WITHOUTCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).BCRCR RS 02 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MOA340-500COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).IF BCRCINSTALLEDORA340-600IF BCRCINSTALLEDR GVI 03 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-200INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).ORA340-300R GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA340-500INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).ORA340-60020.0.211 COCKPITR RS 01 CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY IF - I: 144 MOALLCONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE - I: 144 MOALLCOCKPIT AT LEVEL OF LATERAL FLOOR STRUCTURE BETWEENFR.1 TO FR.11, (EWIS).20.0.221 FWD CABIN UTILITY AREAR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS,NOTEBETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTIONINSTALLED IN THE FWD CABIN UTILITY AREA, (EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.221 * * * * * C O N T I N U E * * * * *SEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN UTILITY - I: 144 MOALLAREA (ONLY IF CONTAMINATED), (EWIS).R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MOALLIN THIS AREA, (EWIS).20.0.223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS AND CIRCUIT BRAKERS "5001 VE" - I: 144 MOALLINSTALLED IN THE FWD CABIN UTILITY AREA OVERHEADCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BRAKERS "5001VE" - I: 144 MOALLAND "G, AND P" ROUTES INSTALLED IN THE FWD CABINUTILITY AREA OVERHEAD COMPARTMENT (ONLY IFCONTAMINATED), (EWIS).20.0.231 FWD CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLEDIN THE FWD CABIN AREA,(EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN AREA - I: 144 MOA340-200(ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 03 CLEANING OF EWIS INSTALLED IN THE FWD CABIN AREA - I: 144 MOA340-500(ONLY IF CONTAMINATED), (EWIS).ORA340-60020.0.233 FWD CABIN OVERHEAD COMPARTMENT* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.233 * * * * * C O N T I N U E * * * * *R RS 01 CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD - I: 144 MOA340-200COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).ORA340-300R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD - I: 144 MOA340-500COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).ORA340-600N GVI 03 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 144 MOA340-200INSTALLED IN THE FORWARD CABIN OVERHEADORCOMPARTMENT, (EWIS).A340-300N GVI 04 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 144 MOA340-500INSTALLED IN THE FWD CABIN OVERHEAD COMPARTMENT,OR(EWIS).A340-60020.0.241 MID CABIN UTILITY AREAR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS,NOTEBETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTIONINSTALLED IN THE MID CABIN UTILITY AREA, (EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MOA340-200AREA (ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 03 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MOA340-500AREA (ONLY IF CONTAMINATED), (EWIS).ORA340-60020.0.243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MOA340-200OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED).OR(EWIS).A340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.243 * * * * * C O N T I N U E * * * * *R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MOA340-500OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED),OR(EWIS).A340-600N RS 03 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA340-200INSTALLED IN THE MID CABIN UTILITY OVERHEADORCOMPARTMENT AREA, (EWIS).A340-300N RS 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA340-500INSTALLED IN THE MID CABIN UTILITY OVERHEADORCOMPARTMENT AREA, (EWIS).A340-60020.0.251 MID CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLEDIN THE MID CABIN AREA, (EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA - I: 144 MOA340-200(ONLY IF CONTAMINATED), (EWIS).ORA340-300R GVI 03 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MOA340-200INSTALLED IN THIS AREA, RH ONLY, (EWIS).ORA340-300R RS 04 CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA - I: 144 MOA340-500(ONLY IF CONTAMINATED), (EWIS).R RS 05 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MOA340-600AREA (ONLY IF CONTAMINATED), (EWIS).N GVI 06 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MOA340-500INSTALLED IN THIS AREA, RH ONLY, (EWIS).N GVI 07 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MOA340-600INSTALLED IN THIS AREA, RH ONLY, (EWIS).ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.253 MID CABIN OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MOA340-200COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MOA340-500COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).R RS 03 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MOA340-600COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).N GVI 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA340-200INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENTORAREA. (EWIS).A340-300N GVI 05 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA340-500INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA,(EWIS).N GVI 06 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA340-600INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA,(EWIS).20.0.261 AFT CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTION, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION,INSTALLED IN THE AFT CABIN AREA,(EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MOA340-200(ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MOA340-500(ONLY IF ONTAMINATED), (EWIS).R RS 04 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MOA340-600(ONLY IF CONTAMINATED), (EWIS).ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.263 AFT CABIN OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MOA340-200COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).ORA340-300R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MOA340-500COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MOA340-600COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).N GVI 04 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MOA340-200THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).ORA340-300N GVI 05 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MOA340-500THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).N GVI 06 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MOA340-600THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).20.0.271 AFT CABIN UTILITY AREAR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOALLATTACHMENT POINTS AND ELECTRICAL CONNECTORS,NOTEBETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTION,INSTALLED IN THE AFT CABIN UTILITY AREA, (EWIS).NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHSEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/CAND/OR SEAT TO SEAT CONNECTION ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY - I: 144 MOALLAREA (ONLY IF CONTAMINATED), (EWIS).R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MOALLIN THIS AREA, (EWIS).20.0.273 AFT CABIN UNTILITY AREA OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS AND CIRCUIT BRAKERS "5005 VE" - I: 144 MOALLINSTALLED IN THE AFT CABIN UTILITY AREA OVERHEADCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.273 * * * * * C O N T I N U E * * * * *R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BRAKERS - I: 144 MOALL"5005 VE" AND "P" ROUTE INSTALLED IN THE AFT CABINUTILITY AREA OVERHEAD COMPARTMENT, (EWIS).20.0.315 TAIL CONE APU AND ACCESSORY COMPARTMENTR GVI 01 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 54 MOALLINSTALLED IN THE TAIL CONE FIREWALL AND APU AREA,(EWIS).20.0.319 HORIZONTAL STABILIZER CENTER BOXR GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).PRE 41600ORA340-300PRE 41600R GVI 02 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).POST 41600ORA340-300POST 41600R GVI 03 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-500CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).ORA340-60020.0.333 HORIZONTAL STABILIZER LATERAL BOXR GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 3 TOORRIB 4 LH / RH (EWIS)A340-300R SDI 02 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPRE 43491RIB 19LH / 20RH (EWIS)ORA340-300PRE 43491* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.333 * * * * * C O N T I N U E * * * * *R SDI 03 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPOST 43491RIB 13LH / 20RH (EWIS)PRE 44818ORA340-300POST 43491PRE 44818R GVI 04 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 13 TOPOST 43491RIB 20LH (EWIS)PRE 44818ORA340-300POST 43491PRE 44818R SDI 05 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPOST 44818RIB 20 LH/RH (EWIS)ORA340-300POST 44818R GVI 06 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-500LATERAL BOX EWIS (AS FAR AS VISIBLE) (EWIS)PRE 54173ORA340-600PRE 54173R GVI 07 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-500LATERAL BOX EWIS (AS FAR AS VISIBLE) (EWIS)POST 54173ORA340-600POST 5417320.0.346 HORIZONTAL STABILIZER SPAR BOX VENT TANKR GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-500SPAR BOX VENT TANK EWIS (AS FAR AS VISIBLE) (EWIS)PRE 54173ORA340-600PRE 54173* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.346 * * * * * C O N T I N U E * * * * *R GVI 02 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA340-500SPAR BOX VENT TANK EWIS (AS FAR AS VISIBLE) (EWIS)POST 54173ORA340-600POST 5417320.0.541 INNER FUEL TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER - I: 144 MOA340-200FUEL TANK (AS FAR AS VISIBLE)(EWIS).ORA340-300R GVI 02 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER - I: 144 MOA340-500FUEL TANK (AS FAR AS VISIBLE)(EWIS).ORA340-60020.0.542 OUTER/INNER FUEL TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS IN THE OUTER FUEL - I: 144 MOA340-200TANK (RIB 23 TO RIB 33)(AS FAR AS VISIBLE)(EWIS).ORA340-300R GVI 02 GENERAL VISUAL INSPECTION OF EWIS IN THE INNER FUEL - I: 144 MOA340-500TANK NO. 1/4 (RIB 6 TO RIB 11 AFT OF CENTRE SPAR TOORRIB 23)(RIB 11 TO RIB 23)(AS FAR AS VISIBLE)(EWIS).A340-60020.0.543 OUTER FUEL TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE OUTER - I: 144 MOA340-500FUEL TANK (AS FAR AS VISIBLE)(EWIS).ORA340-60020.0.550 VENT SURGE TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE VENT - I: 144 MOALLSURGE TANK (AS FAR AS VISIBLE)(EWIS).20.0.571 MAIN LANDING GEAR WELL.* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 11APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section20.0.571 * * * * * C O N T I N U E * * * * *R GVI 01 GENERAL VISUAL INSPECTION OF FUEL PUMP EWIS (AS FAR - I: 144 MOALLAS VISIBLE)(EWIS).* * * * * E N D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 12APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.00.00 AIR CONDITIONING21.21.00 CABIN AIR DISTRIBUTION AND RECIRCULATIONVC 01 VISUAL CHECK OF MIXER UNIT 9 I: 4 CALL02 TASK DELETEDDS 03 DISCARD RECIRCULATION FILTER ELEMENTS (PALL). 7 I: 5600 FHA340-200NOTE 15PRE 41323PRE 45081ORA340-300PRE 41323PRE 45081ORA340-500PRE 52635ORA340-600PRE 47159PRE 4874404 TASK RESERVED05 TASK RESERVEDDS 06 DISCARD VIDEO CONTROL CENTER AIR FILTER ELEMENTS 9 I: 1 AIF VCCNOTE 1INSTALLEDOP 07 OPERATIONAL CHECK OF "STAND ALONE" SMOKE DETECTION 9 I: 2 CA340-200SYSTEM VIA "SMOKE TEST" BUTTONIF VCCINSTALLEDORA340-300IF VCCINSTALLEDOP 08 OPERATIONAL CHECK OF VCC FAN DEACTIVATION BY USING 9 I: 2 CIF VCCTHE FAN OFF SWITCHINSTALLEDWITH A FANOFF SWITCH* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.21.00 * * * * * C O N T I N U E * * * * *R OP 09 OPERATIONAL CHECK TO VERIFY AUTOMATIC AND MANUAL 9 I: 2 CPOST 47197CLOSING OF BULK CREW REST COMPARTMENT ISOLATION NOTE 24ORVALVESPOST 47883ORPOST 50108OP 10 OPERATIONAL CHECK TO VERIFY PROPER FUNCTION OF RETURN 8 I: 20000 FHPOST 47197TO CABIN AURAL AND VISUAL COMMANDORPOST 47883ORPOST 50108DS 11 DISCARD ODOR RECIRCULATION FILTER ELEMENTS. 7 I: 2400 FHA340-200NOTE 15POST 45081ORA340-300POST 45081ORA340-500POST 52635ORA340-600POST 48744DS 12 DISCARD RECIRCULATION FILTER ELEMENTS (LE BOZEC - 7 I: 4000 FHA340-200DONALDSON). NOTE 15POST 41323ORA340-300POST 41323ORA340-600POST 4715921.23.00 LAVATORY/GALLEY VENTILATION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.23.00 * * * * * C O N T I N U E * * * * *DS 01 DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 7 I: 1200 FHA340-200NOTE 1POST 46135ORA340-300POST 46135ORA340-500ORA340-60002 TASK RESERVED21.25.00 AIR CONDITIONING COMPARTMENT VENTILATIONOP 01 OPERATIONAL CHECK OF ABNORMAL VENTILATION WARNING 9 I: CALLDI 02 DETAILED INSPECTION OF TURBOFAN SUPPLY DUCT 9 I: 4 CALLGVI 03 GENERAL VISUAL INSPECTION OF PICCOLO TUBES 9 I: 2 C ZL-193-01-1 ALLZL-193-01-2ZL-195-02-1ZL-195-02-2GVI 04 GENERAL VISUAL INSPECTION OF NACA AIR INLETS AND 9 I: CA340-500PICCOLO TUBES IN HYDRAULIC COMPARTMENTORA340-60021.26.00 AVIONICS EQUIPMENT VENTILATIONOP 01 OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION 9 I: CALLOP 02 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CALL(THIS TASK COVERS TASKS 73.25.00/02-C5 AND73.25.00/01-R5)OP 03 OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL 9 I: 2 CALLOP 04 OPERATIONAL CHECK OF COOLING EFFECT DETECTOR (AEVC 8 I: 10000 FHALLSYSTEM TEST)GVI 05 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-121-02-1 ALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.26.00 * * * * * C O N T I N U E * * * * *INSULATION ZL-121-02-2ZL-121-02-3RS 06 CLEANING OF RELAY BOX VU PANELS GRIDS 9 I: 2 CALL21.27.00 AVIONICS EQUIPMENT GROUND COOLINGOP 01 OPERATIONAL CHECK OF FAULT WARNING 9 I: 2 CPOST 40063PRE 51336PRE 51337GVI 02 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-121-02-1 POST 40063INSULATION ZL-121-02-2 PRE 51336ZL-121-02-3 PRE 51337OP 03 OPERATIONAL CHECK OF GRU START 9 I: 2 CPOST 46386PRE 51336PRE 5133721.28.00 LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING(FWD, AFT AND BULK)OP 01 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 3200 FHALLISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN NOTE 24ACASE OF SMOKE WARNING.(THIS TASK COVERS TASK 26.16.00/02).OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD 8 I: 3200 FHA340-300AIR VALVE IN CASE OF SMOKE WARNING NOTE 24APOST 40097ORA340-200POST 40188ORA340-600POST 47107ORA340-500POST 48738ORA340-600POST 47109* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.28.00 * * * * * C O N T I N U E * * * * *OP 03 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FHPOST 40379LOWER DECK MOBILE CREW REST ISOLATION VALVES IN NOTE 24PRE 56296CASE OF SMOKE WARNING.OR(THIS TASK COVERS TASK 26.18.00/05)A340-600POST 47937ORA340-500POST 48567OP 04 OPERATIONAL CHECK OF HARD WIRED BACKUP TO VERIFY 9 I: 4 CPOST 40379CLOSING OF LOWER DECK MOBILE CREW REST ISOLATIONPRE 56296VALVESORA340-600POST 47937ORA340-500POST 48567OP 05 OPERATIONAL CHECK OF HARD WIRED BACKUP OF VENTILATION 9 I: 4 CALLCONTROLLER (TO VERIFY CLOSING OF ISOLATION VALVES ANDCOLD AIR VALVE)DS 06 DISCARD FILTER ELEMENT OF BULK VIDEO COMPARTMENT 9 I: 2400 FHPOST 46441NOTE 1OP 07 OPERATIONAL CHECK OF AUTOMATIC AND MANUAL SHUT OFF OF 9 I: 2 CPOST 46441BULK VIDEO COMPARTMENT VENTILATION AND ELECTRICALPOWER AND CHECK NON RETURN VALVE IS IN CLOSEDPOSITION21.31.00 PRESSURE CONTROL AND MONITORINGOP 01 OPERATIONAL CHECK OF MANUAL MODE 8 I: 20000 FHALLOP 02 OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN 9 I: 2 CALLDITCHING CONFIGURATIONOP 03 OPERATIONAL CHECK OF OUTFLOW VALVE OPENING (50%) BY 9 I: 2 CALLEMERGENCY RAM AIR SWITCHOP 04 OPERATIONAL CHECK OF LANDING FIELD ELEVATION SELECTOR 9 I: 2 CALLBY MEANS OF INITIATED TEST (VIA MCDU)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.31.00 * * * * * C O N T I N U E * * * * *FC 05 FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P 6,9 I: 24000 FHALLPROTECTION OF SAFETY VALVES OR6 YENOTE 2406 TASK DELETEDOP 07 OPERATIONAL CHECK OF NEGATIVE PRESSURE RELIEF VALVE 9 I: 4 CALLOP 08 OPERATIONAL CHECK OF POSITION INDICATION OF SAFETY 9 I: 4 CALLVALVESRS 09 REMOVE SAFETY VALVE FOR RESTORATION. 9 I: 50000 FHALLOR12 YE21.50.00 AIR COOLING TEMPERATURE CONTROLRS 01 CLEAN FLIGHT DECK TEMPERATURE SENSORS 7 I: CALLOP 02 OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM 9 I: 2 CALLOPENINGDI 03 DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS 9 I: 4 CALLFOR CONDITION AND OPERATIONDI 04 DETAILED INSPECTION OF LP GROUND AIR CHECK VALVE 9 I: 24000 FHPRE 47063FLAPPERS FOR CONDITION AND OPERATION.VC 05 VISUAL CHECK OF PACK AIR SUPPLY DUCTS, CLAMPS AND 9 I: 24000 FHALLBELLOWS (BETWEEN PACK OUTLET AND MIXER UNIT)DI 06 DETAILED INSPECTION OF PACK DOWNSTREAM CHECK VALVES 6,9 I: 24000 FHALLFLAPPERS FOR CONDITION AND OPERATIONGVI 07 GENERAL VISUAL INSPECTION OF TRIM AIR DUCTS BETWEEN 9 I: 4 C ZL-137-01-1 ALLFLOW CONTROL VALVES AND HOT AIR MANIFOLDS ZL-137-01-2ZL-137-01-3ZL-191-02-1ZL-191-02-2* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.50.00 * * * * * C O N T I N U E * * * * *ZL-193-02-1ZL-193-02-2FC 08 REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK 9 I: 2 CPOST 40219NOTE 1RS 09 CLEANING OF CABIN TEMPERATURE SENSORS, SENSE LINES 7 I: 2 APRE 43750AND INLETS NOTE 1PRE 44729PRE 47063DS 10 DISCARD CABIN TEMPERATURE SENSOR FILTERS 7 I: 1 APOST 43750NOTE 1ORPOST 44729ORPOST 47063DI 11 DETAILED INSPECTION OF EMERGENCY RAM AIR AND LP 9 I: 4 CPOST 47063GROUND AIR CONNECTION FLAPPERS FOR CONDITION ANDOPERATIONDS 12 DISCARD FLOW CONTROL VALVE FILTERS 9 I: 2000 FCPOST 50213NOTE 1GVI 13 GENERAL VISUAL INSPECTION OF HEATSHIELDS FOR 8 I: 20000 FHPOST 49520CONDITION AND VISIBLE DAMAGERS 14 CLEANING AND DETAILED INSPECTION FOR EROSION OF PACK 7 I: 2 CALLWATER INJECTOR NOZZELS.DI 15 DETAILED INSPECTION OF EMERGENCY RAM AIR CHECK VALVE, 9 I: 4 CPRE 47063SKIN VALVE FLAPPERS FOR CONDITION AND OPERATION.21.70.00 HUMIDIFICATION SYSTEMN DS 01 DISCARD WATER FILTER ELEMENT. 7 I: 48 MOA340-500POST 47108ORA340-500POST 49639* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section21.70.00 * * * * * C O N T I N U E * * * * *N RS 02 REMOVE DUCT SENSOR UNIT FOR RESTORATION. 7 I: 24 MOA340-500POST 47108ORA340-500POST 49639N RS 03 REMOVE STEAM GENERATING UNIT FOR RESTAURATION. 7 I: 10 YEA340-500POST 47108ORA340-500POST 49639N DS 04 DISCARD STEAM HOSE. 7,9 I: 24 MOA340-500POST 47108ORA340-500POST 49639* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section22.00.00 AUTO FLIGHT22.10.00 AUTOPILOT/FLIGHT DIRECTOROP 01 OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION 9 I: 2 CALLOP 02 OPERATIONAL CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING 9 I: 4 CALLDEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS22.30.00 AUTOTHRUSTOP 01 OPERATIONAL CHECK OF A/THR ISOLATION FROM ENGINE 9 I: 4 CALLCONTROL22.60.00 FLIGHT ENVELOPENO TASK SELECTED22.70.00 FLIGHT MANAGEMENTOP 01 OPERATIONAL CHECK OF BACK-UP NAVIGATION FUNCTION 9 I: CALLOP 02 OPERATIONAL CHECK OF MCDU 3 TRANSFER 9 I: CALLOP 03 OPERATIONAL CHECK OF MCDU ANNUNCIATORS 9 I: CALLOP 04 OPERATIONAL CHECK OF FM SOURCE SWITCHING 9 I: 2 CALL22.90.00 AUTOFLIGHT SYSTEM BITENO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AUTO FLIGHT SECTION: C-22PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section23.00.00 COMMUNICATIONS23.11.00 HF SYSTEM (MOD 40068, 40069)NO TASK SELECTED23.12.00 VHF SYSTEMNO TASK SELECTED23.24.00 AIRCRAFT COMMUNICATIONS ADDRESSING & REPORTING SYSTEM (ACARS)(MOD 40065)NO TASK SELECTED23.28.00 SATELLITE COMMUNICATIONNO TASK SELECTED23.33.00 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)OP 01 OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION 9 I: 2 CIF IFESFROM FLIGHT DECK (IF INSTALLED) AND CABININSTALLEDDS 02 DISCARD IFE-RACK FILTERS. 9 I: 2400 FHIF IFE-RACKSWITHAIR-FILTERSINSTALLEDR RS 03 CLEANING OF VENTILATION GRIDS AND VENTILATOR HOUSING 9 I: 10000 FHIF VCC OR(IF INSTALLED) FROM IFE COMPONENTS INSTALLEDRCCIN THE CABIN (VCC/RCC)INSTALLED23.39.01 SATELLITE TV TRANSCEIVER SYSTEM TAILWIND (TW560) ANDPANASONIC (IDTV)R DS 01 DISCARD ALL FILTER ELEMENTS ON TAILWIND SYSTEM. 7 I: AIF TAILWINDSYSTEMINSTALLEDISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section23.39.02 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION BY BOEING (CBB).OP 01 OPERATIONAL CHECK OF CONNEXION BY BOEING SYSTEM 9 I: 4 CIF CBBPOWER OFF PROCEDURE.SYSTEMINSTALLEDOP 02 OPERATIONAL CHECK OF COOLING LOSS DETECTION OF 9 I: 4 CIF CBBCONNEXION BY BOEING SYSTEM.SYSTEMINSTALLED23.42.00 COCKPIT TO GROUND CREW CALL SYSTEMNO TASK SELECTED23.51.00 AUDIO MANAGEMENT (INTEGRATING/FLIGHT INTERPHONE/SELCAL/CALL)OP 01 OPERATIONAL CHECK OF OXYGEN MASK MICROPHONE 9 I: CALLOP 02 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING 9 I: CALL(COVERED BY MSI 23-71-00, TASK NO1)OP 03 OPERATIONAL CHECK OF CAPTAIN AND F/O ACP SWITCHING TO 9 I: 2 CALLTHIRD ACP23.61.00 STATIC DISCHARGERFC 01 CHECK RESISTANCE FROM THE DISCHARGER TO THE BASE 9 I: CALL(RETAINER) AND FROM THE BASE (RETAINER) TO THEAIRCRAFT STRUCTUREGVI 02 GENERAL VISUAL INSPECTION OF STATIC DISCHARGER. 9 I: CALL23.71.00 COCKPIT VOICE RECORDEROP 01 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING 9 I: CALL(THIS TASK COVERS TASK 23.51.00/02)OP 02 OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING 9 I: CALLTIME DELAY RELAYDS 03 DISCARD ULB BATTERY 9 I: VRALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section23.71.00 * * * * * C O N T I N U E * * * * *OP 04 OPERATIONAL CHECK OF THE ULB 9 I: VRALL23.72.00 COCKPIT DOOR SURVEILLANCE SYSTEM (CDSS)NO TASK SELECTED23.73.00 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)R OP 01 OPERATIONAL CHECK OF CABIN SIGNS VIA MCDU 9 I: 2 AA340-200NOTE 26PRE 44058PRE 45556ORA340-300PRE 44058PRE 45556ORA340-300PRE 48823ORA340-500PRE 47057ORA340-600PRE 47057OP 02 OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU 9 I: 1 CALLNOTE 26R OP 03 OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, 9 I: 2 CALLDEUS-A CUT OFF FUNCTIONOP 04 OPERATIONAL CHECK OF EVAC FUNCTION 9 I: 2 CIF EVACINSTALLEDR OP 05 OPERATIONAL CHECK OF HOT BATTERY BUS POWERED CIDS 9 I: 20000 FHPOST 43319OPERATIONPRE 4931406 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section23.73.00 * * * * * C O N T I N U E * * * * *07 TASK DELETEDOP 08 OPERATIONAL CHECK OF LDL/LDF SIGNS VIA MCDU 9 I: 4 CIF LDL/LDFNOTE 26INSTALLEDR OP 09 OPERATIONAL CHECK OF EMERGENCY CABIN ALERT SYSTEM 9 I: 2 CPOST 50156(ECAS)ORPOST 50157N OP 10 OPERATIONAL CHECK OF BATTERY POWERED CIDS PA 9 I: 20000 FHA340-500OPRERATION.ORA340-600ORPOST 4931423.75.00 TAXI AID CAMERA SYSTEM (TACS)OP 01 OPERATIONAL CHECK OF THE VIDEO DISCONNECTION SWITCH 9 I: CA340-600(999VU) FUNCTIONORA340-500POST 4913023.81.00 RADIO MANAGEMENTOP 01 OPERATIONAL CHECK OF RMP LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF RADIO NAVIGATION BACK-UP MODE 9 I: CALL* * * * * E N D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section24.00.00 ELECTRICAL POWER24.20.00 AC GENERATIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(THIS TASK COVERS TASKS 24.50.00/01 AND 24.60.00/01) NOTE 24OP 02 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FHALLSUPPLY NOTE 24(THIS TASK COVERS TASK 24.30.00/01)03 TASK DELETEDOP 04 OPERATIONAL CHECK OF LIGHTS. 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)DS 05 DRAIN IDG OIL SYSTEM, DISCARD FILTER ELEMENT(S) 7 I: AALLAND REPLENISHFC 06 CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT 9 I: 2100 FHALLOP 07 OPERATIONAL CHECK OF AC GENERATION SIDE 1 AND SIDE 2 9 I: CALLISOLATIONOP 08 OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS 9 I: CALLOP 09 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION MANUAL 9 I: CALLSWITCHINGOP 10 OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC 8 I: 18 MOALLCONNECTION NOTE 24BOP 11 OPERATIONAL CHECK OF EMERGENCY GENERATOR MANUAL 8 I: 18 MOALLCONNECTION NOTE 24OP 12 OPERATIONAL CHECK OF CSM/G DISCONNECTION WITH 8 I: 18 MOALLSIMULATED ENGINES FLAMED OUT CONDITION AND SLATS NOTE 24BEXTENDEDRS 13 CLEAN IDG OIL COOLER 7 I: 4 CALLOP 14 OPERATIONAL CHECK OF IDG DISCONNECT FUNCTION 9 I: 4 CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section24.20.00 * * * * * C O N T I N U E * * * * *OP 15 OPERATIONAL CHECK OF GENERATOR SHUT-DOWN WHEN ENGINE 9 I: 60 MOALLFIRE HANDLE IS OPERATED(COVERED BY MSI 26-21-00, TASK NO3).16 TASK DELETEDOP 17 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION 9 I: CALLAUTOMATIC SWITCHING18 TASK DELETED24.30.00 DC GENERATIONOP 01 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FHALLSUPPLY (COVERED BY MSI 24-20-00, TASK NO2). NOTE 2402 TASK DELETEDR RS 03 REMOVE BATTERIES (1, 2, APU) FOR OVERHAUL 6 I: VRALLOP 04 OPERATIONAL CHECK OF DC MAIN GENERATION SWITCHING 9 I: 1 CALLNOTE 24BOP 05 OPERATIONAL CHECK OF DC ESSENTIAL GENERATION 9 I: CALLSWITCHINGOP 06 OPERATIONAL CHECK OF DC BAT BUS AND DC ESS BUS 8 I: 800 FHALLISOLATION24.40.00 EXTERNAL POWER01 TASK DELETEDISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section24.50.00 AC ELECTRICAL LOAD DISTRIBUTIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(COVERED BY MSI 24-20-00, TASK NO1). NOTE 24OP 02 OPERATIONAL CHECK OF COMMERCIAL LOAD SHEDDING 9 I: CALLOP 03 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MOALL(THIS TASK COVERS TASK 24.60.00/02)OP 04 OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN 9 I: 2 CALLEMERGENCY CONFIGURATION05 TASK RESERVED06 TASK RESERVED24.54.00 ELECTRICAL LOAD MANAGEMENT SYSTEMOP 01 OPERATIONAL CHECK OF THE ELMU OUTPUTS ACTIVATION BY 9 I: 2 CPOST 47019MCDU24.60.00 DC ELECTRICAL LOAD DISTRIBUTIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(COVERED BY MSI 24-20-00, TASK NO1). NOTE 24OP 02 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MOALL(COVERED BY MSI 24-50-00, TASK NO3).* * * * * E N D * * * * *ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.00.00 EQUIPMENT/FURNISHINGS25.11.00 COCKPIT SEATSDI 01 DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT 8 I: 6 YEALLATTACHMENTFC 02 FUNCTIONAL CHECK OF HORIZONTAL/VERTICAL MECHANICAL 6,9 I: CALLCONTROL CABLE ADJUSTMENT OF COCKPIT SEATS25.21.00 PASSENGER COMPARTMENT SEATSGVI 01 GENERAL VISUAL INSPECTION OF SEAT TO FLOOR 8 I: 36 MOALLATTACHMENT.GVI 02 GENERAL VISUAL INSPECTION OF LOWER SEAT STRUCTURE, 8 I: 36 MOALLBAGGAGE RESTRAINT BAR, BACKREST AND BACKREST SUPPORT.OP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MOALLBELT ATTACHMENTSR OP 04 OPERATIONAL CHECK OF ELECTRONIC CIRCUIT OF THE 8 I: VRIF INFLATABLEINFLATABLE RESTRAINT SYSTEM.RESTRAINTSYSTEMINSTALLEDRS 05 REMOVE SEAT BELT SYSTEM FOR RESTORATION OF AIRBAG 7,8 I: VRIF INFLATABLEAND DISCARD BATTERY, HOSE, SQUIB AND GAS STORAGERESTRAINTACCORDING TO CMMSYSTEMINSTALLED25.22.00 CABIN ATTENDANT SEATSGVI 01 GENERAL VISUAL INSPECTION OF SEAT ATTACHMENT POINTS. 8 I: 36 MOALLGVI 02 GENERAL VISUAL INSPECTION OF SEAT STRUCTURE. 8 I: 36 MOALLOP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MOALLBELT ATTACHMENTS25.23.44 LININGS AND FURNISHINGS (DADO PANELS)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.23.44 * * * * * C O N T I N U E * * * * *VC 01 VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS 8 I: 18 MOALLIN CABIN ARE CLOSEDOP 02 OPERATIONAL CHECK OF CABIN DECOMPRESSION PANELS 9 I: 4 CALLOPENING25.24.00 OVERHEAD STOWAGE COMPARTMENTSNO TASK SELECTED25.27.00 DOOR AREA HEATING SYSTEMR OP 01 OPERATIONAL CHECK OF THE DOOR AREA HEATING SYSTEM BY 9 I: 2 CA340-200USING THE TEST BUTTON ON EACH CONTROL UNIT.POST 45670PRE 47423PRE 51617ORA340-300POST 45670PRE 47423PRE 51617ORA340-300POST 45670PRE 5674625.30.00 BUFFET AND GALLEYDS 01 DISCARD GALLEY AIR EXTRACTION FILTER ELEMENT 9 I: 1400 FHALL02 TASK DELETEDDI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 CALLPOINTS(COVERED BY SSI ́S 53.11.72, 53.21.34, 53.31.70,53.41.59, 53.18.72, 53.22.34, 53.38.70 AND 53.42.59)04 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.30.00 * * * * * C O N T I N U E * * * * *OP 05 OPERATIONAL CHECK OF EMERGENCY EXIT HATCH FROM BOTH 8 I: 18 MOPOST 49657SIDES25.34.00 GALLEY COOLINGRS 01 CLEAN AIR CHILLER CONDENSER AIR FILTER. 7 I: 1400 FHIF AIR CHILLERNOTE 1SYSTEMINSTALLEDRS 02 CLEAN REMOTE CHILLER CONDENSER AIR FILTER. 7 I: 1400 FHA340-500NOTE 1POST 48451ORA340-600POST 48451RS 03 CLEAN GAC "AIR OVER" FILTER. 7 I: 1400 FHA340-500NOTE 1POST 48451ORA340-600POST 48451RS 04 CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES 7 I: 1400 FHIF AIR CHILLERIN THE GALLEY CABINET. NOTE 1SYSTEM ANDGALLEY WITHGRILLESINSTALLED25.38.00 LIFT SYSTEMOP 01 OPERATIONAL CHECK OF THE CAGE STOP FUNCTION. 9 I: 40 MOA340-600POST 49657DI 02 DETAILED INSPECTION OF TOOTH BELTS, BELT PULLEYS, 7,9 I: 80 MOA340-600ATTACHMENT POINTS AND FLOOR PAN.POST 49657OP 03 OPERATIONAL CHECK OF LIFT SYSTEM SENSORS, USING THE 9 I: 80 MOA340-600MAINTENANCE PANEL ON THE CONTROL UNIT.POST 49657ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.40.00 LAVATORIESR DI 01 DETAILED INSPECTION OF WASTE COMPARTMENT FOR FIRE 9 I: 1 CALLCONTAINMENT CAPABILITY. ORNRNOTE 8R OP 02 OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP 9 I: 1 CALLORNRNOTE 8DI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 CALLPOINTS(COVERED BY SSI ́S 53.11.72, 53.21.34, 53.31.70,53.41.59, 53.18.72, 53.22.34, 53.38.70 AND 53.42.59)04 TASK DELETED25.47.00 LOWER DECK LAVATORIES01 TASK RESERVED02 TASK RESERVED25.51.00 LOWER DECK CARGO LOADING SYSTEMR OP 01 OPERATIONAL CHECK OF POWER DRIVE UNITS (NOTE 11) 9 I: CA340-200PRE 55380ORA340-300PRE 55380ORA340-500ORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *R DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA340-200PRE 55380ORA340-300PRE 55380ORA340-500ORA340-600R DI 03 REMOVE CREW REST ROOM CONTAINER LATCHES AT C53.7 8 I: 34000 FHA340-200FOR DETAILED INSPECTION.POST 40611R GVI 04 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES 9 I: A ZL-131-01-1 A340-200ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R GVI 05 GENERAL VISUAL INSPECTION OF OVERRIDEABLE Y-DOOR SILL 9 I: A ZL-131-01-1 A340-200LATCHES ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS 9 I: A ZL-131-01-1 A340-200ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *R GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS 9 I: A ZL-131-01-1 A340-200INCLUDING TRANSPORT ROLLER. (NOTE11) ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 300 FCA340-200WEAR AND DAMAGE. (NOTE 11)PRE 55380ORA340-300PRE 55380ORA340-500ORA340-600R GVI 09 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS (NOTE 9 I: 4 A ZL-131-01-1 A340-20011) ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R GVI 10 GENERAL VISUAL INSPECTION OF XZ-LATCHES (NOTE 11) 8 I: 3200 FH ZL-131-01-1 A340-200ZL-131-01-2 PRE 55380ORA340-300PRE 55380ORA340-500ORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *R GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AT C20, C39, 9 I: 4 A ZL-131-01-1 A340-200C53.2 (NOT FOR A340-500), C53.8 (A340-500 ONLY), ZL-131-01-2 PRE 55380C57.1 (WITH MOD 49689), C65 AND C68 (NOTE 11) ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R GVI 12 GENERAL VISUAL INSPECTION OF FIXED, RETRACTABLE AND 9 I: 4 A ZL-131-01-1 A340-200OVERRIDEABLE YZ-LATCHES (NOTE 11) ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600R GVI 13 GENERAL VISUAL INSPECTION OF Y-GUIDE ROLLERS, 9 I: C ZL-131-01-1 A340-200AUTOMATIC Z-GUIDE, GUIDE RAILS, YZ-LATCH GUIDE ZL-131-01-2 PRE 55380ROLLERS, XY-ENTRANCE GUIDE ASSEMBLIES, Y-GUIDES AND ZL-151-01-1 ORY-GUIDE ACTUATION MECHANISMS (A340-200 OR A340-300A340-300ONLY)(AND X-GUIDES WITH MOD40208) (NOTE 11)PRE 55380ORA340-500ORA340-600R DI 14 REMOVE ACT LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA340-300POST 42612ORA340-200POST 44001ORA340-200POST 44004ORA340-200POST 4400315 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *GVI 16 GENERAL VISUAL INSPECTION OF ROLLER KITS. 9 I: A ZL-131-01-2 A340-500ZL-151-01-1 POST 51454ORA340-600POST 51451R GVI 17 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-131-01-1 A340-200ZL-131-01-2 PRE 55380ZL-151-01-1 ORA340-300PRE 55380ORA340-500ORA340-600GVI 18 GENERAL VISUAL INSPECTION OF PALLET STOP. 9 I: 4 A ZL-131-01-1 A340-200POST 42261ORA340-300POST 42261N OP 19 OPERATIONAL CHECK OF BRAKING ROLLER. 9 I: 2 CA340-200PRE 55380ORA340-300PRE 55380ORA340-500ORA340-600N 20 TASK RESERVED25.51.01 ADVANCED LOWER DECK CARGO LOADING SYSTEMN OP 01 OPERATIONAL CHECK OF SWIVEL NOSE AT XZ-LATCHES EG 9 I: 4 CA340-300(ENTRANCE GUIDE) AND SWIVEL NOSES AT OVERRIDEABLEPOST 55380CENTER LATCHES. (NOTE 11)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.01 * * * * * C O N T I N U E * * * * *N DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA340-300POST 55380N 03 TASK RESERVEDN OP 04 OPERATIONAL CHECK OF BRAKING ROLLER AND SWIVEL 9 I: 2 CA340-300CASTER. (NOTE 11)POST 55380N GVI 05 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES AND 9 I: A ZL-131-01-1 A340-300OVERRIDEABLE ARO DEVICES. ZL-151-01-1 POST 55380N GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS, BALL MATS 9 I: A ZL-131-01-1 A340-300AND BALL STRIPS. ZL-151-01-1 POST 55380N GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS, TRANSPORT 9 I: A ZL-131-01-1 A340-300ROLLERS. (NOTE 11) ZL-151-01-1 POST 55380N DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 1500 FCA340-300WEAR AND DAMAGE. (NOTE 11) ORPOST 5538018 MON GVI 09 GENERAL VISUAL INSPECTION OF OVERRIDEABLE CENTER 9 I: 4 A ZL-131-01-1 A340-300LATCHES AND SPLITTER. (NOTE 11) ZL-151-01-1 POST 55380N GVI 10 GENERAL VISUAL INSPECTION OF XZ-LATCHES. (NOTE 11) 8 I: 3200 FHA340-300POST 55380N GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AND 9 I: 4 A ZL-131-01-1 A340-300XZ-LATCHES EG (ENTRANCE GUIDE). (NOTE 11) ZL-151-01-1 POST 55380N GVI 12 GENERAL VISUAL INSPECTION OF FIXED YZ-LATCHES AND 9 I: 4 A ZL-131-01-1 A340-300YZ-LATCHES WITH TRANSPORT ROLLER (MOD 56837). ZL-151-01-1 POST 55380(NOTE 11)N GVI 13 GENERAL VISUAL INSPECTION OF YZ LATCH-GUIDE ROLLERS, 9 I: C ZL-131-01-1 A340-300LATERAL ENTRANCE GUIDE, Y-GUIDE 42 L, SCUFF PLATE ZL-151-01-1 POST 55380ROLLER, SIDE GUIDES, ENTRANCE ROLLER, DOOR SILL LATCHSUPPORT ROLLER AND OVERROLLABLE GUIDE (MOD 56837).(NOTE 11)N GVI 14 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-131-01-1 A340-300ZL-151-01-1 POST 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.51.01 * * * * * C O N T I N U E * * * * *N GVI 15 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS AND 9 I: 4 A ZL-131-01-1 A340-300SWIVEL CASTERS. (NOTE 11) ZL-151-01-1 POST 5538025.52.00 LOWER DECK AFT AND FORWARD CARGO COMPARTMENTVC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING 8 I: 8 DYALLSTRIPS, PROTECTION PLATES, CENTER LINE COVER PLATESAND ACCESS DOORS (NOTE 11).VC 02 VISUAL CHECK OF DECOMPRESSION PANELS (NOTE 11) 8 I: 8 DYALLR VC 03 VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE 9 I: AALLROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OFCLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY.(NOTE 11)N OP 04 OPERATIONAL CHECK OF AIR STOP VALVES FOR HEATED 9 I: 4 CA340-300DRAINAGE SYSTEM.POST 43719ORA340-300POST 56834ORA340-500POST 49059ORA340-600POST 47115N GVI 05 GENERAL VISUAL INSPECTION OF THE DRAINAGE SYSTEM 9 I: 4 C ZL-133-01-1 ALLINSTALLATION. ZL-153-01-1ZL-153-01-2ZL-163-01-1ZL-163-01-2N VC 06 VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR 9 I: AA340-300EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN ASPOST 55380NECESSARY.25.54.00 LOWER DECK BULK CARGO COMPARTMENT* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.54.00 * * * * * C O N T I N U E * * * * *VC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS 8 I: 8 DYA340-200AND ACCESS DOOR AT C73.OR(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDA340-300IN REMAINING AREA)ORA340-500PRE 47883ORA340-600PRE 47883VC 02 VISUAL CHECK OF DECOMPRESSION PANELS. 8 I: 8 DYA340-200(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDORIN REMAINING AREA)A340-300ORA340-500PRE 47883ORA340-600PRE 47883GVI 03 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-161-01-1 A340-200(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDORIN REMAINING AREA)A340-300ORA340-500PRE 47883ORA340-600PRE 47883R DI 04 DETAILED INSPECTION OF DIVIDER NETS, NET 9 I: CA340-200ATTACHMENT POINTS, NET CONNECTING DEVICES AND TENSIONORBUCKLES.A340-300(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDORIN REMAINING AREA)A340-500PRE 47883ORA340-600PRE 47883* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 11APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.54.00 * * * * * C O N T I N U E * * * * *R DI 05 DETAILED INSPECTION OF NET SCREENS, NET SCREEN 9 I: CA340-200ATTACHMENT POINTS AND TENSION BUCKLES.OR(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDA340-300IN REMAINING AREA)ORA340-500PRE 47883ORA340-600PRE 47883R DI 06 DETAILED INSPECTION OF SCREEN DECOMPRESSION 9 I: CA340-200TARPAULINS.OR(NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMEDA340-300IN REMAINING AREA)ORA340-500PRE 47883ORA340-600PRE 4788325.61.00 COCKPIT ESCAPE FACILITIESVC 01 VISUAL CHECK OF EMERGENCY ESCAPE ROPE AND ROPE 8 I: 6 YEALLATTACHMENT25.62.00 CABIN ESCAPE FACILITIESFC 01 REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST 6 I: NRALLORVRR RS 02 RESTORATION OF LIFE RAFTS BY REMOVAL AND REPLACEMENT 8 I: VRALLWITH OVERHAULED.R OP 03 OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT - I: NRALLORVRNOTE 10DS 04 DISCARD SQUIB 8 I: VRA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 12APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.62.00 * * * * * C O N T I N U E * * * * *OP 05 OPERATIONAL CHECK OF THE SRPSU VIA MCDU 8 I: 20000 FHA340-600OP 06 BATTERY CAPACITY CHECK OF THE SRPSU VIA MCDU 8 I: 6 MOA340-600OP 07 OPERATIONAL CHECK OF THE ELECTRICAL CIRCUIT INCLUDING 8 I: 20000 FHA340-600SQUIB NOTE 24B25.65.32 EMERGENCY LOCATOR TRANSMITTER (PORTABLE)R RS 01 REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER 9 I: VRIF SURVIVAL(ELT(S)) FOR WORKSHOP CHECK.ELT INSTALLED25.65.34 EMERGENCY VHF TRANSCEIVERFC 01 REMOVE EMERGENCY VHF TRANSCEIVER FOR SHOP INSPECTION 9 I: VRIF EMERGENCYORVHF TRANSCEIVER24 MOINSTALLED25.65.35 EMERGENCY LOCATOR TRANSMITTER SYSTEMR OP 01 OPERATIONAL CHECK OF AUTOMATIC FIXED 8 I: 18 MOIF AUTOMATICEMERGENCY LOCATOR TRANSMITTER (ELT(AF))FIXED ELTSYSTEM BY MANUAL ACTIVATION.INSTALLEDR RS 02 REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER 8 I: VRIF AUTOMATIC(ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDINGFIXED ELTBATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELTINSTALLEDACTIVATION.25.65.51 MEGAPHONEDS 01 DISCARD MEGAPHONE BATTERIES 9 I: VRALLOP 02 OPERATIONAL CHECK OF MEGAPHONE 9 I: CALL25.66.52 LIFE VESTR RS 01 RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT 9 I: VRALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 13APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.66.52 * * * * * C O N T I N U E * * * * *WITH OVERHAULED.25.74.00 CREW REST ROOM (CABIN)DI 01 DETAILED INSPECTION OF SEAT BELTS, BELT ATTACHMENTS 8 I: 36 MOIF FCRCAND BUNK STRUCTURE.INSTALLEDGVI 02 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-221-02-1 IF FCRCATTACHMENT POINTS OF THE CREW REST ROOM (REST ROOM ZL-221-02-2 INSTALLEDREMOVED). ZL-223-01-225.75.00 CREW REST ROOM (UNDERFLOOR)OP 01 OPERATIONAL CHECK OF EMERGENCY EXIT HATCH OPENING 8 I: 18 MOIF BCRC ORFROM INSIDE AND FROM OUTSIDELDMCR OR DCRINSTALLEDDI 02 DETAILED INSPECTION OF BED BELTS AND BELT ATTACHMENTS 8 I: 36 CRR MOIF BCRC ORON CREW REST BUNKSLDMCR OR DCRINSTALLED03 TASK DELETEDVC 04 VISUAL CHECK OF CARGO COMPARTMENT CEILING WELL, 8 I: 6 YEIF BCRC ORINTERFACE LININGS AND OF THE OUTSIDE OF THE CONTAINERLDMCR OR DCRINSTALLEDGVI 05 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-251-02-1 IF BCRC ORATTACHMENT POINTS OF THE STAIRHOUSE (STAIRHOUSE ZL-251-02-2 LDMCR INSTALLEDREMOVED). ZL-251-02-3ZL-253-01-1OP 06 OPERATIONAL CHECK OF DOOR HINGE AND LOCK 9 I: 36 CRR MOIF LDMCR ANDLDL OR DCRINSTALLEDOP 07 OPERATIONAL CHECK OF FULL BCRC KICK THROUGH PANEL 8 I: 40000 FHIF FULL BCRCFROM BOTH SIDESINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 14APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section25.75.00 * * * * * C O N T I N U E * * * * *VC 08 VISUAL CHECK OF BCRC LINING AND MAINTENANCE ACCESS 8 I: 6 YEIF BCRCPANELSINSTALLEDDI 09 DETAILED INSPECTION OF FULL BCRC FLIGHT CREW SEAT 8 I: 36 MOIF BCRCBELT, SEAT ATTACHMENT AND STRUCTUREINSTALLEDVC 10 VISUAL CHECK OF DECOMPRESSION PANEL 8 I: 800 FHIF BCRCINSTALLEDGVI 11 GENERAL VISUAL INSPECTION OF MAIN AND EMERGENCY HATCH 8 I: 6 YEIF BCRCSEALSINSTALLEDGVI 12 GENERAL VISUAL INSPECTION OF THE LADDER ASSEMBLY 6 I: 2 CIF BCRCINSTALLEDVC 13 VISUAL CHECK OF HATCH SEAL, DOOR SEALS AND BELLOW 8 I: 36 MOIF LDMCR OR DCRSEALS.INSTALLED25.76.00 TIRE DEBRIS RETENTION SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF TYRE DEBRIS RETENTION 9 I: A ZL-147-01-1 A340-200SYSTEMORA340-300* * * * * E N D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 15APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.00.00 FIRE PROTECTION26.11.00 MAIN LANDING GEAR FIRE AND OVERHEAT DETECTIONOP 01 BITE TEST OF THE FDU THROUGH MCDU 8 I: 800 FHA340-500ORA340-60026.12.00 ENGINE FIRE AND OVERHEAT DETECTIONNO TASK SELECTED26.13.00 APU FIRE AND OVERHEAT DETECTIONOP 01 OPERATIONAL CHECK OF APU FIRE AND OVERHEAT DETECTION 9 I: 8000 FHALLLOOPS(COVERED BY MSI 26.22.00, TASK NO1)26.15.00 AVIONICS COMPARTMENT SMOKE DETECTIONOP 01 OPERATIONAL CHECK OF AVIONICS COMPARTMENT SMOKE 9 I: 4 AALLDETECTION BY PTT NOTE 5RS 02 REMOVE AVIONICS SMOKE DETECTION PICCOLO TUBES FOR 8 I: 36 MOALLCLEANING03 TASK DELETED26.16.00 LOWER DECK CARGO COMPARTMENT SMOKE DETECTIONOP 01 OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE 9 I: 4 AALLDETECTION BY PTT NOTE 5OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 9 I: CALLCARGO COMPARTMENT ISOLATION VALVES(COVERED BY MSI 21-28-00, TASK NO1)03 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.16.00 * * * * * C O N T I N U E * * * * *26.17.00 LAVATORY SMOKE DETECTION01 TASK DELETED26.18.00 AUXILIARY AREAS SMOKE DETECTIONOP 01 OPERATIONAL CHECK OF LDMCR 9 I: 2 APOST 40413SMOKE DETECTION BY PTT NOTE 25ORPOST 40716ORPOST 43380ORPOST 51736ORPOST 53319ORPOST 53688RS 02 REMOVE AND CLEAN LDMCR SMOKE 6 I: 72 CRR MOPOST 40413DETECTORSORPOST 40716ORPOST 43380ORPOST 51736ORPOST 53319ORPOST 53688* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.18.00 * * * * * C O N T I N U E * * * * *OP 03 OPERATIONAL CHECK OF LDMCR STAIRHOUSE SMOKE DETECTION 9 I: CPOST 40413SYSTEM BY MCDUORPOST 40716ORPOST 43380ORPOST 51736ORPOST 53319ORPOST 53688OP 04 OPERATIONAL CHECK OF FCRC SMOKE DETECTION SYSTEM 9 I: CPOST 40716BY MCDUORPOST 53391OP 05 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FHPOST 40413LDMCR ISOLATION VALVE (IN CASE OFORFIRE IN LDMCR STAIRHOUSE OR CREW REST ROOM)POST 40716(COVERED BY MSI 21-28-00, TASK NO 3)ORPOST 43380ORPOST 51736ORPOST 53319ORPOST 53688OP 06 OPERATIONAL CHECK OF LDMCR 9 I: 18 CRR MOPOST 40413SMOKE DETECTORS WITH AEROSOLORPOST 40716ORPOST 43380ORPOST 51736ORPOST 53319ORPOST 5368807 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.18.00 * * * * * C O N T I N U E * * * * *OP 08 OPERATIONAL CHECK OF SDCU/CIDS 8 I: 18 MOPOST 51992TO VERIFY AUTOMATIC CLOSINGOROF BCRC ISOLATION VALVE (IN CASE OF FIRE)POST 52634ORPOST 53220OP 09 OPERATIONAL CHECK OF BCRC STAIRHOUSE 9 I: CPOST 51992SMOKE DETECTION SYSTEM BY MCDUORPOST 52634ORPOST 53220OP 10 OPERATIONAL CHECK OF VCC SMOKE DETECTION BY MCDU. 8 I: 18 MOPOST 49101ORPOST 48972ORPOST 50091ORPOST 49829RS 11 REMOVE VCC PICCOLO TUBES FOR CLEANING. 7 I: 18000 FHPOST 49101ORPOST 48972ORPOST 50091ORPOST 49829OP 12 OPERATIONAL CHECK OF IFES SMOKE DETECTION BY MCDU. 8 I: 18 MOPOST 47540ORPOST 48818RS 13 REMOVE IFES PICCOLO TUBES FOR CLEANING. 7 I: 18000 FHPOST 47540ORPOST 48818RS 14 REMOVE AND CLEAN LDF AFT (DCR) SMOKE DETECTOR. 8 I: 72 CRR MOPOST 49657OP 15 OPERATIONAL CHECK OF LDF AFT (DCR) SMOKE DETECTION BY 8 I: 1400 CRRPOST 49657PTT. FHOP 16 OPERATIONAL CHECK OF LDF AFT (DCR) SMOKE DETECTOR 8 I: 18 CRR MOPOST 49657WITH AEROSOL.* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.18.00 * * * * * C O N T I N U E * * * * *RS 17 REMOVE AND CLEAN LDF AFT - AREA AROUND STAIRS SMOKE 6 I: 4 CPOST 49657DETECTOR.OP 18 OPERATIONAL CHECK OF FCC SMOKE DETECTION BY MCDU. 9 I: CPOST 54128N RS 19 REMOVE AND CLEAN PICCOLO TUBES OF FCC RACK SMOKE 8 I: 18000 FHPOST 54128DETECTION.ORPOST 54477ORPOST 54762ORPOST 54946N OP 20 OPERATIONAL CHECK OF ALNAV2 CENTER RACK IV SMOKE 9 I: 18 MOPOST 56389DETECTION BY MCDUN RS 21 REMOVE AND CLEAN PICCOLO TUBES OF ALNAV2 CENTER RACK 8 I: 17000 FHPOST 56389IV SMOKE DETECTION.26.18.01 BULK AVIONICS COMPARTMENT SMOKE DETECTIONRS 01 REMOVE AND CLEAN BULK AVIONICS SMOKE DETECTOR PICCOLO 8 I: 36 MOIF VIDEO RACKTUBESIN BACINSTALLEDOP 02 OPERATIONAL CHECK OF THE BULK AVIONICS COMPARTMENT 9 I: CIF VIDEO RACKSMOKE DETECTION SYSTEM VIA MCDUIN BACINSTALLED26.21.00 ENGINE FIRE EXTINGUISHINGOP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING SYSTEM 9 I: 1 AALLNOTE 5OP 02 OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER BOTTLE 9 I: CALLLOW PRESSURE INDICATING CIRCUITOP 03 OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW 8 I: 18 MOALLFUNCTION(THIS TASK COVERS TASKS 24.20.00/15, 28.24.00/02 AND36.00.00/04)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.21.00 * * * * * C O N T I N U E * * * * *FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,9 I: NR OR VRALLPRESSURE SWITCH SETTING NOTE 805 TASK DELETED06 TASK DELETEDFC 07 FUNCTIONAL CHECK OF FIRING CIRCUIT CONTINUITY 9 I: 2 CALLFC 08 FUNCTIONAL CHECK OF DISTRIBUTION PIPING FOR LEAKAGE 8 I: 12000 FHALLAND OBSTRUCTIONDS 09 DISCARD CARTRIDGE 9 I: VRALL26.22.00 APU FIRE EXTINGUISHINGOP 01 OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM 9 I: 2 AALL(THIS TASK COVERS TASK 26.13.00/01)OP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA 9 I: 4800 FHALLMCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF,6WF)(THIS TASK COVERS TASKS 49.62.00/03 FOR A340-200OR A340-300 AND 49.62.00/04 FOR A340-500 OR A340-600)OP 03 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 9 I: CALLTRIGGER CIRCUIT04 TASK DELETEDFC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 7,9 I: VRALLPRESSURE SWITCH SETTING ORNRNOTE 806 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.22.00 * * * * * C O N T I N U E * * * * *OP 07 OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 9 I: 2 CALLDI 08 DETAILED INSPECTION OF DISTRIBUTION PIPING FOR CRACKS 8 I: 14000 FHALLOP 09 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 36 MOALLOP 10 OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION 8 I: 36 MOALL(THIS TASK COVERS TASKS 28.29.00/01 AND 49.62.00/04FOR A340-200 OR A340-300 AND 49.62.00/03 FOR A340-500OR A340-600)DS 11 DISCARD CARTRIDGE 8 I: VRALL26.23.00 LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT ANDBULK)OP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW 9 I: CALLPRESSURE INDICATION CIRCUIT BY PTTDS 02 DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT 8 I: 15 MOPOST 40041ORPOST 51053ORPOST 51065FC 03 REMOVE BOTTLE FOR WEIGHT CHECK 8 I: 8000 FHALLOP 04 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 10000 FHALLFC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST 6,9 I: VRALLORNRNOTE 8FC 06 FUNCTIONAL CHECK OF PRESSURE REDUCER 8 I: 14000 FHPOST 40041NOTE 24ORPOST 51053ORPOST 51065* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.23.00 * * * * * C O N T I N U E * * * * *07 TASK DELETED08 TASK DELETEDFC 09 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND 8 I: 14000 FHALLOBSTRUCTION10 TASK DELETEDDS 11 DISCARD CARTRIDGE UNIT 8 I: VRALLDI 12 DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND 8 I: 14000 FHPOST 40041CHECK VALVE NOTE 24ORPOST 51053ORPOST 51065FC 13 FUNCTIONAL CHECK OF FLOW METERING COMPACT UNIT (FMCU) 8 I: 14000 FHPOST 47090ORPOST 47091DI 14 DETAILED INSPECTION OF FLOW METERING COMPACT UNIT 8 I: 14000 FHPOST 47090(RESTRICTOR, HALON FILTER AND CHECK VALVE).ORPOST 47091DS 15 DISCARD AND REPLACE WATER ADSORBING FILTER IN FLOW 8 I: 15 MOPOST 47090METERING COMPACT UNIT (FMCU).ORPOST 4709126.24.00 PORTABLE FIRE EXTINGUISHERFC 01 REMOVE BOTTLES FOR WEIGHT CHECK 9 I: VRALLNOTE 26* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.24.00 * * * * * C O N T I N U E * * * * *FC 02 REMOVE BOTTLES FOR HYDROSTATIC TEST 9 I: VRALLORNRNOTE 803 TASK DELETEDGVI 04 GENERAL VISUAL INSPECTION OF PORTABLE FIRE 9 I: 1000 FHALLEXTINGUISHER ATTACHMENT26.25.00 LAVATORY FIRE EXTINGUISHINGOP 01 CHECK PRESSURE OF EXTINGUISHING AGENT 9 I: CALLFC 02 REMOVE BOTTLE FOR WEIGHT CHECK 9 I: 4 CALL26.28.00 AUXILIARY AREAS FIRE EXTINGUISHING (CREW REST ROOM-UNDERFLOOR)01 TASK DELETEDOP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 8 I: 12000 CRRPOST 43380CIRCUIT IN THE LDMCR FHPRE 47549ORPOST 51736PRE 47549ORPOST 53319PRE 47549ORPOST 53688PRE 47549* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *DS 03 DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE 8 I: VRPOST 43380IN THE LDMCRORPOST 51736ORPOST 53319ORPOST 53688FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,8 I: VRPOST 43380PRESSURE SWITCH SETTING IN THE LDMCR ORORNRPOST 51736NOTE 8ORPOST 53319ORPOST 53688OP 05 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES FOR 8 I: 72 CRR MOPOST 43380OBSTRUCTION IN THE LDMCR.ORPOST 51736ORPOST 53319ORPOST 53688OP 06 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY 8 I: 800 CRRPOST 43380IN THE LDMCR FHORPOST 51736ORPOST 53319ORPOST 53688OP 07 OPERATIONAL CHECK OF THE MANUAL FIRE EXTINGUISHING 9 I: 36 CRR MOPOST 43380CIRCUIT IN THE LDMCRORPOST 51736ORPOST 53319ORPOST 53688* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *OP 08 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MOPOST 43380IN THE LDMCRORPOST 51736ORPOST 53319ORPOST 53688OP 09 OPERATIONAL CHECK OF FIRE EXTINGUISHING CIRCUIT IN 8 I: 36 MOPOST 47197THE BCRCORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220FC 10 FUNCTIONAL CHECK OF PRESSURE REDUCER IN THE BCRC 8 I: 36 MOPOST 47197ORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220DI 11 DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND 8 I: 36 MOPOST 47197CHECK VALVE IN THE BCRC.ORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 11APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *12 TASK DELETEDDS 13 DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT 8 I: 15 MOPOST 47197IN THE BCRCORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220OP 14 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES FOR 8 I: 36 MOPOST 47197OBSTRUCTION IN THE BCRC.ORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 5322015 TASK DELETEDOP 16 OPERATIONAL CHECK OF THE PRESSURE 9 I: 2 CPOST 47197INDICATING CIRCUIT IN THE BCRCORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 12APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *OP 17 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY IN THE BCRC. 8 I: 700 FHPOST 47197ORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220FC 18 REMOVE BOTTLE FOR HYDROSTATIC TEST IN THE LDF AFT DCR 8 I: VR OR NRPOST 49657AND CHECK OF PRESSURE SWITCH SETTING. NOTE 8OP 19 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MOPOST 49657IN THE LDF AFT DCR.OP 20 OPERATIONAL CHECK OF LDF AFT DCR 8 I: 36 CRR MOPOST 49657FIRING CIRCUIT CONTINUITY.DS 21 DISCARD CARTRIDGE UNIT LDF AFT DCR 8 I: VRPOST 49657OP 22 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES 8 I: 72 CRR MOPOST 49657FOR OBSTRUCTION IN LDF AFT DCR.OP 23 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY IN THE 8 I: 700 CRRPOST 49657LDF AFT DCR. FHDS 24 DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE IN THE 8 I: VRPOST 47197BCRCORPOST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 13APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *FC 25 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF THE 6,9 I: VRPOST 47197PRESSURE SWITCH SETTING IN THE BCRC. OR NRORNOTE 8POST 47883ORPOST 50108ORPOST 51992ORPOST 52634ORPOST 53220* * * * * E N D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 14APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.00.00 FLIGHT CONTROLS27.14.00 AILERON AND HYDRAULIC ACTUATIONOP 01 OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY 8 I: 10000 FHALLBITE NOTE 24(THIS TASK COVERS TASK 29.10.00/12)VC 02 CHECK AILERON SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FHALLPOSITIONFC 03 CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FHALLEXCESSIVE PLAY AND GENERAL CONDITIONLU 04 LUBRICATION OF AILERON HINGE BEARINGS 9 I: 7500 FHALLOR18 MOLU 05 LUBRICATION OF AILERON SERVO CONTROL ROLLER BEARINGS 8 I: 7500 FHA340-500OROR18 MOA340-600ORA340-200POST 45512ORA340-200POST 47433ORA340-200POST 48221ORA340-300POST 45512ORA340-300POST 47433ORA340-300POST 48221OP 06 OPERATIONAL CHECK OF FCPC AND FCSC AILERON SERVO 9 I: CALLLOOPS. (COVERED BY MSI 27-90-00 TASK 6)ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.21.00 RUDDER MECHANICAL CONTROL01 TASK DELETED02 TASK DELETEDOP 03 OPERATIONAL CHECK OF YAW DAMPER SERVO ACTUATOR 9 I: CA340-200STANDBY SERVO LOOPORA340-300PRE 49144VC 04 CHECK POINTER OF CABLE TENSION REGULATOR WITHIN 9 I: 2 CA340-200LIMITSORA340-300PRE 49144OP 05 OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL 9 I: 2 CA340-200ORA340-300PRE 49144OP 06 OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL 9 I: 2 CA340-200LIMITATION UNITS STANDBY CHANNELORA340-300PRE 49144VC 07 VISUAL CHECK OF RUDDER MECHANICAL CONTROL IN THE FIN 8 I: 20000 FHA340-200ORA340-300PRE 49144DI 08 DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL 6,9 I: 4 CA340-200(EXCLUDING FIN)ORA340-300PRE 49144OP 09 OPERATIONAL CHECK OF AP ARTIFICIAL FEEL SPRING ROD 9 I: 4 CA340-200ORA340-300PRE 49144* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.21.00 * * * * * C O N T I N U E * * * * *10 TASK DELETEDFC 11 FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS 8 I: 42 MOA340-200SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR ORORWORKSHOP CHECK 20000 FHA340-300PRE 49144OP 12 OPERATIONAL CHECK OF CENTERING MECHANISM 8 I: 34000 FHA340-200ORA340-300PRE 49144OP 13 OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE 8 I: 3200 FHA340-200NOTE 24AORA340-300PRE 4914414 TASK DELETEDVC 15 VISUAL CHECK TO CONFIRM INTEGRITY OF CONTROL ROD 8 I: 20000 FHA340-200(ITEM 220 IN IPC 272147-1A) IN PTLU LINKAGE NOTE 24APOST 44442ORA340-300POST 44442PRE 49144LU 16 LUBRICATION OF RUDDER PEDALS ADJUSTMENT MECHANISM 6 I: CALL17 TASK DELETEDDI 18 DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT 6 I: 4 CA340-500ORA340-600ORA340-300POST 49144* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.21.00 * * * * * C O N T I N U E * * * * *OP 19 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY 9 I: 2 CA340-500CHANNELOR(THIS TASK COVERS TASK 27.90.00/18)A340-600ORA340-300POST 49144OP 20 OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL 9 I: 4 CA340-500ORA340-600ORA340-300POST 4914427.24.00 RUDDER HYDRAULIC ACTUATIONLU 01 LUBRICATION OF RUDDER HINGE BEARING NO4 9 I: 7500 FHA340-200OROR18 MOA340-300R OP 02 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH 8 I: 800 FHA340-200INDIVIDUAL HYDRAULIC SYSTEMS (THIS TASK COVERS TASKOR29.10.00/08)A340-300PRE 49144OP 03 OPERATIONAL CHECK OF RUDDER SERVO CONTROL JAMMING 9 I: 2 CA340-200DEVICEORA340-300PRE 49144FC 04 CHECK RUDDER SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 34000 FHALLEXCESSIVE PLAY AND GENERAL CONDITION05 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.24.00 * * * * * C O N T I N U E * * * * *LU 06 LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER 8 I: 7500 FHA340-500BEARING (RUDDER SIDE) OROR18 MOA340-600ORA340-300POST 49144LU 07 LUBRICATION OF RUDDER HINGE BEARING NO 6 9 I: 7500 FHA340-500OROR18 MOA340-600OP 08 OPERATIONAL CHECK OF RUDDER DAMPING MEASUREMENT BY 9 I: 1 CA340-500BITE NOTE 24ORA340-600ORA340-300POST 4914409 TASK DELETEDFC 10 FUNCTIONAL CHECK OF THE INDIVIDUAL RUDDER 9 I: 10000 FHA340-200SERVOCONTROLS NOTE 24AORA340-300PRE 4914427.34.00 ELEVATOR AND HYDRAULIC ACTUATIONOP 01 OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY 8 I: 10000 FHALLBITE OR18 MONOTE 24FC 02 CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FHALLEXCESSIVE PLAY AND GENERAL CONDITIONVC 03 CHECK ELEVATOR SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FHALLPOSITION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.34.00 * * * * * C O N T I N U E * * * * *LU 04 LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING 8 I: 7500 FHA340-200ORPOST 4767418 MOORA340-200POST 49586ORA340-300POST 47674ORA340-300POST 49586ORA340-500ORA340-600OP 05 OPERATIONAL CHECK OF FCPC AND FCSC STANDBY SERVO 9 I: CALLLOOPS ON PITCH CONTROL(COVERED BY MSI 27-90-00 TASK 9 OR 12 ACCORDING TOA/C TYPE)LU 06 LUBRICATION OF THE DIAGONAL BAR BEARING 9 I: 7500 FHA340-500(ELEVATOR SUPPORT STRUT) OROR18 MOA340-60027.40.00 TRIMMABLE HORIZONTAL STABILIZER (THS)OP 01 OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL 8 I: 800 FHALLHYDRAULIC SYSTEMS NOTE 24LU 02 LUBRICATION OF THS ACTUATOR BALL SCREW NUT 8 I: 700 FHALLNOTE 24BSV 03 CHECK OIL LEVEL OF THS ACTUATOR GEARBOX 6,9 I: 8 AALLOP 04 OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION 8 I: 5600 FHALLDEVICE. NOTE 24DI 05 CHECK MAGNETIC CHIP DETECTOR OF THS ACTUATOR GEARBOX 9 I: CALLDI 06 DETAILED INSPECTION OF THS ACTUATOR FAIL SAFE NUT 8 I: 12000 FHALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.40.00 * * * * * C O N T I N U E * * * * *DI 07 DETAILED INSPECTION OF UPPER THS ACTUATOR ATTACHMENT 8 I: 12000 FHALL(PRIMARY AND SECONDARY) AND NO-BACK HOUSINGDI 08 DETAILED INSPECTION OF LOWER THS ACTUATOR ATTACHMENT 8 I: 12000 FHALL(PRIMARY AND SECONDARY).LU 09 LUBRICATION OF THS MECHANICAL CONTROL CHAINS 6 I: 2 CALLFC 10 CHECK MOVABLE INDEX ON THS CABLE TENSION COMPENSATOR 6 I: CALLSCALE IS WITHIN LIMITS.VC 11 CHECK WEAR INDICATOR OF THS ACTUATOR NO-BACK SYSTEM 8 I: 15000 FHALLFC 12 CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT 8 I: 16000 FHALL(PRIMARY AND SECONDARY LOAD PATH).OP 13 OPERATIONAL CHECK OF THS ACTUATOR NO-BACK SYSTEM 8 I: 34000 FHALLDI 14 DETAILED INSPECTION OF THS MECHANICAL CONTROL LOOP 6 I: 4 CALLFC 15 FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE-OFF BRAKE 9 I: 4 CALL(CHECK OF STATIC TORQUE)VC 16 VISUAL CHECK OF THS ACTUATOR DRAIN COLLECTING 9 I: 2 AA340-200CONTAINER ASSEMBLY INCLUDING HOSESPOST 43683ORA340-200POST 45578ORA340-300POST 43683ORA340-300POST 45578ORA340-500POST 52590ORA340-600POST 52590* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.40.00 * * * * * C O N T I N U E * * * * *OP 17 OPERATIONAL CHECK OF THSA ENHANCED RUNAWAY PROTECTION 9 I: CA340-500(ERP).POST 47041(COVERED BY MSI 27.90.00, TASK NO 17)ORA340-600POST 47041OP 18 OPERATIONAL CHECK OF THSA CHECKABLE SHEAR PIN. 9 I: 10000 FHA340-300POST 54880ORA340-200POST 54881ORA340-300POST 54881ORA340-500POST 54882ORA340-600POST 54882ORA340-300POST 5578027.50.00 FLAPSLU 01 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 4 APRE 40701BEARINGS.PRE 47372PRE 49444PRE 50436SV 02 TOP UP PCU TO CONFIRM FLUID LEVEL 6 I: CALLDI 03 DETAILED INSPECTION OF TRANSMISSION ASSY 6 I: 60 MOALLDI 04 DETAILED INSPECTION OF CRUISE ROLLERS, FLAP TRACKS 9 I: 60 MOALLAND CARRIAGES, ROTARY ACTUATORS AND ATTACHMENTSSV 05 DRAIN AND REFILL ROTARY ACTUATOR WITH SEMI-FLUID 6 I: 60 MOALLDI 06 DETAILED INSPECTION OF TRACK 4 SENSORS 9 I: 60 MOALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.50.00 * * * * * C O N T I N U E * * * * *DI 07 DETAILED INSPECTION OF INTERCONNECTION STRUT AND 8 I: 60 MOALLATTACHMENTSFC 08 REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YEALL(THIS TASK COVERS TASK 27.80.00/05)SV 09 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 CALLGVI 10 GENERAL VISUAL INSPECTION OF FLAP TRACK FAIRING 9 I: 4 C ZL-531-02-1 ALLSUPPORT STRUTS AND LINKAGE ZL-531-02-2LU 11 LUBRICATION OF FLAP CARRIAGE (2 TO 5) LEVER BEARINGS 9 I: 4 APRE 43303LU 12 LUBRICATION OF STEADY BEARINGS 6 I: CALLLU 13 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 2 CPOST 50436BEARINGS.OP 14 OPERATIONAL CHECK OF FLAP WTB/POB PERFOMANCE TEST. 8 I: 6400 FHALL27.64.00 SPOILER HYDRAULIC ACTUATIONLU 01 LUBRICATION OF ALL SPOILER LINKAGE BEARINGS PROVIDED 9 I: CALLWITH GREASE NIPPLESDI 02 DETAILED INSPECTION OF LINKAGE AND ATTACHMENT OF 9 I: 4 CALLSPOILERS 1 TO 627.80.00 LIFT AUGMENTING (SLATS)LU 01 LUBRICATION OF ALL SLAT TRACK ROLLER BEARINGS, PINION 6,9 I: 2800 FHALLBEARINGS, RACK AND PINION TEETH AND SLATTRACK 2 AND 3 LEVER BEARINGSSV 02 TOP UP PCU GEARBOX TO CONFIRM FLUID LEVEL 6 I: CALLDI 03 DETAILED INSPECTION OF SLAT TRANSMISSION ASSY 6 I: 4 CALLDI 04 DETAILED INSPECTION OF SLAT TRACKS AND ROLLERS, 9 I: 4 CALLPINIONS AND CURVED RACK GEARS* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.80.00 * * * * * C O N T I N U E * * * * *FC 05 REMOVAL OF CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YEALL(COVERED BY MSI 27-50-00, TASK 08)SV 06 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 CALLLU 07 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE A 6 I: 4 CPOST 50471(TRACK 2-3).ORPOST 50138ORA340-500ORA340-600LU 08 LUBRICATION OF STEADY BEARINGS 6 I: CALLLU 09 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE B 6 I: 4 CALL(TRACK 5-16)OP 10 OPERATIONAL CHECK OF SLAT WTB/POB PERFOMANCE TEST. 8 I: 6400 FHALL27.90.00 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)OP 01 OPERATIONAL CHECK OF TAKEOVER AND PRIORITY FUNCTION 8 I: 18 MOALLOP 02 OPERATIONAL CHECK OF FCPCS AND FCSCS YAW DAMPER SERVO 9 I: CA340-200LOOPS.ORA340-300PRE 4914403 TASK DELETEDOP 04 OPERATIONAL CHECK OF FCPC1 AND FCSC1 POWER SUPPLY 9 I: CALLOP 05 OPERATIONAL CHECK OF FCPC2 AND THS ACTUATOR 9 I: 1 CALLELECTRICAL MOTOR 2 POWER SUPPLY NOTE 24AOP 06 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S AILERON SERVO 9 I: CALLLOOPS(THIS TASK COVERS TASK 27.14.00/06)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.90.00 * * * * * C O N T I N U E * * * * *OP 07 OPERATIONAL CHECK OF GREEN SERVOCONTROLS TRAVEL SPEED 8 I: 18 MOALLLIMITATION WHEN RAT IS EXTENDED NOTE 24OP 08 OPERATIONAL CHECK OF RETURN TO LOW SPEED 9 I: 4 CA340-200CONFIGURATION OF RUDDER AND PEDAL TRAVEL LIMITATIONORUNITSA340-300PRE 49144OP 09 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S STANDBY SERVO 9 I: 15 MOA340-200LOOPS ON PITCH CONTROL NOTE 24AOR(THIS TASK COVERS TASK 27.34.00/05 FOR A340-200 ORA340-300A340-300)OP 10 OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY 9 I: CA340-200POST 44385ORA340-300POST 44385ORA340-500ORA340-60011 TASK RESERVEDOP 12 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S STANDBY SERVO 9 I: 1 CA340-500LOOPS ON PITCH CONTROL NOTE 24BOR(THIS TASK COVERS TASK 27.34.00/05 FOR A340-500 ORA340-600A340-600)OP 13 OPERATIONAL CHECK OF LIGHTS 9 I: 2 AALL(COVERED BY MSI 33-14-00)OP 14 OPERATIONAL CHECK OF THE BACK UP CONTROL MODULE AND 8 I: 5000 FHA340-500BACK UP POWER SUPPLY (BCM/BPS)ORA340-600ORA340-300POST 49144* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 11APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section27.90.00 * * * * * C O N T I N U E * * * * *OP 15 OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP 9 I: CA340-500ORA340-600ORA340-300POST 49144OP 16 OPERATIONAL CHECK OF RUDDER ELECTRICAL BACK UP 8 I: 5000 FHA340-500ORA340-600ORA340-300POST 49144OP 17 OPERATIONAL CHECK OF THSA ENHANCED RUNAWAY PROTECTION 9 I: CA340-500(ERP)OR(THIS TASK COVERS TASK 27.40.00/17)A340-600OP 18 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY 9 I: 2 CA340-500CHANNEL (COVERED BY MSI 27-21-00 TASK NO 19)ORA340-600ORA340-300POST 4914419 TASK RESERVED20 TASK RESERVED* * * * * E N D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 12APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.00.00 FUEL28.11.00 TANKSOP 01 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DYALLFROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS NOTE 1OP 02 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 2 MOALLFROM TRIM TANK AND TRIM VENT SURGE TANK NOTE 1OP 03 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, 9 I: CA340-200USING INDIVIDUAL MOTORS, TO PROVE CORRECT ACTUATORPRE 42855OPERATION AND COCKPIT INDICATIONORA340-300PRE 42855OP 04 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE 8 I: 6 YEA340-200TO PROVE THAT NEITHER VALVE HAS JAMMED IN THE OPENORPOSITION AND TO VERIFY CORRECT OPERATION OF THE P/BSWA340-300OP 05 OPERATIONAL CHECK OF ALL COLLECTOR CELL CLACK VALVES 9 I: 8 CALLTO ENSURE FULL AND FREE MOVEMENT06 TASK DELETED07 TASK DELETED08 TASK RESERVED09 TASK RESERVEDOP 10 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, 9 I: 4 CA340-200USING INDIVIDUAL MOTORS TO PROVE CORRECT ACTUATORPOST 42855OPERATION AND COCKPIT INDICATIONORA340-300POST 42855OP 11 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DYA340-500FROM THE REAR CENTER TANK NOTE 1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.11.00 * * * * * C O N T I N U E * * * * *OP 12 OPERATIONAL CHECK OF THE INNER TANK 2/3 CLACK VALVES 9 I: 8 CA340-500TO ENSURE FULL AND FREE MOVEMENTORA340-600OP 13 OPERATIONAL CHECK OF THE INNER TANK 2/3 CLACK VALVES 8 I: 6 YEA340-500TO ENSURE THAT THEY HAVE NOT FAILED OPENORA340-600GVI 14 GENERAL VISUAL INSPECTION OF WATER DRAIN VALVE PIPES 9 I: 8 C ZL-541-02-1 A340-200FOR SECURITY AND INTEGRITY ZL-542-01-1 ORA340-30028.12.00 TANK VENTING SYSTEMVC 01 VISUAL CHECK OF THE APERTURE LEADING TO WING AND TRIM 9 I: 2 CALLSURGE TANK FLAME ARRESTORS (INSIDE THE NACA INTAKES)FOR BLOCKAGEVC 02 VISUAL CHECK OF THE WING AND TRIM VENT SURGE TANK 9 I: 1 CALLOVERPRESSURE PROTECTORS (BURST DISCS) FOR INTEGRITY NOTE 528.14.00 TRIM PIPE SHROUD DRAINAGE01 TASK DELETED02 TASK DELETEDFC 03 FUNCTIONAL CHECK OF TRIM PIPE SHROUD DRAIN LINE AND C 8 I: 36 MOALLONNECTORS WITHIN PRESSURIZED FUSELAGE (COVERED BY MSI28.27.00 TASK NO 3)28.16.00 FUEL RECIRCULATION FOR COOLINGNO TASK SELECTEDISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.17.00 WATER SCAVANGE01 TASK DELETED28.18.00 IGNITION PREVENTIONDI 01 DETAILED INSPECTION OF THE WING AND TRIM TANK BONDING 9 I: 8 CALLLEADS (SFAR88)GVI 02 GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND 9 I: 8 CALLPROBE ATTACHMENTS (SFAR88)GVI 03 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS 9 I: 8 CALL(SFAR88)DI 04 DETAILED INSPECTION OF THE HEATSHIELDS BELOW THE 8 I: 6 YEA340-200CENTER TANK (SFAR88)POST 49520ORA340-300POST 49520ORA340-500ORA340-600VC 05 VISUAL CHECK OF CENTER TANK FOR LEAKS (SFAR88) 8 I: 700 FHA340-200PRE 49520ORA340-300PRE 49520GVI 06 GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD 9 I: 4 CALLCARGO BAY INSULATION MATS (SFAR88)GVI 07 GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE 9 I: 8 CALLCENTER TANK (SFAR88)GVI 08 GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND 9 I: 8 CALLTRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS(SFAR88)GVI 09 GENERAL VISUAL INSPECTION OF TRIM TANK EXTERNAL 9 I: 8 CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.18.00 * * * * * C O N T I N U E * * * * *ELECTRICAL WIRING AND CONNECTIONS (SFAR88)GVI 10 GENERAL VISUAL INSPECTION OF WING FUEL PUMP 9 I: 8 CALLELECTRICAL CONNECTIONS AND UNDERWING ELECTRICALSUPPLY CABLE (SFAR88)28.21.00 MAIN FUEL PUMP SYSTEMOP 01 OPERATIONAL CHECK TO VERIFY ISOLATION OF STANDBY PUMP 8 I: 10000 FHA340-2004 CONTROL WHEN MAIN PUMP1 IS RUNNING IN ELECTRICAL NOTE 24AOREMERGENCY CONFIGURATIONA340-300OP 02 OPERATIONAL CHECK TO VERIFY THAT RELAY 27QA HAS NOT 8 I: 15000 FHALLFAILED IN THE ENERGISED POSITIONOP 03 OPERATIONAL CHECK OF STANDBY PUMP AUTOMATIC CONTROL. 9 I: CALLOP 04 OPERATIONAL CHECK TO ENSURE THAT STANDBY PUMP 4 8 I: 18 MOA340-200OPERATES WHEN MAIN PUMP 1 IS SWITCHED OFF WITH THEORAIRCRAFT IN AN ELECTRICAL EMERGENCY CONFIGURATIONA340-30005 TASK RESERVEDOP 06 OPERATIONAL CHECK TO ENSURE THAT THE MAIN FUEL PUMP 8 I: 18 MOA340-500NO.3 OPERATES WHEN THE MAIN PUMP NO.2 IS SWITCHED OFFORWITH THE AIRCRAFT IN AN ELECTRICAL EMERGENCYA340-600CONFIGURATIONOP 07 OPERATIONAL CHECK TO VERIFY ISOLATION OF MAIN FUEL 8 I: 10000 FHA340-500PUMP 3 WHEN MAIN FUEL PUMP 2 IS RUNNING IN ELECTRICAL NOTE 24BOREMERGENCY CONFIGURATIONA340-60028.22.00 APU FUEL PUMP SYSTEM01 TASK DELETED02 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.22.00 * * * * * C O N T I N U E * * * * *OP 03 OPERATIONAL CHECK OF FWD APU FUEL FEED PUMP 9 I: CA340-200ACTIVATION CIRCUIT VIA LANDING GEAR LGCIU1 (5GA1)PRE 44604RELAY 12QC AND MAIN BOOSTER PUMP CONTACTORSOR(10QA1- 10QA4, 11QA4)A340-300PRE 44604OP 04 OPERATIONAL CHECK OF AFT APU FUEL PUMP FIRE STOP 9 I: CA340-200CIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS 5WF, 6WFORA340-300GVI 05 GENERAL VISUAL INSPECTION OF APU FUEL SHROUD LINE AND 9 I: 4 C ZL-311-01-1 A340-200FUEL/AIR SEPARATOR FOR INTEGRITY AND ABSENCE OF ZL-313-01-1 ORLEAK PATHS.A340-30006 TASK RESERVEDOP 07 OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO 9 I: 2800 FHA340-200DRAIN ANY ACCUMULATED WATERPOST 42890ORA340-200POST 42921ORA340-300POST 42890ORA340-300POST 42921GVI 08 GENERAL VISUAL INSPECTION OF APU FUEL LINE SHROUD AND 8 I: 6 YEA340-500CONNECTORSORA340-600GVI 09 GENERAL VISUAL INSPECTION OF APU FUEL LINE SHROUD 8 I: 36 MOA340-500DRAIN LINE AND CONNECTORSORA340-600OP 10 OPERATIONAL CHECK TO VERIFY THAT RELAY 15QC HAS NOT 8 I: 36 MOA340-200FAILED IN ENERGIZED POSITION.POST 44604ORA340-300POST 44604ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.23.00 CROSSFEED SYSTEMOP 01 OPERATIONAL CHECK OF CROSSFEED VALVES 1 AND 4 TO 9 I: 2 CA340-200PROVE THAT NEITHER VALVE HAS JAMMED IN CLOSEDORPOSITIONA340-30002 TASK RESERVED03 TASK RESERVEDOP 04 OPERATIONAL CHECK OF THE CROSSFEED VALVES INDICATION 9 I: 1 CALLNOTE 24BOP 05 OPERATIONAL CHECK OF THE CROSSFEED VALVES USING THE 9 I: 2 CALLINDIVIDUAL MOTORS NOTE 24BOP 06 OPERATIONAL CHECK OF THE EMERGENCY ELECTRICAL CONTROL 8 I: 800 FHA340-500CROSSFEED VALVES FUNCTIONORA340-60028.24.00 ENGINE LP FUEL SHUT-OFFOP 01 OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL 9 I: 2 CALLMOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT AND ORCORRECT COCKPIT INDICATION 5000 FCNOTE 24BOP 02 OPERATIONAL CHECK OF THE FIRE CONTROL P/B SW 8 I: 18 MOALLSUB-FUNCTIONS(COVERED BY MSI 26.21.00, TASK NO3)N OP 03 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL 8 I: 6500 FCALLSUPPLY TO ASSOCIATED ENGINE OR12 YE28.25.00 REFUEL/DEFUEL SYSTEMDI 01 DETAILED INSPECTION OF REFUEL COUPLING FOR DAMAGE OR 9 I: 3500 FCALLEVIDENCE OF WEAR02 TASK RESERVED03 TASK RESERVEDISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.26.00 MAIN TRANSFER SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF RCT TRANSFER LINE SHROUD 8 I: 36 MOA340-500AND DRAIN LINE CONNECTORS28.27.00 TRIM TANK TRANSFER SYSTEMR OP 01 OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES 9 I: 2 CALLFOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH NOTE 24R 02 TASK DELETEDR FC 03 FUNCTIONAL CHECK OF TRIM TANK TRANSFER LINE SHROUD 8 I: 36 MOALLCONNECTORS (THIS TASK COVERS TASK 28.14.00/03)28.28.00 ADDITIONAL CENTER TANK TRANSFER SYSTEMOP 01 OPERATIONAL CHECK OF THE LEAK MONITOR FOR EVIDENCE OF 9 I: 500 FHA340-200FUEL LEAKAGE NOTE 21POST 44002ORA340-300POST 42612OP 02 OPERATIONAL CHECK OF THE INTERSPACE OVERBOARD DRAIN 9 I: 60 MOA340-200SYSTEM NOTE 21POST 44002ORA340-300POST 42612OP 03 OPERATE WATER DRAIN VALVES IN THE ACT(S) TO DRAIN 9 I: 42 DYA340-200ACCUMULATED WATER (IF ACT(S) INSTALLED) OR NRPOST 44002NOTE 1ORNOTE 8A340-300POST 42612FC 04 FUNCTIONAL CHECK OF THE ACT INWARD RELIEF VALVE 9 I: 60 ACT MOA340-200NOTE 21POST 44002NOTE 23ORA340-300POST 42612* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.28.00 * * * * * C O N T I N U E * * * * *OP 05 OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM 9 I: 60 MOA340-200NOTE 18POST 44002NOTE 21ORNOTE 24AA340-300POST 42612FC 06 FUNCTIONAL CHECK OF ACT PRESSURE REDUCING VALVE 9 I: 60 MOA340-200NOTE 21POST 44002ORA340-300POST 42612OP 07 OPERATIONAL CHECK OF INDIVIDUAL MOTORS OF THE 9 I: 60 MOA340-200TRANSFER VALVE NOTE 21POST 44002ORA340-300POST 42612DS 08 DISCARD ACT AIR INLET FILTER 6 I: 30 MOA340-200NOTE 21POST 44002ORA340-300POST 42612GVI 09 GENERAL VISUAL INSPECTION OF THE ACT HEAT SHIELD 8 I: 500 FCA340-200NOTE 21POST 44002ORA340-300POST 4261228.29.00 APU LP FUEL SHUT-OFFOP 01 OPERATIONAL CHECK OF APU LP FUEL SHUT OFF VALVE USING 9 I: 2 CALLEACH INDIVIDUAL MOTORS VIA APU FIRE EMERGENCY STOPRELAYS 5WF, 6WF(COVERED BY MSI 26-22-00, TASK NO10)28.31.00 JETTISON SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF JETTISON PIPE FLEXIBLE 9 I: 2 CALLHOSE FOR SECURITY AND CONDITION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section28.31.00 * * * * * C O N T I N U E * * * * *GVI 02 GENERAL VISUAL INSPECTION OF ANTI-CORONA DEVICE FOR 9 I: 2 CALLSECURITY OF ATTACHMENT AND FOR SATISFACTORY CONDITIONOP 03 OPERATIONAL CHECK TO VERIFY CORRECT RESPONSE OF 9 I: 4 CALLJETTISON SYSTEM TO SELECTION OF JETTISON "ON"28.42.00 QUANTITY INDICATINGNO TASK SELECTED28.46.00 TANK LEVEL SENSING01 TASK DELETEDOP 02 OPERATIONAL CHECK OF INNER TANK LOW LEVEL SENSORS AND 8 I: 10000 FHA340-200ASSOCIATED WARNINGSORA340-30028.49.00 FUEL TEMPERATURE MEASUREMENTOP 01 INTERROGATION OF FCMS GROUND REPORT PAGE FOR FAILURE 8 I: 10000 FHA340-200OF OUTER TANK AND TRIM TANK TEMPERATURE SENSORPRE 42191ORA340-300PRE 4219128.51.00 FUEL CONTROL AND MONITORINGOP 01 INTERROGATION OF FCMS GROUND REPORT PAGE FOR FCMC 1 8 I: 10000 FHA340-200(2) FAULTPRE 42191ORA340-300PRE 42191* * * * * E N D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section29.00.00 HYDRAULIC POWER29.10.00 MAIN HYDRAULIC POWERFC 01 CHECK NITROGEN CHARGING PRESSURE ON HYDRAULIC POWER 9 I: 400 FHALLACCUMULATORSVC 02 CHECK CLOGGING INDICATORS OF HIGH PRESSURE (HP), 9 I: AALLRETURN, ENGINE DRIVEN PUMPS (EDP) CASE DRAIN,RESERVOIR FILL AND AIR PRESSURIZATION UNIT (PUA)FILTERSSV 03 DRAINING OF WATER SEPARATORS 9 I: AA340-200PRE 47625ORA340-300PRE 47625SV 04 SERVICING OF LEAKAGE RECOVERY TANKS 9 I: 2 AALLOP 05 OPERATIONAL CHECK OF EDP DEPRESSURIZATION 9 I: CALLDI 06 CHECK FOR CORRECT AIR PRESSURE BY READING GAUGES ON 6 I: CALLEACH RESERVOIRFC 07 FUNCTIONAL CHECK OF PRIORITY VALVE 6,9 I: 4 CALLR OP 08 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH GREEN 8 I: 18 MOALLHYDRAULIC SYSTEM PRESSURIZED(COVERED BY MSI 27-24-00 TASK NO 2)OP 09 OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT-OFF VALVES 8 I: 18 MOALLOP 10 OPERATIONAL CHECK OF AUTOMATIC CONTROL OF FIRE 8 I: 18 MOA340-200SHUT-OFF VALVE IN CASE OF LOW LEVEL ON GREENORHYDRAULIC SYSTEMA340-300FC 11 HYDRAULIC FLUID ANALYSIS 9 I: 2 CALLOP 12 OPERATIONAL CHECK OF AILERON SERVOCONTROL WITH GREEN 9 I: 12500 FHALLHYDRAULIC SYSTEM(COVERED BY MSI 27-14-00 TASK NO 01)FC 13 FUNCTIONAL CHECK OF GREEN LOW LEVEL WARNING SYSTEM 8 I: 12000 FHALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section29.10.00 * * * * * C O N T I N U E * * * * *(COVERED BY MSI 29-20-00 TASK NO 07)OP 14 OPERATIONAL CHECK OF INHIBITION OF MANUAL CONTROL OF 9 I: 4 CALLLEAK MEASUREMENT SOLENOID VALVEFC 15 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 6 I: 4 CALLYELLOW AND BLUE HYDRAULIC SYSTEMSFC 16 REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK 8 I: 6 YEALLGVI 17 GENERAL VISUAL INSPECTION OF SEAL DRAIN SYSTEM 9 I: 4 C ZL-147-01-1 ALLZL-147-01-2ZL-195-01-1ZL-195-02-1ZL-195-02-2FC 18 REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YEA340-200POST 40838ORA340-300POST 40838ORA340-500ORA340-600FC 19 REMOVE SLAT PCU HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YEA340-500ORA340-600OP 20 OPERATIONAL CHECK OF AUTOMATIC EDP DEPRESSURIZATION 9 I: CA340-500THROUGHT FADEC (ECC) CONTROLORA340-600VC 21 VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN 9 I: AA340-200VALVE POSITIONPOST 47625ORA340-300POST 47625ORA340-500ORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section29.10.00 * * * * * C O N T I N U E * * * * *OP 22 OPERATIONAL CHECK OF AUTO CLOSURE OF FIRE SHUT OFF 8 I: 18 MOA340-500VALVES IN CASE OF LOW LEVEL ON GREEN HYDRAULIC SYSTEMORAND ENGINE BURST SIGNALA340-600FC 23 FUNCTIONAL CHECK OF ENGINE BURST DETECTION 8 I: 18 MOA340-500(THIS TASK COVERS TASK 29.20.00/09)ORA340-600FC 24 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE IN 6 I: 10000 FHALLGREEN SYSTEM(COVERED BY MSI 29-20-00 TASK NO 08)29.20.00 AUXILIARY HYDRAULIC POWEROP 01 OPERATIONAL CHECK OF GREEN, YELLOW AND BLUE ELECTRIC 9 I: 4 AALLPUMPSOP 02 OPERATIONAL CHECK OF AUTOMATIC START OF GREEN AND 9 I: 4 AA340-200YELLOW ELECTRIC PUMPSORA340-300OP 03 OPERATIONAL CHECK OF AUTOMATIC RAT DEPLOYMENT 8 I: 18 MOALL04 TASK DELETEDDI 05 DETAILED INSPECTION OF RAT IN DEPLOYED POSITION 8 I: 18 MOALLFC 06 OPERATIONAL CHECK OF MANUAL RAT DEPLOYMENT FOLLOWED 8 I: 18 MOALLBY FUNCTIONAL CHECK OF RAT OPERATION AND INSPECTION NOTE 24OF FILTER ELEMENT BY REFERENCE TO DIFFERENTIALPRESSURE INDICATOR.FC 07 FUNCTIONAL CHECK OF GREEN AND BLUE LOW LEVEL WARNING 8 I: 12000 FHALLSYSTEM (THIS TASK COVERS TASK 29.10.00/13)FC 08 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 8 I: 10000 FHALLGREEN HYDRAULIC SYSTEM(THIS TASK COVERS TASK 29.10.00/24)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section29.20.00 * * * * * C O N T I N U E * * * * *FC 09 FUNCTIONAL CHECK OF ENGINE BURST DETECTION 8 I: 18 MOA340-500(COVERED BY MSI 29-10-00 TASK NO 23)ORA340-60010 TASK RESERVEDN DI 11 DETAILED INSPECTION RAT CASE DRAIN BOTTLE 9 I: 72 MOA340-500ORA340-600N SV 12 SERVICING OF RAT CASE DRAIN BOTTLE 9 I: 10000 FHA340-500OROR18 MOA340-60029.30.00 INDICATINGOP 01 CROSS CHECK FLUID LEVEL ON EACH RESERVOIR, ON ECAM 9 I: 2 AALLHYDRAULIC PAGE AND GROUND SERVICE PANEL INDICATOROP 02 OPERATIONAL CHECK OF OVERHEAT DETECTION SYSTEM 9 I: CALLOP 03 OPERATIONAL CHECK OF RESERVOIRS LOW AIR PRESSURE 9 I: CALLWARNING* * * * * E N D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section30.00.00 ICE AND RAIN PROTECTION30.11.00 WING ICE PROTECTIONDI 01 DETAILED INSPECTION OF TELESCOPIC DUCTS, FLEXIBLE 9 I: 2 CALLSLAT INTERCONNECTION SLEEVES AND, IN WING LEADINGEDGE, ANTI-ICING DUCT COUPLINGS, CLAMPS ANDATTACHMENT POINTS30.21.04 ENGINE AIR INTAKE ICE PROTECTIONDI 01 DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY 6 I: CA340-200DUCTS AND ASSOCIATED HARDWARE IN CORE AND FANORCOMPARTMENTSA340-300OP 02 OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE PROTECTION 9 I: 2 CA340-200FAULT WARNINGORA340-300GVI 03 GENERAL VISUAL INSPECTION OF INLET COWL ANTI-ICE 9 I: 4 C ZL-411-01-1 A340-200SUPPLY DUCT (BETWEEN SWIRL NOZZLE AND AFT BULKHEAD)ORA340-30030.21.05 ENGINE AIR INTAKE ICE PROTECTIONGVI 01 GENERAL VISUAL INSPECTION OF THE NOSE COWL ANTI ICE 9 I: CA340-500DUCTORA340-60030.31.00 PROBE ICE PROTECTIONNO TASK SELECTED30.42.00 WINDSHIELD ANTI-ICING AND DEFOGGINGNO TASK SELECTED30.45.00 WINDSHIELD RAIN PROTECTION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section30.45.00 * * * * * C O N T I N U E * * * * *01 TASK DELETED02 TASK DELETED30.46.00 ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTIONOP 01 OPERATIONAL CHECK OF ESCAPE SLIDE LOCKING MECHANISM 9 I: CA340-200ICE PROTECTIONPOST 40335PRE 51642PRE 51617ORA340-300POST 40335PRE 51642PRE 5161730.70.00 WATER LINESNO TASK SELECTED30.81.00 ICE DETECTIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section31.00.00 INDICATING/RECORDING SYSTEMS31.21.00 ELECTRICAL CLOCKDS 01 DISCARD CLOCK BATTERY 9 I: VRIF CLOCK FITTEDWITH BATTERY31.33.00 DIGITAL FLIGHT DATA RECORDING SYSTEM (DFDRS)R DS 01 DISCARD ULB BATTERY. 9 I: VRA340PRE 47606PRE 48904R OP 02 OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU. 9 I: 1 CA340NOTE 8PRE 47606PRE 48904R OP 03 OPERATIONAL CHECK OF THE ULB. 9 I: VRA340PRE 47606PRE 4890431.36.00 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)NO TASK SELECTED31.36.01 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)R DS 01 DISCARD ULB BATTERY 9 I: VRPOST 47606ORPOST 48904R OP 02 OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU 9 I: 1 CPOST 47606NOTE 8ORPOST 48904R OP 03 OPERATIONAL CHECK OF ULB. 9 I: VRPOST 47606ORPOST 48904* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section31.36.01 * * * * * C O N T I N U E * * * * *N OP 04 OPERATIONAL CHECK OF WGL-QAR/DAR INTERLOCK AND 8 I: 24000 FHPOST 55048TRANSMISSION LOGIC.ORPOST 5629331.44.00 WEIGHT AND BALANCE SYSTEM (IF INSTALLED)NO TASK SELECTED31.50.00 CENTRAL WARNING SYSTEMOP 01 OPERATIONAL CHECK OF ATTENTION GETTER LIGHTS 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1).OP 02 OPERATIONAL CHECK OF AUTOLAND LIGHTS 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 03 OPERATIONAL CHECK OF SLAT AND FLAP SENSOR CIRCUIT VIA 8 I: 34000 FHALLMCDUOP 04 OPERATIONAL CHECK OF DMC OUTPUT CIRCUITS TO FWC ́S 8 I: 34000 FHALL31.60.00 ELECTRONIC INSTRUMENT SYSTEMOP 01 OPERATIONAL CHECK OF PFD/ND AND ECAM/ND MANUAL 9 I: CPRE 50161TRANSFEROP 02 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 9 I: CPRE 50161OP 03 OPERATIONAL CHECK OF CORRECT EFIS AND ECAM TRANSFER 9 I: 2 CPRE 50161WHEN BUSBAR 105XP IS LOST04 TASK DELETEDOP 05 OPERATIONAL CHECK OF EFIS OFFSIDE AND ECAM NON ACTIVE 8 I: 34000 FHPRE 50161MONITORING CIRCUITS31.60.01 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD TECHNOLOGY)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section31.60.01 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL 9 I: CPOST 50161TRANSFEROP 02 OPERATIONAL CHECK OF BRIGHTNESS CONTROL THROUGH MCDU 9 I: CPOST 50161OP 03 OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN 9 I: 2 CPOST 50161BUSBAR 105XP IS LOSTOP 04 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 8 I: 18 MOPOST 50161* * * * * E N D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.00.00 LANDING GEAR32.11.00 MAIN GEARLU 01 LUBRICATION OF MAIN GEAR 6,9 I: 500 FCA340-200OROR4 MOA340-300LU 02 LUBRICATION OF SHORTENING MECHANISM HINGE JOINTS 5 I: 500 FCA340-200OROR4 MOA340-300FC 03 CHECK OF SHOCK ABSORBER NITROGEN CHARGE PRESSURE 6 I: CA340-200ORA340-300SV 04 SERVICE MLG SHOCK ABSORBER 6 I: 2 CA340-200ORA340-300FC 05 CHECK MAIN GEAR TORQUE LINKS FOR EXCESSIVE PLAY 6 I: 2 CA340-200ORA340-300RS 06 RESTORATION OF MAIN GEAR 5 I: NOTE 7A340-200ORA340-300OP 07 REMOVE HYDRAULIC FUSE IN MLG BOGIE PITCH TRIMMER 9 I: 10 YEA340-200SUPPLY LINE FOR OPERATIONAL CHECK IN WORKSHOP.ORA340-300GVI 08 GENERAL VISUAL INSPECTION OF PITCH TRIMMER AND 6 I: A ZL-731-01-1 A340-200ASSOCIATED PIPING AND COMPONENTSORA340-300GVI 09 GENERAL VISUAL INSPECTION OF SHOCK ABSORBER SLIDING 6 I: AA340-200MEMBER FOR SIGNS OF LEAKAGE AND NORMAL EXTENSIONORA340-30010 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.11.00 * * * * * C O N T I N U E * * * * *LU 11 LUBRICATION OF MLG 6,9 I: 500 FCA340-500OROR4 MOA340-600FC 12 FUNCTIONAL CHECK OF MLG TORQUE LINKS FOR EXCESSIVE 9 I: 2 CA340-500PLAYORA340-600RS 13 REMOVE MLG FOR RESTORATION 5,9 I: NOTE 7A340-500ORA340-600FC 14 FUNCTIONAL CHECK OF SHOCK ABSORBER NITROGEN CHARGE 8 I: 36 HRSA340-500PRESSURE (ELAPSED)ORA340-600SV 15 SERVICE MLG SHOCK ABSORBER 8 I: 36 MOA340-500ORA340-600VC 16 VISUAL CHECK OF MLG SHOCK ABSORBER SLIDING TUBE FOR 8 I: 800 FHA340-500SIGNS OF LEAKAGE AND NORMAL EXTENSIONORA340-600LU 17 LUBRICATE SHORTENING MECHANISM HINGE JOINTS 5 I: 500 FCA340-500OROR4 MOA340-600OP 18 REMOVE HYDRAULIC FUSE IN MLG BOGIE PITCH TRIMMER 9 I: 10 YEA340-500SUPPLY LINE FOR OPERATIONAL CHECK IN WORKSHOPORA340-600VC 19 VISUAL CHECK OF PITCH TRIMMER AND ASSOCIATED PIPING 9 I: AA340-500AND COMPONENTSORA340-60032.15.00 CENTERLINE GEARFC 01 FUNCTIONAL CHECK OF SHOCK ABSORBER NITROGEN CHARGE 9 I: 36 HRSA340-200PRESSURE BY READING BOTTOM AND TOP GAUGES (ELAPSED)ORA340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.15.00 * * * * * C O N T I N U E * * * * *LU 02 LUBRICATION OF CENTERLINE GEAR. 6,8 I: 500 FCALLOR4 MOFC 03 FUNCTIONAL CHECK CLG TORQUE LINKS FOR EXCESSIVE PLAY 9 I: 2 CA340-200ORA340-300SV 04 SERVICE CLG SHOCK ABSORBER 9 I: 2 CA340-200ORA340-300RS 05 REMOVE CENTERLINE GEAR FOR RESTORATION 9 I: NOTE 7A340-200ORA340-300VC 06 VISUAL CHECK OF CENTERLINE SHOCK ABSORBER FOR SIGNS 9 I: AA340-200OF LEAKAGEORA340-30007 TASK DELETEDOP 08 OPERATIONAL CHECK OF HYDRAULIC FUSE IN CLG PITCH 9 I: 10 YEA340-500TRIMMER SUPPLY LINEORA340-60009 TASK DELETEDSV 10 SERVICE CLG SHOCK ABSORBER 8 I: 36 MOA340-500ORA340-600FC 11 FUNCTIONAL CHECK OF CLG SHOCK ABSORBER NITROGEN 8 I: 36 HRSA340-500CHARGE PRESSURE BY READING BOTTOM AND TOP GAUGES (ELAPSED)ORA340-600RS 12 RESTORATION OF CENTERLINE GEAR 6,8 I: NOTE 7A340-500ORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.15.00 * * * * * C O N T I N U E * * * * *VC 13 VISUAL CHECK OF CLG SHOCK ABSORBER FOR SIGNS OF 8 I: 800 FHA340-500LEAKAGEORA340-600FC 14 FUNCTIONAL CHECK CLG TORQUE LINKS FOR EXCESSIVE PLAY 8 I: 36 MOA340-500ORA340-60032.21.00 NOSE GEARLU 01 LUBRICATION OF NOSE LANDING GEAR. 6 I: 500 FCALLOR4 MOFC 02 CHECK NOSE GEAR SHOCK ABSORBER NITROGEN CHARGE 6 I: CALLPRESSUREFC 03 FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE 6 I: 2 CALLPLAYSV 04 SERVICE NLG SHOCK ABSORBER 6 I: 2 CALLRS 05 REMOVE NOSE GEAR FOR RESTORATION 6 I: NOTE 7ALL(THIS TASK COVERS TASK 32.50.00/03).GVI 06 GENERAL VISUAL INSPECTION OF NOSE GEAR FOR SIGNS OF 6 I: AALLLEAKAGE AND NORMAL EXTENSION07 TASK DELETED32.30.00 EXTENSION AND RETRACTION POSITION AND WARNINGLU 01 LUBRICATION OF ALL GEAR UP-LOCKS, DOOR UP-LOCK UNITS 6,8 I: 500 FCA340-200AND PINS AND DOOR HINGES OROR4 MOA340-30002 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.30.00 * * * * * C O N T I N U E * * * * *LU 03 LUBRICATE ALL GEAR DOWN LOCK PIVOT PINS 5,8 I: 500 FCALLOR4 MOVC 04 VISUAL CHECK OF DOWNLOCK SPRINGS ON ALL LANDING GEARS 9 I: 2 AALL05 TASK DELETEDOP 06 OPERATIONAL CHECK OF LANDING GEAR INDICATION CIRCUITS 9 I: CA340-200TO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGSOROPERATEA340-30007 TASK DELETEDOP 08 OPERATIONAL CHECK OF LANDING GEAR FREE-FALL SYSTEM 8 I: 8000 FHALLFOR CORRECT OPERATION OF UP-LOCK RELEASE NOTE 24BOP 09 OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK 9 I: 4 CA340-200(AIRCRAFT ON WHEELS)ORA340-300OP 10 OPERATIONAL CHECK OF GROUND DOORS CLOSURE INHIBIT 9 I: 4 CA340-200ORA340-300FC 11 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE CLOSES 9 I: 4 CA340-200AT 280 KTSORA340-300FC 12 FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION 8 I: 6 YEA340-200ORA340-300GVI 13 GENERAL VISUAL INSPECTION OF LANDING GEAR HYDRAULIC 6 I: A ZL-711-01-1 ALLSYSTEM FOR SIGNS OF EXTERNAL LEAKAGE ZL-731-01-1ZL-751-01-1ZL-751-01-214 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.30.00 * * * * * C O N T I N U E * * * * *LU 15 LUBRICATE ALL LANDING GEAR UP-LOCK AND DOOR UP-LOCK 5 I: 500 FCA340-500UNITS AND PINS AND DOOR HINGES OROR4 MOA340-600FC 16 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE OPENS 8 I: 6 YEA340-500BELOW 280 KTSORA340-600FC 17 FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION 8 I: 6 YEA340-500NOTE 24BORA340-600FC 18 FUNCTIONAL CHECK OF LANDING GEAR EXTENSION 9 I: 4 CA340-500ORA340-600FC 19 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE CLOSES 8 I: 6 YEA340-500AT 280 KTSORA340-60032.40.00 WHEELS AND BRAKESVC 01 CHECK HEAT PACK WEAR INDICATOR 9 I: 7 DYALL(PARKING BRAKE APPLIED)FC 02 CHECK TYRE PRESSURES 9 I: 3 DYA340-200ORA340-300FC 03 PERFORM CROSS-CHECK OF TPIS AND TYRE PRESSURE GAUGE 9 I: AIF TPISREADINGINSTALLEDFC 04 FUNCTIONAL CHECK OF NORMAL AND ALTERNATE BRAKE RETURN 6,9 I: 2 AALLACCUMULATORS NITROGEN PRESSURES BY READING GAUGESFC 05 CHECK FLUID LEVEL OF BRAKE LOW PRESSURE RESERVOIR 6 I: CA340-200ORA340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.40.00 * * * * * C O N T I N U E * * * * *FC 06 FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON 9 I: AALLALTERNATE PARKING BRAKE ACCUMULATORS BY READINGGAUGESGVI 07 GENERAL VISUAL INSPECTION OF TYRES 6,9 I: 36 HRSALL(ELAPSED)GVI 08 GENERAL VISUAL INSPECTION OF WHEELS 9 I: 36 HRSALL(ELAPSED)VC 09 VISUAL CHECK OF BRAKES FOR HYDRAULIC LEAKS 9 I: 36 HRSALL(ELAPSED)OP 10 OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE 9 I: 4 AA340-200POST 46231ORA340-300POST 46231SV 11 DRAIN WATER ACCUMULATION IN THE DRAIN TUBE OF BRAKE 9 I: 4 AA340-200DISTRIBUTION DUAL VALVE (BDDV)POST 47210ORA340-300POST 47210FC 12 CHECK TYRE PRESSURES USING TPIS AND MCDU 6 I: 36 HRSA340-500(ELAPSED)ORA340-600OP 13 OPERATIONAL CHECK OF PARKING BRAKE CONTROL VALVE 9 I: CA340-500MOTORS 1 AND 2ORA340-600OP 14 OPERATIONAL CHECK OF THE NORMAL AND ALTERNATE BRAKE 9 I: 10 YEA340-500MANIFOLD HYDRAULIC SAFETY VALVESORA340-600OP 15 REMOVE THE ALTERNATE BRAKE FUSE MANIFOLD HYDRAULIC 9 I: 10 YEA340-500SAFETY VALVES FOR AN OPERATIONAL CHECK IN THEORWORKSHOPA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section32.40.00 * * * * * C O N T I N U E * * * * *OP 16 OPERATIONAL CHECK OF THE AUTOBRAKE SELECTOR SWITCH 8 I: 800 FHA340-500ORA340-60032.50.00 STEERINGLU 01 LUBRICATION OF NOSE LANDING GEAR ROTATING SLEEVE 6 I: 500 FCALLOR4 MOFC 02 CHECK NITROGEN PRESSURE ON NOSE WHEEL STEERING 9 I: CALLACCUMULATORRS 03 REMOVE NOSE LANDING GEAR FOR RESTORATION 9 I: NOTE 7A340-200(COVERED BY MSI 32-21-00, TASK NO5)ORA340-30032.53.00 NOSE LANDING GEAR-STEERING ANGLE PROTECTION (MOD 43442)OP 01 OPERATIONAL CHECK OF COCKPIT AND NLG WARNING LAMPS 9 I: AA340-200POST 43442ORA340-300POST 43442FC 02 FUNCTIONAL CHECK OF OVERSTEER INDICATION SYSTEM 9 I: CA340-200POST 43442ORA340-300POST 43442* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section33.00.00 LIGHTS33.14.00 ANNUNCIATOR LIGHT TEST AND DIMMINGOP 01 OPERATIONAL CHECK OF LIGHTS 9 I: 2 AALL(THIS TASK COVERS TASKS 23.81.00/01, 24.20.00/04,27.90.00/13, 31.50.00/01, 31.50.00/02, 34.13.00/01,34.14.00/01, 34.48.00/01, 34.52.00/01, 35.20.02/06).33.41.00 NAVIGATION LIGHTSNO TASK SELECTED33.48.00 ANTI-COLLISION/STROBE LIGHTINGNO TASK SELECTED33.51.00 CABIN EMERGENCY LIGHTINGOP 01 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA MCDU 9 I: 2 APOST 43069OP 02 BATTERY CAPACITY CHECK VIA MCDU 9 I: 6 MOPOST 43069NOTE 26OP 03 OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM 9 I: 2 CALLAUTOMATIC CONTROL CIRCUIT AND MANUAL ACTIVATION FROMBOTH CONTROL PANELS AND CHECK ALL LIGHTS AND SIGNSILLUMINATED BY BATTERIES04 TASK DELETEDOP 05 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA THE EPSU 9 I: 2 APRE 43069TEST PUSHBUTTON.OP 06 REMOVE BATTERY FOR CAPACITY CHECK. 9 I: 6 MOPRE 43069NOTE 26* * * * * E N D * * * * *ISSUE: JUL 01/10 LIGHTS SECTION: C-33PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section34.00.00 NAVIGATION34.13.00 AIR DATAOP 01 OPERATIONAL CHECK OF ADR SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF PITOT PROBES HEATING (115 VAC) 9 I: 2 CALLAND ADR/AOA POWER SUPPLY (26 VAC) IN EMERGENCYCONFIGURATIONRS 03 FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES 6 I: 24 MOALLNOTE 1FC 04 LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS 6 I: 2 CALLN OP 05 OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY 8 I: 12000 FHPOST 5336834.14.00 ATTITUDE, HEADING AND POSITIONOP 01 OPERATIONAL CHECK OF THE IR SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF ATT/HDG SWITCHING 9 I: CALLOP 03 OPERATIONAL CHECK OF ADIRU 1, 2 AND 3 POWER SUPPLY IN 9 I: 2 CALLEMERGENCY CONFIGURATION34.21.00 ALTITUDE AND AIRSPEED STANDBY DATARS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MOPRE 47244NOTE 1FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 CPRE 4724434.22.00 ATTITUDE AND HEADING STANDBY DATANO TASK SELECTED34.22.20 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section34.22.20 * * * * * C O N T I N U E * * * * *RS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MOPOST 47244NOTE 1FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 CPOST 47244OP 03 OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY 8 I: 800 FHPOST 4724434.35.00 HEAD-UP DISPLAY (HUD) (IF INSTALLED)NO TASK SELECTED34.36.00 INSTRUMENT LANDING SYSTEM (ILS)NO TASK SELECTED34.36.01 MULTI-MODE RECEIVER (MMR)DS 01 DISCARD AND REPLACE THE 2 COAXIAL CABLES FROM GLIDE 6 I: 5000 FCA340-500ANTENNA 2 LOCATED ON NLGORA340-600DI 02 DETAILED INSPECTION OF NLG, NLG BAY BONDING LEADS AND 6 I: 2 CA340-500G/S HEAT ELASTOMETRIC TUBINGORA340-60034.41.00 WEATHER RADAR SYSTEMFC 01 REMOVE RADOME FOR RADIO ELECTRICAL TEST 9 I: 30 MOPOST 44100PRE 44950ORPOST 44754PRE 4495034.42.00 RADIO ALTIMETEROP 01 OPERATIONAL CHECK OF FAN 9 I: NOTEALLNOTE:-36 MONTHS FOR COLLINS RA (POST 41510)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section34.42.00 * * * * * C O N T I N U E * * * * *-30 MONTHS FOR THALES RA (POST 51485 OR POST 45022)AND HONEYWELL RA (POST 43260 OR POST 46732)34.43.00 TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS) (MOD 40256)NO TASK SELECTED34.48.00 TERRAIN AWARNESS AND WARNING SYSTEM (INCLUDING (E)GPWS ANDT2CAS-TAWS)R OP 01 OPERATIONAL CHECK OF GPWS LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1).R OP 02 OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM 9 I: 2 CALL34.51.00 DISTANCE MEASURING EQUIPMENT (DME)NO TASK SELECTED34.52.00 ATC MODE S (SELECT)OP 01 OPERATIONAL CHECK OF ATC SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF THE REMOTE ATC SYSTEM 8 I: 24000 FHPOST 49769PRE 5352234.53.00 AUTOMATIC DIRECTION FINDER (ADF)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section34.53.00 * * * * * C O N T I N U E * * * * *R OP 01 OPERATIONAL CHECK OF ADF 1 IN EMERGENCY CONFIGURATION 9 I: CPRE 50859PRE 53622ORPRE 50859POST 54662ORPOST 50860PRE 53622ORPOST 50860POST 54662ORPRE 47019PRE 53622ORPRE 47019POST 54662ORPOST 47482PRE 53622ORPOST 47482POST 5466234.55.00 VOR/MARKERR OP 01 OPERATIONAL CHECK OF VOR 1 IN EMERGENCY CONFIGURATION 9 I: CPRE 53622ORPOST 5466234.58.00 SATELLITE NAVIGATION (IF INSTALLED)NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.00.00 OXYGEN35.10.00 CREW OXYGENR VC 01 VISUAL CHECK OF OXYGEN MASKS (OUT OF BOX WITH 9 I: 18 MOALLINFLATED HARNESS)R RS 02 CLEANING OF OXYGEN MASKS 8 I: 18 MOALLOP 03 OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK 8 I: 18 MOALLNOTE 5R FC 04 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6,9 I: 72 MOALLFUNCTIONAL CHECK OF CYLINDER PRESSURE GAUGE. OR NROR VRR FC 05 REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK 8 I: 72 MOALLN FC 06 REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL 8 I: 72 MOALLCHECK.N FC 07 CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN 8 I: 6500 FHALLFILL PANEL AND GAUGES ON OXYGEN CYLINDERS. OR24 MO35.20.01 PASSENGER OXYGEN (CHEMICAL)FC 01 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE 9 I: 4 CPRE 40257PRE 48635PRE 48728PRE 55606DI 02 DETAILED INSPECTION OF OXYGEN MASKS 9 I: 4 CPRE 40257NOTE 27PRE 48635PRE 48728PRE 55606OP 03 OPERATIONAL CHECK OF MANUAL MASK RELEASE 8 I: 6 YEPRE 40257PRE 48635PRE 48728PRE 55606* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.20.01 * * * * * C O N T I N U E * * * * *VC 04 VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS 8 I: 6 YEPRE 40257OF DISCHARGEPRE 48635PRE 48728PRE 55606DS 05 DISCARD CHEMICAL OXYGEN GENERATORS 8 I: VRPRE 40257PRE 48635PRE 48728PRE 55606OP 06 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 CIF PASSENGERINTERRUPTIONOXYGEN SYSTEM(CHEMICAL) ANDINSEAT POWERSUPPLYINSTALLEDVC 07 VISUAL CHECK OF CRR CHEMICAL OXYGEN GENERATORS FOR 8 I: 6 YEIF CREW RESTSIGNS OF DISCHARGE. NOTE 26ROOM WITHCHEMICALOXYGENINSTALLEDDS 08 DISCARD CRR CHEMICAL OXYGEN GENERATORS. 8 I: VRIF CREW RESTNOTE 26ROOM WITHCHEMICALOXYGENINSTALLED35.20.02 PASSENGER OXYGEN (GASEOUS)FC 01 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6 I: NR OR VRPOST 40257FUNCTIONAL CHECK OF PRESSURE REDUCER NOTE 8ORNOTE 24APOST 48635ORPOST 48728ORPOST 55606* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *VC 02 CROSS-CHECK OF QUANTITY INDICATIONS ON ECAM 8 I: 1400 FHPOST 40257"DOOR/OXY"-PAGE, OXYGEN FILL PANEL AND OXYGENORCYLINDERSPOST 48635ORPOST 48728ORPOST 55606FC 03 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION 8 I: 18 MOPOST 40257ORPOST 48635ORPOST 48728ORPOST 55606R OP 04 OPERATIONAL CHECK OF SYSTEM SHUT-OFF VALVES (MOD 8 I: 18 MOPOST 4025740257)/ PRESSURE REGULATORS (MOD 48635/48728/55606)OROPENINGPOST 48635ORPOST 48728ORPOST 55606OP 05 OPERATIONAL CHECK OF MANUAL SYSTEM OPERATION 8 I: 18 MOPOST 40257ORPOST 48635ORPOST 48728ORPOST 55606R OP 06 OPERATIONAL CHECK OF "SYS ON" LIGHT BY ANNUNCIATOR 9 I: 1600 FHPOST 40257LIGHT TESTOR(COVERED BY MSI 33-14-00 TASK NO1)POST 48635ORPOST 48728ORPOST 55606* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R OP 07 OPERATIONAL CHECK OF OXYGEN CONTAINER OPENING AND 8 I: 30 MOPOST 40257VENT FUNCTION OF BLEED/VENT VALVEORPOST 48635ORPOST 48728ORPOST 55606R FC 08 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY 8 I: 30 MOPOST 40257CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEMORPOST 48635ORPOST 48728ORPOST 55606VC 09 VISUAL CHECK OF OVERBOARD DISCHARGE LINE FOR DAMAGE 8 I: 60 MOPOST 40257ORPOST 48635ORPOST 48728ORPOST 55606R DI 10 DETAILED INSPECTION OF OXYGEN MASK ASSEMBLIES 8 I: 6 YEPOST 40257ORPOST 48635ORPOST 48728ORPOST 55606R OP 11 OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICES 8 I: 60 MOPOST 40257IN OXYGEN MASK CONTAINERSPRE 48635ORPRE 48728ORPRE 55606* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R FC 12 REMOVE RISER LINE SHUT-OFF VALVES FOR FUNCTIONAL 8 I: 60 MOPOST 40257CHECKORPOST 48635ORPOST 48728ORPOST 55606R OP 13 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM 8 I: 60 MOPOST 40257ORPOST 48635ORPOST 48728ORPOST 55606OP 14 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 CIF PASSENGERINTERRUPTIONOXYGEN SYSTEM(GASEOUS) ANDINSEAT POWERSUPPLYINSTALLEDR FC 15 REMOVE PRESSURE RELIEF VALVE FOR FUNCTIONAL CHECK 9 I: 60 MOPOST 48635ORPOST 48728ORPOST 55606R FC 16 REMOVE PRESSURE REGULATOR FOR PRESSURE REGULATING 8 I: 60 MOPOST 48635AND LEAKAGE TEST IN THE SHOPORPOST 48728ORPOST 55606OP 17 OPERATIONAL CHECK OF CYLINDER VALVE SWITCH 9 I: 4 CPOST 48635ORPOST 48728ORPOST 5560635.30.00 PORTABLE OXYGEN* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section35.30.00 * * * * * C O N T I N U E * * * * *VC 01 VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION 8 I: 8 DYALLOF PROTECTIVE BREATHING EQUIPMENT NOTE 26VC 02 CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE 9 I: 8 DYALLR FC 03 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 9 I: NRPRE 55559ORVRR DS 04 DISCARD PROTECTIVE BREATHING EQUIPMENT 8 I: VRALLNOTE 26R VC 05 VISUAL CHECK OF OXYGEN CYLINDER ATTACHMENT 9 I: 72 MOALLN DI 06 DETAILED VISUAL INSPECTION OF THE CONTINOUS FLOW 9 I: 24 MOALLMASKN FC 07 REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR 9 I: VRPOST 55559HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN ORREGULATOR. NR* * * * * E N D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section36.00.00 PNEUMATIC36.00.00 PNEUMATICDI 01 REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION 6 I: 4800 FHALLOP 02 OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE 9 I: 4000 FCALLFC 03 FUNCTIONAL CHECK OF OVERPRESSURE VALVE 9 I: 2 CALLOP 04 OPERATIONAL CHECK OF CLOSING SIGNAL TO TEMPERATURE 9 I: CALLLIMITATION THERMOSTAT SOLENOID FROM FIRE P/B SW(COVERED BY MSI 26-21-00, TASK NO3)GVI 05 GENERAL VISUAL INSPECTION OF NACA AIR INLETS OF WING 9 I: C ZL-521-01-1 ALLVENTILATION SYSTEM FOR BLOCKAGE AND DAMAGE ZL-521-01-206 TASK RESERVEDR DI 07 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: CA340-200PRE 57418ORA340-300PRE 57418SDI 08 SPECIAL DETAILED INSPECTION OF APU BLEED CHECK VALVE 8 I: 2500 FHA340-500PRE 56234ORA340-600PRE 56234R DI 09 DETAILED INSPECTION OF THE APU ENVELOPE DUCT. 8 I: 72 MOA340-50010 TASK DELETEDDI 11 REMOVE APU BLEED CHECK VALVE FOR DETAILED VISUAL 8 I: 3300 FCA340-500INSPECTION.POST 56234ORA340-600POST 56234* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section36.00.00 * * * * * C O N T I N U E * * * * *N DI 12 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: 10000 FCA340-200POST 57418ORA340-300POST 57418N DS 13 DISCARD OF APU BLEED CHECK VALVE 8 I: 10000 FCA340-500POST 56234ORA340-600POST 56234* * * * * E N D * * * * *ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section38.00.00 WATER/WASTE38.10.00 POTABLER RS 01 DISINFECTION OF POTABLE WATER SYSTEM. 9 I: 3 MOALLNOTE 8N DS 02 DISCARD WATER FILTER CARTRIDGE OF THE LAVATORIES 7,9 I: 3 MOPOST 42704NOTE 8ORPOST 49951ORPOST 57459N DS 03 DISCARD WATER FILTER CARTRIDGE OF THE GALLEYS 7,9 I: 3 MOIF INSTALLEDNOTE 838.31.00 TOILET SYSTEM01 TASK DELETEDGVI 02 GENERAL VISUAL INSPECTION OF WASTE TANKS AND WASTE 9 I: 4 C ZL-171-02-1 ALLDRAIN LINES ZL-171-02-2ZL-171-02-3DS 03 DISCARD WATER SEPARATOR. 9 I: 4 AALLNOTE 1RS 04 CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING 6 I: 350 FHALLAGENT AND CRUSHED ICE. NOTE 1D 05 TASK RESERVEDRS 06 CLEANING OF FILTER OF POLAR CAP ASSY 9 I: 4 AA340-200NOTE 1ORA340-300ORA340-500PRE 53033ORA340-600PRE 53033* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section38.31.00 * * * * * C O N T I N U E * * * * *D 07 TASK RESERVEDN RS 08 CLEANING OF LIQUID LEVEL SENSOR. 7 I: CA340-200ORA340-300ORA340-500PRE 53033ORA340-600PRE 53033N RS 09 CLEANING OF RINSE NOZZELS. 9 I: 4 AALLNOTE 1N RS 10 CLEANING OF WASTE TANKS AND WASTE DRAIN LINES. 6,9 I: CALLN RS 11 CLEANING OF REFERENCE PRESSURE LINE LIQUIDE LEVEL 7 I: 4 AA340-200TRANSMITTER. NOTE 1ORA340-300N RS 12 CLEANING OF ABSOLUTE PRESSURE SENSORS (HAPS, AAPS) 7 I: 4 AA340-500NOTE 1PRE 57393ORA340-600PRE 57393N 13 TASK RESERVED38.32.00 WASTE WATER DRAINGVI 01 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN LINES 9 I: 4 C ZL-133-01-1 ALLIN BILGE AREA FOR LEAKAGE. ZL-133-01-2ZL-153-01-1ZL-153-01-2ZL-153-01-3ZL-171-02-1ZL-171-02-2ZL-171-02-3GVI 02 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN LINES 9 I: 8 C ZL-131-03-1 ALLIN CARGO COMPARTMENTS FOR LEAKAGE. ZL-131-03-2* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section38.32.00 * * * * * C O N T I N U E * * * * *ZL-151-03-1ZL-151-03-2ZL-151-03-3ZL-161-03-1ZL-161-03-2RS 03 CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE 7 I: 600 FHA340-200POST 45556ORA340-200POST 49705ORA340-200POST 50088ORA340-300POST 45556ORA340-300POST 49705ORA340-300POST 50088ORA340-500ORA340-60038.40.00 AIR SUPPLYDI 01 DETAILED INSPECTION OF COMPRESSOR INLET FILTER 9 I: 2 CPOST 40243ORPOST 47086DS 02 DISCARD SYSTEM FILTER ELEMENT 6,9 I: 4 CALLDS 03 DISCARD COMPRESSOR OUTLET FILTER ELEMENT 9 I: 4 CPOST 40243ORPOST 47086* * * * * E N D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section45.00.00 ONBOARD MAINTENANCE SYSTEM45.10.00 CENTRAL MAINTENANCE SYSTEM (CMS)01 TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 ONBOARD MAINTENANCE SYSTEM SECTION: C-45PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section46.00.00 INFORMATION SYSTEMS46.11.00 FLYSMART WITH AIRBUSN RS 01 CALIBRATION OF BASE TRANSCEIVER STATION 7 I: VRA340POST 5864046.11.34 SIU (SERVER INTERFACE UNIT)NO TASK SELECTED46.21.00 ATIMSNO TASK SELECTED46.21.01 ATIMS FANS CONFIGURATIONSR NO TASK SELECTED46.55.00 ON-BOARD INFORMATION TERMINAL (OIT)N NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 INFORMATION SYSTEMS SECTION: C-46PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionAPU 331-35049.00.00 AIRBORNE AUXILIARY POWER49.12.00 APU MOUNTSVC 01 VISUAL CHECK OF APU SUSPENSION SYSTEM INCLUDING 9 I: CA340-200SHOCKMOUNT STRUCTURE AND BRACKETSORA340-30049.13.00 FIRE SEALSGVI 01 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE 8 I: 20000 FHA340-200WALLS INCLUDING FORWARD, AFT, UPPER, SIDE ANDORCOMPARTMENT DOORSA340-30049.16.00 AIR INTAKE SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF DIVERTER AND FLUID 9 I: 2 C ZL-311-01-1 A340-200GUTTERS ZL-313-01-1 ORA340-30049.17.00 POWERPLANT DRAIN SYSTEM01 TASK DELETEDGVI 02 GENERAL VISUAL INSPECTION OF DRAIN PIPES 9 I: C ZL-315-01-1 A340-200ZL-317-01-1 ORA340-30049.20.00 ENGINENO TASK SELECTED49.23.00 LOAD COMPRESSORNO TASK SELECTEDISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-49 PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.26.00 ACCESSORY DRIVE GEARBOXNO TASK SELECTED49.30.00 FUEL DISTRIBUTION AND CONTROLVC 01 VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR 9 I: 1500 AHA340-200BUTTON ON FUEL FILTERORA340-30049.34.00 APU FUEL LOW PRESSURE WARNINGNO TASK SELECTED49.40.00 IGNITION AND STARTINGNO TASK SELECTED49.51.00 BLEED AND SURGE AIRNO TASK SELECTED49.52.00 ACCESSORY COOLINGNO TASK SELECTED49.60.00 ENGINE CONTROLSNO TASK SELECTED49.62.00 EMERGENCY SHUTDOWNOP 01 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CA340-200APU STOP SWITCH 1KLORA340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-49 PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.62.00 * * * * * C O N T I N U E * * * * *OP 02 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CA340-200APU STOP SWITCH 2KLORNOTE: IT IS RECOMMENDED THAT BOTH TASKS 1 AND 2 AREA340-300PERFORMED ALTERNATELYOP 03 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT (APU 9 I: 2 CA340-200FIRE STOP RELAY 5WF)OR(COVERED BY MSI 26-22-00, TASK NO2)A340-300OP 04 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT. (APU 9 I: 2 CA340-200FIRE P/B SW)OR(COVERED BY MSI 26-22-00, TASK NO10)A340-30049.70.00 INDICATINGNO TASK SELECTED49.80.00 EXHAUSTVC 01 VISUAL CHECK OF V-CLAMP AND EXHAUST DUCT 9 I: CA340-200ORA340-300VC 02 VISUAL CHECK OF EXHAUST DUCT HEAT INSULATION 9 I: 2 CA340-200ORA340-300DI 03 DETAILED INSPECTION OF SEALING RING COUPLING AND 9 I: 2 CA340-200BELLOWSORA340-30049.90.00 OILVC 01 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON LUBE 9 I: 500 AHA340-200FILTER.PRE 56284ORA340-300PRE 56284* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-49 PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.90.00 * * * * * C O N T I N U E * * * * *VC 02 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON 9 I: 500 AHA340-200GENERATOR SCAVENGE FILTERPRE 56284ORA340-300PRE 56284* * * * * E N D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-49 PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionAPU 331-60049.00.00 AIRBORNE AUXILIARY POWER49.12.00 APU MOUNTSVC 01 VISUAL CHECK OF APU SUSPENSION SYSTEM INCLUDING 9 I: 5000 FHA340-500SHOCKMOUNT STRUCTURE, BRACKETS AND VISIBLE PART OFORSTRUCTURE ATTACHMENT FITTINGSA340-60049.13.00 FIRE SEALSGVI 01 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE 8 I: 20000 FHA340-500SEALS, WALLS INCLUDING FORWARD, AFT, UPPER, SIDES ANDORCOMPARTMENT DOORSA340-60049.16.00 AIR INTAKE SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF DIVERTER AND FLUID 9 I: 2 C ZL-311-01-2 A340-500GUTTERS ZL-313-01-2 ORA340-600GVI 02 GENERAL VISUAL INSPECTION OF AIR INLET PLENUM AND 9 I: 2 C ZL-311-01-2 A340-500AIR INTAKE DUCTORA340-60049.17.00 POWERPLANT DRAIN SYSTEM01 TASK DELETEDGVI 02 GENERAL VISUAL INSPECTION OF DRAIN PIPES 9 I: C ZL-315-01-1 A340-500ZL-317-01-2 ORA340-60049.21.00 POWER SECTION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-49 PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.21.00 * * * * * C O N T I N U E * * * * *DS 01 DISCARD TURBINE WHEELS 7 I: NOTE 4A340-500ORA340-60049.23.00 LOAD COMPRESSORNO TASK SELECTED49.26.00 ACCESSORY DRIVE GEARBOXNO TASK SELECTED49.30.00 ENGINE FUEL AND CONTROLGVI 01 GENERAL VISUAL INSPECTION OF THE FUEL SYSTEM 9 I: C ZL-315-01-1 A340-500COMPONENTS, SEALS,LINES AND INTERFACE CONNECTIONS FOROREVIDENCE OF LEAKAGEA340-60049.34.00 APU FUEL LOW PRESSURE WARNINGNO TASK SELECTED49.40.00 IGNITION AND STARTINGNO TASK SELECTED49.51.00 BLEED AND SURGE AIRNO TASK SELECTED49.61.00 CONTROL AND MONITORINGNO TASK SELECTED49.62.00 EMERGENCY SHUTDOWN* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-49 PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.62.00 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CA340-500APU STOP SWITCH (1KL)ORA340-600OP 02 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CA340-500APU STOP SWITCH (2KL)ORNOTE: IT IS RECOMMENDED THAT BOTH TASKS 1 AND 2 AREA340-600PERFORMED ALTERNATELYOP 03 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT (APU 9 I: 2 CA340-500FIRE P/B SWITCH)OR(COVERED BY MSI 26.22.00, TASK NO10)A340-600OP 04 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT. (APU 9 I: 2 CA340-500FIRE EMERGENCY STOP RELAY 5WF)OR(COVERED BY MSI 26.22.00, TASK NO02)A340-60049.70.00 INDICATINGNO TASK SELECTED49.80.00 EXHAUSTVC 01 VISUAL CHECK OF V-CLAMP AND EXHAUST MUFFLER IN APU 9 I: CA340-500COMPARTMENTORA340-600VC 02 VISUAL CHECK OF EXHAUST MUFFLER INSULATION 9 I: 2 CA340-500ORA340-600DI 03 DETAILED INSPECTION OF SEALING RING GUIDE ASSY AND 9 I: 2 CA340-500BELLOWSORA340-600VC 04 VISUAL CHECK OF MUFFLER FROM JET PIPE 9 I: CA340-500ORA340-60049.90.00 OIL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-49 PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section49.90.00 * * * * * C O N T I N U E * * * * *NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-49 PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section52.00.00 DOORS52.10.00 PASSENGER/CREW DOORSLU 01 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 6,9 I: CNOTEHANDLENOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. ANY DOORINFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGERCOMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/02OP 02 OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN 9 I: CNOTEPOSITIONNOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. ANY DOORINFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGERCOMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/0303 TASK DELETEDFC 04 FUNCTIONAL CHECK OF LOCKING MECHANISM 6,9 I: 2 CNOTENOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. ANY DOORINFREQUENTLY USED SHALL BE MAINTAINED AS APASSENGER COMPARTMENT EMERGENCY EXIT.REFER TO MSI 52-22-00/05OP 05 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 CALLIS OPENED FROM OUTSIDEOP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 CALLLEVER IS LOCKED IN DISARMED POSITION WHEN DOOR ISOPENGVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-831-01-1 ALLZL-832-01-1ZL-833-01-1VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 CALLFITTINGS* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section52.10.00 * * * * * C O N T I N U E * * * * *FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MOALLSLIDER.52.22.00 PASSENGER COMPARTMENT EMERGENCY EXITOP 01 OPERATIONAL CHECK OF DOOR DAMPING, ESCAPE SLIDE 9 I: CALLRELEASE MECHANISM DISARMING, AND TO ENSURE THAT DOORCANNOT BE LOWERED AND LOCKED WHEN OPENLU 02 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 8 I: 18 MOALLHANDLEOP 03 OPERATIONAL CHECK OF DOOR UNLOCKING/LOCKING AND DOOR 8 I: 18 MOALLOPENING/CLOSING FROM INSIDE AND OUTSIDE AND DOORLATCHING IN FULLY OPEN POSITIONOP 04 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 CALLIS OPENED FROM OUTSIDEFC 05 FUNCTIONAL CHECK OF LOCKING MECHANISM 8 I: 36 MOALLOP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 CALLLEVER IS LOCKED IN DISARMED POSITION WHEN DOOR ISOPENGVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-834-01-1 ALLVC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 CALLFITTINGSFC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MOALLSLIDER.NOTENOTE: TASK NOT APPLICABLE FOR A340-600 OVERWINGEMERGENCY EXIT52.31.00 FWD AND AFT CARGO COMPARTMENT DOORLU 01 LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING, 6,9 I: CALLLATCHING AND INTERLOCK MECHANISMS* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section52.31.00 * * * * * C O N T I N U E * * * * *FC 02 FUNCTIONAL CHECK OF LATCHING AND LOCKING HANDLE 6,9 I: 4 CALLFORCES, AND OF WEAR AND OVERCENTER POSITIONS OFLATCHING, LOCKING AND INTERLOCK MECHANISMSGVI 03 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-821-01-1 ALLZL-821-01-2ZL-822-01-1ZL-822-01-252.33.00 BULK CARGO COMPARTMENT DOOROP 01 OPERATIONAL CHECK OF DOOR BALANCE MECHANISM AND OF 9 I: CA340-200DOOR LATCHING IN FULLY OPEN POSITIONORA340-300ORA340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288GVI 02 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-823-01-1 A340-200ZL-823-01-2 ORA340-300ORA340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section52.33.00 * * * * * C O N T I N U E * * * * *LU 03 LUBRICATION OF BULK CARGO COMPARTMENT DOOR COMPONENTS 6 I: CA340-200ORA340-300ORA340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 4928852.36.00 CARGO COMPARTMENT DOOR HYDRAULIC SYSTEMNO TASK SELECTED52.41.11 AVIONICS COMPARTMENT FWD DOORGVI 01 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-811-01-1 ALLZL-811-01-252.51.11 COCKPIT DOORFC 01 FUNCTIONAL CHECK OF SPRING LOADED DOOR STOP MECHANISM 9 I: 2 CPRE 50014DI 02 DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR 6,9 I: 2 CPOST 50014LOCKING SYSTEMOP 03 OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS 9 I: 2 CPOST 50014FOR RAPID DECOMPRESSION, CHECK OF DOOR OPENING INCASE OF POWER OFF AND BY USING THE EMERGENCY CODER OP 04 OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE 8 I: 11000 FHPOST 50014MECHANISM NOTE 24PRE 57371R DI 05 DETAILED INSPECTION OF FLAP BELLOW 8 I: 36 MOPOST 50014PRE 57371* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section52.51.11 * * * * * C O N T I N U E * * * * *OP 06 OPERATIONAL CHECK OF MANUAL SWITCH OVER 9 I: 2 CPOST 50723ORPOST 53123N OP 07 OPERATIONAL CHECK OF FLAP RELEASE MECHANISM (MANUAL 8 I: 72 MOPOST 57371OPENING).N GVI 08 GENERAL VISUAL INSPECTION OF AIR CYLINDER OF 8 I: 72 MOPOST 57371DECOMPRESSION PANEL.52.70.00 DOOR WARNINGOP 01 OPERATIONAL CHECK OF DOOR WARNING SYSTEM 9 I: 4 CALLFC 02 CHECK BATTERY CAPACITY OF AUTONOMOUS STANDBY POWER 9 I: 8 MOALLSUPPLY UNIT (ASPSU)OP 03 BITE TEST OF AUTONOMOUS STANDBY POWER SUPPLY UNIT 9 I: 4 AALL(ASPSU)OP 04 OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE 9 I: 2 CALLWARNING SYSTEMFC 05 OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING 9 I: 4 CALLSYSTEM AND FUNCTIONAL CHECK OF ASSOCIATED PRESSURESWITCH* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section53.00.00 FUSELAGE53.19.00 FUSELAGE DRAINSVC 01 VISUAL CHECK OF DRAIN HOLES IN LOWER PART OF FR1 AND 9 I: CALLFR80 (FROM INSIDE)VC 02 VISUAL CHECK OF PISTON TYPE DRAIN VALVES IN LOWER 9 I: CALLFUSELAGE SHELL (FROM OUTSIDE) AND IN FWD AND AFTCARGO COMPARTMENT DOORSOP 03 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT UPPER 9 I: CALLAFT END OF CENTER WING BOX (FROM MAIN LANDING GEARBAY).OP 04 OPERATIONAL CHECK OF DRAIN MAST/PIPES AFT OF FR80 9 I: 5 MOALLOP 05 OPERATIONAL CHECK OF DRAIN HOLES IN UNPRESSURIZED 9 I: CALLPART OF FUSELAGE (IN RADOME, FORWARD OF FR1, BEHINDREAR PRESSURE BULKHEAD, IN BELLY FAIRING, TAIL CONEAND IN CARGO COMPARTMENT DOORS).VC 06 VISUAL CHECK OF HOLES OF PISTON TYPE DRAIN OR 9 I: 4 CALLPRESSURE DRAIN VALVES AND PRESSURE SEAL DRAINS FROMINSIDE (IN FUSELAGE BILGE AREA, AT UPPER AFT END OFCENTER WING BOX, IN CARGO COMPARTMENT DOORS AND ATRCT)VC 07 VISUAL CHECK OF PRESSURE SEAL DRAINS AT RCT (FROM 9 I: 4 CA340-500INSIDE)OP 08 OPERATIONAL CHECK OF DRAIN GAPS BETWEEN "THS-CUTOUT 9 I: 10 MOA340-500FAIRING" PANELS AND AT RUBBER SEALORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE SECTION: C-53PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section53.19.00 * * * * * C O N T I N U E * * * * *OP 09 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT BULK 9 I: 1 CA340-200CARGO COMPARTMENT DOOR (FROM OUTSIDE).ORA340-300ORA340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE SECTION: C-53PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section54.00.00 NACELLES/PYLONS54.59.00 PYLON DRAINSOP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: CA340-200F DRAIN SYSTEMORA340-300OP 02 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C, D 9 I: 2 CA340-500AND F DRAIN SYSTEMORA340-600* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section55.00.00 STABILIZERS55.16.00 TRIMMABLE HORIZONTAL STABILIZER ATTACH FITTINGSLU 01 LUBRICATION OF THS HINGE LINE BEARINGS 9 I: 7500 FHALLOR18 MOLU 02 LUBRICATION OF UPPER AND LOWER FRAME ATTACHMENT 9 I: 7500 FHALLBEARINGS OR18 MO* * * * * E N D * * * * *ISSUE: JUL 01/10 STABILIZERS SECTION: C-55PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section56.00.00 WINDOWS56.12.00 SLIDING WINDOWSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 WINDOWS SECTION: C-56PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section57.00.00 WINGS57.29.00 WING DRAINS (OUTER WING)OP 01 OPERATIONAL CHECK OF DRAIN HOSES AND DESIGNATED 9 I: 4 CALLDRAIN HOLES FOR CLOGGING57.39.00 WING DRAINS (WING TIP)OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 CALL57.59.00 WING DRAINS (LEADING/TRAILING EDGE AND LEADING/TRAILING EDGEDEVICES)OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 CALL* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: C-57PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-571.00.00 POWERPLANT71.10.00 COWLINGGVI 01 GENERAL VISUAL INSPECTION OF INLET COWL LIP ASSEMBLY 6 I: 2 AA340-200AND INNER BARREL FAN FLOW AREAORA340-300DI 02 DETAILED INSPECTION OF INLET COWL LIP ASSEMBLY AND 6 I: CA340-200INNER BARREL FAN FLOW AREAORA340-300GVI 03 GENERAL VISUAL INSPECTION OF FAN COWL HINGES AND 9 I: CA340-200ADJACENT STRUCTUREORA340-300GVI 04 GENERAL VISUAL INSPECTION OF FAN COWL LATCHES, 9 I: CA340-200KEEPERS AND ADJACENT STRUCTUREORA340-300DI 05 DETAILED INSPECTION OF INLET COWL ATTACHMENT FEATURES 9 I: CA340-200ORA340-300GVI 06 GENERAL VISUAL INSPECTION OF INLET COWL AFT BULKHEAD 9 I: C ZL-412-01-1 A340-200AND TITANIUM SHIELDORA340-300GVI 07 GENERAL VISUAL INSPECTION OF FAN COWL DOORS NEXTEL 9 I: C ZL-412-01-1 A340-200COVERINGORA340-300GVI 08 GENERAL VISUAL INSPECTION OF FAN COWL DOOR FIRE SEALS 8 I: 18 MOA340-200ORA340-300FC 09 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 9 I: CA340-200ORA340-30071.70.00 POWERPLANT DRAINS* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-CFM56-5-71PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section71.70.00 * * * * * C O N T I N U E * * * * *NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-CFM56-5-71PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-572.00.00 ENGINE72.20.00 FAN SECTION01 TASK DELETEDDI 02 DETAILED INSPECTION OF FAN BLADES AND SPINNER 6 I: 2 AA340-200ORA340-300DI 03 DETAILED INSPECTION OF VISIBLE AREA OF ENGINE INLET 6 I: 2 AA340-200AND FAN OUTLET FOR DAMAGE AND/OR MISSING ABRADABLEORMATERIALA340-300DI 04 DETAILED INSPECTION OF ATTACHMENT POINTS FOR AIR 9 I: 8 CA340-200INTAKE COWL AND THRUST REVERSER "V" GROOVEORA340-300DI 05 DETAILED INSPECTION OF FORWARD ENGINE MOUNT FAN FRAME 9 I: 8 CA340-200ATTACHMENT POINTSORA340-300DS 06 DISCARD LIFE LIMITED PARTS OF FAN SECTION 5 I: NOTE 4A340-200ORA340-300DS 07 DISCARD FAN SHAFT 5 I: NOTE 4A340-200ORA340-300RS 08 DETAILED INSPECTION AND RELUBRICATION OF FAN BLADE 6 I: 1000 FCA340-200DOVETAILS, MIDSPAN SHROUDS, RETAINERS, SPACERS ANDORFAN DISK DOVETAIL SLOTSA340-30072.30.00 HP COMPRESSOR SECTIONDS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4A340-200ORA340-300ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-72PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section72.40.00 COMBUSTION SECTIONSDI 01 BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINERS AND 9 I: 6000 FHA340-200DOME AREAORA340-30072.50.00 TURBINE SECTION01 TASK DELETEDSDI 02 BORESCOPE INSPECTION OF HPT NOZZLE FROM TWO PORTS ON 6 I: 6000 FHA340-200FORWARD SIDEORA340-300SDI 03 BORESCOPE INSPECTION OF HPT BLADES 6 I: 500 FCA340-200ORA340-300DI 04 DETAILED INSPECTION OF AFT MOUNT LUGS FOR STRUCTURAL 9 I: 8 CA340-200INTEGRITY AND DEFORMATIONORA340-300DS 05 DISCARD LIFE LIMITED PARTS OF HP AND LP TURBINE 5 I: NOTE 4A340-200ORA340-300SDI 06 BORESCOPE INSPECTION OF LEADING EDGES OF LPT STAGE 1 - I: 1500 FCA340-200BLADES.PRE 41225PRE 42226ORA340-300PRE 41225PRE 4222672.60.00 ACCESSORY DRIVE SECTION01 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-72PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section72.60.00 * * * * * C O N T I N U E * * * * *DI 02 CHECK TRANSFER GEARBOX AND ACCESSORY GEARBOX SCAVENGE 6 I: CA340-200SCREENS FOR DEBRISOR(COVERED BY MSI 79-20-00, TASK NO3).A340-300GVI 03 GENERAL VISUAL INSPECTION OF TRANSFER GEARBOX AND 6 I: C ZL-412-01-1 A340-200ACCESSORY GEARBOX HOUSINGS FOR LEAKSORA340-300* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-72PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-573.00.00 ENGINE FUEL AND CONTROL73.00.00 ENGINE FUEL AND CONTROL GENERALDS 01 DISCARD FUEL FILTER ELEMENT 9 I: 4000 FHA340-200ORA340-300OP 02 OPERATIONAL CHECK OF THRUST REVERSER DEPLOY SWITCHES 9 I: 5000 FCA340-200ORA340-300OP 03 OPERATIONAL CHECK OF THRUST REVERSER SYSTEM VIA MCDU 9 I: 5000 FCA340-200ORA340-30004 TASK DELETED05 TASK DELETED73.25.00 FUNCTIONAL INTERFACE01 TASK DELETEDOP 02 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CA340-200(COVERED BY MSI 21-26-00, TASK NO2).ORA340-300* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-CFM56-5-73PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-574.00.00 IGNITION74.00.00 IGNITIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 IGNITION SECTION: C-CFM56-5-74PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-575.00.00 AIR75.20.00 COOLINGNO TASK SELECTED75.30.00 COMPRESSOR CONTROLNO TASK SELECTED75.40.00 NACELLE TEMPERATURE INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR SECTION: C-CFM56-5-75PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-576.00.00 ENGINE CONTROLS76.00.00 ENGINE CONTROLS GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-CFM56-5-76PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-577.00.00 ENGINE INDICATING77.00.00 ENGINE INDICATING GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-CFM56-5-77PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-578.00.00 EXHAUST78.10.00 TURBINE EXHAUST SYSTEMDI 01 DETAILED INSPECTION OF NOZZLE, MIXER AND CENTERBODY 9 I: CA340-200FOR STRUCTURAL DAMAGE AND SECURITY OF ATTACHMENTORA340-300DI 02 DETAILED INSPECTION OF MIXER AND CENTERBODY 9 I: CA340-200ATTACHMENT FEATURESORA340-300DI 03 DETAILED INSPECTION OF FIRE SEALS FOR DAMAGE AND 8 I: 18 MOA340-200SECURITY OF ATTACHMENTORA340-30078.31.00 THRUST REVERSER CONTROL AND INDICATING01 TASK DELETEDGVI 02 GENERAL VISUAL INSPECTION OF HYDRAULIC FLEXIBLE HOSES 6 I: CA340-200ORA340-300OP 03 OPERATIONAL CHECK OF ACTUATOR SECONDARY LOCKS 8 I: 8000 FHA340-200NOTE 24AORA340-300DS 04 REMOVE RESTRICTOR/CHECK VALVE IN ADDITIONAL RETURN 8 I: 34000 FHA340-200LINE FOR WORKSHOP CHECK NOTE 24AORA340-30078.32.00 THRUST REVERSER STRUCTUREGVI 01 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, 9 I: CA340-200LATCHES AND STRUCTURE ADJACENT TO HINGES AND LATCHESORA340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-CFM56-5-78PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section78.32.00 * * * * * C O N T I N U E * * * * *GVI 02 GENERAL VISUAL INSPECTION OF "V" GROOVES ON FWD AND 9 I: CA340-200ON AFT FACE OF THRUST REVERSER AND ADAPTER RING OFORENGINE, FAN FRAMEA340-300GVI 03 GENERAL VISUAL INSPECTION OF MOVEABLE KICKER PLATE, 9 I: CA340-200ADJACENT PIVOTING DOOR AND ACTUATOR AREA. (BLOCKERORDOORS DEPLOYED)A340-300GVI 04 GENERAL VISUAL INSPECTION OF THRUST REVERSER 9 I: C ZL-417-01-1 A340-200STRUCTURE IN BLEED AND FLOW AIR PASSAGESORA340-300GVI 05 GENERAL VISUAL INSPECTION OF INNER BARREL FIRE 8 I: 18 MOA340-200THERMAL BLANKETSORA340-300GVI 06 GENERAL VISUAL INSPECTION OF PIVOTING DOOR SEALS 9 I: CA340-200ORA340-30078.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-CFM56-5-78PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-579.00.00 OIL79.10.00 STORAGENO TASK SELECTED79.20.00 DISTRIBUTION01 TASK DELETEDDS 02 DISCARD PRIMARY FILTER 9 I: 4000 FHA340-200ORA340-300DI 03 CHECK OF FWD SUMP, AFT SUMP ACCESSORY GEARBOX AND 6 I: CA340-200TRANSFER GEARBOX SCAVENGE SCREENSOR(THIS TASK COVERS TASK 72.60.00/02-C5)A340-300OP 04 OPERATIONAL CHECK OF ELECTRICAL MAGNETIC CHIP 9 I: CA340-200DETECTORORA340-30079.31.00 OIL QUANTITY TRANSMITTER SYSTEMNO TASK SELECTED79.32.00 OIL TEMPERATURE INDICATING SYSTEMNO TASK SELECTED79.33.00 OIL PRESSURE INDICATING SYSTEMNO TASK SELECTED79.34.00 LOW OIL PRESSURE WARNING SYSTEM* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-CFM56-5-79PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section79.34.00 * * * * * C O N T I N U E * * * * *NO TASK SELECTED79.35.00 OIL FILTER CLOGGING WARNING SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-CFM56-5-79PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionCFM56-580.00.00 STARTING80.10.00 STARTINGDI 01 STARTER OIL LEVEL CHECK/REPLENISH AND CHECK OF 6 I: AA340-200MAGNETIC CHIP DETECTOR FOR PARTICLESORA340-300SV 02 DRAIN AND REPLENISH STARTER OIL 6 I: 2400 FHA340-200ORA340-300* * * * * E N D * * * * *ISSUE: JUL 01/10 STARTING SECTION: C-CFM56-5-80PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50071.00.00 POWERPLANT71.13.00 FAN COWLGVI 01 GENERAL VISUAL INSPECTION OF THE FAN COWL DOORS 9 I: CA340-500/STRAKES FOR CONDITIONORA340-600GVI 02 GENERAL VISUAL INSPECTION OF THE NEXTEL INNER SKIN 9 I: CA340-500FOR DAMAGEORA340-600FC 03 FUNCTIONAL CHECK OF LATCHES TENSION 9 I: CA340-500ORA340-60071.61.00 AIR INTAKE COWLGVI 01 GENERAL VISUAL INSPECTION OF INNER AND OUTER SURFACES 9 I: CA340-500OF AIR INTAKE COWL FOR DAMAGE AND DEFORMATIONORA340-600GVI 02 GENERAL VISUAL INSPECTION OF AIR INTAKE COWL SEALS 9 I: CA340-500FOR DAMAGE OR MISSING PARTSORA340-60071.71.00 POWERPLANT DRAINSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-RR T500-71PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50072.00.00 ENGINE72.22.00 GAS GENERATOR FAIRINGSGVI 01 GENERAL VISUAL INSPECTION OF THE GAS GENERATOR 9 I: C ZL-413-04-1 A340-500FAIRINGS AND UPPER AND LOWER SPLITTER FAIRINGS FORORSIGNIFICANT DAMAGEA340-60072.31.00 LP COMPRESSOR MODULEDI 01 DETAILED INSPECTION OF LP COMPRESSOR BLADES 6,9 I: 2 AA340-500ORA340-600DS 02 DISCARD THE LP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4A340-500ORA340-600RS 03 RE-APPLICATION OF ROOT COATINGS TO LP COMPRESSOR 6 I: 4000 FCA340-500BLADESORA340-600LU 04 RE-LUBRICATION OF LP COMPRESSOR BLADE ROOT COATINGS 6 I: 1200 FCA340-500ORA340-60072.32.00 IP COMPRESSOR MODULEDS 01 DISCARD THE IP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4A340-500(THIS TASK COVERS TASK 72.33.00/02-R5)ORA340-60072.33.00 COMPRESSOR INTERMEDIATE MODULE01 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-72PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section72.33.00 * * * * * C O N T I N U E * * * * *DS 02 DISCARD THE IP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4A340-500(COVERED BY MSI 72.32.00 TASK NO 01)ORA340-600DI 03 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FHA340-500BY MSI 79.30.00, TASK 2)POST 50676ORA340-600POST 5067672.33.40 EXTERNAL GEARBOX DRIVEDI 01 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FHA340-500BY MSI 79.30.00, TASK 2)POST 50676ORA340-600POST 5067672.34.00 LP COMPRESSOR CASINGGVI 01 GENERAL VISUAL INSPECTION OF THE FAN TRACK AND COLD 9 I: CA340-500STREAM DUCT FOR SIGNIFICANT DAMAGEORA340-600GVI 02 GENERAL VISUAL INSPECTION OF THE SPLITTER FAIRING FOR 9 I: CA340-500SIGNIFICANT DAMAGEORA340-60072.40.00 COMBUSTION SECTIONSDI 01 SPECIAL DETAILED BORESCOPE INSPECTION OF COMBUSTOR 9 T: 1000 FCA340-500OROR9000 FHA340-600I: 550 FCOR5000 FH72.41.20 HP COMPRESSOR ASSEMBLY* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-72PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section72.41.20 * * * * * C O N T I N U E * * * * *DS 01 DISCARD THE HP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4A340-500ORA340-60072.41.50 HP TURBINE SECTIONSDI 01 SPECIAL DETAILED BORESCOPE INSPECTION OF THE HPT 6,9 T: 1000 FCA340-500NOZZLE GUIDE VANES OROR9000 FHA340-600I: 500 FCOR4500 FHDS 02 DISCARD THE HP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4A340-500ORA340-600SDI 03 SPECIAL DETAILED BORESCOPE INSPECTION OF THE HPT 6,9 T: 1000 FCA340-500BLADES OROR9000 FHA340-600I: 550 FCOR5000 FH72.51.00 IP/LP TURBINE MODULEDS 01 DISCARD THE IP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4A340-500ORA340-60072.52.00 LP TURBINE MODULEDS 01 DISCARD THE LP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4A340-500ORA340-600VC 02 VISUAL CHECK OF THE TAIL BEARING HOUSING SUPPORT 8 I: 4000 FCA340-500STRUCTURE ATTACHMENT LUGSORA340-600ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-72PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section72.61.00 EXTERNAL GEARBOX MODULEDI 01 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FHA340-500BY MSI 79.30.00, TASK 2)POST 50676ORA340-600POST 5067672.62.00 EXTERNAL GEARBOX DRIVESHAFT AND SHROUDNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-72PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50073.00.00 ENGINE FUEL AND CONTROL73.10.00 FUEL DISTRIBUTIONDS 01 DISCARD LP FUEL FILTER ELEMENT 6,9 I: 1600 FCA340-500OROR10000 FHA340-60073.20.00 ENGINE FUEL AND CONTROLNO TASK SELECTED73.25.00 FUNCTIONAL INTERFACEOP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CA340-500(COVERED BY MSI 21-26-00, TASK NO2)ORA340-60073.30.00 ENGINE FUEL INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-RR T500-73PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50074.00.00 IGNITION74.00.00 IGNITIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 IGNITION SECTION: C-RR T500-74PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50075.00.00 AIR75.21.00 ACCESSORY/ZONE COOLINGGVI 01 GENERAL VISUAL INSPECTION OF COOLING AIR INLET, AIR 9 I: C ZL-400-01-2 A340-500OUTLET FOR DAMAGE AND BLOCKAGE ZL-412-04-1 ORA340-60075.22.00 ENGINE COOLING AND SEALINGNO TASK SELECTED75.24.00 TURBINE CASE COOLING SYSTEMNO TASK SELECTED75.33.00 IP/HP COMPRESSOR AIRFLOW CONTROLNO TASK SELECTED75.41.00 NACELLE TEMPERATURE INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR SECTION: C-RR T500-75PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50076.00.00 ENGINE CONTROLS76.00.00 ENGINE CONTROLSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-RR T500-76PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50077.00.00 ENGINE INDICATING77.00.00 ENGINE INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-RR T500-77PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50078.00.00 EXHAUST78.11.00 TURBINE EXHAUSTGVI 01 GENERAL VISUAL INSPECTION OF THE AIR WASHED SURFACE 9 I: C ZL-417-04-1 A340-500OF THE NOZZLEORA340-600GVI 02 GENERAL VISUAL INSPECTION OF THE AIR WASHED SURFACE 9 I: CA340-500OF THE PLUGSORA340-600GVI 03 GENERAL VISUAL INSPECTION OF THE EXHAUST FIRE SEAL 8 I: 18 MOA340-500FOR DAMAGEORA340-60078.31.00 THRUST REVERSER CONTROL AND INDICATINGGVI 01 GENERAL VISUAL INSPECTION OF HYDRAULIC TUBES AND 6 I: C ZL-417-04-1 A340-500ACTUATOR FOR DAMAGEORA340-600FC 02 FUNCTIONAL CHECK OF THE THRUST REVERSER PRIMARY 6 I: 2700 FCA340-500LOCKS, TERTIARY LOCKS AND SYNCHRO SHAFTS NOTE 24BORA340-60078.32.00 THRUST REVERSER STRUCTUREGVI 01 GENERAL VISUAL INSPECTION OF THE THRUST REVERSER 9 I: C ZL-417-04-1 A340-500INTERNAL AND EXTERNAL AERODYNAMIC SURFACESORA340-600GVI 02 GENERAL VISUAL INSPECTION OF THE FORWARD PRESSURE 9 I: C ZL-417-04-1 A340-500SEAL FOR DAMAGE OR MISSING SEGMENTORA340-600GVI 03 GENERAL VISUAL INSPECTION OF THE FIRE SEALS AND FIRE 8 I: 18 MOA340-500SHIELDS, INCLUDING THE BLEED VALVE DUCT SEALSORA340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T500-78PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant Section78.32.00 * * * * * C O N T I N U E * * * * *GVI 04 GENERAL VISUAL INSPECTION OF THRUST REVERSER 9 I: CA340-500CASCADES, BLOCKER DOORS, LINKS AND HINGES FOR DAMAGEORA340-600GVI 05 GENERAL VISUAL INSPECTION OF THE THERMAL BLANKETS FOR 9 I: CA340-500DAMAGEORA340-600FC 06 FUNCTIONAL CHECK OF THE BLOW OUT DOOR FOR CORRECT 9 I: 8000 FHA340-500TENSIONORA340-60078.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T500-78PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50079.00.00 OIL79.10.00 OIL STORAGENO TASK SELECTED79.20.00 OIL DISTRIBUTIONRS 01 REMOVE, INSPECT, CLEAN AND MARK PRESSURE OIL FILTER 6 I: 3000 FHA340-500ORNOTE: PRESSURE OIL FILTER LIFE SHALL NOT EXCEED 2A340-600CLEANINGSDS 02 DISCARD SCAVENGE OIL FILTER 6 I: 1600 FHA340-500ORA340-60079.30.00 OIL INDICATINGRS 01 CLEANING AND FUNCTIONAL CHECK OF THE MASTER EMCD 6 I: 2500 FHA340-500PRE 50676ORA340-600PRE 50676DI 02 DETAILED INSPECTION OF THE MASTER EMCD 6 I: 130 FHA340-500(THIS TASK COVERS TASKS 72.33.00/03-R5,POST 5067672.33.40/01-R5, 72.61.00/01-R5)ORA340-600POST 50676* * * * * E N D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-RR T500-79PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA340MRB REPORT – Systems and Powerplant SectionRR T50080.00.00 STARTING80.11.00 PNEUMATIC STARTER AND VALVE SYSTEMDI 01 DETAILED INSPECTION OF STARTER MCD 6,9 I: 800 FHA340-500OROR300 FCA340-600SV 02 STARTER OIL CHANGE 6,9 I: 800 FHA340-500OROR300 FCA340-600* * * * * E N D * * * * *ISSUE: JUL 01/10 STARTING SECTION: C-RR T500-80PAGE 1

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-1 SECTION D

STRUCTURES

1. INTRODUCTION

The purpose of this section is to maintain the continuous airworthiness of the aircraft structure

and to control corrosion to Level 1 or better (refer to: paragraph 6. CORROSION PREVENTION

AND CONTROL PROGRAM (CPCP) for definition of Level 1 corrosion).

2. INSPECTION PHILOSOPHY

This section has been developed by considering the following sources of damage:

(FD) Fatigue Damage

For FD, the damage initiation and subsequent damage growth is primarily dependant on the

ground-air-ground loading variation, which occurs once per flight. Therefore, flight cycles (FC)

are used as the unit for thresholds and repeat intervals. Some fatigue related SSI’s are also

sensitive to flight duration. For these SSI’s, a FH limit is stated in addition to the FC limit. The

inspection is to be performed at whichever limit is reached first.

The structure inspection tasks selected for fatigue are derived from damage tolerance evaluation

according to the criteria defined by FAR/JAR 25.571, Amendment 45. The FC and FH data is

based on a combination of calculation, full-scale fatigue test teardown results, and in-service

experience (where available).

(ED) Environmental Deterioration

Since deterioration caused by the environment (e.g corrosion, stress corrosion) is mainly

time dependant, the maintenance requirements are based on calendar time (Years).

(AD) Accidental Damage

AD consists of minor damage which could result in fatigue and/or corrosion damage, and which

could propagate undetected. In the analysis, the fatigue and environmental effects of the

accidental damage are considered. A dedicated AD task is not selected; the AD requirement is

consolidated into either the ED or the FD task, or both, according to the AD consequences. AD

is therefore subject to maintenance requirements expressed in FC (and FH) or calendar time or

both.

3. INSPECTION LEVELS

According to the analysis procedure, for each Structural Significant Item (SSI), various inspection

levels have been considered with the aim of selecting the lowest inspection level compatible with

the type of damage and the expected damage growth. Therefore, one or more of the following

inspection levels have been selected for each SSI:

General Visual Inspection (GVI)

Detailed Inspection (DI)

Special Detailed Inspection (SDI)

For definition of inspection levels refer to GLOSSARY, Appendix 6.

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-2 4. ZONAL SECTION COMPATIBILITY

When General Visual Inspection (GVI) level has been selected for a particular SSI, the

inspection requirement is considered adequately covered by the equivalent Zonal (ZIP) tasks

which are referenced in the ZIP column.

The maintenance programs of individual operators which deviate from the requirements given in

this report (e.g. interval frame, utilisation) will need to be rechecked to ensure Zonal

compatibility.

All structure not selected as Structural Significant Item (SSI) is classed as 'Other Structure'

(Refer to GLOSSARY, Appendix 6) and is covered by the requirements of the Zonal Inspection

Section.

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-3 5. SAMPLING PROGRAM

5.1 INTRODUCTION

The Sampling Program is designed to detect systematic deterioration caused by the environment

and/or fatigue, on a group of aircraft selected from those which have the highest age within a

considered fleet.

The Sampling Program is applicable to both Fatigue Damage (FD) and Environmental

Deterioration (ED) SSIs, where the deterioration, should it occur, is considered as being

progressive with age or operating usage. SSIs which are susceptible to Accidental Damage (AD)

are not considered for the Sampling Program.

Structure inspections fall into the following 3 categories:

100%

Fatigue tasks where calculation and/or test indicate a high fatigue sensitivity, are not

selected for sampling. These tasks have a 100% threshold only. e.g. SSI 534148-01-1

Fatigue or corrosion tasks where accidental damage is likely, are not selected for

sampling. These tasks have a 100% threshold only. e.g. SSI 533823-01-1

Corrosion tasks where in-service experience indicates that damage is likely are not

selected for sampling. These tasks have a 100% threshold only. e.g. SSI 533895-01-1

100% + SAMPLING

Fatigue tasks where calculation and/or test indicate a medium fatigue sensitivity, are

selected for sampling. These tasks have a sampling threshold and a 100% threshold. All

aircraft not inspected as sampling aircraft must be insepected at the 100% threshold.

e.g. 533104-01-2

Corrosion tasks where in-service experience indicates that damage is not likely are

selected for sampling. These tasks have a sampling threshold. All aircraft not inspected as

sampling aircraft must be inspected at the 100% threshold (20 years). e.g. 545130-01-1

SAMPLING

Fatigue tasks where calculation and/or test indicate a low fatigue sensitivity, are selected

for sampling. These tasks have a sampling threshold only. e.g. 574804-02-1

Based on the results of Sampling Program inspections:

- In case of findings, each operator should take appropriate corrective actions, such as

change of program concept to 100%, decrease of interval, application of TPS etc.....

- In case of no findings, the sampling inspections continue to apply. Refer to example on

page D-INTRO-7.

5.2 SELECTION OF AIRCRAFT FOR SAMPLING PROGRAM

For each operator, the Sampling Program inspections are to be performed on the oldest 1/5 of the

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-4 operator's A340 aircraft.

The oldest aircraft are defined as the aircraft with the highest age in years since their initial

manufacturer's delivery date.

For operators with more than one aircraft type in their fleet, e.g A330 and A340, the Sampling

Program aircraft must be determined per aircraft type, e.g. 1/5 of the oldest A330 aircraft + 1/5 of

the oldest A340 aircraft.

For operators with more than one weight variant group in their fleet, the Sampling Program

aircraft have to be determined pe r weight variant group, e.g 1/5 of the oldest Group 43A aircraft

and 1/5 of the oldest Group 43B aircraft.

If the 1/5 sample of the operators aircraft is not a whole number of aircraft, the number is to be

decreased to the next lowest whole number.

A minimum of one aircraft per operator must be selected for the Sampling Program The maximum

number of aircraft to be sampled per operator is 5 aircraft per aircraft type even if the total fleet

size would lead to a higher number applying the 20% rule.

NOTE: Operators operating the same aircraft type in similar operational conditions and having

established common rules acceptable to each operators' Airworthiness Authority may

combine their fleets to form one fleet for the Sampling Program.

A minimum of one aircraft must be selected from each operator in the group, if not already

selected by the above rule.

Any aircraft in a fleet is protected by the respective sample aircraft of this operator’s fleet. If a

“non-sampling” aircraft would be integrated into a new operator’s fleet it could become a

sampling aircraft. However, no retroactive maintenance is required i.e. all inspections are to be

performed at their next due.

Example: An aircraft which was not a sample a/c is 7 years old has been acquired by another

operator. All inspections with an interval of 6 YE would be due at the next 6 YE check; which is

12 YE after entering service.

Any significant changes to an operator's fleet will require a review of the Sampling Program

aircraft. This includes buying and/or selling aircraft and retiring aircraft from the fleet. Operators

may contact Airbus for advice in the selection of the Sampling Program aircraft.

5.3 ARRANGEMENT OF INSPECTIONS

For the selected A/C, the inspections commence at the Sample Threshold and continue at each

subsequent repeat interval.

The selected Sampling Program aircraft are to be inspected at the Sample Threshold.

The same aircraft are to be inspected at each subsequent repeat interval.

NOTE: The 100% Threshold is the threshold for all aircraft not selected for sampling.

Refer to example on page D-INTRO-7.

5.4 SAMPLING PROGRAM ILLUSTRATIONS

A set of illustrations showing the arrangement of Sampling Program inspections for some typical

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-5 SSIs are shown on the following pages. Due to space limitations, not all SSI sub tasks are shown.

The Sampling Program aircraft should first be selected before the subsequent planning of the SSI

details.A340 MRB REPORTIssue : July 2010Page : D-INTRO-6Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrS.T = 60000 FH= Aircraft InspectionI= 17700 FH10Yrs15Yrs20Yrs25YrsTASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY572011-01-1DI 13000 FCOR60000 FH4700 FCOR17700 FHGRP 42AORGRP 43A572011-01-2DI 13000 FCOR60000 FH3700 FCOR13900 FHGRP 42BORGRP 43B572011-01-3DI 13000 FCOR26000 FH4100 FCOR8200 FHGRP 43CExample 1 : SSI 57201143A1243A1143A1043A943A843A743A643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-7Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrS.T = 60000 FH= Aircraft InspectionI= 13900 FHI= 17700 FH10Yrs15Yrs20Yrs25YrsTASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY572011-01-1DI 13000 FCOR60000 FH4700 FCOR17700 FHGRP 42AORGRP 43A572011-01-2DI 13000 FCOR60000 FH3700 FCOR13900 FHGRP 42BORGRP 43B572011-01-3DI 13000 FCOR26000 FH4100 FCOR8200 FHGRP 43CExample 2 : SSI 57201143B1243B1143B1043B943B843B743B643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-8Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrS.T = 13000 FC= Aircraft Inspection100% T= 16600 FCI= 7100 FCI= 7100 FC10Yrs15Yrs20Yrs25YrsExample 3 : SSI 531144TASK REF LevelSAMPLETHRESHOLD100%THRESHOLDINTERVAL APPLICABILITY531144-01-1SDI 13000 FC 16600 FC 7100 FC A340-200ORA340-30043B1243B1143B1043B943B843B743B643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-9Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrI= 5000 FC= Aircraft InspectionI= 5000 FCI= 5000 FC10Yrs15Yrs20Yrs25YrsExample 4 : SSI 533135TASK REF LevelSAMPLETHRESHOLD100%THRESHOLDINTERVAL APPLICABILITY533135-01-1DI 10 YEOR13000 FC10 YE 10 YEOR5000 FCA340-200ORA340-30043B1243B1143B1043B943B843B743B643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-10Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrT= 13000 FC= Aircraft InspectionExample 5 : SSI 533154NOTE: A/C 1 to 4 are Pre mod 41652I= 8100 FC10Yrs15Yrs20Yrs25YrsTASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL APPLICABILITY533154-01-1 DI 13000 FC 8100 FC GRP 42APRE 41652ORGRP 43APRE 41652533154-01-2 DI 13000 FC 13000 FC GRP 42APOST 41652ORGRP 43APOST 41652ORGRP 42BORGRP 43B43A1243A1143A1043A943A843A743A643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-11I= 13000 FCTASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL APPLICABILITY533154-01-1 DI 13000 FC 8100 FC GRP 42APRE 41652ORGRP 43APRE 41652533154-01-2 DI 13000 FC 13000 FC GRP 42APOST 41652ORGRP 43APOST 41652ORGRP 42BORGRP 43BYrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 900 FC/Yr5000 FH/YrT= 13000 FC= Aircraft InspectionExample 6 : SSI 533154I= 8100 FC10Yrs15Yrs20Yrs25YrsNOTE: A/C 1 to 4 are Pre mod 4165243B1243B1143B1043B943B843B743A643A543A443A343A243A1GrpA/CA340 MRB REPORTIssue : July 2010Page : D-INTRO-12Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 700 FC/Yr5200 FH/YrT= 41500 FH= Aircraft InspectionI= 18700 FHExample 7: SSI 574109I= 20100 FHI= 20100 FHI= 18700 FHT= 40600 FHI= 20100 FHI= 20100 FH10Yrs15Yrs20Yrs25YrsTASK REF LevelSAMPLETHRESHOLD100%THRESHOLDINTERVAL EFFECTIVITY574109-01-1DI 10 YE20 YEOR9500 FCOR41500 FH10 YEOR4600 FCOR20100 FHGRP 42AORGRP 43A574109-01-2DI 10 YE20 YEOR9300 FCOR40600 FH10 YEOR4300 FCOR18700 FHGRP 42BORGRP 43B574109-01-3DI 10 YE20 YEOR11900 FCOR23800 FH10 YEOR4700 FCOR9400 FHGRP 43C43B1243B1143B1043B943B843B743B643A543A443A343A243A1GrpA/CI= 18700 FH I= 18700 FH

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-13 6. CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

6.1 INTRODUCTION

The Structures section includes requirements to control corrosion to Level 1 or better on all

structural details, elements or assemblies whose failure could affect the structural integrity

necessary for the safety of the aircraft.

All Corrosion Prevention and Control Program (CPCP) requirements are indicated by the code

'CPCP' in the “CPCP” column.

Some Calendar-time tasks are also covered by the Sampling Program, i.e. they have a Sample

Threshold/Interval. For these tasks, the 100% Threshold is the time at which the task becomes a

CPCP task.

6.2 CORROSION LEVEL DEFINITIONS

The severity of the corrosion damage is categorised into three 'Levels' as follows: -

Level 1 Corrosion

Corrosion damage that does not require structural reinforcement or replacement.

or

Corrosion occurring between successive inspections exceeds allowable limit but is local and

can be attributed to an event not typical of operator usage of other aircraft in the same fleet

(e.g. Mercury spill).

Level 2 Corrosion

Corrosion occurring between successive inspections that requires a single rework/blend-out

which exceeds allowable limits as defined by the manufacturer (SRM, SB, etc.), requiring a

repair/reinforcement or complete or partial replacement of applicable structure.

Level 3 Corrosion

Corrosion found during first or subsequent inspection(s), which is determined (normally by

the operator) to be an urgent airworthiness concern requiring expeditious action.

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-14 6.3 CPCP RULES

The effectiveness of the CPCP is determined by following the General Rules applicable to the

Structures section (refer to Paragraph 7) and by following the rules listed below:-

Level 1 Corrosion Findings

Should inspections consistently reveal corrosion Level 1 findings for a given area during repeat

inspections on particular aircraft operated in similar conditions, then the existing program is

considered effective for the concerned area, and no change to the program is necessary.

Level 2 Corrosion Findings

Should inspections reveal that corrosion is Level 2 for a given area during repeat inspections,

then the existing program is not effective for the concerned area of the particular fleet.

In order to control corrosion to Level 1 or better, consideration should be given to one or more of

the following corrective actions:-

- Decreasing the inspection threshold/interval

- Considering a higher inspection level

- Re-considering the Program Concept

- Application/More frequent application of Temporary Protection System

- Embodiment of preventive modifications, where applicable.

- Installation of parts with improved protection standard, where applicable.

In this way, the program is self-regulating and will adjust itself to the optimum program.

Level 3 Corrosion Findings

Should inspections reveal that corrosion is Level 3 in a given area, then the existing program is

not effective for the concerned area.

In addition to the considerations given for Level 2 corrosion, an action plan calling for a one-time

inspection of the concerned area should be expeditiously agreed with the local Aviation Authority

and carried out on all aircraft of a similar age or older.

Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all

details of findings are to be promptly reported for detailed evaluation and the assistance required

clearly expressed.

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-15 7. GENERAL RULES APPLICABLE TO THE STRUCTURES SECTION

1. The Maintenance tasks are to be carried out 'at or before' the limits stated for Sample

Threshold/Interval and 100% Threshold/Interval.

2. The Threshold is the time at which the maintenance requirement is first due.



# - For FC or FH tasks without mod applicability, the sample thresholds and 100%

thresholds are counted from first flight.



# - For FC or FH tasks with mod applicability, the sample thresholds and 100% thresholds

are counted from point of mod embodiment, unless otherwise stated.



# - For tasks in Years, the sample thresholds and 100% thresholds are counted from

date of initial delivery from manufacturer, unless otherwise stated.

3. For repeat maintenance tasks, the interval starts at the time of the last maintenance task

performed.

4. The thresholds and intervals quoted in calendar time in this section include aircraft time in and

out of service. In other words, operators will not, in general, be allowed to take credit for time

out of service or storage periods to extend corrosion inspection intervals.

5. It is assumed that the structure to be inspected is in a state of cleanliness which allows a

satisfactory inspection to be carried out at the required inspection level.

Where existing Temporary Protection System (TPS) permits unobscured assessment of the

condition of the structure, then that TPS may remain in place for the inspection.

6. If damage is found or suspected (such as bulging skin) then the full extent of any damage

must be clearly identified using appropriate inspection techniques and/or disassembly when

necessary. This may require additional access to that stated for the maintenance task.

All damage is to be evaluated and repaired in accordance with documentation acceptable to

the relevant Airworthiness Authority.

7. If inspections indicate evidence of deterioration, appropriate further actions must be taken to

prevent similar deterioration occurring in the operators fleet.

For corrosion findings refer to Corrosion Prevention and Control Program in this section.

8. The following applies to Temporary Protection System (TPS) application:

Prior to application of TPS, perform an inspection of the area at the inspection level for the

task quoted in calendar time.

Prior to re-fitting/re-connecting/re-installing parts removed to gain access to the inspection

area, TPS is to be applied to each SSI, as quoted in the TPS column of this Structures

section, at least as frequently as the calendar time thresholds and intervals of the respective

SSI. For SSI's where the FC or FH limit is reached before the calendar time limit,

consideration should be given to application of TPS at the FC or FH limit.

The Type of TPS to be applied is provided in the TPS column of the Structures section.

When TPS is only applied to a selected area within an SSI boundary, details are provided as

a note in the Description column.

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-16 Sampling Program tasks do not have TPS selected in the MRB Report Structure section. If an

operator chooses to apply TPS to a particular SSI for aircraft inspected in accordance with the

Sampling Program, these aircraft are no longer representative of the non-sampled aircraft. In

this case, TPS must be applied to all aircraft in this SSI area, including the aircraft not selected

for sampling. This task then effectively becomes 100% for those specific aircraft.

CAUTION: Do not apply TPS on oxygen systems, control cables, pulleys, teflon bearings

and lubricated surfaces.

Drain valves and all open orifices are to be protected from ingress prior to

temporary protection being applied.

9. The access column may contain one of the following instructions concerning insulation

blankets:

Insulation = Insulation to be removed from the inspection area.

Note 1 = Insulation to be displaced as required to complete the required maintenance task.

10. Ensure wet insulation blankets are dried prior to re-installation, or replaced with new.

11. Ensure that all drain holes and drainage paths are clear from obstruction.

12. The condition of the paint system should be verified during the inspections. Re-protection

should be applied where necessary.

13. The requirements stated in years were determined for an aircraft operated in a moderate

humidity environment and not subjected to corrosive products.

Any operators who routinely operate in humid or marine environments and/or carry corrosive

cargo such as seafood, may find that the calendar time maintenance tasks stated in this MRB

Report are not sufficient to control corrosion to Level 1 or better. Operators in this category

should take appropriate further actions.

14. Operators shall report inspection results related to SSI's to the manufacturer in accordance

with the Structures Inspection Reporting System. Refer to Appendix 8.

15. Based on reports made through the Structures Inspection Reporting System, Airbus will:

- Inform all the operators of the significant discrepancies discovered on the A340 fleet.

- Make the appropriate recommendations.

16. "Touch and Go" Cycles can be neglected if they are less than 5% of the total number of Flight

Cycles up to threshold inspection or between two consecutive inspections.

Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to threshold

inspection or between two consecutive inspections.

17. Additional information concerning SSI inspections is provided in the following Airbus

supporting publications:

- Maintenance Planning Document (MPD)

- Aircraft Maintenance Manual (AMM)

- Non-Destructive Testing Manual (NTM)

- Structural Repair Manual (SRM)

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-17 8. NOTES FOR SECTION D

NOTE 1: Insulation to be displaced as required to complete the required inspection.

NOTE 2: - deleted -

NOTE 3: - deleted -

NOTE 4: - deleted -

NOTE 5: - deleted

NOTE 6: - not used -

NOTE 7: Minimum major improvements for cabin floor structure

NOTE 8: The threshold is to be counted from 1st flight.

9. WEIGHT VARIANT APPLICABILITY

The A340 aircraft have different fatigue inspection requirements for the various Weight Variants

(WV) of each aircraft. The Weight variant represents the delivery standard of each aircraft.

The applicable Weight Variant for each individual aircraft can be found in Table 1 of the “Aircraft

Allocation List” in the Structure Repair Manual (SRM) Intro.

Table 2 of the SRM “Aircraft Allocation List” gives additional data for aircraft which have the Weight

Variant status amended due to modifications or Service Bulletin embodiment. Item No. Improvements Document

1 Wet areas well defined AMM 25-28-00

2 Temporary Protection System enlarged SIL 53-078

3 Floor panel – two sealants & “Skyflex” tape A MM 53-00-00

CML 08-109

4 Cosmoline on seat track crown A MM 51-75-13

CML 15-010

5 Mylar foil – Stronger fil CML 08-104

6 Mylar foil – under lavatory AMM 25-28-43

7 Mylar foil – Extended & overlap. dry areas AMM 25-28-43

8 Primer prior silicone on PVC AMM 25-28-42

9 Stronger sealant “Floorsil 2” CML 09-054

10 Joint welded for PVC NTF products A MM 25-28-42

CML 05-128

11 Lavatory floor pan reinforced SB 25-4186

12 Seals at Cabin Attendant Seat /NTF SB 25-4261

SB 25-5092

# A340 MRB REPORT

Issue : July 2010 Page : D-INTRO-18 To minimise the number of individual inspection requirements, the Weight Variant requirements

have been grouped where they are similar. The group number is stated in the Structure section

“APPLICABILITY ” column. Refer to the details below:

WV GROUPS A/C Series Weight Variants

GROUP 42A A340-200 000, 001, 002

GROUP 42B A340-200 021

GROUP 43A A340-300 000, 001, 002, 003, 004

GROUP 43B A340-300 020, 021, 023, 024, 025,

026, 028, 029, 030

GROUP 43C A340-300 027

GROUP 43E A340-300 050, 051, 052, 053, 054

GROUP 45A A340-500 000, 001, 002, 003, 004

GROUP 45B A340-500 101, 102 , 103

GROUP 46A A340-600 000, 001

GROUP 46B A340-600 101, 102, 103

NOTE: The Fatigue figures for WV 027 are based on an average flight time of 2.0 FH/FC. The operator

must contact Airbus if this figure exceeds 2.5 FH/FC.

INTERPRETATION

GROUP X Y

Z

X : Aircraft Type 4 for A3 4 0

Y : Model ( 2 for – 2 00 / 3 for – 3 00)

Z : Various Weight Variants corresponding to a specific certified Type/Model

EXAMPLES

GROUP 42A : A3 4 0- 2 00 WV 000, 001, 002

(1 st 

# WV Group of A340-200 Series)

GROUP 43B : A3 4 0- 3 00 WV 020, 021, 023, 024, 025, 026, 028, 029, 030

(2 nd 

# WV group of A340-300 Series)A340MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-1910. EXPLANATION OF STRUCTURES SECTION FORMATDetailed information is given below concerning the format of the inspection requirements provided on subsequent pages.TASKREFERENCEACCESSZONETASKDESCRIPTIONSAMPLETHRESHOLDINTERVAL100%THRESHOLDINTERVALTPSCPCPZIPREFERENCEAPPLICABILITY1 2 3 4 5 6 7 8 9 101. This column indicates the SSI task number, e.g. 531109-01-01. It is composed of 10 digits as follows:XXXXXX – XX – XXThe SSI number is represented by the six first digits, 531109.The first set of two digits are in accordance with the A340 ATA100breakdown, showing the major section where the SSI is located e.g 53 Fuselage. The second set of two digitsare also in accordance with the A340 ATA 100breakdown, showing the sub section where the SSI is located e.g 53-11 Fwd fuselage. The third set of two digitsare sequential numbers within the section e.g 01,02, 03 up to 99.The Sequential Number is composed of two digits. It follows the SSI number and is separated by a dash e.g. 531109-01. It identifies different inspectionse.g.Detailed or Special Detailed. These two digits are also changed when the inspection areas are physically different (e.g. rib 8 or rib 9) or when the inspectionshave a major difference in access (e.g. actuator removal).The Applicability Index is composed of two digits. It follows the Sequential Number and is separated by a dash, 531109-01-01. It identifies different applicabilitye.g aircraft series, mod status, WV group etc ...The digits are also used to differentiate between minor access differences e.g.different access panel numbers.2. This column indicates the access requirement to adequately perform the required maintenance task, i.e. all items listed must be removed or opened (E.g hingedApplicability indexSequence numberSSI numberA340MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-20panels or doors) unless otherwise stated (e.g. to be lifted).3. This column indicates the zone(s) where the SSI is located. For the zone boundaries refer to Zone Diagrams, APPENDIX 2.4. This column describes the task to be performed, additional information may be added to clarify the inspection area. Detailsof partial application of TPS areprovided, where applicable. The SSI description states the boundaries of the inspection area. All items within this boundary are to be inspected e.g. fasteners,cutouts, attachments, unless otherwise stated.5 This column indicates the Sample Threshold and the repeat Interval. This requirement is only applicable to selected sample A/C.6. This column indicates the 100% Threshold and the repeat interval. This requirement is applicable to all A/C not selected for the Sampling Program.7.This column indicates if a Temporary Protection System (TPS) is to be applied, as indicated below:‘ ‘ : A blank indicates that application of TPS is at the discretion of the operator.‘1’ : Type 1 Grade 2 or Grade 3 TPS is to be applied.‘1+2’ : Type 1 TPS plus a subsequent application of Type 2 TPS is to be applied.‘2’ : Type 2 TPS is to be applied.‘3’ : Type 3 TPS is to be applied.'No' : TPS must not be applied in the area (example: inside fuel tank, pylon).Note: If “1+2” is stated in the TPS column, it is at the discretion of the operator to apply either “Type 1 TPS plus Type 2 TPS”or“Type 3 TPS”If “3” is stated in the TPS column, it is at the discretion of the operator to apply either “Type 3 TPS”or“Type 1 TPS plus Type 2 TPS”The technical specification for corrosion preventive temporary protective compounds can be found in the Process and Material Specifications Manual (PMS),Volume 5 , Section 02-16-00.8. This column indicates whether the considered task is a CPCP requirement.9. This column indicates the equivalent zonal tasks which cover the SSI task requirements.10. This column indicates the A/C model/mod status/engine type to which this requirement is applicable. Some examples are givenbelow:A340MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-21Applicability Task applicable toALL All A340 aircraft.A340-xxx -xxx series aircraft.PRE nnnnn All A340 PRE MOD nnnnn.i.e. A340 that do nothave MOD nnnnn embodied.POST nnnnnAll A340 POST MOD nnnnn.i.e. A340 that dohave MOD nnnnn embodied.POST nnnnn Sxxxxx All A340 POST MOD nnnnn (at least with mod proposal no. Sxxxxx embodied).POST nnnnnPOST mmmmmAll A340 POST MOD nnnnn and POST MOD mmmmm.i.e. A340 that dohave MOD nnnnn andMOD mmmmm embodied.A340-200ORA340-300PRE nnnnnAll A340-200,Or,All A340-300 that do nothave MOD nnnnn embodied.A340-200POST nnnnnORPOST mmmmAll A340-200 that dohave MOD nnnnn embodied,Or,All A340-200 that dohave MOD mmmm embodied.A340-200POST nnnnnORA340-300POST nnnnnPRE mmmmmAll A340-200 that dohave MOD nnnnn embodied,Or,All A340-300 that dohave MOD nnnnn embodied anddo nothave MOD mmmmm embodied.POST nnnnn(xx-yyyy)All A340 that dohave MOD nnnnn embodied.(xx-yyyy) is the Service Bulletin reference associated to the modification.CFM56 All A340 equipped with CFM56 engines.Door Type 1 Door Type 1 = 1.60 m High, 0.61 m Wide - Emergency exit type door.Door Type A Door Type A = 1.93 M High, 1.07 m Wide - Pax type door.A340MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-22Applicability Task applicable toGROUP XYZ All aircraft with weight variant group XYZGROUP XYZPRE nnnnAll aircraft with weight variant group XYZ that do nothave MOD nnnn embodiedGROUP XYZPOST nnnnAll aircraft with weight variant group XYZ that dohave MOD nnnn embodiedAPPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS282801-01-1 821 822 131 DETAILED INSPECTION OF ADDITIONAL CENTER T: 6 YE CPCP ACTACT 132 TANK EXTERNAL STRUCTURE I: 6 YE151 NOTE: INTERVAL AND THRESHOLD CORRESPOND TO THE ACT152 (T: 6 ACT YE AND I:6 ACT YE)282803-01-1 821 822 131 DETAILED INSPECTION OF ADDITIONAL CENTER TANK T: 12 YE CPCP ACTACT 132 INTERNAL STRUCTURE. I: 12 YEBLADDER TANK 151 NOTE: THRESHOLD AND INTERVAL CORRESPOND TO THE ACT152 (T:12 ACT YE AND I:12 ACT YE)* * * * * E N D * * * * *ISSUE: JUL 01/10 FUEL SECTION: D-28PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321101-01-1 N/A 731 DETAILED INSPECTION OF MLG MAIN FITTING. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321102-01-1 MLG FULLY EXTENDED 731 DETAILED INSPECTION OF MLG SLIDING PISTON. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321103-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG UPPER PISTON. T: 10 YE CPCP A340-200741 I: 10 YEORA340-300321104-01-1 N/A 731 DETAILED INSPECTION OF MLG BOGIE BEAM. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321105-01-1 MLG PITCH TRIMMER 731 DETAILED INSPECTION OF MLG PITCH TRIMMER T: 6 YE CPCP A340-200EXTENDED 741 I: 6 YEORA340-300321106-01-1 N/A 731 DETAILED INSPECTION OF MLG SIDESTAY ASSEMBLY. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321107-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCK STAY ASSEMBLY. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321108-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG AXLES. T: 10 YE CPCP A340-200741 I: 10 YEORA340-300321109-01-1 N/A 731 DETAILED INSPECTION OF MLG TORQUE LINK, LOWER AND T: 6 YE CPCP A340-200741 UPPER. I: 6 YEORA340-300ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321110-01-1 N/A 731 DETAILED INSPECTION OF MLG ARTICULATING LINK, LOWER T: 6 YE CPCP A340-200741 AND UPPER. I: 6 YEORA340-300321114-01-1 PINS 731 DETAILED INSPECTION OF BOGIE PIVOT PIN, SIDESTAY T: 10 YE CPCP A340-200741 ASSY PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY I: 10 YEORATTACH PINS, ARTICULATING LINKAGE PINS, PITCHA340-300TRIMMER ATTACH PINS, FORWARD PINTLE PINS ANDSHORTENING LINKAGE PINS.321124-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCKSTAY ACTUATOR. T: 6 YE CPCP A340-200741 I: 6 YEORA340-300321125-01-1 MLG FULLY LOWERED 570 DETAILED INSPECTION OF MLG PINTLE PINS AT OUTER T: 10 YE CPCP A340-200670 WING TRAILING EDGE I: 10 YEORA340-300321126-01-1 PIN 570 DETAILED INSPECTION OF MLG SHORTENING T: 10 YE CPCP A340-200670 MECHANISM AT OUTER WING TRAILING I: 10 YEOREDGE EARTHING PINA340-300321127-01-1 PIN 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE CPCP A340-200670 OUTER WING TRAILING EDGE I: 10 YEORA340-300321151-01-1 N/A 731 DETAILED INSPECTION OF MLG MAIN FITTING. T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321152-01-1 MLG FULLY EXTENDED 731 DETAILED INSPECTION OF MLG SLIDING PISTON. T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321153-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG UPPER PISTON. T: 10 YE CPCP A340-500741 I: 10 YEORA340-600ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321154-01-1 N/A 731 DETAILED INSPECTION OF MLG BOGIE BEAM. T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321155-01-1 MLG PISTON ROD 731 DETAILED INSPECTION OF MLG PITCH TRIMMER. T: 6 YE CPCP A340-500EXTENDED 741 I: 6 YEORA340-600321156-01-1 N/A 731 DETAILED INSPECTION OF MLG SIDESTAY ASSEMBLY. T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321157-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCK PINS ASSEMBLY. T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321158-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG AXLES. T: 10 YE CPCP A340-500741 I: 10 YEORA340-600321159-01-1 N/A 731 DETAILED INSPECTION OF MLG TORQUE LINK, LOWER AND T: 6 YE CPCP A340-500741 UPPER. I: 6 YEORA340-600321160-01-1 N/A 731 DETAILED INSPECTION OF MLG ARTICULATING LINK, LOWER T: 6 YE CPCP A340-500741 AND UPPER. I: 6 YEORA340-600321161-01-1 SHOCK ABSORBER 731 DETAILED INSPECTION OF MLG SHORTENING LINK ASSEMBLY, T: 10 YE CPCP A340-500741 UPPER AND LOWER LINK I: 10 YEORA340-600321164-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF BOGIE PIVOT PIN, SIDESTAY T: 10 YE CPCP A340-500741 ASSY PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY I: 10 YEORATTACH PINS, ARTICULATING LINKAGE PINS, PITCHA340-600TRIMMER ATTACH PINS, FORWARD PINTLE PINS ANDSHORTENING LINKAGE PINS.ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321174-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCKSTAY ACTUATOR T: 6 YE CPCP A340-500741 I: 6 YEORA340-600321175-01-1 MLG 570 DETAILED INSPECTION OF MLG PINTLE PINS AT OUTER T: 10 YE CPCP A340-500670 WING TRAILING EDGE. I: 10 YEORA340-600321176-01-1 PIN 570 DETAILED INSPECTION OF MLG SHORTENING T: 10 YE CPCP A340-500670 MECHANISM AT OUTER WING TRAILING I: 10 YEOREDGE EARTHING PINA340-600321177-01-1 PIN 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE CPCP A340-500670 OUTER WING TRAILING EDGE. I: 10 YEORA340-600321505-01-1 N/A 751 DETAILED INSPECTION OF CLG MAIN FITTING (CYLINDER). T: 6 YE CPCP A340-200I: 6 YEORA340-300321506-01-1 AXLE SLEEVES 751 DETAILED INSPECTION OF CLG SLIDING MEMBER (PISTON). T: 6 YE CPCP A340-200PISTON EXTENDED I: 6 YEORWHEELSA340-300321507-01-1 753 754 755 751 DETAILED INSPECTION OF CLG DRAG STAY ASSEMBLY. T: 6 YE CPCP A340-200756 I: 6 YEORA340-300321508-01-1 753 754 755 751 DETAILED INSPECTION OF CLG LOWER STABILIZER LINK. T: 6 YE CPCP A340-200756 I: 6 YEORA340-300321509-01-1 753 754 755 751 DETAILED INSPECTION OF CLG UPPER STABILIZER LINK. T: 6 YE CPCP A340-200756 I: 6 YEORA340-300ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321510-01-1 753 754 755 751 DETAILED INSPECTION OF CLG FORWARD AND AFT LOCK T: 6 YE CPCP A340-200756 LINKS. I: 6 YEORA340-300321511-01-1 PINS 751 DETAILED INSPECTION OF CLG ATTACHMENT PINS. T: 10 YE CPCP A340-200I: 10 YEORA340-300321512-01-1 AXLE SLEEVES 751 DETAILED INSPECTION OF TORQUE LINKS. T: 6 YE CPCP A340-200PISTON EXTENDED I: 6 YEORWHEELSA340-300321551-01-1 CLG DOORS OPEN 751 DETAILED INSPECTION OF CLG MAIN FITTING. T: 6 YE CPCP A340-500I: 6 YEORA340-600321552-01-1 CLG DOORS OPEN 751 DETAILED INSPECTION OF CLG SLIDING MEMBER. T: 6 YE CPCP A340-500SLIDING MEMBER FULLY I: 6 YEOREXTENDEDA340-600321553-01-1 N/A 751 DETAILED INSPECTION OF CLG TORQUE LINKS T: 6 YE CPCP A340-500I: 6 YEORA340-600321554-01-1 WHEEL WELL DOORS 751 DETAILED INSPECTION OF CLG DRAG STAY ASSEMBLY T: 6 YE CPCP A340-500(UPPER AND LOWER) INCLUDING LOCKLINK. I: 6 YEORA340-600321557-01-1 PINS 751 DETAILED INSPECTION OF CLG PINS T: 10 YE CPCP A340-500- MAIN FITTING PINTLE PINS (LH & RH) I: 10 YEOR- TORQUE LINK PINS (UPPER & LOWER)A340-600- TRIANGULATION ARM PINS (UPPER, APEX, LOWER)- BOGIE PIVOT PIN- BRAKE ROD PIN- DRAG STAY PINS (UPPER PINTLE & APEX)- LOCK LINK PINS (UPPER & APEX)ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS321558-01-1 N/A 751 DETAILED INSPECTION OF CLG BOGIE BEAM, T: 6 YE CPCP A340-500BRAKE RODS AND AXLES I: 6 YEORA340-600321559-01-1 WHEEL WELL DOORS 751 DETAILED INSPECTION OF CLG TRIANGULATION ARMS. T: 6 YE CPCP A340-500I: 6 YEORA340-600322101-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING (BARREL). T: 6 YE CPCP A340-200I: 6 YEORA340-300322102-01-1 SLEEVES 711 DETAILED INSPECTION OF NLG SLIDING MEMBER. T: 6 YE CPCP A340-200SLIDING MEMBER FULLY I: 6 YEOREXTENDEDA340-300WHEELS322103-01-1 N/A 711 DETAILED INSPECTION OF NLG TORQUE LINKS. T: 6 YE CPCP A340-200I: 6 YEORA340-300322104-01-1 713 714 715 711 DETAILED INSPECTION OF NLG DRAGSTAY UPPER ARM. T: 6 YE CPCP A340-200716 I: 6 YEORA340-300322105-01-1 N/A 711 DETAILED INSPECTION OF NLG DRAGSTAY LOWER ARM. T: 6 YE CPCP A340-200I: 6 YEORA340-300322106-01-1 N/A 711 DETAILED INSPECTION OF NLG DOWNLOCK LINK. T: 6 YE CPCP A340-200I: 6 YEORA340-300ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS322107-01-1 PIN 711 DETAILED INSPECTION OF NLG PINS: T: 10 YE CPCP A340-200- MAIN FITTING (BARREL) HINGE PINS (LH AND RH). I: 10 YEOR- TORQUE LINKS HINGE PINS (UPPER, MIDDLE AND LOWER)A340-300- DRAGSTAY HINGE PINS (UPPER, MIDDLE AND LOWER)- DOWNLOCK HINGE PINS (UPPER, MIDDLE AND LOWER)322110-01-1 713 714 715 123 DETAILED INSPECTION OF NLG DRAG STRUT PINTLE PIN. T: 10 YE 1 CPCP A340-200716 I: 5 YEORDRAG STRUTA340-300DISCONNECTEDPINTLE PIN322151-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING. T: 6 YE CPCP A340-500I: 6 YEORA340-600322152-01-1 SLEEVES 711 DETAILED INSPECTION OF NLG SLIDING MEMBER, T: 6 YE CPCP A340-500SLIDING MEMBER FULLY INCLUDING INTEGRAL AXLE. I: 6 YEOREXTENDEDA340-600WHEELS322153-01-1 N/A 711 DETAILED INSPECTION OF NLG TORQUE LINKS. T: 6 YE CPCP A340-500I: 6 YEORA340-600322154-01-1 WHEEL WELL DOORS 711 DETAILED INSPECTION OF NLG DRAG STAY T: 6 YE CPCP A340-500ASSEMBLY (UPPER AND LOWER) INCLUDING I: 6 YEORLOCKLINK.A340-600322157-01-1 PINS 711 DETAILED INSPECTION OF NLG PINS T: 10 YE CPCP A340-500- MAIN FITTING PINTLE PINS (LH & RH) I: 10 YEOR- TORQUE LINK PINS (UPPER, APEX & LOWER)A340-600- DRAG STAY PINS (UPPER PINTLE & APEX)- DOWNLOCK HINGE PINS (UPPER MIDDLE LOWER)* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS521101-01-1 N/A TASK DELETED521103-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 T: 6 YE CPCP ZL-800-01-1 A340-200(FWD PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE. I: 6 YEORA340-300521103-01-2 N/A TASK DELETED521104-01-1 ESCAPE SLIDE 831 DETAILED INSPECTION OF DOOR 1 (FORWARD T: 6 YE 1 CPCP A340-200INSULATION 841 PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YEORLININGA340-300521123-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 T: 6 YE CPCP ZL-800-01-2 A340-500(FORWARD PASSENGER/CREW DOOR) SKIN, I: 6 YEZL-800-01-3 OREXTERNAL SURFACEA340-600521123-01-2 N/A TASK DELETED521124-01-1 ESCAPE SLIDE 831 DETAILED INSPECTION OF DOOR 1 (FORWARD T: 6 YE 1 CPCP A340-500INSULATION 841 PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YEORLININGA340-600521201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 T: 6 YE CPCP ZL-800-01-1 A340-200(MID PASSENGER/CREW DOOR) SKIN, I: 6 YEOREXTERNAL SURFACE.A340-300521201-01-2 N/A TASK DELETEDISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS521202-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 T: 6 YE 1 CPCP A340-200ESCAPE SLIDE 842 (MID PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-300LINING521203-01-1 N/A TASK DELETED521203-01-2 N/A TASK DELETED521221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 T: 6 YE CPCP ZL-800-01-2 A340-500(MID PASSENGER/CREW DOOR) SKIN, I: 6 YEZL-800-01-3 OREXTERNAL SURFACEA340-600521221-01-2 N/A TASK DELETED521222-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 T: 6 YE 1 CPCP A340-500ESCAPE SLIDE 842 (MID PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-600LINING521301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 T: 6 YE CPCP ZL-800-01-1 A340-200(AFT PASSENGER/CREW DOOR) SKIN, I: 6 YEOREXTERNAL SURFACEA340-300521301-01-2 N/A TASK DELETEDISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS521302-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 T: 6 YE 1 CPCP A340-200ESCAPE SLIDE 843 (AFT PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-300LINING521303-01-1 N/A TASK DELETED521303-01-2 N/A TASK DELETED521321-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 T: 6 YE CPCP ZL-800-01-2 A340-500(AFT PASSENGER/CREW DOOR) SKIN, I: 6 YEZL-800-01-3 OREXTERNAL SURFACEA340-600521321-01-2 N/A TASK DELETED521322-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 T: 6 YE 1 CPCP A340-500ESCAPE SLIDE 843 (AFT PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-600LINING522121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF OVERWING EMERGENCY EXIT T: 12 YE CPCP ZL-800-01-3 A340-600DOOR SKIN, EXTERNAL SURFACE I: 12 YEPOST 47050522122-01-1 836 846 836 DETAILED INSPECTION OF OVERWING EMERGENCY EXIT DOOR, T: 6 YE 1 CPCP A340-600INSULATION 846 INTERNAL STRUCTURE. I: 6 YEPOST 47050LINING522201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE CPCP ZL-800-01-1 A340-200(EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 6 YEOREXTERNAL SURFACE.A340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS522201-01-2 N/A TASK DELETED522202-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1 CPCP A340-200ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-300LINING522203-01-1 N/A TASK DELETED522203-01-2 N/A TASK DELETED522221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE CPCP ZL-800-01-3 A340-600(EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 6 YEEXTERNAL SURFACE522221-01-2 N/A TASK DELETED522221-01-3 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 12 YE CPCP ZL-800-01-2 A340-500(EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 12 YEEXTERNAL SURFACE522222-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1 CPCP A340-500ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), I: 6 YEORINSULATION INTERNAL STRUCTUREA340-600LINING523101-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE CPCP ZL-800-01-1 A340-200COMPARTMENT DOOR SKIN, EXTERNAL SURFACE. I: 6 YEORA340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 523101-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FCZL-821-01-1 A340-200COMPARTMENT DOOR SKIN, EXTERNAL SURFACE. I: 3000 FCORA340-300523102-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO T: 12 YE 1 CPCP A340-200821CR 821DR COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YEORLININGA340-300523103-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF T: 12000 FCA340-200FORWARD CARGO COMPARTMENT DOOR (10 PLACES). I: 9000 FCORA340-300523104-01-1 132AR 132BR 132CR 132 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR T: 12 YE 1 CPCP A340-200132DR 132ER 132FR 821 HINGE ASSEMBLIES AT FR 20B TO FR25 (10 PLACES). I: 12 YEOR132GR 132HR 132JRA340-300132KR 132LR523105-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FCA340-200FITTING OF FORWARD CARGO COMPARTMENT DOOR AT I: 8300 FCORFR 22A.A340-300523106-01-1 N/A TASK DELETED523121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE CPCP ZL-800-01-2 A340-500COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YEZL-800-01-3 ORA340-600N 523121-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FCZL-821-01-2 A340-500COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 3000 FCORA340-600523122-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO T: 12 YE 1 CPCP A340-500LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YEORA340-600ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS523123-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF FWD CARGO T: 12000 FCA340-500COMPARTMENT DOOR (10 PLACES) I: 9000 FCORA340-600523124-01-1 132AR 132BR 132CR 132 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT T: 12 YE 1 CPCP A340-500132DR 132ER 132FR 821 DOOR HINGE ASSEMBLIES AT FR 20B TO FR 25 (10 PLACES). I: 12 YEOR132GR 132HR 132JRA340-600132KR 132LR523125-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FCA340-500FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A I: 8300 FCORA340-600523201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO T: 6 YE CPCP ZL-800-01-1 A340-200COMPARTMENTS DOOR SKIN, EXTERNAL SURFACE. I: 6 YEORA340-300R 523201-01-2 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO T: 3000 FCZL-822-01-1 A340-200COMPARTMENTS DOOR SKIN, EXTERNAL SURFACE. I: 3000 FCORA340-300523202-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1 CPCP A340-200822CR 822DR DOOR, INTERNAL STRUCTURE. I: 6 YEORLININGA340-300523203-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF LATCHING HOOKS OF AFT T: 12000 FCA340-200CARGO COMPARTMENT DOOR (10 PLACES). I: 9000 FCORA340-300523204-01-1 152AR 152BR 152CR 152 DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR T: 12 YE 1 CPCP A340-200152DR 152ER 152FR 822 HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES). I: 12 YEOR152GR 152HR 152JRA340-300152KR 152LR523205-01-1 822 822 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FCA340-200FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A. I: 8300 FCORA340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS523221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF T: 6 YE CPCP ZL-800-01-2 A340-500AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL I: 6 YEZL-800-01-3 ORSURFACEA340-600N 523221-01-2 N/A 800 GENERAL VISUAL INSPECTION OF T: 3000 FCZL-822-01-2 A340-500AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL I: 3000 FCORSURFACEA340-600523222-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1 CPCP A340-500LINING DOOR, INTERNAL STRUCTURE. I: 6 YEORA340-600523223-01-1 822 822AR 822BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF AFT CARGO T: 12000 FCA340-500COMPARTMENT DOOR (10 PLACES). I: 9000 FCORA340-600523224-01-1 152AR 152BR 152CR 152 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1 CPCP A340-500152DR 152ER 152FR 822 DOOR HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES) I: 12 YEOR152GR 152HR 152JRA340-600152KR 152LR523225-01-1 N/A TASK DELETEDR 523301-01-1 N/A 823 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 550 FCZL-823-01-1 A340-200DOOR SKIN, EXTERNAL SURFACE. I: 550 FCORA340-300523301-01-2 N/A 823 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE CPCP ZL-800-01-1 A340-200DOOR SKIN, EXTERNAL SURFACE. I: 6 YEORA340-300523302-01-1 823 823 DETAILED INSPECTION OF BULK CARGO T: 12 YE 1 CPCP A340-200LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YEORA340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS523303-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK T: 12 YE 1 CPCP A340-200CARGO COMPARTMENT DOOR. I: 12 YEORA340-300523321-01-1 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO T: 6 YE CPCP ZL-800-01-2 A340-500COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YEZL-800-01-3 PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288N 523321-01-2 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO T: 550 FCZL-823-01-2 A340-500COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 550 FCPRE 49205PRE 49288ORA340-600PRE 49205PRE 49288523322-01-1 823 823 DETAILED INSPECTION OF BULK CARGO T: 12 YE 1 CPCP A340-500LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YEPRE 49205PRE 49288ORA340-600PRE 49205PRE 49288523323-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK T: 12 YE 1 CPCP A340-500CARGO COMPARTMENT DOOR. I: 12 YEPRE 49205PRE 49288ORA340-600PRE 49205PRE 49288524101-01-1 N/A TASK DELETEDISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 8APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS524101-02-2 N/A 800 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT T: 6 YE CPCP ZL-811-01-1 A340-200LOWER ACCESS DOOR SKIN, EXTERNAL SURFACE. I: 6 YEORA340-300524102-01-1 811 121 DETAILED INSPECTION OF AVIONICS COMPARTMENT T: 6 YE 1+2 CPCP A340-200DOOR FLOOR PANEL 122 LOWER ACCESS DOOR INTERNAL STRUCTURE, INCLUDING I: 6 YEOR811 DOOR STOPS AND HINGE FITTINGS ON FUSELAGE.A340-300524103-01-1 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 14300 FCGROUP 42ADOOR FLOOR PANEL 122 STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR I: 14300 FCOR811 CROSS MEMBERS.GROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C524121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT T: 6 YE CPCP ZL-800-01-2 A340-500ACCESS DOOR SKIN, EXTERNAL SURFACE. I: 6 YEZL-800-01-3 ORA340-600524121-02-1 N/A TASK DELETED524122-01-1 811 121 DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER T: 6 YE 1+2 CPCP A340-500122 ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS I: 6 YEOR811 AND HINGE FITTINGS ON FUSELAGE.A340-600524201-01-1 195HB 195 GENERAL VISUAL INSPECTION OF ACCESS DOOR TO BLUE T: 3 YEA340-500HYDRAULIC BAY, INTERNAL AND EXTERNAL SKINS I: 3 YEORA340-600524202-01-1 195HB 195 DETAILED INSPECTION OF HINGES OF ACCESS DOOR TO BLUE T: 6 YE 1 CPCP A340-500HYDRAULIC BAY. I: 6 YEORA340-600ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 9APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS524203-01-1 196PB 196 GENERAL VISUAL INSPECTION OF ACCESS DOOR TO YELLOW T: 3 YEA340-500HYDRAULIC BAY, INTERNAL AND EXTERNAL SKINS I: 3 YEORA340-600524204-01-1 196PB 196 DETAILED INSPECTION OF HINGES OF ACCESS DOOR TO T: 6 YE 1 CPCP A340-500YELLOW HYDRAULIC BAY. I: 6 YEORA340-600528101-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, T: 3 YEZL-734-01-1 A340-200744 MAIN DOOR, EXTERNAL SKIN, LH/RH I: 3 YEORA340-300528102-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, T: 3 YEZL-734-01-1 A340-200744 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YEORA340-300528103-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 12 YE 1 CPCP A340-200744 MAIN DOOR, FORWARD AND AFT FITTINGS, LH/RH. I: 12 YEORA340-300528104-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 6 YE 1 CPCP GROUP 43A744 MAIN DOOR, CENTER FITTING AND SURROUNDING AREA (300 I: 6 YEPRE 41535MM AROUND), LH/RH.ORNOTE: TPS APPLICATION REQUIRED ON FITTING ONLYGROUP 42APRE 41535528104-01-2 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 6 YE 1 CPCP GROUP 42A744 MAIN DOOR CENTER FITTING AND SURROUNDING AREA (300 I: 6 YEPOST 41535MM AROUND), LH/RH.ORNOTE: TPS APPLICATION REQUIRED ON FITTING ONLYGROUP 42BORGROUP 43APOST 41535ORGROUP 43BORGROUP 43CORGROUP 43EISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 10APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS528121-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR DOOR, T: 3 YEZL-734-01-2 A340-500744 EXTERNAL SKIN, LH/RH. I: 3 YEORA340-600528122-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR DOOR, T: 3 YEZL-734-01-2 A340-500744 INTERNAL SKIN, LH/RH. I: 3 YEORA340-600528123-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, T: 6 YE 1 CPCP A340-500744 FWD AND AFT HINGES, INCLUDING FITTINGS ON KEELBEAM, I: 6 YEORLH/RH.A340-600528124-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOOR, AREA T: 3 YEA340-500744 AROUND CENTER FITTING (300 MM AROUND) , LH/RH. I: 3 YEORA340-600528125-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, T: 6 YE 1 CPCP A340-500744 CENTER HINGE, INCLUDING FITTINGS ON KEELBEAM, I: 6 YEORLH/RH.A340-600528126-01-1 N/A TASK DELETED528201-01-1 N/A 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-1 A340-200714 FORWARD DOOR, EXTERNAL SKIN, LH/RH. I: 3 YEORA340-300528202-01-1 713 714 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-1 A340-200714 FORWARD DOOR, INTERNAL SKIN, LH/RH I: 3 YEORA340-300528203-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR T: 6 YE 1 CPCP A340-200714 FORWARD DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDING I: 6 YEORFITTINGS ON FUSELAGE, LH/RHA340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 11APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS528204-01-1 715 716 715 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-715-01-1 A340-200716 AFT DOOR, EXTERNAL AND INTERNAL I: 3 YEORSKINS, LH/RH.A340-300528221-01-1 N/A 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-2 A340-500714 FORWARD DOOR, EXTERNAL SKIN, LH/RH. I: 3 YEORA340-600528222-01-1 713 714 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-2 A340-500714 FORWARD DOOR, INTERNAL SKIN, LH/RH. I: 3 YEORA340-600528223-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1 CPCP A340-500714 DOORS, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS I: 6 YEORON FUSELAGE, LH/RH.A340-600528224-01-1 715 716 700 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-715-01-2 A340-500715 AFT DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH. I: 3 YEOR716A340-600528225-01-1 715 716 715 DETAILED INSPECTION OF NOSE LANDING GEAR, AFT DOOR, T: 6 YE 1 CPCP A340-500716 HINGES (NO4, NO5) INCLUDING FITTINGS ON FUSELAGE, I: 6 YEORLH/RH.A340-600528301-01-1 N/A 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-753-01-1 A340-200754 MAIN DOOR, EXTERNAL SKIN, LH/RH. I: 3 YEORA340-300528302-01-1 753 754 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-753-01-1 A340-200754 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YEORA340-300528303-01-1 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1 CPCP A340-200754 MAIN DOOR FITTINGS, LH/RH. I: 6 YEORA340-300ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 12APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS528303-01-2 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 13000 FCGROUP 43C754 MAIN DOOR FITTINGS, LH/RH. I: 3950 FC528304-01-1 755 756 755 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-755-01-1 A340-200756 AFT DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH. I: 3 YEORA340-300528305-01-1 755 756 755 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1 CPCP A340-200756 AFT DOOR, FORWARD FITTINGS LH/RH. I: 6 YEORA340-300528321-01-1 N/A 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-753-01-2 A340-500754 MAIN DOOR, EXTERNAL SKIN, LH/RH. I: 3 YEORA340-600528322-01-1 753 754 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-753-01-2 A340-500754 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YEORA340-600528323-01-1 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, MAIN T: 6 YE 1 CPCP A340-500754 DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS I: 6 YEORON KEELBEAM, LH/RH.A340-600528324-01-1 N/A 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-755-02-1 A340-500755 MAINTENANCE DOOR, EXTERNAL SKIN, LH/RH. I: 3 YEOR756A340-600528325-01-1 755 756 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-755-02-1 A340-500755 MAINTENANCE DOOR, INTERNAL SKIN, LH/RH. I: 3 YEOR756A340-600528326-01-1 755 756 755 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1 CPCP A340-500756 MAINTENANCE DOOR ATTACHMENT AND LOCK FITTINGS, LH/RH. I: 6 YEORA340-600ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 13APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS528327-01-1 N/A 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YEZL-755-02-1 A340-500752 LEG DOOR, INTERNAL AND EXTERNAL SKIN, LH/RH. I: 3 YEORA340-600528328-01-1 N/A 755 DETAILED INSPECTION OF CENTER LANDING GEAR, LEG T: 6 YE 1 CPCP A340-500756 DOOR FITTINGS, LH/RH. I: 6 YEORA340-600528329-01-1 N/A 752 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 6 YE CPCP ZL-753-01-2 A340-500HINGED DOOR, EXTERNAL SKIN. I: 6 YEORA340-600528330-01-1 N/A 149 DETAILED INSPECTION OF CENTER LANDING GEAR, HINGED T: 6 YE 1 CPCP A340-500DOOR, INTERNAL STRUCTURE AND HINGES. I: 6 YEORA340-600528331-01-1 757 758 149 DETAILED INSPECTION OF CENTER LANDING GEAR, HINGED T: 6 YE 1 CPCP A340-500DOOR, TRIPOD AND ANGLE FITTING. I: 6 YEORA340-600528332-01-1 N/A TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 14APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531101-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT T: 6 YE 3 CPCP A340-200RADOME OPENED PRESSURE BULKHEAD ATTACHED TO FR.1. I: 6 YEORA340-300531102-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, T: 6 YE CPCP A340-200EXTERNAL VISIBLE PORTION OF FRAMEWORK BETWEEN FR 3 I: 6 YEORAND FR 10, LH/RHA340-300531103-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE CPCP ZL-200-01-1 A340-200FR 10 AND FR 18 FROM CABIN FLOOR LEVEL TO STR 9 I: 6 YEOR(FWD AND AFT), EXTERNAL SURFACE, LH/RH.A340-300531104-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, T: 12 YE CPCP A340-200EXTERNAL PORTIONS OF FRAMEWORK COVERED BY I: 12 YEORRETAINERS.A340-300531105-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, T: 6 YE CPCP A340-200EXTERNAL VISIBLE PORTIONS OF RETAINERS. I: 6 YEORA340-300531106-01-1 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FCA340-200FR 9 AND FR 10A AT COCKPIT LATERAL WINDOW LOWER I: 10200 FCORCORNER AREA, EXTERNAL SURFACE, LH/RH.A340-300531106-01-2 N/A TASK DELETEDR 531107-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE CPCP ZL-200-01-1 A340-200FR 0 AND FR 10 FROM FLOOR LEVEL TO CROWN I: 3 YEORCENTERLINE, EXTERNAL SURFACEA340-300531110-02-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 531111-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE CPCP ZL-200-01-1 A340-200FR 10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 3 YEORCENTERLINE, EXTERNAL SURFACE, LH/RH.A340-300531112-02-1 N/A TASK DELETED531115-01-1 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 6 YE CPCP A340-200INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YEPRE 40347CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RHORA340-300PRE 40347531115-01-2 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 12 YE CPCP A340-200INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YEPOST 40347CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RHORA340-300POST 40347531116-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE CPCP ZL-100-01-1 A340-200AND JOINT SURFACES BETWEEN FR 0 AND I: 6 YEORFR 18/19 BELOW CABIN FLOOR LEVEL,A340-300EXTERNAL SURFACE531117-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-200PANELS 122 STRUCTURE BETWEEN FR 1 AND FR 20, FROM CABIN FLOOR I: 12 YEORNOTE 1 LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL, INCLUDINGA340-300CABIN FLOOR SUPPORT STRUCTURE AND NLG BAY PANELS ANDBEAMS.NOTE: TPS APPLICATION REQUIRED ONLY BETWEEN FR 10 ANDFR 20, EXCLUDING NLG BAY PANELS531118-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531120-01-1 713 714 123 GENERAL VISUAL INSPECTION OF NLG BAY INTERNAL T: 6 YE 1+2 CPCP A340-200STRUCTURE, NOSE LANDING GEAR WELL PANELS I: 6 YEORA340-300531120-01-2 N/A TASK DELETED531121-01-1 AVIONIC BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-200PANEL 122 STRUCTURE BETWEEN FR 10 AND FR 20 BELOW AVIONICS I: 12 YEORCOMPARTMENT FLOOR LEVELA340-300531122-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-200PANEL 122 STRUCTURE BETWEEN FR 1 AND FR 10 BELOW AVIONICS I: 12 YEORCOMPARTMENT FLOOR LEVELA340-300531123-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200122 STRUCTURE BELOW GALLEYS AND TOILETS FROM CABIN I: 6 YENOTEFLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVELORBETWEEN FR 10 AND FR 13A, LH/RHA340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA531124-01-1 713 714 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 13000 FCGROUP 42ASIDE PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR I: 9600 FCORBAY FORWARD PANEL TO NOSE LANDING GEAR BAY AFTGROUP 43APANEL, LH/RH.ORGROUP 42BORGROUP 43BISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531124-01-2 713 714 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 13000 FCGROUP 43CSIDE PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR ORBAY FORWARD PANEL TO NOSE LANDING GEAR BAY AFT 26000 FHPANEL, LH/RH. I: 11400 FCOR22800 FH531125-01-1 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT T: 13000 FCGROUP 42AAVIONIC BAY FLOOR 122 TO BOTTOM SKIN FROM STR 48 TO STR 51, LH/RH. I: 5700 FCORPANELSGROUP 43AORGROUP 42BORGROUP 43B531125-01-2 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 13000 FCGROUP 43CAVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STR 48 TO STR 51, LH/RH. ORPANELS 26000 FHI: 5700 FCOR11400 FH531126-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AFT T: 12 YE 1 CPCP A340-200716 SIDE PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, I: 12 YEORLH/RH.A340-300531127-01-1 N/A TASK DELETED531127-02-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FCGROUP 42A716 STRUT FITTING LUG BORE I: 13000 FC531127-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FCGROUP 43A716 STRUT FITTING LUG BORE I: 13000 FCISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531127-02-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FCGROUP 42B716 STRUT FITTING LUG BORE I: 13000 FCORGROUP 43B531127-02-4 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FCGROUP 43C716 STRUT FITTING LUG BORE OR26000 FHI: 13000 FCOR26000 FH531129-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR T: 12 YE 1+2 CPCP A340-200716 FITTING. I: 12 YEORBOLTSA340-300NLG ACTUATORDISCONNECTED531129-02-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING T: 13000 FCGROUP 42A716 GEAR ACTUATOR FITTING. I: 4700 FCORBOLTSGROUP 43ANLG ACTUATORORDISCONNECTEDGROUP 42BORGROUP 43BORGROUP 43C531129-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 13000 FCGROUP 43E716 ACTUATOR FITTING. I: 11500 FCBOLTSNLG ACTUATORDISCONNECTEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531130-01-1 NOTE 1 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42A122 STRUCTURE, FR 16A AT CABIN FLOOR LEVEL, LH/RH. I: 3750 FCPRE 44258ORGROUP 43APRE 44258ORGROUP 43BPRE 44258531131-01-1 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 122 FR16A JOINT AREA BETWEEN STRS 28 AND 30, LH/RH. I: 9800 FCPRE 44258NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASORTASK 531131-02-1GROUP 43APRE 44258ORGROUP 43BPRE 44258531131-02-1 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ANOTE 1 122 STRUCTURE, FR 16A JOINT AREA BETWEEN STRS 28 AND 30, I: 9800 FCPRE 44258LH/RH.ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASGROUP 43ATASK 531131-01-1PRE 44258ORGROUP 43BPRE 44258531132-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42A122 FR14 JOINT BETWEEN STRS 28 AND 30 LEVEL, LH/RH. I: 12900 FCORGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43CISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531133-01-1 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ANOTE 1 122 STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM I: 9800 FCORJUNCTION ON FR12A AT STR 26 LEVEL LH/RH.GROUP 43AORGROUP 42BORGROUP 43B531133-01-2 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 43CNOTE 1 122 STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM I: 9800 FCJUNCTION ON FR12A AT STR 26 LEVEL LH/RH.531133-01-3 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 13000 FCGROUP 43ENOTE 1 122 BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON I: 13000 FCFR12A AT STR 26 LEVEL LH/RH.531135-01-1 N/A TASK DELETED531136-01-1 CEILING PANELS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ANOTE 1 222 STRUCTURE, FRS 12 AND 13 DOUBLER AREA AT CROWN I: 10100 FCPRE 42481CENTERLINE.ORGROUP 43APRE 42481531137-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR DRAG STRUT T: 12 YE 1 CPCP A340-200716 FITTING ATTACHMENTS TO UPPER AND FORWARD CANTED I: 12 YEORPANEL.A340-300531138-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD PRESSURE T: 13000 FCGROUP 42ARADOME OPENED BULKHEAD FORWARD FACE, STRINGERS AND SKIN, I: 9200 FCORFROM Y =-50 TO Y = 50 ABOVE COCKPIT FLOOR LEVELGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43CISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531139-01-1 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ANOTE 1 212 STRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACE I: 9200 FCORVERTICAL BEAMS AND UPPER SHEET AT Y =-330,GROUP 42BY = 0 AND Y = 330, ABOVE COCKPIT FLOOR LEVEL.ORGROUP 43AORGROUP 43BORGROUP 43C531140-01-1 N/A TASK DELETED531141-01-1 LININGS 211 DETAILED INSPECTION OF LATERAL FR11, SPLICE T: 13000 FCGROUP 42ANOTE 1 212 ABOVE COCKPIT FLOOR LEVEL ATTACHMENT, INTERNAL I: 9080 FCPRE 41652STRUCTURE, LH/RH.ORGROUP 43APRE 41652531142-01-1 CEILING PANELS 211 DETAILED INSPECTION OF FR 10 UPPER CURVED T: 13000 FCGROUP 42ANOTE 1 212 MEMBER BETWEEN CROWN CENTERLINE AND UPPER LATERAL I: 5250 FCORSPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.GROUP 42BNOTE : THIS TASK IS AN ALTERNATIVE TO TASKOR531142-02-1.GROUP 43AORGROUP 43BORGROUP 43C531142-02-1 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FR 10 UPPER T: 13000 FCGROUP 42ANOTE 1 212 CURVED MEMBER BETWEEN CROWN CENTERLINE AND UPPER I: 7800 FCORLATERAL SPLICING, SPLICE EXCLUDED, INTERNALGROUP 42BSTRUCTURE, LH/RH.ORNOTE : THIS TASK IS AN ALTERNATIVE TO TASKGROUP 43A531142-01-1.ORGROUP 43BORGROUP 43CISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 8APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531143-01-1 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 122 FLOOR BEAM AND CRUCIFORM FITTING AT FR 14, LH/RH. I: 4000 FCORVACUUM PIPESGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C531144-01-1 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ANOTE 1 122 STRUCTURE, JUNCTION AREA BETWEEN FR 14 AND CRUCIFORM I: 7100 FCORTOILET FITTING, LH/RH.GROUP 42BORGROUP 43AORGROUP 43BORGROUP 43CR 531150-01-1 311VU 312VU 313VU 211 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP A340-200314VU 811 212 BULKHEAD ABOVE FLOOR LEVEL, INCLUDING FR1, AS FAR AS I: 12 YEORACCESS BETWEEN FR1 VISIBLEA340-300AND FR2 FROM AVIONICBAY NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THENOTE 1 PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETEAFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTEDAND ELECTRONIC DEVICE REMOVED.531151-01-1 AVIONICS FORWARD 121 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP A340-200FLOOR PANELS 122 BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR PANELS, I: 6 YEORNOTE 1 INCLUDING FR 1 AND STRINGER CONNECTIONS.A340-300WIRING BUNDLESDISPLACED NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THEPRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETEAFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTEDAND ELECTRONIC DEVICE REMOVED.531152-01-1 LINING 211 DETAILED INSPECTION OF COCKPIT WINDOW FRAMES T: 12 YE T: 20 YE CPCP A340-200NOTE 1 212 AND CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND I: 12 YE I: 12 YEORFORWARD).A340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 9APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531154-01-1 N/A TASK DELETED531154-01-2 INSULATION TO BE 211 DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING T: 13000 FCGROUP 43EDISPLACED AS 212 PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, I: 8100 FCREQUIRED TO COMPLETE INTERNAL STRUCTURE, LH/RH.THE INSPECTIONLININGSNOTE 1SLIDING WINDOWSOPENED531156-01-1 CEILING PANELS 211 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-211-02-1 A340-200FCRC (IF INSTALLED) 212 STRUCTURE ABOVE FLOOR LEVEL, FROM FR1 TO FR 17, I: 12 YEZL-221-02-1 ORGALLEYS AND TOILETS 221 EXCLUDING:ZL-223-01-1 A340-300NOTE 1 222 - UPPER AFT FACE OF FORWARD PRESSURE BULKHEAD.OVERHEAD PANELS 223 - WINDSHIELD AND WINDOW FRAMES SURROUNDINGSSIDEWALL PANELS 224 BETWEEN FWD COCKPIT AND FR 10- INTERNAL STRUCTURE AROUND DOOR 1 (FORWARDPASSENGER/CREW DOOR)531157-01-1 LINING 233 DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPER T: 13000 FCGROUP 42ANOTE 1 234 KEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL, I: 10170 FCPRE 41652INTERNAL STRUCTURE, LH/RH.ORGROUP 43APRE 41652531159-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-200NOTE 1 222 STRUCTURE AROUND DOOR 1 (FORWARD PASSENGER/CREW I: 6 YEORDOOR), BETWEEN FR 13A AND FR 17 AND BETWEEN FLOORA340-300LEVEL AND STR 9 (AFT), LH/RH.531161-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 10APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531162-01-1 831 841 211 SPECIAL DETAILED INSPECTION OF FR 7 AND T: 13000 FCGROUP 42ACOCKPIT FLOOR PANELS 212 CROSS BEAM AT ATTACHMENT AREA I: 7800 FCORGROUP 43AORGROUP 42BORGROUP 43B531162-01-2 831 841 211 SPECIAL DETAILED INSPECTION OF FR 7 AND T: 13000 FCGROUP 43CCOCKPIT FLOOR PANELS 212 CROSS BEAM AT ATTACHMENT AREA I: 7500 FC531170-01-1 COCKPIT FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF COCKPIT FLOOR STRUCTURE T: 12 YE CPCP ZL-211-02-1 A340-200212 BETWEEN FR 1 AND FR 10 I: 12 YEORA340-300531171-01-1 CABIN FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2 CPCP A340-200212 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YEOR221 TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 17A340-300222531172-01-1 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2 CPCP A340-200FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YENOTEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 17OR222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDA340-300IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.NOTE531172-01-2 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2 CPCP A340-200FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YENOTEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 17OR222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDA340-300IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.NOTE531173-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-200122 BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM I: 6 YEORCABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOORA340-300LEVEL, BETWEEN FR 13A AND FR 17, LH/RH.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 11APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531175-01-1 LINING 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 13000 FCGROUP 42ANOTE 1 232 JUNCTION BETWEEN FR 17 AND MACHINED STIFFENERS AT I: 8000 FCORSTRS 14/18/22/24, LH/RH.GROUP 43AORGROUP 42BORGROUP 43B531175-01-2 LININGS 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 13000 FCGROUP 43CNOTE 1 232 JUNCTION BETWEEN FR 17 AND MACHINED STIFFENERS AT I: 8000 FCSTRS 14/18/22/24, LH/RH.531176-01-1 FWD AVIONICS BAY 121 GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE T: 6 YE 1+2 CPCP A340-200DOOR OPENED BELOW BATTERIES BETWEEN FR 10A AND FR 11A AND I: 6 YEORNOTE 1 BETWEEN STR 41 AND STR 43, LHA340-300531180-01-1 N/A TASK DELETED531185-01-1 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 222 FORWARD PASSENGER / CREW DOOR CUTOUT AFT UPPER I: 8850 FCORCORNER, JUNCTION OF INTERNAL PLATE ON FR. 17, BETWEENGROUP 42BSTR.12 AND 13, LH/RH.ORGROUP 43AORGROUP 43BPRE 49194ORGROUP 43C531186-01-1 N/A TASK DELETED531187-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 12APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531188-01-1 N/A TASK DELETED531189-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, I: 8850 FCORFORWARD UPPER LONGERON AT STRINGER 12 LEVEL, BETWEENGROUP 42BFR. 13A AND FR.13B, LH/RH.ORGROUP 43AORGROUP 43BORGROUP 43C531192-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 222 JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9 I: 8100 FCORFORWARD, AND FR 13 AFT FACE AND STR 12, LH/RH.GROUP 42BORGROUP 43AORGROUP 43BORGROUP 43E531192-01-2 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 43CNOTE 1 222 JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9 I: 8100 FCFORWARD, AND FR 13 AFT FACE AND STR 12, LH/RH.531194-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 42ANOTE 1 222 MACHINED STIFFENERS 14 AND 22 BETWEEN FR 17 AND FR I: 8100 FCOR18, LH/RH.GROUP 42BORGROUP 43AORGROUP 43BORGROUP 43EISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 13APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531194-01-2 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 43CNOTE 1 222 MACHINED STIFFENERS 14 AND 22 BETWEEN FR 17 AND FR I: 8100 FC18, LH/RH.531198-01-1 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 13000 FCGROUP 42ANOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 8850 FCORBETWEEN FR 13A AND FR 14 AND FR 16A AND FR 17, LH/RH.GROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C531801-01-1 NOTE 1 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE T: 6 YE 3 CPCP A340-500PANELS BULKHEAD ATTACHED TO FR.1. I: 6 YEORRADOME OPENEDA340-600531802-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, T: 6 YE CPCP A340-500EXTERNAL VISIBLE PORTION OF FRAMEWORK BETWEEN FR 3 I: 6 YEORAND FR 10, LH/RHA340-600531803-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE CPCP ZL-200-01-2 A340-500FR.10 AND FR.18 FROM CABIN FLOOR LEVEL TO STR 9 I: 6 YEOR(FWD AND AFT), EXTERNAL SURFACE, LH/RH.A340-600531804-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 12 YE CPCP A340-500PORTION OF FRAMEWORK COVERED BY RETAINERS. I: 12 YEORA340-600531805-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 6 YE CPCP A340-500VISIBLE PORTION OF RETAINERS. I: 6 YEORA340-600531807-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE CPCP ZL-200-01-2 A340-500FR 0 AND FR 10 FROM FLOOR LEVEL TO CROWN CENTERLINE, I: 6 YEOREXTERNAL SURFACE, LH/RH.A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 14APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531810-01-1 N/A TASK DELETED531811-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE CPCP ZL-200-01-2 A340-500FR 10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 12 YEORCENTERLINE, EXTERNAL SURFACE, LH/RH.A340-600531812-01-1 N/A TASK DELETED531815-01-1 SCUFF PLATE 100 DETAILED INSPECTION OF FUSELAGE STRUCTURE OF DOOR 1 T: 12 YE CPCP A340-500(FWD PASSENGER/CREW DOOR), CUTOUT UNDERNEATH THE I: 6 YEORSCUFF-PLATE, LH/RH.A340-600531816-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND T: 6 YE CPCP ZL-100-01-2 A340-500JOINT SURFACES BETWEEN FR 0 AND FR 18/19 BELOW I: 6 YEORCABIN FLOOR LEVEL, EXTERNAL SURFACE.A340-600531816-01-2 N/A TASK DELETED531817-01-1 811 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-500NOTE 1 122 STRUCTURE BETWEEN FR 1 AND FR 20 FROM CABIN I: 12 YEORFLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL,A340-600INCLUDING CABIN FLOOR SUPPORT STRUCTURE ANDNLG BAY PANELS AND BEAMS.NOTE: TPS APPLICATION REQUIRED ONLYBETWEEN FR 10 AND FR 20, EXCLUDING NLG BAY PANELS.531818-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 15APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531820-01-1 713 714 123 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY T: 6 YE 1+2 CPCP A340-500INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS I: 6 YEORA340-600531820-01-2 N/A TASK DELETED531821-01-1 AVIONIC BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-500PANELS 122 STRUCTURE BELOW AVIONICS COMPARTMENT FLOOR I: 12 YEORLEVEL BETWEEN FR.10 AND FR. 20, LH/RH.A340-600531822-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP A340-500PANELS 122 STRUCTURE BELOW AVIONICS COMPARTMENT FLOOR I: 12 YEORNOTE 1 LEVEL BETWEEN FR.1 AND FR.10, LH/RH.A340-600531823-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-500122 BELOW GALLEYS AND TOILETS FROM CABIN FLOOR LEVEL TO I: 6 YENOTEAVIONICS COMPARTMENT FLOOR LEVEL BETWEEN FR 10 ANDORFR 13A, LH/RH.A340-600NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA531824-01-1 N/A TASK DELETED531826-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 12 YE 1 CPCP A340-500716 LATERAL PANELS AROUND DRAG STRUT AND NOSE LANDING I: 12 YEORGEAR ATTACHMENT FITTINGS, LH/RH.A340-600531827-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY, ANGLE T: 6 YE 1 CPCP A340-500716 FITTINGS LINKING FORWARD CANTED PANEL TO ROOF PANEL. I: 6 YEORA340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 16APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531827-01-2 N/A TASK DELETED531829-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AND NOSE T: 12 YE 1 CPCP A340-500716 LANDING GEAR DOORS ACTUATOR FITTINGS, LH/RH. I: 12 YEORBOLTSA340-600DOORS ACTUATORDISCONNECTED531835-01-1 N/A TASK DELETEDR 531850-01-1 311VU 312VU 313VU 211 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP A340-500314VU 811 212 BULKHEAD ABOVE COCKPIT FLOOR LEVEL, INCLUDING FR 1, I: 12 YEORACCESS BETWEEN FR1 AS FAR AS VISIBLE.A340-600AND FR2 FROM AVIONIC NOTE: IF CORROSION IS FOUND ON THE LOWER PART OFBAY THE PRESSURE BULKHEAD (SEE SSI 53-18-51),THENOTE 1 COMPLETE AFT FACE (UPPER AND LOWER AREA)HAS TO BE INSPECTED AND ELECTRONIC DEVICE REMOVED531851-01-1 AVIONIC FWD FLOOR 121 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP A340-500PANELS TO BE REMOVED 122 BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR I: 12 YEORINSULATION AND PANELS, INCLUDING FR.1 AND STRINGER CONNECTIONS.A340-600WIRING BUNDLES TO BE NOTE: IF CORROSION IS FOUND ON THE LOWER PART OFDISPLACED PRESSURE BULKHEAD, THE COMPLETE AFT FACE (UPPER ANDLOWER AREA) HAS TO BE INSPECTED AND ELECTRONICDEVICE REMOVED (SEE SSI 53-18-50)531852-01-1 LINING 211 DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND T: 12 YE T: 20 YE CPCP A340-500NOTE 1 212 CLOSING PANELS, INTERNAL STRUCTURE (FR10 AND I: 12 YE I: 12 YEORFORWARD).A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 17APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531856-01-1 CEILING PANELS 210 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-211-02-2 A340-500FCRC (IF INSTALLED) 220 STRUCTURE ABOVE FLOOR LEVEL, FROM FR 1 TO FR 17, I: 12 YEZL-221-02-2 ORGALLEYS AND TOILETS 230 EXCLUDING :ZL-223-01-2 A340-600(IF INSTALLED) - UPPER AFT FACE OF FORWARD PRESSURE BULKHEAD,NOTE 1 - WINDSHIELD AND WINDOW FRAMES SURROUNDINGS BETWEENOVERHEAD PANELS FWD COCKPIT AND FR 10,SIDEWALL PANELS - INTERNAL STRUCTURE AROUND DOOR 1 (FORWARDPASSENGER/CREW DOOR)531859-01-1 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2 CPCP A340-500NOTE 1 222 AROUND DOOR 1 (FORWARD PASSENGER / CREW DOOR), I: 6 YEORBETWEEN FR13A AND FR17 AND BETWEEN FLOOR LEVEL ANDA340-600STR 9 AFT, LH/RH.531870-01-1 831 841 211 GENERAL VISUAL INSPECTION OF COCKPIT FLOOR T: 12 YE CPCP ZL-211-02-2 A340-500COCKPIT FLOOR PANELS 212 STRUCTURE BETWEEN FR.1 AND FR.10. I: 12 YEORA340-600531871-01-1 831 841 211 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2 CPCP A340-500CABIN FLOOR PANELS 212 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YEOR221 TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.A340-600222531872-01-1 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2 CPCP A340-500FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YENOTEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.OR(IF INSTALLED) 222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDA340-600IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.NOTE531872-01-2 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2 CPCP A340-500FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YENOTEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.OR(IF INSTALLED) 222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDA340-600IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.NOTE531873-01-1 811 821 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-500NOTE 1 122 BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM I: 6 YEORCABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOORA340-600LEVEL BETWEEN FR 13A AND FR 17, LH/RH.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 18APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS531876-01-1 FLOOR PANELS 121 DETAILED INSPECTION OF FUSELAGE STRUCTURE BELOW T: 6 YE 1+2 CPCP A340-500FWD AVIONICS BAY BATTERIES FROM FR10 TO 17 AND FROM STR 40 TO BOTTOM I: 6 YEORDOOR CENTERLINE AND NLG BAY LATERAL PANEL, LH.A340-600NOTE 1531880-01-1 N/A TASK DELETED532101-01-1 N/A TASK DELETED532101-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-100-01-1 A340-200SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO I: 6 YEORBOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAPA340-300JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING,LH/RH.532102-01-1 821 133 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200CARGO COMPARTMENT 134 STRUCTURE BETWEEN FR 20 AND FR 39.1 BELOW I: 6 YEORFLOOR PANELS CARGO COMPARTMENT FLOOR PANELS.A340-300R 532103-01-1 821 131 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-131-03-1 A340-200CARGO COMPARTMENT 132 STRUCTURE BETWEEN MAIN DECK FLOOR I: 12 YEORCEILING PANELS PANELS AND CARGO COMPARTMENT FLOOR FROM FR 20A340-300LINING TO FR 39.1.NOTE 1R 532104-01-1 821 131 DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE T: 6 YE 1+2 CPCP A340-200CARGO COMPARTMENT 132 FROM MAIN DECK FLOOR TO CARGO COMPARTMENT I: 6 YENOTELINING FLOOR, BELOW AND 0.75 M FWD AND AFT OF GALLEYS ANDORNOTE 1 TOILETS, FROM FR 20 TO FR 39.1 LH/RH.A340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED ABOVE THIS AREA.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 19APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532105-01-1 821 134 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200BALLMATS STRUCTURE BELOW FORWARD CARGO COMPARTMENT DOOR I: 6 YEORCUT-OUT BETWEEN FR 19 AND FR 26 FROM CARGOA340-300COMPARTMENT FLOOR TO STR 46 RH.532107-01-1 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1+2 CPCP A340-200COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND I: 6 YEORFR 25 (10 PLACES)A340-300532107-01-2 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 7500 FCZL-821-01-1 A340-200COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND I: 7500 FCORFR 25 (10 PLACES)A340-300R 532107-02-1 821 134 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO T: 6 YE T: 20 YE CPCP A340-200ECCENTRIC BOLTS COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND I: 6 YE I: 6 YEORFR 25A340-300532108-01-1 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1 CPCP A340-200INSULATION 132 STRUCTURE AROUND FORWARD CARGO COMPARTMENT DOOR I: 12 YEORLINING CUT-OUT BETWEEN FR 19 AND FR 26 FROM STR 26 RH TOA340-300CARGO COMPARTMENT FLOOR LEVEL.532109-01-1 N/A TASK DELETED532110-01-1 N/A TASK DELETED532111-01-1 N/A TASK DELETED532114-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 20APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532114-01-2 N/A TASK DELETED532115-01-1 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1 CPCP A340-200COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL I: 6 YEORFRAMES (FR 20A AND FR 25A)A340-300532115-01-2 N/A TASK DELETED532116-01-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE CPCP A340-200234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YEPRE 42069PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 6 ANDPRE 44826CROWN CENTERLINE, LH/RH.ORA340-300PRE 42069PRE 44826532116-02-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE CPCP A340-200234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YEPRE 44826PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 13 ANDPOST 42069CROWN CENTERLINE, LH/RH.ORA340-300PRE 44826POST 42069532116-03-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE CPCP A340-200234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YEPOST 44826PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 3 ANDORCROWN CENTERLINE AND BETWEEN STR 7 TO STR 17, LH/RH.A340-300POST 44826532117-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 21APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 532117-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-1 A340-200SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, I: 12 YEORLH/RH.A340-300532118-01-1 N/A TASK DELETEDR 532119-01-1 832 842 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-231-02-1 A340-200NOTE 1 232 STRUCTURE BETWEEN FR 17 AND FR 36, FROM STR 15 I: 12 YEZL-241-02-1 ORSIDEWALL LINING 241 (OVERHEAD STOWAGE BINS LOWER SURFACE) TOA340-300242 MAIN DECK FLOOR, LH/RH.532120-01-1 832 842 233 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-233-01-1 A340-200CEILING PANELS 234 STRUCTURE BETWEEN FR 17 AND FR 36 FROM STR 15 I: 12 YEZL-243-01-1 ORNOTE 1 243 TO CROWN CENTER LINE, LH/RH.A340-300OVERHEAD STOWAGE 244BINS532121-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-200-01-1 A340-200SURFACE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YEORCUT-OUT BETWEEN FR 32 AND FR 36, FROM STR 9 TO STRA340-30026, LH/RH.R 532122-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200AIR CONDITION DUCTS 132 STRUCTURE BELOW DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YEORNOTE 1 CUT-OUT BETWEEN FR 32 AND FR 36, FROM MAIN DECK FLOORA340-300SIDEWALL LINING DOWN TO STR 30, LH/RH.R 532123-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1 CPCP A340-200NOTE 1 242 STRUCTURE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 12 YEORSIDEWALL/DOOR FRAME 243 CUT-OUT BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOORA340-300LINING 244 UP TO STR 9, LH/RH.532124-01-1 832 842 100 DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW T: 12 YE CPCP A340-200SCUFF PLATE 200 DOOR) CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH I: 6 YEORA340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 22APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532124-02-1 N/A TASK DELETED532124-02-2 N/A TASK DELETED532124-02-3 N/A TASK DELETED532125-01-1 N/A TASK DELETED532125-01-2 N/A TASK DELETED532125-01-3 N/A TASK DELETED532128-01-1 N/A TASK DELETED532129-01-1 N/A TASK DELETED532130-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 23APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 532134-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2 CPCP A340-200FLOOR PANELS 232 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YENOTEGALLEYS AND TOILETS 241 DOOR ENTANCE AREAS, FROM FR 17 TO FR 36.OR242A340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.R 532134-01-2 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 1+2 CPCP A340-200FLOOR PANELS 232 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YENOTEGALLEYS AND TOILETS 241 DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.OR242A340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATEDR 532135-01-1 831 841 231 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE CPCP ZL-231-02-1 A340-200FLOOR PANELS 232 STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND TOILETS, I: 12 YEZL-241-02-1 OR241 AND DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.A340-300242532138-01-1 N/A TASK DELETED532142-01-1 N/A TASK DELETED532143-01-1 N/A TASK DELETED532144-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 24APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532145-01-1 N/A TASK DELETED532146-01-1 N/A TASK DELETED532147-01-1 N/A TASK DELETED532148-01-1 N/A TASK DELETED532149-01-1 N/A TASK DELETED532150-01-1 N/A TASK DELETED532152-01-1 N/A TASK DELETED532153-01-1 N/A TASK DELETED532154-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 25APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532155-01-1 N/A TASK DELETED532156-01-1 N/A TASK DELETED532157-01-1 N/A TASK DELETED532158-01-1 N/A TASK DELETED532158-02-1 N/A TASK DELETED532159-01-1 N/A TASK DELETED532160-01-1 N/A TASK DELETED532161-01-1 N/A TASK DELETED532162-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 26APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532163-01-1 N/A TASK DELETED532165-01-1 N/A TASK DELETED532165-02-1 N/A TASK DELETEDN 532166-01-2 N/A 200 GENERAL VISUAL INPECTION OF FUSELAGE SKIN EXTERNAL T: 3 YE CPCP ZL-200-01-1 A340-200SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO I: 3 YEORCROWN CENTER LINE.A340-300532201-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE CPCP ZL-100-01-2 A340-500EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 I: 6 YEORFROM STR 26 LH/RH TO BOTTOM CENTER LINE,A340-600EXCLUDING AREA UNDERNEATH BELLY FAIRING.532201-01-2 N/A TASK DELETED532202-01-1 821 133 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 134 STRUCTURE BETWEEN FR 20 AND FR 39 BELOW CARGO I: 6 YEORCARGO COMPARTMENT COMPARTMENT FLOOR PANELS.A340-600FLOOR PANELS532203-01-1 821 131 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE CPCP ZL-131-03-2 A340-500ACT (IF INSTALLED) 132 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN I: 12 YEORCARGO COMPARTMENT FLOOR AND CARGO COMPARTMENT FLOOR, FROM FR 20A340-600LINING TO FR 39, LH/RH.NOTE 1ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 27APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532204-01-1 821 131 DETAILED INSPECTION OF FUSELAGE SIDE SHELL INTERNAL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 132 STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YENOTECARGO COMPARTMENT CARGO COMPARTMENT FLOOR, BELOW AND 0.75 M FWDORINSULATION AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FR 20A340-600LINING TO FR 39, LH/RH.NOTENOTE: TASK APPLICABLE IF GALLEYS AND TOILETS AREFITTED ABOVE THE AREA.532205-01-1 132AZ 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-500BALLMATS 134 BELOW FWD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEORFR 19 AND FR 26 FROM CARGO COMPARTMENT FLOOR TOA340-600STR 47, RH.532207-01-1 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1+2 CPCP A340-500COMPARTMENT DOOR LOCK FITTINGS AND BUSHES I: 6 YEORAT 10 POSITIONS BETWEEN FR 20B AND FR 25.A340-600532207-01-2 N/A TASK DELETED532207-02-1 821 134 DETAILED INSPECTION OF FORWARD CARGO T: 6 YE T: 20 YE CPCP A340-500ECCENTRIC BOLTS COMPARTMENT DOOR ECCENTRIC BOLTS AT I: 6 YE I: 6 YEOR10 POSITIONS BETWEEN FR 20B AND FR 25.A340-600532208-01-1 132AZ 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-500INSULATION 132 AROUND FWD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEORLINING FR 19 AND FR 26 FROM STR 26 TO CARGO COMPARTMENTA340-600FLOOR, RH.532215-01-1 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1 CPCP A340-500COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF I: 6 YEORLATERAL FRAMES (FR 20A AND FR 25A).A340-600532215-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 28APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 532217-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-2 A340-500SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, I: 12 YEORLH/RH.A340-600532219-01-1 832 842 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-231-02-2 A340-500NOTE 1 232 STRUCTURE BETWEEN FR 17 AND FR 37.11, FROM STR 15 I: 12 YEZL-241-02-2 ORSIDEWALL LINING 241 (OVERHEAD STOWAGE BINS LOWER SURFACE) TOA340-600242 PASSENGER CABIN FLOOR, LH/RH.532220-01-1 832 842 233 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-233-01-2 A340-500CEILING PANELS 234 STRUCTURE BETWEEN FR 17 AND FR 37.11, FROM I: 12 YEZL-243-01-2 ORNOTE 1 243 STR 15 TO CROWN CENTER LINE, LH/RH.A340-600OVERHEAD STOWAGE 244BINS532221-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-200-01-2 A340-500SURFACE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YEORCUT-OUT BETWEEN FR 37.7 AND FR 37.11, FROM STR 9 TOA340-600STR 26, LH/RH.532222-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-500ACT (IF INSTALLED) 132 BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YEORINSULATION BETWEEN FR 37.7 AND FR 37.11, FROM PASSENGER CABINA340-600LINING FLOOR TO CARGO COMPARTMENT FLOOR, LH/RH.532223-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-500INSULATION 242 AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 12 YEORLINING 243 BETWEEN FR 37.7 AND FR 37.11 FROM PASSENGER CABINA340-600244 FLOOR TO STR 9, LH/RH.532224-01-1 832 842 100 DETAILED INSPECTION OF DOOR 2 T: 12 YE CPCP A340-500SCUFF PLATE 200 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YEORUNDERNEATH SCUFF PLATE, LH/RH.A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 29APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS532234-01-1 821 831 841 131 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 132 STRUCTURE BELOW AND 0,75 M AROUND GALLAYS AND I: 5 YENOTECARGO COMPARTMENT 231 TOILETS, INCLUDING DOOR ENTRANCE AREAS FROMORCEILINGS 232 FR 20 TO FR 39.A340-600FLOOR PANELS 241NOTEGALLEYS AND TOILETS 242 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED532234-01-2 821 831 841 131 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 132 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YENOTECARGO COMPARTMENT 231 TOILETS, INCLUDING DOOR ENTRANCE AREAS FROMORCEILINGS 232 FR 20 TO FR 39.A340-600FLOOR PANELS 241NOTEGALLEYS AND TOILETS 242 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED532235-01-1 831 841 231 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE CPCP ZL-231-02-2 A340-500FLOOR PANELS 232 STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND I: 12 YEZL-241-02-2 OR241 TOILETS, AND DOOR ENTRANCE AREAS, FROM FR 20 TOZL-251-02-2 A340-600242 FR 39.ZL-251-02-3N 532266-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 3 YE CPCP ZL-200-01-2 A340-500SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO I: 3 YEORCROWN CENTER LINE.A340-600533001-01-1 196AB 196BB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FCGROUP 42ASTRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON I: 5500 FCPRE 41410ARCH MEMBER AT Y =-1445.ANDPRE 43451ORGROUP 43APRE 41410ANDPRE 43451ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 30APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533001-01-3 196EB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FCGROUP 42ASTRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON I: 5500 FCPOST 41410ARCH MEMBER AT Y =-1445.ANDPRE 43451ORGROUP 43APOST 41410ANDPRE 43451533002-01-1 196AB 196BB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FCGROUP 42AFRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 10800 FCPRE 41410LONGITUDINAL WEB AT Y =-493ANDPRE 43727ORGROUP 43APRE 41410ANDPRE 43727533002-01-3 196GB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FCGROUP 42AFRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 10800 FCPOST 41410LONGITUDINAL WEB AT Y =-493ANDPRE 43727ORGROUP 43APOST 41410ANDPRE 43727ORGROUP 43BPRE 43727533003-01-1 197AB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE, FR T: 13000 FCGROUP 42A197 53.2 WEB AT Y =-1042, Y =-728.7 AND Y = 728.7 BELOW I: 10800 FCPRE 43727198 LONGITUDINAL WEB ATTACHMENTORGROUP 43APRE 43727ORGROUP 43BPRE 43727ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 31APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533004-01-1 197GB 198GB 197 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FCGROUP 42A198 STRUCTURE AFT OF FR 53.8, T-SECTION JUNCTION ON I: 5500 FCPRE 43451LONGITUDINAL BEAM, LH/RH.ORGROUP 43APRE 43451R 533005-01-1 191AB 191AT 191BB 191 DETAILED INSPECTION OF FUSELAGE SKIN AT T: 13000 FCGROUP 42A191CB 192AT 192BB 192 BELLY FAIRING SEALING LIP ATTACHMENT FROM FR 37.1 OROR192CB 197AT 197FB 197 TO FR 38 AND FROM FR 53.6 TO FR 56 75000 FHGROUP 43A197GB 197HB 198AT 198 I: 4750 FCOR198GB 198HB ORGROUP 42B32300 FHORGROUP 43BORGROUP 43E533006-01-1 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YEA340-200148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 3 YEPRE 50675197BB 197EB 197FB 149OR197GB 197HB 198AT 197A340-300198BB 198EB 198GB 198PRE 50675198HB 734 744753 754533006-01-2 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YEA340-200148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 6 YEPOST 50675197BB 197EB 197FB 149OR197GB 197HB 198AT 197A340-300198BB 198EB 198GB 198POST 50675198HB 734 744753 754533007-01-1 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YEA340-200191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB I: 3 YEPRE 43352192BB 192CBANDPRE 50675ORA340-300PRE 43352ANDPRE 50675ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 32APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533007-01-2 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YEA340-200191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB I: 6 YEPRE 43352192BB 192CBANDPOST 50675ORA340-300PRE 43352ANDPOST 50675533008-01-1 N/A 190 DETAILED INSPECTION OF BELLY FAIRING PANELS AND T: 3 YEA340-200FASTENERS AT WING UPPER SURFACE TO FUSELAGE JUNCTION, I: 3 YEORFROM WING LEADING EDGE TO TRAILING EDGE, LH/RH.A340-300533011-01-1 251PC 251QC 252PC 253 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 42A252QC 254 CIRCUMFERENTIAL JOINT AT FR 53.3 FROM STR 4 TO STR I: 13000 FCPRE 41652NOTE 1 5, LH/RH (64 FASTENER POSITIONS).PRE 52911OVERHEAD STOWAGEORBINS NOTE:GROUP 43ARIVETS TO BE REMOVED - ROTOTEST INSPECTION. FASTENER REMOVAL- 64 POSITIONSPRE 41652- THIS TASK IS AN ALTERNATIVE TO TASK 533011-02-1PRE 52911533011-02-1 251PC 251QC 252PC 253 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 42A252QC 254 CIRCUMFERENTIAL JOINT AT FR 53.3 FROM STR 4 TO STR 5, I: 3830 FCPRE 41652NOTE 1 LH/RH (64 FASTENER POSITIONS).PRE 52911OVERHEAD STOWAGEORBINS NOTE:GROUP 43A- X-RAY INSPECTIONPRE 41652- THIS TASK IS AN ALTERNATIVE TO TASK 533011-01-1PRE 52911533019-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 42ACIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM I: 6000 FCORCENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 ANDGROUP 42BSTRG5) LH/RHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 33APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 533035-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 2.5 YE 1+2 CPCP A340-200BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 2.5 YEPRE 50675A340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.47OR(FOR A340-200) AND FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING,A340-300FR.47 FROM Y=-2390 EXTERNAL SURFACE, LH/RH.PRE 50675TO Y=2390R 533035-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A340-200BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 6 YEPOST 50675A340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.47OR(FOR A340-200) AND FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING,A340-300FR.47 FROM Y=-2390 EXTERNAL SURFACE, LH/RH.POST 50675TO Y=2390R 533036-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 5 YE 1+2 CPCP A340-200BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 5 YEPRE 50675FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390. FAIRING, EXTERNAL SURFACE, LH/RH.A340-300PRE 50675R 533036-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A340-200BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 6 YEPOST 50675FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390. FAIRING, EXTERNAL SURFACE, LH/RH.A340-300POST 50675N 533037-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 12 YE 1+2 CPCP A340-200BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 I: 12 YEORA340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.56A340-300(FOR A340-200) AND COVERED BY BELLY FAIRING, EXTERNAL SURFACE, EXCLUDINGFR.56 EXCLUDING AREA FROM Y=-2390 TO Y=2390, LH/RH.PANELS FROM Y=-2390TO Y=2390533101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE NO CPCP ZL-100-01-1 A340-200200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 12 YEZL-200-01-1 ORTO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RHA340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 34APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533101-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FCGROUP 42A200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 4000 FCORTO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RHGROUP 43A533101-01-3 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FCGROUP 42B200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 5700 FCORTO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RHGROUP 43B533101-01-4 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FCGROUP 43C200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING ORTO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 26000 FHI: 5200 FCOR10400 FH533101-01-5 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FCGROUP 43E200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO ORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 65000 FHI: 4000 FCOR27100 FH533102-01-1 N/A TASK DELETEDR 533103-02-1 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 13000 FCGROUP 42ASKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR ORPRE 4165219, LH/RH. 75000 FHPRE 45749I: 7300 FCORORGROUP 43A49500 FHPRE 41652PRE 45749ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 35APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533104-01-1 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50MM AROUND T: 13000 FCGROUP 42ALIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 I: 6100 FCOROBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48GROUP 43AINSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEENORSTRINGER 1 LH AND STRINGER 1 RHGROUP 42B- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 ANDORFR.40.1 (IF INSTALLED)GROUP 43BR 533104-01-2 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN STRINGER T: 13000 FCGROUP 43CLIGHTS, ANTENNAS AND 1LH AND 1RH 50 MM AROUND: OROBTURATORS WHERE - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 26000 FHINSTALLED - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 I: 7200 FCAND FR.49 AND BETWEEN FR.52 AND FR.53 OR- AFIS ANTENNA CUTOUT BETWEEN FR.40 AND FR.40.1 (IF 14400 FHINSTALLED).533104-01-3 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 13000 FCGROUP 43ELIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 OROBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 65000 FHINSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 5800 FCSTRINGER 1 LH AND STRINGER 1 RH OR- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND 39100 FHFR.40.1533105-01-1 N/A TASK DELETEDR 533106-01-1 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 13000 FCGROUP 43CFASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE ORSKIN BETWEEN STR 18 AND STR 22, FROM FRAME 38 TO 26000 FH53.3, LH/RH. I: 8450 FCOR16900 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 36APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 533107-01-1 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42ADUCTS 132 STRUCTURE, FR.39 TO 39.2, WEB HOLE (AREA JUST BELOW ORORLINING 137 STRINGER 28) AND FASTENERS AREA AT FRAMES JUNCTION 60000 FHGROUP 43ANOTE 1 138 (BELOW STRINGER 29 LEVEL), LH/RH. I: 10400 FCORORGROUP 42B70600 FHORGROUP 43BR 533107-01-2 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 43CDUCTS 132 STRUCTURE, FR.39 TO 39.2, WEB HOLE (AREA JUST BELOW ORLINING 137 STRINGER 28) AND FASTENERS AREA AT FRAMES JUNCTION 26000 FHNOTE 1 138 (BELOW STRINGER 29 LEVEL), LH/RH. I: 12700 FCOR25400 FH533111-01-1 N/A TASK DELETEDR 533113-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 13000 FCGROUP 42ASTRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 ORORTO ABOVE STR 24 LEVEL, LH/RH. 60000 FHGROUP 43AI: 9200 FCOR62300 FH533113-01-2 N/A TASK DELETED533113-01-3 N/A TASK DELETED533114-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 37APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533114-01-2 N/A TASK DELETED533115-01-1 N/A TASK DELETED533115-01-2 N/A TASK DELETED533115-01-3 N/A TASK DELETED533116-01-1 N/A TASK DELETED533117-01-1 191KB 192PB 193BB 191 DETAILED INSPECTION OF FR 40 PRESSURE BULKHEAD, AFT T: 12 YE 1 CPCP A340-200RH ONLY: AIR 192 FACE BELOW CENTER WING BOX. I: 12 YEORCONDITIONING PACK 193A340-300533117-01-2 N/A TASK DELETED533122-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR T: 6 YE 1+2 CPCP A340-200754 148 WELL, KEEL BEAM INTERNAL STRUCTURE AND PANELS I: 6 YEOR149 BETWEEN FR 47 AND FR 53.2A340-300533123-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 6 YE 1 CPCP A340-200148 PRESSURE DIAPHRAGMS AND PRESSURIZED FLOORS LOWER I: 6 YEORSURFACE, BETWEEN FR.47 AND FR.53.2.A340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 38APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533124-01-1 734 744 753 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FCGROUP 42A754 148 CENTER LANDING GEAR DOOR CUTOUT, "Z" STIFFENER AT I: 13000 FCPOST 42605149 HINGE 3 LOCATION, LH/RH.S11998ORGROUP 43APOST 42605S11998ORGROUP 42BORGROUP 43BORGROUP 43CORGROUP 43E533125-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR T: 6 YE 1 CPCP A340-200754 148 53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENT I: 6 YEORAREA OF THE CENTER LANDING GEAR TRUNNION FITTINGSA340-300533125-01-2 N/A TASK DELETEDR 533126-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND T: 6 YE 1 CPCP A340-200754 148 CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO I: 6 YEOR149 AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.A340-300533126-01-2 N/A TASK DELETED533126-01-3 N/A TASK DELETED533126-01-4 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 39APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533127-01-1 N/A TASK DELETED533127-02-1 FAIRING PANELS 191 GENERAL VISUAL INSPECTION OF AREA AROUND AIR T: 6 YE 1 CPCP A340-200BETWEEN FR 39.1 AND 192 CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM I: 6 YEORFR 47 193 (6.0 IN) EXTERNAL SURFACEA340-300195196533127-02-2 N/A TASK DELETED533127-03-1 N/A TASK DELETED533127-03-2 N/A TASK DELETED533129-01-1 734 744 753 143 DETAILED INSPECTION OF KEEL BEAM INTERNAL AND T: 12 YE 1 CPCP A340-200754 149 EXTERNAL STRUCTURE, SKIN AND ADJACENT FUSELAGE I: 12 YEORFAIRING PANELS 191 STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE.A340-300BETWEEN FR 40 AND FR 19247 193195196533130-01-1 753 754 149 DETAILED INSPECTION OF FORWARD AND AFT FACE T: 12 YE 1 CPCP A340-200OF ATTACH FITTING FOR CLG DOOR ACTUATOR AND CLG I: 12 YEORDRAG STRUT FITTING INCLUDING THEIR ATTACHMENT TOA340-300KEEL BEAM TORQUE BOX.533130-02-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 40APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533130-02-2 N/A TASK DELETED533132-02-1 753 754 149 SPECIAL DETAILED INSPECTION OF CLG TRUNNION T: 13000 FCGROUP 42AFITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARD ORPOST 45300FLANGES RADIUS, LH/RH. 22000 FHPRE 46190I: 9300 FCS14212OROR22000 FHGROUP 43APOST 45300PRE 46190S14212ORGROUP 42BPOST 45300PRE 46190S14212ORGROUP 43BPOST 45300PRE 46190S14212R 533132-02-2 753 754 149 SPECIAL DETAILED INSPECTION OF CLG TRUNNION T: 13000 FCGROUP 43CFITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARD ORPRE 46190FLANGES RADIUS, LH/RH. 22000 FHS14212I: 9550 FCOR19100 FH533133-01-1 753 754 149 DETAILED INSPECTION OF CLG LATERAL REACTION T: 12 YE 1 CPCP A340-200FITTING AT FR 53.1, RH. I: 12 YEORA340-300533134-01-1 753 754 149 DETAILED INSPECTION OF ATTACH FITTING FOR CLG T: 12 YE 1 CPCP A340-200ACTUATOR ACTUATOR AND ITS ATTACHMENT TO THE CENTER LINE I: 12 YEORDISCONNECTED STIFFENER AT FR 53.2.A340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 41APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533134-02-1 N/A TASK DELETED533135-01-1 734 744 753 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 12 YE 1 CPCP A340-200754 148 FITTINGS NO.1 THROUGH NO.6, DOOR ACTUATOR FITTINGS I: 12 YEOR149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH.A340-300533135-01-2 734 744 753 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 13000 FCA340-200754 148 FITTINGS NO.1 THROUGH NO.6, DOOR ACTUATOR FITTINGS I: 5000 FCOR149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH.A340-300533136-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING T: 13000 FCA340-200148 NO.1 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FCORA340-300533138-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCA340NOTE 1 146 STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y = 1959, ORPOST MSBAT FR 48 LEVEL, LH/RH. 60000 FH53-4021I: 13000 FCR 533139-01-1 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FCGROUP 42A756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG ORPOST 42606ACTUATOR FITTING UPPER END. 75000 FHS11993I: 5550 FCORORGROUP 43A37600 FHPOST 42606S11993ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 42APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533139-01-2 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FCGROUP 42A756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG I: 8100 FCPOST 42606ACTUATOR FITTING UPPER END.S11997ORGROUP 43APOST 42606S11997ORGROUP 42BORGROUP 43BORGROUP 43ER 533139-01-3 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FCGROUP 43C756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG ORACTUATOR FITTING UPPER END. 26000 FHI: 8050 FCOR16100 FH533140-01-1 743 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 42A148 INTERNAL STRUCTURE, FR 53.2 BULKHEAD FORWARD FACE, I: 6800 FCORANGLE SPLICE AT STR 42, LH/RH.GROUP 43AORGROUP 42BORGROUP 43BORGROUP 43E533140-01-2 743 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 43C148 INTERNAL STRUCTURE, FR 53.2 BULKHEAD FORWARD FACE, I: 6000 FCANGLE SPLICE AT STR 42, LH/RH.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 43APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533141-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR 53.2 T: 12 YE 1 CPCP A340-200ACT (IF INSTALLED) 152 AND PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE I: 12 YEORCARGO FLOOR PANELS AND CARGO COMPARTMENT FLOOR PANEL.A340-300LD-MCR (IFINSTALLED)LININGNOTE 1533142-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 12 YE 1 CPCP A340-200LINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 12 YEORNOTE 1 INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE ANDA340-300STR 40, FROM AFT FACE OF CARGO COMPARTMENT REAR PANELTO FR 40.533143-01-1 822 153 DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND T: 6 YE 1+2 CPCP A340-200ACT (IF INSTALLED) 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR I: 6 YEORCARGO FLOOR PANELS LEVEL.A340-300LD-MCR (IFINSTALLED)533144-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 6 YE 1+2 CPCP A340-200LINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 6 YEORNOTE 1 INTERNAL STRUCTURE BELOW STR 40, FROM FR 39.1 TO FRA340-30040.NOTE : APPLY AFTER INSPECTION IN ADDITION TO TYPE 1TYPE 2 TEMPORARY PROTECTION SYSTEM ON FWD FACEOF FR 40 AND ON FUSELAGE STRUCTURE FROM 25 CMAFTER FR 39.2 TO FR 40533145-01-1 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 13000 FCGROUP 42B198HB 197 BUTT JOINT AT STR 31 LEVEL FROM FR 53.3 TO FR 54, I: 6000 FCOR198 LH/RH.GROUP 43BPRE 49202D 533145-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 44APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533146-01-1 N/A TASK DELETED533147-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-253-01-1 A340-200LINING 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM STR 15 TO I: 12 YEORNOTE 1 253 CROWN CENTER LINE, LH/RH.A340-300OVERHEAD STOWAGE 254BINS533148-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-251-02-1 A340-200LINING 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM STR 15 TO I: 12 YEORNOTE 1 CABIN FLOOR LEVEL, LH/RH.A340-300533149-01-1 N/A TASK DELETED533150-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 6 YE 1 CPCP A340-200GALLEYS AND TOILETS 252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 6 YENOTEFUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.ORNOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA340-300FITTED ABOVE THIS AREA.NOTE533150-02-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 12 YE 1 CPCP A340-200252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 12 YENOTEFUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.ORNOTE :A340-300- TEMPORARY PROTECTION SYSTEM APPLICATION MAY BENOTELIMITED TO PRESSURIZED FLOORS AND PRESSURE DIAPHRAGM.- TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTFITED ABOVE THIS AREAISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 45APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533152-01-1 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FCGROUP 42BACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6000 FCPRE 40379FAIRING LEVEL, LH/RH.ORGROUP 43BPRE 40379ANDPRE 49202R 533152-01-2 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FCGROUP 42BACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8POST 40379LD-MCR (IF FAIRING LEVEL, LH/RH. I: 6000 FCORINSTALLED)GROUP 43BPOST 40379ANDPRE 49202533152-01-3 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FCGROUP 43CACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6000 FCPRE 40379FAIRING LEVEL, LH/RH.ANDPRE 49202R 533152-01-4 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FCGROUP 43CACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8POST 40379LD-MCR (IF FAIRING LEVEL, LH/RH. I: 6000 FCANDINSTALLED)PRE 49202533154-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 46APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533154-01-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42AGALLEYS AND TOILETS 146 STRUCTURE, RIVET ROWS AT SHEAR PANELS AND I: 13000 FCPOST 41652LONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1,ORLH/RH.GROUP 43APOST 41652ORGROUP 42BORGROUP 43BORGROUP 43ER 533154-01-3 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 43CGALLEYS AND TOILETS 146 STRUCTURE, RIVET ROWS AT SHEAR PANELS AND ORLONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1, 26000 FHLH/RH. I: 13300 FCOR26600 FH533157-01-1 N/A TASK DELETEDR 533162-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING T: 13000 FCGROUP 42A148 GEAR BAY, LOWER FLANGE OF GANTRY Y = 1456, 40 ORPRE 43852FASTENERS FORWARD AND AFT OF FR 48 DATUM, LH/RH. 60000 FHORI: 9000 FCGROUP 43AORPRE 4385261000 FHORGROUP 43BPRE 43852533163-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 47APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 533164-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FCGROUP 42A148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR ORORBEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 60000 FHGROUP 43AY = 1959, LH/RH. I: 8800 FCORORGROUP 42B59600 FHORGROUP 43BR 533164-01-2 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FCGROUP 43C148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR ORBEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 26000 FHY = 1959, LH/RH. I: 9900 FCOR19800 FHR 533164-01-3 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FCGROUP 43E148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR ORBEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 65000 FHY = 1959, LH/RH. I: 8300 FCOR56300 FH533165-01-1 N/A TASK DELETED533166-01-1 N/A TASK DELETED533167-01-1 N/A TASK DELETED533168-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 48APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533169-01-1 N/A TASK DELETED533170-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2 CPCP A340-200GALLEYS AND TOILETS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 5 YENOTEAND FR 53.5ORNOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREA340-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.533170-01-2 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2 CPCP A340-200GALLEYS AND TOILETS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 6 YENOTEAND FR 53.5.ORNOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREA340-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.533171-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2 CPCP A340-200252 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YEORTOILETS, BETWEEN FR 36 AND FR 53.5.A340-300533179-01-1 251MG 251SG 252MG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FCGROUP 42A252SG 146 STRUCTURE, FR 48 TO FR 53.1, VERTICAL LEG AT ORPOST 43904GALLEYS AND TOILETS STRINGER PASSAGE LH/RH. 60000 FHORNOTE 1 I: 11100 FCGROUP 43APOST 43904533180-01-1 N/A TASK DELETED533180-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 49APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533181-01-1 N/A TASK DELETED533181-01-2 N/A TASK DELETED533184-01-1 N/A TASK DELETED533186-01-1 N/A TASK DELETEDR 533190-01-1 834 844 261 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-200INSULATION 262 AROUND DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YEORLINING CUT-OUT, BETWEEN FR 53.4 AND FR 53.8 FROM MAIN DECKA340-300FLOOR LEVEL TO STR 9, LH/RH.R 533191-01-1 151EW 151GW 152EW 151 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-200152GW 822 152 BELOW DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YEORACT (IF INSTALLED) CUT-OUT, BETWEEN FR 53.4 AND FR 53.8 FROM MAIN DECKA340-300FLOOR PANELS FLOOR DOWN TO CARGO FLOOR LEVEL LH/RH.INSULATIONLDL TOILETS ANDFURNISHING (IFINSTALLED)LDMCR (IF INSTALLED)533192-01-1 N/A TASK DELETED533193-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 50APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533193-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE CPCP ZL-100-01-1 A340-200200 (INCLUDING DOOR 3 CUTOUT) BETWEEN FR 53.3 AND FR 54 I: 6 YEZL-200-01-1 ORFROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERA340-300LINE, EXTERNAL SURFACE, LH/RH.533194-01-1 N/A TASK DELETED533194-01-2 N/A TASK DELETED533194-01-3 N/A TASK DELETED533194-01-4 N/A TASK DELETED533194-01-9 N/A TASK DELETED533195-01-1 834 844 100 DETAILED INSPECTION OF DOOR 3 CUT-OUT, STRUCTURE T: 12 YE CPCP A340-200SCUFF PLATE UNDERNEATH SCUFF PLATE, LH/RH. I: 6 YEORA340-300533195-02-1 N/A TASK DELETED533195-02-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 51APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533195-02-3 N/A TASK DELETED533195-02-4 N/A TASK DELETED533195-02-9 N/A TASK DELETED533716-01-1 734 744 753 149 DETAILED INSPECTION OF KEEL BEAM, CENTER LANDING GEAR T: 12 YE 1+2 CPCP A340-500754 FITTING INTERNAL STRUCTURE, LH/RH. I: 12 YEOREXTERNAL ANDA340-600INTERNAL PLUGS533717-01-1 192GB 193FB 193JB 193 DETAILED INSPECTION OF KEEL BEAM, SPLICE TO FR41, T: 12 YE 1+2 CPCP A340-500195GB INTERNAL SURFACE, LH/RH. I: 12 YEORLEFT AIRA340-600CONDITIONING PACK533718-01-1 197AB 197 DETAILED INSPECTION OF KEEL BEAM, SPLICE TO FR 53.3, T: 12 YE 1+2 CPCP A340-500198 INTERNAL SURFACE, LH/RH. I: 12 YEORA340-600533719-01-1 192EB 193CB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM, INTERFACE T: 6 YE T: 12 YE 1+2 CPCP A340-500LEFT AND RIGHT AIR 192 BETWEEN UPPER SPAR, ANGLE FITTINGS AND FORWARD LOWER I: 6 YE I: 12 YEORINLET SHELL PANEL FROM FR38.1 TO FR40.3, AS FAR AS VISIBLE,A340-600LH/RH.NOTE: TPS APPLICATION ONLY FOR 100 % TASK.533720-01-1 191AB 192AB 192GB 191 DETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TO T: 12 YE 1+2 CPCP A340-500192KB 193CB 193FB 192 FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN I: 12 YEORLEFT RAM AIR INLET 193 OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 52APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533721-01-1 197EB 198EB 197 SPECIAL DETAILED INSPECTION OF KEEL BEAM, INTERFACE T: 6 YE T: 12 YE 1+2 CPCP A340-500198 BETWEEN UPPER SPAR, ANGLE FITTINGS AND AFT LOWER I: 6 YE I: 12 YEORSHELL PANEL FROM FR53.2 TO FR53.6, AS FAR AS VISIBLE,A340-600LH/RH.NOTE: TPS APPLICATION ONLY FOR 100 % TASK.533722-01-1 197EB 198EB 197 DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO T: 12 YE 1+2 CPCP A340-500198 FR 53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND I: 12 YEORSKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RHA340-600533723-01-1 192EB 192GB 192LB 191 DETAILED INSPECTION OF KEEL BEAM- T-SECTION BEAM, T: 12 YE 1+2 CPCP A340-500192QB 195GB 195LB 192 LH/RH. I: 12 YEOR734 744 195A340-600AIR CONDITIONING 196PACKSHEATSHIELDSR 533728-01-1 192EB 192GB 193CB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM INTERNAL T: 6 YE T: 12 YE 1+2 CPCP A340-500193FB 193GB 193JB 192 SURFACE, NUTPLATE BETWEEN RIB 2 AND RIB 7, LH/RH. I: 6 YE I: 12 YEPRE 50217ACCESS THROUGH NOTE: TPS APPLICATION ONLY FOR 100 % TASK.ORELLIPTICAL HOLES ONA340-600DAMPING PANELSPRE 50217533729-01-1 143AB 753 754 143 DETAILED INSPECTION OF KEEL BEAM, INTERNAL SURFACE T: 12 YE 1+2 CPCP A340-500OF TORQUE BOX. I: 12 YEORA340-600533730-01-1 143AB 753 754 143 DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX T: 6 YE 1+2 CPCP A340-500EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH. I: 6 YEORA340-600533730-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 53APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533731-01-1 192GB 193FB 193LB 143 DETAILED INSPECTION OF KEEL BEAM, EXTERNAL SURFACE , T: 6 YE 1+2 CPCP A340-500195GB 753 754 192 FROM FR40.3 TO FR47, INCLUDING RODS AND ATTACHMENT I: 6 YEORLEFT AIR 195 FITTINGS AT RIB 6, 10,13 AND 16, LH/RH.A340-600CONDITIONING PACKLEFT RAM AIR INLET533731-01-2 N/A TASK DELETED533732-01-1 734 744 753 147 DETAILED INSPECTION OF KEEL BEAM EXTERNAL SURFACE T: 6 YE 1+2 CPCP A340-500754 148 FROM FR 47 TO FR 53.2, INCLUDING ATTACH FITTING FOR I: 6 YEOR149 MLG DOOR ACTUATOR, LH/RH.A340-600NOTE: TPS APPLICATION ONLY ON ATTACH FITTINGFOR MLG DOOR ACTUATOR533732-01-2 N/A TASK DELETEDR 533735-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 2.5 YE 1+2 CPCP A340-500BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1 I: 2.5 YEPRE 51066FR.47 FROM Y=-2360 AND FR 47 FROM Y=-2360 TO Y=2360, COVERED BY BELLYANDTO Y=2360 FAIRING, EXTERNAL SURFACE, LH/RH.PRE 56418ORA340-600PRE 51066ANDPRE 56418R 533735-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A340-500BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1 I: 6 YEPOST 51066FR.47 FROM Y=-2360 AND FR 47 FROM Y=-2360 TO Y=2360, COVERED BY BELLYORTO Y=2360 FAIRING, EXTERNAL SURFACE, LH/RH.POST 56418ORA340-600POST 51066ORPOST 56418ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 54APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 533736-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 5 YE 1+2 CPCP A340-500BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 5 YEPRE 51066FR.56 FROM Y=-2360 AND FR.56 FROM Y=-2360 TO Y=2360, COVERED BY BELLYANDTO Y=2360. FAIRING, EXTERNAL SURFACE, LH/RH.PRE 56418ORA340-600PRE 51066ANDPRE 56418R 533736-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A340-500BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 6 YEPOST 51066FR.56 FROM Y=-2360 AND FR.56 FROM Y=-2360 TO Y=2360, COVERED BY BELLYORTO Y=2360. FAIRING, EXTERNAL SURFACE, LH/RH.POST 56418ORA340-600POST 51066ORPOST 56418N 533737-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 12 YE 1+2 CPCP A340-500BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 I: 12 YEORFR.56 EXCLUDING AND FR.56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE,A340-600PANELS FROM Y=-2360 EXCLUDING AREA FROM Y=-2360 TO Y=2360.TO Y=2360533801-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE CPCP ZL-100-01-2 A340-500200 FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO I: 12 YEZL-200-01-2 ORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.A340-600533817-01-1 192GB 192LB 191 DETAILED INSPECTION OF AFT FACE OF FR40 PRESSURE T: 12 YE 1 CPCP A340-500192 BULKHEAD BELOW CENTER WING BOX. I: 12 YEOR193A340-600195533823-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY UPPER T: 6 YE 1 CPCP A340-500148 PRESSURE PANELS, LOWER SURFACE, BETWEEN FR 47 AND I: 6 YEORFR 53.2A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 55APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533823-01-2 N/A TASK DELETED533825-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF FWD FACE OF FR.53.2 T: 6 YE 1 CPCP A340-500754 148 PRESSURE BULKHEAD INCLUDING FOOTFRAME, I: 6 YEOR149 FLAP-TRACK BRACKETS, UPPER SUPPORT BRACKET ANDA340-600CONNECTION PLATES LATERAL PANEL.533825-01-2 N/A TASK DELETED533828-01-1 734 744 753 147 DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT T: 6 YE 1 CPCP A340-500754 148 FITTING ON FR 53.2 I: 6 YEOR149A340-600533828-01-2 N/A TASK DELETED533831-01-1 734 744 753 147 DETAILED INSPECTION OF FORWARD FACE OF FR 53.2 T: 6 YE 1 CPCP A340-500754 148 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9. I: 6 YEOR149A340-600533831-01-2 N/A TASK DELETED533834-01-1 734 744 753 149 DETAILED INSPECTION OF ATTACH FITTING FOR CLG T: 12 YE 1 CPCP A340-500754 ACTUATOR AND UPLOCK BRACKET. I: 12 YEORACTUATOR BOLTA340-600ACTUATORDISCONNECTEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 56APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533841-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR53.2 AND T: 12 YE 1 CPCP A340-600ACT (IF INSTALLED) 152 PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND I: 12 YELDMCR (IF INSTALLED) CARGO COMPARTMENT FLOOR LEVEL, INCLUDING BEAMS ANDLINING INTERCOSTALS.NOTE 1533842-01-1 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 6 YE 1+2 CPCP A340-500AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 6 YENOTEDUCTS INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE ANDORGALLEYS AND TOILETS STGR 41, FROM FR39 TO FR40.A340-600LINING NOTE: TASK APPLICABLE IF GALLEYS OR TOILETSNOTENOTE 1 FITTED ABOVE THE AREAREAR PANEL OF FWDCARGO COMPARTMENT533842-01-2 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 12 YE CPCP A340-500AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 12 YENOTEDUCTS INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE ANDORLINING STGR 41, FROM FR39 TO FR40.A340-600NOTE 1 NOTE: TASK APPLICABLE IF NO GALLEYS OR TOILETSNOTEREAR PANEL OF FWD FITTED ABOVE THE AREACARGO COMPARTMENT533843-01-1 822 153 DETAILED INSPECTION OF AFT FACE OF FR53.2 AND T: 6 YE 1+2 CPCP A340-600ACT 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR I: 6 YECARGO COMPARTMENT LEVEL.FLOOR PANELSLDMCR533844-01-1 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 6 YE 1+2 CPCP A340-500AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 6 YEORDUCTS INTERNAL STRUCTURE BELOW STGR 41, FROM FR39 TO FR40.A340-600LININGNOTE 1 NOTE: TPS IS REQUIRED ONLY ON FWD FACE OF FR40 ANDREAR PANEL OF FWD ON FUSELAGE INTERNAL STRUCTURE FROM 25 CM AFTERCARGO COMPARTMENT FR39.2 TO FR40.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 57APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533847-01-1 GALLEYS AND TOILETS 253 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-253-01-2 A340-500LINING 254 STRUCTURE BETWEEN FR 37.11 AND FR 53.4 (FOR -500), I: 12 YEZL-253-01-3 ORNOTE 1 FR 56.1 (FOR -600), ABOVE STR 15, LH/RH.A340-600OVERHEAD STOWAGEBINS533848-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-251-02-2 A340-500LINING 252 STRUCTURE BETWEEN FR 37.11 AND FR 53.4 (FOR -500), I: 12 YEZL-251-02-3 ORNOTE 1 FR 56.1 (FOR -600), BETWEEN STR 15 AND CABIN FLOORA340-600LEVEL, LH/RH.533849-01-1 N/A TASK DELETED533849-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE NOA340-500STRUCTURE, LINER INSIDE RCT FROM FR.53.2 TO FR.53.7 I: 6 YE(RCT5) OR TO FR.53.9 (RCT9), AS FAR AS VISIBLE533850-01-1 822 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 6 YE 1+2 CPCP A340-500CABIN FLOOR PANELS 146 BETWEEN FR47 AND FR53.2, FROM CABIN FLOOR LEVEL TO I: 6 YENOTEFWD PANEL OF AFT HORIZONTAL PRESSURE PANEL.ORCARGO COMPARTMENT NOTE: TASK APPLICABLE IF GALLEYS OR TOILETSA340-600GALLEYS AND TOILETS FITTED ABOVE THE AREANOTE533850-01-2 822 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 12 YE CPCP A340-500CABIN FLOOR PANELS 146 BETWEEN FR47 AND FR53.2, FROM CABIN FLOOR LEVEL TO I: 12 YENOTEFWD PANEL OF AFT HORIZONTAL PRESSURE PANEL.ORCARGO COMPARTMENT NOTE: TASK APPLICABLE IF NO GALLEYS OR TOILETSA340-600FITTED ABOVE THE AREANOTE533852-01-1 197AB 155 DETAILED INSPECTION OF REAR CENTER TANK, LOWER T: 6 YE CPCP A340-500FUSELAGE SKIN FROM FR 53.2 TO FR 53.8 , BETWEEN STR I: 6 YE54 LH AND STR 54 RH, MANHOLE AND PUMP HOLE FITTINGS,AND CRASH SKIDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 58APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533853-01-1 N/A TASK DELETED533853-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK, T: 12 YE NO CPCP ZL-155-01-1 A340-500FUEL PUMPS INTERNAL STRUCTURE, LOWER AREA BELOW STR 46 FROM FR I: 12 YELINER 53.2 TO FR 53.7 (FOR 5 FRAME BAY LENGTH) , TO FR.53.9PIPING (FOR 7 FRAME BAY LENGTH), AND MAN HOLE CUT-OUT, ANDANTI CRASH RODS, AS FAR AS VISIBLE533854-01-1 FLOOR PANELS 151 DETAILED INSPECTION OF ANGLE BETWEEN FUSELAGE AND RCT T: 6 YE 1+2 CPCP A340-500GALLEYS AND TOILETS 152 OBLIQUE PANELS, BETWEEN FR.53.2 AND FR.53.7 (FOR 5 I: 6 YENOTEFRAME BAY LENGTH) AND FR.53.9 (FOR 7 FRAME BAYLENGTH), FROM THE JUNCTION TO STGR 31.NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREFITTED IN THIS AREA533854-01-2 FLOOR PANELS 151 DETAILED INSPECTION OF ANGLE BETWEEN FUSELAGE AND RCT T: 12 YE 1+2 CPCP A340-500152 OBLIQUE PANELS, BETWEEN FR.53.2 AND FR.53.7 (FOR 5 I: 12 YENOTEFRAME BAY LENGTH) AND FR.53.9 (FOR 7 FRAME BAYLENGTH), FROM THE JUNCTION TO STGR 31.NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTFITTED IN THIS AREA533855-01-1 822 151 DETAILED INSPECTION OF REAR CENTER TANK, AFT FACE OF T: 12 YE 1 CPCP A340-500INSULATION 152 FR.53.7 (FOR 5 FRAME BAY LENGTH), FR.53.9 (FOR 7 I: 12 YELINING FRAME BAY LENGTH), BETWEEN CABIN FLOOR STRUCTURE ANDCARGO COMPARTMENT FLOOR LEVEL.533856-01-1 822 153 DETAILED INSPECTION OF REAR CENTER TANK, AFT FACE OF T: 6 YE 1+2 CPCP A340-500LININGS 154 FR.53.7 (FOR 5 FRAME BAY LENGTH), OF FR.53.9 (FOR 7 I: 6 YENOTE 1 FRAME BAY LENGTH), BELOW CARGO COMPARTMENT FLOORLEVEL.533857-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 59APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533857-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK T: 12 YE NO CPCP ZL-155-01-1 A340-500INTERNAL STRUCTURE ABOVE STR 46, EXCLUDING STRUTS I: 12 YEONLY533858-01-1 N/A TASK DELETED533858-01-2 153AZ 155AZ 197CB 155 DETAILED INSPECTION OF REAR CENTER TANK, COMPOSITE T: 12 YE NOA340-500STRUTS (20 PLACES FOR 5 FRAME BAY LENGTH AND 21 I: 12 YEPLACES FOR 7 FRAMES BAY LENGTH)533859-01-1 N/A TASK DELETED533859-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK, 3 FWD T: 12 YE NO CPCP A340-500METALLIC STRUTS (FOR 7 FRAME BAY LENGTH) I: 12 YEPOST 47968533870-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW T: 5 YE 1+2 CPCP A340-500GALLEYS AND TOILETS 252 AND 0.75M AROUND GALLEYS AND TOILETS, BETWEEN FR.39 I: 5 YENOTEANDOR- FR53.2 (FOR-600),A340-600- FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYSNOTELENGTH),- FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYSLENGTH).NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 60APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533870-01-2 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW T: 6 YE 1+2 CPCP A340-500GALLEYS AND TOILETS 252 AND 0.75M AROUND GALLEYS AND TOILETS, BETWEEN FR.39 I: 6 YENOTEANDOR- FR53.2 (FOR-600),A340-600- FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYSNOTELENGTH),- FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYSLENGTH)NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.533871-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, T: 12 YE 1+2 CPCP A340-500TO BE REMOVED 252 EXCLUDING AREAS BELOW AND 0.75M AROUND GALLEYS AND I: 12 YEORTOILETS, BETWEEN FR.39 ANDA340-600- FR53.2 (FOR-600),- FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYSLENGTH),- FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYSLENGTH).533881-01-1 LINING PANELS TO BE 251 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2 CPCP A340-600REMOVED 252 AROUND OVERWING EMERGENCY DOOR FROM STRINGER 12 TO I: 12 YENOTE 1 FLOOR LEVEL BETWEEN FR40.6 AND FR44, LH/RH.533890-01-1 LINING PANELS TO BE 261 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND T: 12 YE 1+2 CPCP A340-500REMOVED 262 DOOR 3 (EMERGENCY DOOR) CUT-OUT, BETWEEN FR53.3 AND I: 12 YENOTE 1 FR53.8 FROM CABIN FLOOR LEVEL TO STR 9, LH/RH.533891-01-1 822 151 DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN, T: 6 YE 1+2 CPCP A340-500FLOOR PANELS 152 BETWEEN FR.53.2 AND FR.53.7 (FOR 5 FRAME BAY LENGTH), I: 6 YENOTEGALLEYS AND TOILETS AND FR.53.9 (FOR 7 FRAME BAY LENGTH), FROM CABINFLOOR LEVEL TO STRINGER 31NOTE: TASK APPLICABLE IF TOILETS OR GALLEYSARE INSTALLED IN THIS AREAISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 61APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS533891-01-2 822 151 DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN, T: 12 YE 1+2 CPCP A340-500FLOOR PANELS 152 BETWEEN FR.53.2 AND FR.53.7 (FOR 5 FRAME BAY LENGTH), I: 12 YENOTEAND FR.53.9 (FOR 7 FRAME BAY LENGTH), FROM CABINFLOOR LEVEL TO STRINGER 31NOTE:TASK APPLICABLE IF TOILETS OR GALLEYSARE NOT INSTALLED IN THIS AREA533895-01-1 SCUFF PLATE 200 DETAILED INSPECTION OF DOOR 3 (EMERGENCY DOOR) T: 12 YE CPCP A340-500CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH. I: 6 YE534102-01-1 N/A TASK DELETED534102-01-2 N/A TASK DELETED534104-01-1 N/A TASK DELETED534104-01-2 N/A TASK DELETED534104-01-3 N/A TASK DELETED534104-01-5 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 62APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534105-01-1 N/A TASK DELETED534105-01-2 N/A TASK DELETED534107-01-1 N/A TASK DELETED534107-01-3 N/A TASK DELETED534108-01-1 N/A TASK DELETED534110-01-1 N/A TASK DELETED534120-01-1 N/A TASK DELETED534122-01-1 N/A TASK DELETED534124-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 63APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 534124-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE CPCP ZL-200-01-1 A340-200FR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH EXCLUDING I: 12 YEORAREA UNDER VERTICAL STABILIZER FAIRING, EXTERNALA340-300SURFACE.534125-01-1 N/A TASK DELETED534126-01-1 N/A TASK DELETED534126-02-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-100-01-1 A340-200SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH I: 6 YEORTO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES ANDA340-300LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREAOF SKIN AFT OF THE BELLY FAIRING AND FORWARD OFFR 54534127-01-1 822 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.2 AND FR 73 BELOW CARGO I: 6 YEORCARGO COMPARTMENT 163 COMPARTMENT FLOOR PANELS.A340-300FLOOR PANELS 164INSULATION NOTE: IF LDL INSTALLED, INSPECTION AREA BETWEEN FRLDMCR (IF INSTALLED) 54A AND FR 73.R 534128-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200NOTE 1 172 STRUCTURE BETWEEN FR 73 AND FR 80 BELOW MAIN DECK I: 6 YEORFLOOR INCLUDING MAIN DECK FLOOR STRUCTUREA340-300534130-01-1 N/A 100 GENERAL VISUAL INSPECTION OF T: 6 YE CPCP ZL-100-01-1 A340-200200 FUSELAGE SKIN AT DOOR 4 (AFT PASSENGER/CREW DOOR) I: 6 YEZL-200-01-1 ORCUT-OUT BETWEEN FR 73 AND FR 76, FROM STR 9 TO STR 26A340-300LH/RH, EXTERNAL SURFACEISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 64APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534130-01-2 N/A TASK DELETED534131-01-1 N/A TASK DELETED534132-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT T: 12 YE CPCP A340-200SCUFF PLATE 200 PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YEORUNDERNEATH SCUFF PLATE, LH/RH.A340-300534132-02-1 N/A TASK DELETEDR 534133-01-1 833 843 271 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-200DOOR FRAME LININGS 272 AROUND DOOR 4 (AFT PASSENGER/CREW DOOR) BETWEEN FR I: 12 YEORINSULATION 72 AND FR 77 FROM MAIN DECK FLOOR LEVEL TOA340-300LINING STR 9 LH/RH.R 534134-01-1 162ZW 823 171 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-200NOTE 1 172 BELOW DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, I: 6 YEORBETWEEN FR 73 AND FR 76 FROM MAIN DECK FLOOR LEVELA340-300TO STR 30 LH/RH.534135-01-1 N/A TASK DELETED534136-01-1 N/A TASK DELETED534137-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 65APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534137-01-3 N/A TASK DELETED534138-01-1 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT T: 12 YE 1 CPCP A340-200INSULATION 154 CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND I: 12 YEORLINING FR 66, FROM STR 26 RH TO CARGO FLOOR LEVEL.A340-300534139-01-1 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1 CPCP A340-200154 DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES I: 6 YEOR(FR 59A AND FR 65) AS FAR AS VISIBLEA340-300534139-01-2 N/A TASK DELETED534140-01-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR T: 6 YE T: 20 YE CPCP A340-200ECCENTRIC BOLTS AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN I: 6 YE I: 6 YEORFR 59A AND FR 65A340-300R 534140-02-1 822 152 GENERAL VISUAL INSPECTION OF T: 6 YE 1+2 CPCP A340-200LOCK FITTINGS AND BUSHES FOR AFT I: 6 YEORCARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEENA340-300FR 59A AND FR 65534140-02-2 N/A TASK DELETED534141-01-1 N/A TASK DELETED534143-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 66APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534143-01-3 N/A TASK DELETED534144-01-1 823 100 DETAILED INSPECTION OF BULK CARGO T: 12 YE CPCP A340-200SCUFF PLATE COMPARTMENT DOOR CUT-OUT STRUCTURE I: 6 YEORUNDERNEATH SCUFF PLATE.A340-300534144-02-1 N/A TASK DELETED534144-02-2 N/A TASK DELETED534145-01-1 823 162 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-200FLOOR PANELS AROUND BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEORLINING FR 66 AND FR 70 FROM STR 31 TO STR 48, RH.A340-300NOTE 1534146-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1+2 CPCP A340-200DOOR STOP FITTINGS AT 10 POSITIONS AT FR 67 AND FR 69 I: 6 YEORA340-300534146-01-2 N/A TASK DELETED534148-01-1 N/A TASK DELETED534149-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1 CPCP A340-200DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 67 I: 6 YEORAND FR 69) AS FAR AS VISIBLEA340-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 67APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534149-01-2 N/A TASK DELETED534150-01-1 N/A TASK DELETED534154-01-1 N/A TASK DELETED534155-01-1 N/A TASK DELETED534156-01-1 N/A TASK DELETED534156-01-2 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-200CARGO COMPARTMENT 154 BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT I: 6 YEORFLOOR PANELS BETWEEN FR 59 AND FR 67, FROM CARGO FLOOR LEVELA340-300INSULATION TO STR 47 RHLININGR 534157-01-1 833 843 261 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE CPCP ZL-261-02-1 A340-200FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS, I: 12 YEZL-271-02-1 OR271 AND DOOR ENTRANCE AREAS FROM FR 53.5 TO FR 80.A340-300272ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 68APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 534158-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1 CPCP A340-200ACT (IF INSTALLED) 152 STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND I: 12 YEORCARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 53.2 TO FR 73,A340-300CEILING PANELS 162 INCLUDING MAIN DECK FLOOR STRUCTURELDL TOILETS AND 171FURNISHING (IF 172INSTALLED)LDMCR (IF INSTALLED)LININGNOTE 1R 534159-01-1 833 843 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2 CPCP A340-200FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS INCLUDING I: 5 YENOTETOILETS AND GALLEYS 271 DOOR ENTRANCE AREAS FROM FR 53.5 TO FR 80.OR272A340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATEDR 534159-01-2 833 843 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 1+2 CPCP A340-200FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS INCLUDING I: 6 YENOTETOILETS AND GALLEYS 271 DOOR ENTRANCE AREAS, FROM FR 53.5 TO FR 80.OR272A340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED534160-01-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-263-01-1 A340-200CEILING PANELS 264 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM STR 15 TO I: 12 YEZL-273-01-1 ORNOTE 1 273 CROWN CENTER LINE, LH/RH.A340-300OVERHEAD STOWAGE 274BINSR 534161-01-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-261-02-1 A340-200NOTE 1 262 STRUCTURE BETWEEN FR 53.5 AND FR 80 FROM STR 15 I: 12 YEZL-271-02-1 ORSIDEWALL LINING 271 (OVERHEAD STOWAGE BINS LOWER SURFACE)A340-300272 TO MAIN DECK FLOOR, LH/RH.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 69APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 534162-01-1 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2 CPCP A340-200ACT (IF INSTALLED) 152 STRUCTURE FROM MAIN DECK FLOOR TO CARGO I: 6 YENOTECARGO COMPARTMENT 161 COMPARTMENT FLOOR, BELOW AND 0.5M FWD AND AFT OFORCEILING PANELS 162 UPPER DECK GALLEYS AND TOILETS, FROM FR 53.5 TOA340-300LAVATORY/GALLEY 171 FR 80, LH/RHNOTEEXTRACTION DUCT (FR 172 NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE78-79) FITTED ABOVE THE AREALDL TOILETS ANDFURNISHING (IFINSTALLED)LDMCR (IF INSTALLED)LININGLOWER DECK CARGOCOMPARTMENTVENTILATION DUCT (FR70-71)NOTE 1534163-01-1 833 843 151 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-200FLOOR PANELS 152 STRUCTURE IN LDL AREA FROM FR 53,2 TO FR 54A AND I: 6 YENOTEINSULATION 153 FROM STR 37 TO BOTTOM CENTER LINE, LH/RH,ORLDL CEILING 154 INCLUDING LDL UPPER AND LOWER ATTACHMENT POINTS.A340-300LINING NOTE: TASK ONLY APPLICABLE IF LDL INSTALLEDNOTETOILETS FURNISHING534166-01-1 N/A TASK DELETED534166-02-1 N/A TASK DELETEDN 534177-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE CPCP ZL-200-01-1 A340-200FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER I: 3 YEORLINE, EXCLUDING AREA UNDER VERTICAL STABILIZERA340-300FAIRING, EXTERNAL SURFACE.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 70APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 534224-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-2 A340-500SURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TO STR 26, I: 12 YEORLH/RH, EXCLUDING AREA COVERED BY VERTICAL STABILIZERA340-600FAIRING.534226-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE CPCP ZL-100-01-2 A340-500EXTERNAL SURFACE BETWEEN FR 54 AND FR 80 I: 6 YEORFROM STR 26 LH/RH TO BOTTOM CENTER LINE,A340-600EXCLUDING AREA UNDERNEATH BELLY FAIRING.534226-01-2 N/A TASK DELETED534227-01-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-600ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.2 AND FR 73 BELOW I: 6 YECARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.FLOOR PANELS 164LDF FURNISHING ANDEQUIPMENT (IFINSTALLED)LDMCR (IF INSTALLED)534227-02-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.7 AND FR 73 BELOW I: 6 YEPOST 47021CARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.FLOOR PANELS 164LDF FURNISHING ANDEQUIPMENT (IFINSTALLED)LDMCR (IF INSTALLED)534227-03-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.9 AND FR 73 BELOW I: 6 YEPOST 47968CARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.FLOOR PANELS 164LDF FURNISHING ANDEQUIPMENT (IFINSTALLED)LDMCR (IF INSTALLED)ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 71APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534228-01-1 161AZ 822 171 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP A340-500IF LDF (PARTIAL OR 172 STRUCTURE BETWEEN FR 73 AND FR 80 BELOW I: 6 YEORFULL BULK) PASSENGER CABIN FLOOR.A340-600INSTALLED: 161 MQ NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3NOTE 1 FOR THE COMPLETE AREA AND ADDITIONAL TPS TYPE IIBELOW STR 40, LH/RH.534230-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE CPCP ZL-200-01-2 A340-500EXTERNAL SURFACE AROUND DOOR 4 (AFT PASSENGER/ I: 6 YEORCREW DOOR) CUT-OUT BETWEEN FR 73 AND FR 76,A340-600FROM STR 9 TO STR 26 LH/RH.534232-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT T: 12 YE CPCP A340-500SCUFF PLATE 200 PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH I: 6 YEORSCUFF PLATE LH/RH.A340-600534233-01-1 833 843 271 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-500INSULATION 272 AROUND DOOR 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT I: 6 YEORLINING 273 BETWEEN FR 73 AND FR 76 FROM PASSENGER CABIN FLOORA340-600274 TO STR 9, LH/RH534234-01-1 161AZ 823 171 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-500IF LDF (PARTIAL OR 172 BELOW DOOR 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT I: 6 YEORFULL BULK) BETWEEN FR 73 AND FR 76 FROM PASSENGER CABIN FLOORA340-600INSTALLED: 161 MQ TO STR 43, LH/RHINSULATION534238-01-1 822 152 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-500INSULATION AROUND AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEORLINING FR 59 AND FR 66, FROM STR 26 TO CARGO COMPARTMENTA340-600FLOOR, RH.534239-01-1 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1 CPCP A340-500DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES I: 6 YEOR(FR 59A AND FR 65).A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 72APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534239-01-2 N/A TASK DELETED534240-01-1 822 152 GENERAL VISUAL INSPECTION OF LOCK FITTINGS AND BUSHES T: 6 YE 1+2 CPCP A340-500154 FOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS I: 6 YEORBETWEEN FR 59A AND FR 65A340-600534240-01-2 N/A TASK DELETED534240-02-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO T: 6 YE T: 20 YE CPCP A340-500ECCENTRIC BOLTS 154 COMPARTMENT DOOR AT 10 POSITIONS BETWEEN I: 6 YE I: 6 YEORFR 59A AND FR 65A340-600534244-01-1 823 100 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR T: 12 YE CPCP A340-500SCUFF PLATE CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. I: 6 YEPRE 49205PRE 49288ORA340-600PRE 49205PRE 49288534245-01-1 823 162 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-500CARGO COMPARTMENT 164 AROUND BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEPRE 49205FLOOR PANELS FR 66 AND FR 70 FROM STR 31 TO STR 48, RH.PRE 49288IF LDF (FULL BULK) NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3 FORORINSTALLED: LDF THE COMPLETE AREA AND ADDITIONAL TPS TYPE II BELOWA340-600FURNISHING AND STR 40.PRE 49205EQUIPMENTPRE 49288INSULATIONLININGISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 73APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534246-01-1 823 162 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS OF T: 6 YE 1+2 CPCP A340-500BULK CARGO COMPARTMENT DOOR, AT 10 POSITIONS I: 6 YEPRE 49205AT FR 67 AND FR 69.PRE 49288ORA340-600PRE 49205PRE 49288534246-01-2 N/A TASK DELETED534249-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO T: 6 YE 1 CPCP A340-500COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL I: 6 YEPRE 49205FRAMES (FR 67 AND FR 69).PRE 49288ORA340-600PRE 49205PRE 49288534249-01-2 N/A TASK DELETED534256-01-1 822 154 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-500BALLMATS BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEORFR 59 AND FR 66, FROM CARGO COMPARTMENT FLOOR TOA340-600STR 47, RH.534257-01-1 833 843 261 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE CPCP ZL-261-02-2 A340-500FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILTETS I: 12 YEZL-271-02-2 POST 47021271 AND DOOR ENTRANCE AREAS FROM FR 53.7 TO FR 80.272534257-02-1 833 843 261 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE CPCP ZL-261-02-2 A340-500FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YEZL-271-02-2 POST 47968271 AND DOOR ENTRANCE AREAS FROM FR 53.9 TO FR 80.272ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 74APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534257-03-1 833 843 251 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE CPCP ZL-251-02-3 A340-600FLOOR PANELS 252 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YEZL-261-02-3261 AND DOOR ENTRANCE AREAS FROM FR 53.2 TO FR 80.ZL-271-02-2262271272534258-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1 CPCP A340-500ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YEPOST 47021CARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 53.7 TO FR 73.LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFTLDF FURNISHING AND 171 OF FR 68, LH/RH.EQUIPMENT (IF 172INSTALLED)LDMCR (IF INSTALLED)NOTE 1534258-02-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1 CPCP A340-500ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YEPOST 47968CARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 63.9 TO FR 73.LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFTLDF FURNISHING AND 171 OF FR 68, LH/RH.EQUIPMENT (IF 172INSTALLED)LDMCR (IF INSTALLED)NOTE 1534258-03-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1 CPCP A340-600ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YECARGO COMPARTMENT 161 COMPARTMENT FLOOR FROM FR 53.2 TO FR 73.LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFTLDF FURNISHING AND 171 OF FR 68, LH/RH.EQUIPMENT (IF 172INSTALLED)LDMCR (IF INSTALLED)NOTE 1ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 75APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534259-01-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2 CPCP A340-600833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YENOTECARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.2CEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 251 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 252 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATEDINSTALLED: LDF 261FURNISHINGAND 262EQUIPMENT 271272534259-01-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2 CPCP A340-600833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YENOTECARGO COMPARTMENT 161 TOILETS, INCLUDINM DOOR ENTRANCE AREAS, FROM FR 53.2CEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 251 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 252 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATEDINSTALLED: LDF 261FURNISHINGAND 262EQUIPMENT 271272534259-02-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2 CPCP A340-500833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YEPOST 47021CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.7NOTECEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATEDINSTALLED: LDF 271FURNISHINGAND 272EQUIPMENTISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 76APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534259-02-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2 CPCP A340-500833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YEPOST 47021CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTANCE AREAS, FROM FR 53.7NOTECEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATEDINSTALLED: LDF 271FURNISHINGAND 272EQUIPMENT534259-03-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2 CPCP A340-500833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YEPOST 47968CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.9NOTECEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATEDINSTALLED: LDF 271FURNISHINGAND 272EQUIPMENT534259-03-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2 CPCP A340-500833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YEPOST 47968CARGO COMPARTMENT 161 TOILETS, INCLUDING DOORENTRANCE AREAS, FROM FR 53.9NOTECEILING PANELS 162 TO FR 80.FLOOR PANELS 171GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREIF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDFULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATEDINSTALLED: LDF 271FURNISHINGAND 272EQUIPMENT534260-01-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-263-01-2 A340-500CEILING PANELS 264 STRUCTURE BETWEEN FR 53.4 AND FR 80, FROM STR 15 TO I: 12 YEZL-273-01-2NOTE 1 273 CROWN CENTER LINE, LH/RH.OVERHEAD STOWAGE 274BINSISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 77APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534260-02-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-263-01-3 A340-600CEILING PANELS 264 STRUCTURE BETWEEN FR 56.1 AND FR 80, FROM STR 15 TO I: 12 YEZL-273-01-3NOTE 1 273 CROWN CENTER LINE, LH/RH.OVERHEAD STOWAGE 274BINS534261-01-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-261-02-2 A340-500NOTE 1 262 STRUCTURE BETWEEN FR 53.4 AND FR 80, FROM STR 15 I: 12 YEZL-271-02-2SIDEWALL LINING 271 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO PASSENGER272 CABIN FLOOR, LH/RH.R 534261-02-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-261-02-3 A340-600NOTE 1 262 INTERNAL STRUCTURE BETWEEN FR 56.1 AND FR 80, FROM I: 12 YEZL-271-02-2SIDEWALL LINING 271 STR 15 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO272 PASSENGER CABIN FLOOR, LH/RH.534262-01-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2 CPCP A340-600ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YENOTEIF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWDFULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FRINSTALLED: LDF 171 53.2 TO FR 80, LH/RHFURNISHINGAND 172EQUIPMENT NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS AREINSULATION FITTED ABOVE THE AREALDMCR (IF INSTALLED)LINING534262-02-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YEPOST 47021IF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWDNOTEFULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FRINSTALLED: LDF 171 53.7 TOFURNISHINGAND 172 FR 80, LH/RH (WITH RCT, 5 FRAME BAYS)EQUIPMENTINSULATION NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARELDMCR (IF INSTALLED) FITTED ABOVE THE AREALININGISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 78APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS534262-03-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2 CPCP A340-500ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YEPOST 47968IF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWDNOTEFULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FRINSTALLED: LDF 171 53.9 TOFURNISHINGAND 172 FR 80, LH/RH (WITH RCT, 7 FRAME BAYS)EQUIPMENTINSULATION NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARELDMCR (IF INSTALLED) FITTED ABOVE THE AREALINING534267-01-1 833 843 261 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A340-600INSULATION 262 AROUND DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YELINING CUT-OUT, BETWEEN FR 56 AND FR 56.4 FROM PASSENGERCABIN FLOOR TO STR 9, LH/RH.534268-01-1 822 151 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1 CPCP A340-600ACT (IF INSTALLED) 152 BELOW DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YECARGO COMPARTMENT CUT-OUT, BETWEEN FR 56 AND FR 56.4 FROM PASSENGERINSULATION CABIN FLOOR CARGO COMPARTMENT FLOOR, LH/RH.LDF FURNISHING ANDEQUIPMENT (IFINSTALLED)LDMCR (IF INSTALLED)LINING534270-01-1 N/A 200 GENERAL VISUAL INSPECTION OF T: 6 YE CPCP ZL-200-01-2 A340-600FUSELAGE SKIN EXTERNAL SURFACE AROUND DOOR 3 I: 6 YE(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTBETWEEN FR 56 AND FR 56.4, FROM STR 9 TO STR 26,LH/RH.534272-01-1 834 844 100 DETAILED INSPECTION OF DOOR 3 T: 12 YE CPCP A340-600SCUFF PLATE 200 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, I: 6 YESTRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.N 534277-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE CPCP ZL-200-01-2 A340-500FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER I: 3 YEORLINE, EXCLUDING AREA UNDER VERTICAL STABILIZERA340-600FAIRING, EXTERNAL SURFACE.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 79APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 535101-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE T: 20 YE CPCP A340-200INSULATION 272 FACE ABOVE MAIN DECK FLOOR LEVEL INCLUDING FR 80/82, I: 12 YE I: 12 YEPRE 48980TOILETS AND GALLEYS RIM ANGLE AND ATTACHMENT TO SKIN.ORA340-300PRE 48980R 535102-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE T: 6 YE 1+2 CPCP A340-200172 BULKHEAD FWD FACE BELOW MAIN DECK FLOOR LEVEL I: 6 YEPRE 48980INCLUDING FR 80/82, RIM ANGLE ATTACHMENT ANDORATTACHMENT TO SKINA340-300PRE 48980R 535103-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE T: 20 YE CPCP A340-200312 FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 I: 12 YE I: 12 YEPRE 48980LH/RH AND CROWN CENTERLINE.ORA340-300PRE 48980535103-01-2 N/A TASK DELETED535103-02-1 N/A TASK DELETEDR 535104-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE T: 6 YE 1+2 CPCP A340-200312 BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN I: 6 YEPRE 48980BETWEEN STR 26 LH/RH, AND BOTTOM CENTER LINEORA340-300PRE 48980535104-02-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 80APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS535105-01-1 N/A TASK DELETED535106-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1 CPCP A340-200CEILING PANELS 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YEORNOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWNA340-300TOILETS AND GALLEYS CENTERLINE AND AT FR 79 AND FR 80.535107-01-1 312AR 311 DETAILED INSPECTION OF FIN TO FUSELAGE MID T: 12 YE 1 CPCP A340-200312 AND AFT ATTACH FITTINGS IN AREA OF ATTACHMENTS TO I: 6 YEORFUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RHA340-300TO CROWN CENTER LINE AND AT FR 84, 85, 86 AND 87.535108-01-1 N/A TASK DELETED535109-01-1 N/A TASK DELETED535110-01-1 312AR 311 DETAILED INSPECTION OF ATTACH FITTINGS FOR T: 12 YE T: 20 YE CPCP A340-200312 HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 86 I: 12 YE I: 12 YEORAND FR 87.A340-300R 535111-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE CPCP ZL-300-01-1 A340-200CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YEPRE 44205FROM FR 84 TO FR 85 AND BETWEEN STR 27 RH ANDORSTR 39 RH, EXTERNAL SURFACE.A340-300PRE 44205535111-02-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE CPCP ZL-300-01-1 A340-200CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YEPOST 44205FROM FR 84 TO FR 85 AND BETWEEN STR 27 RH ANDORSTR 39 RH, EXTERNAL SURFACE.A340-300POST 44205ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 81APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS535112-01-1 N/A TASK DELETED535113-01-1 N/A TASK DELETED535114-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM T: 12 YE CPCP ZL-300-01-1 A340-200FR 80/82 TO FR 101 FROM CROWN TO BOTTOM CENTER LINE, I: 12 YEOREXTERNAL SURFACE, AS FAR AS VISIBLE, LH/RH.A340-300535115-01-1 N/A TASK DELETED535116-01-1 321AL 323AL 323AR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 1 CPCP A340-200323BL 323BR 323 SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN I: 6 YEORTO FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOADA340-300FITTINGS535117-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF REAR FUSELAGE INTERNAL T: 6 YE 1 CPCP A340-200312 STRUCTURE BETWEEN FR 80/82 AND FR 95 FROM CROWN TO I: 6 YEOR313 BOTTOM CENTER LINE, LH/RHA340-300314 NOTE: APPLY AFTER INSPECTION TYPE 1 GRADE 2 OR 3TEMPORARY PROTECTION SYSTEM FROM FR 80/82TO FR 91 BELOW STR 25 LH/RH, FROM FR 92 TO FR 95BELOW STR 13 LH/RH AND IN AREA BETWEEN FR 86 ANDFR 88 BELOW STR 15535118-01-1 312AR 313AL 311 DETAILED INSPECTION OF REAR FUSELAGE INTERNAL T: 12 YE T: 20 YE CPCP A340-200312 STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT BETWEEN I: 6 YE I: 6 YEORFR 86 AND FR 91 FROM STR 15 TO STR 30 AND FR 91A340-300ASSEMBLY FROM CROWN TO BOTTOM CENTER LINE INCLUDINGTAIL CONE ATTACHMENT FITTINGS, LH/RH.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 82APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 535121-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YEZL-271-02-1 A340-300GALLEYS AND TOILETS 272 FWD FACE ABOVE MAIN DECK FLOOR LEVEL. I: 12 YEZL-273-01-1 POST 48980(IF INSTALLED) 273NOTE 1 274R 535122-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YEZL-171-02-1 A340-300IF LDF (PARTIAL OR 172 FWD FACE BELOW MAIN DECK FLOOR LEVEL I: 6 YEPOST 48980FULL BULK)INSTALLED: 833 843161AZR 535123-01-1 312AR 311 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YEZL-311-01-1 A340-300312 AFT FACE FROM CROWN TO BOTTOM CENTER LINE. I: 12 YEPOST 48980R 535124-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2 CPCP A340-300312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 6 YEPOST 48980BOTTOM CENTER LINER 535129-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE CPCP A340-300GALLEYS AND TOILETS 272 FACE ATTACHMENT TO RIM ANGLE, ABOVE MAIN DECK FLOOR I: 12 YEPOST 48980(IF INSTALLED) 273 LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.NOTE 1 274R 535130-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2 CPCP A340-300IF LDF (PARTIAL OR 172 FACE ATTACHMENT TO RIM ANGLE, BELOW MAIN DECK FLOOR I: 6 YEPOST 48980FULL BULK) LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKININSTALLED: 833 843161AZR 535131-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE CPCP A340-300312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 12 YEPOST 48980CROWN CENTER LINER 535201-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE T: 12 YEA340-500NOTE 1 272 BULKHEAD FWD FACE ABOVE CABIN FLOOR LEVEL I: 12 YEORTOILETS AND GALLEYSA340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 83APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS535202-01-1 161AZ 822 171 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YEZL-171-02-2 A340-500IF LDF (PARTIAL OR 172 FWD FACE BELOW CABIN FLOOR LEVEL I: 6 YEZL-171-02-3 ORFULL BULK)A340-600INSTALLED: 833 843161AZR 535203-01-1 312AR 311 GENERAL VISUAL INSPECTION OF REAR PRESSURE T: 12 YEA340-500312 BULKHEAD AFT FACE FROM CROWN TO BOTTOM CENTER LINE I: 12 YEORA340-600535204-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2 CPCP A340-500312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 6 YEORBOTTOM CENTER LINE.A340-600535206-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1 CPCP A340-500CEILING PANELS 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YEORNOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWNA340-600TOILETS AND GALLEYS CENTERLINE AND TO FR 79 AND FR 80.535207-01-1 312AR 311 DETAILED INSPECTION OF FIN TO FUSELAGE MID T: 12 YE 1 CPCP A340-500312 AND AFT ATTACH FITTINGS IN AREA OF ATTACHMENTS TO I: 6 YEORFUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RHA340-600TO CROWN CENTER LINE AND AT FR 84, 85, 86 AND 87.535210-01-1 312AR 311 DETAILED INSPECTION OF ATTACH FITTINGS FOR T: 12 YE T: 20 YE CPCP A340-500312 HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 85 I: 12 YE I: 12 YEORAND FR 86.A340-600535211-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE CPCP ZL-300-01-2 A340-500CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YEORBETWEEN FR 84 AND FR 85 AND BETWEEN STR 27 RH ANDA340-60037 RH, EXTERNAL SURFACE.535214-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM FR 80 T: 12 YE CPCP ZL-300-01-2 A340-500TO FR 100 FROM CROWN TO BOTTOM CENTER LINE, EXTERNAL I: 12 YEORSURFACE, AS FAR AS VISIBLE, LH/RH.A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 84APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS535216-01-1 321AL 323DL 323DR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 1 CPCP A340-500323EL 323ER 325LL 323 SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN I: 6 YEOR325LR TO FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOADA340-600FITTINGS535217-01-1 312AR 313BL 311 GENERAL VISUAL INSPECTION OF T: 6 YE 1+2 CPCP A340-500312 REAR FUSELAGE INTERNAL STRUCTURE BETWEEN FR 80 I: 6 YEOR313 AND FR 95 FROM CROWN TO BOTTOM CENTER LINE, LH/RHA340-600314 NOTE: TPS TYPE I + TYPE II APPLICATION IS FROM FR 80TO FR 91 BELOW STRINGER 25 LH / RH, FROM FR 91TO FR 95 BELOW STRINGER 11 LH / RH, AND TPS TYPE I,GRADE 2 OR 3 APPLICATION IN AREA BETWEEN FR 86AND FR 88 BETWEEN STRINGER 15 AND 25, LH/RH.535218-01-1 312AR 313BL 311 DETAILED INSPECTION OF REAR FUSELAGE INTERNAL T: 12 YE T: 20 YE CPCP A340-500312 STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT LH/RH I: 6 YE I: 6 YEORBETWEEN FR 86 AND FR 91 FROM STR 15 TO STR 30, ANDA340-600AND FR 91 ASSEMBLY FROM CROWN TO BOTTOM CENTER LINEINCLUDING TAIL CONE ATTACHMENT FITTINGS.R 535219-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE CPCP A340-500NOTE 1 272 FACE ATTACHMENT TO RIM ANGLE, ABOVE CABIN FLOOR I: 12 YEORTOILETS AND GALLEYS 273 LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.A340-600274R 535220-01-1 161AZ 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2 CPCP A340-500IF LDF (PARTIAL OR 172 FACE ATTACHMENT TO RIM ANGLE, BELOW CABIN FLOOR I: 6 YEORFULL BULK) LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.A340-600INSTALLED: 833 843161AZR 535221-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE CPCP A340-500312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 12 YEORCROWN CENTER LINE.A340-600ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 85APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS535222-01-1 311BL 311CL 311DL 311 DETAILED INSPECTION OF REAR FUSELAGE SKIN EXTERNAL T: 10 YE 1+2 CPCP A340-500311EL 311FL 312BR 312 SURFACE UNDERNEATH THS-FAIRING, INCLUDING FAIRING I: 10 YEOR312CR 312DR 312ER BRACKETS.A340-600312FR 331AT 333AB333AT 341AT 343AB343AT535223-01-1 312AR 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 10 YEA340-500312 SUPPORT MEMBERS. I: 10 YEORA340-600* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 86APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545101-01-1 N/A TASK DELETED545102-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE T: 12 YE NO CPCP A340-200463 ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT I: 12 YEOR473 MOUNT FITTING.A340-300483545103-01-1 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON T: 13000 FCGROUP 42A463 PYRAMID, END OF ARMS AT ENGINE FORWARD MOUNT OROR473 FITTING. 60000 FHGROUP 43A483 I: 13000 FCORORGROUP 42B60000 FHORGROUP 43B545103-01-3 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON T: 13000 FCGROUP 43C463 PYRAMID, END OF ARMS AT ENGINE FORWARD MOUNT OR473 FITTING. 26000 FH483 I: 13000 FCOR26000 FH545103-01-4 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID,END OF T: 13000 FCGROUP 43EREMOVAL 463 ARMS AT ENGINE FORWARD MOUNT FITTING OR473 65000 FH483 I: 13000 FCOR65000 FH545104-01-1 N/A TASK DELETED545104-01-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545104-01-6 N/A TASK DELETEDR 545104-01-7 415AL 416AR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 13000 FCGROUP 43B418AR 425AL 426AR 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN ORPOST 49203427AL 428AR 435AL 473 RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 60000 FH436AR 437AL 438AR 483 I: 4100 FC445AL 446AR 447AL OR448AR 27600 FHR 545104-01-8 415AL 416AR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 13000 FCGROUP 43E418AR 425AL 426AR 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN OR427AL 428AR 435AL 473 RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 65000 FH436AR 437AL 438AR 483 I: 4100 FC445AL 446AR 447AL OR448AR 27600 FH545108-01-1 N/A TASK DELETED545110-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT T: 12 YE NO CPCP A340-200418AR 425AL 426AR 463 ATTACHMENT BEAM AT RIB 3. I: 12 YEOR427AL 428AR 435AL 473A340-300436AR 437AL 438AR 483445AL 446AR 447AL448AR545112-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-200453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300473AR 473BL 473BR 483 TIME AS TASK 545112-02-1483AL 483AR 483BL483BRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545112-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-200453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300473AR 473BL 473BR 483 TIME AS TASK 545112-01-1483AL 483AR 483BL483BR545116-01-1 453CL 453CR 463CL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-200463CR 473CL 473CR 463 UPPER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YEOR483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300483 TIME AS TASK 545116-02-1545116-02-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-200463CR 473CL 473CR 463 UPPER SURFACE, BETWEEN RIB 8 AND RIB 11. I: 12 YE I: 12 YEOR483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300483 TIME AS TASK 545116-01-1545118-01-1 414 415AL 416AR 453 DETAILED INSPECTION OF PYLON LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-200417AL 418AR 424 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 14. I: 12 YE I: 12 YEOR425AL 426AR 427AL 473A340-300428AR 434 435AL 483436AR 437AL 438AR444 445AL 446AR447AL 448AR 454CL464CL 474CL 484CL545121-01-1 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE NO CPCP A340-200452DR 452EL 462AL 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YEPRE 41371462AR 462CL 462CR 473OR462DL 462FR 472AL 483A340-300472AR 472CL 472CRPRE 41371472ER 472FL 482AL482AR 482CR 482DL482ERISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545121-01-2 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A340-200452DR 452GL 462AL 463 SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YEPOST 41371462AR 462CL 462CR 473AND462GL 462HR 472AL 483PRE 42283472AR 472CL 472CROR472HL 472JR 482ALA340-300482AR 482CR 482GLPOST 41371482HRANDPRE 42283545121-01-3 452FL 452JL 452JR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A340-200452KL 452KR 462AL 463 SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YEPOST 42283462AR 462CL 462CR 473OR462DL 462FR 472AL 483A340-300472AR 472CL 472CRPOST 42283472ER 472FL 482JL482JR 482KR 482ML482MR545124-01-1 452DR 452EL 452FR 453 DETAILED INSPECTION OF PYLON UPPER SPAR T: 12 YE NO CPCP A340-200454AL 454AR 462DL 463 UPPER SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YEPRE 41371462FR 462GR 462HL 473OR464AL 464AR 472ER 483A340-300472FL 472GL 472HRPRE 41371474AL 474AR 482DL482ER 482FL 484AL484AR545124-01-2 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO CPCP A340-200454AL 454AR 462GL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YEPOST 41371462GR 462HL 462HR 473AND464AL 464AR 472GL 483PRE 42283472HL 472HR 472JRAND474AL 474AR 482FLPRE 43183482GL 482HR 484ALOR484ARA340-300POST 41371ANDPRE 42283ANDPRE 43183ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545124-01-3 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO CPCP A340-200454AL 454AR 462DL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YEPOST 41371462FR 462GR 462HL 473AND464AL 464MR 472ER 483PRE 42283472FL 472GL 472HRAND474AL 474AR 482FLPOST 43183482GL 482HR 484ALOR484ARA340-300POST 41371ANDPRE 42283ANDPOST 43183545124-01-4 452KL 452KR 452MR 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO CPCP A340-200454AL 454KR 462DL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YEPOST 42283462FR 462GR 462HL 473OR464AL 464AR 472ER 483A340-300472FL 472GL 472HRPOST 42283474AL 474MR 482ML482MR 482NL 484ML484MR545126-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-200464BR 474BL 474BR 463 UPPER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YEPRE 43183484BL 484BR 473OR483A340-300PRE 43183545126-01-2 454BL 454BR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-200464KR 474KL 474KR 463 SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YEPOST 43183484BL 484BR 473AND483PRE 42283ORA340-300POST 43183ANDPRE 42283ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545126-01-3 454BL 454MR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-200464KR 474KL 474KR 463 SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YEPOST 42283484NL 484NR 473OR483A340-300POST 42283545130-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-200453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300473AR 473BL 473BR 483 TIME AS TASK 545130-02-1483AL 483AR 483BL483BR545130-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-200453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300473AR 473BL 473BR 483 TIME AS TASK 545130-01-1483AL 483AR 483BL483BR545131-01-1 453CL 453CR 463CL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-200463CR 473CL 473CR 463 LOWER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YEOR483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300483 TIME AS TASK 545131-02-1545131-02-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-200463CR 473CL 473CR 463 LOWER SURFACE, BETWEEN RIB 8 AND RIB 11. I: 12 YE I: 12 YEOR483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAMEA340-300483 TIME AS TASK 545131-01-1545139-01-1 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 42AAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORORDOORS (6 ACCESS DOORS PER PYLON). 60000 FHGROUP 43AI: 5110 FCOR35400 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545139-01-2 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 42BAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORORDOORS (6 ACCESS DOORS PER PYLON). 60000 FHGROUP 43BI: 4130 FCOR28600 FH545139-01-4 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43CAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORDOORS (6 ACCESS DOORS PER PYLON). 26000 FHI: 6000 FCOR12000 FH545139-01-5 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43EAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORPRE 48769DOORS (6 ACCESS DOORS PER PYLON). 65000 FHI: 4190 FCOR28300 FH545139-01-6 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43EAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORPOST 48769DOORS (6 ACCESS DOORS PER PYLON). 65000 FHI: 2330 FCNOTE: THIS TASK IS AN ALTERNATIVE TO ORTASK 545139-02-1 15700 FH545139-02-1 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43EAREAS OF FASTENERS SECURING SUPPORTS OF ACCESS ORPOST 48769DOORS (6 ACCESS DOORS PER PYLON). 65000 FHI: 13000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO ORTASK 545139-01-6 65000 FH545142-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545142-01-2 N/A TASK DELETED545143-01-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF T: 13000 FCGROUP 42A453BR 463AL 463AR 463 ACCESS DOOR CUTOUTS AND MATING SURFACES, RIB 3 AND OROR463BL 463BR 473AL 473 RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B PYLON) AND 60000 FHGROUP 43A473AR 473BL 473BR 483 BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 6000 FCOR483AL 483AR 483BL ORGROUP 42B483BR 41600 FHORGROUP 43B545143-01-2 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43C453BR 463AL 463AR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACES, OR463BL 463BR 473AL 473 RIB 3 AND RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B 26000 FH473AR 473BL 473BR 483 PYLON) AND BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 6000 FC483AL 483AR 483BL OR483BR 12000 FH545143-01-3 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FCGROUP 43E453BR 463AL 463AR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACES, OR463BL 463BR 473AL 473 RIB 3 AND RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B 65000 FH473AR 473BL 473BR 483 PYLON) AND BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 13000 FC483AL 483AR 483BL OR483BR 65000 FHD 545146-01-1 N/A TASK DELETEDD 545146-01-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 8APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545146-01-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON LOWER SPAR AND T: 13000 FCGROUP 43E418AR 425AL 426AR 463 LATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4. OR427AL 428AR 435AL 473 65000 FH436AR 437AL 438AR 483 I: 10300 FC445AL 446AR 447AL OR448AR 453AL 453AR 65000 FH463AL 463AR 473AL473AR 483AL 483AR545150-01-1 452CL 452DR 452EL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 42A452FR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. ORPRE 41371462DL 462FR 462GR 473 60000 FHOR462HL 472CL 472CR 483 I: 2470 FCGROUP 43A472ER 472FL 472GL ORPRE 41371472HR 482CR 482DL 16900 FH482ER 482FL545150-01-2 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 42B452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OROR462GL 462HL 462HR 473 60000 FHGROUP 43B462JR 472CL 472CR 483 I: 2180 FC472GL 472HL 472HR OR472JR 482CR 482FL 14900 FH482GL 482HR545150-01-3 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 43C452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR462GL 462HL 462HR 473 26000 FH462JR 472CL 472CR 483 I: 3250 FC472GL 472HL 472HR OR472JR 482CR 482FL 6500 FH482GL 482HRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 9APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545150-01-4 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 43E452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR462GL 462HL 462HR 473 65000 FH462JR 472CL 472CR 483 I: 3180 FC472GL 472HL 472HR OR472JR 482CR 482FL 21500 FH482GL 482HR545150-01-5 452CL 452DR 452FR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 42A452GL 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. ORPOST 41371462GL 462GR 462HL 473 60000 FHAND462HR 472CL 472CR 483 I: 2470 FCPRE 42283472GL 472HL 472HR OROR472JR 482CR 482FL 16900 FHGROUP 43A482GL 482HRPOST 41371ANDPRE 42283545150-01-6 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FCGROUP 42A452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. ORPOST 42283462GL 462HL 462HR 473 60000 FHOR462JR 472CL 472CR 483 I: 2470 FCGROUP 43A472GL 472HL 472HR ORPOST 42283472JR 482CR 482FL 16900 FH482GL 482HR545166-01-1 N/A TASK DELETED545166-01-2 N/A TASK DELETED545168-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 10APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545168-01-2 N/A TASK DELETED545170-01-1 452DR 452EL 452FR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A340-200462DL 462FR 462GR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YEPRE 41371472ER 472FL 472GL 473 PER PYLON).OR482DL 482ER 482FL 483A340-300BOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUTPRE 41371ENGINE REMOVAL AS FAR AS VISIBLELINKSSLEEVES545170-01-2 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A340-200462GL 462GR 462HR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YEPOST 41371472GL 472HL 472JR 473 PER PYLON).PRE 42283482FL 482GL 482HR 483ORBOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUTA340-300ENGINE REMOVAL AS FAR AS VISIBLEPOST 41371LINKSPRE 42283SLEEVES545170-01-3 452KL 452KR 452MR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A340-200462DL 462FR 462GR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YEPOST 42283472ER 472FL 472GL 473 PER PYLON).OR482ML 482MR 482NL 483A340-300BOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUTPOST 42283ENGINE REMOVAL AS FAR AS VISIBLELINKSSLEEVESD 545174-01-1 N/A TASK DELETEDD 545174-01-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 11APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545174-01-3 454BL 454MR 464KL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 13000 FCGROUP 43E464KR 474KL 474KR 463 FITTING LUG AND LINKS AT RIB 14. OR484NL 484NR 473 65000 FH483 I: 13000 FCOR65000 FHD 545174-01-4 N/A TASK DELETEDD 545174-01-5 N/A TASK DELETED545180-01-1 454FL 454FR 464FL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE CPCP A340-200464FR 474FL 474FR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YEPRE 43183484FL 484FR 473 PYLON).ORBOLTS 483A340-300ENGINEPRE 43183LINKSSLEEVES545180-01-2 454FL 454FR 464JL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE CPCP A340-200464JR 474JL 474JR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YEPOST 43183484FL 484FR 473 PYLON).ANDBOLTS 483PRE 42283ENGINEORLINKSA340-300SLEEVESPOST 43183ANDPRE 42283545180-01-3 454NR 454QL 464JL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE CPCP A340-200464JR 474JL 474JR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YEPOST 42283484PL 484PR 473 PYLON).ORENGINE 483A340-300LINKSPOST 42283ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 12APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545180-02-1 N/A TASK DELETED545180-02-2 454NR 454QL 464JL 453 SPECIAL DETAILED INSPECTION OF PYLON TO WING T: 13000 FCGROUP 43C464JR 474JL 474JR 463 ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 OR484PL 484PR 473 PLACES PER PYLON). 26000 FHBOLTS 483 I: 13000 FCENGINE ORLINKS 26000 FHSLEEVES545182-01-1 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FCGROUP 42A453CR 463BL 463BR 463 8 WEB CUT-OUT. OROR463CL 463CR 473BL 473 60000 FHGROUP 43A473BR 473CL 473CR 483 I: 6000 FCOR483BL 483BR 483CL ORGROUP 42B483CR 42200 FHORGROUP 43B545182-01-2 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FCGROUP 43C453CR 463BL 463BR 463 8 WEB CUT-OUT. OR463CL 463CR 473BL 473 65000 FH473BR 473CL 473CR 483 I: 6000 FC483BL 483BR 483CL OR483CR 12000 FH545182-01-3 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FCGROUP 43E453CR 463BL 463BR 463 8 WEB CUT-OUT. OR463CL 463CR 473BL 473 65000 FH473BR 473CL 473CR 483 I: 13000 FC483BL 483BR 483CL OR483CR 65000 FH545701-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 13APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545705-01-1 N/A TASK DELETED545721-01-1 N/A TASK DELETED545721-01-2 N/A TASK DELETED545725-01-1 N/A TASK DELETED545725-01-2 N/A TASK DELETED545801-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO CPCP A340-500463 THE ENGINE FORWARD MOUNT FITTING. I: 12 YEOR473A340-600483545801-02-1 N/A TASK DELETED545802-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO CPCP A340-500463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING. I: 12 YEOR473A340-600483545802-01-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 14APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545808-01-1 N/A TASK DELETED545810-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT T: 12 YE NO CPCP A340-500418AR 425AL 426AR 463 ATTACHMENT BEAM AT RIB 6. I: 12 YEOR427AL 428AR 435AL 473A340-600436AR 437AL 438AR 483445AL 446AR 447AL448AR545810-01-2 N/A TASK DELETED545812-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473A340-600473AR 473BL 473BR 483 NOTE:483AL 483AR 483BL - THIS TASK IS AN ALTERNATIVE TO TASK 545812-02-01.483BR - THIS TASK MUST BE PERFORMED AT THE SAME TIME ASTASK 545812-03-1.545812-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473A340-600473AR 473BL 473BR 483 NOTE:483AL 483AR 483BL - THIS TASK IS AN ALTERNATIVE TO TASK 545812-01-1.483BR - THIS TASK MUST BE PERFORMED AT THE SAME TIMEENGINE AS TASK 545812-03-1.THRUST REVERSERDEPLOYED545812-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA340-600473AR 473BL 473BR 483 TASKS 545812-01-1 OR 545812-02-1.483AL 483AR 483BL483BRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 15APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545816-01-1 453CL 453CR 453DL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500453DR 463CL 463CR 463 SURFACE, BETWEEN RIB 8 AND RIB 14. I: 12 YE I: 12 YEOR463DL 463DR 473CL 473A340-600473CR 473DL 473DR 483483CL 483CR 483DL483DR545818-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON LOWER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A340-500416AR 417AL 418AR 463 SURFACE, BETWEEN RIB 1 AND RIB 14. I: 12 YE I: 12 YEOR424AL 424AR 425AL 473A340-600426AR 427AL 428AR 483434AL 434AR 435AL436AR 437AL 438AR444AL 444AR 445AL446AR 447AL 448AR452FR 452HL 462FR462HL 472FR 472HL482FR 482HL545821-01-1 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500452DR 462AL 462AR 463 SURFACE, BETWEEN RIB 1 AND RIB 6. I: 12 YE I: 12 YEOR462CL 462CR 462DL 473A340-600472AR 472BL 472CL 483472CR 472DL 482AR482BL 482CR 482DL545824-01-1 452CR 452EL 452GR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500452KL 454AL 454AR 463 SURFACE, BETWEEN RIB 6 AND RIB 9. I: 12 YE I: 12 YEOR462CR 462DL 462EL 473A340-600462GR 462JL 464AL 483464AR 472ER 472FL472GL 472HR 474AL474AR 482CR 482EL482GR 482JL 484AL484AR545826-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A340-500464BR 474BL 474BR 463 SURFACE, BETWEEN RIB 9 AND RIB 14. I: 12 YE I: 12 YEOR484BL 484BR 473A340-600483ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 16APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545830-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473A340-600473AR 473BL 473BR 483 NOTE:483AL 483AR 483BL - THIS TASK IS AN ALTERNATIVE TO TASK 545830-02-1.483BR - THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 545830-03-1.545830-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473A340-600473AR 473BL 473BR 483 NOTE:483AL 483AR 483BL - THIS TASK IS AN ALTERNATIVE TO TASK 545830-01-1.483BR - THIS TASK MUST BE PERFORMED AT THE SAME TIMEENGINE AS TASK 545830-03-1.THRUST REVERSERDEPLOYED545830-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A340-500453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YEOR463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA340-600473AR 473BL 473BR 483 TASKS 545830-01-1 OR 545830-02-1.483AL 483AR 483BL483BR545831-01-1 453CL 453CR 453DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A340-500453DR 463CL 463CR 463 SURFACE, BETWEEN RIB 8 AND RIB 14. I: 12 YE I: 12 YEOR463DL 463DR 473CL 473A340-600473CR 473DL 473DR 483483CL 483CR 483DL483DR545833-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 12 YE T: 20 YE NO CPCP A340-500453BR 453CL 453CR 463 INTERNAL SURFACE, FROM RIB 1 TO RIB 3. I: 12 YE I: 12 YEOR463AL 463AR 463BL 473A340-600463BR 463CL 463CR 483 NOTE:473AL 473AR 473BL - THIS TASK IS AN ALTERNATIVE TO TASK 545833-02-1.473BR 473CL 473CR - THIS TASK MUST BE PERFORMED AT THE SAME TIME483AL 483AR 483BL AS TASK 545833-03-1.483BR 483CL 483CRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 17APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545833-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, INTERNAL T: 12 YE T: 20 YE NO CPCP A340-500453BR 453CL 453CR 463 SURFACE, FROM RIB 1 TO RIB 3. I: 12 YE I: 12 YEOR463AL 463AR 463BL 473A340-600463BR 463CL 463CR 483 NOTE:473AL 473AR 473BL - THIS TASK IS AN ALTERNATIVE TO TASK 545833-01-1.473BR 473CL 473CR - THIS TASK MUST BE PERFORMED AT THE SAME TIME483AL 483AR 483BL AS TASK 545833-03-1.483BR 483CL 483CRENGINETHRUST REVERSERDEPLOYED545833-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, INTERNAL T: 12 YE T: 20 YE NO CPCP A340-500453BR 453CL 453CR 463 SURFACE, FROM RIB 3 TO RIB 14. I: 12 YE I: 12 YEOR463AL 463AR 463BL 473A340-600463BR 463CL 463CR 483 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME473AL 473AR 473BL AS TASK 545833-01-1 OR 545833-02-1.473BR 473CL 473CR483AL 483AR 483BL483BR 483CL 483CR545835-01-1 452DR 452EL 452FR 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, EXTERNAL T: 12 YE T: 20 YE NO CPCP A340-500452GR 452KL 454AL SURFACE AS FAR AS VISIBLE AND EXTERNAL UPPER AREAS I: 12 YE I: 12 YEOR454AR 462DR 462FR COVERED BY FAIRINGS.A340-600464AL 464AR 464BL472DR 472FR 482CR482DR 482EL 482FR482GR 482JL 484AL484AR545837-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, EXTERNAL T: 12 YE T: 20 YE NO CPCP A340-500416AR 424AL 424AR 463 LOWER AREAS COVERED BY REVERSER COWLS AND NOZZLE. I: 12 YE I: 12 YEOR425AL 426AR 434AL 473A340-600434AR 435AL 436AR 483444AL 444AR 445AL446AR545842-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 18APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS545858-01-1 N/A TASK DELETED545860-01-1 N/A TASK DELETED545870-01-1 452CR 452EL 452GR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A340-500462CR 462EL 462GR 463 FITTING SLEEVES, LINKS AND BOLTS AT RIB 8 (4 PLACES I: 12 YEOR462JL 472CR 472EL 473 PER PYLON).A340-600472GR 472JL 482CR 483482EL 482GR NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUTBOLTS REMOVAL AS FAR AS VISIBLEENGINELINKSSLEEVES545880-01-1 454AL 454AR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A340-500454BR 464AR 464BL 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YEOR464BR 464CL 474AL 473 PYLON).A340-600474BL 474BR 474CR 483484AL 484AR 484BL484BRBOLTSENGINELINKSSLEEVES* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 19APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551001-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP A340-200312 ASSEMBLY OF TRIM ACTUATING ARMS, SUPPORT FITTINGS AND I: 12 YE I: 12 YEORUPPER AND LOWER ATTACHMENT PLATES.A340-300551002-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200312 TRIM ACTUATING ARM LUGS AND SUPPORT FITTING I: 15000 FCORLUGS.A340-300551004-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP A340-200312 ASSEMBLY OF HINGE FITTING AT RIB 3, UPPER AND LOWER I: 12 YE I: 12 YEORATTACH FITTINGS, LH/RH.A340-300551007-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-1 A340-200312 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 12 YEORSPAR AND BETWEEN FUSELAGE FAIRING LINESA340-300551008-01-1 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200312 CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN I: 8600 FCORFUSELAGE FAIRING LINES. ORGROUP 43A44500 FHORGROUP 43BORGROUP 43E551008-01-2 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43C312 CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN I: 12300 FCFUSELAGE FAIRING LINES. OR24600 FH551009-01-1 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCA340-200REARMOST UPPER 343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM I: 5300 FCORFAIRING SUPPORT FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE ORGROUP 43AFITTING FAIRING LINE, LH/RH. 27200 FHORGROUP 43BORGROUP 43EISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551009-01-2 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCGROUP 43CREARMOST UPPER 343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM I: 9800 FCFAIRING SUPPORT FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE ORFITTING FAIRING LINE, LH/RH. 19600 FH551010-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-1 A340-200312 CENTER BOX BOTTOM SKIN LOWER SURFACE FROM FRONT TO I: 12 YEORREAR SPAR AND BETWEEN FUSELAGE FAIRING LINESA340-300551011-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 12 YE T: 20 YE CPCP A340-200312 SPAR AFT FACE JOINT PLATE INBOARD OF RIB 3, LH/RH OR I: 12 YEOR15000 FCA340-300I: 12 YEOR15000 FC551011-02-1 N/A TASK DELETED551012-01-1 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE CPCP ZL-311-01-1 A340-200312 CENTER BOX REAR SPAR AFT FACE BETWEEN RIB 3 LH AND I: 15000 FC I: 12 YEORRIB 3 RH, EXCLUDING INBOARD JOINT PLATESA340-300551013-01-1 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE 1 CPCP A340-200312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12 YEOR334 LH/RH.A340-300344551013-01-2 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 10000 FCOR334 LH/RH. ORGROUP 43A344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 51800 FHORTIME AS TASK 551013-02-1GROUP 43BORGROUP 43EISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551013-01-3 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43C312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12900 FC334 LH/RH. OR344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 25800 FHTIME AS TASK 551013-02-2551013-02-1 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 10000 FCOR334 LH/RH. ORGROUP 43A344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 51800 FHORTIME AS TASK 551013-01-2GROUP 43BORGROUP 43E551013-02-2 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43C312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12900 FC334 LH/RH. OR344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 25800 FHTIME AS TASK 551013-01-3551015-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE CPCP ZL-311-01-1 A340-200312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 15000 FC I: 12 YEORRIB 3 RHA340-300551016-01-1 N/A TASK DELETED551016-01-3 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43E312 CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD I: 15000 FCOF RIB 3, LH/RH551018-01-1 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-319-02-1 A340-200319BL 319BR 319CR CENTER BOX INTERNAL STRUCTURE I: 12 YEPRE 41600DISCONNECT SCAVENGEORWATER SYSTEM PIPEA340-300PRE 41600ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 551018-01-2 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NOA340-200319BL 319DR 319ER CENTER BOX INTERNAL STRUCTURE I: 12 YEPOST 41600ORA340-300POST 41600551019-01-1 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCA340-200312 STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 5800 FCORATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH ORGROUP 43ATO RIB 3 RH. 29700 FHORGROUP 43BORGROUP 43E551019-01-2 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCGROUP 43C312 STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 7500 FCATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH ORTO RIB 3 RH. 15000 FH551020-01-1 N/A 300 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES I: 15000 FCOROUTBOARD OF FUSELAGE FAIRINGSA340-300551020-02-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE CPCP ZL-300-01-1 A340-200CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE I: 6 YEORSPLICES OUTBOARD OF FUSELAGE FAIRINGSA340-300551021-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE CPCP ZL-300-01-1 A340-200CENTER BOX BOTTOM SKIN LOWER SURFACE CHORDWISE I: 6 YEORSPLICES OUTBOARD OF FUSELAGE FAIRINGSA340-300551022-01-1 331AT 331BT 333AB 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL T: 12 YE NO CPCP A340-200333AL 333AT 341AT 343 BOX INTERNAL STRUCTURE BETWEEN RIB 3 AND RIB 4 I: 12 YEOR341BT 343AB 343ARA340-300343ATISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551024-01-1 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE CPCP ZL-331-01-1 A340-200333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 15000 FC I: 12 YEOR343AB 343AT RIB 4A340-300551025-01-1 331AT 331BT 331CT 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-331-01-1 A340-200331DT 331ET 332AB 332 LATERAL BOX FRONT SPAR FORWARD FACE FROM RIB 4 I: 12 YEZL-332-01-1 OR332AT 333AB 333AT 341 TO END RIB AND EXTERNAL SURFACE OF END RIBA340-300341AT 341BT 341CT 342341DT 341ET 342AB342AT 343AB 343AT551026-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-300-01-1 A340-200LATERAL BOX TOP SKIN UPPER SURFACE FROM I: 6 YEORCHORDWISE SPLICE TO END RIBA340-300551027-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 3 YEA340-200LATERAL BOX BOTTOM SKIN LOWER SURFACE FROM I: 3 YEORCHORDWISE SPLICE LINE TO END RIBA340-300551028-01-1 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 3000 FCORFIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF ORGROUP 43EFUSELAGE FAIRINGS 16000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-1551028-01-2 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43A343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 4100 FCORFIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF ORGROUP 43BFUSELAGE FAIRINGS 22200 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-2551028-01-3 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCGROUP 43C343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 5100 FCFIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF ORFUSELAGE FAIRINGS 10200 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-3ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551028-02-1 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCA340-200343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 8000 FCORCHORDWISE SPLICE, FIVE( 5) REARMOST ROWS OF ORGROUP 43EFASTENERS OUTBOARD OF FUSELAGE FAIRINGS 43700 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-1551028-02-2 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCGROUP 43A343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 12400 FCORCHORDWISE SPLICE, FIVE (5) REARMOST ROWS OF ORGROUP 43BFASTENERS OUTBOARD OF FUSELAGE FAIRINGS 67400 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-2551028-02-3 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCGROUP 43C343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 15000 FCCHORDWISE SPLICE, FIVE (5) REARMOST ROWS OF ORFASTENERS OUTBOARD OF FUSELAGE FAIRINGS 30000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-3551029-01-1 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200319BL 319BR 319CR CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT I: 15000 FCPRE 41600DISCONNECT SCAVENGE TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3 RHORWATER SYSTEM PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEA340-300AS TASK 551029-02-1PRE 41600R 551029-01-2 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FCA340-200319BL 319DR 319ER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT I: 15000 FCPOST 41600TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3 RH.ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEA340-300AS TASK 551029-02-2POST 41600551029-02-1 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCA340-200319BL 319BR 319CR STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 15000 FCPRE 41600DISCONNECT SCAVENGE ATTACHMENT TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3ORWATER SYSTEM PIPE RH.A340-300NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEPRE 41600AS TASK 551029-01-1ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 551029-02-2 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FCA340-200319BL 319DR 319ER STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 15000 FCPOST 41600ATTACHMENT TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3ORRHA340-300NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASPOST 41600TASK 551029-01-2551030-01-1 334AB 334BB 334CB 334 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-334-02-1 A340-200334DB 334EB 334FB 344 LATERAL BOX REAR SPAR AFT FACE FROM RIB 3 I: 6 YEOR334GB 344AB 344BB OUTBOARD JOINT PLATE TO END RIBA340-300344CB 344DB 344EB344FB 344GB551031-01-1 334BB 334CB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 6 YE 1 CPCP A340-200335BB 344BB 344CB 344 HINGE FITTINGS NO.2 AND 3 AND SUPPORT RIBS. I: 15000 FC I: 6 YEOR344DB 345BBA340-300551031-02-1 N/A TASK DELETED551032-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 6 YE 1 CPCP A340-200344CT 344 ACTUATOR ATTACHMENT FITTING AND REACTION BAR AT I: 15000 FC I: 6 YEORRIBS 8 AND 9, LH AND RH.A340-300551032-02-1 N/A TASK DELETED551033-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 15000 FC T: 12 YE 1 CPCP A340-200334EB 334FB 334GB 344 FITTINGS NO.1, 4, 5, 6 AND 7 AND SUPPORT RIBS I: 15000 FC I: 12 YEOR335AB 335CB 335DBA340-300335EB 335FB 344AB344BB 344DB 344EB344FB 344GB 345AB345CB 345DB 345EB345FBISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551033-02-1 N/A TASK DELETEDR 551035-01-1 332AB 332AT 333BB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A340-200333CB 333DB 333EB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YEPOST 41471333FB 333GB 343BB RIB, LH / RHPRE 43491343CB 343DB 343EBOR343FB 343GB 344GBA340-300346ABPOST 41471PEELABLE HOLE COVERSPRE 43491R 551035-01-2 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A340-200333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND I: 12 YEPOST 43491343DB 343EB 343FB RIB 13 LH / END RIB RH.PRE 44818343GB 344GB 346ABORPEELABLE HOLE COVERSA340-300POST 43491PRE 44818R 551035-01-3 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A340-200333EB 333FB 333GB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YEPOST 44818334AZ 334GB 343BB RIB, LH / RHOR343CB 343DB 343EBA340-300343FB 343GB 344GBPOST 44818346ABPEELABLE HOLE COVERSN 551035-01-4 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A340-200333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND I: 12 YEPRE 41471343DB 343EB 343FB RIB 13 LH / END RIB RH.OR343GB 344GB 346ABA340-300PEELABLE HOLE COVERSPRE 41471ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 8APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 551035-02-1 331ET 332AB 332AT 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-333-01-2 A340-200333EL 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 13 AND END I: 12 YEPRE 41471PEELABLE HOLE COVERS RIB LHORPOST 43491PRE 44818ORA340-300PRE 41471ORPOST 43491PRE 44818551053-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP A340-500312 SCREW JACK FITTING. I: 12 YE I: 12 YEORA340-600551054-01-1 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP A340-500312 REAR SPAR, AFT FACE, CENTRAL JOINING PLATE, I: 12 YE I: 12 YEOREXTERNAL SURFACE.A340-600551055-01-1 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE 1 CPCP A340-500312 REAR SUPPORT FITTING AT RIB 3, INCLUDING UPPER AND I: 12 YE I: 12 YEORLOWER ATTACH FITTINGS, LH/RH.A340-600551056-01-1 331AT 331BT 331CT 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-331-01-2 A340-500331DT 331ET 331FT 332 FRONT SPAR, FORWARD FACE, FROM RIB 3 TO END RIB I: 12 YEZL-332-01-2 OR332AB 332AT 341AT 341 (RIB 21) AND EXTERNAL SURFACE OF END RIB, LH/RH.A340-600341BT 341CT 341DT 342341ET 341FT 342AB342AT551057-01-1 331CT 331DT 341CT 331 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP A340-500341DT 341 FRONT SPAR, FORWARD FACE, JOINING PARTS AT RIB 10, I: 12 YE I: 12 YEOREXTERNAL SURFACE, LH/RH.A340-600551058-01-1 334AB 334BB 334CB 334 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YEZL-334-02-2 A340-500334DB 334EB 334FB 344 REAR SPAR, AFT FACE, FROM RIB 3 TO END RIB (RIB 21), I: 12 YEOR344AB 344BB 344CB LH/RH.A340-600344DB 344EB 344FBISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 9APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551059-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 6 YE 1 CPCP A340-500344CT 344 ACTUATOR FITTING NO 1 AND 2, LH/RH. I: 6 YEORA340-600551060-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE 1 CPCP A340-500334EB 334FB 344AB 344 ELEVATOR HINGE FITTINGS NO 1 TO 8 AND SUPPORT RIB, I: 12 YEOR344BB 344DB 344EB LH/RH.A340-600344FB551061-01-1 312AR 313BL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YEZL-311-01-2 A340-500312 UPPER AND LOWER SKIN, INBOARD OF FUSELAGE FAIRINGS I: 12 YEOR(INSIDE FUSELAGE), EXTERNAL SURFACE.A340-600551062-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-2 A340-500312 FRONT SPAR, FORWARD FACE, FROM RIB 3 LH TO RIB 3 RH. I: 12 YEORA340-600551063-01-1 313BL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YEZL-311-01-2 A340-500312 REAR SPAR, AFTER FACE, FROM RIB 3LH TO RIB 3RH. I: 12 YEORA340-600551064-01-1 311CZ 311DZ 312AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-319-02-3 A340-500312CZ 312DZ 313BL INTERNAL STRUCTURE, BETWEEN RIB 3LH AND RIB 3 RH. I: 12 YEORA340-600551065-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-300-01-2 A340-500TOP SKIN, UPPER SURFACE, OUTBOARD OF FUSELAGE I: 6 YEORFAIRINGS, LH/RH.A340-600551066-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-300-01-2 A340-500BOTTOM SKIN, LOWER SURFACE, OUTBOARD OF FUSELAGE I: 6 YEORFAIRINGS, LH/RH.A340-600ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 10APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS551067-01-1 331AT 331AZ 333BB 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-333-02-1 A340-500333CB 333DB 333EB 343 INTERNAL STRUCTURE, BETWEEN RIB 3LH AND RIB 15LH, I: 12 YEZL-346-01-1 PRE 54173333FB 333GB 333HB 346 AND BETWEEN RIB 3RH AND RIB 16RH.OR333JB 333KB 333LBA340-600333MB 341AT 341AZPRE 54173343BB 343CB 343DB343EB 343FB 343GB343HB 343JB 343KB343LB 346AB551068-01-1 331ET 331FT 332AB 337 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-337-01-1 A340-500332AT 334EB 334FB 347 INTERNAL STRUCTURE, BETWEEN RIB 15 LH AND I: 12 YEPRE 54173334FT 341FT 342AB END RIB (RIB 21LH), AND BETWEEN RIB 16 RH AND END RIBOR342AT 344EB 344FB (RIB 21RH).A340-600344FTPRE 54173PEELABLE HOLE COVERS551069-01-1 331AT 331AZ 333BB 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-333-02-2 A340-500333CB 333DB 333EB 343 INTERNAL STRUCTURE, BETWEEN RIB 3 AND RIB 20 LH / RH I: 12 YEZL-346-01-2 POST 54173333FB 333GB 333HB 346OR333JB 333KB 333LBA340-600333MB 333NB 333PBPOST 54173333QB 333RB 333SB333TB 341AT 341AZ343BB 343CB 343DB343EB 343FB 343GB343HB 343JB 343KB343LB 343MB 343NB343PB 346AB 346BB346CB551070-01-1 332AB 332AT 334FB 337 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-337-01-2 A340-500334FT 342AB 342AT 347 INTERNAL STRUCTURE, BETWEEN RIB 20 LH / RH AND END I: 12 YEPOST 54173344FB 344FT RIB (RIB 21 LH / RH)ORPEELABLE HOLE COVERSA340-600POST 54173R 552001-01-1 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR TOP T: 3 YEZL-300-01-1 A340-200AND BOTTOM SKIN PANELS INCLUDING TRAILING EDGE, I: 3 YEOREXTERNAL SURFACEA340-300ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 11APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS552002-01-1 334BB 334CB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE T: 15000 FC T: 6 YE 1 CPCP A340-200335BB 344BB 344CB 345 FITTINGS NO.2 AND 3 AND ACTUATOR FITTINGS, LH AND I: 15000 FC I: 6 YEOR344DB 345BB RHA340-300552002-02-1 N/A TASK DELETED552003-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR SPAR FORWARD T: 12 YEA340-200334DB 334EB 334FB 345 FACE. I: 12 YEOR334GB 335AB 335BBA340-300335CB 335DB 335EB335FB 344AB 344BB344CB 344DB 344EB344FB 344GB 345AB345BB 345CB 345DB345EB 345FB552004-01-1 N/A 300 SPECIAL DETAILED INSPECTION OF ELEVATOR TOP AND T: 6 YEA340-200BOTTOM SKIN PANELS IN AREA OF HINGE FITTINGS NO.2 I: 6 YEORAND 3 AND AREA OF ACTUATOR FITTINGS, EXTERNALA340-300SURFACE.552005-01-1 334AB 334BB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE T: 15000 FC T: 12 YE 1 CPCP A340-200334EB 334FB 334GB 345 FITTINGS NO.1, 4, 5, 6 AND 7 I: 15000 FC I: 12 YEOR335AB 335CB 335DBA340-300335EB 335FB 344AB344BB 344DB 344EB344FB 344GB 345AB345CB 345DB 345EB345FB552005-02-1 N/A TASK DELETEDISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 12APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS552051-01-1 334AB 334BB 334CB 335 GENERAL VISUAL INSPECTION OF ELEVATOR, FRONT SPAR T: 12 YEZL-335-02-2 A340-500334DB 334EB 334FB 345 FORWARD FACE. I: 12 YEOR335AB 335BB 335CBA340-600335DB 335EB 335FB335GB 335HB 335JB344AB 344BB 344CB344DB 344EB 344FB345AB 345BB 345CB345DB 345EB 345FB345GB 345HB 345JB552052-01-1 334CB 334CT 335CB 335 DETAILED INSPECTION OF ELEVATOR, ACTUATOR FITTINGS T: 6 YE 1 CPCP A340-500335DB 335EB 344CB 345 NO 1 AND 2. I: 6 YEOR344CT 345CB 345DBA340-600345EB552053-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR, HINGE FITTINGS T: 12 YE 1 CPCP A340-500334DB 334EB 334FB 345 NO 1 TO 8. I: 12 YEOR335AB 335BB 335CBA340-600335DB 335EB 335FB335GB 335HB 335JB344AB 344BB 344CB344DB 344EB 344FB345AB 345BB 345CB345DB 345EB 345FB345GB 345HB 345JB552054-01-1 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR, TOP T: 6 YEZL-300-01-2 A340-500AND BOTTOM SKIN, EXTERNAL SURFACE. I: 6 YEORA340-600ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 13APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS552055-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR, INTERNAL STRUCTURE T: 12 YE CPCP A340-500334DB 334EB 334FB 345 AS FAR AS VISIBLE. I: 12 YEOR335AB 335BB 335CBA340-600335DB 335EB 335FB335GB 335HB 335JB344AB 344BB 344CB344DB 344EB 344FB345AB 345BB 345CB345DB 345EB 345FB345GB 345HB 345JBPEELABLE HOLE COVERS553004-01-1 N/A TASK DELETED553005-01-1 N/A TASK DELETED553008-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEA340-200SKIN PANELS FROM FRONT TO REAR SPAR AND I: 6 YEORFROM FIN/FUSELAGE FAIRING TO TOP, EXTERNALA340-300SURFACE LH/RH.553009-01-1 325AL 325BL 325CL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-325-02-1 A340-200325DL 325EL 325FL REAR SPAR AFT FACE INCLUDING SUPPORT FITTINGS I: 6 YEOR325GL 325HL 325JL FOR RUDDER HINGE ARMSA340-300325KL553010-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-322-01-1 A340-200324AT 324BT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YEZL-324-01-1 ORFACE.A340-300553011-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-323-01-1 A340-200STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 6 YEORRIB 1 AND RIB 8, INCLUDING LOWER SURFACE OF RIB 1A340-300ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 14APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS553012-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, T: 6 YEA340-200FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD I: 6 YEORFITTINGS.A340-300553013-01-1 322BL 322CL 324AT 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-323-02-1 A340-200325DL 325EL 325FL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 8 AND I: 12 YEOR325GL 325HL 325JL RIB 18.A340-300325KLPEELABLE HOLE COVERS553014-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE 1 CPCP A340-200RIB 1 AND RIB 5, METALLIC REINFORCEMENTS AT I: 6 YEPRE 40843THE MANHOLES.ORA340-300PRE 40843553015-01-1 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1 CPCP A340-200325HL 325KL 326BL SUPPORT FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YEPRE 40904326DL 326DR 326FLOR326HL 326KLA340-300PRE 40904553015-01-2 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1 CPCP A340-200325HL 325KL 326DL SUPPORT FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YEPOST 40904326DRORA340-300POST 40904553070-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEA340-500SKIN PANELS FROM FRONT TO REAR SPAR AND I: 6 YEORFROM FIN/FUSELAGE FAIRING TO TOP, EXTERNALA340-600SURFACE LH/RH.553071-01-1 325LL 325NL 325SL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-325-02-2 A340-500325TL 325UL 325VL REAR SPAR AFT FACE. I: 6 YEORA340-600ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 15APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS553072-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-322-01-2 A340-500322EL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING I: 12 YEZL-324-01-2 ORRIB UPPER FACE.A340-600553073-01-1 311AZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-323-01-2 A340-500STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 6 YEORRIB 1 AND RIB 5 INCLUDING LOWER SURFACE OF RIB 1.A340-600R 553074-01-1 311AZ 312AR 323DL 323 DETAILED INSPECTION OF VERTICAL STABILIZER, T: 6 YEA340-500323EL 325LL FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD I: 6 YEORFITTINGS.A340-600553075-01-1 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-323-02-2 A340-500324CT 325NL 325SL 324 STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 12 YEZL-324-01-2 OR325TL 325UL 325VL RIB 5 AND RIB 13A.A340-600PEELABLE HOLE COVERS553076-01-1 325LL 325NL 325SL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1 CPCP A340-500325TL 325UL 325VL ACTUATOR SUPPORT FITTINGS. I: 6 YEOR326ML 326NL 326PLA340-600326RL 326SLR 554001-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YEZL-300-01-1 A340-200EXTERNAL SURFACE LH/RH I: 6 YEORA340-300R 554003-01-1 324BT 325AL 325BL 326 SPECIAL DETAILED INSPECTION OF RUDDER FRONT SPAR T: 6 YEA340-200325CL 325DL 325EL I: 6 YEPRE 40904325FL 325GL 325HLOR325JL 325KL 326ALA340-300326BL 326CL 326DLPRE 40904326EL 326FL 326GL326HL 326JL 326KL326LLPEELABLE HOLE COVERSISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 16APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 554003-01-2 324BT 325AL 325BL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YEA340-200325CL 325DL 325EL I: 6 YEPOST 40904325FL 325GL 325HLOR325JL 325KL 326DLA340-300PEELABLE HOLE COVERSPOST 40904D 554005-01-1 N/A TASK DELETEDD 554005-02-1 N/A TASK DELETED554006-01-1 N/A TASK DELETED554007-01-1 N/A TASK DELETED554007-01-2 N/A TASK DELETED554008-01-1 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A340-200325HL 325KL 326BL I: 6 YEPRE 40904326BR 326DL 326DROR326FL 326FR 326HLA340-300326HR 326KL 326KRPRE 40904554008-01-2 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A340-200325HL 325KL 326DL I: 6 YEPOST 40904326DRORA340-300POST 40904ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 17APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 554009-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA340-200BOOSTER AREA, LH/RH. I: 6 YEORA340-300N 554010-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 3 YEA340-200AREA OF FRONT SPAR AND RIB 0. I: 3 YEPRE 40904ORA340-300PRE 40904N 554010-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA340-200AREA OF FRONT SPAR AND RIB 0. I: 6 YEPOST 40904ORA340-300POST 40904N 554011-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA340-200AREA OF HOISTING POINTS AND TRAILING EDGE SCREW LINE, I: 6 YEORLH/RH.A340-300N 554012-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA340-200ATTACH FITTING AREA, LH/RH. I: 6 YEPRE 40904ORA340-300PRE 40904N 554012-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA340-200ATTACH FITTING AREA, LH/RH. I: 6 YEPOST 40904ORA340-300POST 40904N 554013-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YEA340-200INTERNAL STRUCTURE, LH/RH. I: 6 YEORA340-300ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 18APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 554014-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0. T: 6 YEZL-300-01-1 A340-200I: 6 YEORA340-300R 554070-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YEZL-300-01-2 A340-500EXTERNAL SURFACE LH/RH. I: 6 YEORA340-600R 554071-01-1 325LL 325LR 325NL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YEA340-500325NR 325SL 325SR I: 6 YEOR325TL 325TR 325ULA340-600325UR 325VL 325VR326AT 326ML 326NL326PL 326RL 326SLPEELABLE HOLE COVERSD 554072-01-1 N/A TASK DELETEDR 554073-01-1 325LL 325NL 325SL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A340-500325TL 325UL 325VL I: 6 YEOR326ML 326NL 326PLA340-600326RL 326SLN 554074-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA340-500BOOSTER AREA, LH/RH. I: 6 YEORA340-600N 554075-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA340-500AREA OF FRONT SPAR AND RIB 0. I: 6 YEORA340-600N 554076-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA340-500AREA OF HOISTING POINTS AND TRAILING EDGE SCREW I: 6 YEORLINE, LH/RH.A340-600ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 19APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 554077-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA340-500ATTACH FITTING AREA, LH/RH. I: 6 YEORA340-600N 554078-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YEA340-500INTERNAL STRUCTURE, LH/RH. I: 6 YEORA340-600N 554079-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0. T: 6 YEZL-300-01-2 A340-500I: 6 YEORA340-600* * * * * E N D * * * * *ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 20APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 562101-01-1 830 840 221 DETAILED INSPECTION OF MAIN DECK WINDOW PANES T: 6 YEA340-200222 INCLUDING PASSENGER/CREW DOOR AND EMERGENCY EXIT I: 6 YEOR231 WINDOW PANES.A340-300232241242251252261262271272562102-01-1 830 840 221 DETAILED INSPECTION OF PASSENGER CABIN T: 6 YEA340-500222 WINDOW PANES INCLUDING PASSENGER/CREW DOOR AND I: 6 YEOR231 EMERGENCY EXIT WINDOW PANES.A340-600232241242251252261262271272* * * * * E N D * * * * *ISSUE: JUL 01/10 WINDOWS SECTION: D-56PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571102-01-1 N/A TASK DELETED571102-01-2 N/A TASK DELETED571102-01-3 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FCGROUP 43EAIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER ORDUCTS 38 LEVEL, LH/RH. 65000 FHLINING I: 5530 FCNOTE 1 OR37300 FH571103-01-1 N/A TASK DELETEDD 571103-01-2 N/A TASK DELETED571103-02-1 N/A TASK DELETEDD 571103-02-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571105-01-1 734 744 143 DETAILED INSPECTION OF CENTER WING BOX, T: 12 YE 1 CPCP A340-200AIR CONDITIONING 191 LOWER SKIN LOWER SURFACE FROM FR.40 TO FR.47 I: 12 YEORPACKS 192 BETWEEN RIB 1 LH AND RIB 1 RHA340-300FAIRING PANELS 193BETWEEN FR 40 AND FR 19547 196HEATSHIELDS571106-01-1 191HB 191QB 192HB 191 GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER T: 12 YE 1 CPCP A340-200192QB 192 SPLICE AT RIB 1 BETWEEN FR 40 AND FR 47 I: 12 YEOR195A340-300196571107-01-1 N/A TASK DELETED571107-01-2 N/A TASK DELETEDR 571107-01-3 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C196 BOX LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN ORSTRINGERS 20 AND 21, LH/RH 26000 FHI: 4900 FCOR9850 FH571108-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571108-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FCGROUP 42A744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OROR60000 FHGROUP 43AI: 7300 FCPOST 40123OR51000 FHR 571108-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FCGROUP 42B744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OROR60000 FHGROUP 43BI: 5900 FCOR40000 FHR 571108-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FCGROUP 43C744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR26000 FHI: 6700 FCOR13400 FH571108-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FCGROUP 43E744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR65000 FHI: 6500 FCOR43900 FH571114-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571114-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42A744 142 BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS OROR27 AND 28 60000 FHGROUP 43AI: 12600 FCPOST 40123OR60000 FH571114-01-3 N/A TASK DELETEDD 571114-01-4 N/A TASK DELETED571114-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43E744 142 BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS OR27 AND 28 65000 FHI: 6500 FCOR43900 FH571116-01-1 N/A TASK DELETED571116-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 4APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 571116-01-3 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43CBOX LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA ORBETWEEN STRINGERS 21 AND 22, AT Y =-567.5 26000 FHI: 4900 FCOR9850 FH571118-01-1 N/A TASK DELETED571118-01-2 N/A TASK DELETED571118-01-3 N/A TASK DELETED571118-01-4 N/A TASK DELETEDR 571118-01-5 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 43CBETWEEN FR 44 AND FR 195 LOWER PANEL, HYDRAULIC CONNECTOR AREAS AT Y =-2230 OR47 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 26000 FH27 AND STR 28. I: 4900 FCOR9850 FH571118-01-6 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 5APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571121-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 42A148 INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND I: 6000 FCORLONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANELGROUP 42BFROM Y =-1959 TO Y = 1959.OR(9 ASSYS TO BE INSPECTED)GROUP 43AORGROUP 43BORGROUP 43E571121-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FCGROUP 43C148 INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND ORLONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL 26000 FHFROM Y =-1959 TO Y = 1959. I: 6000 FC(9 ASSYS TO BE INSPECTED) OR12000 FH571122-01-1 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42A196 BOX EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR ORORLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM 60000 FHGROUP 43AY = 953 TO Y = 1959, LH/RH. I: 5500 FCOR27500 FH571122-01-2 N/A TASK DELETEDR 571122-01-3 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C196 BOX EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR ORLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM 26000 FHY = 953 TO Y = 1959, LH/RH. I: 4650 FCOR9350 FH571123-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 6APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571123-01-2 N/A TASK DELETED571123-01-3 N/A TASK DELETEDR 571125-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42B148 BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 ORORAND FR 47 LOWER CORNER FITTING, LH/RH 75000 FHGROUP 43BI: 3850 FCOR26000 FHR 571125-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C148 BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 ORAND FR 47 LOWER CORNER FITTING, LH/RH 26000 FHI: 4200 FCOR8400 FH571125-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 13000 FCGROUP 43E148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 ORAND FR 47 LOWER CORNER FITTING, LH/RH 65000 FHI: 3910 FCOR26400 FH571126-01-1 N/A TASK DELETEDD 571126-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 7APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571126-01-3 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 13000 FCGROUP 43ESPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORLOWER CORNER 65000 FHI: 9900 FCOR65000 FH571129-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 42A744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OROR60000 FHGROUP 43AI: 12100 FCOR60000 FH571129-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 42B744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OROR60000 FHGROUP 43BI: 8000 FCOR60000 FH571129-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 43C744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR26000 FHI: 9200 FCOR18400 FH571129-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 13000 FCGROUP 43E744 142 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR65000 FHI: 8200 FCOR55400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 8APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571130-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FCGROUP 42A744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OROR147 60000 FHGROUP 43A148 I: 5710 FCORORGROUP 42B38500 FHORGROUP 43B571130-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FCGROUP 43C744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OR147 26000 FH148 I: 7700 FCOR15400 FH571130-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FCGROUP 43E744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OR147 65000 FH148 I: 8300 FCOR56000 FH571131-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CENTER WING BOX, REAR T: 6 YE 1 CPCP A340-200148 SPAR, AFT FACE I: 6 YEORA340-300571133-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 42A744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD ORORFITTING CONNECTIONS (63 PLACES) 60000 FHGROUP 43AI: 7300 FCOR45800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 9APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 571133-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 42B744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD ORORFITTING CONNECTIONS (63 PLACES) 75000 FHGROUP 43BI: 4700 FCOR31900 FHR 571133-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FCGROUP 43C744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD ORFITTING CONNECTIONS (63 PLACES) 26000 FHI: 5450 FCOR10900 FH571137-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 42A192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORPOST 41652AT FR 40, LH/RH 60000 FHORI: 6000 FCGROUP 43AORPOST 4165242300 FHORGROUP 42BORGROUP 43B571137-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 43C192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORAT FR 40, LH/RH 26000 FHI: 6000 FCOR12000 FH571137-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 43E192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORAT FR 40, LH/RH 65000 FHI: 13000 FCOR65000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 10APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571138-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 42A744 142 INTERNAL STRUCTURE, LOWER L-FITTING AT CONNECTION ORPOST 43577WITH LOWER SKIN PANEL AT KEEL BEAM LEVEL, LH/RH. 60000 FHORI: 6000 FCGROUP 43AORPOST 4357742300 FH571140-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP T: 6 YE 1 CPCP A340-200GALLEYS AND TOILETS 146 SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL I: 6 YENOTEFUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47.ORA340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED ABOVE THIS AREA571140-02-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP T: 12 YE 1 CPCP A340-200146 SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL I: 12 YENOTEFUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47.ORA340-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTNOTEFITTED ABOVE THIS AREA571141-01-1 N/A TASK DELETED571144-01-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 13000 FCGROUP 43E192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 65000 FH196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5090 FCSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORLH/RH. 34300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 11APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571145-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CWB, INTERNAL T: 13000 FCGROUP 43E744 142 STRUCTURE, RIB1 LOWER TEE FITTING INBOARD FLANGE, ORSEALANT REMOVAL FASTENERS IN RADIUS AREA AT STR16, STR20, STR21 AND 65000 FHAND STR25 TO STR29, LH/RH I: 5230 FCOR35300 FH571146-01-1 N/A TASK DELETED571146-01-2 N/A TASK DELETED571146-01-3 N/A TASK DELETEDR 571146-02-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 42A192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OROR195 OF RIB 1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND 60000 FHGROUP 43A196 STR25 TO STR29, LH/RH. I: 9500 FCOR64100 FH571146-02-2 N/A TASK DELETEDD 571146-02-3 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 12APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571148-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 42A192 PANEL, KEEL BEAM FITTING 4 FIRST BORE HOLES AFT FRAME ORPOST 4357740 DATUM, LH/RH. 60000 FHORI: 6000 FCGROUP 43AORPOST 4357745900 FH571149-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42A192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE ORPOST 41652FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH 60000 FHPRE 44360I: 6000 FCORORGROUP 42A38300 FHPOST 45968ORGROUP 42BPOST 41652PRE 44360ORGROUP 42BPOST 45968ORGROUP 43APOST 41652PRE 44360ORGROUP 43APOST 45968ORGROUP 43BPOST 41652PRE 44360ORGROUP 43BPOST 45968571149-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 13APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 571149-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE ORPRE 45968FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH 26000 FHI: 7200 FCOR14400 FH571149-01-4 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE ORPOST 45968FROM FR 40 TO STR 1 LEVEL, LH/RH 26000 FHI: 8000 FCOR16000 FH571149-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FCGROUP 43E192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FR 40 TO ORSTR 1 LEVEL, LH/RH 65000 FHI: 6500 FCOR43700 FHR 571152-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42A744 142 BOX INTERNAL STRUCTURE,CENTER SPAR FITTING FLANGE, ORPRE 41652RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 75000 FHORFASTENERS 3 TO 12, LH/RH. I: 5900 FCGROUP 43AORPRE 4165240000 FHR 571153-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 43C744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF ORSEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 26000 FHWITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 6000 FCRADIUS ON EACH SIDE OF GUSSET, LH/RH OR12000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 14APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571153-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 43E744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF ORSEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 65000 FHWITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 12100 FCRADIUS ON EACH SIDE OF GUSSET, LH/RH OR82000 FHR 571153-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 42A744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF ORPOST 44360SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 60000 FHORWITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 6000 FCPOST 44440RADIUS ON EACH SIDE OF GUSSET, LH/RH ORS1327640700 FHORPOST 44440S13090ORGROUP 43APOST 44440S13276ORGROUP 42BORGROUP 43B571154-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX T: 12 YE NO CPCP ZL-141-01-1 A340-200744 142 INTERNAL STRUCTURE EXCLUDING STRUTS I: 12 YEORA340-300571157-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 43B744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, ORPOST 49202SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 60000 FHCONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 13000 FCOR60000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 15APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571157-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FCGROUP 43E744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, ORSEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 65000 FHCONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 13000 FCOR65000 FH571158-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 13000 FCGROUP 43B192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN ORPOST 49202CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 60000 FHI: 4520 FCOR22600 FH571158-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 13000 FCGROUP 43E192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN ORCONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 65000 FHI: 4290 FCOR29000 FH571159-01-1 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 42A146 BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPAR ORORVERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 60000 FHGROUP 42BBEAMS). I: 8200 FCORORGROUP 43A60000 FHORGROUP 43B571159-01-2 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FCGROUP 43C146 BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPAR ORVERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 26000 FHBEAMS). I: 11300 FCOR22600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 16APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571159-01-3 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 13000 FCGROUP 43E146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS). 65000 FHI: 9200 FCOR61900 FH571160-01-1 147AZ 148AZ 141 DETAILED INSPECTION OF CENTER WING BOX T: 12 YEA340-200142 STRUTS (54 PLACES) I: 12 YEORA340-300571165-01-1 N/A TASK DELETED571165-01-2 N/A TASK DELETED571805-01-1 192EB 192GB 192JB 143 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN T: 12 YE 1 CPCP A340-500192LB 192NB 192QB 191 LOWER SURFACE FROM FR.40 TO FR.47 BETWEEN RIB 1 LH I: 12 YEOR195GB 195HB 195JB 192 AND RIB 1 RH.A340-600195LB 195NB 734 193744 195AIR CONDITIONING 196PACKSHEATSHIELDS571806-01-1 191FB 192FB 192JB 191 GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER T: 12 YE 1 CPCP A340-500192NB 195JB 195NB 192 SPLICE AT RIB 1 BETWEEN FR.40 AND FR.47. I: 12 YEOR195A340-600196571831-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CENTER WING BOX , REAR T: 6 YE 1 CPCP A340-500148 SPAR, AFT FACE. I: 6 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 17APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS571831-02-1 N/A TASK DELETED571840-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A340-500GALLEYS AND TOILETS 146 FROM FR40 TO FR47, BETWEEN CABIN FLOOR LEVEL AND I: 6 YENOTEINSULATION CENTER WING BOX UPPER PANEL.ORLININGA340-600NOTE: TASK APPLICABLE IF GALLEYS OR TOILETSNOTEFITTED ABOVE THE AREA571840-01-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2 CPCP A340-500INSULATION 146 FROM FR40 TO FR47, BETWEEN CABIN FLOOR LEVEL AND I: 12 YENOTELINING CENTER WING BOX UPPER PANEL.ORA340-600NOTE : TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTNOTEFITTED ABOVE THIS AREA.571854-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX INTERNAL T: 12 YE NO CPCP ZL-141-01-2 A340-500744 142 STRUCTURE AND ACCESS DOORS, EXCLUDING STRUTS. I: 12 YEORA340-600571860-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUTS (90 T: 12 YEA340-500744 142 PLACES). I: 12 YEORA340-600572001-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 60000 FHGROUP 43APYLON FAIRING AND PYLON REINFORCING I: 7200 FCOR27200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 18APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572001-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 60000 FHGROUP 43BPYLON FAIRING AND PYLON REINFORCING I: 7600 FCOR28700 FH572001-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 26000 FHPYLON FAIRING AND PYLON REINFORCING I: 8200 FCOR16400 FH572001-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 65000 FHPYLON FAIRING AND PYLON REINFORCING I: 10400 FCOR45200 FH572002-01-1 464BL 464BR 464FL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A464FR 474BL 474BR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A ORPOST 43142474FL 474FR 472 60000 FHPRE 43183474 I: 9500 FCORORGROUP 43A35900 FHPOST 43142PRE 43183572002-01-11 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR474KL 474KR 472 65000 FH474 I: 5400 FCOR23700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 19APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572002-01-2 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OROR474KL 474KR 472 60000 FHGROUP 43B474 I: 7200 FCOR27200 FH572002-01-3 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR474KL 474KR 472 26000 FH474 I: 7800 FCOR15600 FHR 572002-01-7 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A ORPOST 43142474KL 474KR 472 60000 FHPOST 43183474 NOTE 8ORI: 9500 FCGROUP 43AORPOST 4314235900 FHPOST 43183572003-01-1 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FCGROUP 42A464AR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE ORPRE 43183474AL 474AR 472 60000 FHOR474 I: 7200 FCGROUP 43AORPRE 4318327200 FH572003-01-10 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FCGROUP 43E464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR474AL 474MR 472 65000 FH474 I: 21500 FCOR93400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 20APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572003-01-2 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FCGROUP 42B464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OROR474AL 474MR 472 60000 FHGROUP 43B474 I: 7600 FCOR28700 FH572003-01-3 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FCGROUP 43C464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR474AL 474MR 472 26000 FH474 I: 8200 FCOR16400 FH572003-01-7 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FCGROUP 42A464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE ORPOST 43183474AL 474MR 472 60000 FHOR474 I: 7200 FCGROUP 43AORPOST 4318327200 FH572003-02-1 462GR 462HL 464AL 462 GENERAL VISUAL INSPECTION OF OUTER WING LOWER T: 12 YE CPCP ZL-452-01-1 A340-200464AR 472GL 472HR 464 SURFACE VISIBLE PORTION OF INBOARD PYLON REINFORCING I: 12 YEZL-452-01-2 PRE 43183474AL 474AR 472 PLATEZL-452-01-4 OR474ZL-454-02-1 A340-300PRE 43183572003-02-2 462GR 462HL 464AL 462 GENERAL VISUAL INSPECTION OF OUTER WING LOWER T: 12 YE CPCP ZL-452-01-1 A340-200464MR 472GL 472HR 464 SURFACE VISIBLE PORTION OF INBOARD PYLON REINFORCING I: 12 YEZL-452-01-2 POST 43183474AL 474MR 472 PLATEZL-452-01-4 OR474ZL-454-02-2 A340-300ZL-454-02-3 POST 43183ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 21APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572004-01-1 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FHGROUP 43AMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5100 FCFAIRING AND PYLON FAIRING. OR19200 FH572004-01-2 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FHGROUP 43BMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5300 FCPRE 48437FAIRING AND PYLON FAIRING. OR20000 FH572004-01-3 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 26000 FHMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5700 FCFAIRING AND PYLON FAIRING. OR11400 FH572004-01-4 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 65000 FHMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 3700 FCFAIRING AND PYLON FAIRING. OR16300 FH572005-01-1 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF THE OUTER T: 13000 FCGROUP 42A641CB 641 WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA ORPRE 41114MASKED BY MAIN LANDING GEAR REINFORCING PLATE 60000 FHORINCLUDING ATTACHMENT TO REAR SPAR I: 5700 FCGROUP 43AORPRE 4111421500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 22APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572005-01-2 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER T: 13000 FCGROUP 42A641 WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA ORPOST 41114MASKED BY MAIN LANDING GEAR REINFORCING PLATE 60000 FHORINCLUDING ATTACHMENT TO REAR SPAR I: 5700 FCGROUP 43AORPOST 4111421500 FH572005-01-3 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FCGROUP 42B641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN ORORLANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 60000 FHGROUP 43BTO REAR SPAR I: 5600 FCOR21100 FH572005-01-4 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FCGROUP 43C641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN ORLANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 26000 FHTO REAR SPAR I: 6000 FCOR12000 FH572005-01-5 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FCGROUP 43E641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN ORLANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 65000 FHTO REAR SPAR I: 9400 FCOR40900 FH572006-01-1 N/A TASK DELETED572006-01-2 N/A TASK DELETED572006-01-3 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 23APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572006-01-4 N/A TASK DELETED572006-01-5 N/A TASK DELETED572006-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO CPCP ZL-500-01-1 GROUP 42A600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YEOR60000 FHGROUP 43AI: 4200 FCOR15800 FH572006-02-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO CPCP ZL-500-01-1 GROUP 42B600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YEOR60000 FHGROUP 43BI: 4700 FCOR17700 FH572006-02-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 6 YE NO CPCP ZL-500-01-1 GROUP 43C600 MAIN LANDING GEAR REINFORCING PLATE I: 6 YE572006-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FCGROUP 43C600 MAIN LANDING GEAR REINFORCING PLATE OR26000 FHI: 5400 FCOR10800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 24APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572006-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO CPCP ZL-500-01-1 GROUP 43E600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YE65000 FHI: 9700 FCOR42300 FH572007-01-1 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN ORORAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 60000 FHGROUP 43APYLON FAIRING I: 11200 FCOR42300 FH572007-01-2 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN ORORAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 60000 FHGROUP 43BPYLON FAIRING I: 10000 FCPRE 48437OR37800 FH572007-01-3 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN ORAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 26000 FHPYLON FAIRING I: 10800 FCOR21600 FH572007-01-4 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN ORAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 65000 FHPYLON FAIRING I: 6300 FCOR27300 FH572007-01-5 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE T: 20 YE CPCP A340-200474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN I: 12 YE I: 12 YEORAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARDA340-300PYLON FAIRINGISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 25APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572008-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA ORORCOVERED BY FLAP TRACK 2 FAIRING 60000 FHGROUP 42BI: 5000 FCORORGROUP 43A18900 FHORGROUP 43B572008-01-2 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA ORCOVERED BY FLAP TRACK 2 FAIRING 26000 FHI: 5400 FCOR10800 FH572008-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA ORCOVERED BY FLAP TRACK 2 FAIRING 65000 FHI: 5800 FCOR25300 FH572008-02-1 531AB 631AB 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE CPCP ZL-531-02-1 A340-200631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA I: 12 YEORCOVERED BY FLAP TRACK 2 FAIRINGA340-300572009-01-1 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 ORORINBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FHGROUP 43AFAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 2400 FC25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), ORSTRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 9000 FH2-3).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-02-1ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 26APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572009-01-2 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 42B474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY ORORINBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 60000 FHGROUP 43BFAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 2800 FCBAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR(RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 10500 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-02-2572009-01-3 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43C474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY ORINBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 26000 FHFAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 3200 FCBAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR(RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 6400 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-02-3572009-01-9 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43E474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY ORINBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 65000 FHFAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 5500 FCBAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR(RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 24000 FH572009-02-1 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 ORORINBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FHGROUP 43AFAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 5100 FC25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), ORSTRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 19200 FH2-3).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-01-1ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 27APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572009-02-2 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 ORORINBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FHGROUP 43BFAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 6100 FC25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), ORSTRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 23000 FH2-3).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-01-2572009-02-3 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 ORINBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 26000 FHFAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 6800 FC25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), ORSTRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 13600 FH2-3).NOTE: THIS TASK IS AN ALTERNATIVE TO TASK572009-01-3572010-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE T: 20 YE NO CPCP A340-200541DB 541EB 541FB 641 SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS I: 12 YE I: 12 YEOR641AB 641BB 641CB DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 ANDA340-300641DB 641EB 641FB 11-12572010-02-1 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OROR641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 60000 FHGROUP 43A641DB 641EB 641FB 9-10 AND 11-12 I: 5800 FCOR21900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 28APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572010-02-2 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OROR641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 60000 FHGROUP 43B641DB 641EB 641FB 9-10 AND 11-12 I: 6700 FCOR25300 FH572010-02-3 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 26000 FH641DB 641EB 641FB 9-10 AND 11-12 I: 7500 FCOR15000 FH572010-02-4 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 65000 FH641DB 641EB 641FB 9-10 AND 11-12 I: 5700 FCOR24700 FH572011-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR ORORBETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 60000 FHGROUP 43APYLON FAIRING. I: 4700 FCOR17700 FH572011-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR ORORBETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 60000 FHGROUP 43BPYLON FAIRING. I: 3700 FCOR13900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 29APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572011-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR ORBETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 26000 FHPYLON FAIRING. I: 4100 FCOR8200 FH572011-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR ORBETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 65000 FHPYLON FAIRING. I: 5900 FCOR25600 FH572012-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE BETWEEN RIB 1 AND ORORRIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 60000 FHGROUP 43AFRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5000 FCORCOVERED BY PYLON FAIRING AND PYLON ORGROUP 42BREINFORCING PLATE. 18900 FHORGROUP 43B572012-01-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE BETWEEN RIB 1 AND ORRIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 26000 FHFRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5400 FCCOVERED BY PYLON FAIRING AND PYLON ORREINFORCING PLATE. 10800 FH572012-01-3 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE BETWEEN RIB 1 AND ORRIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 65000 FHFRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5700 FCCOVERED BY PYLON FAIRING AND PYLON ORREINFORCING PLATE. 24900 FH572012-02-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 30APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572012-03-1 FUEL PUMP FAIRINGS 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ZL-500-01-1 A340-200600 LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN I: 6 YEORRIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPARA340-300EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLONREINFORCING PLATE.572013-01-1 464AL 464AR 464BL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 42A464BR 464FL 464FR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, ORPRE 43183464GL 464GR 464HL EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 60000 FHOR474AL 474AR 474BL AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5000 FCGROUP 43A474BR 474FL 474FR ORPRE 43183474GL 474GR 474HL 18900 FH572013-01-2 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43C464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 26000 FH474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5400 FC474HL 474JL 474JR OR474KL 474KR 474MR 10800 FH572013-01-3 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 42A464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, ORPOST 43183464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 60000 FHOR474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5000 FCGROUP 43A474HL 474JL 474JR ORPOST 43183474KL 474KR 474MR 18900 FHORGROUP 42BORGROUP 43B572013-01-4 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43E464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 65000 FH474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5700 FC474HL 474JL 474JR OR474KL 474KR 474MR 24900 FH572013-02-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 31APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572013-02-2 464AL 464AR 464GL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-454-02-1 A340-200464GR 464HL 464JL 474 LOWER SURFACE IN AREA COVERED BY INBOARD PYLON I: 12 YEPRE 43183464JR 464KL 464KR FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCINGOR474AL 474AR 474GL PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCINGA340-300474GR 474HL 474JL PLATEPRE 43183474JR 474KL 474KR572013-02-3 464AL 464GL 464GR 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP A340-200464HL 464JL 464JR 474 LOWER SURFACE IN AREA COVERED BY INBOARD PYLON I: 12 YEPOST 43183464KL 464KR 464MR FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCINGOR474AL 474GL 474GR PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCINGA340-300474HL 474JL 474JR PLATEPOST 43183474KL 474KR 474MR572014-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 42A600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FHGROUP 43AFAIRINGS. I: 8900 FCOR33600 FH572014-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 42B600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 ORORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FHGROUP 43BFAIRINGS. I: 8100 FCOR30600 FH572014-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43C600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 26000 FHFAIRINGS. I: 8700 FCOR17400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 32APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572014-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43E600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 ORBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 65000 FHFAIRINGS. I: 6300 FCOR27300 FH572015-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP A340-200600 SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF I: 6 YEORFRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1A340-300AND RIB 12572015-02-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 60000 FHGROUP 43ARIB 12 I: 9100 FCOR34300 FH572015-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 60000 FHGROUP 43BRIB 12 I: 7400 FCOR27900 FH572015-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 26000 FHRIB 12 I: 8100 FCOR16200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 33APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572015-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 65000 FHRIB 12 I: 5200 FCOR22500 FH572016-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP A340-200600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES I: 6 YEORBETWEEN RIB 2 AND RIB 4.A340-300572016-02-1 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES ORORBETWEEN RIB 2 AND RIB 4 60000 FHGROUP 43AI: 4100 FCOR15400 FH572016-02-2 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES ORORBETWEEN RIB 2 AND RIB 4 60000 FHGROUP 43BI: 4400 FCOR16600 FH572016-02-3 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES ORBETWEEN RIB 2 AND RIB 4 26000 FHI: 4800 FCOR9600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 34APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572016-02-4 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES ORBETWEEN RIB 2 AND RIB 4 65000 FHI: 6100 FCOR26500 FH572017-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 ORPOST 4328360000 FHORI: 8600 FCGROUP 43AORPOST 4328332500 FH572017-01-2 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OROR60000 FHGROUP 43BI: 8000 FCOR30200 FH572017-01-3 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR26000 FHI: 8400 FCOR16800 FH572017-01-4 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR65000 FHI: 10600 FCOR46000 FH572017-02-1 541AB 641AB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP ZL-541-01-1 A340-200641 SKIN ROOT JOINT FITTING ON STR 13 AND STR 20 I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 35APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572018-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 ORPRE 40610541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHOR541FZ 641AB 641AZ I: 7300 FCGROUP 43A641BB 641BZ 641CB ORPRE 40610641CZ 641DB 641DZ 27500 FH641EZ 641FZ572018-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 ORPOST 40610541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHOR541FZ 641AB 641AZ I: 7300 FCGROUP 43A641BB 641BZ 641CB ORPOST 40610641CZ 641DB 641DZ 27500 FH641EZ 641FZ572018-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OROR541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHGROUP 43B541FZ 641AB 641AZ I: 7700 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 29100 FH641EZ 641FZ572018-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 26000 FH541FZ 641AB 641AZ I: 8200 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 16400 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 36APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572018-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 65000 FH541FZ 641AB 641AZ I: 10800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 47100 FH641EZ 641FZ572018-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 I: 12 YEOR541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20A340-300541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572019-01-1 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 ORPRE 40610AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHORI: 7300 FCGROUP 43AORPRE 4061027500 FH572019-01-2 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 ORPOST 40610AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHORI: 7300 FCGROUP 43AORPOST 4061027500 FH572019-01-3 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 ORORAND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FHGROUP 43BI: 7700 FCOR29100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 37APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572019-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 ORAND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 26000 FHI: 8200 FCOR16400 FH572019-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 ORAND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 65000 FHI: 10800 FCOR47100 FH572019-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 I: 12 YEORAND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20A340-300572020-01-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ZL-541-02-1 A340-200641AB 641AZ 641BZ 641 UPPER SURFACE INCLUDING STRINGERS AND BUTTSTRAPS I: 6 YEORBETWEEN RIB 1 AND RIB 3A340-300NOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENT572021-01-1 464FL 464FR 464GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A464GR 474FL 474FR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 ORPRE 43183474GL 474GR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FHOR631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FCGROUP 43AORPRE 4318344200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 38APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572021-01-2 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OROR474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FHGROUP 43B631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 10900 FCOR41200 FH572021-01-3 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 26000 FH631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FCOR23400 FH572021-01-4 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 ORPOST 43183474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FHOR631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FCGROUP 43AORPOST 4318344200 FH572021-01-5 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 65000 FH631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 6700 FCOR29400 FH572021-02-1 464FL 464FR 464GL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE CPCP ZL-454-02-1 A340-200464GR 474FL 474FR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 I: 12 YEZL-454-02-2 PRE 43183474GL 474GR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLONZL-454-02-3 OR631AB 631 FAIRING AND FLAP TRACK 2 FAIRINGZL-531-02-1 A340-300PRE 43183572021-02-2 464GL 464GR 464JL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE CPCP ZL-454-02-1 A340-200464JR 474GL 474JL 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 I: 12 YEZL-531-02-1 POST 43183474JR 531AB 631AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLONOR631 FAIRING AND FLAP TRACK 2 FAIRINGA340-300POST 43183ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 39APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572022-01-1 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42ASEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY ORORPER NTM 10-11, FROM STR 6 TO STR 7 60000 FHGROUP 43AI: 9800 FCOR37000 FH572022-01-2 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42BSEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY ORORPER NTM 10-11, FROM STR 6 TO STR 7 60000 FHGROUP 43BI: 5800 FCOR21900 FH572022-01-3 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43CSEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY ORPER NTM 10-11, FROM STR 6 TO STR 7 26000 FHI: 6300 FCOR12600 FH572022-01-4 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43ESEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY ORPER NTM 10-11, FROM STR 6 TO STR 7 65000 FHI: 13000 FCOR65000 FH572023-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ZL-500-01-1 A340-200600 AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 I: 6 YEORFROM FRONT SPAR TO REAR SPAR EXCLUDING AREASA340-300COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAINLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2FAIRINGISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 40APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572023-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OROR10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 60000 FHGROUP 43ACOVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5000 FCORLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 ORGROUP 42BFAIRING 18900 FHORGROUP 43B572023-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OR10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 26000 FHCOVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5400 FCLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 ORFAIRING 10800 FH572023-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OR10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 65000 FHCOVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5800 FCLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 ORFAIRING 25300 FH572025-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A641AB 641BB 641CB 641 SKIN STRINGER JOINTS AT STR 11 BETWEEN RIBS 3 AND ORPRE 44245NUT REMOVAL AS PER RIBS 4 AND STR 12 AND 14 BETWEEN RIBS 5 AND 6 60000 FHORNTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7100 FCGROUP 43ATASK 572025-02-1 ORPRE 4424527200 FH572025-01-2 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B641AB 641BB 641CB 641 SKIN STRINGER JOINTS AT STR 11 BETWEEN RIBS 3 AND ORPRE 44245NUT REMOVAL AS PER RIBS 4 AND STR 12 AND 14 BETWEEN RIBS 5 AND 6 60000 FHORNTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7500 FCGROUP 43BTASK 572025-02-2 ORPRE 4424528800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 41APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572025-02-1 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A641AB 641BB 641CB 641 BOTTOM SKIN STRINGER JOINTS AT STR 11 BETWEEN ORPRE 44245NUT REMOVAL AS PER RIBS 3 AND RIBS 4 AND STR 12 AND 14 BETWEEN 60000 FHORNTM RIBS 5 AND 6 I: 7100 FCGROUP 43ANOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORPRE 44245TASK 572025-01-1 27200 FH572025-02-2 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B641AB 641BB 641CB 641 BOTTOM SKIN STRINGER JOINTS AT STR 11 BETWEEN ORPRE 44245NUT REMOVAL AS PER RIBS 3 AND RIBS 4 AND STR 12 AND 14 BETWEEN 60000 FHORNTM RIBS 5 AND 6 I: 7500 FCGROUP 43BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORPRE 44245TASK 572025-01-2 28800 FH572026-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OROR541DB 541DZ 541EZ 60000 FHGROUP 43A541FZ 641AB 641AZ I: 5700 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 21500 FH641EZ 641FZ572026-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OROR541DB 541DZ 541EZ 60000 FHGROUP 43B541FZ 641AB 641AZ I: 5500 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 20700 FH641EZ 641FZ572026-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR541DB 541DZ 541EZ 26000 FH541FZ 641AB 641AZ I: 5900 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 11800 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 42APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572026-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR541DB 541DZ 541EZ 65000 FH541FZ 641AB 641AZ I: 8800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 38100 FH641EZ 641FZ572026-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP ZL-541-02-1 A340-200541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 I: 12 YEOR541DB 541DZ 541EZA340-300541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572027-01-1 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB ORPRE 40610541DB 541DZ 541EZ 1 AND RIB 9 60000 FHOR541FZ 641AB 641AZ I: 13300 FCGROUP 43A641BB 641BZ 641CB ORPRE 40610641CZ 641DB 641DZ 50200 FH641EZ 641FZ572027-01-2 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB ORPOST 40610541DB 541DZ 541EZ 1 AND RIB 9 60000 FHOR541FZ 641AB 641AZ I: 13300 FCGROUP 43A641BB 641BZ 641CB ORPOST 40610641CZ 641DB 641DZ 50200 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 43APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572027-01-3 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OROR541DB 541DZ 541EZ 1 AND RIB 9 60000 FHGROUP 43B541FZ 641AB 641AZ I: 10900 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 41200 FH641EZ 641FZ572027-01-4 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR541DB 541DZ 541EZ 1 AND RIB 9 26000 FH541FZ 641AB 641AZ I: 11700 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 23400 FH641EZ 641FZ572027-01-5 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR541DB 541DZ 541EZ 1 AND RIB 9 65000 FH541FZ 641AB 641AZ I: 8600 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 37600 FH641EZ 641FZ572027-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN I: 12 YEOR541DB 541DZ 541EZ RIB 1 AND RIB 9.A340-300541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 44APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572028-01-1 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 ORORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43ATASK 572028-02-1 I: 5700 FCOR21500 FH572028-01-2 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 ORPRE 44245NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORTASK 572028-02-2 I: 5500 FCGROUP 43BORPRE 4424520700 FH572028-02-1 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 ORPRE 44245NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORNTM TASK 572028-01-1 I: 5700 FCGROUP 43AORPRE 4424521500 FH572028-02-2 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 ORPRE 44245NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORNTM TASK 572028-01-2 I: 5500 FCGROUP 43BORPRE 4424520700 FH572029-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN ORORRIB 1 AND RIB 12 60000 FHGROUP 43AI: 4200 FCORORGROUP 42B22300 FHORGROUP 43BPRE 48437ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 45APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572029-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN ORRIB 1 AND RIB 12 26000 FHI: 5300 FCOR10600 FH572029-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN ORRIB 1 AND RIB 12 65000 FHI: 6100 FCOR28100 FH572030-01-1 N/A TASK DELETED572030-01-2 N/A TASK DELETED572030-01-3 N/A TASK DELETED572030-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN ORRIB 9 AND RIB 11 65000 FHI: 8900 FCOR41200 FH572032-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 46APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572032-01-2 N/A TASK DELETED572032-01-3 N/A TASK DELETED572033-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT ORORSPAR TO REAR SPAR 60000 FHGROUP 43AI: 4200 FCOR22600 FH572033-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT ORORSPAR TO REAR SPAR 60000 FHGROUP 43BI: 4600 FCOR24800 FH572033-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT ORSPAR TO REAR SPAR 26000 FHI: 6100 FCOR12200 FH572033-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT ORSPAR TO REAR SPAR 65000 FHI: 6300 FCOR29000 FH572033-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 A340-200600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT I: 6 YEORSPAR TO REAR SPAR.A340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 47APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572034-01-1 N/A TASK DELETED572034-01-2 N/A TASK DELETED572034-01-3 N/A TASK DELETED572035-01-1 N/A TASK DELETED572035-01-2 N/A TASK DELETED572035-01-3 N/A TASK DELETED572035-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE FROM STRINGERS 12 TO 19 AND FROM RIB OR4 TO RIB 8 65000 FHI: 13000 FCOR65000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 48APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572036-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO ORORREAR SPARS 60000 FHGROUP 43AI: 5100 FCOR21900 FH572036-01-2 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 13000 FCGROUP 42B641AB 641AZ 641BZ 641 CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS OROR60000 FHGROUP 43BI: 5000 FCPRE 48437OR21700 FH572036-01-3 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO ORREAR SPARS 26000 FHI: 6200 FCOR12400 FH572036-01-4 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO ORREAR SPARS 65000 FHI: 9700 FCOR44700 FH572036-02-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO I: 12 YEORREAR SPARS.A340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 49APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572037-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OROR541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR 60000 FHGROUP 43A541FZ 641AB 641AZ I: 5500 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 29500 FH641EZ 641FZ572037-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OROR541DB 541DZ 541EZ FRONT SPAR TO REAR 60000 FHGROUP 43B541FZ 641AB 641AZ SPAR I: 8800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 47100 FH641EZ 641FZ572037-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR541DB 541DZ 541EZ FRONT SPAR TO REAR 26000 FH541FZ 641AB 641AZ SPAR I: 10800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 21600 FH641EZ 641FZ572037-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR541DB 541DZ 541EZ FRONT SPAR TO REAR 65000 FH541FZ 641AB 641AZ SPAR I: 9800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 45100 FH641EZ 641FZ572037-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM I: 12 YEOR541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR.A340-300541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 50APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572038-01-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641FB 641 REINFORCING PLATE LOWER SURFACE AT INNER PYLON I: 12 YEORA340-300572039-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OROR7 TO RIB 9 AND FROM RIB 11 TO RIB 12 60000 FHGROUP 43AI: 4200 FCOR22300 FH572039-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OROR7 TO RIB 9 AND FROM RIB 11 TO RIB 12 60000 FHGROUP 43BI: 4200 FCPRE 48437OR22300 FH572039-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR7 TO RIB 9 AND FROM RIB 11 TO RIB 12 26000 FHI: 5200 FCOR10400 FH572039-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR7 TO RIB 9 AND FROM RIB 11 TO RIB 12 65000 FHI: 8900 FCOR41200 FH572040-01-1 N/A TASK DELETED572040-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 51APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572040-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB OR11 AND RIB 13 26000 FHI: 13000 FCOR26000 FH572040-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB OR11 AND RIB 13 65000 FHI: 13000 FCOR65000 FH572041-01-1 573DB 573FB 673DB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE CPCP ZL-571-01-1 A340-200673FB 573 AFT FACE BETWEEN RIB 1 AND RIB 12. I: 12 YEZL-573-01-1 ORFLAPS EXTENDED 671A340-300673572043-01-1 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42A673 AFT FACE SPAR JOINT PLATE AT RIB 9 OROR60000 FHGROUP 43AI: 7100 FCOR31200 FH572043-01-2 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42B673 AFT FACE SPAR JOINT PLATE AT RIB 9 OROR60000 FHGROUP 43BI: 5400 FCOR23800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 52APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572043-01-3 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43C673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR26000 FHI: 6000 FCOR12000 FH572043-01-4 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43E673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR65000 FHI: 9400 FCOR42400 FH572043-02-1 573FB 673FB 573 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE CPCP ZL-573-01-1 A340-200673 AFT FACE SPAR JOINT PLATE AT RIB 9. I: 12 YEORA340-300572045-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE NO CPCP A340-200641AB 641AZ 641BZ 641 FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YEORA340-300572046-01-1 N/A TASK DELETED572046-01-2 N/A TASK DELETED572046-01-3 N/A TASK DELETED572046-02-1 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-02-1 A340-200541DB 541EB 541FB 641 FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP I: 12 YEOR641AB 641BB 641CB AND BOTTOM FLANGES.A340-300641DB 641EB 641FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 53APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572047-01-1 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OROR641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 60000 FHGROUP 43A641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FCORSEALANT REMOVAL AS RIB 7 ORGROUP 42BPER NTM 60000 FHORGROUP 43B572047-01-2 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OR641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 26000 FH641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FCSEALANT REMOVAL AS RIB 7 ORPER NTM 26000 FH572047-01-3 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OR641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 65000 FH641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FCSEALANT REMOVAL AS RIB 7 ORPER NTM 65000 FH572047-02-1 541AB 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR T: 12 YE NO CPCP ZL-541-02-1 A340-200541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD I: 12 YEOR641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING ANDA340-300641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 ANDRIB 7.572049-01-1 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORRIB 9 60000 FHGROUP 43AI: 10700 FCOR46800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 54APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572049-01-2 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORRIB 9 60000 FHGROUP 43BI: 8100 FCOR35700 FH572049-01-3 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORRIB 9 26000 FHI: 9100 FCOR18200 FH572049-01-4 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORRIB 9 65000 FHI: 11700 FCOR53000 FH572050-01-1 N/A TASK DELETED572050-01-2 N/A TASK DELETED572050-01-3 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 55APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572050-01-4 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43EFLAPS EXTENDED 573 AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 OR671 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7 65000 FH673 I: 13000 FCOR65000 FH572051-01-1 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42ASEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 ORPOST 46241PER NTM 60000 FHORI: 5200 FCGROUP 43AORPOST 4624122700 FH572051-01-2 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42ASEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 ORPOST 42547PER NTM 60000 FHORI: 5200 FCGROUP 43AORPOST 4254722700 FH572051-01-3 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42BSEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 ORORPER NTM 60000 FHGROUP 43BI: 13000 FCPRE 48437OR60000 FH572051-01-4 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43CSEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 ORPER NTM 26000 FHI: 13000 FCOR26000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 56APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572051-01-5 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43ESEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 ORPER NTM 65000 FHI: 13000 FCOR65000 FH572052-01-1 N/A TASK DELETED572052-01-2 N/A TASK DELETED572052-01-3 N/A TASK DELETED572052-02-1 541BB 541CB 641BB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-02-1 A340-200641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP I: 12 YEORAND BOTTOM FLANGES.A340-300572054-01-1 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42A671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 ORPOST 4614160000 FHORI: 4500 FCGROUP 43AORPOST 4614119700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 57APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572054-01-2 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42B671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 ORPRE 4369260000 FHPOST 46141I: 3300 FCORORGROUP 43B14500 FHPRE 43692POST 46141572054-01-3 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 42B671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 ORPOST 4369260000 FHORI: 7000 FCGROUP 43BORPOST 4369230600 FH572054-01-4 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FCGROUP 43C671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 OR26000 FHI: 7800 FCOR15600 FH572061-01-1 521AB 521BB 521CB 521 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE CPCP ZL-521-01-1 A340-200521DB 521EB 521FB 522 FORWARD FACE BETWEEN RIB 1 AND RIB 12 INCLUDING I: 6 YEZL-522-01-1 OR521GB 521HB 521JB 621 ALL CUTOUTS AND IN VICINITY OF FORWARD PYLONA340-300522AB 522BB 522CB 622 ATTACHMENT FITTING IN REGION OF RIB BAY 10-10A522DB 522EB 621AB AND BUILD DOOR621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB572062-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP A340-200641 UPPER AND LOWER ROOT JOINT FITTINGS I: 12 YE I: 12 YEORA340-300572063-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 58APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572063-01-2 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42A541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 ORPOST 40610641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 60000 FHOR641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 7100 FCGROUP 43AREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING ORPOST 40610INBOARD OF RIB 12 31000 FH572063-01-3 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42B541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 OROR641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 60000 FHGROUP 43B641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 8100 FCREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING ORINBOARD OF RIB 12 35800 FH572063-01-4 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 43C541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 OR641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 26000 FH641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 12300 FCREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING ORINBOARD OF RIB 12 24600 FH572063-02-1 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-541-02-1 A340-200541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 I: 12 YEOR641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,A340-300641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS INREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTINGINBOARD OF RIB 12.572064-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 59APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572064-01-2 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42A640 AFT FACE BETWEEN RIB 8 AND RIB 10 ORPOST 4061060000 FHORI: 7100 FCGROUP 43AORPOST 4061031000 FH572064-01-3 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42B640 AFT FACE BETWEEN RIB 8 AND RIB 10 OROR60000 FHGROUP 43BI: 8100 FCOR35800 FH572064-01-4 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 43C640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR26000 FHI: 12300 FCOR24600 FH572064-01-5 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 43E640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR65000 FHI: 13000 FCOR65000 FH572064-02-1 541EB 641EB 540 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-541-02-1 A340-200640 AND AFT FACE BETWEEN RIB 8 AND RIB 10. I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 60APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572065-01-1 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42A622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12 OROR60000 FHGROUP 43AI: 6900 FCOR30300 FH572065-01-2 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42B622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OROR60000 FHGROUP 43BI: 6600 FCPRE 48437OR28800 FH572065-01-3 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 43C622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OR26000 FHI: 9900 FCOR19800 FH572065-01-4 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 43E622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OR65000 FHI: 13000 FCOR65000 FH572065-01-5 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 12 YE T: 20 YE CPCP A340-200622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. I: 6 YE I: 6 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 61APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572066-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORRIB 12 60000 FHGROUP 43AI: 6900 FCOR30300 FH572066-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORRIB 12 60000 FHGROUP 43BI: 6600 FCOR28800 FH572066-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORRIB 12 26000 FHI: 9900 FCOR19800 FH572066-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORRIB 12 65000 FHI: 13000 FCOR65000 FH572067-01-1 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FCGROUP 42A541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OROR641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 60000 FHGROUP 43ASTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 12000 FCOR52600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 62APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572067-01-2 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FCGROUP 42B541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OROR641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 60000 FHGROUP 43BSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 12400 FCOR54400 FH572067-01-3 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FCGROUP 43C541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 26000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 13000 FCOR26000 FH572067-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FCGROUP 43E541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 65000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 5200 FCOR23600 FH572067-02-1 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6 T: 12 YE NO CPCP ZL-541-02-1 A340-200541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS I: 12 YEOR641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OFA340-300STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.572068-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 63APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572068-01-2 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FCGROUP 42B541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OROR641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FHGROUP 43BREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 4800 FCSURROUNDS OR21000 FH572068-01-3 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FCGROUP 43C541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 26000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FCSURROUNDS OR10400 FH572068-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FCGROUP 43E541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 65000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FCSURROUNDS OR23600 FH572068-02-1 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7 T: 12 YE NO CPCP ZL-541-02-1 A340-200541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN I: 12 YEOR641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,A340-300REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.572069-01-1 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FCGROUP 42A641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ORORATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FHGROUP 43AREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5400 FCSURROUNDS OR23900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 64APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572069-01-2 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FCGROUP 42B641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ORORATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FHGROUP 43BREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 6100 FCSURROUNDS OR26700 FH572069-01-3 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FCGROUP 43C641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ORATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 26000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 7200 FCSURROUNDS OR14400 FH572069-01-4 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FCGROUP 43E641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ORATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 65000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FCSURROUNDS OR23600 FH572069-02-1 541DB 541FZ 641DB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 8 AND 9 T: 12 YE NO CPCP ZL-541-02-1 A340-200641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS I: 12 YEORINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OFA340-300STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.572071-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FCGROUP 42A541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OROR541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 60000 FHGROUP 43A641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 5500 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING OR24300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 65APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572071-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FCGROUP 42B541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OROR541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 60000 FHGROUP 43B641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 6200 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE ORBOLTING 27200 FH572071-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FCGROUP 43C541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 26000 FH641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 7300 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE ORBOLTING 14600 FH572071-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FCGROUP 43E541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 65000 FH641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 13000 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE ORBOLTING 65000 FH572071-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 2,3,4 T: 12 YE NO CPCP ZL-541-02-1 A340-200541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A I: 12 YEOR541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPARA340-300641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLEBOLTING.572072-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 66APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572073-01-1 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FCGROUP 42A641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 60000 FHGROUP 43AREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13000 FCSURROUNDS OR60000 FH572073-01-2 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FCGROUP 42B641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 60000 FHGROUP 43BREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13300 FCSURROUNDS OR58200 FH572073-01-3 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FCGROUP 43C641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 26000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13000 FCSURROUNDS OR26000 FH572073-01-4 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FCGROUP 43E641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 65000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FCSURROUNDS OR23600 FH572073-02-1 541FB 541GB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB T: 12 YE NO CPCP ZL-541-02-1 A340-200641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN I: 12 YEORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,A340-300REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS572074-01-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB T: 12 YE NO CPCP ZL-541-02-1 A340-200641FB 641 10 FORWARD, RIB 10 A AND PYLON DIAPHRAGM. I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 67APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572075-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOX, RIB 1 EXTERNAL T: 12 YE T: 20 YE NO CPCP A340-200641 SURFACE AND UPPER SURFACE OF TRIFORM FITTING, BETWEEN I: 12 YE I: 12 YEORFRONT SPAR AND REAR SPAR.A340-300572081-01-1 N/A TASK DELETED572081-01-2 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC NOGROUP 42A641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. ORPOST 43021NOTE: TASK APPLICABLE IF MOD 43021 CARRIED OUT BY 60000 FHUP TO MSN 104RETROFIT SOLUTION I: 7500 FCNOTEOROR33100 FHGROUP 43APOST 43021UP TO MSN 104NOTE572081-01-3 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 42B641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OROR60000 FHGROUP 43BI: 4800 FCPRE 48437OR21300 FH572081-01-4 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 43C641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 OR26000 FHI: 5500 FCOR11000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 68APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572081-01-5 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 43E641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 OR65000 FHI: 5400 FCOR24300 FH572081-01-6 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 12 YE T: 20 YE NO CPCP A340-200641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 I: 12 YE I: 12 YEORA340-300572082-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 42A541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES ORPRE 40610541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FHOR541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 8500 FCGROUP 43A641BB 641CB 641DB CONDUIT HOLES. ORPRE 40610641DZ 641EB 641EZ 37400 FH641FB 641FZ572082-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 42A541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES ORPOST 40610541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FHOR541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 8500 FCGROUP 43A641BB 641CB 641DB CONDUIT HOLES. ORPOST 40610641DZ 641EB 641EZ 37400 FH641FB 641FZ572082-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 42B541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OROR541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FHGROUP 43B541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 10800 FCPRE 48437641BB 641CB 641DB CONDUIT HOLES. OR641DZ 641EB 641EZ 47300 FH641FB 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 69APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572082-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 43C541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 26000 FH541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 16300 FC641BB 641CB 641DB CONDUIT HOLES. OR641DZ 641EB 641EZ 32600 FH641FB 641FZ572082-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FCGROUP 43E541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 65000 FH541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 13000 FC641BB 641CB 641DB CONDUIT HOLES. OR641DZ 641EB 641EZ 65000 FH641FB 641FZ572082-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING CENTER SPAR T: 12 YE NO CPCP ZL-541-02-1 A340-200541CB 541DB 541DZ 641 BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES I: 12 YEOR541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAA340-300541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND641BB 641CB 641DB CONDUIT HOLES.641DZ 641EB 641EZ641FB 641FZ572083-01-1 541AB 541BZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 12 YE T: 20 YE NO CPCP A340-200641BZ 641 SPAR ASSEMBLY AFT FACE BETWEEN RIB 1 AND RIB 2 I: 12 YE I: 12 YEORA340-300572084-01-5 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 13000 FCGROUP 43ESEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB1 LOWER T FITTING OUTBOARD ORPER NTM FLANGE IN RADIUS AREA AT STR11, STR14, STR18 TO STR20 65000 FHAND AT STR23 TO STR28, LH/RH I: 7000 FCOR47400 FH572085-01-1 191BT 191CT 192BT 191 GENERAL VISUAL INSPECTION OF OUTER WING BOX, T: 12 YE 1 CPCP A340-200192CT 192 CRUCIFORM FITTING, OUTBOARD FLANGE UPPER SURFACE AS I: 12 YEORFAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RH.A340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 70APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572091-01-1 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10 ORORNUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43ANTM TASK 572091-02-1 I: 7100 FCOR26800 FH572091-01-2 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10 ORPRE 44245NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORNTM TASK 572091-02-2 I: 7500 FCGROUP 43BORPRE 4424528300 FH572091-02-1 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A641FB 641 BOTTOM SKIN STRINGER 10 JOINT BETWEEN RIB 9 AND ORORNUT REMOVAL AS PER RIB 10 60000 FHGROUP 43ANTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7100 FCSEALANT REMOVAL AS TASK 572091-01-1 ORPER NTM 26800 FH572091-02-2 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B641FB 641 BOTTOM SKIN STRINGER 10 JOINT BETWEEN RIB 9 AND ORPRE 44245NUT REMOVAL AS PER RIB 10 60000 FHORNTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7500 FCGROUP 43BSEALANT REMOVAL AS TASK 572091-01-2 ORPRE 44245PER NTM 28300 FH572092-01-1 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OROREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 60000 FHGROUP 43AI: 5700 FCOR21500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 71APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572092-01-2 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OROREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 60000 FHGROUP 43BI: 5500 FCOR20700 FH572092-01-3 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 26000 FHI: 5900 FCOR11800 FH572092-01-4 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 65000 FHI: 8800 FCOR38100 FH572092-02-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, I: 12 YEOREXCLUDING JOINT OF STRINGER 15 TO CENTER SPARA340-300572093-01-1 N/A TASK DELETED572093-01-2 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FCGROUP 42A641 OF STRINGER 15 TO CENTER SPAR ORPOST 40610NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHPOST 45415TASK 572093-02-2 I: 10400 FCUP TO MSN 44OROR39300 FHGROUP 43APOST 40610POST 45415UP TO MSN 44ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 72APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572093-01-3 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FCGROUP 42A641 OF STRINGER 15 TO CENTER SPAR ORMSN 46 AND SUBNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORTASK 572093-02-3 I: 10400 FCGROUP 43AORMSN 46 AND SUB39300 FH572093-01-4 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FCGROUP 42B641 OF STRINGER 15 TO CENTER SPAR ORORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43BTASK 572093-02-4 I: 9200 FCOR34700 FH572093-01-5 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FCGROUP 43C641 OF STRINGER 15 TO CENTER SPAR ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FHTASK 572093-02-5 I: 9900 FCOR19800 FH572093-01-6 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FCGROUP 43E641 OF STRINGER 15 TO CENTER SPAR ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FHTASK 572093-02-6 I: 5200 FCOR22500 FH572093-02-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 73APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572093-02-2 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPOST 40610PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHPOST 45415TASK 572093-01-2 I: 10400 FCUP TO MSN 44OROR39300 FHGROUP 43APOST 40610POST 45415UP TO MSN 44572093-02-3 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORMSN 46 AND SUBPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHORTASK 572093-01-3 I: 10400 FCGROUP 43AORMSN 46 AND SUB39300 FH572093-02-4 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42BSEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORORPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43BTASK 572093-01-4 I: 9200 FCOR34700 FH572093-02-5 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43CSEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FHTASK 572093-01-5 I: 9900 FCOR19800 FH572093-02-6 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43ESEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FHTASK 572093-01-6 I: 5200 FCOR22500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 74APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572093-03-1 541FB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641 JOINT OF STRINGER 15 TO CENTER SPAR. I: 12 YEORA340-300572094-01-1 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB ORPRE 406109 AND RIB 12 60000 FHORI: 13300 FCGROUP 43AORPRE 4061050200 FH572094-01-2 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB ORPOST 406109 AND RIB 12 60000 FHORI: 13300 FCGROUP 43AORPOST 4061050200 FH572094-01-3 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OROR9 AND RIB 12 60000 FHGROUP 43BI: 10900 FCOR41200 FH572094-01-4 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR9 AND RIB 12 26000 FHI: 11700 FCOR23400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 75APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572094-01-5 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR9 AND RIB 12 65000 FHI: 8600 FCOR37600 FH572094-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB I: 12 YEOR9 AND RIB 12.A340-300572095-01-1 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 ORPRE 4061060000 FHORI: 7300 FCGROUP 43AORPRE 4061027500 FH572095-01-2 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 ORPOST 4061060000 FHORI: 7300 FCGROUP 43AORPOST 4061027500 FH572095-01-3 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OROR60000 FHGROUP 43BI: 7700 FCOR29100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 76APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572095-01-4 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR26000 FHI: 8200 FCOR16400 FH572095-01-5 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR65000 FHI: 8600 FCOR37600 FH572101-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORORREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 60000 FHGROUP 43AAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4500 FCOR17000 FH572101-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORORREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 60000 FHGROUP 43BAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4300 FCOR16200 FH572101-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 26000 FHAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4600 FCOR9200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 77APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572101-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 65000 FHAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 8000 FCOR34900 FH572102-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 42A600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OROR60000 FHGROUP 43AI: 5800 FCOR21900 FH572102-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 42B600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OROR60000 FHGROUP 43BI: 5000 FCOR18900 FH572102-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 43C600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR26000 FHI: 5700 FCOR11400 FH572102-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 43E600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR65000 FHI: 13000 FCOR65000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 78APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572104-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORORREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 60000 FHGROUP 43AAREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 5600 FCPLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN ORJOINTS AT RIB 27 AND RIB 39 21100 FH572104-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 65000 FHAREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 8000 FCPLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN ORJOINTS AT RIB 27 AND RIB 39 34900 FH572104-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORORREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 60000 FHGROUP 43BAREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 4600 FCPLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN ORJOINTS AT RIB 27 AND RIB 39 17300 FH572104-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 26000 FHAREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 4900 FCPLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN ORJOINTS AT RIB 27 AND RIB 39 9800 FH572106-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORORBETWEEN RIB 12 AND RIB 23 60000 FHGROUP 43AI: 7700 FCOR29100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 79APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572106-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORORBETWEEN RIB 12 AND RIB 23 60000 FHGROUP 43BI: 8000 FCOR30200 FH572106-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORBETWEEN RIB 12 AND RIB 23 26000 FHI: 8600 FCOR17200 FH572106-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORBETWEEN RIB 12 AND RIB 23 65000 FHI: 5300 FCOR23200 FH572107-01-1 560BB 560CB 560DB 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A660BB 660CB 660DB 600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORORBETWEEN RIB 23 AND RIB 39 60000 FHGROUP 43AI: 7700 FCOR29100 FH572107-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORORBETWEEN RIB 23 AND RIB 39 60000 FHGROUP 43BI: 8000 FCOR30200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 80APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572107-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORBETWEEN RIB 23 AND RIB 39 26000 FHI: 8600 FCOR17200 FH572107-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS ORBETWEEN RIB 23 AND RIB 39 65000 FHI: 5300 FCOR23200 FH572108-01-1 454FL 454FR 484FL 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP GROUP 42A484FR 532AB 533AB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YEOR534AB 541GB 541HB 641 IN ALL BAYS BETWEEN RIB 12 AND RIB 27GROUP 43A541JB 541KB 541LB 642541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 560CB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB 660CB572108-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 81APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572108-01-3 454FL 454FR 484FL 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP GROUP 42B484FR 532AB 533AB 542 AND LOWER MATING SURFACE AROUND ACCESS DOOR CUTOUTS I: 6 YEOR534AB 541GB 541HB 641 IN ALL BAYS BETWEEN RIB 12 AND RIB 27GROUP 43B541JB 541KB 541LB 642OR541MB 541NB 541PBGROUP 43C541QB 541RB 541SBOR542AB 542BB 542CBGROUP 43E542DB 632AB 633AB634AB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB572108-02-1 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OROR534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 60000 FHGROUP 43A541JB 541KB 541LB 642 I: 9000 FC541MB 541NB 541PB OR541QB 541RB 541SB 34000 FH542AB 542BB 542CB542DB 560CB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB 660CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 82APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572108-02-11 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 65000 FH541JB 541KB 541LB 642 I: 5200 FC541MB 541NB 541PB OR541QB 541RB 541SB 22500 FH542AB 542BB 542CB542DB 632AB 633AB634AB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB572108-02-2 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OROR534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 60000 FHGROUP 43B541JB 541KB 541LB 642 I: 11800 FC541MB 541NB 541PB OR541QB 541RB 541SB 44600 FH542AB 542BB 542CB542DB 632AB 633AB634AB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 83APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572108-02-3 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 26000 FH541JB 541KB 541LB 642 I: 12800 FC541MB 541NB 541PB OR541QB 541RB 541SB 25600 FH542AB 542BB 542CB542DB 632AB 633AB634AB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB572109-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP A340-200542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR I: 6 YEOR550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEENA340-300550DB 550EB 550FB 650 RIBS 27 AND 39642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB572109-02-1 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OROR550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 60000 FHGROUP 43A550DB 550EB 550FB 650 RIBS 27 AND 39 I: 11400 FC642EB 642FB 642GB OR642HB 642JB 642KB 43000 FH650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 84APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572109-02-2 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OROR550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 60000 FHGROUP 43B550DB 550EB 550FB 650 RIBS 27 AND 39 I: 8200 FC642EB 642FB 642GB OR642HB 642JB 642KB 30900 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-3 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 26000 FH550DB 550EB 550FB 650 RIBS 27 AND 39 I: 9400 FC642EB 642FB 642GB OR642HB 642JB 642KB 18800 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-4 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 65000 FH550DB 550EB 550FB 650 RIBS 27 AND 39 I: 5200 FC642EB 642FB 642GB OR642HB 642JB 642KB 22500 FH650AB 650BB 650CB650DB 650EB 650FB572110-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM ORORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FHGROUP 43AFLAP TRACK FAIRINGS 3, 4 AND 5 I: 10700 FCOR40400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 85APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572110-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM ORORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FHGROUP 43BFLAP TRACK FAIRINGS 3, 4 AND 5 I: 9700 FCOR36600 FH572110-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43C600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 26000 FHFAIRINGS 3, 4 AND 5 I: 10400 FCOR20800 FH572110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43E600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 65000 FHFAIRINGS 3, 4 AND 5 I: 7700 FCOR33500 FH572110-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP ZL-500-01-1 A340-200600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM I: 6 YEORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BYA340-300FLAP TRACK FAIRINGS 3, 4 AND 5.572111-01-1 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A533CB 534AB 534CB 533 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK OROR632AB 632CB 633AB 534 FAIRINGS 3, 4 AND 5 60000 FHGROUP 43A633CB 634AB 634CB 632 I: 10700 FC633 OR634 40400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 86APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572111-01-2 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B533CB 534AB 534CB 533 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK OROR632AB 632CB 633AB 534 FAIRINGS 3, 4 AND 5 60000 FHGROUP 43B633CB 634AB 634CB 632 I: 9700 FC633 OR634 36600 FH572111-01-3 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43C533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 OR632AB 632CB 633AB 534 AND 5 26000 FH633CB 634AB 634CB 632 I: 10400 FC633 OR634 20800 FH572111-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FCGROUP 43E533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 OR632AB 632CB 633AB 534 AND 5 65000 FH633CB 634AB 634CB 632 I: 8300 FC633 OR634 36200 FH572111-02-1 532AB 532CB 533AB 532 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE CPCP ZL-531-02-1 A340-200533CB 534AB 534CB 533 LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS I: 6 YEOR632AB 632CB 633AB 534 3, 4 AND 5.A340-300633CB 634AB 634CB 632633634572112-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM ORORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FHGROUP 43AFLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 10100 FCPLASTRON FAIRING OR38100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 87APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572112-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM ORORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FHGROUP 43BFLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 9100 FCPLASTRON FAIRING OR34300 FH572112-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM ORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 26000 FHFLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 10100 FCPLASTRON FAIRING OR20200 FH572112-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM ORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 65000 FHFLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 7700 FCPLASTRON FAIRING OR33500 FH572112-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-500-01-1 A340-200600 LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT I: 12 YEORSPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPA340-300TRACK FAIRING 5, OUTBOARD PYLON FAIRING ANDPLASTRON FAIRING.572113-01-1 452FR 454AL 454AR 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A454BL 454BR 454FL 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD ORPRE 42283454FR 482FL 484AL 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FHOR484AR 484BL 484BR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FCGROUP 43A484FL 484FR FITTING ORPRE 4228338100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 88APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572113-01-2 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OROR454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FHGROUP 43B484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 9100 FC484PL 484PR FITTING OR34300 FH572113-01-3 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 26000 FH484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FC484PL 484PR FITTING OR20200 FH572113-01-4 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD ORPOST 42283454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FHOR484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FCGROUP 43A484PL 484PR FITTING ORPOST 4228338100 FH572113-01-5 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 65000 FH484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 8300 FC484PL 484PR FITTING OR36200 FH572113-02-1 452FR 454AL 454AR 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-452-01-1 A340-200454BL 454BR 454FL 454 LOWER SURFACE IN AREA COVERED BY OUTBOARD PYLON I: 12 YEZL-452-01-2 PRE 42283454FR 482FL 484AL 482 FAIRING, BUT EXCLUDING AREA COVERED BY OUTBOARD PYLONZL-454-02-1 OR484AR 484BL 484BR 484 PICK-UP PLATE AND AFT ATTACHMENT FITTING.ZL-454-02-2 A340-300484FL 484FRPRE 42283572113-02-2 452MR 454AL 454BL 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-452-01-4 A340-200454KR 454MR 454NR 454 LOWER SURFACE IN AREA COVERED BY OUTBOARD PYLON I: 12 YEZL-454-02-3 POST 42283454QL 482NL 484AR 482 FAIRING, BUT EXCLUDING AREA COVERED BY OUTBOARD PYLONOR484ML 484NL 484NR 484 PICK-UP PLATE AND AFT ATTACHMENT FITTING.A340-300484PL 484PRPOST 42283ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 89APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572114-01-1 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT ORORRIB 26 60000 FHGROUP 43AI: 5100 FCOR22300 FH572114-01-2 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT ORORRIB 26 60000 FHGROUP 43BI: 5400 FCOR23600 FH572114-01-3 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT ORRIB 26 26000 FHI: 6000 FCOR12000 FH572114-01-4 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT ORRIB 26 65000 FHI: 6700 FCOR29100 FH572115-01-1 452FR 454AL 454AR 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-452-01-1 A340-200454BL 454BR 482FL 454 LOWER SURFACE, VISIBLE PORTION OF OUTBOARD PYLON I: 12 YEZL-452-01-2 PRE 42283484AL 484AR 484BL 482 REINFORCING PLATE.ZL-454-02-1 OR484BR 484ZL-454-02-2 A340-300PRE 42283572115-01-2 452MR 454AL 454BL 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-452-01-4 A340-200454KR 454MR 482NL 454 LOWER SURFACE, VISIBLE PORTION OF OUTBOARD PYLON I: 12 YEZL-454-02-3 POST 42283484AR 484ML 484NL 482 REINFORCING PLATE.OR484NR 484A340-300POST 42283ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 90APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572116-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 42A600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 ORORAND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 60000 FHGROUP 43AAS VISIBLE. I: 8200 FCOR30900 FH572116-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 42B600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 ORORAND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 60000 FHGROUP 43BAS VISIBLE. I: 7300 FCOR27500 FH572116-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 43C600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 ORAND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 26000 FHAS VISIBLE. I: 7900 FCOR15800 FH572116-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCZL-500-01-1 GROUP 43E600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 ORAND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 65000 FHAS VISIBLE. I: 9100 FCOR39600 FH572117-01-1 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OROR632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 60000 FHGROUP 43A633CB 634AB 634CB 632 3, 4 AND 5 I: 10000 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 37800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 91APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572117-01-2 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OROR632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 60000 FHGROUP 43B633CB 634AB 634CB 632 3, 4 AND 5 I: 9400 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 35500 FH572117-01-3 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 26000 FH633CB 634AB 634CB 632 3, 4 AND 5 I: 10100 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 20200 FH572117-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 65000 FH633CB 634AB 634CB 632 3, 4 AND 5 I: 12300 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 53600 FH572119-01-1 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP A340-200600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK I: 6 YEORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAINA340-300HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR,BETWEEN RIB 12 AND RIB 23572119-01-2 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK ORORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 60000 FHGROUP 43AHOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 7100 FCBETWEEN RIB 12 AND RIB 23 OR26800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 92APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572119-01-3 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK ORORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 60000 FHGROUP 43BHOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 7800 FCBETWEEN RIB 12 AND RIB 23 OR29400 FH572119-01-4 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK ORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 26000 FHHOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 8900 FCBETWEEN RIB 12 AND RIB 23 OR17800 FH572119-01-5 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK ORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 65000 FHHOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 9800 FCBETWEEN RIB 12 AND RIB 23 OR42400 FH572120-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT ORORSTRINGER 20 IN RIB BAY 22-23 60000 FHGROUP 43AI: 3800 FCOR14300 FH572120-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT ORORSTRINGER 20 IN RIB BAY 22-23 60000 FHGROUP 43BI: 3600 FCOR13600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 93APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572120-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT ORSTRINGER 20 IN RIB BAY 22-23 26000 FHI: 11300 FCOR22600 FH572120-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT ORSTRINGER 20 IN RIB BAY 22-23 65000 FHI: 5300 FCOR23100 FH572121-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OROR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 60000 FHGROUP 43A541RB 541SB 641GB AND 20 I: 4900 FC641HB 641JB 641KB OR641LB 641MB 641NB 20000 FH641PB 641QB 641RB641SB572121-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OROR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 60000 FHGROUP 43B541RB 541SB 641GB AND 20 I: 5000 FC641HB 641JB 641KB OR641LB 641MB 641NB 20400 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 94APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572121-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 26000 FH541RB 541SB 641GB AND 20 I: 5400 FC641HB 641JB 641KB OR641LB 641MB 641NB 10800 FH641PB 641QB 641RB641SB572121-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 65000 FH541RB 541SB 641GB AND 20 I: 9600 FC641HB 641JB 641KB OR641LB 641MB 641NB 41600 FH641PB 641QB 641RB641SB572121-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING I: 12 YEOR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13A340-300541RB 541SB 641GB AND 20.641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB572122-01-1 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OROR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 60000 FHGROUP 43A550CB 550DB 550EB 650 I: 8400 FC550FB 560CB 642AB OR642BB 642CB 642FB 31700 FH642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 95APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572122-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OROR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 60000 FHGROUP 43B550CB 550DB 550EB 650 I: 8800 FC550FB 642AB 642BB OR642CB 642FB 642GB 33200 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 26000 FH550CB 550DB 550EB 650 I: 9400 FC550FB 642AB 642BB OR642CB 642FB 642GB 18800 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 65000 FH550CB 550DB 550EB 650 I: 9600 FC550FB 642AB 642BB OR642CB 642FB 642GB 41600 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42A542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB I: 12 YEZL-550-01-1 OR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 & 18.GROUP 43A550CB 550DB 550EB 650550FB 560CB 642AB642BB 642CB 642FB642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 96APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572122-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42B542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB I: 12 YEZL-550-01-1 OR542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 & 18.GROUP 43B550CB 550DB 550EB 650OR550FB 642AB 642BBGROUP 43C642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572123-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP A340-200542HB 542JB 542KB 550 SKIN ACCESS DOORS BETWEEN RIB 27 AND RIB 39 I: 6 YEOR550AB 550BB 550CB 642 INCLUDING NACA DUCT DOOR.A340-300550DB 550EB 550FB 650642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB572124-01-1 542AB 560CB 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP GROUP 42A660CB 642 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YEORGROUP 43ANOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORETO BE ADJUSTED BY INDIVIDUAL OPERATORS INCONSIDERATION OF THEIR OWN IN-SERVICEEXPERIENCE AND OPERATIONAL ENVIRONMENT572124-01-2 542AB 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP GROUP 42B642 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YEORGROUP 43BNOTE: TASK INTERVAL MAY BE INFLUENCED BYORMICROBIOLOGICAL CONTAMINATION AND IS THEREFOREGROUP 43CTO BE ADJUSTED BY INDIVIDUAL OPERATORS INCONSIDERATION OF THEIR OWN IN-SERVICEEXPERIENCE AND OPERATIONAL ENVIRONMENT572125-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 97APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572125-01-2 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO CPCP GROUP 42A484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YEOR642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FCGROUP 43AORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHTASK 572125-02-1 I: 12 YEOR12300 FCOR46400 FH572125-01-3 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO CPCP GROUP 42B484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YEOR642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FCGROUP 43BORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHTASK 572125-02-2 I: 12 YEOR11900 FCOR44900 FH572125-01-4 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO CPCP GROUP 43C484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FCORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FHTASK 572125-02-3 I: 12 YEOR13000 FCOR26000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 98APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572125-01-5 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO CPCP GROUP 43E484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FCORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FHTASK 572125-02-4 I: 12 YEOR13000 FCOR65000 FH572125-02-1 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OROR642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 60000 FHGROUP 43ASEALANT REMOVAL AS I: 12300 FCPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-2 46400 FH572125-02-2 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OROR642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 60000 FHGROUP 43BSEALANT REMOVAL AS I: 11900 FCPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-3 44900 FH572125-02-3 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 26000 FHSEALANT REMOVAL AS I: 13000 FCPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-4 26000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 99APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572125-02-4 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 65000 FHSEALANT REMOVAL AS I: 13000 FCPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-5 65000 FH572126-01-1 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO CPCP A340-200642 SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YE I: 12 YEORA340-300572126-01-2 N/A TASK DELETED572126-02-1 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OROR60000 FHGROUP 43AI: 6300 FCOR23800 FH572126-02-2 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OROR60000 FHGROUP 43BI: 7600 FCOR28700 FH572126-02-3 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR26000 FHI: 8800 FCOR17600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 100APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572126-02-4 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR65000 FHI: 10600 FCOR46000 FH572127-01-1 550AB 650AB 550 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP A340-200650 UPPER SURFACE BETWEEN RIB 33 AND RIB 34. I: 6 YEORA340-300NOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORETO BE ADJUSTED BY INDIVIDUAL OPERATORS INCONSIDERATION OF THEIR OWN IN-SERVICEEXPERIENCE AND OPERATIONAL ENVIRONMENT572128-01-1 542CB 560CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A660CB 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB ORORSEALANT REMOVAL AS BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 60000 FHGROUP 43APER NTM I: 8800 FCOR38500 FH572128-01-2 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42BSEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB ORORPER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 60000 FHGROUP 43BI: 5300 FCOR23200 FH572128-01-3 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43CSEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB ORPER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 26000 FHI: 6000 FCOR12000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 101APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572128-01-4 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43ESEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB ORPER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 65000 FHI: 13000 FCOR65000 FH572129-01-1 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641 STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23 OROR60000 FHGROUP 43ANOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FCTASK 572129-02-1 OR23000 FH572129-01-2 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641 STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23 ORPRE 4424560000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6000 FCGROUP 43BTASK 572129-02-2 ORPRE 4424522600 FH572129-02-1 541SB 641SB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42ASEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND ORORPER NTM RIB 23 60000 FHGROUP 43AI: 6100 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572129-01-1 23000 FH572129-02-2 541SB 641SB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42BSEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND ORPRE 44245PER NTM RIB 23 60000 FHORI: 6000 FCGROUP 43BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORPRE 44245TASK 572129-01-2 22600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 102APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572130-01-1 542AB 560CB 642AB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A660CB 642 SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24 OROR60000 FHGROUP 43ANOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8400 FCTASK 572130-02-1 OR31700 FH572130-01-2 542AB 642AB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B642 SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24 ORPRE 4424560000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8800 FCGROUP 43BTASK 572130-02-2 ORPRE 4424533200 FH572130-02-1 542AB 560CB 642AB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A660CB 642 BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND ORORSEALANT REMOVAL AS RIB 24 60000 FHGROUP 43APER NTM I: 8400 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572130-01-1 31700 FH572130-02-2 542AB 642AB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42BSEALANT REMOVAL AS 642 BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND ORPRE 44245PER NTM RIB 24 60000 FHORI: 8800 FCGROUP 43BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORPRE 44245TASK 572130-01-2 33200 FH572131-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 103APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572131-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND ORORREAR SPAR BETWEEN RIB 12 AND RIB 27 60000 FHGROUP 43BI: 4200 FCPRE 48437OR22300 FH572131-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FCGROUP 43C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 12 AND RIB 27 26000 FHI: 5300 FCOR10600 FH572131-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FCGROUP 43E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 12 AND RIB 27 65000 FHI: 6100 FCOR28100 FH572132-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FCGROUP 42A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORORBETWEEN RIB 27 TO RIB 39 60000 FHGROUP 43AI: 4200 FCORORGROUP 42B22300 FHORGROUP 43B572132-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORSPAR BETWEEN RIB 27 TO RIB 39 26000 FHI: 4900 FCOR9800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 104APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572132-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORSPAR BETWEEN RIB 27 TO RIB 39 65000 FHI: 6100 FCOR28100 FH572133-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT ORORSPAR TO REAR SPAR. 60000 FHGROUP 43AI: 4200 FCOR22300 FH572133-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT ORORSPAR TO REAR SPAR 60000 FHGROUP 43BI: 4100 FCPRE 48437OR22000 FH572133-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FCGROUP 43C600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORREAR SPAR. 26000 FHI: 5300 FCOR10600 FH572133-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FCGROUP 43E600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORREAR SPAR. 65000 FHI: 6300 FCOR29000 FH572133-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 A340-200600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT I: 6 YEORSPAR TO REAR SPAR.A340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 105APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572134-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORORSPAR TO REAR SPAR 60000 FHGROUP 43AI: 7100 FCOR37900 FH572134-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORORSPAR TO REAR SPAR 60000 FHGROUP 43BI: 6900 FCOR36500 FH572134-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORSPAR TO REAR SPAR 26000 FHI: 8900 FCOR17800 FH572134-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORSPAR TO REAR SPAR 65000 FHI: 6300 FCOR29000 FH572134-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 A340-200600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT I: 6 YEORSPAR TO REAR SPARA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 106APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572135-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 42A600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 60000 FHGROUP 43ASTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 6300 FCOR33600 FH572135-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 42B600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 60000 FHGROUP 43BAT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 6300 FCOR33600 FH572135-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43C600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 26000 FHAT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 8200 FCOR16400 FH572135-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43E600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 65000 FHAT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 13000 FCOR65000 FH572138-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OROR60000 FHGROUP 43AI: 9800 FCOR51900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 107APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572138-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 42B600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OROR60000 FHGROUP 43BI: 9800 FCOR51900 FH572138-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43C600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR26000 FHI: 13000 FCOR26000 FH572138-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43E600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR65000 FHI: 13000 FCOR65000 FH572139-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OROR60000 FHGROUP 43AI: 10800 FCOR57500 FH572139-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 42B600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OROR60000 FHGROUP 43BI: 10800 FCOR57500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 108APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572139-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43C600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR26000 FHI: 13000 FCOR26000 FH572139-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FCZL-500-02-1 GROUP 43E600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR65000 FHI: 13000 FCOR65000 FH572140-01-1 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 42A541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OROR541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 60000 FHGROUP 43A541PB 541QB 541RB I: 11100 FC541SB 641EB 641FB OR641GB 641HB 641JB 59300 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-01-2 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 42B541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OROR541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 60000 FHGROUP 43B541PB 541QB 541RB I: 7000 FC541SB 641EB 641FB OR641GB 641HB 641JB 37100 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 109APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572140-01-3 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 43C541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 26000 FH541PB 541QB 541RB I: 8200 FC541SB 641EB 641FB OR641GB 641HB 641JB 16400 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 43E541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 65000 FH541PB 541QB 541RB I: 9800 FC541SB 641EB 641FB OR641GB 641HB 641JB 45100 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541HB 541JB 541KB 641 STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING I: 12 YEOR541LB 541MB 541NB BUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGERA340-300541PB 541QB 541RB JOINTS.541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572141-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 110APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572141-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 42B542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OROR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 60000 FHGROUP 43B542KB 550AB 550BB 650 I: 6100 FC550CB 550DB 550EB OR550FB 642AB 642BB 32300 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572141-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 43C542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 26000 FH542KB 550AB 550BB 650 I: 7600 FC550CB 550DB 550EB OR550FB 642AB 642BB 15200 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572141-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FCGROUP 43E542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 65000 FH542KB 550AB 550BB 650 I: 13000 FC550CB 550DB 550EB OR550FB 642AB 642BB 65000 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 111APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572141-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42A542DB 542EB 542FB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING I: 12 YEZL-550-01-1 OR542GB 542HB 542JB 642 BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT INGROUP 43A542KB 550AB 550BB 650 RIB BAY 23-24.550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642DB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB660CB572141-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42B542DB 542EB 542FB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING I: 12 YEZL-550-01-1 OR542GB 542HB 542JB 642 BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT INGROUP 43B542KB 550AB 550BB 650 RIB BAY 23-24.OR550CB 550DB 550EBGROUP 43C550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572142-01-1 N/A TASK DELETED572143-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 112APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572144-01-1 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42A642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27 OROR60000 FHGROUP 43AI: 4900 FCOR27000 FH572144-01-2 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FCGROUP 42B642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27 OROR60000 FHGROUP 43BI: 4900 FCOR27000 FH572144-01-3 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 13000 FCGROUP 43C642 SURFACE AT CHORDWISE JOINT AT RIB 27 OR26000 FHI: 6900 FCOR13800 FH572144-01-4 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 13000 FCGROUP 43E642 SURFACE AT CHORDWISE JOINT AT RIB 27 OR65000 FHI: 13000 FCOR65000 FH572144-02-1 542EB 642EB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 A340-200642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YEORA340-300572145-01-1 542BB 542CB 542DB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42A560CB 642BB 642CB 642 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YEOR642DB 660CBGROUP 43AISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 113APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572145-01-2 542BB 542CB 542DB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42B642BB 642CB 642DB 642 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YEORGROUP 43BORGROUP 43C572147-01-1 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP MSN 001 THRU641 MANUAL REFUELING APERTURE REINFORCING PLATE IN RIB I: 12 YEMSN 015BAY 22-23572148-01-1 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OROR60000 FHGROUP 43AI: 12300 FCOR46400 FH572148-01-2 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OROR60000 FHGROUP 43BI: 11900 FCOR44900 FH572148-01-3 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR26000 FHI: 13000 FCOR26000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 114APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572148-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR65000 FHI: 13000 FCOR65000 FH572148-02-1 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 A340-200642EB 642 STRINGERS IN RIB BAYS 26 TO 28 INCLUDING BUTTSTRAPS. I: 12 YEORA340-300572149-01-1 560CB 660CB 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO CPCP GROUP 42A600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEORAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 60000 FHGROUP 43ASPAR, BETWEEN RIBS 23 AND 39 I: 8500 FCOR32100 FH572149-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO CPCP GROUP 42B600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEORAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 60000 FHGROUP 43BSPAR, BETWEEN RIBS 23 AND 39 I: 8200 FCOR30900 FH572149-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO CPCP GROUP 43C600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 26000 FHSPAR, BETWEEN RIBS 23 AND 39 I: 9400 FCOR18800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 115APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572149-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO CPCP GROUP 43E600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 65000 FHSPAR, BETWEEN RIBS 23 AND 39 I: 9800 FCOR42400 FH572151-01-1 560DB 574AT 574BB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE CPCP GROUP 42A574CB 574DB 574EB 674 AFT FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YEOR574FB 574GB 574HBGROUP 43A574JB 574KB 574LB574MB 574NB 660DB674AT 674BB 674CB674DB 674EB 674FB674GB 674HB 674JB674KB 674LB 674MB674NB572151-01-2 574AT 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE CPCP GROUP 42B574DB 574EB 574FB 674 AFT FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YEOR574GB 574HB 574JBGROUP 43B574KB 574LB 574MBOR574NB 674AT 674BBGROUP 43C674CB 674DB 674EB674FB 674GB 674HB674JB 674KB 674LB674MB 674NB572152-01-1 574AT 575AT 575BT 575 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE CPCP A340-200591AB 591BB 591CB 675 AFT FACE BETWEEN RIB 27 AND RIB 39. I: 12 YE I: 12 YEOR591DB 592AB 592BBA340-300592CB 592DB 674AT675AT 675BT 691AB691BB 691CB 691DB692AB 692BB 692CB692DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 116APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572153-01-1 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP GROUP 42A575 JOINT PLATE AT RIB 27. OR I: 12 YEOR674 13000 FCGROUP 43A675 OR60000 FHI: 12 YEOR7100 FCOR31200 FH572153-01-2 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP GROUP 42B575 JOINT PLATE AT RIB 27. OR I: 12 YEOR674 13000 FCGROUP 43B675 OR60000 FHI: 12 YEOR5400 FCOR23800 FH572153-01-3 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP GROUP 43C575 JOINT PLATE AT RIB 27. OR I: 12 YE674 13000 FC675 OR26000 FHI: 12 YEOR5400 FCOR10800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 117APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572153-01-4 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP GROUP 43E575 JOINT PLATE AT RIB 27. OR I: 12 YE674 13000 FC675 OR65000 FHI: 12 YEOR9400 FCOR42400 FH572154-01-1 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP GROUP 42A541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YEOR541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FCGROUP 43A541QB 541RB 541SB 642 OR542AB 542BB 542CB 60000 FH542DB 542EB 542GB I: 12 YE560CB 641FB 641GB OR641HB 641JB 641KB 7300 FC641LB 641MB 641NB OR641PB 641QB 641RB 32100 FH641SB 642AB 642BB642CB 642DB 642EB642GB 660CB572154-01-2 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP GROUP 42B541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YEOR541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FCGROUP 43B541QB 541RB 541SB 642 OR542AB 542BB 542CB 60000 FH542DB 542EB 542GB I: 12 YE641FB 641GB 641HB OR641JB 641KB 641LB 6200 FC641MB 641NB 641PB OR641QB 641RB 641SB 27400 FH642AB 642BB 642CB642DB 642EB 642GBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 118APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572154-01-3 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP GROUP 43C541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YE541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FC541QB 541RB 541SB 642 OR542AB 542BB 542CB 26000 FH542DB 542EB 542GB I: 12 YE641FB 641GB 641HB OR641JB 641KB 641LB 6200 FC641MB 641NB 641PB OR641QB 641RB 641SB 12400 FH642AB 642BB 642CB642DB 642EB 642GBN 572154-01-4 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP GROUP 43E541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND I: 12 YE I: 12 YE541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.541QB 541RB 541SB 642542AB 542BB 542CB542DB 542EB 542GB641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GB572155-01-1 542HB 542JB 542KB 542 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE NO CPCP A340-200550AB 550BB 550CB 550 FORWARD FACE BETWEEN RIB 30 AND RIB 39. I: 12 YE I: 12 YEOR550DB 550EB 550FB 642A340-300642HB 642JB 642KB 650650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 119APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572156-01-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORSEALANT REMOVAL AS RIB 27 60000 FHGROUP 43APER NTM I: 7100 FCOR31200 FH572156-01-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORSEALANT REMOVAL AS RIB 27 60000 FHGROUP 43BPER NTM I: 5400 FCOR23800 FH572156-01-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORSEALANT REMOVAL AS RIB 27 26000 FHPER NTM I: 5400 FCOR10800 FH572156-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORSEALANT REMOVAL AS RIB 27 65000 FHPER NTM I: 11700 FCOR53000 FH572158-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND ORPRE 40610541NB 541PB 541QB RIB 23 60000 FHOR541RB 541SB 641GB I: 6900 FCGROUP 43A641HB 641JB 641KB ORPRE 40610641LB 641MB 641NB 27900 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 120APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572158-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND ORPOST 40610541NB 541PB 541QB RIB 23 60000 FHOR541RB 541SB 641GB I: 6900 FCGROUP 43A641HB 641JB 641KB ORPOST 40610641LB 641MB 641NB 27900 FH641PB 641QB 641RB641SB572158-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OROR541NB 541PB 541QB RIB 23 60000 FHGROUP 43B541RB 541SB 641GB I: 7300 FC641HB 641JB 641KB OR641LB 641MB 641NB 29400 FH641PB 641QB 641RB641SB572158-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR541NB 541PB 541QB RIB 23 26000 FH541RB 541SB 641GB I: 7800 FC641HB 641JB 641KB OR641LB 641MB 641NB 15600 FH641PB 641QB 641RB641SB572158-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR541NB 541PB 541QB RIB 23 65000 FH541RB 541SB 641GB I: 6400 FC641HB 641JB 641KB OR641LB 641MB 641NB 27900 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 121APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572158-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND I: 12 YEOR541NB 541PB 541QB RIB 23.A340-300541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB572159-01-1 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 ORPRE 40610642CB 660CB 60000 FHORI: 6900 FCGROUP 43AORPRE 4061027900 FH572159-01-2 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 ORPOST 40610642CB 660CB 60000 FHORI: 6900 FCGROUP 43AORPOST 4061027900 FH572159-01-3 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OROR60000 FHGROUP 43BI: 7300 FCOR29400 FH572159-01-4 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR26000 FHI: 7800 FCOR15600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 122APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572159-01-5 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR65000 FHI: 6400 FCOR27900 FH572159-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42A560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. I: 12 YEOR642CB 660CBGROUP 43A572159-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42B642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. I: 12 YEORGROUP 43BORGROUP 43C572161-01-1 522EB 522FB 522GB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 42B522HB 522JB 522KB 523 FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. I: 6 YE I: 6 YEOR522LB 522MB 522NB 622GROUP 43B522PB 522QB 522RB 623OR522SB 522TB 523ABGROUP 43C523BB 523CB 523DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 622TB 623AB623BB 623CB 623DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 123APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572161-01-2 522EB 522FB 522GB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 42A522HB 522JB 522KB 523 FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. I: 6 YE I: 6 YEOR522LB 522MB 522NB 622GROUP 43A522PB 522QB 522RB 623522SB 522TB 523AB523BB 523CB 523DB560AB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622QB622RB 622SB 622TB623AB 623BB 623CB623DB 660AB572162-01-1 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42A623 FORWARD FACE SPAR JOINT PLATE AT RIB 27. OROR60000 FHGROUP 43AI: 6900 FCOR30300 FH572162-01-2 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FCGROUP 42B623 FORWARD FACE SPAR JOINT PLATE AT RIB 27 OROR60000 FHGROUP 43BI: 6600 FCPRE 48437OR28800 FH572162-01-3 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 13000 FCGROUP 43C623 FACE SPAR JOINT PLATE AT RIB 27. OR26000 FHI: 8900 FCOR17800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 124APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572162-01-4 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 13000 FCGROUP 43E623 FACE SPAR JOINT PLATE AT RIB 27. OR65000 FHI: 13000 FCOR65000 FH572162-01-5 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP A340-200623 FACE SPAR JOINT PLATE AT RIB 27. I: 6 YE I: 6 YEORA340-300572163-01-1 523EB 523FB 523GB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 12 YE T: 20 YE CPCP A340-200523HB 523JB 523KB 623 FORWARD FACE BETWEEN RIB 27 AND RIB 39. I: 6 YE I: 6 YEOR523LB 523MB 523NBA340-300623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB572164-01-1 N/A TASK DELETED572164-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42A541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YEPOST 40610541NB 541PB 541QB 641 FLANGES 13000 FCOR541RB 541SB 542AB 642 ORGROUP 43A542BB 542CB 542DB 60000 FHPOST 40610560CB 641GB 641HB I: 12 YE641JB 641KB 641LB OR641MB 641NB 641PB 4300 FC641QB 641RB 641SB OR642AB 642BB 642CB 18800 FH642DB 660CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 125APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572164-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42B541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YEOR541NB 541PB 541QB 641 FLANGES 13000 FCGROUP 43B541RB 541SB 542AB 642 OR542BB 542CB 542DB 60000 FH641GB 641HB 641JB I: 12 YE641KB 641LB 641MB OR641NB 641PB 641QB 4600 FC641RB 641SB 642AB OR642BB 642CB 642DB 20300 FH572164-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 43C541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE541NB 541PB 541QB 641 FLANGES 13000 FC541RB 541SB 542AB 642 OR542BB 542CB 542DB 26000 FH641GB 641HB 641JB I: 12 YE641KB 641LB 641MB OR641NB 641PB 641QB 6300 FC641RB 641SB 642AB OR642BB 642CB 642DB 12600 FH572164-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42A541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YEPRE 40610541NB 541PB 541QB 641 FLANGESOR541RB 541SB 542AB 642GROUP 43A542BB 542CB 542DBPRE 40610641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 126APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572164-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 43E541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE541NB 541PB 541QB 641 FLANGES 13000 FC541RB 541SB 542AB 642 OR542BB 542CB 542DB 65000 FH641GB 641HB 641JB I: 12 YE641KB 641LB 641MB OR641NB 641PB 641QB 8100 FC641RB 641SB 642AB OR642BB 642CB 642DB 36500 FH572165-01-1 N/A TASK DELETED572165-01-2 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42A542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEPOST 40610550AB 550BB 550CB 642 FLANGES 13000 FCOR550DB 550EB 550FB 650 ORGROUP 43A642EB 642FB 642GB 60000 FHPOST 40610642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 4300 FCOR18800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 127APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572165-01-3 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42B542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEOR550AB 550BB 550CB 642 FLANGES 13000 FCGROUP 43B550DB 550EB 550FB 650 OR642EB 642FB 642GB 60000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 4600 FCOR20300 FH572165-01-4 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 43C542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE550AB 550BB 550CB 642 FLANGES 13000 FC550DB 550EB 550FB 650 OR642EB 642FB 642GB 26000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 6300 FCOR12600 FH572165-01-5 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 42A542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YEPRE 40610550AB 550BB 550CB 642 FLANGESOR550DB 550EB 550FB 650GROUP 43A642EB 642FB 642GBPRE 40610642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 128APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572165-01-6 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 43E542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE550AB 550BB 550CB 642 FLANGES 13000 FC550DB 550EB 550FB 650 OR642EB 642FB 642GB 65000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 13000 FCOR65000 FH572166-01-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORSEALANT REMOVAL AS RIB 27 60000 FHGROUP 43APER NTM I: 6900 FCOR30300 FH572166-01-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORORSEALANT REMOVAL AS RIB 27 60000 FHGROUP 43BPER NTM I: 6600 FCOR28800 FH572166-01-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORSEALANT REMOVAL AS RIB 27 26000 FHPER NTM I: 8900 FCOR17800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 129APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572166-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT ORSEALANT REMOVAL AS RIB 27 65000 FHPER NTM I: 13000 FCOR65000 FH572171-01-1 541HB 541JB 541KB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB T: 12 YE T: 20 YE NO CPCP GROUP 42A541LB 541MB 541NB 542 39, AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION I: 12 YE I: 12 YEOR541PB 541QB 541RB 550 OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 AND 26GROUP 43A541SB 542AB 542BB 641542CB 542DB 542EB 642542FB 542GB 542HB 650542JB 542KB 550AB550BB 550CB 550DB550EB 550FB 560CB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB 660CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 130APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572171-01-2 541HB 541JB 541KB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB T: 12 YE T: 20 YE NO CPCP GROUP 42B541LB 541MB 541NB 542 39, AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION I: 12 YE I: 12 YEOR541PB 541QB 541RB 550 OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 AND 26GROUP 43B541SB 542AB 542BB 641OR542CB 542DB 542EB 642GROUP 43C542FB 542GB 542HB 650542JB 542KB 550AB550BB 550CB 550DB550EB 550FB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642FB642GB 642HB 642JB642KB 650AB 650BB650CB 650DB 650EB650FB572172-01-1 542CB 542DB 560CB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 12 YE T: 20 YE NO CPCP GROUP 42A642CB 642DB 660CB 642 26 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YE I: 12 YEORGROUP 43A572172-01-2 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 12 YE T: 20 YE NO CPCP GROUP 42B642DB 642 26 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YE I: 12 YEORGROUP 43BORGROUP 43C572173-01-1 560AB 560BB 560CB 560 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 10 YE CPCP GROUP 42A560DB 660AB 660BB 660 LOWER SURFACE COVERED BY PLASTRON FAIRING I: 10 YEOR660CB 660DBGROUP 43AISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 131APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572173-02-1 560AB 560BB 560CB 560 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A560DB 660AB 660BB 660 SKIN LOWER SURFACE COVERED BY PLASTRON OROR660CB 660DB FAIRING 60000 FHGROUP 43AI: 10100 FCOR38100 FH572174-01-1 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 42A541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YEOR641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FCGROUP 43A641NB 641SB 642AB 642 OR60000 FHI: 12 YEOR5400 FCOR23900 FH572174-01-2 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 42B541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YEOR641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FCGROUP 43B641NB 641SB 642AB 642 OR60000 FHI: 12 YEOR6100 FCOR26700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 132APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572174-01-3 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 43C541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YE641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FC641NB 641SB 642AB 642 OR26000 FHI: 12 YEOR7200 FCOR14400 FH572174-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 43E642EB 642 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YESEALANT REMOVAL AS CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FCPER NTM OR65000 FHI: 12 YEOR13000 FCOR65000 FH572180-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A541KB 541LB 541MB 641 SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB OROR541NB 541PB 541QB 23 60000 FHGROUP 43A541RB 541SB 641GB I: 5000 FC641HB 641JB 641KB OR641LB 641MB 641NB 20600 FH641PB 641QB 641RB641SB572180-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B541KB 541LB 541MB 641 SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB OROR541NB 541PB 541QB 23 60000 FHGROUP 43B541RB 541SB 641GB I: 5500 FC641HB 641JB 641KB OR641LB 641MB 641NB 22600 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 133APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572180-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23 OR541NB 541PB 541QB 26000 FH541RB 541SB 641GB I: 5900 FC641HB 641JB 641KB OR641LB 641MB 641NB 11800 FH641PB 641QB 641RB641SB572180-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 A340-200541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. I: 12 YEOR541NB 541PB 541QBA340-300541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB572181-01-1 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A560CB 642AB 642BB 642 SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB OROR642CB 660CB 26 60000 FHGROUP 43AI: 5000 FCOR18900 FH572181-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B642AB 642BB 642CB 642 SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB OROR26 60000 FHGROUP 43BI: 5500 FCOR20700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 134APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572181-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26 OR26000 FHI: 5900 FCOR11800 FH572181-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26 OR65000 FHI: 7400 FCOR32000 FH572181-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42A560CB 642AB 642BB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. I: 12 YEOR642CB 660CBGROUP 43A572181-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 GROUP 42B642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. I: 12 YEORGROUP 43BORGROUP 43C572182-01-1 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OROR550BB 550CB 550DB 642 39 60000 FHGROUP 43A550EB 550FB 642FB 650 I: 12800 FC642GB 642HB 642JB OR642KB 650AB 650BB 48300 FH650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 135APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572182-01-2 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42B542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OROR550BB 550CB 550DB 642 39 60000 FHGROUP 43B550EB 550FB 642FB 650 I: 12500 FC642GB 642HB 642JB OR642KB 650AB 650BB 47200 FH650CB 650DB 650EB650FB572182-01-3 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR550BB 550CB 550DB 642 39 26000 FH550EB 550FB 642FB 650 I: 13000 FC642GB 642HB 642JB OR642KB 650AB 650BB 26000 FH650CB 650DB 650EB650FB572182-01-4 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR550BB 550CB 550DB 642 39 65000 FH550EB 550FB 642FB 650 I: 7400 FC642GB 642HB 642JB OR642KB 650AB 650BB 32000 FH650CB 650DB 650EB650FB572182-02-1 542FB 542GB 542HB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 A340-200542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. I: 12 YEZL-550-01-1 OR550BB 550CB 550DB 642A340-300550EB 550FB 642FB 650642GB 642HB 642JB642KB 650AB 650BB650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 136APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572183-01-1 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORORSTRINGER JOINTS 60000 FHGROUP 43ANOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12800 FCTASK 572183-02-1 OR48300 FH572183-01-2 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORORSTRINGER JOINTS 60000 FHGROUP 43BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12500 FCTASK 572183-02-2 OR47200 FH572183-01-3 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSTRINGER JOINTS 26000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FCTASK 572183-02-3 OR26000 FH572183-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSTRINGER JOINTS 65000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7400 FCTASK 572183-02-4 OR32000 FH572183-02-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND ORORSEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 60000 FHGROUP 43APER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12800 FCTASK 572183-01-1 OR48300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 137APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572183-02-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND ORORSEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 60000 FHGROUP 43BPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12500 FCTASK 572183-01-2 OR47200 FH572183-02-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND ORSEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 26000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FCTASK 572183-01-3 OR26000 FH572183-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND ORSEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 65000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7400 FCTASK 572183-01-4 OR32000 FH572183-03-1 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 A340-200642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING I: 12 YEORSTRINGER JOINTS.A340-300572184-01-1 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42A641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43ATASK 572184-02-1 I: 6100 FCOR23000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 138APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572184-01-2 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 42B641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FHGROUP 43BTASK 572184-02-2 I: 6000 FCOR22600 FH572184-01-3 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43C641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FHTASK 572184-02-3 I: 6400 FCOR12800 FH572184-01-4 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43E641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FHTASK 572184-02-4 I: 13000 FCOR65000 FH572184-02-1 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42ASEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND ORORPER NTM RIB 21 60000 FHGROUP 43ANOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FCTASK 572184-01-1 OR23000 FH572184-02-2 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42BSEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND ORORPER NTM RIB 21 60000 FHGROUP 43BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6000 FCTASK 572184-01-2 OR22600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 139APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572184-02-3 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43CSEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FHTASK 572184-01-3 I: 6400 FCOR12800 FH572184-02-4 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FCGROUP 43ESEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 ORPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FHTASK 572184-01-4 I: 13000 FCOR65000 FH572201-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE CPCP ZL-500-01-2 A340-500600 SKIN LOWER SURFACE BETWEEN RIB 1 AND RIB 12 I: 6 YEORFROM FRONT TO REAR SPAR EXCLUDING AREAS COVEREDA340-600BY INBOARD PYLON FAIRING AND REINFORCING PLATE,MAIN LANDING GEAR REINFORCING PLATE AND FLAPTRACK 2 FAIRING.572202-01-1 PYLON FAIRINGS 460 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP ZL-452-04-1 A340-500470 SKIN LOWER SURFACE VISIBLE PORTION OF INBOARD I: 12 YEORPYLON REINFORCING PLATE AND LOWER SKIN UNDERA340-600PYLON FAIRING.572203-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE CPCP ZL-500-01-2 A340-500600 SKIN MAIN LANDING GEAR REINFORCING PLATE LOWER I: 6 YEORSURFACE.A340-600572204-01-1 FLAP TRACK FAIRINGS 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE CPCP ZL-531-02-2 A340-500631 SKIN IN AREA COVERED BY FLAP TRACK 2 FAIRING. I: 6 YEORA340-600572205-01-1 541AB 541BB 542AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO CPCP A340-500542BB 542CB 542DB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 12 YE I: 12 YEOR641AB 641BB 642AB 641 IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 & 11-12.A340-600642BB 642CB 642DB 642ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 140APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572206-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE CPCP A340-500600 SURFACE AT MLI HOLES AND DRAIN HOLES AFT OF FRONT I: 6 YEORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.A340-600572207-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN VISIBLE T: 6 YE NO CPCP A340-500600 SURFACES OF FUEL PUMP APERTURES IN RIB BAYS I: 6 YEOR3-4 AND 5-6.A340-600572208-01-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP A340-500542AB 542AZ 542BZ 542 UPPER SURFACE, INCLUDING STRINGERS AND BUTTSTRAPS, I: 6 YEOR542DB 641AB 641AZ 641 BETWEEN RIB 1 AND RIB 3 FROM FRONT SPAR TO REAR SPAR,A340-600641BZ 642AB 642AZ 642 BETWEEN RIB 5 AND RIB 7 FROM CENTER SPAR TO REAR SPAR642BZ 642DB AND BETWEEN RIB 11 AND 12 FROM FRONT SPAR TO CENTERSPAR.NOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENT572209-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-03-1 A340-500541BZ 541CZ 542AB 542 STRINGERS BETWEEN RIB 1 & RIB 12, INCLUDING STRINGER I: 12 YEOR542AZ 542BB 542BZ 641 JOINTS, BUTTSTRAPS, JOINT FITTINGS AND ROOT JOINTA340-600542CB 542CZ 542DB 642 FITTINGS.542DZ 542EZ 641AB641AZ 641BB 641BZ641CZ 642AB 642AZ642BB 642BZ 642CB642CZ 642DB 642DZ642EZ572231-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-2 A340-500600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM I: 6 YEORFRONT TO REAR SPAR.A340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 141APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572232-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-03-1 A340-500541BZ 541CZ 542AB 542 STRINGERS BETWEEN RIB 1 AND RIB 12, INCLUDING I: 12 YEZL-542-02-1 OR542AZ 542BB 542BZ 641 STRINGER JOINTS, BUTTSTRAPS, JOINT FITTINGS AND ROOTA340-600542CB 542CZ 542DB 642 JOINT FITTINGS.542DZ 542EZ 641AB641AZ 641BB 641BZ641CZ 642AB 642AZ642BB 642BZ 642CB642CZ 642DB 642DZ642EZ572233-01-1 542BB 542CB 542CZ 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-02-1 A340-500542DB 542DZ 542EZ 642 REINFORCING PLATE LOWER SURFACE AT INNER PYLON. I: 12 YEOR642BB 642CB 642CZA340-600642DB 642DZ 642EZ572241-01-1 573BB 573FB 673BB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE CPCP A340-500673FB 573 AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER I: 12 YEORFLAPS EXTENDED 671 AND LOWER ATTACHMENT ANGLES AND JOINT PLATEA340-600673 AT RIB 9.572244-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP A340-500641 FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YEORA340-600572245-01-1 541AB 541BB 542AB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-03-1 A340-500542BB 542CB 542DB 542 FORWARD FACE BETWEEN RIB 1 AND RIB 12 INCLUDING TOP I: 12 YEZL-542-02-1 OR641AB 641BB 642AB 641 AND BOTTOM FLANGES AND BOLTING.A340-600642BB 642CB 642DB 642572261-01-1 521AB 521BB 521CB 521 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE CPCP ZL-521-01-2 A340-500521DB 521EB 521FB 522 FORWARD FACE BETWEEN RIB 1 AND RIB 12. I: 6 YEZL-522-01-2 OR521GB 521HB 522AB 621A340-600522BB 522CB 621AB 622621BB 621CB 621DB621EB 621FB 621GB621HB 622AB 622BB622CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 142APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572263-01-1 541AZ 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-541-03-1 A340-500541CZ 542AB 542AZ 542 AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING TOP I: 12 YEZL-542-02-1 OR542BB 542BZ 542CB 641 AND BOTTOM FLANGES.A340-600542CZ 542DB 542DZ 642641AZ 641BB 641BZ641CZ 642AB 642AZ642BB 642BZ 642CB642CZ 642DB 642DZ572264-01-1 522EB 622EB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP A340-500622 FACE JOINT PLATE AT RIB 12. I: 12 YE I: 12 YEORA340-600572271-01-1 542AB 542AZ 542BZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6, T: 12 YE NO CPCP ZL-541-03-1 A340-500642AB 642AZ 642BZ 642 FORWARD AND AFT OF CENTER SPAR, AT SKIN ATTACHMENTS I: 12 YEZL-542-02-1 OR(INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OFA340-600STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.572272-01-1 542AB 542BZ 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7, T: 12 YE NO CPCP ZL-542-02-1 A340-500642BZ 642 FORWARD AND AFT OF CENTER SPAR, AT SKIN I: 12 YEORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,A340-600REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.572273-01-1 542BB 542CB 542CZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 8 T: 12 YE NO CPCP ZL-542-02-1 A340-500642BB 642CB 642CZ 642 AND 9, FORWARD AND AFT OF CENTER SPAR, AT SKIN I: 12 YEORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,A340-600REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS. FORWARD FLAP TRACK BRACKET.572274-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 2, T: 12 YE NO CPCP ZL-541-03-1 A340-500541BZ 641AB 641AZ 641 3, 4 AND 5, FORWARD AND AFT OF CENTER SPAR, I: 12 YEOR641BB 641BZ AT SKIN ATTACHMENTS (INCLUDING CLEATS),A340-600SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS,ACCESS CUTOUT SURROUNDS AND MANHOLE BOLTING.572275-01-1 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING BOX, RIB 1 AND T: 6 YE T: 20 YE NO CPCP A340-500641AZ 641 UPPER SURFACE OF TRIFORM FITTING BETWEEN FRONT SPAR I: 6 YE I: 6 YEORAND REAR SPAR.A340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 143APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572276-01-1 542CB 542DB 542DZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 10 T: 12 YE NO CPCP ZL-542-02-1 A340-500542EZ 642CB 642DB 642 FORWARD, RIB 10A AND PYLON DIAPHRAGM. I: 12 YEOR642DZ 642EZA340-600572277-01-1 542AB 542AZ 542BB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 10 T: 12 YE NO CPCP ZL-542-02-1 A340-500542BZ 542CB 542CZ 642 AFT, 11 AND 12, FORWARD AND AFT OF CENTER SPAR, I: 12 YEOR542DB 542DZ 542EB AT SKIN ATTACHMENTS (INCLUDING CLEATS),A340-600542EZ 642AB 642AZ SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS642BB 642BZ 642CB AND ACCESS CUTOUT SURROUNDS.642CZ 642DB 642DZ642EB 642EZ572281-01-1 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 10 YE T: 20 YE NO CPCP A340-500641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. I: 10 YE I: 10 YEORA340-600572282-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING CENTER T: 12 YE NO CPCP ZL-541-03-1 A340-500541BZ 542AB 542AZ 542 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD I: 12 YEZL-542-02-1 OR542BB 542BZ 542CB 641 AND AFT FACES INCLUDING SKIN ATTACHMENTS,A340-600542CZ 542DB 542DZ 642 RIB ATTACHMENTS, AREA AROUND ACCESS HOLES,542EZ 641AB 641AZ DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.641BB 641BZ 642AB642AZ 642BB 642BZ642CB 642CZ 642DB642DZ 642EZ572283-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO CPCP A340-500641 ASSEMBLY AFT FACE BETWEEN RIB 1 AND RIB 2. I: 12 YE I: 12 YEORA340-600572285-01-1 191BT 192BT 192CT 191 DETAILED INSPECTION OF OUTER WING BOX, T: 12 YE 1 CPCP A340-500195CT 192 CRUCIFORM FITTING OUTBOARD FLANGE UPPER SURFACE AS I: 12 YEOR195 FAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RH.A340-600572301-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE CPCP ZL-500-01-2 A340-500600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 27 I: 6 YEORFROM FRONT SPAR TO REAR SPAR EXCLUDING AREASA340-600COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 ANDOUTBOARD PYLON FAIRING.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 144APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572302-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE CPCP ZL-500-01-2 A340-500600 SKIN LOWER SURFACE BETWEEN RIB 27 AND RIB 41 I: 12 YEORFROM FRONT SPAR TO REAR SPAR.A340-600572303-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP A340-500542HB 542JB 542KB 642 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YEOR542LB 542MB 542NB IN ALL BAYS BETWEEN RIBS 12 AND 21 AND BETWEEN RIBSA340-600642EB 642FB 642GB 21 AND 22 FWD.642HB 642JB 642KB642LB 642MB 642NB572304-01-1 542PB 542QB 542SB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP A340-500543AB 543BB 543CB 543 AND I: 6 YEOR543DB 543EB 543FB 550 LOWER SURFACE AROUND ACCESS DOOR CUTOUTS, INCLUDINGA340-600543GB 543HB 543JB 642 NACA DUCT, IN ALL BAYS BETWEEN RIBS 21 AND 22 AFT AND543KB 543LB 543MB 643 BETWEEN RIBS 22 AND 41.543NB 543PB 543QB 650543RB 543SB 543TB543UB 543VB 550AB550BB 550CB 550DB550EB 550FB 642PB642QB 642SB 643AB643BB 643CB 643DB643EB 643FB 643GB643HB 643JB 643KB643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VB 650AB 650BB650CB 650DB 650EB650FB572305-01-1 FLAP TRACK FAIRINGS 450 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP ZL-454-04-1 A340-500OUTBOARD PYLON 480 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP I: 6 YEZL-531-02-2 ORFAIRINGS 532 TRACK FAIRINGS 3, 4, 5 AND OUTBOARD PYLON FAIRING.A340-600533534632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 145APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572306-01-1 PYLON FAIRINGS 450 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO CPCP ZL-452-04-1 A340-500480 SKIN LOWER SURFACE AT FRONT SPAR VISIBLE I: 12 YEZL-454-04-1 ORPORTION OF OUTBOARD PYLON REINFORCING PLATE.A340-600572307-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE CPCP A340-500600 LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK I: 6 YEORCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAINA340-600HOLES AFT OF FRONT SPAR AND FORWARD OF REARSPAR BETWEEN RIBS 12 AND 41.572308-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-02-1 A340-500542HB 542JB 542KB 642 STRINGERS BETWEEN RIB 12 AND RIB 23, INCLUDING I: 12 YEOR542LB 542MB 542NB STRINGER JOINTS, BUTTSTRAPS AND JOINT FITTINGS.A340-600542PB 542QB 542RB542SB 642EB 642FB642GB 642HB 642JB642KB 642LB 642MB642NB 642PB 642QB642RB 642SB572309-01-1 543AB 543BB 543CB 543 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-543-01-1 A340-500543DB 543EB 543FB 550 STRINGERS BETWEEN RIB 23 AND RIB 41, INCLUDING I: 12 YEZL-550-02-1 OR543GB 543HB 543JB 643 STRINGER JOINTS, BUTTSTRAPS AND JOINT FITTINGS.A340-600543KB 543LB 543MB 650543NB 543PB 543QB543RB 543SB 543TB543UB 543VB 550AB550BB 550CB 550DB550EB 550FB 643AB643BB 643CB 643DB643EB 643FB 643GB643HB 643JB 643KB643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VB 650AB 650BB650CB 650DB 650EB650FBVENT PIPES DISPLACEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 146APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572310-01-1 542PB 542QB 542SB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ACCESS T: 12 YE T: 20 YE NO CPCP A340-500543AB 543BB 543CB 543 DOORS BETWEEN RIBS 21 AND 22 AFT AND BETWEEN RIBS 22 I: 12 YE I: 12 YEOR543DB 543EB 543FB 550 AND 41 INCLUDING NACA DUCT DOORA340-600543GB 543HB 543JB 642543KB 543LB 543MB 643543NB 543PB 543QB 650543RB 543SB 543TB543UB 543VB 550AB550BB 550CB 550DB550EB 550FB 642PB642QB 642SB 643AB643BB 643CB 643DB643EB 643FB 643GB643HB 643JB 643KB643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VB 650AB 650BB650CB 650DB 650EB650FB572311-01-1 543AB 543NB 643AB 543 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP A340-500643NB 643 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YEORNOTE: TASK INTERVAL MAY BE INFLUENCED BYA340-600MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENT572312-01-1 550AB 650AB 550 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP A340-500650 UPPER SURFACE BETWEEN RIB 35 AND RIB 36. I: 6 YEORNOTE: TASK INTERVAL MAY BE INFLUENCED BYA340-600MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENT572331-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-2 A340-500600 UPPER SURFACE BETWEEN RIB 12 AND RIB 41 I: 6 YEORFROM FRONT SPAR TO REAR SPAR.A340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 147APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572332-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-02-1 A340-500542HB 542JB 542KB 642 STRINGERS BETWEEN RIB 12 AND RIB 23 INCLUDING I: 12 YEOR542LB 542MB 542NB BUTTSTRAPS AND ALL STRINGER JOINTS.A340-600542PB 542QB 642EB642FB 642GB 642HB642JB 642KB 642LB642MB 642NB 642PB642QB572333-01-1 543AB 543BB 543CB 543 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-543-01-1 A340-500543DB 543EB 543FB 550 STRINGERS BETWEEN RIB 23 AND RIB 41 INCLUDING I: 12 YEZL-550-02-1 OR543GB 543HB 543JB 643 BUTTSTRAPS AND ALL STRINGER JOINTS.A340-600543KB 543LB 543MB 650543NB 543PB 543QB543RB 543SB 543TB543UB 543VB 550AB550BB 550CB 550DB550EB 550FB 643AB643BB 643CB 643DB643EB 643FB 643GB643HB 643JB 643KB643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VB 650AB 650BB650CB 650DB 650EB650FBVENT PIPES DISPLACED572334-01-1 543NB 543PB 543QB 543 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-543-01-1 A340-500643NB 643PB 643QB 643 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YEOROUTBOARD PYLONA340-600FAIRINGSISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 148APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572341-01-1 574AB 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE CPCP A340-500574DB 574EB 574FB 674 FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YEOR574GB 574HB 574JBA340-600574KB 574LB 574MB574NB 674AB 674BB674CB 674DB 674EB674FB 674GB 674HB674JB 674KB 674LB674MB 674NB572342-01-1 575AB 575BB 575CB 575 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE CPCP A340-500575DB 575EB 675AB 675 FACE BETWEEN RIB 27 AND RIB 41. I: 12 YE I: 12 YEOR675BB 675CB 675DBA340-600675EB572343-01-1 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE CPCP A340-500575 FACE SPAR JOINT PLATE AT RIB 27 I: 12 YE I: 12 YEOR674A340-600675572345-01-1 542DB 542EB 542FB 542 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-542-02-1 A340-500542GB 542HB 542JB 543 FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING I: 12 YEZL-543-01-1 OR542KB 542LB 542MB 642 TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATA340-600542NB 542PB 542QB 643 RIB 27.543AB 543BB 543CB543DB 543EB 543FB543GB 642DB 642EB642FB 642GB 642HB642JB 642KB 642LB642MB 642NB 642PB642QB 643AB 643BB643CB 643DB 643EB643FB 643GBVENT PIPES DISPLACEDFROM RIB 23 OUTBOARDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 149APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572346-01-1 543HB 543JB 543KB 543 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP A340-500543LB 543MB 550AB 550 FACE BETWEEN RIB 30 AND RIB 41. I: 12 YE I: 12 YEOR550BB 550CB 550DB 643A340-600550EB 550FB 643HB 650643JB 643KB 643LB643MB 650AB 650BB650CB 650DB 650EB650FBVENT PIPES DISPLACED572361-01-1 522EB 522GB 522HB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP A340-500522KB 522MB 522PB 523 FACE BETWEEN RIB 12 AND RIB 26, AS FAR AS VISIBLE. I: 6 YE I: 6 YEOR523AB 523BB 523CB 622A340-600523DB 622EB 622GB 623622HB 622KB 622MB622PB 623AB 623BB623CB 623DB572362-01-1 523DB 623DB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP A340-500623 FACE SPAR JOINT PLATE AT RIB 26. I: 12 YE I: 12 YEORA340-600572364-01-1 523DB 523FB 523HB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP A340-500523KB 523MB 523PB 623 FACE BETWEEN RIB 26 AND RIB 41. I: 6 YE I: 6 YEOR523QB 623DB 623FBA340-600623HB 623KB 623MB623PB 623QB572365-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-542-02-1 A340-500542HB 542JB 542KB 543 AFT FACE BETWEEN RIB 12 AND RIB 26 INCLUDING TOP AND I: 12 YEZL-543-01-1 OR542LB 542MB 542NB 642 BOTTOM FLANGES.A340-600542RB 542SB 543NB 643543PB 642EB 642FB642GB 642HB 642JB642KB 642LB 642MB642NB 642RB 642SB643NB 643PBVENT PIPES DISPLACEDFROM RIB 23 OUTBOARDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 150APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572366-01-1 543JB 543KB 543LB 543 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT T: 12 YE T: 20 YE NO CPCP A340-500543MB 543QB 543RB 550 FACE BETWEEN RIB 26 AND 41 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YEOR543SB 543TB 543UB 643 FLANGES,A340-600543VB 550AB 550BB 650550CB 550DB 550EB550FB 643JB 643KB643LB 643MB 643QB643RB 643SB 643TB643UB 643VB 650AB650BB 650CB 650DB650EB 650FBVENT PIPES DISPLACED572371-01-1 542FB 542GB 542HB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 14 T: 12 YE NO CPCP ZL-542-02-1 A340-500542JB 542KB 542LB 543 TO 41 AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND I: 12 YEZL-543-01-1 OR542MB 542NB 542PB 550 REGION OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 & 25ZL-550-02-1 A340-600542QB 542RB 542SB 642543AB 543BB 543CB 643543DB 543EB 543FB 650543GB 543HB 543JB543KB 543LB 543MB543NB 543PB 543QB543RB 543SB 543TB543UB 543VB 550AB550BB 550CB 550DB550EB 550FB 642FB642GB 642HB 642JB642KB 642LB 642MB642NB 642PB 642QB642RB 642SB 643AB643BB 643CB 643DB643EB 643FB 643GB643HB 643JB 643KB643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VB 650AB 650BB650CB 650DB 650EB650FBVENT PIPES DISPLACEDFROM RIB 23 OUTBOARDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 151APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572372-01-1 543BB 543CB 543PB 543 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 25 T: 12 YE NO CPCP ZL-543-01-1 A340-500543QB 643BB 643CB 643 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YEOR643PB 643QBA340-600OUTBOARD PYLONFAIRINGSVENT PIPES DISPLACEDFROM RIB 23 OUTBOARD572373-01-1 542EB 542FB 542KB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 13, T: 12 YE NO CPCP ZL-542-02-1 A340-500542LB 542QB 542SB 543 18 AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGER I: 12 YEZL-543-01-1 OR543AB 543NB 642EB 642 CUTOUTS AND FORWARD FLAP TRACK BRACKETS.A340-600642FB 642KB 642LB 643642QB 642SB 643AB643NB572601-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE CPCP ZL-571-01-1 A340-200671 LANDING GEAR SIDE STAY FITTING (RIB 2). I: 12 YEORA340-300572602-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE CPCP ZL-571-01-1 A340-200671 LANDING GEAR FORWARD PINTLE FITTING (RIB 5). I: 12 YEORA340-300572603-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE CPCP ZL-571-01-1 A340-200671 LANDING GEAR RETRACTION JACK FITTING. I: 12 YEORA340-300572604-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE CPCP ZL-571-01-1 A340-200671 LANDING GEAR SUPPORT RIB 6. I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 152APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572605-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42A673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YEORFLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FCGROUP 43AINTERFACE PLATE AND THRUST PADS). I: 12 YEORORGROUP 42B4700 FCORGROUP 43B572605-01-2 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43C673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YEFLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FCINTERFACE PLATE AND THRUST PADS). I: 12 YEOR5600 FC572605-01-5 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43E673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YEFLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FCINTERFACE PLATE AND THRUST PADS). I: 12 YEOR13000 FC572606-01-1 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 T: 13000 FCA340-200632CB 633CB 634CB 533 AND 5 AFT PICK-UP ASSEMBLY I: 13000 FCOR534GROUP 43A632OR633GROUP 43B634PRE 48437ORGROUP 43C572606-02-1 532CB 533CB 534CB 532 GENERAL VISUAL INSPECTION OF OUTER WING FLAP TRACKS T: 12 YE CPCP ZL-531-02-1 A340-200632CB 633CB 634CB 533 3, 4 AND 5 AFT PICK-UP ASSEMBLY I: 12 YEOR534A340-300632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 153APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572607-01-1 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE CPCP GROUP 42A532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YEOR534AB 534CB 631AB 533 13000 FCGROUP 43A631CB 632AB 632CB 534 I: 12 YEOR633AB 633CB 634AB 631 ORGROUP 42B634CB 632 9200 FCOR633GROUP 43B634572607-01-2 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE CPCP GROUP 43C532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YE534AB 534CB 631AB 533 13000 FC631CB 632AB 632CB 534 I: 12 YE633AB 633CB 634AB 631 OR634CB 632 7300 FC633634572607-01-3 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE CPCP GROUP 43E532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YE534AB 534CB 631AB 533 13000 FC631CB 632AB 632CB 534 I: 12 YE633AB 633CB 634AB 631 OR634CB 632 9200 FC633634572607-02-1 N/A TASK DELETED572608-01-1 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCA340-200522CT 622AB 622AT 622 INNER PYLON INBOARD AND OUTBOARD FORWARD I: 13000 FCOR622BB 622CT ATTACHMENT FITTINGSA340-300ENGINELINKSSLEEVESISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 154APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572609-01-1 523AB 523AT 523BB 523 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCA340-200523CT 523QB 623AB 623 OUTER PYLON INBOARD AND OUTBOARD FORWARD I: 13000 FCOR623AT 623BB 623CT ATTACHMENT FITTINGSA340-300623QBENGINELINKSSLEEVES572610-01-1 462GR 462HL 463CL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON SPIGOT T: 12 YE T: 20 YE NO CPCP A340-200463CR 464AL 464AR 641 FITTING. I: 12 YE I: 12 YEPRE 43183472GL 472HR 473CLOR473CR 474AL 474ARA340-300SPIGOT SLEEVEPRE 43183572610-01-3 462GR 462HL 463CL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON SPIGOT T: 12 YE T: 20 YE NO CPCP A340-200463CR 464AL 464MR 641 FITTING. I: 12 YE I: 12 YEPOST 43183472GL 472HR 473CLOR473CR 474AL 474MRA340-300SPIGOT SLEEVEPOST 43183572610-02-1 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FCA340-200464AR 472GL 472HR 641 SPIGOT FITTING I: 13000 FCPRE 43183474AL 474ARORGROUP 43APRE 43183ORGROUP 43BPRE 43183ORGROUP 43CPRE 43183ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 155APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572610-02-6 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FCA340-200464MR 472GL 472HR 641 SPIGOT FITTING I: 13000 FCPOST 43183474AL 474MRORGROUP 43APOST 43183ORGROUP 43BPOST 43183ORGROUP 43CPOST 43183572610-02-7 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FCGROUP 43E464MR 472GL 472HR 641 SPIGOT FITTING OR474AL 474MR 65000 FHI: 11400 FCOR51500 FH572611-01-1 452EL 452FR 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO CPCP A340-200453CR 454AL 454AR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YEPRE 42283482ER 482FL 483CLPRE 41371483CR 484AL 484ARORSPIGOT SLEEVEA340-300PRE 42283PRE 41371572611-01-2 452KL 452MR 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO CPCP A340-200453CR 454AL 454KR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YEPOST 41371482MR 482NL 483CLPOST 42283483CR 484AR 484MLORSPIGOT SLEEVEA430-300POST 41371POST 42283ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 156APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572611-01-3 452FR 452GL 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO CPCP A340-200453CR 454AL 454AR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YEPOST 41371482FL 482HR 483CLPRE 42283483CR 484AL 484ARORSPIGOT SLEEVEA340-300POST 41371PRE 42283572611-02-1 452EL 452FR 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCA340-200454AR 482ER 482FL 642 OUTER PYLON SPIGOT FITTING I: 13000 FCPRE 42283484AL 484ARPRE 41371ORGROUP 43APRE 42283PRE 41371ORGROUP 43BPRE 42283PRE 41371ORGROUP 43CPRE 42283PRE 41371572611-02-2 452KL 452MR 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCA340-200454KR 482MR 482NL 642 OUTER PYLON SPIGOT FITTING I: 13000 FCPOST 41371484AR 484MLPOST 42283ORA430-300POST 41371POST 42283572611-02-3 452FR 452GL 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCA340-200454AR 482FL 482HR 642 OUTER PYLON SPIGOT FITTING I: 13000 FCPOST 41371484AL 484ARPRE 42283ORA340-300POST 41371PRE 42283ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 157APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572611-02-4 452FR 452GL 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E454AR 482FL 482HR 642 OUTER PYLON SPIGOT FITTING OR484AL 484AR 65000 FHI: 11400 FCOR51500 FH572612-01-1 464BL 464BR 464FL 541 DETAILED INSPECTION OF OUTER WING INNER T: 12 YE T: 20 YE NO CPCP A340-200464FR 474BL 474BR 641 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEPRE 43183474FL 474FRORPIPE SUPPORT BRACKETA340-300REMOVED OR DISPLACEDPRE 43183572612-01-2 464JL 464JR 464KL 541 DETAILED INSPECTION OF OUTER WING INNER T: 12 YE T: 20 YE NO CPCP A340-200464KR 474JL 474JR 641 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEPOST 43183474KL 474KRORPIPE SUPPORT BRACKETA340-300REMOVED OR DISPLACEDPOST 43183572612-02-1 464BL 464BR 464FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A464FR 474BL 474BR 641 INNER PYLON AFT ATTACHMENT FITTING ORPRE 43183474FL 474FR 60000 FHORPIPE SUPPORT BRACKET I: 13000 FCGROUP 43AREMOVED OR DISPLACED ORPRE 4318360000 FH572612-02-13 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING OR474KL 474KR 65000 FHPIPE SUPPORT BRACKET I: 13000 FCREMOVED OR DISPLACED OR65000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 158APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572612-02-2 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING OR474KL 474KR 26000 FHPIPE SUPPORT BRACKET I: 13000 FCREMOVED OR DISPLACED OR26000 FH572612-02-3 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING ORPOST 43183474KL 474KR 60000 FHORPIPE SUPPORT BRACKET I: 13000 FCGROUP 43AREMOVED OR DISPLACED ORPOST 4318360000 FHORGROUP 42BORGROUP 43B572613-01-1 N/A TASK DELETED572613-01-3 454BL 454BR 454FL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO CPCP A340-200454FR 484BL 484BR 642 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEPRE 42283484FL 484FRORA340-300PRE 42283572613-01-4 454BL 454MR 454NR 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO CPCP A340-200454QL 484NL 484NR 642 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEPOST 42283484PL 484PRORA340-300POST 42283ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 159APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572613-02-1 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING ORPRE 42283484FL 484FR 60000 FHORI: 13000 FCGROUP 43AORPRE 4228360000 FHORGROUP 42BPRE 42283ORGROUP 43BPRE 42283572613-02-2 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING OR484FL 484FR 26000 FHI: 13000 FCOR26000 FH572613-02-3 454BL 454MR 454NR 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A454QL 484NL 484NR 642 OUTER PYLON AFT ATTACHMENT FITTING ORPOST 42283484PL 484PR 60000 FHORI: 13000 FCGROUP 43AORPOST 4228360000 FHORGROUP 42BPOST 42283ORGROUP 43BPOST 42283572613-02-4 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING OR484FL 484FR 65000 FHI: 13000 FCOR65000 FH572614-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 160APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572614-02-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE CPCP ZL-733-01-1 A340-200743 HINGED DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YEORA340-300572615-01-1 N/A TASK DELETED572615-02-1 732 742 732 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR LEG T: 6 YE CPCP ZL-732-01-1 A340-200742 FAIRING ATTACHMENT ASSEMBLIES TO LEG STRUCTURE. I: 6 YEORA340-300572616-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING LOWER T: 3 YEGROUP 42A600 SURFACE PLASTRON FAIRING ASSEMBLY (LOWER I: 3 YEORSURFACE)GROUP 43AN 572617-01-1 734 744 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YEA340-200671 SUPPORT RIB 6 BEARING LUGS. I: 12 YEPOST 49353ORA340-300POST 49353572651-01-1 732 742 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE CPCP ZL-572-01-2 A340-500671 LANDING GEAR SIDE STAY FITTING (RIB 2). I: 12 YEORA340-600572652-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE CPCP A340-500671 FORWARD PINTLE FITTING (RIB 5). I: 12 YEORA340-600572653-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE CPCP A340-500671 RETRACTION JACK FITTING, I: 12 YEORA340-600572654-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE CPCP A340-500671 SUPPORT RIB 6. I: 12 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 161APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572655-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-500673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND I: 12 YE I: 12 YEORFLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET,A340-600INTERFACE PLATE AND THRUST PADS).572656-01-1 532SB 533SB 534SB 574 GENERAL VISUAL INSPECTION OF OUTER WING FLAP T: 12 YE CPCP ZL-531-02-2 A340-500632SB 633SB 634SB 674 TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. I: 12 YEORA340-600572657-01-1 531VT 531WB 532VT 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, T: 12 YE T: 20 YE CPCP A340-500532WB 533VT 533WB 532 4 AND 5 FORWARD PICK-UP FITTINGS LUGS. I: 12 YE I: 12 YEOR534VT 534WB 631VT 533A340-600631WB 632VT 632WB 534633VT 633WB 634VT 631634WB 632633634572660-01-1 462GR 462JL 464AL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON T: 12 YE T: 20 YE NO CPCP A340-500464AR 472GR 472JL 641 SPIGOT FITTING. I: 12 YE I: 12 YEOR474AL 474ARA340-600SPIGOT SLEEVE572661-01-1 452EL 452GR 454AL 542 DETAILED INSPECTION OF OUTER WING OUTER PYLON T: 12 YE T: 20 YE NO CPCP A340-500482EL 482GR 484AL 642 SPIGOT FITTING. I: 12 YE I: 12 YEORSPIGOT SLEEVEA340-600572662-01-1 464AL 464AR 464BL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON T: 12 YE T: 20 YE NO CPCP A340-500464BR 474AL 474AR 641 AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEOR474BL 474BRA340-600572663-01-1 454AL 454AR 454BL 542 DETAILED INSPECTION OF OUTER WING OUTER PYLON T: 12 YE T: 20 YE NO CPCP A340-500454BR 484AL 484AR 642 AFT ATTACHMENT FITTING. I: 12 YE I: 12 YEOR484BL 484BRA340-600572664-01-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE CPCP ZL-733-01-2 A340-500743 HINGED DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 162APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS572665-01-1 732 742 732 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE CPCP ZL-731-01-1 A340-500742 LEG FAIRING ATTACHMENT ASSEMBLIES TO LEG STRUCTURE. I: 6 YEZL-732-01-2 ORA340-600573001-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP GROUP 42A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YEPRE 41460REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FCORORGROUP 43A60000 FHPRE 41460I: 12 YEOR5500 FCOR28900 FH573001-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP GROUP 42A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YEPOST 41460REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FCORORGROUP 43A60000 FHPOST 41460I: 12 YEOR2900 FCOR15300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 163APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS573001-01-3 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP GROUP 42B635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YEORREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FCGROUP 43BOR60000 FHI: 12 YEOR4200 FCOR22300 FH573001-01-4 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP GROUP 43C635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YEREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FCOR26000 FHI: 12 YEOR5100 FCOR10200 FH573001-01-5 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP GROUP 43E635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YEREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FCOR65000 FHI: 12 YEOR6900 FCOR31200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 164APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS573002-01-1 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE ORPRE 4146060000 FHORI: 5500 FCGROUP 43AORPRE 4146029400 FH573002-01-2 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FCGROUP 42A600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE ORPOST 4146060000 FHORI: 2900 FCGROUP 43AORPOST 4146015300 FH573002-01-3 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FCGROUP 42B600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OROR60000 FHGROUP 43BI: 4200 FCOR22300 FH573002-01-4 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FCGROUP 43C600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR26000 FHI: 5100 FCOR10200 FH573002-01-5 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FCGROUP 43E600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR65000 FHI: 6900 FCOR31200 FH573002-02-1 N/A 500 GENERAL VISUAL INSPECTION OF WING TIP BOX TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 A340-200600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. I: 6 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 165APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS573003-01-1 WINGLET 535 DETAILED INSPECTION OF WINGTIP TO WINGLET T: 12 YE T: 20 YE CPCP A340-200635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET) I: 12 YE I: 12 YEORA340-300573003-02-1 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FCGROUP 42A635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND ORORWINGLET) 60000 FHGROUP 43AI: 6400 FCOR33900 FH573003-02-2 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FCGROUP 42B635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND ORORWINGLET) 60000 FHGROUP 43BI: 6100 FCPRE 48437OR32400 FH573003-02-3 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FCGROUP 43C635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND ORWINGLET) 26000 FHI: 7300 FCOR14600 FH573003-02-4 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FCGROUP 43E635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND ORWINGLET) 65000 FHI: 12700 FCOR57400 FH573004-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE CPCP A340-200635BZ 635 AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 166APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS573004-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 13000 FCGROUP 43E635BZ 635 AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. OR65000 FHI: 6700 FCOR30200 FC573005-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WING WINGTIP TO T: 12 YE CPCP A340-200635BB 635 WINGLET JOINT BOLTS. I: 12 YEORJOINT BOLTSA340-300573006-01-1 N/A 500 GENERAL VISUAL INSPECTION OF WINGLET EXTERNAL SURFACE T: 5 YE NO CPCP ZL-500-02-1 A340-200600 I: 5 YEORA340-300573051-01-1 535AT 535CZ 635AT 535 SPECIAL DETAILED INSPECTION OF OUTER WING WINGTIP TO T: 12 YE T: 20 YE CPCP A340-500635CZ 635 MAIN WINGBOX JOINT AT RIB 41 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YEORTRAILING EDGE SKINS, FRONT AND REAR SPARS AND ALL FITTINGS ANDA340-600SECTION BUTTSTRAPS.573052-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING WINGTIP T: 6 YE CPCP ZL-500-02-2 A340-500600 BOX TOP SKIN UPPER SURFACE AND BOTTOM SKIN I: 6 YEORLOWER SURFACE.A340-600573053-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WINGTIP TO WINGLET T: 12 YE T: 20 YE CPCP A340-500635BB 635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). I: 12 YE I: 12 YEORA340-600573054-01-1 535AB 535BB 635AB 535 SPECIAL DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE CPCP A340-500635BB 635 AFT I: 12 YE I: 12 YEORFITTING BOTTOM FLANGE TO SKIN ATTACHMENTA340-600573055-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE CPCP A340-500635BB 635 TO WINGLET JOINT BOLTS. I: 12 YE I: 12 YEORJOINT BOLTSA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 167APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS573056-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING WINGLET T: 10 YE CPCP ZL-500-02-2 A340-500600 EXTERNAL SURFACE. I: 10 YEORA340-600574101-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP A340-200521GB 521JB 522CB 522 LEADING EDGE TRACK RIBS 1 TO 16. I: 12 YE I: 12 YEOR522JB 522LB 522NB 523A340-300522RB 522TB 523CB 621523EB 523GB 523JB 622523LB 523NB 621BB 623621CB 621DB 621GB621JB 622CB 622JB622LB 622NB 622RB622TB 623CB 623EB623GB 623JB 623LB623NB574102-01-1 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OROR522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 60000 FHGROUP 43A522RB 522TB 523CB 621 I: 11000 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 48000 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-2 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OROR522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 60000 FHGROUP 43B522RB 522TB 523CB 621 I: 10400 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 45400 FH622JB 622LB 622NB622RB 622TB 623CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 168APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574102-01-3 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 26000 FH522RB 522TB 523CB 621 I: 10400 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 20800 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-4 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 65000 FH522RB 522TB 523CB 621 I: 13000 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 65000 FH622JB 622LB 622NB622RB 622TB 623CB574103-01-1 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42A522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YEOR522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FCGROUP 43A522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR522UB 523AB 523BB 622 60000 FH560AB 621DB 621FB 623 I: 12 YE621GB 622AB 622BB OR622CB 622EB 622GB 4300 FC622HB 622JB 622NB OR622RB 622UB 623AB 18700 FH623BB 660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 169APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574103-01-2 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42B522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YEOR522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FCGROUP 43B522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR522UB 523AB 523BB 622 60000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 5300 FC622JB 622NB 622RB OR622UB 623AB 623BB 23100 FH574103-01-3 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43C522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR522UB 523AB 523BB 622 26000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 5300 FC622JB 622NB 622RB OR622UB 623AB 623BB 10600 FH574103-01-4 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43E522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR522UB 523AB 523BB 622 65000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 5500 FC622JB 622NB 622RB OR622UB 623AB 623BB 25100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 170APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574104-01-1 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FCGROUP 42A521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OROR521GB 521JB 522AB 523 60000 FHGROUP 43A522BB 522CB 522DB 621 I: 13000 FC522EB 522FB 522GB 622 OR522HB 522JB 522LB 623 60000 FH522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB523GB 523HB 523JB523LB 523MB 523NB523PB 560AB 621AB621BB 621CB 621DB621EB 621FB 621GB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622LB 622MB622NB 622PB 622QB622RB 622SB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623LB623MB 623NB 623PB660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 171APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574104-01-2 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FCGROUP 42B521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OROR521GB 521JB 522AB 523 60000 FHGROUP 43B522BB 522CB 522DB 621 I: 8900 FC522EB 522FB 522GB 622 OR522HB 522JB 522LB 623 38800 FH522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB523GB 523HB 523JB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622LB 622MB 622NB622PB 622QB 622RB622SB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 172APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574104-01-3 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FCGROUP 43C521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR521GB 521JB 522AB 523 26000 FH522BB 522CB 522DB 621 I: 8900 FC522EB 522FB 522GB 622 OR522HB 522JB 522LB 623 17800 FH522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB523GB 523HB 523JB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622LB 622MB 622NB622PB 622QB 622RB622SB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 173APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574104-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FCGROUP 43E521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR521GB 521JB 522AB 523 65000 FH522BB 522CB 522DB 621 I: 7800 FC522EB 522FB 522GB 622 OR522HB 522JB 522LB 623 35200 FH522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB523GB 523HB 523JB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622LB 622MB 622NB622PB 622QB 622RB622SB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623LB 623MB623NB 623PB574105-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42A521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YEOR522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FCGROUP 43A522RB 522TB 523CB 621 OROR523EB 523GB 523JB 622 60000 FHGROUP 42B523LB 523NB 621BB 623 I: 12 YEOR621CB 621DB 621GB ORGROUP 43B621JB 622CB 622JB 4400 FC622LB 622NB 622RB OR622TB 623CB 623EB 19200 FH623GB 623JB 623LB623NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 174APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574105-01-2 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43C521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YE522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 26000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 6500 FC622LB 622NB 622RB OR622TB 623CB 623EB 13000 FH623GB 623JB 623LB623NB574105-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43E521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YE522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 65000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 7400 FC622LB 622NB 622RB OR622TB 623CB 623EB 33400 FH623GB 623JB 623LB623NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 175APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574106-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42A521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OROR521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 60000 FHGROUP 43A522CB 522DB 522EB 621 I: 13000 FC522FB 522GB 522HB 622 OR522JB 522KB 522LB 623 60000 FH522MB 522NB 522PB522QB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB560AB 621BB 621CB621DB 621EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB 660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 176APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574106-01-2 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42B521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OROR521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 60000 FHGROUP 43B522CB 522DB 522EB 621 I: 13000 FC522FB 522GB 522HB 622 OR522JB 522KB 522LB 623 60000 FH522MB 522NB 522PB522QB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 177APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574106-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43C521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 26000 FH522CB 522DB 522EB 621 I: 13000 FC522FB 522GB 522HB 622 OR522JB 522KB 522LB 623 26000 FH522MB 522NB 522PB522QB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 178APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574106-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43E521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 65000 FH522CB 522DB 522EB 621 I: 13000 FC522FB 522GB 522HB 622 OR522JB 522KB 522LB 623 65000 FH522MB 522NB 522PB522QB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 179APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574106-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP A340-200521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK I: 12 YE I: 12 YEOR521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16.A340-300522CB 522DB 522EB 621522FB 522GB 522HB 622522JB 522KB 522LB 623522MB 522NB 522PB522QB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB560AB 621BB 621CB621DB 621EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB 660AB574107-01-1 521FB 521GB 521JB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42A522AB 522BB 522CB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YEOR522DB 522EB 522FB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12.GROUP 43A522GB 522HB 522JB 621522KB 522LB 522MB 622522NB 522PB 522QB 623523AB 523BB 523CB523DB 523EB 560AB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 623AB623BB 623CB 623DB623EB 660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 180APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574107-01-3 521FB 521GB 521JB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42B522AB 522BB 522CB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YEOR522DB 522EB 522FB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12.GROUP 43B522GB 522HB 522JB 621OR522KB 522LB 522MB 622GROUP 43C522NB 522PB 522QB 623523AB 523BB 523CB523DB 523EB 523FB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622LB 622MB 622NB622PB 622QB 622RB622SB 623AB 623BB623CB 623DB 623EB623FB574107-02-1 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OROR522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 60000 FHGROUP 43A522GB 522HB 522JB 621 I: 9700 FC522KB 522LB 522MB 622 OR522NB 522PB 522QB 623 42300 FH523AB 523BB 523CB523DB 523EB 560AB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 623AB623BB 623CB 623DB623EB 660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 181APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574107-02-2 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OROR522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 60000 FHGROUP 43B522GB 522HB 522JB 621 I: 9100 FC522KB 522LB 522MB 622 OR522NB 522PB 522QB 623 39700 FH523AB 523BB 523CB523DB 523EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB574107-02-3 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OR522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 26000 FH522GB 522HB 522JB 621 I: 9400 FC522KB 522LB 522MB 622 OR522NB 522PB 522QB 623 18800 FH523AB 523BB 523CB523DB 523EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB574108-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE CPCP ZL-521-01-1 A340-200621 LEADING EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, I: 12 YEORMAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.A340-300574109-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 182APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574109-01-2 N/A TASK DELETED574109-01-3 N/A TASK DELETED574109-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43E521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND OR521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS 65000 FH522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND I: 5200 FC522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS. OR522HB 522JB 522KB 623 23400 FH522LB 522MB 522NB522PB 522QB 523AB523BB 523CB 523DB523EB 523FB 523GB523HB 523JB 523LB523MB 523NB 523QB621AB 621BB 621CB621DB 621EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623LB623MB 623NB 623QBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 183APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574109-01-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42A521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND I: 12 YE I: 12 YEOR521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBSGROUP 43A522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS.522HB 522JB 522KB 623522LB 522MB 522NB522PB 522QB 523AB523BB 523CB 523DB523EB 523FB 523GB523HB 523JB 523LB523MB 523NB 523QB560AB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623LB623MB 623NB 623QB660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 184APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574109-01-6 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42B521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND I: 12 YE I: 12 YEOR521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBSGROUP 43B522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) ANDPRE 48437522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS.OR522HB 522JB 522KB 623GROUP 43C522LB 522MB 522NBOR522PB 522QB 523ABGROUP 43E523BB 523CB 523DB523EB 523FB 523GB523HB 523JB 523LB523MB 523NB 523QB621AB 621BB 621CB621DB 621EB 621FB621GB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623LB623MB 623NB 623QB574110-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO CPCP GROUP 42A600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YEORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 60000 FHGROUP 43AI: 10400 FCOR39300 FH574110-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO CPCP GROUP 42B600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YEORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 60000 FHGROUP 43BI: 11200 FCOR42300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 185APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574110-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC NOGROUP 43C600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE ORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 26000 FHI: 11600 FCOR23200 FH574110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 6 YE NO CPCP GROUP 43C600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 6 YEFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9574110-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO CPCP GROUP 43E600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YEFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 65000 FHI: 13000 FCOR65000 FH574111-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42A600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE ORORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 60000 FHGROUP 43AI: 9400 FCOR49800 FH574111-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42B600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE ORORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 60000 FHGROUP 43BI: 10100 FCOR53500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 186APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574111-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43C600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE ORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 26000 FHI: 11600 FCOR23200 FH574111-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43E600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE ORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 65000 FHI: 7200 FCOR33200 FH574111-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE NO CPCP ZL-500-02-1 A340-200600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE I: 6 YEORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39A340-300574112-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP A340-200623NB 623 LEADING EDGE HOLD DOWN RIB BETWEEN SLAT TRACK RIB I: 12 YE I: 12 YEOR15 AND SLAT TRACK 16, AREA OF SLAT TRACK BRAKEA340-300FITTING.574114-01-1 560AB 660AB 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42A600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE ORORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 60000 FHGROUP 43A26 TO RIB 39 I: 10400 FCOR39300 FH574114-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 42B600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE ORORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 60000 FHGROUP 43B26 TO RIB 39 I: 11200 FCOR42300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 187APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574114-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43C600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE ORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26000 FH26 TO RIB 39 I: 11600 FCOR23200 FH574114-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FCGROUP 43E600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE ORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 65000 FH26 TO RIB 39 I: 13000 FCOR65000 FH574114-02-1 560AB 660AB 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE NO CPCP ZL-500-01-1 GROUP 42A600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 12 YEORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIBGROUP 43A26 TO RIB 39.574114-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE NO CPCP GROUP 42B600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 12 YEORFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIBGROUP 43B26 TO RIB 39.ORGROUP 43CISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 188APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574115-01-1 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42A523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YEOR560AB 622AB 622BB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FCGROUP 43A622CB 623AB 623BB 623 AND RIB 24 TO RIB 26 OR623CB 660AB 60000 FHI: 12 YEOR4200 FCOR15800 FH574115-01-2 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 42B523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YEOR622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FCGROUP 43B623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR60000 FHI: 12 YEOR3100 FCOR11700 FH574115-01-3 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43C523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR26000 FHI: 12 YEOR4600 FCOR9200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 189APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574115-01-4 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP GROUP 43E523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR65000 FHI: 12 YEOR13000 FCOR65000 FH574116-01-1 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 42A521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEOR521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FCGROUP 43A522BB 522CB 522DB 621 HOLD DOWN RIBS OR522EB 522FB 522GB 622 60000 FH522HB 522JB 522KB 623 I: 12 YE522LB 522MB 522NB OR522PB 522QB 523AB 5500 FC523BB 523CB 523DB OR523EB 523FB 523GB 24000 FH523HB 523JB 523KB523LB 523MB 523NB523PB 560AB 621AB621BB 621CB 621DB621EB 621FB 621GB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 623AB 623BB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PB660ABISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 190APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574116-01-2 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 42B521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEOR521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FCGROUP 43B522BB 522CB 522DB 621 HOLD DOWN RIBS OR522EB 522FB 522GB 622 60000 FH522HB 522JB 522KB 623 I: 12 YE522LB 522MB 522NB OR522PB 522QB 523AB 3100 FC523BB 523CB 523DB OR523EB 523FB 523GB 13500 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622QB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 191APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574116-01-3 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 43C521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC522BB 522CB 522DB 621 HOLD DOWN RIBS OR522EB 522FB 522GB 622 26000 FH522HB 522JB 522KB 623 I: 12 YE522LB 522MB 522NB OR522PB 522QB 523AB 9400 FC523BB 523CB 523DB OR523EB 523FB 523GB 18800 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622QB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 192APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574116-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 43E521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC522BB 522CB 522DB 621 HOLD DOWN RIBS OR522EB 522FB 522GB 622 65000 FH522HB 522JB 522KB 623 I: 12 YE522LB 522MB 522NB OR522PB 522QB 523AB 13000 FC523BB 523CB 523DB OR523EB 523FB 523GB 65000 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622QB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PB574119-01-1 521BB 521GB 523GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE CPCP A340-200523JB 523LB 523NB 523 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YEOR621BB 621GB 623GB 621 STRAPS AT TRACKS RIBS 1 AND 2 AND TRACKA340-300623JB 623LB 623NB 623 RIBS 13 TO 16ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 193APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574151-01-1 521BB 521CB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500521HB 522CB 522EB 522 TRACK RIBS 1 TO 17. I: 12 YE I: 12 YEOR522GB 522HB 522KB 523A340-600522MB 522PB 523BB 621523CB 523DB 523FB 622523HB 523KB 523MB 623523PB 523QB 621BB621CB 621FB 621HB622CB 622EB 622GB622HB 622KB 622MB622PB 623BB 623CB623DB 623FB 623HB623KB 623MB 623PB623QB574153-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING I: 12 YE I: 12 YEOR522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.A340-600522KB 522MB 522PB 621522QB 522RB 522UB 622523AB 523BB 523DB 623523FB 523HB 523KB523MB 523PB 523QB621CB 621EB 621FB622AB 622BB 622CB622EB 622GB 622HB622KB 622MB 622PB622QB 622RB 622UB623AB 623BB 623DB623FB 623HB 623KB623MB 623PB 623QBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 194APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574155-01-1 521BB 521CB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500521HB 522BB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 17. I: 12 YE I: 12 YEOR522EB 522GB 522HB 523A340-600522KB 522MB 522QB 621523BB 523CB 523DB 622523FB 523HB 523KB 623523MB 523PB 523QB621BB 621CB 621FB621HB 622BB 622CB622EB 622GB 622HB622KB 622MB 622QB623BB 623CB 623DB623FB 623HB 623KB623MB 623PB 623QB574156-01-1 522BB 522CB 522EB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500522GB 522HB 522KB 523 BOTTOM SUB SPAR JOINT STRAPS ON TRACK RIB 5 TO TRACK I: 12 YE I: 12 YEOR522MB 522PB 523BB 622 RIB 14.A340-600523CB 523DB 523FB 623523HB 523KB 622BB622CB 622EB 622GB622HB 622KB 622MB622PB 623BB 623CB623DB 623FB 623HB623KB574157-01-1 521FB 521HB 522CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500522EB 522GB 522HB 522 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YEOR522KB 522MB 522PB 523 RIB 3 TO TRACK RIB 12.A340-600523BB 523CB 523DB 621523FB 621FB 621HB 622622CB 622EB 622GB 623622HB 622KB 622MB622PB 623BB 623CB623DB 623FB574158-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE CPCP ZL-521-01-2 A340-500621 LEADING EDGE FAIRING SUPPORT INBOARD OF RAMP I: 12 YEORRIB, MAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.A340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 195APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574159-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 12 YE T: 20 YE CPCP A340-500522AB 522BB 522CB 522 EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR I: 12 YE I: 12 YEOR522EB 522GB 522HB 523 JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGA340-600522KB 522MB 522PB 621 TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.522RB 522UB 523AB 622523BB 523DB 523FB 623523HB 523KB 523MB523PB 523QB 621CB621EB 621FB 622AB622BB 622CB 622EB622GB 622HB 622KB622MB 622PB 622RB622UB 623AB 623BB623DB 623FB 623HB623KB 623MB 623PB623QB574160-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE CPCP ZL-500-02-2 A340-500600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER I: 6 YEORSURFACE FORWARD OF FRONT SPAR FROM ROOTA340-600TO INBOARD PYLON FAIRINGS.574161-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE CPCP ZL-500-02-2 A340-500600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE I: 6 YEORFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 41.A340-600574162-01-1 523MB 523PB 623MB 523 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500623PB 623 INTERMEDIATE RIB BETWEEN SLAT TRACK RIB 15 AND SLAT I: 12 YE I: 12 YEORTRACK 16, AREA OF SLAT TRACK BRAKE FITTING.A340-600574164-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE CPCP ZL-500-01-2 A340-500600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER I: 12 YEORSURFACE FORWARD OF FRONT SPAR FROM INBOARDA340-600PYLON FAIRINGS TO WINGTIP, EXCLUDING AREA HIDDENBY OUTBOARD PYLON FAIRINGS.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 196APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574165-01-1 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500523AB 523BB 523CB 523 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF I: 12 YE I: 12 YEOR523DB 622AB 622BB 622 FRONT SPAR BETWEEN RIBS 9 AND 11 AND BETWEEN RIBS 23A340-600622CB 623AB 623BB 623 AND 26.623CB 623DB574166-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500522AB 522BB 522CB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS I: 12 YE I: 12 YEOR522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCTS) ANDA340-600522KB 522MB 522PB 621 SLAT HOLD DOWN RIBS.522RB 522UB 523AB 622523BB 523DB 523FB 623523HB 523KB 523MB523PB 523QB 621CB621EB 621FB 622AB622BB 622CB 622EB622GB 622HB 622KB622MB 622PB 622RB622UB 623AB 623BB623DB 623FB 623HB623KB 623MB 623PB623QB574169-01-1 521BB 521CB 523HB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A340-500523KB 523MB 523PB 523 TOP I: 12 YE I: 12 YEOR523QB 621BB 621CB 621 SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACKA340-600623HB 623KB 623MB 623 RIBS 1 AND 2 AND TRACK RIBS 13 TO 17.623PB 623QBR 574301-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FCGROUP 42A611 3, VISIBLE PART OF ROLLER CONTACT AREA. OROR65000 FHGROUP 43AI: 9400 FCORORGROUP 42B47000 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 197APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574301-01-2 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FCGROUP 43C611 3, VISIBLE PART OF ROLLER CONTACT AREA. OR26000 FHI: 11200 FCOR22400 FHR 574301-01-3 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FCGROUP 43E611 3, VISIBLE PART OF ROLLER CONTACT AREA. OR65000 FHI: 4500 FCOR22500 FHR 574303-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 12 YE CPCP A340-200611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEORBOLTS, LINKS AND LINK PLATE, LH/RH.A340-300N 574303-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FCGROUP 42A611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574303-02-2 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FCZL-500-01-1 GROUP 43C611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 198APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574303-02-3 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FCZL-500-01-1 GROUP 43E611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574304-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN T: 12 YE T: 20 YE NO CPCP A340-200611 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574304-03-1.R 574304-02-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FCGROUP 42A611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BR 574304-02-2 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FCGROUP 43C611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR26000 FHI: 10500 FCOR21000 FHR 574304-02-3 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FCGROUP 43E611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR65000 FHI: 5500 FCOR20000 FHR 574304-03-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP A340-200611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-300TASK 574304-01-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 199APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574305-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200611 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574306-01-1 N/A TASK DELETEDR 574306-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200611 LOWER FACE, 100 MM FORWARD OF AFT EDGE, LH/RH. I: 3 YEORA340-300R 574307-01-1 521DB 521GB 621DB 511 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 T: 12 YE T: 20 YE CPCP A340-200621GB 611 ACTUATION LINK CONNECTION BOLTS LH/RH. I: 6 YE I: 6 YEORREMOVAL OF THE BOLTSA340-300ONE AT A TIME.SLAT FULLY EXTENDEDR 574308-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL T: 6 YE NO CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574353-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 12 YE NO CPCP A340-500611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEORBOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574354-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN T: 12 YE T: 20 YE NO CPCP A340-500611 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEORINTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574354-03-1.R 574354-03-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 12 YE T: 20 YE NO CPCP A340-500611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-600TASK 574354-01-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 200APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574356-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500611 LOWER FACE, 100 MM FROM LEFT EDGE, LH/RH. I: 3 YEORA340-600R 574357-01-1 521CB 521FB 621CB 521 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 T: 12 YE T: 20 YE NO CPCP A340-500621FB 621 ACTUATION LINK CONNECTION BOLTS, LH/RH. I: 6 YE I: 6 YEORREMOVAL OF THE BOLTSA340-600ONE AT A TIME.SLAT FULLY EXTENDED574358-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600R 574401-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FCGROUP 42A612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43AI: 5200 FCORORGROUP 42B26000 FHORGROUP 43BR 574401-01-2 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FCGROUP 43C612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 6200 FCOR12400 FHR 574401-01-3 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FCGROUP 43E612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574401-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 12 YE T: 20 YE CPCP A340-200612 6 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 201APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574403-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 12 YE CPCP A340-200612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEORBOLTS, LINKS AND LINK PLATE, LH/RH.A340-300R 574403-02-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FCZL-500-01-1 GROUP 42A612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574403-02-2 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FCZL-500-01-1 GROUP 43C612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FH574403-02-3 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FCZL-500-01-1 GROUP 43E612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574404-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO CPCP A340-200612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574404-03-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 202APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574404-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FCGROUP 42A612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BR 574404-02-2 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FCGROUP 43C612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 26000 FHI: 10500 FCOR21000 FHR 574404-02-3 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FCGROUP 43E612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 65000 FHI: 5500 FCOR20000 FHR 574404-03-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE CPCP A340-200612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574404-01-1.R 574405-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200612 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574406-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200612 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 203APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 574407-01-1 522CB 522FB 622CB 522 DETAILED INSPECTION OF SLAT 2, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200622FB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.574408-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 2, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574451-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 12 YE T: 20 YE NO CPCP A340-500612 6 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600R 574453-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 TO 6 T: 12 YE NO CPCP A340-500612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEORBOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574454-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO CPCP A340-500612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574454-03-1.R 574454-03-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO CPCP A340-500612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574454-01-1.R 574455-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2 HOLD DOWN T: 12 YE T: 20 YE NO CPCP A340-500612 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-600R 574456-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500612 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 204APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 574457-01-1 522CB 522EB 622CB 522 DETAILED INSPECTION OF SLAT 2, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500622EB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.574458-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 2, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600R 574501-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE T: 20 YE CPCP A340-200613 8, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300R 574501-02-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FCGROUP 42A613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43AI: 5200 FCOR26000 FHR 574501-02-2 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FCGROUP 42B613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43BI: 3100 FCOR15500 FHR 574501-02-3 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FCGROUP 43C613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 3700 FCOR7400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 205APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574501-02-4 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FCGROUP 43E613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574503-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE CPCP A340-200613 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-300574503-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FCZL-500-01-1 GROUP 42A613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574503-02-2 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FCZL-500-01-1 GROUP 43C613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FH574503-02-3 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FCGROUP 43E613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574504-01-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO CPCP A340-200613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574504-03-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 206APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574504-02-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FCGROUP 42A613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BR 574504-02-2 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FCGROUP 43C613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 26000 FHI: 10500 FCOR21000 FHR 574504-02-3 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FCGROUP 43E613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 65000 FHI: 5500 FCOR20000 FHR 574504-03-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE CPCP A340-200613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574504-01-1.R 574505-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 3 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200612 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574506-01-1 N/A TASK DELETEDR 574506-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200613 LOWER FACE, 100 MM FORWARD OF AFT EDGE, LH/RH. I: 3 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 207APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574507-01-1 N/A TASK DELETEDN 574507-01-2 522JB 522LB 622JB 522 DETAILED INSPECTION OF SLAT 3, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200622LB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.574508-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574551-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE T: 20 YE NO CPCP A340-500613 8 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600R 574553-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE NO CPCP A340-500613 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574554-01-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO CPCP A340-500613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574554-03-1.R 574554-03-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO CPCP A340-500613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574554-01-1.R 574555-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3 HOLD DOWN T: 12 YE T: 20 YE NO CPCP A340-500613 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 208APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574556-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500613 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YEORA340-600N 574557-01-1 522JB 522LB 622JB 522 DETAILED INSPECTION OF SLAT 3, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500622LB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.574558-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600N 574558-02-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, T: 6 YE NOA340-500600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEORA340-600R 574601-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FCGROUP 42A614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43AI: 5200 FCORORGROUP 42B26000 FHORGROUP 43BR 574601-01-2 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FCGROUP 43C614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 6200 FCOR12400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 209APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574601-01-3 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FCGROUP 43E614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574601-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 12 YE T: 20 YE CPCP A340-200614 10, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300R 574603-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 & T: 12 YE NO CPCP A340-200614 10 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-300574603-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FCZL-500-01-1 GROUP 42A614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORORLUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574603-02-2 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FCZL-500-01-1 GROUP 43C614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FH574603-02-3 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FCZL-500-01-1 GROUP 43E614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 210APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574604-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN T: 12 YE T: 20 YE NO CPCP A340-200614 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574604-03-1.R 574604-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FCGROUP 42A614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BR 574604-02-2 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FCGROUP 43C614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR26000 FHI: 10500 FCOR21000 FHR 574604-02-3 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FCGROUP 43E614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR65000 FHI: 5500 FCOR20000 FHR 574604-03-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP A340-200614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-300TASK 574604-01-1.R 574605-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200614 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 211APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574606-01-1 N/A TASK DELETEDR 574606-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200614 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YEORA340-300N 574607-01-1 522NB 522RB 622NB 522 DETAILED INSPECTION OF SLAT 4, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200622RB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.574608-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 4, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574651-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 12 YE T: 20 YE NO CPCP A340-500614 10 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600R 574653-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 TO T: 12 YE NO CPCP A340-500614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574654-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN T: 12 YE T: 20 YE NO CPCP A340-500614 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574654-03-1.R 574654-03-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 12 YE T: 20 YE NO CPCP A340-500614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-600TASK 574654-01-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 212APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574655-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN T: 12 YE T: 20 YE NO CPCP A340-500614 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-600R 574656-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500614 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YEORA340-600N 574657-01-1 522MB 522PB 622MB 522 DETAILED INSPECTION OF SLAT 4, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500622PB 622 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.574658-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 4, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600R 574701-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE T: 20 YE CPCP A340-200615 12, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300574701-02-1 N/A TASK DELETEDR 574701-02-2 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FCGROUP 42A615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 42BI: 5200 FCORORGROUP 43A26000 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 213APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574701-02-3 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FCGROUP 43C615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 6200 FCOR12400 FHR 574701-02-4 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FCGROUP 43E615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574703-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE CPCP A340-200615 12 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-300574703-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FCZL-500-01-1 GROUP 42A615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574703-02-2 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FCZL-500-01-1 GROUP 43C615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 214APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574703-02-3 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FCZL-500-01-1 GROUP 43E615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574704-01-1 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO CPCP A340-200615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574704-03-1.R 574704-02-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FCGROUP 42A615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BR 574704-02-2 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FCGROUP 43C615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 26000 FHI: 10500 FCOR21000 FHR 574704-02-3 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FCGROUP 43E615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 65000 FHI: 5500 FCOR20000 FHR 574704-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE CPCP A340-200615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574704-01-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 215APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574705-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200615 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574706-01-1 N/A TASK DELETED574706-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5 TRAILING EDGE, T: 3 YE CPCP ZL-500-01-1 A340-200615 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YEORA340-300N 574707-01-1 523CB 523FB 623CB 523 DETAILED INSPECTION OF SLAT 5, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200623FB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.R 574708-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 5, EXTERNAL SURFACE T: 6 YE CPCP ZL-500-01-1 A340-200600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574751-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE T: 20 YE NO CPCP A340-500615 12 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600R 574753-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE NO CPCP A340-500615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574754-01-1 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO CPCP A340-500615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574754-03-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 216APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574754-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO CPCP A340-500615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574754-01-1.R 574755-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5 HOLD DOWN T: 12 YE T: 20 YE NO CPCP A340-500615 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-600R 574756-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500615 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YEORA340-600N 574757-01-1 523CB 523EB 623CB 523 DETAILED INSPECTION OF SLAT 5, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500623EB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.R 574758-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 5, EXTERNAL SURFACE T: 6 YE NO CPCP ZL-500-01-2 A340-500600 OF UPPER AN LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600R 574801-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE T: 20 YE CPCP A340-200616 14, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300R 574801-02-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FCGROUP 42A616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43AI: 5200 FCORORGROUP 42B26000 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 217APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574801-02-2 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FCGROUP 43C616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 6200 FCOR12400 FHR 574801-02-3 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FCGROUP 43E616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574803-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE CPCP A340-200616 14 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-300574803-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FCZL-500-01-1 GROUP 42A616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43B574803-02-2 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FCZL-500-01-1 GROUP 43C616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 218APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574803-02-3 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FCZL-500-01-1 GROUP 43E616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORBOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574804-01-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO CPCP A340-200616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574804-03-1.R 574804-02-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FCGROUP 42A616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43AI: 8800 FCOR31900 FHR 574804-02-2 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FCGROUP 42B616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43BI: 6800 FCOR24600 FHR 574804-02-3 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FCGROUP 43C616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 26000 FHI: 8100 FCOR16200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 219APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574804-02-4 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FCGROUP 43E616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 65000 FHI: 5500 FCOR20000 FHR 574804-03-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE CPCP A340-200616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574804-01-1.R 574805-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200616 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574806-01-1 N/A TASK DELETEDR 574806-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200616 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YEORA340-300N 574807-01-1 523GB 523JB 623GB 523 DETAILED INSPECTION OF SLAT 6, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200623JB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.574808-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 6, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574851-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE T: 20 YE NO CPCP A340-500616 14 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 220APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574853-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE NO CPCP A340-500616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-600R 574854-01-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO CPCP A340-500616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574854-03-1.R 574854-03-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO CPCP A340-500616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-600NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574854-01-1.R 574855-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6 HOLD DOWN T: 12 YE T: 20 YE NO CPCP A340-500616 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-600R 574856-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRAILING EDGE T: 3 YE NO CPCP ZL-500-01-2 A340-500616 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YEORA340-600N 574857-01-1 523HB 523KB 623HB 523 DETAILED INSPECTION OF SLAT 6, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500623KB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.574858-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 6, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600R 574901-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 12 YE T: 20 YE CPCP A340-200617 16 ;VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 221APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574901-02-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FCGROUP 42A617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT ORORAREA, LH/RH. 65000 FHGROUP 43AI: 5200 FCORORGROUP 42B26000 FHORGROUP 43BR 574901-02-2 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FCGROUP 43C617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 26000 FHI: 6200 FCOR12400 FHR 574901-02-3 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FCGROUP 43E617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT ORAREA, LH/RH. 65000 FHI: 4500 FCOR22500 FHR 574903-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 12 YE CPCP A340-200617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YEORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.A340-300574903-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FCZL-500-01-1 GROUP 42A617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHGROUP 43AI: 3400 FCORORGROUP 42B17000 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 222APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS574903-02-2 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FCZL-500-01-1 GROUP 43C617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FHI: 4000 FCOR8000 FH574903-02-3 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FCZL-500-01-1 GROUP 43E617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK ORLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FHI: 2000 FCOR10000 FHR 574904-01-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO CPCP A340-200617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, INTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574904-02-1.R 574904-02-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE CPCP A340-200617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YEORSTATIONS, EXTERNAL, LH/RH.A340-300NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574904-01-1.R 574904-02-2 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FCGROUP 42A617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORORSTATIONS, EXTERNAL, LH/RH. 65000 FHGROUP 43AI: 8800 FCORORGROUP 42B31900 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 223APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574904-02-3 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FCGROUP 43C617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 26000 FHI: 10500 FCOR21000 FHR 574904-02-4 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FCGROUP 43E617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB ORSTATIONS, EXTERNAL, LH/RH. 65000 FHI: 5500 FCOR20000 FHR 574905-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7 HOLD DOWN T: 12 YE T: 20 YE CPCP A340-200617 BRACKET, LH/RH. I: 12 YE I: 12 YEORA340-300574906-01-1 N/A TASK DELETEDR 574906-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 A340-200617 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YEORA340-300N 574907-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF SLAT 7, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-200623NB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-300THE TASK IS COVERED BY MSI 27.80.00.574908-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 7, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 574951-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 TO 17, T: 12 YE T: 20 YE NO CPCP A340-500617 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 224APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 574953-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 TO 17 T: 12 YE NO CPCP A340-500617 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEORBOLTS AND LINKS, LH/RH.A340-600R 574954-01-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO CPCP A340-500617 CONNECTIONS AT TRACK RIB STATIONS, INTERNAL, LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-600TASK 574954-02-1.R 574954-02-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO CPCP A340-500617 CONNECTIONS AT TRACK RIB STATIONS, EXTERNAL, LH/RH. I: 12 YE I: 12 YEORNOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASA340-600TASK 574954-01-1.R 574956-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRAILING EDGE, T: 3 YE NO CPCP ZL-500-01-2 A340-500617 LOWER FACE, 100 MM FROM AFT EDGE,H/RH. I: 3 YEORA340-600N 574957-01-1 523MB 523QB 623MB 523 DETAILED INSPECTION OF SLAT 7, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOA340-500623QB 623 LH/RH. I: 6 YE I: 6 YEORSLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.A340-600THE TASK IS COVERED BY MSI 27.80.00.574958-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 7, EXTERNAL T: 6 YE NO CPCP ZL-500-01-2 A340-500600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-2 ORA340-600575001-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42ASPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YEOR13000 FCGROUP 43AI: 12 YEORORGROUP 42B5200 FCORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 225APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575001-01-2 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43CSPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YE13000 FCI: 12 YEOR4500 FC575001-01-3 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43ESPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YE13000 FCI: 12 YEOR5400 FC575002-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200673BB 673DB 673FB 673 EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR SPAR I: 12 YE I: 12 YEOROR FALSE REAR SPAR AND SPOILER 1 HINGE FITTINGS.A340-300575003-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200SPOILERS EXTENDED 674 EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT I: 12 YE I: 12 YEORFITTING (5 PLACES) LUGS AND ATTACHMENT TO BOTTOMA340-300SKIN OVERHANG.575004-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 42ASPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING OR I: 12 YEOR(5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 13000 FCGROUP 43AOVERHANG I: 12 YEORORGROUP 42B5200 FCORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 226APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575004-01-2 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 43CSPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING OR I: 12 YE(5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 13000 FCOVERHANG I: 12 YEOR4500 FC575004-01-3 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 43ESPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING OR I: 12 YE(5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 13000 FCOVERHANG I: 12 YEOR6300 FC575005-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200SPOILERS EXTENDED 674 EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS I: 12 YE I: 12 YEORAND OUTER LINK HINGE RIBS (16 PLACES)A340-300575006-01-1 575AB 575CB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200675CB 675 EDGE INBOARD AND OUTBOARD AILERON JACK BRACKETS (4 I: 12 YE I: 12 YEORPLACES) AT LUG AND ATTACHMENT TO TOP AND BOTTOMA340-300SKIN OVERHANGS (INTERNAL AND EXTERNAL)575008-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200SPOILERS EXTENDED 574 EDGE RIB 10 FLAP CRUISE ROLLERS SUPPORT I: 12 YE I: 12 YEOR673A340-300674575009-01-1 573BB 573CB 573DB 573 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP A340-200573EB 573FB 573GB 673 EDGE RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, TOP I: 12 YEOR673BB 673CB 673DB AND BOTTOM SKIN OVERHANGS AND OUTER FLAP CRUISEA340-300673EB 673FB 673GB ROLLER SUPPORT ATTACHMENT TO TRAILING EDGE RIB 10ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 227APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575010-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42A673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEOR13000 FCGROUP 43AOR60000 FHI: 12 YEOR9100 FCOR34600 FH575010-01-2 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42B673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEOR13000 FCGROUP 43BOR60000 FHI: 12 YEOR8700 FCOR32900 FH575010-01-3 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43C673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE13000 FCOR26000 FHI: 12 YEOR11700 FCOR23400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 228APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575010-01-4 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43E673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE13000 FCOR65000 FHI: 12 YEOR7400 FCOR33600 FH575011-01-1 N/A TASK DELETED575011-01-2 N/A TASK DELETED575011-01-3 N/A TASK DELETED575011-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE NO CPCP ZL-500-02-1 A340-200600 EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR I: 12 YEORBETWEEN RIB 1 AND RIB 14.A340-300575012-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42A600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORORBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 60000 FHGROUP 43AFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 3100 FCREAR SPAR JUST INBOARD OF GEAR RIB 6. OR11800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 229APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575012-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42B600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORORBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 60000 FHGROUP 43BFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 7000 FCPRE 48437REAR SPAR JUST INBOARD OF GEAR RIB 6. OR26500 FH575012-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43C600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 26000 FHFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 9400 FCREAR SPAR JUST INBOARD OF GEAR RIB 6. OR18800 FH575012-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43E600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 65000 FHFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 4600 FCREAR SPAR JUST INBOARD OF GEAR RIB 6. OR20000 FH575012-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 6 YE NO CPCP ZL-500-01-1 A340-200600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 6 YEORBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYA340-300FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR RIB 6.575013-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 42A600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR ORORSPAR JUST INBOARD OF GEAR SUPPORT RIB 6 60000 FHGROUP 43AI: 10500 FCORORGROUP 42B39900 FHORGROUP 43BISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 230APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575013-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43C600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR ORSPAR JUST INBOARD OF GEAR SUPPORT RIB 6 26000 FHI: 13000 FCOR26000 FH575013-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FCGROUP 43E600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR ORSPAR JUST INBOARD OF GEAR SUPPORT RIB 6 65000 FHI: 8900 FCOR38700 FH575013-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO CPCP ZL-500-01-1 A340-200600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR I: 6 YEORSPAR JUST INBOARD OF GEAR SUPPORT RIB 6A340-300575014-01-1 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A670 TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED ORORBY MLG REINFORCING 60000 FHGROUP 43AI: 9200 FCOR34800 FH575014-01-2 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED ORORBY MLG REINFORCING 60000 FHGROUP 43BI: 10700 FCOR40800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 231APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575014-01-3 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED ORBY MLG REINFORCING 26000 FHI: 13000 FCOR26000 FH575014-01-4 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED ORBY MLG REINFORCING 65000 FHI: 13000 FCOR65000 FH575015-01-1 454HL 464HL 532AB 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE NO CPCP ZL-454-02-1 A340-200533AB 534AB 632AB 464 EDGE BOTTOM SKIN LOWER SURFACE AFT REAR SPAR FROM I: 12 YEZL-454-02-2 OR633AB 634AB 500 RIB 12 TO RIB 39.ZL-454-02-3 A340-300532ZL-500-01-1533ZL-531-02-1534600632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 232APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575016-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42A631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YEORUNDER FLAP TRACK 2 FAIRING. 13000 FCGROUP 43AOR60000 FHI: 12 YEOR5600 FCOR21400 FH575016-01-2 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 42B631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YEORUNDER FLAP TRACK 2 FAIRING. 13000 FCGROUP 43BOR60000 FHI: 12 YEOR3200 FCOR12400 FH575016-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43C631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YEUNDER FLAP TRACK 2 FAIRING. 13000 FCOR26000 FHI: 12 YEOR5600 FCOR11200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 233APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575016-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP GROUP 43E631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YEUNDER FLAP TRACK 2 FAIRING. 13000 FCOR65000 FHI: 12 YEOR11800 FCOR51100 FH575016-02-1 N/A TASK DELETED575017-01-1 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42A673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE ORORCUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 60000 FHGROUP 43AJUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 4800 FCOR18200 FH575017-01-2 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 42B673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE ORORCUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 60000 FHGROUP 43BJUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 2700 FCOR10500 FH575017-01-3 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43C673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE ORCUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 26000 FHJUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 5200 FCOR10400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 234APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575017-01-4 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FCGROUP 43E673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE ORCUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 65000 FHJUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 13000 FCOR65000 FH575017-02-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 6 YE NO CPCP A340-200673 EDGE BOTTOM SKIN 50MM AROUND MANHOLE CUTOUT, I: 6 YEORINTERNAL AND EXTERNAL, AFT OR REAR SPAR JUSTA340-300OUTBOARD OF GEAR SUPPORT RIB 6.575018-01-1 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42A192CT 672 EDGE ATTACHMENT OF SHROUD BOX ORORFLAPS EXTENDED 60000 FHGROUP 43AI: 6800 FCORORGROUP 42B26000 FHORGROUP 43B575018-01-2 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43C192CT 672 EDGE ATTACHMENT OF SHROUD BOX ORFLAPS EXTENDED 26000 FHI: 9200 FCOR18400 FH575018-02-1 147AT 148AT 191CT 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 10 YE CPCP A340-200192CT 672 EDGE ATTACHMENT OF SHROUD BOX. I: 10 YEORFLAPS EXTENDEDA340-300575019-01-1 147AT 148AT 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 10 YE CPCP A340-200671 EDGE ATTACHMENT OF OVERWING PANEL. I: 10 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 235APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575022-01-1 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42A675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12300 FCORATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINGROUP 43AOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TOHINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575022-01-2 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42B675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12300 FCORATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINGROUP 43BOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TOHINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575022-01-3 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43C675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 10600 FCATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TOHINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575022-01-6 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12 YE I: 12 YEORATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINA340-300OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TOHINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575023-01-1 N/A TASK DELETED575023-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 236APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575023-01-5 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-200675DB 675 EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT I: 12 YE I: 12 YEORATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINA340-300OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TOHINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575025-01-1 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42A531 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORPOST 45739600 FROM RIB 8 TO RIB 12 60000 FHOR631 I: 5200 FCGROUP 43AORPOST 4573919700 FH575025-01-2 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 42B531 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OROR600 FROM RIB 8 TO RIB 12 60000 FHGROUP 43B631 I: 3700 FCOR14200 FH575025-01-3 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43C600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORFROM RIB 8 TO RIB 12 26000 FHI: 5000 FCOR10000 FH575025-01-9 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FCGROUP 43E600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORFROM RIB 8 TO RIB 12 65000 FHI: 4600 FCOR20000 FH575025-02-1 531AB 631AB 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP ZL-500-01-1 A340-200600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 12 YEORFROM RIB 8 TO RIB 12.A340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 237APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575051-01-1 N/A TASK DELETED575053-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, T: 12 YE T: 20 YE CPCP A340-200FLAPS EXTENDED 148 DRIVE LINK, DRIVE LEVER, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YEPRE 45326ORA340-300PRE 45326575053-01-2 N/A TASK DELETEDR 575054-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR T: 12 YE T: 20 YE CPCP A340-200FLAPS EXTENDED 148 BOX, FORK ASSY, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YEPOST 45326ORA340-300POST 45326575055-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, T: 12 YE T: 20 YE CPCP A340-200148 ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), I: 12 YE I: 12 YEORINCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.A340-300575055-01-2 N/A TASK DELETED575057-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 238APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575059-01-1 AFT FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, T: 12 YE T: 20 YE CPCP A340-200FAIRINGS 532 4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH I: 12 YE I: 12 YEORFLAPS EXTENDED 533 TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINKA340-300534 AND TRAVELLING BEAM AT TRACK NO.4.631632633634575059-01-2 N/A TASK DELETEDR 575061-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, T: 12 YE T: 20 YE CPCP A340-200532 4 AND 5, CARRIAGE ASSEMBLIES. I: 12 YE I: 12 YEOR533A340-300534631632633634575061-01-2 N/A TASK DELETED575063-01-1 N/A TASK DELETED575063-01-2 FLAP TRACK FAIRING 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO. 2, 3, 4 T: 12 YE CPCP A 340-200REMOVED 532 AND 5 LOWER FLANGES, STRAP AND ANGLES. I: 12 YEPOST 55652533OR534A 340-300631POST 55652632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 239APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575065-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO CPCP A340-200532 NO.2, 3, 4 AND 5, INTERNAL STRUCTURE. I: 12 YE I: 12 YEOR533A340-300534631632633634R 575067-01-1 FWD FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2,3,4 T: 12 YE T: 20 YE CPCP A340-200FAIRINGS 532 AND 5, FORWARD ATTACHMENT SPIGOTS,EXTERNAL STRUCTURE. I: 12 YE I: 12 YEOR533A340-300534631632633634575067-01-2 N/A TASK DELETEDR 575067-02-1 FS BOLTS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO CPCP A340-200FWD FLAP TRACK 532 NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS, I: 12 YE I: 12 YEORFAIRINGS 533 INTERNAL STRUCTURE.A340-300534631632633634575067-02-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 240APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575069-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO CPCP A340-200532 NO.2, 3, 4 AND 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YEOR533A340-300534631632633634575069-01-2 N/A TASK DELETEDR 575074-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOX T: 12 YE T: 20 YE CPCP A340-500FLAPS EXTENDED 148 SUPPORT, FORK ASSEMBLY, DRIVE STRUT AND I: 12 YE I: 12 YEORCARRIAGE.A340-600R 575075-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, ATTACHMENT T: 12 YE T: 20 YE CPCP A340-500148 TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING I: 12 YE I: 12 YEORSUPPORT STRUTS WITH ATTACHMENT FITTING.A340-600R 575079-01-1 AFT FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, T: 12 YE T: 20 YE NO CPCP A340-500FAIRINGS 532 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH I: 12 YE I: 12 YEORFLAPS EXTENDED 533 TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORTA340-600534 LINK AND TRAVELING BEAM AT TRACK NO.4.631632633634R 575081-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, T: 12 YE T: 20 YE CPCP A340-500532 CARRIAGE ASSEMBLIES. I: 12 YE I: 12 YEOR533A340-600534631632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 241APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575083-01-1 FLAP TRACK FAIRINGS 531 FLAP TRACK BEAM NO.2, 3, 4 AND 5 LOWER FLANGES, T: 12 YE CPCP A 340-500532 STRAP AND ANGLES. I: 12 YEPOST 55652533OR534A 340-600631POST 55652632633634R 575085-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, T: 12 YE T: 20 YE NO CPCP A340-500532 3, 4 AND 5, INTERNAL STRUCTURE. I: 12 YE I: 12 YEOR533A340-600534631632633634R 575087-01-1 FS BOLT 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 T: 12 YE T: 20 YE NO CPCP A340-500FWD FLAP TRACK 532 AND 5, FORWARD ATTACHMENT SPIGOTS. I: 12 YE I: 12 YEORFAIRINGS 533A340-600534631632633634R 575087-02-1 FS BOLT 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO CPCP A340-500FWD FLAP TRACK 532 NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS. I: 12 YE I: 12 YEORFAIRINGS 533A340-600534631632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 242APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575089-01-1 FLAP TRACK FAIRINGS 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 T: 12 YE T: 20 YE CPCP A340-500532 AND 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YEOR533A340-600534631632633634575101-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-500SPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING. I: 12 YE I: 12 YEORA340-600575102-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE CPCP A340-500673FB 673 EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR I: 12 YE I: 12 YEORSPAR OR FALSE REAR SPAR AND SPOILER 1 HINGEA340-600FITTINGS.575103-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500SPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING I: 12 YE I: 12 YEOR(5 PLACES) LUGS AND ATTACHMENT TO REAR SPAR ANDA340-600TOP AND BOTTOM SKIN OVERHANGS.575105-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500SPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS AND I: 12 YE I: 12 YEOROUTER LINK HINGE RIBS (18 RIBS).A340-600575106-01-1 575AB 575CB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500675CB 675 INBOARD AND OUTBOARD AILERON JACK BRACKETS I: 12 YE I: 12 YEOR(4 PLACES) AT LUG AND ATTACHMENT TO TOP ANDA340-600BOTTOM SKIN OVERHANGS (INTERNAL AND EXTERNAL).575108-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500SPOILERS EXTENDED 574 RIB 10 FLAP CRUISE ROLLERS SUPPORT. I: 12 YE I: 12 YEOR673A340-600674ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 243APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575109-01-1 573BB 573FB 673BB 573 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP A340-500673FB 673 EDGE RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, I: 12 YEORTOP AND BOTTOM SKIN OVERHANGS AND OUTER FLAPA340-600CRUISE ROLLER SUPPORT ATTACHMENT TO TRAILINGEDGE RIB 10.575110-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. I: 12 YE I: 12 YEORA340-600575111-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP ZL-500-02-2 A340-500600 EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR I: 12 YEORBETWEEN RIB 1 AND RIB 14.A340-600575112-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 6 YE CPCP ZL-500-01-2 A340-500600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR I: 6 YEORSPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAA340-600COVERED BY FLAP TRACK 2 FAIRING.575115-01-1 FLAP TRACK 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP ZL-500-01-2 A340-500PYLON FAIRINGS 464 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR I: 12 YEZL-531-02-2 OR500 SPAR FROM RIB 12 TO RIB 41.A340-600532533534600632633634575116-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 12 YE I: 12 YEORUNDER FLAP TRACK 2 FAIRING.A340-600575117-01-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO CPCP A340-500673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL I: 6 YEORAND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OFA340-600GEAR RIB 6.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 244APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575118-01-1 732 742 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP ZL-572-01-2 A340-500FLAPS EXTENDED 672 EDGE ATTACHMENT OF SHROUD BOX. I: 12 YEORA340-600575119-01-1 732 742 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE CPCP ZL-572-01-2 A340-500FLAPS EXTENDED 671 EDGE ATTACHMENT OF OVERWING PANEL. I: 12 YEORA340-600575122-01-1 575AB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE- T: 12 YE T: 20 YE CPCP A340-500675 INNER AILERON HINGES 1-3 AND THE TOP AND BOTTOM SKIN I: 12 YE I: 12 YEOROVERHANGS UPPER AND LOWER SURFACES AT THESEA340-600LOCATIONS.575123-01-1 575CB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE- T: 12 YE T: 20 YE CPCP A340-500675 OUTER AILERON HINGES 1-3 AND THE TOP AND BOTTOM SKIN I: 12 YE I: 12 YEOROVERHANGS UPPER AND LOWER SURFACES AT THESEA340-600LOCATIONS.575126-01-1 575BB 675BB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500675 INNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS I: 12 YE I: 12 YEORAND THE TOP AND BOTTOM SKINS UPPER AND LOWERA340-600SURFACES AT THE ATTACHMENTS TO THE POSTS.575127-01-1 575DB 675DB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A340-500675 OUTER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS I: 12 YE I: 12 YEORAND THE TOP AND BOTTOM SKINS UPPER AND LOWERA340-600SURFACES AT THE ATTACHMENTS TO THE POSTS.575401-01-1 N/A TASK DELETED575401-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL T: 6 YE CPCP ZL-500-01-1 A340-200600 SURFACE OF UPPER AND LOWER SKIN. I: 6 YEZL-500-02-1 ORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 245APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575401-02-1 N/A TASK DELETED575402-01-1 N/A TASK DELETEDR 575403-01-1 581AB 681AB 734 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP A340-200744 681 SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL I: 12 YE I: 12 YEORAND EXTERNAL.A340-300575403-01-2 N/A TASK DELETEDR 575403-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200744 681 INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, I: 12 YE I: 12 YEORSPEED TAPES INTERNAL.A340-300N 575404-01-1 FLAPS EXTENDED 581 GENERAL VISUAL INSPECTION OF INBOARD FLAP TRAILING T: 6 YEA340-200681 EDGE. I: 6 YEORA340-300N 575404-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 6 YEA340-200681 EDGE. I: 6 YEPRE 47798PRE 49008PRE SBA340-57-4076ORA340-300PRE 47798PRE 49008PRE SBA340-57-4076ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 246APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 575404-03-2 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 12 YEA340-200681 EDGE. I: 12 YEPOST 47798ORPOST 49008ORPOST SBA340-57-4076ORA340-300POST 47798ORPOST 49008ORPOST SBA340-57-4076R 575405-01-1 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP A340-200631CB 681 SUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVE I: 12 YE I: 12 YEPRE 49008FLAPS EXTENDED STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDEORARM ATTACHMENT BRACKET.A340-300PRE 49008575405-01-2 N/A TASK DELETEDR 575405-01-3 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP A340-200631CB 681 SUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVE I: 12 YE I: 12 YEPOST 49008FLAPS EXTENDED STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDEORARM ATTACHMENT BRACKET.A340-300POST 49008R 575405-02-1 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200631CB 681 INTERNAL SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YEPRE 49008FLAPS EXTENDEDORSPEED TAPESA340-300PRE 49008ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 247APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575405-02-2 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200631CB 681 INTERNAL SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YEPOST 49008FLAPS EXTENDEDORSPEED TAPESA340-300POST 49008R 575407-01-1 FLAPS EXTENDED 581 DETAILED INSPECTION OF INBOARD FLAP, OUTER T: 12 YE T: 20 YE NO CPCP A340-200RUBBER SEALS 681 END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT I: 12 YE I: 12 YEORATTACHMENT BRACKET.A340-300R 575409-01-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP A340-200SPEED TAPES 681 STRUCTURE. I: 12 YE I: 12 YEORA340-300R 575451-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, T: 6 YE CPCP ZL-500-01-2 A340-500600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN. I: 6 YEZL-500-02-2 ORA340-600575451-01-2 N/A TASK DELETEDR 575453-01-1 581AB 681AB 734 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE CPCP A340-500744 681 FITTING AT TRACK NO.1 AND TRUNION, INTERNAL AND I: 12 YE I: 12 YEOREXTERNAL.A340-600R 575453-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500744 681 INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNION, I: 12 YE I: 12 YEORPLUGS INTERNAL.A340-600SPEED TAPESN 575454-01-1 FLAPS EXTENDED 581 GENERAL VISUAL INSPECTION OF INBOARD FLAP TRAILING T: 6 YEA340-500681 EDGE. I: 6 YEORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 248APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSN 575454-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP T: 12 YEA340-500681 TRAILING EDGE. I: 12 YEORA340-600R 575455-01-1 531SB 531VT 631SB 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE CPCP A340-500631VT 681 FITTING AT TRACK NO.2 AND EXTERNAL DRIVE STRUT I: 12 YE I: 12 YEORFLAPS EXTENDED BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARMA340-600SPEED TAPES ATTACHMENT BRACKET.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575455-02-01.R 575455-02-1 531SB 531VT 631SB 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500631VT 681 INTERNAL SUPPORT FITTING AT TRACK NO. 2. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-600SPEED TAPES575457-01-1 FLAPS EXTENDED 581 DETAILED INSPECTION OF INBOARD FLAP, OUTER T: 12 YE T: 20 YE CPCP A340-500RUBBER SEALS 681 END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT I: 12 YE I: 12 YEORATTACHMENT BRACKET.A340-600R 575459-01-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP A340-500SPEED TAPES 681 STRUCTURE. I: 12 YE I: 12 YEORA340-600575501-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YEZL-500-01-1 A340-200600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN I: 6 YEORA340-300N 575501-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YEA340-200600 EXTERNAL SURFACES OF UPPER AND LOWER SKIN. I: 6 YEORA340-300R 575503-01-1 532AT 532CB 632AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE CPCP A340-200632CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.3, AND I: 12 YE I: 12 YEORFLAPS EXTENDED EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINKA340-300TO CARRIAGE WITH ASSOCIATED ATTACHMENT FITTINGAND GUIDE ARM ATTACHMENT FITTING.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 249APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575503-01-2 N/A TASK DELETEDR 575503-02-1 532AT 532CB 632AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200632CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.3. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-300SPEED TAPES575503-02-2 N/A TASK DELETEDR 575505-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE CPCP A340-200633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.4, AND I: 12 YE I: 12 YEORFLAPS EXTENDED EXTERNAL FWD SUPPORT LINK AND AFT SUPPORT LINKA340-300ATTACH FITTING.575505-01-2 N/A TASK DELETEDR 575505-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE CPCP A340-200633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.4. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-300SPEED TAPES575505-02-2 N/A TASK DELETEDR 575507-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE CPCP A340-200633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.5, AND I: 12 YE I: 12 YEORFLAPS EXTENDED EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TOA340-300CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDEARM ATTACH FITTING.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 250APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575507-01-2 N/A TASK DELETEDR 575507-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.5. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-300SPEED TAPES575507-02-2 N/A TASK DELETED575509-01-1 FLAPS EXTENDED 583 DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 12 YE T: 20 YE CPCP A340-200RUBBER SEALS 683 SURFACE OF INNER END RIB INCLUDING ROLLER AND I: 12 YE I: 12 YEORINTERCONNECTION STRUT ATTACHMENT BRACKET.A340-300575509-01-2 N/A TASK DELETED575509-02-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-200RUBBER SEALS 683 INTERNAL STRUCTURE OF INNER END RIB. I: 12 YE I: 12 YEORSPEED TAPESA340-300575509-02-2 N/A TASK DELETEDR 575551-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YEZL-500-01-2 A340-500600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN RH/LH. I: 6 YEZL-500-02-2 ORA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 251APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPSR 575553-01-1 532SB 532VT 632SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP A340-500632VT 683 SUPPORT FITTING AT TRACK NO. 3, AND EXTERNAL DRIVE I: 12 YE I: 12 YEORFLAPS EXTENDED STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGEA340-600WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.R 575553-02-1 532SB 532VT 632SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500632VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 3. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-600SPEED TAPESR 575555-01-1 533SB 533VT 633SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP A340-500633VT 683 SUPPORT FITTING AT TRACK NO. 4, AND EXTERNAL FWD I: 12 YE I: 12 YEORFLAPS EXTENDED SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.A340-600R 575555-02-1 533SB 533VT 633SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500633VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 4. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-600SPEED TAPESR 575557-01-1 533SB 533VT 633SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP A340-500633VT 683 SUPPORT FITTING AT TRACK NO. 5, AND EXTERNAL DRIVE I: 12 YE I: 12 YEORFLAPS EXTENDED STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITHA340-600ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.R 575557-02-1 533SB 533VT 633SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500633VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 5. I: 12 YE I: 12 YEORFLAPS EXTENDEDA340-600SPEED TAPES575559-01-1 FLAPS EXTENDED 583 DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 12 YE T: 20 YE CPCP A340-500RUBBER SEALS 683 SURFACE OF INNER END RIB INCLUDING ROLLER AND I: 12 YE I: 12 YEORINTERCONNECTION STRUT ATTACHMENT BRACKET.A340-600575559-02-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500RUBBER SEALS 683 INTERNAL STRUCTURE OF INNER END RIB. I: 12 YE I: 12 YEORSPEED TAPESA340-600ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 252APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS575561-01-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP A340-500PLUGS 683 INTERNAL STRUCTURE. I: 12 YE I: 12 YEORSPEED TAPESA340-600576101-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, T: 6 YEA340-200690 UPPER AND LOWER SKINS, EXTERNAL SURFACE. I: 6 YEORA340-300576103-01-1 ONLY OUTBOARD 592 DETAILED INSPECTION OF OUTBOARD AILERON END T: 12 YE T: 20 YE CPCP A340-200AILERON DEFLECTED 692 RIBS, EXTERNAL SURFACE. I: 12 YE I: 12 YEORA340-300576104-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON T: 12 YE T: 20 YE CPCP A340-200592AB 592BB 592CB 692 FITTINGS (7 PLACES). I: 12 YE I: 12 YEOR592DB 675BT 675CBA340-300675DB 692AB 692BB692CB 692DB576106-01-1 JACK FITTING FAIRING 592 DETAILED INSPECTION OF OUTBOARD AILERONS, T: 14600 FCA340-200692 FIRST LINE OF FASTENERS ON OUTER JACK FITTING I: 5100 FCORFLANGE, LH/RH.A340-300NOTE : THIS TASK IS AN ALTERNATIVE TO TASK576106-02-1576106-02-1 JACK FITTING FAIRING 592 SPECIAL DETAILED INSPECTION OF OUTBOARD T: 14600 FCA340-200692 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 14600 FCORFITTING FLANGE, LH/RH.A340-300NOTE : THIS TASK IS AN ALTERNATIVE TO TASK576106-01-1576111-01-1 N/A 500 DETAILED INSPECTION OF INBOARD AILERON, T: 6 YEA340-200600 UPPER AND LOWER SKINS, EXTERNAL SURFACE. I: 6 YEORA340-300576113-01-1 INBOARD AILERON ONLY 591 DETAILED INSPECTION OF INBOARD AILERON END T: 12 YE T: 20 YE CPCP A340-200DEFLECTED 691 RIBS, EXTERNAL SURFACE. I: 12 YE I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 253APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS576114-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON T: 12 YE T: 20 YE CPCP A340-200591AB 591BB 591CB 691 FITTINGS (7 PLACES). I: 12 YE I: 12 YEOR591DB 675AB 675ATA340-300675BB 691AB 691BB691CB 691DB576116-01-1 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD T: 13000 FCGROUP 42A691 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 6200 FCPRE 40597FITTING FLANGE, LH/RHORGROUP 43APRE 40597576116-01-2 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD T: 14600 FCGROUP 42A691 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 14600 FCPOST 40597FITTING FLANGE, LH/RH.ORNOTE : THIS TASK IS AN ALTERNATIVE TO TASKGROUP 43A576116-02-1.POST 40597ORGROUP 42BORGROUP 43BORGROUP 43CORGROUP 43E576116-02-1 JACK FITTING FAIRING 591 DETAILED INSPECTION OF INBOARD AILERONS, T: 14600 FCGROUP 42A691 FIRST LINE OF FASTENERS ON OUTER JACK FITTING I: 5100 FCPOST 40597FLANGE, LH/RH.ORNOTE : THIS TASK IS AN ALTERNATIVE TO TASKGROUP 43A576116-01-2.POST 40597ORGROUP 42BORGROUP 43BORGROUP 43CORGROUP 43EISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 254APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS576151-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, UPPER AND T: 6 YEA340-500592 LOWER SKINS, EXTERNAL SURFACE. I: 6 YEOR690A340-600576153-01-1 ONLY OUTBOARD 592 DETAILED INSPECTION OF OUTBOARD AILERON END RIBS, T: 12 YE T: 20 YE CPCP A340-500AILERON DEFLECTED 692 EXTERNAL SURFACE. I: 12 YE I: 12 YEORA340-600576154-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS T: 12 YE T: 20 YE CPCP A340-500592AB 592BB 592CB 692 (7 PLACES). I: 12 YE I: 12 YEOR592DB 675BT 675CBA340-600675DB 692AB 692BB692CB 692DB576161-01-1 N/A 590 DETAILED INSPECTION OF INBOARD AILERON, UPPER AND T: 6 YEA340-500690 LOWER SKINS, EXTERNAL SURFACE. I: 6 YEORA340-600576163-01-1 ONLY INBOARD AILERON 591 DETAILED INSPECTION OF INBOARD AILERON END RIBS, T: 12 YE T: 20 YEA340-500DEFLECTED 691 EXTERNAL SURFACE. I: 12 YE I: 12 YEORA340-600576164-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON FITTINGS T: 12 YE T: 20 YE NO CPCP A340-500591AB 591BB 591CB 691 (7 PLACES). I: 12 YE I: 12 YEOR591DB 675AB 675ATA340-600675BB 691AB 691BB691CB 691DBR 577001-01-1 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO.1, T: 6 YEZL-500-01-1 A340-200SPOILERS DEPLOYED 682 UPPER AND LOWER SKIN, EXTERNAL SURFACE, LH/RH. I: 6 YEZL-500-02-1 ORA340-300R 577003-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO.1, HINGE T: 12 YE T: 20 YE CPCP A340-200SPOILERS DEPLOYED 682 AND ACTUATOR ATTACHMENT FITTINGS. I: 12 YE I: 12 YEORA340-300ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 255APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS577003-01-2 N/A TASK DELETED577003-02-1 N/A TASK DELETEDR 577051-01-1 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO. 1 AND 2, T: 6 YEZL-500-02-2 A340-500SPOILERS DEPLOYED 584 UPPER AND LOWER SKIN, EXTERNAL SURFACE. I: 6 YEOR682A340-600684R 577053-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO.1 AND NO.2, HINGE T: 12 YE T: 20 YE CPCP A340-500SPOILERS DEPLOYED 584 AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES). I: 12 YE I: 12 YEOR682A340-600684* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 256APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS711151-01-1 415AL 416AR 425AL 411 DETAILED INSPECTION OF INLET COWL ATTACHMENT AND T: 6 YE NO CPCP A340-500426AR 435AL 436AR 421 SURROUNDING STRUCTURE (15 CM AROUND THE A1 FLANGE). I: 6 YEOR445AL 446AR 431A340-600441711311-02-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL HINGE FITTINGS T: 6 YE NO CPCP ZL-415-01-1 A340-200426AR 435AL 436AR 416 AND SURROUNDING STRUCTURE (15 CM AROUND HINGES) I: 6 YEOR445AL 446AR 425A340-300426435436445446711312-01-2 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL LATCHES AND T: 6 YE NO CPCP A340-200426AR 435AL 436AR 416 SURROUNDING STRUCTURE 15 CM AROUND LATCHES I: 6 YEOR445AL 446AR 425A340-300426435436445446711351-01-1 N/A TASK DELETED711352-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL LATCH T: 6 YE NO CPCP A340-500426AR 435AL 436AR 416 FITTINGS AND SURROUNDING STRUCTURE I: 6 YEOR445AL 446AR 425 (15 CM AROUND FITTINGS).A340-600426435436445446712101-01-1 N/A TASK DELETEDISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS712101-01-2 N/A TASK DELETED712101-02-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT T: 12 YE NO CPCP A340-200FORWARD ENGINE MOUNT 423 INSTALLATION . I: 12 YEORDISASSEMBLED 433A340-300443712151-01-1 415AL 416AR 417AL 413 DETAILED INSPECTION OF TRENT 500-ENGINE FORWARD MOUNT T: 12 YE NO CPCP A340-500418AR 425AL 426AR 423 INSTALLATION. I: 12 YEOR427AL 428AR 435AL 433A340-600436AR 437AL 438AR 443445AL 446AR 447AL448ARENGINEENGINE MOUNTDISASSEMBLED712152-01-1 N/A TASK DELETED712153-01-1 N/A TASK DELETED712201-01-1 N/A TASK DELETED712201-01-2 N/A TASK DELETEDISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS712201-02-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION. T: 12 YE NO CPCP A340-200DISASSEMBLED 423 I: 12 YEORENGINE 433A340-300443712251-01-1 415AL 416AR 417AL 413 DETAILED INSPECTION OF TRENT 500-ENGINE REAR MOUNT T: 12 YE NO CPCP A340-500418AR 425AL 426AR 423 INSTALLATION. I: 12 YEOR427AL 428AR 435AL 433A340-600436AR 437AL 438AR 443445AL 446AR 447AL448ARENGINEREAR ENGINE MOUNT712252-01-1 N/A TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 3APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS722301-02-1 415AL 416AR 417AL 412 GENERAL VISUAL INSPECTION OF FAN CASE V-GROOVE INNER T: 6 YE NO CPCP ZL-417-01-1 A340-200418AR 425AL 426AR 422 RADIUS I: 6 YEOR427AL 428AR 435AL 432A340-300436AR 437AL 438AR 442445AL 446AR 447AL448AR723151-01-1 415AL 416AR 417AL 412 DETAILED INSPECTION OF TRENT 500- LP COMPRESSOR REAR T: 6 YE NO CPCP A340-500418AR 425AL 426AR 422 FANCASE V GROOVE. I: 6 YEOR427AL 428AR 435AL 432 NOTE : TASK TO BE PERFORMED AT THE SAME TIME AS TASKA340-600436AR 437AL 438AR 442 783255-01-1445AL 446AR 447AL448AR* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: D-72PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS783205-02-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER J-RING RADIUS T: 6 YE NO CPCP A340-200418AR 425AL 426AR 418 I: 6 YEOR427AL 428AR 435AL 427A340-300436AR 437AL 438AR 428445AL 446AR 447AL 437448AR 438447448783207-01-1 415AL 416AR 425AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 6 YE NO CPCP ZL-417-01-1 A340-200426AR 435AL 436AR 418 12 O ́CLOCK BEAM AND FORWARD FRAME JUNCTION I: 6 YEOR445AL 446AR 427A340-300THRUST REVERSER 428DEPLOYED 437438447448783208-01-1 415AL 416AR 425AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 6 YE NO CPCP ZL-417-01-1 A340-200426AR 435AL 436AR 418 6 O ́CLOCK BEAM AND FORWARD FRAME JUNCTION I: 6 YEOR445AL 446AR 427A340-300THRUST REVERSER 428DEPLOYED 437438447448783209-01-1 415AL 416AR 425AL 417 DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME T: 6 YE NO CPCP A340-200426AR 435AL 436AR 418 LOWER AND UPPER FITTINGS I: 6 YEOR445AL 446AR 427A340-300428437438447448ISSUE: JUL 01/10 EXHAUST SECTION: D-78PAGE 1APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS783211-02-1 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER COWL T: 6 YE NO CPCP A340-200418AR 425AL 426AR 418 HINGE FITTINGS AND SURROUNDING STRUCTURE (15 CM I: 6 YEOR427AL 428AR 435AL 427 AROUND FITTINGS)A340-300436AR 437AL 438AR 428445AL 446AR 447AL 437448AR 438HINGE ACCESS PANEL 447448783212-01-2 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER COWL LATCH T: 6 YE NO CPCP A340-200418AR 425AL 426AR 418 ASSEMBLY AND SURROUNDING STRUCTURE (15 CM AROUND I: 6 YEOR427AL 428AR 435AL 427 FITTINGS)A340-300436AR 437AL 438AR 428445AL 446AR 447AL 437448AR 438447448783251-01-1 417EL 418ER 427EL 417 DETAILED INSPECTION OF THRUST REVERSER HINGE LUGS AND T: 6 YE NO CPCP A340-500428ER 437EL 438ER 418 SURROUNDING STRUCTURE (15 CM AROUND HINGE LUGS). I: 6 YEOR447EL 448ER 427A340-600428437438447448783251-01-2 N/A TASK DELETED783252-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER 6 O ́CLOCK BEAM T: 6 YE NO CPCP A340-500417FL 418AR 425AL 418 LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING I: 6 YEOR426AR 427AL 427FL 427 STRUCTURE (15 CM AROUND LATCH FITTINGS).A340-600428AR 435AL 436AR 428437AL 437FL 438AR 437445AL 446AR 447AL 438447FL 448AR 447448ISSUE: JUL 01/10 EXHAUST SECTION: D-78PAGE 2APPLICABILITYA340MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCPALI100%THRESHOLDINTERVALTPS783253-01-1 414AL 414AR 415AL 414 DETAILED INSPECTION OF THRUST REVERSER AFT CORE COWL T: 6 YE NO CPCP A340-500416AR 417AL 417FL 424 LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING I: 6 YEOR418AR 424AL 424AR 434 STRUCTURE (15 CM AROUND LATCH FITTING).A340-600425AL 426AR 427AL 444427FL 428AR 434AL434AR 435AL 436AR437AL 437FL 438AR444AL 444AR 445AL446AR 447AL 447FL448AR783254-01-1 415AL 416AR 417CL 417 DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME T: 6 YE NO CPCP A340-500417DL 417EL 418CR 418 AND TRANSCOWL ACTUATOR FITTINGS AND ITS ATTACHMENTS I: 6 YEOR418DR 418ER 425AL 427 (6 PLACES ON EACH HALF).A340-600426AR 427CL 427DL 428427EL 428CR 428DR 437428ER 435AL 436AR 438437CL 437DL 437EL 447438CR 438DR 438ER 448445AL 446AR 447CL447DL 447EL 448CR448DR 448ER783254-01-2 N/A TASK DELETED783255-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER J RING (V T: 6 YE NO CPCP A340-500417FL 418AR 425AL 418 BLADE). I: 6 YEOR426AR 427AL 427FL 427 NOTE : TASK TO BE PERFORMED AT THE SAME TIME AS TASKA340-600428AR 435AL 436AR 428 723151-01-1437AL 437FL 438AR 437445AL 446AR 447AL 438447FL 448AR 447448* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: D-78PAGE 3

# A340 MRB REPORT

Issue : July 2010 Page : E-INTRO-1 SECTION E

ZONAL INSPECTION

1. GENERAL

This section provides the General Visual Inspection (GVI) requirements for each aircraft zone to

inspect system and powerplant installations and structure for security and general condition.

Inspections are to be accomplished at or before the stated intervals.

The inspections are specified by quoting the relevant zone number, zone description, access

requirements and intervals.

The extent of the inspection is defined by the preparation and access requirements

The zone is to be inspected as visible with the relevant access open.

There are zones which will require more than one inspection at different intervals, because the

depth at which the zone is to be examined may necessitate differing levels of accessibility.

The tasks inspect :

- Structure by looking for signs of accidental damage, corrosion, cracks and for

general condition of fasteners.

- System installations for proper attachment ,security and general condition

(components, wiring, ducting, tubing, pulleys, bearings, electrical bonding, leaks,

chafing marks etc...).

- The general condition of any fairings, panels, or other items which are

removed/opened to gain access to a particular zone.

- Condition of L/HIRF (Lightning & High Intensity Radiated Field) protection

- For accumulation of any kind of contamination (including potential combustible

material) for EZAP (Enhanced Zonal Analysis Procedure) concerns.

The items in the zone are to be visually inspected from within touching distance where physically

possible unless otherwise specified. A mirror may be necessary to enhance visual access to all

exposed surfaces in the inspection area. The inspection is made under normally available lighting

conditions such as daylight, hangar lighting, fl ashlight or drop-light and may require removal or

opening of access panels or doors. Access to zones should be easily accomplished and should

not require the use of special tools. Stands, ladder s or platforms may be required to gain proximity

to the area being checked.

It is expected that the area to be inspected is clean enough to minimise the possibility that

accumulated dirt or grease might hide unsatisfactory conditions. Any cleaning that is considered

necessary should be performed before the Zonal inspection.

Any evolution of Zonal Inspection tasks involving an escalation to the inspection task interval

should consider that credit has been taken for many of these tasks providing the most appropriate

opportunity to detect degradation of wiring installations, electrical bonding and structural

corrosion. As a result, operators should consider the need to identify dedicated tasks if findings

suggest that interval escalation might lead to an unacceptable level of deterioration of these

particular features prior to the repeat inspection. This action would allow any ZIP task interval

escalation to proceed while at the same time ensuring that operators do not overlook the potential

impact on EWIS, L/HIRF and structural corrosion issues.

# A340 MRB REPORT

Issue : July 2010 Page : E-INTRO-2 In view of the fact that all zonal tasks contribute to the identification of degradation that, if

ignored, could ultimately lead to a reduction in certification margins, zonal tasks must not

be deleted from an operator’s maintenance program.

With respect to General Rule 17 in Section B, operators shall consider that all Zonal tasks

identified with “(EWIS)” after the task description in Section E are required to support compliance with

Electrical Wiring Interconnection System (EWIS) requirements.

2. COMPATIBILITY WITH SYSTEMS AND STRUCTURES SECTIONS

The inspection tasks in this Zonal section do not provide a complete summary of all structure and

systems items to be inspected in the affected zone. It is therefore considered that the person

performing the inspection has an adequate knowledge of the aircraft construction and of its

system installation.

GVI tasks arising from EZAP Analysis considered not fully covered by the Zonal section and any

non-GVI task arising from the EZAP analysis are included within ATA 20 of the Systems and

Powerplant, Section C of the MRBRand are identified by “(EWIS)” after the task description. These

dedicated tasks remain under the responsibility of the Zonal MWG. All ATA 20 tasks under

responsibility of the Zonal MWG are uniquely identified in the Systems and Powerplant Section

with (EWIS) after the task description to prevent the inadvertent deletion or escalation of

dedicated EZAP derived tasks without proper consideration of associated risk basis for task and

interval.

A list of GVI MSI tasks and SSIs from the Systems and Powerplant and Structures sections has

been provided for reference. These inspections are considered as being adequately covered by

this ZIP. Therefore, a dedicated inspection is not required for these SSIs and MSIs if the

equivalent ZIP task is performed at least as frequently as the intervals stated for those inspections

in the Systems and Powerplant and Structures Programs.

As a result of the CPCP requirement to control corrosion to Level 1 or better (Refer to Section D),

operators shall report corrosion findings to the m anufacturer in accordance with the Structures

Reporting System (Refer to Appendix 8).

3. INSPECTIONS MORE FREQUENT THAN 'A' CHECK

The routine content of inspections with frequencies below 'A'-check shall be developed by the

operator. Consequently, even when the Zonal working group has used its experience or

engineering judgement to select an interval below 'A' check, this has not been included in the

Zonal section. However, since the justification for these inspections was based on the likelihood of

random accidental damage, they have been stated below for completeness.

It is recommended that these inspections are consid ered by all operators, for inclusion in their

routine maintenance programs. Recommended intervals are provided where no similar

inspections already exist on comparable fleets.

It is recognised that these inspections are of a lesser intensity than a General Visual Inspection,

since they are to be performed 'from the ground, as far as visible'.

RECOMMENDED

ZONE DESCRIPTION CALENDAR

INTERVAL

100 Lower half of fuselage 36 hours

200 Upper half of fuselage 36 hours

300 Empennage and fuselage tail 36 hours

400 Power plants, nacelles and pylons 36 hours

500/600 Wings, L/H and R/H 36 hours

700 Landing gear & landing gear doors 36 hours

# A340 MRB REPORT

Issue : July 2010 Page : E-INTRO-3 800 Doors 36 hours

123 Nose gear well 7 days

149 Center line gear well 7 days

711 Nose landing gear 7 days

731/741 LH & RH main landing gear 7 days

4. INSPECTION INTERVALS

It is recommended that these inspection intervals are considered by all operators:

Check Interval

A - Check & multiples - 800 FH & multiples

C - Check - 18 month

2C - Check - 36 month

4C - Check - 6 Yrs

8C - Check - 12 Yrs

. 5. NOTES FOR SECTION E

NOTE 1 : Insulation to be displaced as required to complete the required inspection.

NOTE 2 : - reserved -

NOTE 3 : Interval to be adjusted by individual operators in consideration of their own in-service

experience and operational environment.A340 MRB REPORTIssue :July 2010Page : E-INTRO-46. EXPLANATION OF ZONAL SECTION FORMATDetailed information is given below concerning the format of the inspection requirements provided on subsequent pages.TASKREFERENCEACCESSZONEDESCRIPTIONINTERVALMSI / SSIREFERENCEAPPLICABILITY123 45 671- This column indicates the zonal task number, e.g. ZL 151-01-1. It is composed of 9 digits as follows:ZL XXX – XX – XXThe Zone number is represented by the three first digits, ZL 151-01-01. The first digit, ZL151-01-01, is in accordance with the A340 ATA 100breakdown, showing the major section where the zone is located e.g 100 Lower Half of Fuselage. The second digit, ZL151-01-01, is also in accordancewith the A340 ATA 100 breakdown, showing the sub section where the zone is located e.g 150 Aft Cargo Compartment. The third digit, ZL 15101-1,shows the sub section where the zone is located e.g (RH- or LH - side of the zone).The Sequential Number is composed of two digits. It follows the Zone number and is separated by a dash e.g. ZL 151-01-01. It identifies differentcontent inspections at different intervals .The Applicability Index is composed of one digit. It follows the Sequential Number and is separated by a dash, ZL 151-01-01. It identifies differentapplicability e.g aircraft model/mod status etc ...This digit is also used to differentiate between access differences e.g. different access panel numbersand differences in reference information.Applicability index: Identifies successive variants of the taskSequence number: Indicates separate tasks within in the same zoneZone number: Indicates the zone numberZL: Abbreviation for ZonalA340 MRB REPORTIssue :July 2010Page : E-INTRO-52- This column indicates the access and preparation requirements to adequately perform the inspection.(i) It lists all access panels, doors and fairings or indicates boundaries between the access panels have to be opened or removed(ii)It defines the configuration of the aircraft, if necessarye.g. "Slats and flaps extended"(iii) The removal or displacement of insulation is indicated by either 'Insulation' or 'NOTE 1' respectively.(iv) To take account of customisation and the Flexible Cabin Concept :- Galleys, toilets, stairhouse, ACT and crew rest rooms are quoted in conjunction with the note "If installed"-Floor panels are not given individual panel numbers, the term "Floor panels from FR XX TO FRXY " is used for simplicity.3- This column indicates the Zone(s).4- This column provides the description of the Zone, which is shown underlined. In certain cases, additional information is provided in brackets to precisethe Inspection areae.g. ELEVATOR(AREA BETWEEN RIBS 8 AND 9)5- This column provides the inspection interval.For the ZIP the threshold is equal to the interval. The interval starts at the time of the last inspection performed.6- A task reference information lists all MSI and SSI General Visual Inspection tasks which are contained in and covered by.Note : The last 2 digits, after the dash(-) of a MSI, indicate the Engine or APU model.Example : MSI 49.13.00/01-35, MSI 49.17.00/02-60, MSI 78.32.00/02-C5, MSI 78.31.00/01-R5,35 stands for APU331-35060 stands for APU331-600C5 stands for CFM56-5 engineR5 stands for RRT500 engine7- This column indicates the A/C model/Mod status/engine type to which this requirement is applicableA340 MRB REPORTThis page intentionally left blankAPPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-100-01-1 N/A 100 LOWER HALF OF FUSELAGE I: C MSI NONE A340-200ORSSI 531116-01-1 A340-300SSI 532101-01-2SSI 533101-01-1SSI 533193-01-2SSI 534126-02-1SSI 534130-01-1ZL-100-01-2 N/A 100 LOWER HALF OF FUSELAGE I: C MSI NONE A340-500ORSSI 531816-01-1 A340-600SSI 532201-01-1SSI 533801-01-1SSI 534226-01-1R ZL-110-01-1 110AL 110 RADOME (EWIS) I: 2 C MSI NONE ALLSSI NONER ZL-121-01-1 132AZ 821 121 AVIONICS COMPARTMENT (EWIS) I: C MSI NONE A340-200122ORSSI NONE A340-300R ZL-121-01-2 121AL 121BL 121CL 121 AVIONICS COMPARTMENT (EWIS) I: C MSI NONE A340-500121DL 121EL 132AZ 122OR821 SSI NONE A340-600R ZL-121-02-1 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 21.26.00/05 A340-200121DF 121EF 121FF 122 MSI 21.27.00/02 OR121GF 121HF 121KFA340-300122CF 122DF 122FF SSI NONE122GF 122HF 122JF122LF 122MF 122NF122PF 131AW 131BW132AZ 132CW 821NOTE 1R ZL-121-02-2 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 21.26.00/05 A340-500* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-121-02-2 * * * * * C O N T I N U E * * * * *121DF 121EF 121FF 122 MSI 21.27.00/02 PRE 47483121GF 121HF 121JFOR121KF 121LF 122AF SSI NONE A340-600122AZ 122BF 122CFPRE 47483122DF 122EF 122FF122GF 122HF 122JF131AW 131BW 132AZ132CW 821NOTE 1R ZL-121-02-3 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 21.26.00/05 A340-500121DF 121EF 121GF 122 MSI 21.27.00/02 POST 47483121HF 121JF 121KFOR121LF 122AF 122AZ SSI NONE A340-600122BF 122CF 122DFPOST 47483122EF 122FF 122GF122HF 122JF 131AW131BW 132AZ 132CW821NOTE 1R ZL-123-01-1 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI NONE A340-200ORSSI NONE A340-300R ZL-123-01-2 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI NONE A340-500ORSSI NONE A340-600R ZL-131-01-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: A MSI 25.51.00/04 A340-200132 MSI 25.51.00/05 ORMSI 25.51.00/06 A340-300MSI 25.51.00/07MSI 25.51.00/09MSI 25.51.00/10MSI 25.51.00/11MSI 25.51.00/12MSI 25.51.00/13MSI 25.51.00/17* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-131-01-1 * * * * * C O N T I N U E * * * * *MSI 25.51.00/18MSI 25.51.01/05MSI 25.51.01/06MSI 25.51.01/07MSI 25.51.01/09MSI 25.51.01/11MSI 25.51.01/12MSI 25.51.01/13MSI 25.51.01/14MSI 25.51.01/15SSI NONER ZL-131-01-2 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: A MSI 25.51.00/04 A340-500132 MSI 25.51.00/05 ORMSI 25.51.00/06 A340-600MSI 25.51.00/07MSI 25.51.00/09MSI 25.51.00/10MSI 25.51.00/11MSI 25.51.00/12MSI 25.51.00/13MSI 25.51.00/16MSI 25.51.00/17SSI NONER ZL-131-02-1 131BC 131FC 131KC 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-200131KW 131MC 131PC 132OR131QW 131RC 131TC SSI NONE A340-300131VC 132QW 132SW132UW 821R ZL-131-02-2 131AA 131CX 131DA 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-500131DM 131NA 131PM 132131QA 131SA 131TM SSI NONE131UA 131WA 131YA132AZ 132CX 132EW132PM 132RM 132VM132ZM 821ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-131-02-3 131AA 131CX 131DA 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-600131DM 131GA 131HM 132131JA 131LA 131NA SSI NONE131PM 131QA 131SA131TM 131UA 131WA132AZ 132CX 132EW132HM 132KM 132MM132PM 132RM 132TM132VM 821R ZL-131-03-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-200NOTE 1 132ORSIDEWALL AND CEILING SSI 532103-01-1 A340-300PANELS FROM FR20 TOFR 39.2R ZL-131-03-2 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-500NOTE 1 132ORSIDEWALL AND CEILING SSI 532203-01-1 A340-600PANELS FROM FR 20 TOBETWEEN FR 39/FR39.1R ZL-133-01-1 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A340-200FLOOR PANELS FROM FR 134 MSI 38.32.00/01 OR20 TO FR 39A340-300NOTE 1 SSI NONER ZL-133-01-2 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 38.32.00/01 A340-500FLOOR PANELS FROM FR 134OR20 TO FR 39 SSI NONE A340-600NOTE 1R ZL-137-01-1 131BX 131CG 131CX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 21.50.00/07 A340-200131DG 131DX 132CG 138OR132CX 132DG 132DX SSI NONE A340-300821R ZL-137-01-2 131BX 131CX 131DX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 21.50.00/07 A340-500* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-137-01-2 * * * * * C O N T I N U E * * * * *131JK 131LK 131MK 138 SSI NONE132CX 132DX 132JK132LK 132MK 821R ZL-137-01-3 131BX 131CX 131DX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 21.50.00/07 A340-600131MH 131TH 131VH 138132CX 132DX 132MH SSI NONE132TH 132VH 132WH821R ZL-141-01-1 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI NONE A340-200744 142ORSSI 571154-01-1 A340-300R ZL-141-01-2 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI NONE A340-500744 142ORSSI 571854-01-1 A340-600R ZL-143-01-1 734 744 143 AREA BETWEEN KEEL BEAMS (EWIS) I: 8 C MSI NONE ALLSSI NONER ZL-145-01-1 834 844 145 ZONE UNDER CABIN FLOOR (EWIS) I: 8 C MSI NONE ALLFLOOR PANELS FROM FR 14640 TO FR 53.2 SSI NONER ZL-147-01-1 734 744 147 MLG WELL AND HYDRAULIC COMPARTMENT (EWIS) I: A MSI 25.76.00/01 A340-200148 MSI 29.10.00/17 ORA340-300SSI NONER ZL-147-01-2 734 744 147 MLG WELL AND HYDRAULIC COMPARTMENT (EWIS) I: A MSI 29.10.00/17 A340-500148ORSSI NONE A340-600ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-149-01-1 753 754 149 CENTER LINE GEAR WELL (EWIS) I: C MSI NONE A340-200ORSSI NONE A340-300R ZL-149-01-2 753 754 149 CENTER LINE GEAR WELL (EWIS) I: C MSI NONE A340-500ORSSI NONE A340-600R ZL-149-02-1 149AB 149CB 753 149 CENTER LINE GEAR WELL (EWIS) I: 8 C MSI NONE ALL754SSI NONER ZL-151-01-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: A MSI 25.51.00/04 ALL152 MSI 25.51.00/05(IF LD-MCR OR LDF AND/OR DCR AND/OR ACT(S) MSI 25.51.00/06INSTALLED , AS FAR AS VISIBLE) MSI 25.51.00/07MSI 25.51.00/09MSI 25.51.00/11MSI 25.51.00/12MSI 25.51.00/13MSI 25.51.00/16MSI 25.51.00/17MSI 25.51.01/05MSI 25.51.01/06MSI 25.51.01/07MSI 25.51.01/09MSI 25.51.01/11MSI 25.51.01/12MSI 25.51.01/13MSI 25.51.01/14MSI 25.51.01/15SSI NONER ZL-151-02-1 151BC 151BW 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-200151HC 151JW 151KC 152WITHOUT ACT(S)151PC 151TW 152BW SSI NONE OR152DW 152EW 152GWA340-300152JW 152LW 822WITHOUT ACT(S)LD-MCR (IFINSTALLED)ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 6APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-151-02-2 151BW 151BY 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-200151HC 151JW 151KC 152WITH ACT(S)151PC 151TW 152AX SSI NONE OR152BW 152BX 152DWA340-300152JW 152LW 822WITH ACT(S)ACT(S)LD-MCR (IFINSTALLED)R ZL-151-02-3 151BQ 151HM 151NA 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-500151RA 151RM 151UA 152151WA 151YA 151YM SSI NONE152BQ 152CQ 152NA152PW 152RA 152UA152UW 152VM 152WA152XM 152YA 822LD-MCR (IFINSTALLED)R ZL-151-02-4 151AA 151BW 151CA 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-600151EA 151GA 151HM 152151JA 151LA 151NA SSI NONE151RA 151RM 152AA152BM 152BW 152CA152CW 152EA 152FM152GA 152HM 152JA152KM 152LA 152MM152NA 152PW 152RA152UW 822LD-MCR OR LDFFURNISHING AND/ORDCR (IF INSTALLED)R ZL-151-03-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-200ACT(S) AND/OR LD-MCR 152OR(IF INSTALLED) SSI NONE A340-300LDL FURNISHINGNOTE 1SIDEWALL AND CEILINGPANELS FROM FR 53.2TO FR 66ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 7APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-151-03-2 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-500LD-MCR (IF 152INSTALLED) SSI NONENOTE 1SIDEWALL AND CEILINGPANELS FROM FR 53.7TO FR 66R ZL-151-03-3 822 000 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-600LD-MCR OR LDF 151FURNISHING AND/OR 152 SSI NONEDCR (IF INSTALLED)NOTE 1SIDEWALL AND CEILINGPANELS FROM FR 53.2TO FR 66R ZL-153-01-1 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A340-200FLOOR PANELS FROM FR 154 MSI 38.32.00/01 OR53.2 TO FR 66A340-300LD-MCR AND/OR ACT(S) SSI NONE(IF INSTALLED)NOTE 1R ZL-153-01-2 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A340-500FLOOR PANELS FROM FR 154 MSI 38.32.00/0153.7 TO FR 66LD-MCR (IF SSI NONEINSTALLED)NOTE 1R ZL-153-01-3 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 38.32.00/01 A340-600FLOOR PANELS FROM FR 15453.2 TO FR 66 SSI NONELD-MCR OR LDFFURNISHING AND/ORDCR (IF INSTALLED)NOTE 1R ZL-155-01-1 153AZ 155AZ 197CB 155 REAR CENTER TANK (EWIS) I: 8 C MSI NONE A340-500* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 8APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-155-01-1 * * * * * C O N T I N U E * * * * *FUEL PUMPS AND PIPES SSI 533853-01-2LINERS TO BE REMOVED SSI 533857-01-2R ZL-161-01-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: A MSI 25.54.00/03 ALL162(IF BCRC OR WASTE CHUTE CONTAINER INSTALLED, AS FAR SSI NONEAS VISIBLE)R ZL-161-02-1 161AC 161BC 161CW 161 BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE AICRAFT WITHOUT161EC 162LW 162RW 162BCRC162SW 162TW 162WW SSI NONE822R ZL-161-02-2 161FQ 161MY 161NQ 161 BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A340-500161NY 161QY 161SY 162IF BCRC162FY 162HY 162JY SSI NONE INSTALLED162KY 162LY 833OR843A340-600IF BCRCINSTALLEDR ZL-161-03-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-200NOTE 1 162ORSIDEWALL AND CEILING SSI NONE A340-300PANELS FROM FR 65 TOFR 73R ZL-161-03-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A340-500BCRC FURNISHINGS OR 162ORWASTE CHUTE (IF SSI NONE A340-600INSTALLED)NOTE 1SIDEWALL AND CEILINGPANELS FROM FR 65 TOFR 73R ZL-163-01-1 164AR 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A340-200* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 9APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-163-01-1 * * * * * C O N T I N U E * * * * *FLOOR PANELS FROM FR 164 SSI NONE OR65 TO FR 73A340-300NOTE 1R ZL-163-01-2 164AR 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A340-500BCRC FURNISHINGS OR 164ORWASTE CHUTE (IF SSI NONE A340-600INSTALLED)FLOOR PANELS FROM FR65 TO FR 73NOTE 1R ZL-171-01-1 162ZW 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI NONE A340-200172ORSSI NONE A340-300R ZL-171-01-2 161AZ 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI NONE A340-500172IF NOT BCRCSSI NONE INSTALLEDORA340-600IF NOT BCRCINSTALLEDR ZL-171-01-3 161AZ 161MQ 171AL 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI NONE A340-500833 843 172IF BCRCSSI NONE INSTALLEDORA340-600IF BCRCINSTALLEDR ZL-171-02-1 162ZW 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 38.31.00/02 A340-200FLOOR PANELS FROM FR 172 MSI 38.32.00/01 OR73 TO FR 80A340-300NOTE 1 SSI 535122-01-1ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 10APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-171-02-2 161AZ 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 38.31.00/02 A340-500FLOOR PANELS FROM FR 172 MSI 38.32.00/01 IF NOT BCRC73 TO FR 80INSTALLEDNOTE 1 SSI 535202-01-1 ORA340-600IF NOT BCRCINSTALLEDR ZL-171-02-3 161AZ 161MQ 171AL 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 38.31.00/02 A340-500833 843 172 MSI 38.32.00/01 IF BCRCFLOOR PANELS FROM FRINSTALLED73 TO FR 80 SSI 535202-01-1 ORNOTE 1A340-600IF BCRCINSTALLEDR ZL-191-01-1 191FB 191KB 192JB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI NONE A340-200192PB 192ORSSI NONE A340-300R ZL-191-01-2 191BB 191DB 192BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI NONE A340-500192DB 192JB 192PB 192ORSSI NONE A340-600R ZL-191-02-1 191AB 191AT 191BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 A340-200191BT 191CB 191CT 192OR191DB 191EB 191FB SSI NONE A340-300191HB 191KB 191QB192AT 192BB 192BT192CB 192CT 192GB192HB 192JB 192MB192NB 192PB 192QBR ZL-191-02-2 191AB 191AT 191BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 A340-500191BT 191CB 191CTOR191DB 191FB 192AT SSI NONE A340-600192BB 192BT 192CB192CT 192DB 192FB192GB 192HB 192JB192MB 192NB 192PB* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 11APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-191-02-2 * * * * * C O N T I N U E * * * * *192QBR ZL-193-01-1 193BB 193DB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 21.25.00/03 A340-200ORSSI NONE A340-300R ZL-193-01-2 193BB 193DB 193HB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 21.25.00/03 A340-500ORSSI NONE A340-600R ZL-193-02-1 193AB 193BB 193CB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 A340-200193DBORSSI NONE A340-300R ZL-193-02-2 193AB 193BB 193CB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 A340-500193DB 193FB 193HBORSSI NONE A340-600R ZL-195-01-1 734 744 195 HYDRAULIC COMPARTMENT AND FAIRINGS (AS FAR AS I: A MSI 29.10.00/17 ALL196 VISIBLE) (EWIS)SSI NONER ZL-195-02-1 195AB 195BB 196AB 195 HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) I: 2 C MSI 21.25.00/03 A340-200196BB 196 MSI 29.10.00/17 ORA340-300SSI NONER ZL-195-02-2 195CT 195GB 195JB 195 HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) I: 2 C MSI 21.25.00/03 A340-500195NB 195PB 195QB 196 MSI 29.10.00/17 OR734 744A340-600SSI NONER ZL-197-01-1 734 744 197 REAR FAIRINGS (EWIS) I: A MSI NONE ALL198* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 12APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-197-01-1 * * * * * C O N T I N U E * * * * *SSI NONER ZL-197-02-1 197EB 198EB 197 REAR FAIRINGS (EWIS) I: 4 C MSI NONE A340-200198ORSSI NONE A340-300R ZL-197-02-2 197AB 197AT 197FB 197 REAR FAIRINGS (EWIS) I: 4 C MSI NONE A340-500197GB 197HB 198AB 198OR198AT 198FB 198GB SSI NONE A340-600198HB* * * * * E N D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 13APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-200-01-1 N/A 200 UPPER HALF OF FUSELAGE I: 2 C MSI NONE A340-200ORSSI 531103-01-1 A340-300SSI 531107-01-1SSI 531111-01-1SSI 532117-01-2SSI 532121-01-1SSI 532166-01-2SSI 533101-01-1SSI 533193-01-2SSI 534124-01-2SSI 534130-01-1SSI 534177-01-2R ZL-200-01-2 N/A 200 UPPER HALF OF FUSELAGE I: 2 C MSI NONE A340-500ORSSI 531803-01-1 A340-600SSI 531807-01-1SSI 531811-01-1SSI 532217-01-1SSI 532221-01-1SSI 532266-01-1SSI 533801-01-1SSI 534224-01-1SSI 534230-01-1SSI 534270-01-1SSI 534277-01-1R ZL-211-01-1 211JW 211KW 212JW 211 COCKPIT (EWIS) I: 2 C MSI NONE ALL212KW 831 841 212SSI NONER ZL-211-02-1 211AC 211AW 211BC 211 COCKPIT (EWIS) I: 8 C MSI NONE A340-200211BW 211CC 211CW 212OR211DC 211DW 211EC SSI 531156-01-1 A340-300211EW 211FC 211FW SSI 531170-01-1211GC 211GW 211HC211HW 211JC 211JW211KC 211KW 211LC211LW 211MC 211MW211PW 212BC 212CC212CW 212DC 212DW* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-211-02-1 * * * * * C O N T I N U E * * * * *212EW 212FC 212FW212GC 212GW 212HC212HW 212JC 212JW212KW 212LW 212MW212NC 212NW 212QW831 841FLOOR PANELS FROM FR1 TO FR 11NOTE 1R ZL-211-02-2 211AC 211AW 211BC 211 COCKPIT (EWIS) I: 8 C MSI NONE A340-500211BW 211CC 211CW 212OR211DC 211DW 211EC SSI 531856-01-1 A340-600211EW 211FC 211FW SSI 531870-01-1211GC 211GW 211HC211HW 211JC 211JW211KC 211KW 211LC211LW 211MC 211MW211PW 212BC 212CC212CW 212DC 212DW212EW 212FC 212FW212GC 212GW 212HC212HW 212JC 212JW212KW 212LW 212MW212NC 212NW 212QW831 841FLOOR PANELS FROM FR1 TO FR 11NOTE 1R ZL-221-02-1 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 25.74.00/02 A340-200DOOR FRAME LININGS 222ORFCRC (IF INSTALLED) SSI 531156-01-1 A340-300FLOOR PANELS FROM FR11 TO FR 17GALLEYS AND TOILETSNOTE 1SEATS ANDFURNISHINGSISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-221-02-2 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 25.74.00/02 A340-500DOOR FRAME LININGS 222ORFCRC (IF INSTALLED) SSI 531856-01-1 A340-600FLOOR PANELS FROM FR11 TO FR 17GALLEYS AND TOILETSNOTE 1SEATS ANDFURNISHINGSR ZL-223-01-1 221AZ 221BZ 222AZ 223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-200222BZ 831 841 224ORCEILING PANELS FROM SSI 531156-01-1 A340-300FR 11 TO FR 17FCRCGALLEYS AND TOILETS(IF INSTALLED)NOTE 1R ZL-223-01-2 221AZ 221BZ 222AZ 223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 25.74.00/02 A340-500222BZ 831 841 224ORCEILING PANELS SSI 531856-01-1 A340-600FCRCGALLEYS AND TOILETSFROM FR 11 TO FR 17(IF INSTALLED)NOTE 1ZL-231-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-231-02-1 831 841 231 FWD CABIN (EWIS) I: 8 C MSI NONE A340-200GALLEYS AND TOILETS 232OR(IF INSTALLED) SSI 532119-01-1 A340-300NOTE 1 SSI 532135-01-1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 17 TOFR 31ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-231-02-2 831 841 231 FWD CABIN (EWIS) I: 8 C MSI NONE A340-500GALLEYS AND TOILETS 232OR(IF INSTALLED) SSI 532219-01-1 A340-600NOTE 1 SSI 532235-01-1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 17 TOFR 37.7R ZL-233-01-1 831 841 233 FWD CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-200CEILING PANELS 234ORGALLEYS AND TOILETS SSI 532120-01-1 A340-300(IF INSTALLED)NOTE 1OVERHEAD STOWAGEBINS FROM FR 17 TOFR 31R ZL-233-01-2 831 841 233 FWD CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-500CEILING PANELS 234ORGALLEYS AND TOILETS SSI 532220-01-1 A340-600(IF INSTALLED)NOTE 1OVERHEAD STOWAGEBINS FROM FR 17 TOFR 37.7ZL-241-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-241-02-1 832 842 241 MID CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A340-200DOOR FRAME LININGS 242ORFLOOR PANELS FROM FR SSI 532119-01-1 A340-30031 TO FR 36 SSI 532135-01-1GALLEYS AND TOILETS(IF INSTALLED)NOTE 1SEATS ANDFURNISHINGSISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-241-02-2 832 842 241 MID CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A340-500DOOR FRAME LININGS 242ORFLOOR PANELS FROM FR SSI 532219-01-1 A340-60037.7 TO FR 37.11 SSI 532235-01-1GALLEYS AND TOILETS(IF INSTALLED)NOTE 1SEATS ANDFURNISHINGSR ZL-243-01-1 832 842 243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-200CEILING PANELS FROM 244ORFR 31 TO FR 36 SSI 532120-01-1 A340-300GALLEYS AND TOILETS(IF INSTALLED)NOTE 1R ZL-243-01-2 832 842 243 MID CABIN UTILITY AREA OVERHEAD COMPARTMEN (EWIS) I: 8 C MSI NONE A340-500CEILING PANELS FROM 244ORFR 37.7 TO FR 37.11 SSI 532220-01-1 A340-600GALLEYS AND TOILETS(IF INSTALLED)NOTE 1ZL-251-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-251-02-1 832 842 251 MID CABIN (EWIS) I: 8 C MSI 25.75.00/05 A340-200NOTE 1 252ORSEATS, FURNISHINGS SSI 533148-01-1 A340-300GALLEYS, TOILETS ANDSTAIRHOUSE (IFINSTALLED)SIDEWALL AND FLOORPANELS FROM FR 36 TOFR 53.5R ZL-251-02-2 832 842 251 MID CABIN (EWIS) I: 8 C MSI 25.75.00/05 A340-500252* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-251-02-2 * * * * * C O N T I N U E * * * * *GALLEYS, TOILETS AND SSI 532235-01-1STAIRHOUSE (IF SSI 533848-01-1INSTALLED)NOTE 1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 37.11TO FR 53.4R ZL-251-02-3 832 842 251 MID CABIN (EWIS) I: 8 C MSI 25.75.00/05 A340-600GALLEYS, TOILETS AND 252STAIRHOUSE (IF SSI 532235-01-1INSTALLED) SSI 533848-01-1NOTE 1 SSI 534257-03-1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 37.11TO FR 56.1R ZL-253-01-1 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 25.75.00/05 A340-200CEILING PANELS 254OROVERHEAD STOWAGE SSI 533147-01-1 A340-300BINS FROM FR 36 TOFR 53.5GALLEYS AND TOILETS(IF INSTALLED)NOTE 1R ZL-253-01-2 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-500CEILING PANELS 254OVERHEAD STOWAGE SSI 533847-01-1BINSGALLEYS AND TOILETSFROM FR 37.11 TO FR53.4 (IF INSTALLED)NOTE 1ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 6APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-253-01-3 832 842 253 MID CABIN OVERHEAD COMPARTMEN (EWIS) I: 8 C MSI NONE A340-600CEILING PANELS 254OVERHEAD STOWAGE SSI 533847-01-1BINS FROM FR 37.11TO FR 56.1GALLEYS AND TOILETS(IF INSTALLED)NOTE 1ZL-261-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-261-02-1 834 844 261 AFT CABIN (EWIS) I: 8 C MSI NONE A340-200DOOR FRAME LININGS 262ORGALLEYS AND TOILETS SSI 534157-01-1 A340-300(IF INSTALLED) SSI 534161-01-1NOTE 1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 53.5TO FR 72R ZL-261-02-2 834 844 261 AFT CABIN (EWIS) I: 8 C MSI NONE A340-500DOOR FRAME LININGS 262GALLEYS AND TOILETS SSI 534257-01-1(IF INSTALLED) SSI 534257-02-1NOTE 1 SSI 534261-01-1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 53.4TO FR 72R ZL-261-02-3 834 844 261 AFT CABIN (EWIS) I: 8 C MSI NONE A340-600DOOR FRAME LININGS 262GALLEYS AND TOILETS SSI 534257-03-1(IF INSTALLED) SSI 534261-02-1NOTE 1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 7APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-261-02-3 * * * * * C O N T I N U E * * * * *SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 56.1TO FR 72R ZL-263-01-1 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-200CEILING PANELS 264OROVERHEAD STOWAGE SSI 534160-01-1 A340-300BINSGALLEYS AND TOILETSFROM FR 53.5 TO FR72 (IF INSTALLED)NOTE 1R ZL-263-01-2 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-500CEILING PANELS 264OVERHEAD STOWAGE SSI 534260-01-1BINSGALLEYS AND TOILETSFROM FR 53.4 TO FR72 (IF INSTALLED)NOTE 1R ZL-263-01-3 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-600CEILING PANELS 264OVERHEAD STOWAGE SSI 534260-02-1BINS FROM FR 56.1 TOFR 72GALLEYS AND TOILETS(IF INSTALLED)NOTE 1ZL-271-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-271-02-1 833 843 271 AFT CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A340-200* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 8APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-271-02-1 * * * * * C O N T I N U E * * * * *DOOR FRAME LININGS 272 SSI 534157-01-1 ORFLOOR PANELS FROM FR SSI 534161-01-1 A340-30072 TO FR 80 SSI 535121-01-1GALLEYS AND TOILETS(IF INSTALLED)NOTE 1SEATS ANDFURNISHINGSR ZL-271-02-2 833 843 271 AFT CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A340-500DOOR FRAME LININGS 272ORFLOOR PANELS FROM FR SSI 534257-01-1 A340-60072 TO FR 80 SSI 534257-02-1GALLEYS AND TOILETS SSI 534257-03-1(IF INSTALLED) SSI 534261-01-1NOTE 1 SSI 534261-02-1SEATS ANDFURNISHINGSSIDEWALL LININGR ZL-273-01-1 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-200272AZ 272BZ 272CZ 274OR833 843 SSI 534160-01-1 A340-300CEILING PANELS FROM SSI 535121-01-1FR 72 TO FR 80GALLEYS AND TOILETS(IF INSTALLED)NOTE 1R ZL-273-01-2 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-500272AZ 272BZ 272CZ 274833 843 SSI 534260-01-1CEILING PANELS FROMFR 72 TO FR 80GALLEYS AND TOILETS(IF INSTALLED)NOTE 1R ZL-273-01-3 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A340-600* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 9APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-273-01-3 * * * * * C O N T I N U E * * * * *272AZ 272BZ 272CZ 274 SSI 534260-02-1833 843CEILING PANELS FROMFR 72 TO FR 80GALLEYS AND TOILETS(IF INSTALLED)NOTE 1* * * * * E N D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 10APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-300-01-1 N/A 300 STABILIZERS AND FUSELAGE REAR SECTION I: 2 C MSI NONE A340-200ORSSI 535111-01-1 A340-300SSI 535111-02-1SSI 535114-01-1SSI 551020-02-1SSI 551021-01-1SSI 551026-01-1SSI 552001-01-1SSI 554001-01-1SSI 554014-01-1R ZL-300-01-2 N/A 300 STABILIZERS AND FUSELAGE REAR SECTION I: 2 C MSI NONE A340-500ORSSI 535211-01-1 A340-600SSI 535214-01-1SSI 551065-01-1SSI 551066-01-1SSI 552054-01-1SSI 554070-01-1SSI 554079-01-1R ZL-311-01-1 312AR 313AL 311 REAR FUSELAGE SECTION (EWIS) I: C MSI 28.22.00/05 A340-200312 MSI 49.16.00/01-35 ORA340-300SSI 535123-01-1SSI 551007-01-1SSI 551010-01-1SSI 551012-01-1SSI 551015-01-1R ZL-311-01-2 312AR 313BL 311 REAR FUSELAGE SECTION (EWIS) I: C MSI 49.16.00/01-60 A340-500TRANSFER PUMP 312 MSI 49.16.00/02-60 ORCOVER/SEALING CASEA340-600SSI 551061-01-1SSI 551062-01-1SSI 551063-01-1R ZL-313-01-1 313AL 313 TAIL CONE APU AIR INTAKE AREA (EWIS) I: C MSI 28.22.00/05 A340-200314 MSI 49.16.00/01-35 ORA340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-313-01-1 * * * * * C O N T I N U E * * * * *SSI NONER ZL-313-01-2 313BL 313 TAIL CONE APU AIR INTAKE AREA (EWIS) I: C MSI 49.16.00/01-60 A340-500314ORSSI NONE A340-600R ZL-315-01-1 315AL 316AR 315 TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS) I: C MSI 49.17.00/02-35 ALL316 MSI 49.17.00/02-60MSI 49.30.00/01-60SSI NONER ZL-317-01-1 317AL 317 TAIL CONE APU EXHAUST AREA (EWIS) I: C MSI 49.17.00/02-35 A340-200ORSSI NONE A340-300R ZL-317-01-2 317BL 317 TAIL CONE APU EXHAUST AREA (EWIS) I: C MSI 49.17.00/02-60 A340-500ORSSI NONE A340-600ZL-319-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-319-02-1 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL) (EWIS) I: 8 C MSI NONE A340-200319AR 319BL 319BRPRE 41600319CR SSI 551018-01-1 ORDISCONNECT SCAVENGEA340-300WATER SYSTEM PIPEPRE 41600R ZL-319-02-2 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL) (EWIS) I: 8 C MSI NONE A340-200319AR 319BL 319DRPOST 41600319ER SSI NONE ORA340-300POST 41600ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-319-02-3 311CZ 311DZ 312AR 319 HORIZONTAL STABILIZER SPAR BOX INSIDE FUSELAGE I: 8 C MSI NONE A340-500312CZ 312DZ 313BL (INTERNAL) (EWIS)ORSSI 551064-01-1 A340-600R ZL-321-01-1 321AL 321 DORSAL FIN (EWIS) I: 8 C MSI NONE ALLSSI NONER ZL-322-01-1 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A340-200ORSSI 553010-01-1 A340-300R ZL-322-01-2 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A340-500322ELORSSI 553072-01-1 A340-600R ZL-323-01-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 4 C MSI NONE A340-200ORSSI 553011-01-1 A340-300R ZL-323-01-2 311AZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 4 C MSI NONE A340-500ORSSI 553073-01-1 A340-600R ZL-323-02-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI NONE A340-200322AL 322BL 322CLOR323AL 323BL 325AL INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 553013-01-1 A340-300325BL 325CL 325DL FITTINGS325EL 325FL 325GL325HL 325JL 325KLPEELABLE HOLE COVERSR ZL-323-02-2 311AZ 312AR 322AL 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI NONE A340-500322BL 322CL 322ELOR323DL 323EL 325LL INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 553075-01-1 A340-600325NL 325SL 325TL FITTINGS325UL 325VL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-323-02-2 * * * * * C O N T I N U E * * * * *PEELABLE HOLE COVERSR ZL-324-01-1 324AT 324BT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A340-200ORSSI 553010-01-1 A340-300R ZL-324-01-2 324CT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A340-500ORSSI 553072-01-1 A340-600SSI 553075-01-1R ZL-325-01-1 325DL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A340-200ORSSI NONE A340-300R ZL-325-01-2 325NL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A340-500ORSSI NONE A340-600R ZL-325-02-1 325AL 325BL 325CL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A340-200325DL 325EL 325FLOR325GL 325HL 325JL SSI 553009-01-1 A340-300325KLR ZL-325-02-2 325LL 325NL 325SL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A340-500325TL 325UL 325VLORSSI 553071-01-1 A340-600R ZL-326-01-1 326DL 326 RUDDER (EWIS) I: C MSI NONE A340-200OR(AREA OF BEARINGS 2, 3 AND 4) SSI NONE A340-300R ZL-326-01-2 325NL 326ML 326NL 326 RUDDER (EWIS) I: C MSI NONE A340-500326PLOR(AREA OF BEARINGS 2, 3, 4 AND 5) SSI NONE A340-600ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-326-02-1 326BL 326DL 326FL 326 RUDDER (EWIS) I: 4 C MSI NONE A340-200326HL 326KLPRE 40904(AREA OF BEARINGS 1 TO 7) SSI NONE ORA340-300PRE 40904R ZL-326-02-2 325BL 325FL 325HL 326 RUDDER (EWIS) I: 4 C MSI NONE A340-200325KL 326DLPOST 40904(AREA OF BEARINGS 1 TO 7) SSI NONE ORA340-300POST 40904R ZL-326-03-1 325AL 325BL 325DL 326 RUDDER (EWIS) I: 8 C MSI NONE A340-200325FL 325HL 325KLPRE 40904326AL 326BL 326BR (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI NONE OR326CL 326DL 326DR VISIBLE)A340-300326EL 326FL 326FRPRE 40904326GL 326HL 326HR326JL 326KL 326KR326LLR ZL-326-03-2 325AL 325BL 325CL 326 RUDDER (EWIS) I: 8 C MSI NONE A340-200325CR 325DL 325ELPOST 40904325ER 325FL 325GL (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI NONE OR325GR 325HL 325JL VISIBLE)A340-300325JR 325KL 326ATPOST 40904326DL 326DRR ZL-326-03-3 324CT 325LL 325LR 326 RUDDER (EWIS) I: 8 C MSI NONE A340-500325NL 325NR 325SLOR325SR 325TL 325TR (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI NONE A340-600325UL 325VL 325VR VISIBLE)326AT 326ML 326NL326PL 326RL 326SLR ZL-326-04-1 325NL 325SL 325TL 326 RUDDER (EWIS) I: 4 C MSI NONE A340-500325UL 325VL 326MLOR326NL 326PL 326RL (IN AREA OF BEARINGS 1 TO 8) SSI NONE A340-600326SLISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-331-01-1 331AT 331BT 331CT 331 HORIZONTAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A340-200331DT 331ET 333AB 341OR333AT 341AT 341BT SSI 551024-01-1 A340-300341CT 341DT 341ET SSI 551025-01-1343AB 343ATR ZL-331-01-2 331AT 331BT 331CT 331 HORIZONTAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A340-500331DT 331ET 331FT 341OR341AT 341BT 341CT SSI 551056-01-1 A340-600341DT 341ET 341FTR ZL-332-01-1 332AB 332AT 342AB 332 HORIZONTAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A340-200342AT 342ORSSI 551025-01-1 A340-300R ZL-332-01-2 332AB 332AT 342AB 332 HORIZONTAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A340-500342AT 342ORSSI 551056-01-1 A340-600R ZL-333-01-1 331AT 331BT 333AB 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI NONE A340-200333AL 333AT 341AT 343OR341BT 343AB 343AR (RIB 3 TO RIB 4). SSI NONE A340-300343ATR ZL-333-01-2 331ET 332AB 332AT 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI NONE A340-200333EL 343POST 43491(RIB 13 TO END RIB LH). SSI 551035-02-1 PRE 44818ORA340-300POST 43491PRE 44818R ZL-333-02-1 331AT 331AZ 333BB 333 HORIZONTAL STABILIZER SPAR BOX FUEL TANK (EWIS) I: 8 C MSI NONE A340-500333CB 333DB 333EB 343PRE 54173333FB 333GB 333HB (FROM RIB 3 TO RIB 15LH/14RH). SSI 551067-01-1 OR333JB 333KB 333LBA340-600333MB 341AT 341AZPRE 54173343BB 343CB 343DB343EB 343FB 343GB* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 6APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-333-02-1 * * * * * C O N T I N U E * * * * *343HB 343JB 343KB343LBR ZL-333-02-2 331AT 331AZ 333BB 333 HORIZONTAL STABILIZER SPAR BOX FUEL TANK (EWIS) I: 8 C MSI NONE A340-500333CB 333DB 333EB 343POST 54173333FB 333GB 333HB (FROM RIB 3 TO RIB 20 LH, RIB 17 RH). SSI 551069-01-1 OR333JB 333KB 333LBA340-600333MB 333NB 333PBPOST 54173333QB 333SB 333TB341AT 341AZ 343BB343CB 343DB 343EB343FB 343GB 343HB343JB 343KB 343LB343MB 343NB 343PBR ZL-334-01-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A340-200344AB 344BB 344CB 344OR(FUSELAGE FAIRING TO RIB 10) SSI NONE A340-300R ZL-334-01-2 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A340-500334CT 344AB 344BB 344OR344CB 344CT (FROM FUSELAGE FAIRING TO RIB 10) SSI NONE A340-600R ZL-334-02-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A340-200334DB 334EB 334FB 344OR334GB 344AB 344BB (FUSELAGE FAIRING TO RIB 21) SSI 551030-01-1 A340-300344CB 344DB 344EB344FB 344GBR ZL-334-02-2 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A340-500334DB 334EB 334FB 344OR344AB 344BB 344CB (FROM FUSELAGE FAIRING TO RIB 21) SSI 551058-01-1 A340-600344DB 344EB 344FBR ZL-335-01-1 334BB 334CB 334DB 335 ELEVATOR (EWIS) I: C MSI NONE A340-200335BB 344BB 344CB 345OR344DB 345BB (AREA BETWEEN RIBS 8 AND 9) SSI NONE A340-300ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 7APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-335-02-1 334AB 334BB 334CB 335 ELEVATOR (EWIS) I: 8 C MSI NONE A340-200334DB 334EB 334FB 345OR334GB 335AB 335BB (LEADING EDGE AS FAR AS VISIBLE) SSI NONE A340-300335CB 335DB 335EB335FB 344AB 344BB344CB 344DB 344EB344FB 344GB 345AB345BB 345CB 345DB345EB 345FBR ZL-335-02-2 334AB 334BB 334CB 335 ELEVATOR (EWIS) I: 8 C MSI NONE A340-500334DB 334EB 334FB 345OR335AB 335BB 335CB (LEADING EDGE AS FAR AS VISIBLE) SSI 552051-01-1 A340-600335DB 335EB 335FB335GB 335HB 335JB344AB 344BB 344CB344DB 344EB 344FB345AB 345BB 345CB345DB 345EB 345FB345GB 345HB 345JBR ZL-335-03-1 334CB 335CB 335DB 335 ELEVATOR (EWIS) I: C MSI NONE A340-500335EB 344CB 345CB 345OR345DB 345EB (AREA BETWEEN RIB 9 AND 10) SSI NONE A340-600R ZL-337-01-1 331ET 331FT 332AB 337 HORIZONTAL STABILIZER SPAR BOX DRY BAY (EWIS) I: 8 C MSI NONE A340-500332AT 334EB 334FB 347PRE 54173334FT 341FT 342AB (FROM RIB 15LH/16RH TO RIB 21 LH/RH) SSI 551068-01-1 OR342AT 344EB 344FBA340-600344FTPRE 54173PEELABLE HOLE COVERSR ZL-337-01-2 332AB 332AT 334ET 337 HORIZONTAL STABILIZER SPAR BOX DRY BAY (EWIS) I: 8 C MSI NONE A340-500334FB 342AB 342AT 347POST 54173344ET 344FB (FROM RIB 20 TO RIB 21 LH/RH). SSI 551070-01-1 ORPEELABLE HOLE COVERSA340-600POST 54173R ZL-346-01-1 346AB 346 HORIZONTAL STABILIZER SPAR BOX VENT TANK (EWIS) I: 8 C MSI NONE A340-500PRE 54173* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 8APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-346-01-1 * * * * * C O N T I N U E * * * * *(FROM RIB 14RH TO RIB 16RH) SSI 551067-01-1 ORA340-600PRE 54173R ZL-346-01-2 346AB 346BB 346CB 346 HORIZONTAL STABILIZER SPAR BOX VENT TANK (EWIS) I: 8 C MSI NONE A340-500POST 54173(FROM RIB 17 RH TO RIB 20 RH). SSI 551069-01-1 ORA340-600POST 54173* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 9APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-400-01-1 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI NONE A340-200ORSSI NONE A340-300ZL-400-01-2 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI 75.21.00/01-R5 A340-500ORSSI NONE A340-600R ZL-411-01-1 411AR 421AR 431AR 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI 30.21.04/03 ALL441AR 421431 SSI NONE441R ZL-411-02-1 411AR 411AZ 411BZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI NONE CFM411CZ 411DZ 415AL 421416AR 421AR 421AZ 431 SSI NONE421BZ 421CZ 421DZ 441425AL 426AR 431AR431AZ 431BZ 431CZ431DZ 435AL 436AR441AR 441AZ 441BZ441CZ 441DZ 445AL446ARZL-411-04-1 N/A ENGINE AIR INTAKE AND INTAKE LIP MSI NONETASK DELETED SSI NONER ZL-411-04-2 411AL 411AR 411AZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI NONE RR411BZ 415AL 416AR 421421AL 421AR 421AZ 431 SSI NONE421BZ 425AL 426AR 441431AL 431AR 431AZ431BZ 435AL 436AR441AL 441AR 441AZ441BZ 445AL 446ARISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-412-01-1 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 71.10.00/06-C5 CFM426AR 435AL 436AR 422 MSI 71.10.00/07-C5445AL 446AR 432 MSI 72.60.00/03-C5442SSI NONER ZL-412-04-1 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 75.21.00/01-R5 RR426AR 435AL 436AR 422445AL 446AR 432 SSI NONE442R ZL-413-01-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI NONE CFM418AR 425AL 426AR 423427AL 428AR 435AL 433 SSI NONE436AR 437AL 438AR 443445AL 446AR 447AL448ARR ZL-413-04-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI 72.22.00/01-R5 RR417FL 418AR 425AL 423426AR 427AL 427FL 433 SSI NONE428AR 435AL 436AR 443437AL 437FL 438AR445AL 446AR 447AL447FL 448ARR ZL-414-01-1 417AL 418AR 427AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI NONE CFM428AR 437AL 438AR 424447AL 448AR 434 SSI NONE444R ZL-414-04-1 415AL 416AR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI NONE RR417FL 418AR 425AL 424426AR 427AL 427FL 434 SSI NONE428AR 435AL 436AR 444437AL 437FL 438AR445AL 446AR 447AL447FL 448ARISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-415-01-1 415AL 415BL 416AR 415 FAN COWL (EWIS) I: 2 C MSI NONE CFM416BR 416CR 425AL 416425BL 426AR 426BR 425 SSI 711311-02-1426CR 435AL 435BL 426436AR 436BR 436CR 435445AL 445BL 446AR 436446BR 446CR 445446R ZL-415-04-1 415AL 415CL 416AR 415 FAN COWL (EWIS) I: 2 C MSI NONE RR416BR 416CR 425AL 416425CL 426AR 426BR 425 SSI NONE426CR 435AL 435CL 426436AR 436BR 436CR 435445AL 445CL 446AR 436446BR 446CR 445446R ZL-417-01-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 78.32.00/04-C5 CFM417BL 417CL 417DL 418417EL 418AR 418BR 427 SSI 722301-02-1418CR 418DR 418ER 428 SSI 783207-01-1425AL 426AR 427AL 437 SSI 783208-01-1427BL 427CL 427DL 438427EL 428AR 428BR 447428CR 428DR 428ER 448437AL 437BL 437CL437DL 437EL 438AR438BR 438CR 438DR438ER 445AL 446AR447AL 447BL 447CL447DL 447EL 448AR448BR 448CR 448DR448ERTHRUST REVERSERDEPLOYEDR ZL-417-04-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 78.11.00/01-R5 RR417BL 417CL 417DL 418 MSI 78.31.00/01-R5417EL 417FL 418AR 427 MSI 78.32.00/01-R5418BR 418CR 418DR 428 MSI 78.32.00/02-R5418ER 425AL 426AR 437* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-417-04-1 * * * * * C O N T I N U E * * * * *427AL 427BL 427CL 438 SSI NONE427DL 427EL 427FL 447428AR 428BR 428CR 448428DR 428ER 435AL436AR 437AL 437BL437CL 437DL 437EL437FL 438AR 438BR438CR 438DR 438ER445AL 446AR 447AL447BL 447CL 447DL447EL 447FL 448AR448BR 448CR 448DR448ERTHRUST REVERSERDEPLOYEDR ZL-419-01-1 415AL 416AR 417AL 419 EXHAUST PLUG (EWIS) I: 2 C MSI NONE RR417FL 418AR 425AL 429426AR 427AL 427FL 439 SSI NONE428AR 435AL 436AR 449437AL 437FL 438AR445AL 446AR 447AL447FL 448ARR ZL-451-01-1 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI NONE CFM451CR 461BL 461BR 461461CL 461CR 471BL 471 SSI NONE471BR 471CL 471CR 481481BL 481BR 481CL481CRR ZL-451-04-1 451AR 451BL 451BR 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI NONE RR451CL 461AR 461BL 461461BR 461CL 471AR 471 SSI NONE471BL 471BR 471CL 481481AR 481BL 481BR481CLR ZL-452-01-1 452AL 452AR 452AZ 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI NONE CFM* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-452-01-1 * * * * * C O N T I N U E * * * * *452BL 452BZ 452CL 462 SSI 572003-02-1 PRE 41371452CZ 452DR 452EL 472 SSI 572003-02-2 PRE 42283452FR 462AL 462AR 482 SSI 572113-02-1462BL 462CL 462CR SSI 572115-01-1462DL 462EL 462FR462GR 462HL 472AL472AR 472BL 472CL472CR 472DL 472ER472FL 472GL 472HR482AL 482AR 482AZ482BL 482BZ 482CR482CZ 482DL 482ER482FLR ZL-452-01-2 452AL 452AR 452AZ 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI NONE CFM452BL 452BZ 452CL 462POST 41371452CZ 452DR 452FR 472 SSI 572003-02-1 PRE 42283452GL 462AL 462AR 482 SSI 572003-02-2462BL 462CL 462CR SSI 572113-02-1462EL 462GL 462GR SSI 572115-01-1462HL 462HR 472AL472AR 472BL 472CL472CR 472DL 472GL472HL 472HR 472JR482AL 482AR 482AZ482BL 482BZ 482CR482CZ 482FL 482GL482HRZL-452-01-3 N/A TASK DELETED MSI NONESSI NONER ZL-452-01-4 452DZ 452EZ 452FL 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI NONE CFM452HL 452JL 452JR 462POST 42283452KL 452KR 452MR 472 SSI 572003-02-1462AL 462AR 462BL 482 SSI 572003-02-2462CL 462CR 462DL SSI 572113-02-2462EL 462FR 462GR SSI 572115-01-2462HL 472AL 472AR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-452-01-4 * * * * * C O N T I N U E * * * * *472BL 472CL 472CR472DL 472ER 472FL472GL 472HR 482DZ482JL 482JR 482KL482KR 482ML 482MR482NLR ZL-452-04-1 452AL 452AR 452BL 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI NONE RR452BR 452CL 452CR 462452DL 452DR 452EL 472 SSI 572202-01-1452ER 452FL 452FR 482 SSI 572306-01-1452GL 452GR 452HL452JL 462AL 462AR462BL 462BR 462CL462CR 462DL 462DR462EL 462ER 462FL462FR 462GL 462GR462HL 462JL 472AL472AR 472BL 472BR472CL 472CR 472DL472DR 472EL 472ER472FL 472FR 472GL472GR 472HL 472JL482AL 482AR 482BR482CR 482DL 482DR482EL 482ER 482FL482FR 482GL 482GR482HL 482JLR ZL-453-01-1 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI NONE CFM453BR 453CL 453CR 463463AL 463AR 463BL 473 SSI NONE463BR 463CL 463CR 483473AL 473AR 473BL473BR 473CL 473CR483AL 483AR 483BL483BR 483CL 483CRR ZL-453-04-1 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI NONE RR453BR 453CL 453CR 463* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 6APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-453-04-1 * * * * * C O N T I N U E * * * * *453DL 453DR 453EL 473 SSI NONE453ER 463AL 463AR 483463BL 463BR 463CL463CR 463DL 463DR473AL 473AR 473BL473BR 473CL 473CR473DL 473DR 483AL483AR 483BL 483BR483CL 483CR 483DL483DR 483EL 483ERR ZL-454-01-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI NONE CFM454BR 454EL 454ER 464PRE 42283454FL 454GL 454JL 474 SSI NONE PRE 43183454JR 454KL 464AL 484464AR 464BL 464BR464EL 464ER 464FL464GL 464HL 474AL474AR 474BL 474BR474EL 474ER 474FL474GL 474HL 484AL484AR 484BL 484BR484EL 484ER 484FL484GL 484JL 484JR484KLR ZL-454-01-2 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI NONE CFM454BR 454EL 454ER 464PRE 42283454FL 454GL 454JL 474 SSI NONE POST 43183454JR 454KL 464AL 484464EL 464ER 464GL464HL 464JL 464KL464KR 464MR 474AL474EL 474ER 474GL474HL 474JL 474KL474KR 474MR 484AL484AR 484BL 484BR484EL 484ER 484FL484GL 484JL 484JR484KLISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 7APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-454-01-3 454AL 454BL 454EL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI NONE CFM454ER 454JL 454JR 464POST 42283454KL 454KR 454MR 474 SSI NONE POST 43183454QL 454SL 464AL 484464EL 464ER 464GL464HL 464JL 464KL464KR 464MR 474AL474EL 474ER 474GL474HL 474JL 474KL474KR 474MR 484EL484ER 484JL 484JR484KL 484KR 484ML484NL 484NR 484PL484QLR ZL-454-02-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI NONE CFM454BR 454CL 454DL 464PRE 42283454EL 454ER 454FL 474 SSI 572003-02-1 PRE 43183454FR 454GL 454GR 484 SSI 572013-02-2454HL 454JL 454JR SSI 572021-02-1454KL 464AL 464AR SSI 572021-02-2464BL 464BR 464CL SSI 572113-02-1464DL 464EL 464ER SSI 572115-01-1464FL 464FR 464GL SSI 575015-01-1464GR 464HL 474AL474AR 474BL 474BR474CL 474DL 474EL474ER 474FL 474FR474GL 474GR 474HL484AL 484AR 484BL484BR 484CL 484DL484EL 484ER 484FL484FR 484GL 484GR484HL 484JL 484JR484KLR ZL-454-02-2 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI NONE CFM454BR 454CL 454DL 464PRE 42283454EL 454ER 454FL 474 SSI 572003-02-2 POST 43183454FR 454GL 454GR 484 SSI 572021-02-1454HL 454JL 454JR SSI 572113-02-1454KL 464AL 464CL SSI 572115-01-1464DL 464EL 464ER SSI 575015-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 8APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-454-02-2 * * * * * C O N T I N U E * * * * *464GL 464GR 464HL464JL 464JR 464KL464KR 464MR 474AL474CL 474DL 474EL474ER 474GL 474GR474HL 474JL 474JR474KL 474KR 474MR484AL 484AR 484BL484BR 484CL 484DL484EL 484ER 484FL484FR 484GL 484GR484HL 484JL 484JR484KLR ZL-454-02-3 454AL 454BL 454CL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI NONE CFM454DL 454EL 454ER 464POST 42283454HL 454JL 454JR 474 SSI 572003-02-2 POST 43183454KL 454KR 454MR 484 SSI 572021-02-1454NR 454PR 454QL SSI 572113-02-2454SL 464AL 464CL SSI 572115-01-2464DL 464EL 464ER SSI 575015-01-1464GL 464GR 464HL464JL 464JR 464KL464KR 464MR 474AL474CL 474DL 474EL474ER 474GL 474GR474HL 474JL 474JR474KL 474KR 474MR484CL 484DL 484EL484ER 484HL 484JL484JR 484KL 484KR484ML 484NL 484NR484PL 484PR 484QL484QRR ZL-454-03-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI NONE RR454BR 464AL 464AR 464464BL 464BR 464CL 474 SSI NONE464FL 474AL 474AR 484474BL 474BR 474CR474ER 484AL 484AR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 9APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-454-03-1 * * * * * C O N T I N U E * * * * *484BL 484BRR ZL-454-04-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI NONE RR454BR 454CL 454CR 464454DL 454DR 464AL 474 SSI 572305-01-1464AR 464BL 464BR 484 SSI 572306-01-1464CL 464CR 464DL464EL 464FL 474AL474AR 474BL 474BR474CL 474CR 474DL474DR 474ER 484AL484AR 484BL 484BR484CL 484CR 484DL484DR* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 10APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-500-01-1 FLAPS EXTENDED 500 WING LOWER SURFACE (EWIS) I: C MSI NONE A340-200SLATS EXTENDED 600OR(INCLUDING SLATS AND FLAPS, EXCLUDING AREA COVERED BY SSI 572006-02-2 A340-300PLASTRON FAIRING) SSI 572006-02-3SSI 572006-02-4SSI 572006-02-6SSI 572012-03-1SSI 572023-01-1SSI 572102-01-1SSI 572102-01-2SSI 572102-01-3SSI 572102-01-4SSI 572110-02-1SSI 572112-02-1SSI 572116-01-1SSI 572116-01-2SSI 572116-01-3SSI 572116-01-4SSI 574114-02-1SSI 574303-02-2SSI 574303-02-3SSI 574306-02-1SSI 574308-01-1SSI 574403-02-1SSI 574403-02-2SSI 574403-02-3SSI 574406-01-1SSI 574408-01-1SSI 574503-02-1SSI 574503-02-2SSI 574506-02-1SSI 574508-01-1SSI 574603-02-1SSI 574603-02-2SSI 574603-02-3SSI 574606-02-1SSI 574608-01-1SSI 574703-02-1SSI 574703-02-2SSI 574703-02-3SSI 574706-02-1SSI 574708-01-1SSI 574803-02-1SSI 574803-02-2SSI 574803-02-3* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-500-01-1 * * * * * C O N T I N U E * * * * *SSI 574806-02-1SSI 574808-01-1SSI 574903-02-1SSI 574903-02-2SSI 574903-02-3SSI 574906-02-1SSI 574908-01-1SSI 575012-02-1SSI 575013-02-1SSI 575015-01-1SSI 575025-02-1SSI 575401-01-2SSI 575501-01-1SSI 577001-01-1R ZL-500-01-2 FLAPS EXTENDED 500 WING LOWER SURFACE (EWIS) I: C MSI NONE A340-500SLATS EXTENDED 600OR(INCLUDING SLATS AND FLAPS) SSI 572201-01-1 A340-600SSI 572203-01-1SSI 572301-01-1SSI 572302-01-1SSI 574164-01-1SSI 574356-02-1SSI 574358-01-1SSI 574456-01-1SSI 574458-01-1SSI 574556-02-1SSI 574558-01-1SSI 574656-02-1SSI 574658-01-1SSI 574756-02-1SSI 574758-01-1SSI 574856-02-1SSI 574858-01-1SSI 574956-02-1SSI 574958-01-1SSI 575112-01-1SSI 575115-01-1SSI 575451-01-1SSI 575551-01-1ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-500-02-1 FLAPS EXTENDED 500 WING UPPER SURFACE (EWIS) I: 2 C MSI NONE A340-200SLATS EXTENDED 600ORSPOILERS EXTENDED (INCLUDING SLATS, FLAPS AND SPOILERS) SSI 572033-02-1 A340-300SSI 572133-02-1SSI 572134-02-1SSI 572135-01-1SSI 572135-01-2SSI 572135-01-3SSI 572135-01-4SSI 572138-01-2SSI 572138-01-3SSI 572138-01-4SSI 572139-01-2SSI 572139-01-3SSI 572139-01-4SSI 573002-02-1SSI 573006-01-1SSI 574111-02-1SSI 574308-01-1SSI 574408-01-1SSI 574508-01-1SSI 574608-01-1SSI 574708-01-1SSI 574808-01-1SSI 574908-01-1SSI 575011-02-1SSI 575401-01-2SSI 577001-01-1R ZL-500-02-2 FLAPS EXTENDED 500 WING UPPER SURFACE (EWIS) I: 2 C MSI NONE A340-500SLATS EXTENDED 600ORSPOILERS EXTENDED (INCLUDING SLATS, FLAPS AND SPOILERS) SSI 572231-01-1 A340-600SSI 572331-01-1SSI 573052-01-1SSI 573056-01-1SSI 574160-01-1SSI 574161-01-1SSI 574358-01-1SSI 574458-01-1SSI 574558-01-1SSI 574658-01-1SSI 574758-01-1SSI 574858-01-1SSI 574958-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-500-02-2 * * * * * C O N T I N U E * * * * *SSI 575111-01-1SSI 575451-01-1SSI 575551-01-1SSI 577051-01-1R ZL-521-01-1 521AB 521BB 521CB 521 INBOARD FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI 36.00.00/05 A340-200521DB 521FB 521GB 621OR521JB 621AB 621BB SSI 572061-01-1 A340-300621CB 621DB 621FB SSI 574108-01-1621GB 621JBSLATS EXTENDEDR ZL-521-01-2 521AB 521BB 521CB 521 INBOARD FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI 36.00.00/05 A340-500521DB 521EB 521FB 621OR521GB 521HB 521JB SSI 572261-01-1 A340-600621AB 621BB 621CB SSI 574158-01-1621DB 621EB 621FB621GB 621HB 621JBSLATS EXTENDEDR ZL-522-01-1 522AB 522AT 522BB 522 CENTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE A340-200522BT 522CB 522CT 622OR522EB 522HB 522JB SSI 572061-01-1 A340-300522LB 522NB 522QB522RB 522TB 522UB622AB 622AT 622BB622BT 622CB 622CT622EB 622HB 622JB622LB 622NB 622QB622RB 622TB 622UBSLATS EXTENDEDR ZL-522-01-2 522AB 522AT 522BB 522 CENTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE A340-500522BT 522CB 522CT 622OR522EB 522GB 522HB SSI 572261-01-1 A340-600522KB 522MB 522PB622AB 622AT 622BB622BT 622CB 622CT622EB 622GB 622HB* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-522-01-2 * * * * * C O N T I N U E * * * * *622KB 622MB 622PBSLATS EXTENDEDR ZL-523-01-1 523AB 523AT 523BB 523 OUTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE A340-200523BT 523CB 523CT 623OR523EB 523GB 523JB SSI NONE A340-300523LB 523NB 623AB623AT 623BB 623BT623CB 623CT 623EB623GB 623JB 623LB623NBSLATS EXTENDEDR ZL-523-01-2 523AB 523AT 523BB 523 OUTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE A340-500523BT 523CB 523DB 623OR523FB 523HB 523KB SSI NONE A340-600523MB 523PB 523QB623AB 623BB 623BT623CB 623DB 623FB623HB 623KB 623MB623PB 623QBSLATS EXTENDEDR ZL-531-01-1 531CB 532CB 533CB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 2 C MSI NONE A340-200534CB 631CB 632CB 532OR633CB 634CB 533 SSI NONE A340-300FLAPS EXTENDED 534631632633634R ZL-531-01-2 531SB 532SB 533SB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 2 C MSI NONE A340-500534SB 631SB 632SB 532OR633SB 634SB 533 SSI NONE A340-600FLAPS EXTENDED 534631632633* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-531-01-2 * * * * * C O N T I N U E * * * * *634R ZL-531-02-1 531AB 531CB 532AB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 4 C MSI 27.50.00/10 A340-200532CB 533AB 533CB 532OR534AB 534CB 631AB 533 SSI 572008-02-1 A340-300631CB 632AB 632CB 534 SSI 572021-02-1633AB 633CB 634AB 631 SSI 572021-02-2634CB 632 SSI 572111-02-1FLAPS EXTENDED 633 SSI 572606-02-1634 SSI 575015-01-1R ZL-531-02-2 531KB 531SB 532KB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 4 C MSI 27.50.00/10 A340-500532SB 533KB 533SB 532OR534KB 534SB 631KB 533 SSI 572204-01-1 A340-600631SB 632KB 632SB 534 SSI 572305-01-1633KB 633SB 634KB 631 SSI 572656-01-1634SB 632 SSI 575115-01-1FLAPS EXTENDED 633634R ZL-535-01-1 535AB 535BB 635AB 535 WING TIP (EWIS) I: 4 C MSI NONE A340-200635BB 635ORSSI NONE A340-300R ZL-535-01-2 535AB 535AT 535BB 535 WING TIP (EWIS) I: 4 C MSI NONE A340-500535CZ 635AB 635AT 635OR635BB 635CZ SSI NONE A340-600R ZL-541-01-1 541AB 541BB 541BZ 541 INNER FUEL TANK (EWIS) I: 4 C MSI NONE A340-200541CB 541CZ 641AB 641 NOTE 3OR641BB 641BZ 641CB (RIB 1 TO RIB 7) SSI 572017-02-1 A340-300641CZR ZL-541-02-1 541AB 541AZ 541BB 541 INNER FUEL TANK (EWIS) I: 8 C MSI 28.11.00/14 A340-200541BZ 541CB 541CZ 641OR541DB 541DZ 541EB (RIB 1 TO RIB 23) SSI 572018-02-1 A340-300541EZ 541FB 541FZ SSI 572019-02-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 6APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-541-02-1 * * * * * C O N T I N U E * * * * *541GB 541GZ 541HB SSI 572020-01-1541JB 541KB 541LB SSI 572026-02-1541MB 541NB 541PB SSI 572027-02-1541QB 541RB 541SB SSI 572036-02-1641AB 641AZ 641BB SSI 572037-02-1641BZ 641CB 641CZ SSI 572038-01-1641DB 641DZ 641EB SSI 572046-02-1641EZ 641FB 641FZ SSI 572047-02-1641GB 641GZ 641JB SSI 572052-02-1641KB 641LB 641MB SSI 572063-02-1641NB 641PB 641QB SSI 572064-02-1641RB 641SB 642HB SSI 572067-02-1SSI 572068-02-1SSI 572069-02-1SSI 572071-02-1SSI 572073-02-1SSI 572074-01-1SSI 572082-02-1SSI 572092-02-1SSI 572093-03-1SSI 572094-02-1SSI 572121-02-1SSI 572140-02-1SSI 572158-02-1SSI 572180-02-1R ZL-541-03-1 541AB 541AZ 541BB 541 INNER FUEL TANK NO 2/3 (EWIS) I: 8 C MSI NONE A340-500541BZ 541CZ 641AB 641OR641AZ 641BB 641BZ (RIB 1 TO RIB 6 REAR OF CENTER SPAR) SSI 572209-01-1 A340-600641CZ (RIB 1 TO RIB 11 FORWARD OF CENTER SPAR) SSI 572232-01-1SSI 572245-01-1SSI 572263-01-1SSI 572271-01-1SSI 572274-01-1SSI 572282-01-1R ZL-542-01-1 542AB 542BB 542CB 542 OUTER FUEL TANK (EWIS) I: 8 C MSI 28.11.00/14 A340-200542DB 542EB 542FB 642OR542GB 542HB 542JB (RIB 23 TO RIB 33) SSI 572122-02-1 A340-300542KB 560DB 642AB SSI 572122-02-2642BB 642CB 642DB SSI 572141-02-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 7APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-542-01-1 * * * * * C O N T I N U E * * * * *642EB 642FB 642GB SSI 572141-02-2642HB 642JB 642KB SSI 572144-02-1660DB SSI 572145-01-1SSI 572145-01-2SSI 572148-02-1SSI 572159-02-1SSI 572159-02-2SSI 572181-02-1SSI 572181-02-2SSI 572182-02-1SSI 572183-03-1R ZL-542-02-1 542AB 542AZ 542BB 542 INNER FUEL TANK 1/4 (EWIS) I: 4 C MSI NONE A340-500542BZ 542CB 542CZ 642OR542DB 542DZ 542EB (RIB 6-11 AFT OF CENTER SPAR TO RIB 23) SSI 572232-01-1 A340-600542EZ 542FB 542FZ (RIB 11-23) SSI 572233-01-1542GB 542GZ 542HB SSI 572245-01-1542JB 542KB 542LB SSI 572263-01-1542MB 542NB 542PB SSI 572271-01-1542QB 542RB 542SB SSI 572272-01-1642AB 642AZ 642BB SSI 572273-01-1642BZ 642CB 642CZ SSI 572276-01-1642DB 642DZ 642EB SSI 572277-01-1642EZ 642FB 642FZ SSI 572282-01-1642GB 642GZ 642HB SSI 572308-01-1642JB 642KB 642LB SSI 572332-01-1642MB 642NB 642PB SSI 572345-01-1642QB 642RB 642SB SSI 572365-01-1SSI 572371-01-1SSI 572373-01-1R ZL-543-01-1 543AB 543BB 543CB 543 OUTER FUEL TANK (EWIS) I: 8 C MSI NONE A340-500543DB 543EB 543FB 643OR543GB 543HB 543JB (RIB 23 TO RIB 35) SSI 572309-01-1 A340-600543KB 543LB 543MB SSI 572333-01-1543NB 543PB 543QB SSI 572334-01-1543RB 543SB 543TB SSI 572345-01-1543UB 543VB 643AB SSI 572365-01-1643BB 643CB 643DB SSI 572371-01-1643EB 643FB 643GB SSI 572372-01-1643HB 643JB 643KB SSI 572373-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 8APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-543-01-1 * * * * * C O N T I N U E * * * * *643LB 643MB 643NB643PB 643QB 643RB643SB 643TB 643UB643VBR ZL-550-01-1 550AB 550BB 550CB 550 VENT SURGE TANK (EWIS) I: 8 C MSI NONE A340-200550DB 550EB 550FB 650OR650AB 650BB 650CB (RIB 33 TO RIB 39) SSI 572122-02-1 A340-300650DB 650EB 650FB SSI 572122-02-2SSI 572141-02-1SSI 572141-02-2SSI 572182-02-1R ZL-550-02-1 550AB 550BB 550CB 550 VENT SURGE TANK RIB 35-41 (EWIS) I: 8 C MSI NONE A340-500550DB 550EB 550FB 650OR650AB 650BB 650CB GENERAL VISUAL INSPECTION OF SURGE TANK WING BOX SSI 572309-01-1 A340-600650DB 650EB 650FB RIBS 35 TO 45. SSI 572333-01-1SSI 572371-01-1R ZL-571-01-1 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI NONE A340-200671ORSSI 572041-01-1 A340-300SSI 572601-01-1SSI 572602-01-1SSI 572603-01-1SSI 572604-01-1R ZL-571-01-2 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI NONE A340-500671ORSSI NONE A340-600R ZL-572-01-1 572BB 572CB 572EB 572 SHROUD BOX (EWIS) I: 4 C MSI NONE A340-200672BB 672CB 672EB 672ORSSI NONE A340-300R ZL-572-01-2 572BB 572CB 572EB 572 SHROUD BOX (EWIS) I: 4 C MSI NONE A340-500672BB 672CB 672EB 672OR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 9APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-572-01-2 * * * * * C O N T I N U E * * * * *SSI 572651-01-1 A340-600SSI 575118-01-1SSI 575119-01-1R ZL-573-01-1 573CB 573DB 573GB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-200673CB 673DB 673GB 673ORFLAPS EXTENDED SSI 572041-01-1 A340-300SSI 572043-02-1R ZL-573-01-2 573CB 573DB 573FB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-500573GB 673CB 673DB 673OR673FB 673GB SSI NONE A340-600FLAPS EXTENDEDR ZL-574-01-1 574AT 674AT 574 CENTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-200FLAPS EXTENDED 674OR(RIB 12 TO RIB 27) SSI NONE A340-300R ZL-574-01-2 574AT 574BT 674AT 574 CENTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-500674BT 674ORFLAPS EXTENDED SSI NONE A340-600R ZL-575-01-1 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-200575BT 575CB 575DB 675OR575EB 675AB 675AT (RIB 27 TO RIB 39) SSI NONE A340-300675BB 675BT 675CB675DB 675EBR ZL-575-01-2 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE A340-500575BT 575CB 575DB 675OR575EB 675AB 675AT SSI NONE A340-600675BB 675BT 675CB675DBR ZL-591-01-1 575AB 575BB 591AB 591 INBOARD AILERON (EWIS) I: 2 C MSI NONE ALL591BB 591CB 591DB 691* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 10APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-591-01-1 * * * * * C O N T I N U E * * * * *675AB 675BB 691AB SSI NONE691BB 691CB 691DBR ZL-592-01-1 575CB 575DB 592AB 592 OUTBOARD AILERON (EWIS) I: 2 C MSI NONE ALL592BB 592CB 592DB 692675CB 675DB 692AB SSI NONE692BB 692CB 692DB* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 11APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-633-01-1 N/A TASK DELETED MSI NONESSI NONEZL-633-02-1 N/A TASK DELETED MSI NONESSI NONEZL-633-03-1 N/A TASK DELETED MSI NONESSI NONE* * * * * E N D * * * * *ISSUE: JUL 01/10 RH WING SECTION: E-600PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-700-01-1 N/A TASK DELETED MSI NONESSI NONEZL-700-01-2 N/A TASK DELETED MSI NONESSI NONER ZL-711-01-1 713 714 711 NOSE LANDING GEAR (EWIS) I: A MSI 32.30.00/13 ALLSSI NONER ZL-713-01-1 713 714 713 NOSE LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE A340-200714ORSSI 528201-01-1 A340-300SSI 528202-01-1R ZL-713-01-2 713 714 713 NOSE LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE A340-500714ORSSI 528221-01-1 A340-600SSI 528222-01-1R ZL-715-01-1 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI NONE A340-200716ORSSI 528204-01-1 A340-300R ZL-715-01-2 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI NONE A340-500716ORSSI 528224-01-1 A340-600R ZL-731-01-1 731 741 734 LH AND RH MAIN LANDING GEAR (EWIS) I: A MSI 32.11.00/08 ALL744 MSI 32.30.00/13SSI 572665-01-1R ZL-732-01-1 734 744 732 MAIN LANDING GEAR- LEG DOORS (EWIS) I: A MSI NONE A340-200742OR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-732-01-1 * * * * * C O N T I N U E * * * * *SSI 572615-02-1 A340-300R ZL-732-01-2 734 744 732 MAIN LANDING GEAR- LEG DOORS (EWIS) I: A MSI NONE A340-500742ORSSI 572665-01-1 A340-600R ZL-733-01-1 N/A 733 MAIN LANDING GEAR- HINGE DOOR (EWIS) I: A MSI NONE A340-200743ORSSI 572614-02-1 A340-300R ZL-733-01-2 N/A 733 MAIN LANDING GEAR- HINGE DOOR (EWIS) I: A MSI NONE A340-500743ORSSI 572664-01-1 A340-600R ZL-734-01-1 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE A340-200744ORSSI 528101-01-1 A340-300SSI 528102-01-1R ZL-734-01-2 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE A340-500744ORSSI 528121-01-1 A340-600SSI 528122-01-1R ZL-751-01-1 753 754 751 CENTER LINE LANDING GEAR (EWIS) I: A MSI 32.30.00/13 A340-200ORSSI NONE A340-300R ZL-751-01-2 753 754 755 751 CENTER LINE LANDING GEAR (EWIS) I: A MSI 32.30.00/13 A340-500756ORSSI NONE A340-600R ZL-753-01-1 753 754 753 CENTER LINE GEAR MAIN AND LEG DOORS (EWIS) I: A MSI NONE A340-200754ORSSI 528301-01-1 A340-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-753-01-1 * * * * * C O N T I N U E * * * * *SSI 528302-01-1R ZL-753-01-2 753 754 755 752 CENTER LINE GEAR MAIN, LEG DOORS AND MAINTENANCE DOOR I: A MSI NONE A340-500756 753 (EWIS)OR754 SSI 528321-01-1 A340-600755 SSI 528322-01-1756 SSI 528329-01-1R ZL-755-01-1 755 756 755 CENTER LINE GEAR AFT DOORS (EWIS) I: A MSI NONE A340-200756ORSSI 528304-01-1 A340-300R ZL-755-02-1 755 756 755 CENTER LINE GEAR AFT DOORS (EWIS) I: A MSI NONE A340-500756ORSSI 528324-01-1 A340-600SSI 528325-01-1SSI 528327-01-1* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-800-01-1 N/A 800 DOORS I: C MSI NONE A340-200ORSSI 521103-01-1 A340-300SSI 521201-01-1SSI 521301-01-1SSI 522201-01-1SSI 523101-01-1SSI 523201-01-1SSI 523301-01-2ZL-800-01-2 N/A 800 DOORS I: C MSI NONE A340-500SSI 521123-01-1SSI 521221-01-1SSI 521321-01-1SSI 522221-01-3SSI 523121-01-1SSI 523221-01-1SSI 523321-01-1SSI 524121-01-1ZL-800-01-3 N/A 800 DOORS I: C MSI NONE A340-600SSI 521123-01-1SSI 521221-01-1SSI 521321-01-1SSI 522121-01-1SSI 522221-01-1SSI 523121-01-1SSI 523221-01-1SSI 523321-01-1SSI 524121-01-1R ZL-811-01-1 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 52.41.11/01 A340-200ORSSI 524101-02-2 A340-300R ZL-811-01-2 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 52.41.11/01 A340-500ORSSI NONE A340-600ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 1APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-821-01-1 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 A340-200OR(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEAL; SSI 523101-01-2 A340-300DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SSI 532107-01-2SILL)R ZL-821-01-2 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 A340-500OR(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 523121-01-2 A340-600DOOR FRAMES AT FUSELAGE, DOOR SEALS AND VISIBLE PARTOF DOOR SILL)R ZL-821-02-1 132AR 132BR 132CR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE ALL132DR 132ER 132FR132GR 132HR 132JR SSI NONE132KR 132LR 821821AR 821BR 821CR821DRR ZL-821-03-1 821 821AR 821BR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI NONE ALL821CR 821DRINSULATION SSI NONER ZL-822-01-1 822 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 A340-200OR(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 523201-01-2 A340-300DOOR FRAMES AT FUSELAGE, DOOR SEALS AND VISIBLE PARTOF DOOR SILL)R ZL-822-01-2 822 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 A340-500OR(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 523221-01-2 A340-600DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOORSILL)R ZL-822-02-1 152AR 152BR 152CR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE ALL152DR 152ER 152FR152GR 152HR 152JR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) SSI NONE152KR 152LR 822* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 2APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-822-02-1 * * * * * C O N T I N U E * * * * *822AR 822BR 822CR822DRR ZL-822-03-1 822 822AR 822BR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI NONE ALL822CR 822DRINSULATION SSI NONER ZL-823-01-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.33.00/02 A340-200OR(INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE SSI 523301-01-1 A340-300FRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL)R ZL-823-01-2 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.33.00/02 A340-500PRE 49205(INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE SSI 523321-01-2 ORFRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL)PRE 49288ORA340-600PRE 49205ORPRE 49288R ZL-823-02-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE A340-200INSULATIONORSSI NONE A340-300R ZL-823-02-2 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE A340-500INSULATIONPRE 49205SSI NONE ORPRE 49288ORA340-600PRE 49205ORPRE 49288R ZL-831-01-1 831 841 831 FWD PASSENGER / CREW DOORS (EWIS) I: C MSI 52.10.00/07 ALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 3APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-831-01-1 * * * * * C O N T I N U E * * * * *841 (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI NONEAND SCUFF PLATES)R ZL-831-02-1 831 831AZ 831BZ 831 FWD PASSENGER / CREW DOOR (EWIS) I: 8 C MSI NONE ALL831CZ 831DZ 831EZ 841831FZ 831GZ 831HZ SSI NONE831JZ 841 841AZ841BZ 841CZ 841DZ841EZ 841FZ 841GZ841HZ 841JZINSULATIONR ZL-832-01-1 832 842 832 MID PASSENGER / CREW DOORS (EWIS) I: C MSI 52.10.00/07 ALL842(INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI NONEAND SCUFF PLATES)ZL-832-01-2 N/A MID PASSENGER / CREW DOOR MSI NONETASK DELETED SSI NONER ZL-832-02-1 832 832AZ 832BZ 832 MID PASSENGER / CREW DOOR (EWIS) I: 8 C MSI NONE ALL832CZ 832DZ 832EZ 842832FZ 832GZ 832HZ SSI NONE832JZ 842 842AZ842BZ 842CZ 842DZ842EZ 842FZ 842GZ842HZ 842JZINSULATIONR ZL-833-01-1 833 843 833 AFT PASSENGER / CREW DOORS (EWIS) I: C MSI 52.10.00/07 ALL843(INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI NONEAND SCUFF PLATES)ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 4APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-833-02-1 833 833AZ 833BZ 833 AFT PASSENGER / CREW DOORS (EWIS) I: 8 C MSI NONE ALL833CZ 833DZ 833EZ 843833FZ 833GZ 833HZ SSI NONE833JZ 843 843AZ843BZ 843CZ 843DZ843EZ 843FZ 843GZ843HZ 843JZINSULATIONR ZL-834-01-1 834 844 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: C MSI 52.22.00/07 ALL844(INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI NONEAND SCUFF PLATES)ZL-834-01-2 N/A EMERGENCY EXIT MSI NONETASK DELETED SSI NONER ZL-834-02-1 834 834AZ 834BZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI NONE TYPE A834CZ 834DZ 834EZ 844834FZ 834GZ 834HZ SSI NONE834JZ 844 844AZ844BZ 844CZ 844DZ844EZ 844FZ 844GZ844HZ 844JZINSULATIONR ZL-834-02-2 834 834KZ 834LZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI NONE A340-200834MZ 834NZ 834PZ 844TYPE 1834QZ 844 844KZ SSI NONE OR844LZ 844MZ 844NZA340-300844PZ 844QZTYPE 1INSULATIONR ZL-834-02-3 834 834RZ 834SZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI NONE A340-500834TZ 834UZ 834VZ 844TYPE 1844 844RZ 844SZ SSI NONE844TZ 844UZ 844VZ* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 5APPLICABILITYA340MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-834-02-3 * * * * * C O N T I N U E * * * * *INSULATIONR ZL-836-01-1 836 846 836 OVERWING EXIT (EWIS) I: C MSI NONE A340-600846TYPE III(INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS) SSI NONER ZL-836-02-1 836 836AZ 836BZ 836 OVERWING EXIT (EWIS) I: 8 C MSI NONE A340-600836CZ 836DZ 836EZ 846TYPE III836FZ 846 846AZ SSI NONE846BZ 846CZ 846DZ846EZ 846FZINSULATION* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 6

# A340 MRB REPORT

Issue: July 2010 Page: F1 SECTION F

REQUIREMENTS FOR UNITED STATES (U. S.) OPERATORS

GENERAL

This section details the requirements which must be embodied in sections A, B, C, D and E of this MRB Report to

provide all the initial maintenance requirements acceptable by the Federal Aviation Administration (FAA)

Maintenance Review Board (MRB) for the Airplane, related Engines, Appliances, Products and interfacing

Systems, for the A340 aircraft operated by U. S. certificated operators.

The tasks and their thresholds/intervals contained in this Report, together with the Certification Maintenance

Requirements and Airworthiness Limitations, form the instructions considered essential for proper maintenance

as required by certification requirements for Title 14 Code of Federal Regulations (CFR) part 25.1529 and 14

CFR part 25 Appendix H, Instructions for Continued Airworthiness (ICA).

The basic requirements outlined in this MRB Report are intended to allow each U. S. certificated operator to

develop a maintenance program that would be compatible with its own maintenance policy and requirements.

The contents of this Report will also assist the operator in the preparation of its original Operations Specifications;

further guiding the assigned FAA inspector in the approval of those Operations Specifications. This information

may be maintained in separate documents providing each document is appropriately referenced on the

Operations Specifications.

The additional requirements which must also be embodied to complete the ICA for U.S. operators are listed as

follows under the relevant section heading:

. SECTION A

1. The responsible FAA inspector shall ascertain that all of the applicable scheduled maintenance/inspection

requirements contained in this MRB Report are included in the certificated operator’s initial continuous

airworthiness maintenance program.

SECTION B

General Rules

1. Operators may not take credit for scheduled maintenance program tasks when accomplished by the flight

crew in accordance with an approved/accepted flight crew normal check list.

SECTION C

General

1 U.S. Operators should perform maintenance and inspections for the nose and main landing gear in

accordance with Appendix 11 of MRB Report, as applicable, until such time as applicable and effective

interim tasks are developed through the MSG-3 process currently in progress.

# A340 MRB REPORT

Issue: July 2010 Page: F2 2 Inspections, hydrostatic test and life limits of pressure cylinders will be accomplished as set forth in 49 CFR,

Part 173, Subpart B, Chapter 1 and all applicable vendor manuals, currently in effect. For foreign

manufactured containers, inspect, retire, and test per manufacturers technical data currently in effect.

The following additional required tasks are subject to Section C:

TASK TASK ATA CHAPTER FEC INTERVAL APPLICABILITY

REF. CODE TASK DESCRIPTION

31-33-00

Digital Flight Data Recording System

1. OPC Download and readout of DFDR data to

ensure recorded parameters meet the

range and accuracies required by

14 CFR Part 121, Appendix M. - 12 MO A340

34-52-00

ATC/MODE S (SELECT)

2. FNC Functional Check of the Air Traffic

Control Transponder System per

14 CFR Part 91.413. - 24 MO A340

SECTION D

None applicable at this time

SECTION E

None applicable at this time

# A340 MRB REPORT

Issue : July, 2010 Page : APX 1.1 APPENDIX 1

CERTIFICATION MAINTENANCE REQUIREMENTS AND AIRWORTHINESS LIMITATION ITEMS

Up until MRB Report rev 9, this Appendix served as a repository for the following documents.

Appendix 1a

A340 Certification Maintenance Requirements (CMRs)

Appendix 1b

A340 Airworthiness Limitation Items (ALIs) - (Later re-titled Damage-Tolerant ALIs)

The above documents are now located in the Airworthiness Limitations Section (ALS), which provides

those Instructions for Continuous Airworthiness that are required by FAR/JAR 25 Appendix H, paragraph

25.4. The ALS is the repository for the following stand-alone documents that are approved independently

from each other:

Part 1: Safe Life Airworthiness Limitation Items

Part 2: Damage-Tolerant Airworthiness Limitation Items

Part 3: Certification Maintenance Requirements

Part 4: Ageing Systems Maintenance

Part 5: Fuel Airworthiness Limitations

The ALS Parts were previously issued in hard copy but are now exclusively issued in digital format and

published on AirbusWorld. A CD-Rom or transmission by e-mail can be provided on request where

access to AirbusWorld is not available.

The availability of new revisions of the ALS Parts is by an email, sent by the ALS tool, to those

AirbusWorld subscribers who have chosen to receive automatic notifications.

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : APX 2. 1 APPENDIX 2

ZONE DIAGRAMS

1. The A340 aircraft is sub-divided into 8 major zones as follows :

A. Major Zones (External)

100 Lower half of fuselage to rear pressure bulkhead

200 Upper half of fuselage to rear pressure bulkhead

300 Fuselage tail section and stabilizers

400 Power Plant, Nacelles and Pylons

500 Left Wing

600 Right Wing

700 Landing Gear & Landing Gear Doors

800 Doors

B. Major Sub-Zones (Internal)

These are sub-divisions of the Major Zones, e.g. 100 is divided into 110, 120, 130,

140 etc.

C. Zones

These are sub-divisions of Major Sub-Zones, e.g. 120 is divided into 121, 122, 123, 124

etc.

Left or Right Zones

One figure indicates, where applicable, left or right hand zones, by the

use of an odd figure for left and an even figure for right, e.g.

121 left side of avionics compartment 731 left main gear

or

122 right side of avionics compartment 741 right main gear

In general odd numbers run preferentially from inboard to outboard,

front to rear in the wing ; forward to aft and away from the floor line in

the fuselage and from root to tip in the vertical stabilizer.

2. Wherever possible, physical boundaries such as frames, ribs, stringers, bulkheads etc... have

been used as the limits of each zone.

A general description of each zone and zone diagrams are provided in this appendix.

Further details are presented in the A340 Maintenance Planning Document (MPD) -

Section 10 and the Aircraft Maintenance Manual (AMM) - Chapter 06.A340 MRB REPORTIssue : July 2010Page : APX 2. 2200800(A340-600)MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 3MAJOR ZONES : A340 -200100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR)INCLUDING RADOME TOFORWARD FACE OF AFTPRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA56347200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA56347300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA56347TO FR106 - STA64998TOP OF RUDDER - STA65772ELEVATOR - STA65803400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSMAJOR ZONES : A340 -300100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR)INCLUDING RADOME TOFORWARD FACE OF AFTPRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA60614200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA60614300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA60614TO FR106 - STA69265TOP OF RUDDER - STA70040ELEVATOR - STA70070400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSMAJOR ZONES : A340 -500100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR)INCLUDING RADOME TOFORWARD FACE OF AFTPRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA64327200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA64327300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA64327TO FR100 - STA71772TOP OF RUDDER - STA71772ELEVATOR - STA71772400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSMAJOR ZONES : A340 -600100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR)INCLUDING RADOME TOFORWARD FACE OF AFTPRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA71760200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA71760300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA71760TO FR100 - STA79205TOP OF RUDDER - STA79205ELEVATOR - STA79205400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSA340 MRB REPORTIssue : July 2010Page : APX 2. 4A340 MRB REPORTIssue : July 2010Page : APX 2. 5A340-200/300A340 MRB REPORTIssue : July 2010Page : APX 2. 6A340 MRB REPORTIssue : July 2010Page : APX 2. 7MAJOR SUB ZONES A340-300110 RADOME (NOSE CONE TO FR 1)- STA6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA30372,1140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA30372,1TO FR53,2 - STA39930,9150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA39930,9TO BETWEEN FR65 - STA52134,5AND FR66 - STA52664,5160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR65 - STA52134,5AND FR66 - STA52664,5TO FR73 - STA53674,5170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA56374,4TO FR80/82 - STA60614,5190 BELLY FAIRING, AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR37,2 - STA26651,9AND FR37,3 - STA27185,3TO FR57,2 - STA46824,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5MAJOR SUB ZONES A340-200110 RADOME (NOSE CONE TO FR 1)- STA6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA28247,5140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA28247,5TO FR53,2 - STA37797,3150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA37797,3TO BETWEEN FR65 - STA47867,3AND FR66 - STA48397,3160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA52107,3TO FR80/82 - STA56347,3190 BELLY FAIRING, AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR33 - STA23468,5AND FR34 - STA23998,5TO FR56 - STA43097,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5MAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 8MAJOR SUB ZONES A340-300230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR31 - STA22408,5240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR31 - STA22408,5TO FR36 - STA25058,5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR36 - STA25058,5TO FR53,5 - STA39387,3260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR53,5 - STA39387,3TO FR72 - STA51577,3270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA51577,3TO FR80/82 - STA56347,3310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA56347,3TO FR106 - STA64998,3320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER, L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS750 CENTERLINE GEAR AND DOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSMAJOR SUB ZONES A340-200230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR31 - STA22408,5240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR31 - STA22408,5TO FR36 - STA25058,5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR36 - STA25058,5TO FR53,5 - STA41520,9260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR53,5 - STA41520,9TO FR72 - STA55844,5270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA55844,5TO FR80/82 - STA60614,5310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA60614,5TO FR106 - STA69265,5320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER, L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS750 CENTERLINE GEAR AND DOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 9MAJOR SUB ZONES A340-500110 RADOME (NOSE CONE TO FR 1)- STA6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA30372,1140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA30372,1TO FR53,2 - STA39930,9150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA39930,9TO BETWEEN FR65 - STA52134,5AND FR66 - STA52664,5160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR65 - STA52134,5AND FR66 - STA52664,5TO FR73 - STA53674,5170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA56374,4TO FR80/82 - STA60614,5190 BELLY FAIRING, AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR37,2 - STA26651,9AND FR37,3 - STA27185,3TO FR57,2 - STA46824,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5MAJOR SUB ZONES A340-600110 RADOME (NOSE CONE TO FR 1)- STA6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA28247,5140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA28247,5TO FR53,2 - STA37797,3150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA37797,3TO BETWEEN FR65 - STA47867,3AND FR66 - STA48397,3160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA52107,3TO FR80/82 - STA56347,3190 BELLY FAIRING, AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR33 - STA23468,5AND FR34 - STA23998,5TO FR56 - STA43097,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5MAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 10MAJOR SUB ZONES A340-500230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR37.7 - STA23998,5240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR37.7 - STA23998,5TO FR37.11 - STA26118.5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR37.11 - STA23998,5TO FR53,4 - STA43110.9260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR53,4 - STA43110.9TO FR72 - STA59031.3270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA59031,3TO FR80/82 - STA64327.3310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA64327.3TO FR100 - STA717723320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER, L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS750 CENTERLINE GEAR AND DOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSMAJOR SUB ZONES A340-600230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR37.7 - STA29298.5240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR37.7 - STA29398,5TO FR37.11 - STA26118,5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR37.11 - STA226118,5TO FR56.1 - STA53187,1260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR56,1 - STA53187,1TO FR72 - STA66464,9270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA66464,9TO FR80/82 - STA71760,9310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA71760,9TO FR100 - STA79205,6320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER, L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS750 CENTERLINE GEAR AND DOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 11A340-200/-300A340-500-600MAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 12MAJOR SUB ZONES A340-300410 ENGINE 1 (LEFT OUTBOARDENGINE), ENGINE AIR INTAKE, FANAND ACCESSORY GEAR BOX,THRUST REVERSER, EXHAUSTNOZZLE AND COWLS420 ENGINE 2 (LEFT INBOARD ENGINE)ENGINE AIR INTAKE, FAN ANDACCESSORY GEAR BOX, THRUSTREVERSER, EXHAUST NOZZLEAND COWLS450 ENGINE 1 PYLON460 ENGINE 2 PYLON510 SLATS520 FIXED LEADING EDGE530 FLAP TRACK FAIRINGS AND WINGTIP540 FUEL TANKRIB1 - STA0TO RIB33 - STA21905550 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566570 AFT SECTION OF WING ANDTRAILING EDGE FIXEDSTRUCTURE580 FLAPS AND SPOILERS590 AFT OUTBOARD SECTION OFWING TRAILING EDGEMAJOR SUB ZONES A340-200430 ENGINE 3 (RIGHT INBOARDENGINE), ENGINE AIR INTAKE, FANAND ACCESSORY GEAR BOX,THRUST REVERSER, EXHAUSTNOZZLE AND COWLS440 ENGINE 4 (RIGHT OUTBOARDENGINE) ENGINE AIR INTAKE, FANAND ACCESSORY GEAR BOX,THRUST REVERSER, EXHAUSTNOZZLE AND COWLS470 ENGINE 3 PYLON480 ENGINE 4 PYLON610 SLATS620 FIXED LEADING EDGE630 FLAP TRACK FAIRINGS AND WINGTIP640 FUEL TANKRIB1 - STA0TO RIB33 - STA21905650 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566670 AFT SECTION OF WING ANDTRAILING EDGE FIXEDSTRUCTURE680 FLAPS AND SPOILERS690 AFT OUTBOARD SECTION OFWING TRAILING EDGEMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESMAJORSUBZONESDESCRIPTION/BOUNDARIESMAJORSUBZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 13MAJOR SUB ZONES A340-500/600410 ENGINE 1 (LEFT OUTBOARDENGINE), ENGINE AIR INTAKE, FANAND ACCESSORY GEAR BOX,THRUST REVERSER, EXHAUSTNOZZLE AND COWLS420 ENGINE 2 (LEFT INBOARD ENGINE)ENGINE AIR INTAKE, FAN ANDACCESSORY GEAR BOX, THRUSTREVERSER, EXHAUST NOZZLEAND COWLS450 ENGINE 1 PYLON460 ENGINE 2 PYLON510 SLATS520 FIXED LEADING EDGE530 FLAP TRACK FAIRINGS AND WINGTIP540 FUEL TANKRIB1 - STA0TO RIB35 - STA27826550 VENT SURGE TANKRIB35 - STA27826TO RIB41 - STA32358570 AFT SECTION OF WING ANDTRAILING EDGE FIXEDSTRUCTURE580 FLAPS AND SPOILERS590 AFT OUTBOARD SECTION OFWING TRAILING EDGEA340 MRB REPORTIssue : July 2010Page : APX 2. 14A340-200/-300A340 MRB REPORTIssue : July 2010Page : APX 2. 15Sub zones A340-200121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR20 - ST14448,5TO FR39,1 - STA27178,5AND FR39,2 - STA27708,5133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14458,5TO FR39,1 - STA27178,5AND FR39,1 - STA27708,5137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGOCOMPARTMENT TO FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX : FROM LOWER SIDEOF PAX COMPARTMENT FLOORTO BOTTOM CENTER LINE (STR26L/R)FR39,1 - STA27178,5AND FR39,2 - STA27708,5TO FR39 - STA26648,5AND FR40 - STA28245,5141/142 WING CENTER BOXFR40 - STA28245,5AND FR47 - STA33538,5143 AREA BETWEEN KEEL BEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGEBETWEEN FR44 AND FR45STA 32042,6TO FR49 STA 34603,2145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX, MAIN GEARWELL AND CABIN FLOORFR40 - STA28247,5TO FR53,2 - STA37797,3147/148 MAIN GEAR WELL ANDHYDRAULIC COMPARTMENTFR47 - STA33538,5TO FR53,2 - STA37797,3149 CENTERLINE GEAR WELLBETWEEN KEEL BEAMS UNDERZONE 143BETWEEN FR44 AND FR45STA 32042,6TO FR49 STA 34603,2AND BETWEEN KEEL BEAMSFR49 STA 34603,2TO FR53,2 STA 37797,3Sub zones A340- 300121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR20 - ST14448,5TO FR39,1 - STA29312,1AND FR39,2 - STA28842,1133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14458,5TO FR39,1 - STA29312,1AND FR39,1 - STA29842,1137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGOCOMPARTMENT TO FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX : FROM LOWER SIDEOF PAX COMPARTMENT FLOORTO BOTTOM CENTER LINE (STR26L/R)FR39,1 - STA29312,1AND FR39,2 - STA29842,1TO FR39 - STA28782,1AND FR40 - STA30372,1141/142 WING CENTER BOXFR40 - STA30372,1AND FR47 - STA35672,1143 AREA BETWEEN KEEL BEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGEBETWEEN FR44 AND FR45STA 34176,2TO FR49 STA 36736,8145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX, MAIN GEARWELL AND CABIN FLOORFR40 - STA30372,1TO FR53,2 - STA39930,9147/148 MAIN GEAR WELL ANDHYDRAULIC COMPARTMENTFR47 - STA35672,1TO FR53,2 - STA39930,9149 CENTERLINE GEAR WELLBETWEEN KEEL BEAMS UNDERZONE 143BETWEEN FR44 AND FR45STA 34176,2TO FR49 STA 36736,8AND BETWEEN KEEL BEAMSFR49 STA 36136,8TO FR53,2 STA 339930,9SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 16Sub zones A340-200151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 INCYLINDRICAL SECTION)FR53,2 - STA37797,3TO FR65 - STA47867,3AND FR66 - STA48397,3153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/RIN CYLINDRICAL SECTION)FR53,2 - STA37797,3TO FR65 - STA47867,3AND FR66 - STA48397,3161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA52107,3TO FR80 - STA56347,3191 DRY BAY AND FAIRINGS :BETWEEN FR31 AND FR37,1STA23681,5 TO BETWEEN FR44AND FR45 STA32042,6192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37 AND FR37,1STA23681,5 TO BETWEEN F44 ANDFR45 STA32042,6193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR40 STA28247,51BETWEEN FR44 AND FR45STA32042,6195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS :BETWEEN FR44 AND FR45STA32042,6 TO FR47 STA33538,5197/198 REAR FAIRINGS :FR53,2 STA37797,3TO FR56 STA43097,3Sub zones A340-300151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 INCYLINDRICAL SECTION)FR53,2 - STA39930,9TO FR65 - STA52134,5AND FR66 - STA52664,5153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/RIN CYLINDRICAL SECTION)FR53,2 - STA39930,9TO FR65 - STA52134,5AND FR66 - STA52664,5161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR65 - STA52134,5AND FR66 - STA52664,5TO FR73 - STA56374,5163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA52134,5AND FR66 - STA52664,5TO FR73 - STA56374,5171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA56374,5TO FR80 - STA60614,5191 DRY BAY AND FAIRINGS :BETWEEN FR31 AND FR37,1STA25815,1 TO BETWEEN FR44AND FR45 STA34176,2192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37 AND FR37,1STA25815,1 TO BETWEEN F44 ANDFR45 STA34176,2193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR40 STA30381,1BETWEEN FR44 AND FR45STA34176,2195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS :BETWEEN FR44 AND FR45STA34176,2 TO FR47 STA35672,1197/198 REAR FAIRINGS :FR53,2 STA39930,9TO FR56 STA45240,9SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 17Sub zones A340-200211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR31 - STA22408,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR31 - STA22408,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR31 - STA22408,5TO FR36 - STA25058,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENTFROM CROWN CENTER LINE TOSTR15 L/RFR31 - STA22408,5TO FR36 - STA25058,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)FR39.6 - STA25056,5TO FR53,5 - STA39387,3253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR36 - STA25058,5TO FR53,5 - STA39387,3261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR53,5 - STA39387,3TO FR72 - STA51577,3Sub zones A340-300211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR31 - STA22408,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR31 - STA22408,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR31 - STA22408,5TO FR36 - STA25058,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENTFROM CROWN CENTER LINE TOSTR15 L/RFR31 - STA22408,5TO FR36 - STA25058,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)Frr396 - STA25056,5TO FR53,5 - STA41520,9253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR36 - STA25058,5TO FR53,5 - STA41520,9261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR53,5 - STA41520,9TO FR72 - STA55844,5SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 18Sub zones A340-200263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR53,5 - STA39387,3TO FR72 - STA51577,3271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION )FR72 - STA51577,3TO FR80 - STA56347,3273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA51577,3TO FR80 - STA56347,3311/312 REAR FUSELAGE SECTIONFR80/82 - STA56347,3TO BETWEEN FR91/92 STA60851,3313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA60851,3TO FR95 - STA61779,3315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR95 - STA61779,3TO FR101 - STA63664,3317 TAIL CONE APU EXHAUST AREAFR101 - STA63664,3TO FR106 - STA64998,3321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERSub zones A340-300263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR53,5 - STA41520,9TO FR72 - STA55844,5271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION )FR72 - STA55844,5TO FR80 - STA60614,5273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA55844,5TO FR80 - STA60614,5311/312 REAR FUSELAGE SECTIONFR80/82 - STA60614,5TO BETWEEN FR91/92 STA65118,5313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA65118,5TO FR95 - STA66046,5315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR95 - STA66046,5TO FR101 - STA67931,5317 TAIL CONE APU EXHAUST AREAFR101 - STA67931,5TO FR106 - STA69265,5321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERA340 MRB REPORTIssue : July 2010Page : APX 2. 19A340-500155A340 MRB REPORTIssue : July 2010Page : APX 2. 20A340-600251252836846SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 21Sub zones A340-500121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR20 - ST14448,5TO FR39,1 - STA29301,9AND FR39,2 - STA30361,9133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - ST14448,5TO FR39,1 - STA29301,9AND FR39,2 - STA30361,9137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGOCOMPARTMENT TO FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX : FROM LOWER SIDEOF PAX COMPARTMENT FLOORTO BOTTOM CENTER LINE(STR26 L/R)FR39,1 - STA29301,9AND FR39,2 - STA30361,9TO FR39 - STA29301,9AND FR40 - STA36191,9141/142 WING CENTER BOXFR40 - STA30891,9AND FR47 - STA37796,1143 AREA BETWEEN KEEL BEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGEBETWEEN FR44 AND FR45STA 36202,1TO FR49 STA 38856,2145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX, MAIN GEARWELL AND CABIN FLOORFR40 - STA30891,9TO FR53,2 - STA42050,9147/148 MAIN GEAR WELL ANDHYDRAULIC COMPARTMENTFR47 - STA37796,1TO FR53,2 STA42050,9149 CENTERLINE GEAR WELLBETWEEN KEEL BEAMS UNDERZONE 143BETWEEN FR44 AND FR45STA 36732,1TO FR49 STA 38856,8AND BETWEEN KEEL BEAMSFR49 - STA 38856,8TO FR53,2 - STA 4250,9Sub zones A340- 600121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR20 - ST14448,5TO FR39,1 - STA35131,9AND FR39,2 - STA35661,9133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - ST14448,5TO FR39,1 - STA35131,9AND FR39,2 - STA35661,9137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGOCOMPARTMENT TO FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX : FROM LOWER SIDEOF PAX COMPARTMENT FLOORTO BOTTOM CENTER LINE(STR26 L/R)FR39,1 - STA35131,9AND FR39,2 - STA35661,9TO FR39 - STA34601,9AND FR40 - STA36191,9141/142 WING CENTER BOXFR40 - STA36191,9AND FR47 - STA43096,1143 AREA BETWEEN KEEL BEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGEBETWEEN FR44 AND FR45STA 41502.1TO FR49 STA 44156,8145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX, MAIN GEARWELL AND CABIN FLOORFR40 - STA36191,9TO FR53,2 - STA47350,9147/148 MAIN GEAR WELL ANDHYDRAULIC COMPARTMENTFR47 - STA43096,1TO FR53,2 STA47350,9149 CENTERLINE GEAR WELLBETWEEN KEEL BEAMS UNDERZONE 143BETWEEN FR44 AND FR45STA 41502,1TO FR49 STA 44156,8AND BETWEEN KEEL BEAMSFR49 - STA 44156,8TO FR53,2 - STA 47350,9SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 22Sub zones A340-500151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 INCYLINDRICAL SECTION)FR53,7 - STA44370,9TO FR65 - STA55321,3AND FR66 - STA55851,3153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/RIN CYLINDRICAL SECTION)FR53,7 - STA44370,9TO FR65 - STA55321,3AND FR66 - STA55851,3155 REAR CENTER TANKFR 53.2 -STA42050.9FR 53.7 -STA44700.9ORFR53.9 -STA45760.9161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR65 - STA44370,9AND FR66 - STA55851,3TO FR73 - STA59561,3163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA44370,9AND FR66 - STA55851,3TO FR73 - STA59561,3171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA59561,3TO FR80 - STA63197,3191 DRY BAY AND FAIRINGS :BETWEEN FR37.11 AND FR40.1STA26118.5 TO STA31421.3192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37.11 TO F44STA26118.5 TO STA 36202.5193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR37.13 TO FR44STA27178.5 TO STA 36202,5195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS :BETWEEN FR40.1 AND FR47TO STA31421.3 TO STA37796.1197/198 REAR FAIRINGS :FR44 STA36202.1TO FR47 STA37796.1SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 23Sub zones A340-600151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 INCYLINDRICAL SECTION)FR53,2 - STA47350,9TO FR65 - STA62754,9AND FR66 - STA63284,3153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/RIN CYLINDRICAL SECTION)FR53,2 - STA47350,9TO FR65 - STA62754,9AND FR66 - STA63284,3161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OFCARGO COMPARTMENT FLOOR(STR26 L/R TO STR41 L/R INCYLINDRICAL SECTION)FR65 - STA62754,9AND FR66 - STA63284,9TO FR73 - STA66994,9163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA62754,9AND FR66 - STA63284,9TO FR73 - STA66994,9171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA66994,9TO FR80 - STA71234,9191 DRY BAY AND FAIRINGS :BETWEEN FR37.11 TO 40.1STA31416.5 TO STA 36721.9192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37 AND FR37,11TO FR44 STA31416.1 TOSTA 36721.9193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR37.13 STA32476.5 TO FR44STA41502.1195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS :BETWEEN FR40.1 AND FR47STA36721.1 TO FR4743624.1197/198 REAR FAIRINGS :FR53,2 STA47350.9TO FR56.2 STA53717.1SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 24Sub zones A340-500211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR37.7 - STA23998,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR37.7 - STA23998,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR37.7 - STA23998,5TO FR37.11 - STA26118,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENTFROM CROWN CENTER LINE TOSTR15 L/RFR37.7 - STA23998,5TO FR37.11 - STA26118,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)FR37.11 - STA26118,5TO FR53,4 - STA43110,9253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR37.11 - STA26118,5TO FR53,4 - STA43110,9261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR53,4 - STA43110,9TO FR72 - STA59031.3Sub zones A340-600211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR37.7 - STA29298,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR37.7 - STA29298,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR37.7 - STA29298,5TO FR37.11 - STA31416,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENTFROM CROWN CENTER LINE TOSTR15 L/RFR37.7 - STA29298,5TO FR37.11 - STA31416,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)FR37.11 - STA31416,5TO FR56.1 - STA53187,7253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR37.11 - STA31416,5TO FR56.1 - STA53187,7261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION)FR56,1 - STA53187,7TO FR72 - STA66464,9SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 25Sub zones A340-500263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR53,4 - STA43110,9TO FR72 - STA59031.3271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION )FR72 - STA59031.3TO FR80 - STA63801.3273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA59031.3TO FR80 - STA63801.3311/312 REAR FUSELAGE SECTIONFR80/82 - STA63197,3TO BETWEEN FR91/92 STA68233.3313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA68233.3TO FR94 - STA69223.3315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR94 - STA69223.3TO FR98 - STA71323,3317 TAIL CONE APU EXHAUST AREAFR98 - STA71323,3TO FR100 - STA72220.7321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERSub zones A340-600263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR56,1 - STA53187,7TO FR72 - STA66464,9271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26L/R IN CYLINDRICAL SECTION )FR72 - STA66464.9TO FR80 - STA71234.3273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA66464.9TO FR80 - STA71234.3311/312 REAR FUSELAGE SECTIONFR80/82 - STA71234,3TO BETWEEN FR91/92 STA75666.9313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA75666.3TO FR94 - STA76666.9315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR94 - STA76666.9TO FR98 - STA78756.9317 TAIL CONE APU EXHAUST AREAFR98 - STA78756.9TO FR100 - STA72220.7321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERA340 MRB REPORTIssue : July 2010Page : APX 2. 26A340-200/-300SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 27CFM ENGINE 1 (L OUTBOARD)411 ENGINE AIR INTAKE AND AIRINTAKE LIP412 FAN AND ACCESSORY GEAR BOX415 L FAN COWL416 R FAN COWL417 L THRUST REVERSER418 R THRUST REVERSER413 HOT SECTION414 EXHAUST NOZZLE451 PYLON LEADING EDGE452 UPPER FWD PYLON453 LOWER PYLON454 LOWER AND REAR PYLONFAIRINGSCFM ENGINE 2 (L INBOARD)421 ENGINE AIR INTAKE AND AIRINTAKE LIP422 FAN AND ACCESSORY GEAR BOX425 L FAN COWL426 R FAN COWL427 L THRUST REVERSER428 R THRUST REVERSER423 HOT SECTION424 EXHAUST NOZZLE461 PYLON LEADING EDGE462 UPPER FWD PYLON463 LOWER PYLON464 LOWER AND REAR PYLONFAIRINGSCFM ENGINE 3 (R INBOARD)431 ENGINE AIR INTAKE AND AIRINTAKE LIP432 FAN AND ACCESSORY GEAR BOX435 L FAN COWL436 R FAN COWL437 L THRUST REVERSER438 R THRUST REVERSER433 HOT SECTION434 EXHAUST NOZZLE471 PYLON LEADING EDGE472 UPPER FWD PYLON473 LOWER PYLON474 LOWER AND REAR PYLONFAIRINGSCFM ENGINE 4 (R OUTBOARD)441 ENGINE AIR INTAKE AND AIRINTAKE LIP442 FAN AND ACCESSORY GEAR BOX445 L FAN COWL446 R FAN COWL447 L THRUST REVERSER448 R THRUST REVERSER443 HOT SECTION444 EXHAUST NOZZLE481 PYLON LEADING EDGE482 UPPER FWD PYLON483 LOWER PYLON484 LOWER AND REAR PYLONFAIRINGSA340 MRB REPORTIssue : July 2010Page : APX 2. 28431441432442435/436445/446433433437/438447/448434444439449471481472482473483474484411421412422415/416425/426413423417/418427/428414424419429451461452462453463454464A340-500/600 PYLONS AND ENGINES 1 AND 2A340-500/600 PYLONS AND ENGINES 3 AND 4SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 29A340-500/600RR- ENGINE 1 (L OUTBOARD)411 ENGINE AIR INTAKE AND AIRINTAKE LIP412 FAN AND ACCESSORY GEAR BOX415 L FAN COWL416 R FAN COWL417 L THRUST REVERSER418 R THRUST REVERSER419 EXHAUST PLUG413 HOT SECTION414 EXHAUST NOZZLE451 PYLON LEADING EDGE452 UPPER FWD PYLON453 LOWER PYLON454 LOWER AND REAR PYLONFAIRINGSA340-500/600RR- ENGINE 2 (L INBOARD)421 ENGINE AIR INTAKE AND AIRINTAKE LIP422 FAN AND ACCESSORY GEAR BOX425 L FAN COWL426 R FAN COWL427 L THRUST REVERSER428 R THRUST REVERSER429 EXHAUST PLUG423 HOT SECTION424 EXHAUST NOZZLE461 PYLON LEADING EDGE462 UPPER FWD PYLON463 LOWER PYLON465 LOWER AND REAR PYLONFAIRINGSA340-500/600RR-ENGINE 3 (R INBOARD)431 ENGINE AIR INTAKE AND AIRINTAKE LIP432 FAN AND ACCESSORY GEAR BOX435 L FAN COWL436 R FAN COWL437 L THRUST REVERSER438 R THRUST REVERSER439 EXHAUST PLUG433 HOT SECTION434 EXHAUST NOZZLE471 PYLON LEADING EDGE472 UPPER FWD PYLON473 LOWER PYLON474 LOWER AND REAR PYLONFAIRINGSA340-500/600RR ENGINE 4 (R OUTBOARD)441 ENGINE AIR INTAKE AND AIRINTAKE LIP442 FAN AND ACCESSORY GEAR BOX445 L FAN COWL446 R FAN COWL447 L THRUST REVERSER448 R THRUST REVERSER449 EXHAUST PLUG443 HOT SECTION444 EXHAUST NOZZLE481 PYLON LEADING EDGE482 UPPER FWD PYLON483 LOWER PYLON484 LOWER AND REAR PYLONFAIRINGSSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 30TRIMMABLE HORIZONTALSTABILIZER CENTER SPAR BOXFUEL TANKHORIZONTAL TAIL (LH)331 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE332 TRIMMABLE HORIZONTALSTABILIZER TIP333 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX334 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE335 ELEVATOR337 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB19 TO RIB21HORIZONTAL TAIL (RH)341 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE342 TRIMMABLE HORIZONTALSTABILIZER EDGE343 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX344 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE345 ELEVATOR346 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX VENT TANK347 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB20 TO RIB21A340-200/300SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 31TRIMMABLE HORIZONTALSTABILIZER CENTER SPAR BOXFUEL TANKHORIZONTAL TAIL (LH)331 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE332 TRIMMABLE HORIZONTALSTABILIZER TIP333 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX334 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE335 ELEVATOR337 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB19 TO RIB21HORIZONTAL TAIL (RH)341 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE342 TRIMMABLE HORIZONTALSTABILIZER EDGE343 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX344 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE345 ELEVATOR346 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX VENT TANK347 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB20 TO RIB21A340-500/600Horizontal tail unit zones , left and right sidesA340 MRB REPORTIssue : July 2010Page : APX 2. 32A340-200/300SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 33A340-200/300511 SLAT 1512 SLAT 2513 SLAT 3514 SLAT 4515 SLAT 5516 SLAT 6517 SLAT 7521 INBOARD FIXED LEADING EDGESTRUCTURERIB 1 - STA0TO RIB9 - STA5676522 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA5676TO RIB24 - STA16009523 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA16009TO RIB39 - STA25566531 FLAP TRACK 2 FAIRING532 FLAP TRACK 3 FAIRING533 FLAP TRACK 4 FAIRING534 FLAP TRACK 5 FAIRING535 WING TIP541 INNER TANKRIB1 - STA0TO RIB23 - STA15298542 OUTER TANKRIB23 - STA15298TO RIB33 - STA21905550 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566562 PLASTRON FAIRING571 MLG WELL572 SHROUD BOX573 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12574 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27575 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB39581 INBOARD FLAP 1582 SPOILER 1583 OUTBOARD FLAP 2584 SPOILER 2585 SPOILER 3586 SPOILER 4587 SPOILER 5588 SPOILER 6591 INBOARD AILERON592 OUTBOARD AILERONSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 34A340-200/300611 SLAT 1612 SLAT 2613 SLAT 3614 SLAT 4615 SLAT 5616 SLAT 6617 SLAT 7621 INBOARD FIXED LEADING EDGESTRUCTURERIB 1 - STA0TO RIB9 - STA5676622 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA5676TO RIB24 - STA16009623 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA16009TO RIB39 - STA25566631 FLAP TRACK 2 FAIRING632 FLAP TRACK 3 FAIRING633 FLAP TRACK 4 FAIRING634 FLAP TRACK 5 FAIRING635 WING TIP641 INNER TANKRIB1 - STA0TO RIB23 - STA15298642 OUTER TANKRIB23 - STA15298TO RIB33 - STA21905650 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566662 PLASTRON FAIRING671 MLG WELL672 SHROUD BOX673 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12674 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27675 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB39681 INBOARD FLAP 1682 SPOILER 1683 OUTBOARD FLAP 2684 SPOILER 2685 SPOILER 3686 SPOILER 4687 SPOILER 5688 SPOILER 6691 INBOARD AILERON692 OUTBOARD AILERONA340 MRB REPORTIssue : July 2010Page : APX 2. 35A340-500/600SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 36A340-500/600511 SLAT 1512 SLAT 2513 SLAT 3514 SLAT 4515 SLAT 5516 SLAT 6517 SLAT 7521 INBOARD FIXED LEADING EDGESTRUCTURERIB 1 - STA0TO RIB9 - STA6778522 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA6778TO RIB24 - STA19156523 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA19156TO RIB41 - STA32358531 FLAP TRACK 2 FAIRING532 FLAP TRACK 3 FAIRING533 FLAP TRACK 4 FAIRING534 FLAP TRACK 5 FAIRING535 WING TIP541 INNER TANKRIB1 - STA0TO RIB 6 - STA4375TO RIB 11 - STA 9092542 OUTER TANKRIB23 - STA18492TO RIB35 - STA27826550 VENT SURGE TANKRIB35 - STA27826TO RIB41 - STA32358571 MLG WELL572 SHROUD BOX573 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12574 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27575 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB41581 INBOARD FLAP 1582 SPOILER 1583 OUTBOARD FLAP 2584 SPOILER 2585 SPOILER 3586 SPOILER 4587 SPOILER 5588 SPOILER 6591 INBOARD AILERON592 OUTBOARD AILERONSPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 37A340-500/600611 SLAT 1612 SLAT 2613 SLAT 3614 SLAT 4615 SLAT 5616 SLAT 6617 SLAT 7621 INBOARD FIXED LEADING EDGESTRUCTURERIB 1 - STA0TO RIB9 - STA5676622 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA5676TO RIB24 - STA16009623 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA16009TO RIB39 - STA25566631 FLAP TRACK 2 FAIRING632 FLAP TRACK 3 FAIRING633 FLAP TRACK 4 FAIRING634 FLAP TRACK 5 FAIRING635 WING TIP641 INNER TANKRIB1 - STA0TO RIB23 - STA15298642 OUTER TANKRIB23 - STA15298TO RIB33 - STA21905650 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566662 PLASTRON FAIRING671 MLG WELL672 SHROUD BOX673 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12674 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27SPECIFZONESDESCRIPTION/BOUNDARIESSPECIFZONESSPECIFZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 38675 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB39681 INBOARD FLAP 1682 SPOILER 1683 OUTBOARD FLAP 2684 SPOILER 2685 SPOILER 3686 SPOILER 4687 SPOILER 5688 SPOILER 6691 INBOARD AILERON692 OUTBOARD AILERONSPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 39NOSE LANDING GEAR711 NOSE GEAR712 LEG DOOR713/174 MAIN DOORS715/716 AFT DOORSMAIN LANDING GEAR (LH)731 L MAIN GEAR732 MLG - LEGDOOR733 MLG -HINGE DOOR734 MLG - MAIN DOORMAIN LANDING GEAR (RH)741 R MAIN GEAR742 MLG- LEG DOOR743 MLG –HINGE DOOR744 MLG- MAIN DOORCENTERLINE LANDING GEAR751 CENTERLINE GEAR752 LEG DOOR753/754 CLG -MAIN DOORS755/756 CLG- AFT DOORSLanding GearSPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 40A340-200/300811 FORWARD AVIONICSCOMPARTMENT DOOR FR7 ANDFR8 TO FR9 AND FR10821 LOWER DECK FORWARD CARGOCOMPARTMENT DOOR BETWEENFR20A AND FR25A822 LOWER DECK AFT CARGOCOMPARTMENT DOOR BETWEENFR59A AND FR65823 LOWER DECK BULK CARGOCOMPARTMENT DOOR BETWEENFR67 AND FR69831 L FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A832 L MID PASSENGER/CREW DOORBETWEEN FR33 TO FR35A833 L AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A834 L EMERGENCY EXIT BETWEENFR53,5 TO FR53,7 AND FR53,8841 R FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A842 R MID PASSENGER/CREW DOORBETWEEN FR33 TO FR35A843 R AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A844 R EMERGENCY EXIT BETWEENFR53,5 TO FR53,7ASPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 41A340-500811 FORWARD AVIONICSCOMPARTMENT DOOR FR7 ANDFR8 TO FR9 AND FR10821 LOWER DECK FORWARD CARGOCOMPARTMENT DOOR BETWEENFR20A AND FR25A822 LOWER DECK AFT CARGOCOMPARTMENT DOOR BETWEENFR59A AND FR65823 LOWER DECK BULK CARGOCOMPARTMENT DOOR BETWEENFR67 AND FR69831 L FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A832 L MID PASSENGER/CREW DOORBETWEEN FR37.7A TO FR37.9A833 L AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A834 L EMERGENCY EXIT BETWEENFR53,5 TO FR53,7 AND FR53,8841 R FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A842 R MID PASSENGER/CREW DOORBETWEEN FR37.7A TO FR37.9A843 R AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A844 R EMERGENCY EXIT BETWEENFR53,5 TO FR53,7ASPECIFZONESDESCRIPTION/BOUNDARIESA340 MRB REPORTIssue : July 2010Page : APX 2. 42811A340-600811 FORWARD AVIONICSCOMPARTMENT DOOR FR7 ANDFR8 TO FR9 AND FR10821 LOWER DECK FORWARD CARGOCOMPARTMENT DOOR BETWEENFR20A AND FR25A822 LOWER DECK AFT CARGOCOMPARTMENT DOOR BETWEENFR59A AND FR65823 LOWER DECK BULK CARGOCOMPARTMENT DOOR BETWEENFR67 AND FR69831 L FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A832 L MID PASSENGER/CREW DOORBETWEEN FR37.7A TO FR37.9A833 L AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A834 L EMERGENCY EXIT BETWEENFR56.1A TO FR56.3A836 OVERWING EXIT DOORFR41A TO FR42A841 R FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A842 R MID PASSENGER/CREW DOORBETWEEN FR37.7 TO FR37.10843 R AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A844 R EMERGENCY EXIT BETWEENFR56.1A TO FR56.3A846 OVERWING EXIT DOORFR41A TO FR42A846836836846

# A340 MRB REPORT

Issue : July 2010 Page : APX 3. 1 APPENDIX 3

Not applicable to the A340 aircraft

NB: In the A330 MRB Report, this appendix identifies ETOPS Maintenance Standards.

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : APX 4.1 APPENDIX 4

SSI’s WITHOUT REQUIREMENTS

DELETED

Appendix 4 deleted in MRB Report Rev7 following ISC/MWG decision that information was of no

practical value

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.1 APPENDIX 5

ADMINISTRATION - COMPOSITION OF WORKING BODIES

Note : This report has been developed through a

joint A330/A340 process by the following

working bodies

A330/A340 MAINTENANCE REVIEW BOARD (Feb 90 to Dec 94)

JAA MEMBERS

J. HEURLIN DGAC (Chairman) Feb 90 to Sep 94

D. LEWIS CAA Feb 90 to Dec 92

T. CROW CAA Sep 92 to Dec 94

Th. H. de GROOT RLD Feb 90 to Dec 94

H. PRUIS RLD Feb 90 to Dec 94

W. SCHULZE-MARMELING LBA Feb 90 to Oct 91

T. JAUERNIG LBA Oct 91 to Dec 94

G. CORMIER BV Feb 90 to Sep 90

D. MASSAT BV Sep 90 to Sep 93

D. DUMORTIER BV Sep 93 to Dec 94

FAA REPRESENTATIVES

R. HOSTENSKE Feb 90 to 0ct 91

Sep 92 to Dec.93

B. PRUDENTE Oct 91 to Sep 92

Dec 93 to Dec 94

A330/A340 MAINTENANCE REVIEW BOARD (1995 to 1999)

(‘end 99’ implies that membership will continue in 2000 with the launch of the A340-500/600 ISC

activities. ‘Dec 99’ indicates that membership ceases at the end of 1999)

JAA MEMBERS

G.THIRION DGAC (Chairman) Sep 95 to Sep 99

F. LEBLOND DGAC (Chairperson) Sep 99 to end 99

T. CROW CAA Sep 95 to Oct 96

M. MCMENEMY CAA Feb 97 to Sep 99

R. MONDON CAA Sep 99 to end 99

Th. H. de GROOT RLD Sep 95 to end 99

T. JAUERNIG LBA Sep 95 to end 99

D. DUMORTIER GSAC Sep 95 to end 99

P. CABANES GSAC Sep 95 to end 99

FAA REPRESENTATIVE

B. PRUDENTE Sep 95 to end 99

TRANSPORT CANADA REPRESENTATIVE

R. CAMPBELL Sep 95 to Feb 97

H. DYCK Mar 97 to Jan 98

J. PHIPPS Jan 98 to end 99

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.2 A330/A340 MAINTENANCE REVIEW BOARD (2000 onwards)

EASA MEMBERS

F JOUVARD DGAC/EASA (Chairperson) Mar 00 to Jun 06

F. LEBLOND DGAC (Chairperson) Jan 00 to Mar 02

D. DUMORTIER EASA Chairperson Jun 06 onwards

R. MONDON CAA Jan 00 to Jul 01

N. WILLIAMS CAA Jul 01 to Nov 04

M. EUSTICE CAA Nov 04 onwards

C. VAN LIESHOUT RLD Jan 00 onwards

T. JAUERNIG LBA Jan 00 to Mar 01

D. DUMORTIER GSAC Jan 00 to Jun 06

P. CABANES GSAC Jan 00

V. BERTHON GSAC Dec 02 to Mar 07

B. BACHA GSAC Mar 02 onwards

T. BADIA GSAC Jan 08 onwards

FAA REPRESENTATIVE

B. PRUDENTE Jan 00 to Nov 04

J. GLEITER Nov 04 to Dec 07

R. PATZKE Dec 07 onwards

TRANSPORT CANADA REPRESENTATIVE

J. PHIPPS Jan 00 to Dec 00

B. HAWES Dec 00 to Dec 02

R. PENNANEN Dec 02 to Nov 04

B. HAWES Nov 04 onwards

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.3 A330/A340 INDUSTRY STEERING COMMITTEE (Feb 90 to Dec 94)

NB The number in brackets refers to the number of meetings the ISC member or his representative

were able to attend.

A. MARCOUT ITF (Chairman from Apr 91) Feb 90 to Dec 94 (17)

R. CUTLER AIB (Co-chairman) Feb 90 to Dec 94 (17)

T. HARBOTTLE AIB (Secretary) Feb 90 to Dec 94 (17)

G. MONTEGU AFR Feb 90 to Oct 91 (7)

K. OKADA ANA Apr 91 to Jun 91 (1)

K. IIJIMA ANA Jun 91 to Dec 94 (8)

H. STROMMER AUA Oct 91 to Dec 94 (7)

R. TILNEY COA Jun 90 to Dec 92 (7)

A. KLEIN DLH Feb 90 to Dec 94 (11)

L. GARCIA IBE Feb 90 to Jan 91 (4)

D. BARTUREN IBE Jun 91 to Oct 91 (2)

J. GANDARILLAS IBE Sep 92 to Dec 94 (6)

F. ROSE LTU Feb 90 to Dec 94 (4)

J. LEWIS MON Feb 90 to Jun 90 (1)

D. NAKATA NWA Feb 90 to Dec 92 (4)

T. LARSON NWA Sep 90 to Dec 92 (8)

E. DE VOS SAB (Chairman up to Jan 91) Feb 90 to Jan 91 (4)

J. MERCKX SAB Jan 92 to Dec 92 (2)

M. PEREIRA TAP Feb 90 to Sep 92 (7)

C. LEITAO TAP Dec 92 to Dec 94 (3)

SUKASEM N. THA Feb 90 to Sep 90 (2)

TUMMASAK C. THA Sep 90 to Jan 92 (4)

PAIRAT P. THA Jan 92 to Dec 94 (6)

A. LUJIN TWA Feb 90 to Dec 94 (11)

B. BOURGOIN UTA Feb 90 to Dec 92 (12)

P. RAFFY CFMI Feb 90 to Oct 91 (7)

G. REBEYROL CFMI Oct 91 to Dec 94 (6)

J. LAWSON GE Feb 90 to Apr 91 (5)

R. MUNGIN GE Apr 91 to Jun 91 (1)

R. GIELEGHEM GE Jun 91 to Dec 94 (8)

B. STUBAUS PW Sep 90 to Jun 91 (1)

G. HOLTSINGER PW Jan 91 to Oct 91 (3)

A. GIMBEL PW Oct 91 to Apr 92 (2)

K. GERRITY PW Apr 92 to Dec 94 (5)

J. CHAMBERS RR Feb 90 to Dec 94 (14)

Ph GACHOD AS Feb 90 to Dec 92 (12)

T. REVEL AS Sep 92 to Dec 94 (8)

M. LACEBY BAe Feb 90 to Jun 91 (6)

P. MANLEY BAe Jun 91 to Dec 94 (11)

P. WEYH DA Feb 90 to Dec 94 (17)

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.4 A330/A340 INDUSTRY STEERING COMMITTEE (1995 to 1999)

(‘end 99’ implies that membership will continue in 2000 with the launch of the A340-500/600 ISC

activities. ‘Dec 99’ indicates that membership ceases at the end of 1999)

A. MARCOUT ITF (Chairman) Sep 95 to Oct 96

R. RODRIGUEZ AFR (Chairman) Feb 97 to end 99

T. HARBOTTLE AIB (Co-chairman) Sep 95 to Dec 99

K. PARTRIDGE AIB (Secretary) Sep 95 to end 99

S.J. LEE AAR Jan 98 to end 99

G. HIROSE ACA Feb 97 to Jan 98

G. LEPAGE ACA Jan 98 to end 99

R. RODRIGUEZ AFR Sep 95 to Feb 97

A. BENDALL AIH Sep 98 to Jan 99

C. HOLLAND AIH Jan 99 to end 99

W. KRAUS AUA Oct 96 to end 99

G. TOMKINSON CPA Jan 98 to Sep 98

DICK TSE CPA Sep 98 to end 99

W. SCHOLZ DLH Sep 95 to end 99

A. KOSCHARRE DLH Sep 95 to Oct 96

J. COELIUS DLH Oct 96 to end 99

L. SISK EIN Sep 95 to end 99

M.C. TYAGI GFA/GAMCO Jan 98 to end 99

F. ROSE LTU Sep 95 to Jan 98

J. RIDDERBECK LTU Jan 98 to end 99

J. LEWIS MON Jan 98 to end 99

E. MOYSEN SAB Feb 97 to Sep 98

G. VAN HUMBEECK SAB Sep 98 to end 99

M. MEYER SWR Feb 97 to Jan 98

R. WIDMER SWR Jan 98 to Sep 99

O. KOLLER SWR Sep 99 to end 99

C. LEITAO TAP Sep 95 to Oct 96

V.M. SANTOS TAP Oct 96 to end 99

M. ERCIHAN BAYIR THY Sep 95 to end 99

A. LUJIN TWA Sep 95 to Sep 98

A. OSMAN UAE Jan 98 to end 99

J. MITTERER USA Jan 98 to end 99

I. TAYLOR VIR Sep 95 to Oct 96

P. WOOLLACOTT VIR Oct 96 to Feb 97

M. HAINES VIR Feb 97 to end 99

P. FOURNIER CFMI Sep 95 to Jan 98

F. GREMONT CFMI Jan 98 to end 99

R. GIELEGHEM GE Sep 95 to end 99

J. CHAMBERS RR Sep 95 to Jan 98

M. COOPER RR Jan 98 to end 99

K. GERRITY PW Sep 95 to Feb 97

Jan 98 to end 99

R. SPERRY PW Feb 97 to Jan 98

M. POSTAL AS Sep 95 to Sep 98

T. REVEL AS Sep 98 to end 99

P. MANLEY BAe Sep 95 to Feb 97

R. WILBY BAe Feb 97 to Sep 99

K. SHERRIN BAe Sep 99 to Dec 99

J. BERNSTORFF DA Sep 95 to Feb 97

A. ERDINC DA Feb 97 to Jan 98

H. HEYDECKE DA Jan 98 to end 99

LF. PANIAGUA CASA Sep 95 to end 99

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.5 A330/A340 INDUSTRY STEERING COMMITTEE (2000 onwards)

R. RODRIGUEZ AFR (Chairman) Jan 00 to Jun 00

M. HAINES VIR (Chairman) Jun 00 to Dec 02

T. FODOR ACA (Chairman) May 03 to Jun 06

R. WALFORD ACA (Chairman) Mar 07 to Mar 08

C. RAMME AIB (Co-chairman) Jan 00 to Dec 02

A. SMITH AIB (Co-chairman) Dec 02 onwards

K. PARTRIDGE AIB (Secretary) Jan 00 to Jun 00

L. DARDY AIB (Secretary) Jun 00 to Dec 04

J.F HUIX AIB (Co-chairman Assistant) Dec 04 to June 06

B. HOVINE AFR Jan 00 to Mar 01

P. GROSEILLE AFR Mar 01 to Dec 02

J-F DERU AFR Apr 03 to Sep 05

J-F DERU AFR-KLM Sep 05 to June 06

P. DUMEZ AFR-KLM Jun 06 onwards

C. HOLLAND AIH Jan 00 to Nov 04

D. SWAIN AIH Nov 04 onwards

W. KRAUS AUA Jan 00 onwards

L. MINNS BMI Dec 00 to Nov 04

M. McALLISTER BMI Nov 04 onwards

B. DYSON CPA Jan 00 to Jun 00

M. HOLDEN CPA Jun 00 to Dec 02

M. KANAGASABAI CPA Dec 02 onwards

W. SCHOLZ DLH Jan 00 to Dec 02

W. REICHER DLH Dec 02 onwards

E. PALAZZI EEZ Nov 04 onwards

L. SISK EIN Jan 00 onwards

M.C. TYAGI GFA/GAMCO Jan 00 onwards

G. HARYANTO GIA Mar 01 onwards

S. SELLS JMC Mar 01 onwards

J.S. LEE KAL Mar 01 onwards

B. SCHULZ KLM Nov 04 to Sep 05

J. COELIUS LHT Jan 00 to May 03

U. LUCAS LHT May 03 onwards

J. RIDDERBECK LTU Jan 00 to Jun 00

R. DORKA LTU Jun 00 to Dec 02

M. BOCK LTU Dec 02 to Nov 04

K. SPECHT LTU Nov 04 onwards

J. CRUZ LXR Nov 04 onwards

S. SRINIVASAN MAS Nov 04 onwards

J. LEWIS MON Jan 00 to Jul 01

T. SATTLER MON Jul 01 onwards

L. HORTON NWA Dec 02 onwards

J. GRAHAM QFA Jul 01 to May 034

M. BLUESTONE QFA May 03 to Sep 05

D. SPIRITOSANTO QFA Sep 05 onwards

G. VAN HUMBEECK SAB Jan 00 to Dec 02

H. STRUYF SAB Dec 02 to Nov 04

R. MEYER SAS Mar 01 to Jul 01

L. RASMUSSEN SAS Jul 01 onwards

K. LINDAHL SAS Technical Services Nov 04 onwards

K. DELANNEY SRT Nov 04 onwards

O. KOLLER SWR Jan 00 to Mar 01

M. CAMENZIND SWR Mar 01 to Dec 02

S. RICHARD SWR Dec 02 onwardsV.M. SANTOS

TAP Jan 00 to Mar 01

F. MOREIRA TAP Mar 01 onwards

E. BAYIR THY Jan 00 to Nov 04

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.6 A. SUNGUR THY Nov 04 onwards

S. SELLS TCX May 03 onwards

A. OSMAN UAE Jan 00 to May 03

M. BOUZEGHOUB UAE May 03 onwards

J. MITTERER USA Jan 00 to Mar 01

H. SIMPSON USA Mar 01 onwards

M. HAINES VIR Jan 00 to Jun 00

C. MAC PHERSON VIR Jun 00 onwards

R. VIOLA VLE May 03 onwards

F. GREMONT CFMI Jan 00 to May 03

F. OBRECHT CFMI May 03 onwards

R. GIELEGHEM GE Jan 00 to Dec 02

J. BRUGGER GE Dec 02 onwards

M. COOPER RR Jan 00 to Jun 00

P. EMMOTT RR Jun 00 to Dec 00

R. WEAVER RR Dec 00 to Jul 01

D. HARDY RR Jul 01 onwards

K. GERRITY PW Jan 00 to May 01

G. LAPIS PW May 01 to Dec 02

A. DOLECKI PW Dec 02 to Sep 05

B. IVES PW Sep 05 onwards

J.P LALANNE HH Dec 02 to Nov 04

J.F CRIBELIER HH Sep 05 onwards

T. REVEL Airbus France Jan 00 to May 03

P. BALCHIN Airbus UK Jan 00 to May 03

H. HEYDECKE Airbus Germany Jan 00 to May 03

LF. PANIAGUA Airbus Spain Jan 00 to May 03

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.7 MAINTENANCE WORKING GROUP No.1 (until 1999)

(Systems ATA 27, 29, 32, 55 (THS attachment fittings))

J. BOYD AIB Chairman

H. FLEISCHER DLH

R. THAENERT DLH

J.C. BOISSEAU ITF

J.B. GARCIA ITF

G. MACART ITF

C. NICEY ITF

D. ROYER ITF

S. HILALI NWA

R. LILLY NWA

P. HENDRIKX SAB

J. MERCKX SAB

A. FADIGAS TAP

C. LEITAO TAP

CHATTAWANICH K. THA

KOSOL C. THA

PAIRAT P. THA

P. BERGER UTA

F. JOUAN UTA

Y. MELISSE UTA

L. BERNADAC AS

M. POSTAL AS

K. SHERRIN BAe

M. BRUNKE DA

J. CRAMER DA

A. ERDINC DA

A. FARMAKORIS DA

H. HEYDECKE DA

MRB ADVISORS

D. DUMORTIER BV (JAA)

F. SMITH FAA

MAINTENANCE WORKING GROUP No.2 (until 1999)

(Systems ATA 21, 25, 30, 35, 36, 38, 52, 53 (Drainage), 56 (Sliding windows),

57 (Drainage))

J. BERNSTORFF DA Chairman

W. FIEBIG DLH

J. COELIUS DLH

Mr. TREDE DLH

H. DETMERING DLH

A. BARJA IBE

M. NIETO IBE

P. SAEZ IBE

J. GARCIA ITF

G. LAABAN ITF

D. MOQUET ITF

C. NICEY ITF

D. ROYER ITF

R. LILLY NWA

T. CARLSON NWA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.8 J. DAVIS NWA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.9 J. ANDRE SAB

P. HENDRIX SAB

J. KIRSCHFINK SAB

R. STAUBAUT SAB

A. ASSUNCAO TAP

F. MOREIRA TAP

AAT L. THA

EKACHAI K. THA

KOSOL C. THA

JONGRAK P. THA

JN. CARTER TWA

RJ. CARTER TWA

B. BANASZEWSKI UTA

B. MARTIN UTA

R. RODRIGUEZ UTA

L. BERNADAC AS

C. DELMAS AS

K. DEACON BAe

J. COOPER DA

W. ERIKSON DA

U. GOGOLL DA

H. HEYDECKE DA

B. KOENIG DA

M. KORAN DA

U. KÜHN DA

U. LASZIG DA

C. MACPHERSON DA

M. MOLL DA

P. OBERSCHELP-MÜLLER DA

E. PODIEN DA

T. ROEGER DA

O. SCHULZ DA

P. SCHUMACHER DA

N. SEEHAFER DA

K.P. SELLMANN DA

A.V. SONER DA

MRB ADVISORS

T. LLEWELLYN CAA (JAA)

M. McMENEMY CAA (JAA)

RG. ELMORE FAA

R. HOSTENSKE FAA

MAINTENANCE WORKING GROUP No.3 (until 1999)

(Systems & powerplant ATA 28, 49, 71 to 80)

M. O'KEEFFE AIB Chairman

Sub-group ATA 28

H. BOURY ITF

G. MACARY ITF

J.B. GARCIA ITF

J. BENTO ITF

S.P. ROBINS DLH

A. SCHEFFER NWA

J. MERCKX SAB

E. VAN LOO SAB

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.10 CHATTAWANICH K. THA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.11 TUMPRAYOTH C. THA

P. DUMAS UTA

B. MARTIN UTA

R. PARSONS BAe

G. HILLS BAe

H. HOFFMANN DA

MRB ADVISORS

P. VAQUEZ BV (JAA)

H. PRUIS RLD (JAA)

W. MACHADO FAA

P. PRUDENTE FAA

Sub-group A340-300B (including single ACT)

M. LYNCH VIR

S. MAYES CPA

A. ERDINC DA

H. HOFFMANN DA

G. HILLS BAe

M. WOODS BAe

MRB ADVISORS

P. VAQUEZ GSAC (JAA)

H. PRUIS RLD (JAA)

S. LEEPER FAA

Sub-group ATA 49

G. MACARY ITF

M. LINNEMANN DLH

A. SCHEFFER NWA

J. VIEGAS TAP

YUTHASIT SUWANLOY THA

D. TAMZALI UTA

H. HOFFMANN DA

K.P. SELLMANN DA

B. SHALK GARRETT

MRB ADVISORS

P. VAQUEZ BV (JAA)

H. PRUIS RLD (JAA)

K. MILLER FAA

Sub-group powerplant ATA 71 to 80

B. HEINRICH AFR

C. BLOHM DLH

H. HAERTEL DLH

S.P. ROBINS DLH

R. TORRES IBE

A. SCHEFFER NWA

C. MARTINS TAP

A. CABRITA TAP

C. FIGUERES UTA

C. DELMAS AS

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.12 D. ROVATTI AS

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.13 D. OTTONE CFMI/SNECMA

M. BERNSTEIN CFMI/GE

R. CREAMER ROHR

N. MOULAC HISPANO SUIZA

MRB ADVISORS

P. VAQUEZ BV (JAA)

H. PRUIS RLD (JAA)

W. MACHADO FAA

MAINTENANCE WORKING GROUP No.4 (until 1999)

(Systems 22, 23, 24, 26, 31, 33, 34, 45)

M. ERAN-TASKER Chairman

C. GLASHAGEN DLH

A. NESSEL DLH

G. ALCOL IBE

A. GORDO IBE

G. BOUSSAC ITF

D. LE BON ITF

J. MARCHEBOUT ITF

R. ROYER ITF

J.E. DAVIS NWA

W. DECANT SAB

D. WERQUIN SAB

F. MAGALHAES TAP

M. A.TERENO TAP

ANEKBOON P. THA

NONKAMPA A. THA

J.J. KOCH TWA

K.W. WEIGMANN TWA

J.C. CATHELINEAU UTA

P. DUMAS UTA

V. MAHIEU UTA

L. BERNADAC AS

P. BOUTET AS

K. DEACON BAe

P. FRIEDRICH DA

H. HOFFMANN DA

C. MACPHERSON DA

O. MITTELSTEINER DA

P. SCHUMACHER DA

J. WESTERMANN DA

K.G. WIEN DA

MRB ADVISORS

D. LEWIS CAA (JAA)

T.H. DE GROOT RLD (JAA)

J. RAMEL STNA (JAA)

P. BIEVER FAA

T. DEAN FAA

W. PEART FAA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.14

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.15 MAINTENANCE WORKING GROUP No.5 (until 1999)

(Structures ATA 32, 52, 53, 54, 55, 56, 57, 71)

C. RAMME AIB Chairman

N. TSUCHIYA ANA

H. BARGMANN DLH

W. CONRADI DLH

J. GANDARILLAS IBE

C. MASSET ITF

C. NICEY ITF

M. SOAVE ITF

M. HILLBORN NWA

A. BRANCO TAP

A. FERREIRA TAP

MARAYAT J. THA

PAITOON M. THA

D. DROLLINGER TWA

R. RODRIGUEZ UTA

A.J. SMITH AIB

B. BORG AS

P. GUYOT AS

M. JONES BAe

F. DELGADO CASA

W. KOSTEWICZ DA

N. SEEHAFER DA

M. SULEAU SONACA

MRB ADVISORS

T. JAUERNIG LBA (JAA)

S. LAGNEL BV (JAA)

C. CLARK FAA

R. HOSTENSKE FAA

MAINTENANCE WORKING GROUP No.6 (until 1999)

(Zonal)

G. ADLER DA Chairman

H. AOYAMA ANA

W. CONRADI DLH

J. GANDARILLAS IBE

C. MASSET ITF

C. NICEY ITF

J.P. RAMELET ITF

M. SOAVE ITF

R. CHELBERG NWA

M. EVANS NWA

A. BRANCO TAP

C. LEITAO TAP

SURACHAI P. THA

R.H. BETTS TWA

G. CORVEST UTA

A.J. SMITH AIB

P. MEREAU AS

K. DEACON BAe

I. RIANO CASA

M. EREN DA

P. OBERSCHELP-MÜLLER DA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.16 MRB ADVISORS

S. LAGNEL BV (JAA)

S. LEEPER FAA

CREW REST ROOM (UNDERFLOOR) MWG – May 97

O. MITTELSTEINER AIB (Chairman)

A. WOOTTEN VIR

A. SUNGUR THY

J. COELIUS DLH

F.L. MOREIRA TAP

H.J. SCHEFFLER DA

W. BOGDAHN DA

B. RIEDEL DA

V. KUTTIMALAI DA

A. ERDINC DA

K.G. WIEN DA

F. JAEHN DA

J. WESTERMANN DA

M. MOLL DA

MRB ADVISOR

D. DUMORTIER GSAC (JAA)

A330/A340 EVOLUTION WG (A-CHECK) - Nov 97

O. MITTELSTEINER AIB (Chairman)

M. HOLDEN CPA

T. KELLY EIN

M.C. TYAGI GFA/GAMCO

O.R. AL-ANZI KAC

S.H. JUN KAL

J. COELIUS LHT

SELVAMANY SRINIVASAN MAS

N.H. MINA MSR

L.E. HWEE SIA

W.K.A. KANG SIA

R. WIDMER SRT

V.M. SANTOS TAP

C. SENTURK THY

M.D. HAINES VIR

T. HARBOTTLE AIB

M. POSTAL AS

K.. SHERRIN BAe

H. HEYDECKE DA

MRB ADVISORS

D. DUMORTIER GSAC (JAA)

P. CABANES GSAC (JAA)

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.17 A340-500/600 MAINTENANCE WORKING GROUP AND A330/A340 EVOLUTION WORKING GROUP

MAINTENANCE WORKING GROUP No. 1

(Systems ATA 27, 29, 32, 55 (THS attachment fittings))

B. LIPSCOMBE AIB Chairman

L. MINNS BMA

H. LEUNG CPA

D. PARSONS CPA

P. HARDING FLS

M.K. KNOTH LHT

M. OTTERSBACH LHT

P. WITTMER SWR

A. WOOTTEN VIR

M. DOWNEY VIR

T. WILSON VIR

R. CARRERE Airbus France

F. BRETHES Airbus France

F. AMELLER Airbus France

P. SANTI Airbus France

R. MORVAN Airbus France

D. LITOUX Airbus France

H. LE BERRE Airbus France

R. DAYRE Airbus France

M. EREN Airbus Germany

H. HEYDECKE Airbus Germany

F. JAEHN Airbus Germany

H. OTTE Airbus Germany

J. HUELSMANN Airbus Germany

T. HOYLE Airbus UK

K. SHERRIN Airbus UK

J. GOODRUM Airbus UK

P. Mc LANAGHAN Airbus UK

A. KIBBY Airbus UK

P. BALCHIN Airbus UK

B. STIRLING Airbus UK

A. WOMBWELL Airbus UK

M. HARRIS Airbus UK

M. JONES Airbus UK

P. COLLINS Airbus UK

M. JONES Messier-Dowty

S. ROLLIN Messier-Dowty

MRB ADVISORS

R. PATZKE FAA

T. NEWCOMBE FAA

B. PRUDENTE FAA

N. CLOUT GSAC (JAA)

ISC ADVISOR

M. HAINES VIR

MAINTENANCE WORKING GROUP No. 2

(Systems ATA 21, 25, 30, 35, 36, 38, 52, 53 (Drainage), 56 (Sliding windows), 57 (Drainage))

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.18 T. ROEGER AIB Chairman

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.19 E. NG CPA

J. KWOK CPA

D.J. LEE KAL

D.W. JEON KAL

H.O. CHOI KAL

D.W. JEON KAL

K. BEHNKE LHT

K. WINTER LHT

W. KO SIA

C.L. SIM SIA

R. KONRAD SWR

R. HALLER SWR

A. WOOTTEN VIR

D. HEATH VIR

M. DOWNEY VIR

R. MURPHY VIR

J. WESTERMANN Airbus Germany

U. LUCAS Airbus Germany

W. ERIKSON Airbus Germany

K-G. WIEN Airbus Germany

P. FRIEDRICH Airbus Germany J. KRÜGER Airbus Germany

A. WERTHER Airbus Germany

E. PODIEN Airbus Germany

M. EREN Airbus Germany

H. SCHMIDT Airbus Germany

K.P. SELLMANN Airbus Germany

B. RANDERATH Airbus Germany

N. WINKLER Airbus Germany

B. GEIDEL Airbus Germany

S. KLAUBERT Airbus Germany

P. BALCHIN Airbus UK

R. FIDEL Airbus France

M. REVEL Airbus France

D. SAUVAGE Airbus France

J. NEVEUX Airbus France

MRB ADVISORS

R. PATZKE FAA

H. HOFFMANN FAA

B. HAWES Transport Canada

T. JAUERNIG LBA (JAA)

ISC ADVISOR

J. COELIUS LHT

MAINTENANCE WORKING GROUP No. 3

(Systems ATA 49, 71 to 80)

J-F. HUIX AIB Chairman

R. PARKER ACA

F. RUEST ACA

P. REBY AFR

G. MACARY AFR

S. TRIGONA AFR

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.20 B. GABLER AUA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.21 C. WYATT BMA

F. LEE CPA

V. LOK CPA

P. BRAUNY DLH

J. GILDEA FLS

P. BRUDLER LHT

H.J. JOHN LHT

W. RÖLL LHT

A. LIEW SIA

E. WAEGELI SWR

R. HALLER SWR

S. GRIFFITHS VIR

G. SAMPSON VIR

M. SMYTH VIR

M. FABRITZ HONEYWELL

F. GREMONT CFMI

R. GIELGHEM GE

M. WEETMAN PW

S. FURNESS RR

S. POOLE RR

J. LI RR

A. ABRAMS RR

A. DOWEY RR

P. STOW RR

S. HEATH RR

R. WEAVER RR

P. LAURENT AIRCELLE

C. RABIET AIRCELLE

A. CARTER AIRCELLE

D. TISSIE AIRCELLE

M. JEANVOINE HISPANO SUIZA

M. ANSCIEAU Airbus France

F. HERUBEL Airbus France

J-P. PELLISSIER Airbus France

A. CORNU Airbus France

H. HOFFMANN Airbus Germany

MRB ADVISORS

R. MONDON CAA (JAA)

R.H. LOVE FAA

J.R HARRINGTON FAA

ISC ADVISOR

O. KOLLER SWR

P. EMMOTT RR

R. WEAVER RR

C. MAC PHERSON VIR

L. MINNS BMA

MAINTENANCE WORKING GROUP No.4

(Systems ATA 22, 23, 24, 26, 31, 33, 34, 45, 46)

D. DESCHEEMAEKER AIB Chairman

L. LEE CPA

E. ELZ LHT

J. ROSSEL LHT

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.22 B. LAMBERT LHT

A. SCHMIDT LHT

J. DIMKE LHT

S.L. LOW SIA

H. SCHMID SWR

M. DI LAURENZIO SWR

H. MEIER SWR

A. WOOD VIR

A. POND VIR

J. THORPE VIR

C. DELMAS Airbus France

C. GELINET Airbus France

R. FIDEL Airbus France

J-Y. NICOLAS Airbus France

L. PARIS Airbus France

G. TATHAM Airbus France

A. ABGUILLERM Airbus France

D. GUILLOT-SALOMON Airbus France

S. FERRAN Airbus France

F. RAPENNE Airbus France

H. KERHOAS Airbus France

P. PONSOT Airbus France

P. SANTI Airbus France

J. SAULNIER Airbus France

B. BOURDIEU Airbus France

D. SAUVAGE Airbus France

B. REYNES Airbus France

J. TREBOSC Airbus France

P. CALVAIRAC Airbus France

J.J. BOUYER Airbus France

B. CARAYON Airbus

T. SICK Airbus Germany

J. WESTERMANN Airbus Germany

K. BUCKOW Airbus Germany

W. MEIßNER Airbus Germany

H. ZANKE Airbus Germany

MRB ADVISORS

N. CLOUT GSAC (JAA)

F. LEBLOND GSAC (JAA)

D. LAMOTHE GSAC (JAA)

D. STRICKLAND FAA

ISC ADVISOR

C. MACPHERSON VIR

MAINTENANCE WORKING GROUP No.5

(Structures ATA 32, 52, 53, 54, 55, 56, 57, 71, 78)

A. SMITH AIB Chairman

R. WALFORD ACA

Y. KIM MAN CPA

F. POON CPA

J. YUK CPA

H. LANGFELDT LHT Co-chairman

T. HOLIN LHT

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.23 M. EL TOBGY MSR

W. KO AH KANG SIA

L. SIM CHEN SIA

C. CATTAROSSI SWR

P. WEBER SWR

C. MAURRAY VIR

W. KOSTEWICZ Airbus Germany R. MÖBIUS Airbus Germany

J. HUELSMANN Airbus Germany

C. DUCAMP Airbus France

G. MOREAU Airbus France

C. GALLIER Airbus France

J. KRUMMENACKER Airbus France

H. ENJALRIC Airbus France

C. LEDENTU Airbus France

S. COSMA Airbus France

E. DUMONT Airbus France

X. KARST Airbus France

L. SAMMITO Airbus France

M. HIRST Airbus UK

H. WYATT Airbus UK

F. DELGADO Airbus Spain

F. CERVANTES Airbus Spain

R. APPOYO Airbus Spain

J. MOTTA Airbus Spain

S. WANTENS SONACA

J. LI RR

E. VAIN AIRCELLE

M. JONES Messier-Dowty

S. ROLLIN Messier-Dowty

MRB ADVISORS

D. JONES FAA

P. ROMAIN RLD (JAA)

P. CABANES GSAC (JAA)

A. HOWELL Transport Canada

ISC ADVISOR

M. HAINES VIR

J. LEWIS MON

MAINTENANCE WORKING GROUP No.6

(Zonal)

F. JAEHN AIB Chairman

H. LANGFELDT LHT

L. SIM CHEN SIA

S. RICHARDI SWR

C. MURRAY VIR

M. EREN Airbus Germany

G. MOREAU Airbus France

M. CARMIER Airbus France

C.B. LOWER Airbus UK

P. MAC LENHAGHAM Airbus UK

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.24 F. DELGADO Airbus Spain

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.25 F. CERVANTES Airbus Spain

R. APPOYO Airbus Spain

MRB ADVISORS

D. JONES FAA

ISC ADVISOR

M. HOLDEN CPA

MAINTENANCE WORKING GROUP No.7

(Systems ATA 28)

O. SCHOLZ AIB Chairman

C. TSE CPA

D. KOWALZIK LHT

T.K. SIM SIA

R. HALLER SWR

D. HEATH VIR

M. DOWNEY VIR

T. HOYLE Airbus UK

G. HILLS Airbus UK

M. WIGHELL Airbus UK

P. BALCHIN Airbus UK

J. GOODMAN Airbus UK

M. DIMMERY Airbus UK

T. DO Airbus UK

R. SLADE Airbus UK

S. FOX Airbus UK

H. HOFFMANN Airbus Germany

MRB ADVISORS

B. PRUDENTE FAA

R. PATZKE FAA

D. LAMOTHE GSAC (JAA)

ISC ADVISOR

D. HEATH VIR

SYSTEMS AND POWERPLANT MAINTENANCE WORKING GROUP (APRIL 2003)

J. NEVEUX Airbus France Chairman

F-R. OENZIL GIA

H-J. LEE KAL

P. WITTMER SR Technics

B. BOLOT AIF

A. WHITE USA

L. HORTON NWA

D. FALKOWSKI Airbus Deutschland

L. WENK Airbus Deutschland

W. MEISSNER Airbus Deutschland

M. POULUS Airbus Deutschland

J-F. HUIX Airbus France

L. DARDY Airbus Central Entity

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.26 R. CARRERE Airbus France

C. LAMONT Airbus Central Entity

R. LAFORGUE Airbus Central Entity

S. VERGNAT Airbus France

A. CORNU Airbus France

J. SAULNIER Airbus France

G. VIADER Airbus Central Entity

G. THOMAS Airbus France

J. GOODRUM Airbus UK

MRB ADVISORS

Neil WILLIAMS CAA

Harry HOFFMAN FAA

SYSTEMS AND POWERPLANT MAINTENANCE WORKING GROUP (FEBRUARY 2005)

J. NEVEUX Airbus Central Entity Chairman

B. BOLOT AIF

P. RUDNIANYN AIF

B. CHUANG CAL

F. ALIBAKSH GAMCO

R. AL-MASKERY GAMCO

S.ALRIYAMI GAMCO

M. CAMAHALAN LHT PHILIPPINES

M. FOSTER MON

J. PAPAGIANIS QFA

I. BARGFREDE Airbus Deutschland

C. BENDER Airbus Deutschland

A. EBERT Airbus Deutschland

A. HERTERICH Airbus Deutschland

S. KIRCHNER Airbus Deutschland

S. KLAUBERT Airbus Deutschland

R. PORTILLO Airbus Deutschland

G. RAMME Airbus Deutschland

J. SEUSS Airbus Deutschland

S. STAHLKOPF Airbus Deutschland

A. WERTHER Airbus Deutschland

E. BARRIERES Airbus Central Entity

B. BOURDIEU Airbus Central Entity

E. CLAIR Airbus Central Entity

R. LAFORGUE Airbus Central Entity

J. MARTINEZ Airbus Central Entity

L. MORA-FIGUEROA Airbus Central Entity

V. FONDEVIOLE Airbus Central Entity

P. SALLES-PARFOUBY Airbus Central Entity

L. SARTRE Airbus Central Entity

N. THIBAUD Airbus Central Entity

G. VENDITTO Airbus Central Entity

S. VERGNAT Airbus Central Entity

G. VIADER Airbus Central Entity

H. ZITOUNI Airbus Central Entity

J. GOODRUM Airbus UK

ISC ADVISOR

S. SRINIVASAN MAS

MRB ADVISOR

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.27 H. HOFFMAN FAA

SYSTEMS AND POWERPLANT MAINTENANCE WORKING GROUP (APRIL 2005)

J. NEVEUX Airbus Central Entity Chairman

B. BOLOT AIF

H. FAJARDO LHT PHILIPPINES

M. OTTERSBACH LHT FRANKFURT

S. SRINIVASAN MAS

M. FOSTER MON

J. HAMILTON MYT

B. ERICKSON NWA

M-P. CALATA PAL

D. WELLADSEN QFA

L. RASMUSSEN SAS

C. Trige PEDERSEN SAS

A. KAPUGEEKIYANA ALK

H. SIMPSON USA

I. BARGFREDE Airbus Deutschland

C. BENDER Airbus Deutschland

D. DANIELS Airbus Deutschland

M. DEEKE Airbus Deutschland

A. EBERT Airbus Deutschland

H. HEYDECKE Airbus Deutschland

S. KIRCHNER Airbus Deutschland

S. KLAUBERT Airbus Deutschland

T. KNAUER Airbus Deutschland

H. LETMATHE Airbus Deutschland

W. MEISSNER Airbus Deutschland

S. POMMERENING Airbus Deutschland

R. PORTILLO Airbus Deutschland

M-J. POULUS Airbus Deutschland

G. RAMME Airbus Deutschland

M. SCHOETTLER Airbus Deutschland

J. SEUSS Airbus Deutschland

S. STAHLKOPF Airbus Deutschland

A. WERTHER Airbus Deutschland

O. WEISS Airbus Deutschland

F. BRETHES Airbus Central Entity

N. CHALOU Airbus Central Entity

E. CLAIR Airbus Central Entity

A. CORNU Airbus Central Entity

L. DARDY Airbus Central Entity

V. GIRARD Airbus Central Entity

R. LAFORGUE Airbus Central Entity

C. LAMONT Airbus Central Entity

J. MARTINEZ Airbus Central Entity

L. MORA-FIGUEROA Airbus Central Entity

S. PLAN Airbus Central Entity

S. VERGNAT Airbus Central Entity

G. VIADER Airbus Central Entity

H. ZITOUNI Airbus Central Entity

J. GOODRUM Airbus UK

D. SANZ-MERINO Airbus Spain

MRB ADVISOR

B. BACHA GSAC

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.28 ISC ADVISOR

M. McALLISTER BMI

Zonal Maintenance Working Group 2005.1 (HGW and 4C Evolution)

Guerino Venditto Airbus France Chairman

Selvamany Srinivasan Malaysia Airlines

Francois Turpin Air France

Mike Foster Monarch

Iver S.Hansson SAS

Igor Carvutto Eurofly

Enrico Palazzi Eurofly

Mustafa Eren Airbus Deutschland

Frans Priyatna Airbus Deutschland

Jim Goodrum Airbus UK

Luis Cordon-Torres Airbus France

Daniel Wiborg Airbus France

Francisco Cervantes Airbus Spain

Tony Montilla Airbus UK

Bjoern Diekjobst Airbus France

Jochen Hillingshauser Airbus France

Jean Comte Airbus France

Hicham Berrada Airbus France

François Montegut Airbus France

Yvan Faure Airbus France

MRB Advisor

Boualem Bacha GSAC

ISC Advisor

Selvamany Srinivasan Malaysia Airlines

Zonal Maintenance Working Group 2005.2 (EZAP)

Guerino Venditto Airbus France Chairman

Eric Pesce Air France

Herbert Gunther Lanchile

Iver S.Hansson SAS

Frank.C. Jensen SAS

Cidalia Piedade Da Costa TAP

Mark McAllister BMI

John A. Tasseron TCA

Frank Jaehn Airbus Deutschland

Mustafa Eren Airbus Deutschland

Frans Priyatna Airbus Deutschland

Jim Goodrum Airbus UK

Paul Clarke Airbus UK

Francisco Cervantes Airbus Spain

Marc Carmier-dit-Boillet Airbus France

Colin Kane Airbus France

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.29 Thomsas Domise Sonovision

MRB Advisor

Ronald J. Gleiter FAA

Malcolm Eustice CAA

Pierre Gaucherand GSAC

John A. Tasseron TCA

ISC Advisor

Rob Walford Air Canada

Zonal Maintenance Working Group 2007.1 March 2007 (A & 8C Evolution)

Luis Cordon-Torres Airbus Chairman

Mike FOSTER Monarch

Paul MICALLEF Qantas

Perets FREDERICK Garuda Indonesia

Zuriati AKMAN Garuda Indonesia

Tulay BORKLU Turkish Airlines

Imdat YILMAZ Turkish Airlines

John W HAMILTON My Travel

Greg SIMMONS Northwest Airlines

Jose Antonio HUERTAS-DIEZ Airbus

Bill DAVIES Airbus

Jacqueline SAULNIER Airbus

Mustafa EREN Airbus

Sebastián SANCHO Airbus

Alan SMITH (part time) Airbus (part time)

A330 A340 Zonal MRB advisors

MRB Advisors

Brent BRINGLE FAA

Veronique BERTHON GSAC

Dominique DUMORTIER GSAC (part time)

ISC Advisor

None

Zonal Maintenance Working Group 2007.2 June 2007 (A & 8C Evolution)

Luis CORDON-TORRES Airbus Chairman

Paul MICALLEF Qantas

Carsten MARKS Lufthansa Technik

Ivor HANSSON SAS

Tulay BORKLU Turkish Airlines

Bilal DEMIR Turkish Airlines

John W. HAMILTON My Travel

Greg SIMMONS Northwest Airlines

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.30 Jose Antonio HUERTAS-DIEZ Airbus

Frans PRIYATNA Airbus

Jacqueline SAULNIER Airbus

Mustafa EREN Airbus

Lorenz WENK Airbus

Frank JAEHN Airbus

MRB Advisor

Mr Malcolm, EUSTICE CAA

ISC Advisor

James, MILNER Virgin Atlantic

STRUCTURES MAINTENANCE WORKING GROUP (MARCH 2005)

G. POST Airbus GE Chairman

H. LANGFELDT LH Technik Co-Chairman

C. MARKS LH Technik

C. PETIT Air France

F. VIDMAR Qantas

J. YUK Cathay Pacific

P. J. HENDRICK Northwest Airlines

M. EL-TOGBY Egyptair

M. FOSTER Monarch

P. ROSSIER SR Technics

G. DARD Airbus FR

L. CORDON Airbus FR

M. GANTER Sonovision

R. MOEBIUS Airbus GE

J. HUELSMANN Airbus GE

H. WYATT Airbus UK

F. CERVANTES-GONZALES Airbus ES

H. DANDO Airbus FR

W. KOSTEWICZ Airbus GE

M. HIRST Airbus UK

ISC ADVISOR

S. SRINIVASAN Malaysia Airlines

MRB ADVISOR

B. BACHA DGAC

STRUCTURES MAINTENANCE WORKING GROUP (MAY 2005)

G. POST Airbus GE Chairman

H. LANGFELDT LH Technik Co-Chairman

W. PRESS LH Technik

C. PETIT Air France

F. VIDMAR Qantas

J. YUK Cathay Pacific

M. FOSTER Monarch

P. ROSSIER SR Technics

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.31 A. KAMTHITA Thai Airways

I. HANSSON SAS

R. WALFORD Air Canada

G. DARD Airbus FR

L. CORDON Airbus FR

M. GANTER Sonovision

R. MOEBIUS Airbus GE

J. HUELSMANN Airbus GE

H. WYATT Airbus UK

P. ROJAS-BARCI Airbus ES

H. DANDO Airbus FR

A. MAURIZI Airbus FR

M. BOZZOLO Airbus FR

ISC ADVISOR

S. SRINIVASAN Malaysia Airlines

MRB ADVISOR

B. BACHA DGAC

R. R. PATZKE FAA

STRUCTURES MAINTENANCE WORKING GROUP (NOV 2005)

Guenter POST Airbus (Chair)

Harald LANGFELDT Lufthansa Technik (Co-Chair)

Ferdy VIDMAR QANTAS

Iver HANSSON SAS

Mike FOSTER Monarch

Philippe ROSSIER SR Technics

Charles PETIT Air France

Johnny YUK Cathay Pacific

Lars RASMUSSEN SAS

Walter PRESS Lufthansa Technik

Richard NEWTON Virgin Atlantic

Walter KOSTEWICZ Airbus

Celine LEDENTU Airbus

Jan HUELSMANN Airbus

Jan ZEGAREK Airbus

Rainer MOEBIUS Airbus

Luis CORDON-TORRES Airbus

Pilar ROJAS-BARCI Airbus

Helen WYATT Airbus

John MASON Airbus

Bob LIPSCOMBE Airbus

Karl BRAZIER Messier-Dowty

Glen CHISHOLM Messier-Dowty

ISC ADVISOR

None

MRB ADVISOR

Boualem BACHA DGAC

Richard E. JONES FAA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.32 STRUCTURES MAINTENANCE WORKING GROUP (NOV 2006)

Guenter POST Airbus (Chair)

Charles PETIT Air France (Co-Chair)

Ferdy VIDMAR QANTAS

Shane HARLEY SR Technics

Mike FOSTER Monarch

Philippe ROSSIER SR Technics

Francois TURPIN Air France

Dan VO Cathay Pacific

Simon CHAN Air Canada

Walter PRESS Lufthansa Technik

Carsten MARKS Lufthansa Technik

Richard NEWTON Virgin Atlantic

Harald LANGFELDT Lufthansa Technik

Auttagon KAMTHITA Thai Airways

Salahuddin Ahmed MORSHED Emirates

Nasir MUNEER Emirates

Jess BARRIER US Airways

Walter KOSTEWICZ Airbus

Lorenz WENK Airbus

Celine LEDENTU Airbus

Jan HUELSMANN Airbus

Jose Antonio HUERTAZ-DIEZ Airbus

Rainer MOEBIUS Airbus

Luis CORDON-TORRES Airbus

Daniel WIBORG Airbus

Helen WYATT Airbus

Andre DELANNOY Airbus

Andreas BEHRMANN Airbus

Davide CAVAZZONI Airbus

ISC ADVISOR

None

MRB ADVISOR

Boualem BACHA DGAC

Ronald J. Gleiter FAA

Laurent PINSARD EASA (STG Advisor)

STRUCTURES MAINTENANCE WORKING GROUP (MAR 2007)

Guenter POST Airbus (Chair)

Charles PETIT Air France (Co-Chair)

Wayne NELSON QANTAS

Mike FOSTER Monarch

Philippe ROSSIER SR Technics

Francois TURPIN Air France

Dan VO Cathay Pacific

Walter PRESS Lufthansa Technik

Carsten MARKS Lufthansa Technik

Richard NEWTON Virgin Atlantic

Iver HANSSON SAS

Auttagon KAMTHITA Thai Airways

Ned WIDENER Northwest Airlines

Jess BARRIER US Airways

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.33 Pascal CANGUILHEM Airbus

Lucien SANTI Airbus

Celine LEDENTU Airbus

Jan HUELSMANN Airbus

Jose Antonio HUERTAZ-DIEZ Airbus

Rainer MOEBIUS Airbus

Luis CORDON-TORRES Airbus

Daniel WIBORG Airbus

Helen WYATT Airbus

Thomas FRISCH Airbus

Andreas BEHRMANN Airbus

Davide CAVAZZINI Airbus

Frederic MORVAN Airbus/Sonovision

Michel GANTER Airbus/Sonovision

ISC ADVISOR

None

MRB ADVISOR

Ralf Schneider LBA

Ronald J. Gleiter FAA

Laurent PINSARD EASA (STG Advisor)

STRUCTURES MAINTENANCE WORKING GROUP (MAY 2007)

Mr. Guenter POST Airbus (Chair)

Charles PETIT Air France (Co-Chair)

Wayne NELSON QANTAS

Philippe ROSSIER SR Technics

Dan VO Cathay Pacific

Walter PRESS Lufthansa Technik

Carsten MARKS Lufthansa Technik

Richard NEWTON Virgin Atlantic

Auttagon KAMTHITA Thai Airways

Ned WIDENER Northwest Airlines

Shane HARLEY SR Technics

Salahuddin Ahmed MORSHED Emirates

Celine LEDENTU Airbus

Jan HUELSMANN Airbus

Jose Antonio HUERTAZ-DIEZ Airbus

Luis CORDON-TORRES Airbus

Daniel WIBORG Airbus

Helen WYATT Airbus

John Mason Airbus

Thomas FRISCH Airbus

Frederic MORVAN Airbus/Sonovision

ISC ADVISOR

None

MRB ADVISOR

Ralf Schneider LBA

Ronald J. Gleiter FAA

Laurent PINSARD EASA (STG Advisor)

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.34 STRUCTURES MAINTENANCE WORKING GROUP (June 2009)

Guenter POST Airbus (Chair)

Carsten MARKS Lufthansa Technik (Co-Chair)

Fredy VIDMAR QANTAS

Philippe ROSSIER SR Technics

Dan VO Cathay Pacific

Walter PRESS Lufthansa Technik

Mark A. SCHWEITZER Delta Airlines

Richard NEWTON Virgin Atlantic

Auttagon KAMTHITA Thai Airways

Jess BARRIER US Airways

Shane HARLEY SR Technics

Shoaib REHMATULLAH Emirates

Mathias SAILER Swiss

Alexandre HAYET CorsAir

Laurent GROUES CorsAir

Iver S. HANSSON SAS

Charles PETIT Air France

William ko ah KANG Singapore Air

Mohamed El TOGBY Egypt Air

Mike FOSTER Monarch

Selvamany SRINIVASAN Malaysia Airlines

Simon CHAN Air Canada

Ludwig ZOELLNER Swiss

Paul BISHOP Thomas Cook

Pieter JANS Brussels Airlines

Celine LEDENTU Airbus

Altay KANBUR Airbus

Alberto GARCIA-ALVAREZ Airbus

Helen WYATT Airbus

Benoit ZWICK Airbus

Rainer MOEBIUS Airbus

ISC ADVISOR

None

MRB ADVISOR

Ralf SCHNEIDER LBA

Roy PATZKE FAA

Laurent PINSARD EASA (STG Advisor)

SYSTEMS MAINTENANCE WORKING GROUP (FEBRUARY 2007)

J. NEVEUX Airbus Central Entity Chairman

R. MARTINEZ AEA

J-M. JEAN-ALPHONSE AFR

T. STEVENS AFR

R. DILMAHAMOOD MAU

Y. MERMET THT

KC. MULONGA BMI

T. SIMHANI BMI

M. DOWNEY CPA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.35 A. HAYET CRL

A. SALEM MSR

M. AHMAD ETD

V. RUOTSALAINEN FIN

D. Ryan V. DIZON LUFTHANSA TECHNIK PHILIPPINES

P. SCHNELLRIEDER LUFTHANSA TECHNIK

M. FOSTER MON

J. HAMILTON MYT

R. BOBEK NWA

S. ROACH QFA

C. ØSTER SAS

L. GAUDERS DAT

J. FIELDS SR Technics Ireland

D. MUTABDZIC SR Technics Switzerland

Y. MERMET THT

C. LOWEN VIR

A. EBERT Airbus Deutschland

T. ERTL Airbus Deutschland

R. GOESS Airbus Deutschland

S. KIRCHNER Airbus Deutschland

S. KLAUBERT Airbus Deutschland

W. MEISSNER Airbus Deutschland

A. NOESKE Airbus Deutschland

S. POMMERENING Airbus Deutschland

G. RAMME Airbus Deutschland

O. RICHTER Airbus Deutschland

M. SCHOETTLER Airbus Deutschland

J. SEUSS Airbus Deutschland

S. SVERDRUP Airbus Deutschland

U. WASSMANN Airbus Deutschland

O. WEISS Airbus Deutschland

C.COWLEY Airbus UK

MRB advisors

B. BACHA EASA

H. HOFFMAN FAA

SYSTEMS MAINTENANCE WORKING GROUP (APRIL 2007)

J. NEVEUX Airbus Central Entity Chairman

B. BOLOT AFR

T. STEVENS AFR

R. DILMAHAMOOD MAU

KC. MULONGA BMI

T. SIMHANI BMI

L. ZHIYONG CCA

M. DOWNEY CPA

M. OTTERSBACH Lufthansa Technik

D. FROEHLICH Lufthansa Technik

J. HAMILTON MYT

R. BOBEK NWA

D. MUTABDZIC SR Technics Switzerland

C. LOWEN VIR

D. DANIELS Airbus Deutschland

H. HEYDECKE Airbus Deutschland

S. KLAUBERT Airbus Deutschland

S. KLEMM Airbus Deutschland

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.36 H. LETMATHE Airbus Deutschland

F. SEEDORF Airbus Deutschland

A. TSCHAFFLER Airbus Deutschland

O. WEISS Airbus Deutschland

B. BOURDIEU Airbus Central Entity

L. BOYER Airbus Central Entity

F. BRETHES Airbus Central Entity

P. CARLE Airbus Central Entity

N. CHALOU Airbus Central Entity

V.GIRARD Airbus Central Entity

D. SORIA Airbus Central Entity

G. VIADER Airbus Central Entity

J. VESLOT Airbus Central Entity

H. ZITOUNI Airbus Central Entity

J. FOSTER Airbus UK

J. GOODRUM Airbus UK

D. SANZ-MERINO Airbus Spain

S. PENA-GONZALES Airbus Spain

MRB advisors

B. BACHA EASA

H. HOFFMAN FAA

POWERPLANT AND APU MAINTENANCE WORKING GROUP (APRIL 2007)

J. NICOLAS Airbus Central Entity Chairperson

Eric WOON SEK LAW AIR MAURITIUS

Wilfried ROELL Lufthansa Technik AG

Danilo COLOMBO Livingston Energy Flight SpA

Tommy STRAND Scandinavian Airlines System

Nilüfer KAYA Turkish Airlines

Emine Büsra YILMAZ Turkish Airlines

Martin SHARP MyTravel Aircraft Engineering Limited

Allan F RENNIE Thomas Cook Airlines UK Limited

Herbert DOENGES LTU

Karen MACCLURE NORTHWEST AIRLINES

Paul Eric GUSTAFFSON Finnair

Mike Fabritz Honeywell

Richard BARKLEY Rolls-Royce

Gary SANDERS Hamilton Sundstrand

Jean-Pierre MARQUET CFM Nacelle

Frederic OBRECHT CFM

Amine TAOURCHI Airbus Central Entity

Jean-Francois HUIX Airbus Central Entity

Raquel SANCHEZ-GARCIA Airbus Central Entity

Vincent FONDEVIOLE Airbus Central Entity

Stephane GIROUD-GARAPON Airbus Central Entity

Rafael MARIN SEBASTIAN Airbus Central Entity

Thibaut Marc Airbus Central Entity

Vincent Swiderski Airbus Central Entity

David SANZ-MERINO Airbus Spain

MRB advisors

Boualem BACHA EASA

Donald LEVESQUE FAA

# A340 MRB REPORT

Issue : July 2010 Page : APX 5.37

# This page is intentionally left blank

# A340 MRB REPORT

Issue : July 2010 Page : APX 6. 1 APPENDIX 6

GLOSSARY OF TERMS

ACCIDENTAL DAMAGE (AD) :

Physical deterioration of an item caused by contact or impact with an object or influence which is

not a part of the aircraft, or by human error during manufacturing, operation of the aircraft, or

maintenance practices.

AIRWORTHINESS LIMITATIONS :

A section of the Instructions for Continued Airworthiness that contains each mandatory

replacement time, structural inspection interval, and related structural inspection tasks. This

section may also be used to define a threshold for the fatigue related inspections and the need to

control corrosion to Level 1 or better. The information contained in the Airworthiness Limitations

section may be changed to reflect service and/or test experience or new analysis methods.

CERTIFICATION MAINTENANCE REQUIREMENT (CMR) :

A maintenance task with particular limitations arising from the Type Certification process.

DAMAGE TOLERANT :

A qualification standard for aircraft structure. An item is judged to be damage tolerant if it can

sustain damage and the remaining structure can withstand reasonable loads without structural

failure or excessive structural deformation until the damage is detected.

DISCARD :

The removal from service of an item at a specified life limit.

ENVIRONMENTAL DETERIORATION (ED) :

Physical deterioration of an item's strength or resistance to failure as a result of chemical

interaction with its climate or environment.

FATIGUE DAMAGE (FD) :

The initiation of a crack or cracks due to cyclic loading and subsequent propagation.

# A340 MRB REPORT

Issue : July 2010 Page : APX 6. 2 FUNCTIONAL CHECK :

A quantitative check to determine if one or more functions of an item performs within specified

limits.

INSPECTION - DETAILED :

An intensive visual examination of a specific structural area, system, installation or assembly to

detect damage, failure or irregularity. Available lighting is normally supplemented with a direct

source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors,

magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures

may be required.

INSPECTION - GENERAL VISUAL :

A visual examination of an interior or exterior area, installation or assembly to detect obvious

damage, failure or irregularity. This level of inspection is made from within touching distance

unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed

surfaces in the inspection area. This level of inspection is made under normally available lighting

conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or

opening of access panels or doors. Stands, ladders or platforms may be required to gain

proximity to the area being checked.

INSPECTION - SPECIAL DETAILED :

An intensive examination of a specific item, installation, or assembly to detect damage, failure or

irregularity. The examination is likely to make extensive use of specialised Inspection Techniques

and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be

required.

ITEM :

Any level of hardware assembly (i.e., system, sub-system, module, accessory, component, unit,

part, etc.).

LUBRICATION AND SERVICING :

Any act of lubricating or servicing for the purpose of maintaining inherent design capabilities.

MAINTENANCE SIGNIFICANT ITEM (MSI) :

Items identified by the manufacturer whose failure :

a) could affect safety (on ground or in flight), and/or

b) is undetectable during operations, and/or

c) could have significant operational impact, and/or

d) could have significant economic impact.

# A340 MRB REPORT

Issue : July 2010 Page : APX 6. 3 OPERATING CREW NORMAL DUTIES :

Operating Crew - Qualified cockpit and cabin attendant personnel who are on

duty

Normal Duties - Those duties associated with the routine operation of the

aircraft, on a daily basis, to include the following :

a) Procedures and checks performed during aircraft operation ;

b) Recognition of abnormalities or failures by the operating crew through the use

of normal physical senses (e.g., odor, noise, vibration, temperature, visual

observation of damage or failure, changes in physical input force requirements,

etc.).

OPERATIONAL CHECK :

An operational check is a task to determine that an item is fulfilling its intended purpose. Does

not require quantitative tolerances. This is a failure finding task.

OTHER STRUCTURE :

Structure which is judged not to be a Structural Significant Item. "Other Structure" is defined both

externally and internally within zonal boundaries.

RESTORATION :

That work necessary to return the item to a specific standard. Restoration may vary from

cleaning or replacement of single parts up to a complete overhaul.

STRUCTURAL SIGNIFICANT ITEM (SSI) :

Any detail, element or assembly, which contributes significantly to carrying flight, ground,

pressure or control loads and whose failure could affect the structural integrity necessary for the

safety of the aircraft.

TASKS - MAINTENANCE :

An action or set of actions required to achieve a desired outcome which restores an item to or

maintains an item in serviceable condition, including inspection and determination of condition.

THRESHOLD :

The initial accomplishment of a specific maintenance task expressed in flight cycle, flight hours,

and/or calendar time.

USAGE PARAMETER :

The unit of measure, Flight Hours (FH), Flight Cycles (FC), Calendar Time (HOURS, DAYS,

MONTHS, YEARS), Engine Cycles (CY) or APU HOURS, for inspection intervals where a letter

check is not appropriate.

# A340 MRB REPORT

Issue : July 2010 Page : APX 6. 4 VISUAL CHECK :

A visual check is an observation to determine that an item is fulfilling its intended purpose. Does

not require quantitative tolerances. This is a failure finding task.

# A340 MRB REPORT

Issue : July 2010 Page : APX 7. 1 APPENDIX 7

ABBREVIATIONS USED IN THE MRB REPORT

AAPS Ambient Absolute Pressure Sensor

A/C Aircraft

AC Alternating Current

ACARS Aircraft Communications Addressing & Reporting System

ACMS Aircraft Condition Monitoring System

ACP Audio Control Panel

ACT Additional Center Tank

ACMS Aircraft Condition Monitoring System

AD Accidental Damage

ADF Automatic Direction Finder

ADIRU Air Data / Inertial Reference Unit

ADR Air Data Reference

AEVC Avionics Equipment Ventilation Computer

AFT Average Flight Time

AH Apu Hours

ALI Airworthiness Limitation Item

AMM Aircraft Maintenance Manual

AOA Angle Of Attack

AP Autopilot

APU Auxiliary Power Unit

ARO Anti Roll Out

ASPSU Autonomous Standby Power Supply Unit

ATC Air Traffic Control

A/THR Autothrust

ATIMS Air Traffic And Information Management System

ATT Attitude

BAT Battery

BAC Bulk Avionics Compartment

BCRC Bulk Crew Rest Compartment

BITE Built In Test Equipment

CBB Connexion By Boeing

CPCP Corrosion Prevention And Control Program

CDU Center Drive Unit

CIDS Cabin Intercommunication Data System

CLG Center Landing Gear

CMR Certification Maintenance Requirement

CMS Central Maintenance System

CRR(C) Crew Rest Room (Cabin)

CRR(U) Crew Rest Room (Underfloor)

CSM/G Constant Speed Motor/Generator

CSU Command Sensor Unit

CVR Cockpit Voice Recorder

CY Cycles (Engine)

DAR Digital ACMS Recorder

DC Direct Current

DCR Dock on Crew Rest

DEU Decoder/Encoder Unit

DI Detailed Inspection

DFDR Digital Flight Data Recorder

DMC Display Management Computer

DME Distance Measuring Equipment

# A340 MRB REPORT

Issue : July 2010 Page : APX 7. 2 DS Discard

DY Days

EASA European Aviation Safety Agency

ECAM Electronic Centralised Aircraft Monitoring

ECAS Emergency Cabin Alert System

ECU Engine Control Unit

ED Environmental Deterioration

EDP Engine Driven Pump

EEC Engine Electronic Controller

EFCS Electrical Flight Control System

EFIS Electronic Flight Instrument System

EG Entrance Guide

ELT(AF) (Automatic Fixed) Emergency Transmitter LocatorEMCD Electric

Magnetic Chip Detector

EPSU Emergency Power Supply Unit

ERP Enhanced Runaway Protection

ESM Engine Shop Manual

ESS Essential

EVAC Evacuation

EWIS Electrical Wiring Interconnection System

FAA Federal Aviation Administration

F-BCRC Full Bulk Crew Rest Compartment

FADEC Full Authority Digital Engine Control

FANS Future Air Navigation System

FAR Federal Aviation Regulation

FC Flight Cycles

FC Functional Check

FCC FWD Cargo Compartment

FCRC Flight Crew Rest Compartment

FDU Fire Detection Unit

FEC Failure Effect Category

FH Flight Hours

FCMC Fuel Control And Monitoring Computer

FCMS Fuel Control And Monitoring System

FCPC Flight Control Primary Computer

FCSC Flight Control Secondary Computer

FD Fatigue Damage

FM Flight Management

FMCU Flow Metering Compact Unit

FMS Flow Metering System

FR Frame

FWC Flight Warning Computer

FWD Forward

GAC Galley Air Cooler

GCU Generator Control Unit

GE General Electric

GPWC Ground Proximity Warning Computer

GPWS Ground Proximity Warning System

GRP Group

GVI General Visual Inspection

HAPS Hydrostatic Absolute Pressure Sensor

HDG Heading

HF High Frequency

HIRF High Intensity Radiated Fields

HP High Pressure

# A340 MRB REPORT

Issue : July 2010 Page : APX 7. 3 HPT High Pressure Turbine

HRS Hours (Elapsed Time)

I Interval

IDG Integrated Drive Generator

IFE In Flight Entertainment

IFES In Flight Entertainment System

ILS Instrument Landing System

IN Inspection

IP Intermediate Pressure

IR Inertial Reference

JAA Joint Airworthiness Authorities

JAA Joint Aviation Authorities

JAR Joint Airworthiness Requirement

JAR Joint Aviation Requirement

KTS Knots – Nautical Miles Per Hour

LDL Lower Deck Lavatories

LDF Lower Deck Facilities

LDMCR Lower Deck Mobile Crew Rest

LGCIU Landing Gear Control And Interface Unit

LH Left Hand

LP Low Pressure

LPT Low Pressure Turbine

LU Lubrication

MCD Magnetic Chip Detector

MCDU Multi Control Display Unit

MLG Main Landing Gear

MO Months

MPD Maintenance Planning Document

MRB Maintenance Review Board

MRBR MRB Report

MSI Maintenance Significant Item

MSN Manufacturers Serial Number

MTHS Months

N/A Not Applicable

ND Navigation Display

NLG Nose Landing Gear

No Number

NR National Requirement

NT Note

NTM Non-Destructive Testing Manual

OP Operational

QAR Quick Access Recorder

PA Public Address

P/B SW Pushbutton Switch

P-BCRC Partial Bulk Crew Rest Compartment

PCU Power Control Unit

PDU Power Drive Unit

PFD Primary Flight Display

POB Pressure-OFF Brake

PTT Press To Test

# A340 MRB REPORT

Issue : July 2010 Page : APX 7. 4 PUA Air Pressurisation Unit

PW Pratt & Whitney

RAT Ram Air Turbine

RCC Remote Control Centre

RCT Rear Center Tank

RH Right Hand

RMP Radio Management Pane

lRS Restoration

RSVR Reservoir

RR Rolls Royce

RTA Rudder Trim Actuator

RTLU Rudder Travel Limitation Unit

RVSM Reduced Vertical Separation Minima

SB Service Bulletin

SDI Special Detailed Inspection

SIU Server Interface Unit

SMR Scheduled Maintenance Report

SRM Structure Repair Manual

SSA System Safety Assessment

SSI Structural Significant Item

ST Sample Threshold

STR Stringer

SV Servicing

T Threshold

TBO Time Between Overhaul

TCAS Traffic Collision Avoidance System

THS Trimmable Horizontal Stabiliser

TPIS Tyre Pressure Indication System

TPS Temporary Protection System

ULB Underwater Locator Beacon

VC Visual Check

VCC Video Control Center

VHF Very High Frequency

VOR Vhf Omnibearing Range

VR Vendor Recommendation

WGL-QAR/DAR Wireless Ground Link – Quick Access Recorder/Digital ACMS Recorder

WTB Wing Tip Brake

WV Weight Variant

YE Years

YRS Years

ZIP Zonal Inspection Program

# A340 MRB REPORT

Issue : July 2010 Page : APX 8.1 APPENDIX 8

STRUCTURES INSPECTION REPORTING SYSTEM

The Structural Inspection Report form provided overleaf may be used by operators/maintenance

organisations to report structural inspection results to Airbus. However investigations are in progress

to develop a means to transmit the required data electronically.

The following rules apply to the reporting:

a) A completed Structural Inspection Report is required any time a structurally significant defect

occurs.

b) The responsibility for reporting rests with the operator.

c) The reports should be sent to Airbus via the Resident Customer Support Manager or directly

to Airbus at the following address:

AIRBUS

Customer Service Directorate

Attn.: Department SEE - Structure Engineering

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

# A340 MRB REPORT

Issue : July 2010 Page : APX 8.2 

# AIRBUS Ref :



# Structural Inspection Report

A300 [ ] A310 [ ] A300-600 [ ] A319 [ ] A320 [ ] A321 [ ] A330 [ ] A340 [ ]

Date of inspection :

Operator Code : MSN : A/C FC :

Station : Registration : A/C FH :

Inspection : Task reference: ............................... (if available)

..............................

Inspection method used : General Visual [ ] X-ray [ ]

Detailed Visual [ ] Eddy Current [ ]

Ultrasonic [ ] Ultrasonic [ ]

Magnetic Particle [ ] Other [ ] ............

Reason for reporting/recording :

Level Temporary

Corrosion [ ] 1 [ ] 2 [ ] 3 [ ] Disbonding [ ] Protection

crack [ ] Composite damage [ ] System (TPS)

nil finding [ ] Other [ ] Visible :

Yes [ ] No [ ]

Location of damage :

Zone number : between stringer : and : LH[ ]/RH[ ]

ATA 100 code : between frame : and :

between rib : and : LH [ ]/RH[ ]

Part concerned :

Longeron/stringer [ ] chord [ ] rib [ ]

bracket/shear tie [ ] web [ ] bulkhead [ ]

frame [ ] skin [ ] fitting [ ]

other [ ] ................ doubler [ ]

Time since last maintenance task for concerned part : ........ Months ........ FC ........ FH

Repair Approval Sheet (RAS) number (if available) :

Extent of damage : (ref. to SRM 51.10.13/51.11.13 for criteria)

Length : mm [ ] inches [ ]

Width :

Depth :

Description of damage/cause of damage/corrective action :

(Additional photograph/details of findings to be provided if available)

Submitted by : Maintenance

Name : organization : Date :

# A340 MRB REPORT

Issue : July 2010 Page : APX9. 1 APPENDIX 9

HIRF/LIGHTNING PROTECTION

1 Background

During development of the initial A340 MRB Report, the MRB required the manufacturer to

identify an appropriate method by which to confir m that in-service operation will not reduce the

HIRF and Lightning protection to a level that is inadequate to maintain Type Certification

objectives.

Airbus has reached agreement with the MRB and the Aircraft Certification Offices of EASA, FAA

and Transport Canada that compliance with this request may be shown by a combination of two

methods:

a) Identification of dedicated maintenance tasks to supplement the inspections already

included in Sections C, D and E of the MRB Report. These additional tasks are to be

performed by operators on all A340 aircraft at defined intervals. They are listed in this

Appendix to the MRB Report and are approved by the MRB.

b) Identification of an A330/A340 ‘HIRF / Lightning Protection Assurance Plan’ that requires

the manufacturer to perform specific tests on a representative sample of the world

A330/A340 fleet at specified intervals. These tests and intervals are agreed with the

Aircraft Certification Offices . See paragraph 5 for further details.

Though the specific HIRF / Lightning related scheduled tasks are identified in an Appendix to the

MRB Report, operators are to consider them as MRB tasks and include them in their approved

maintenance programs.

2 HIRF and Lightning Protection – design concept

The coupling phenomena between lightning or HIRF and the aircraft give rise to induced threats

which can interfere with electrical / electronic systems.

HIRF has a real-time effect on systems but results in no residual damage. A HIRF encounter

cannot be detected after the event by a physical examination of hardware.

A Lightning encounter can result in permanent physical degradation of hardware as well as

possible real-time effects.

Aircraft protection against HIRF and Lightning indirect effects is achieved by complementary

means:

a) aircraft structure continuity

This continuity is ensured by metal to metal contact and bonding leads.

b) electrical wiring protection

In exposed areas, overshielding ensures protection of cables. This is provided by:

- raceways in wings

- braided conduits in the belly fairing, fin, tailplane, on engines, in tail cone

and landing gear area and at interface between pylon/wing and

wing/fuselage

# A340 MRB REPORT

Issue : July 2010 Page : APX9. 2 - individual shielding for engine cables (nacelle, pylon,wing)

c) equipment protection

In addition to the equipment inherent protection (circuit layout and box design), clamping

and filtering devices at inputs/outputs prevent damage from voltage/current resulting

from Lightning and HIRF.

d) systems architecture

Systems architecture is designed to achieve systems safety and availability objectives

and contributes to increasing the non-susceptibility of systems to HIRF and Lightning

effects. Main features are:

- segregation of electrical wiring routes

- different locations of equipment

- redundancy and dissimilarity

For the types of protection described in paragraphs a, b and c, appropriate means have

been determined to confirm the continued integrity of the features. The protection

described in paragraph d will not degrade and thus is not addressed.

3 Identification of dedicated tasks in this Appendix

At aircraft level, for each item or group of items providing HIRF/Lightning protection, the

following analysis has been performed:

a) from parameters such as type and location of protection element the consequence of

protection degradation has been assessed.

b) from design features such as material, installation techniques, etc, the causes of

degradation have been identified.

c) from the type of degradation foreseen, the location of items and their accessibility, the

most applicable and effective task to detect the discrepancy has been selected.

At equipment level, taking into account functional criticality, a dedicated review of components

fitted with Lightning protection devices that also act as HIRF protection has been performed.

Component Maintenance Manuals (CMMs) have been verified to include the need for

appropriate checks using Automatic Test Equipment (ATE) prior to re-release for service.

The tasks were not identified using an MSG-3 type logic approach.

4 Scheduled Maintenance philosophy

With respect to structure continuity, existing General Visual Inspections required by the Zonal

section (MRB Report Section E) are applicable and effective.

With respect to electrical wiring, analysis has highlighted that for some specific devices the GVI

required as part of the ZIP is not adequate to identify degradation of HIRF/Lightning protection.

For these design features, this Appendix identifies the need for either a dedicated GVI, a higher

level of inspection or a security check (tactile check) to ensure that degradation will be detected.

# A340 MRB REPORT

Issue : July 2010 Page : APX9. 3 The number of tasks required by this Appendix have been kept to a minimum and the type of

task has been identified as the least intrusive compatible with the target of identifying

degradation that causes a loss of protection below certification values.

The accomplishment procedures to satisfy the tasks are given in the Aircraft Maintenance

Manual. No task requires the disconnection of connectors or dismantling of fixations, restraints

or bonding leads though this may be necessary if there is evidence of degradation.

For the majority of the wiring installation, it is concluded that significant deterioration will be

identified and corrected during application of the existing Zonal section. To support this

conclusion, Airbus have agreed to establish a HIRF/Lightning Protection Assurance Plan (see

paragraph 5). Findings resulting from the activities detailed in this Plan will be used to justify

amendments to this Appendix.

Evolution or short term extension of ATA 20 tasks should be assessed in a similar way to Zonal

Inspections and calendar related structural inspections. They are not classified as either safety

or non-safety related. However, though intervals should be adjusted in accordance with

experience the tasks shall not be deleted from an operators program. It is expected that

escalations justified by good experience will be limited to a value necessary to maintain the task

in the same check package.

Short-term extensions or variations are permitted in exceptional circumstances as for other

scheduled maintenance tasks not subject to CN/AD action. The maximum value of these onetime extensions should be in accordance with local authority agreements.

5 HIRF/Lightning Protection Assurance Plan

The joint A330/A340 HIRF/Lightning Assurance Plan is required to:

a) monitor the effectiveness of the scheduled maintenance tasks identified in the MRB

Report and its Appendix 9 and identify any shortcomings

b) address the special requirements for HIRF/Lightning continuous airworthiness arising

from Type Certification issues

Airbus will measure, on selected aircraft, the level of electrical installation electromagnetic

protection. This level of protection will be compared to that of a new aircraft. Using a loop

resistance tester, a measurement is made of the impedance of a loop created by a protection

element (e.g. braided conduit or a raceway), its bonding to the aircraft structure and the aircraft

structure.

The initial sample size will be 8 aircraft. These will comprise a mix of five A330 and A340-

200/300 models plus three A340-500/600 from different climatic areas.

The tests will be performed at the opportunity of a 4C-check or 8C-check and will be repeated

on a different set of 8 aircraft every 6 years. Though the measurements must be accomplished

before any activity (such as cleaning) disturbs the protection elements and associated wiring,

they may be performed concurrently with other maintenance work.

Airbus is responsible for identifying appropriate aircraft and for making the initial contact with the

operator at least four months prior to 4C/8C-check accomplishment. All operators should be

prepared to provide an aircraft for these purposes. The tests will be performed by the

manufacturer over five days and can be carried out during the course of the 4C/8C-check.

A summary report of each set of tests will be submitted to the Type Certification Authorities and

the MRB. This may include recommendations for corrective action. Any changes proposed to

Appendix 9 will be handled as for other changes to the MRB Report.

# A340 MRB REPORT

Issue : July 2010 Page : APX9. 4 Details of the A330/A340 HIRF/Lightning Assurance Plan are given in document 524.5012-01

prepared by Airbus dept EYDVB.A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 520- 00- 01- 1 522622522AB 522BB 462DL 622AB622BB 472 ER4C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the following harnesses end fittings, from rib 9 torib 10A :- 7021VP, 7001VC- A, 7021VC- A, 7025VC- A, 10HA2, LH side- 7024VP, 7002VC-A, 7022VC-A, 7026VC-A, 10HA3, RH sideA340 -200/-30020- 00- 01- 2 523623523AB 452EL623AB 482ER2C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the following harnesses end fittings, from rib 24 torib 29:- 10HA1, 7003VC- A, 7013VC- A, 7015VC- A, 7023VC- A, 7033VCA, LH side- 10HA4, 7004VC- A, 7014VC- A, 7016VC- A, 7024VC- A, 7034VCA, RH sideA340 -200/-30020- 00- 01- 3 633 RAT extended 2C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the connectors located on the RATALLR 20- 00- 01- 4 523623523NB 575DB 535AB 535CZ623NB 675DB 635AB 635CZC WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of elements fitted on the following harnesses end fittings fromwing tip to rib 39:- 7621VB, 7623VB, 7625VB, 7627VB, LH side- 7622VB, 7624VB, 7626VB, 7628VB, RH sideA340 -200/-30020- 00- 01- 5 533633533AB 574CB 574DB 574EB574FB 533CB633AB 674CB 674DB 674EB674FB 633CBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of elements fitted on the following harnesses end fittings, fromrib19 to rib 14 :- 7633VB LH side- 7634VB RH sideA340 -200/-300A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 620- 00- 01- 6 531631531CB 573CB 573BB 573DB631CB 673CB 673BB 673DBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSDET inspection of elements fitted on the following harnesses endfittings, from rib 6 to fuselage :- 7651VB, 7681VB, 7683VB, LH side- 7652VB, 7682VB, 7684VB, RH sideA340 -200/-300PRE MOD 4316520- 00- 01- 7 571671Removal of fuel pump frontfairing2C WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of the following braided conduit end fittings, from rib 6 tofuselage :- 100QA1- A, 101QA1- A, 100QA2- A, 101QA2- A, LH side- 100QA3-A, 101QA3-A, 100QA4-A, 101QA4-A, RH sideA340 -200/-30020- 00- 01- 8 RESERVED20- 00- 01- 9 531631531CB 573CB 573BB 573DB631CB 673CB 673BB 673DBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSDET inspection of elements fitted on the following harnesses endfittings, from rib 6 to fuselage:- 7652VB, 7646VB, 7634VB, RH side- 7651VB, 7645VB, 7633VB, LH sideA340 -200/-300POST MOD4316520- 00- 01- 10 522622522AB622AB4C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the following harnesses end fittings, from rib 9 torib 10A :- 7001VC- A, 7021VC- A, 7025VC- A, LH side- 7008VC-A, 7022VC-A, 7026VC-A, RH sideA340 -500/-600A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 720- 00- 01- 11 523623523AB623AB2C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the following harnesses end fittings, from rib 24 torib 29:***** CONTINUED *****- 7003VC- A, 7013VC- A, 7015VC- A, 7023VC-A, 7029VC-A,7033VC-A LH side- 7004VC- A, 7014VC- A, 7016VC- A, 7024VC- A, 7034VC-A RHsideA340 -500/-60020- 00- 01- 12 523623575DB 575EB 523RB 535AB575CZ 535CB675EB 623RB 675DB 635AB635CZ 635CBSlats extendedC WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of elements fitted on the following harnesses end fittings fromwing tip to rib 41:- 7621VB, 7623VB, 7625VB, 7627VB, LH side- 7622VB, 7624VB, 7626VB, 7628VB, RH sideA340 -500/-60020- 00- 01- 13 533633573FB 573BB 573CB 573DB673BB 673CB 673DB 673FBFLAP TRACK FAIRING 2Flaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSDET of elements fitted on the following harnesses end fittings, fromrib 11 to fuselage :- 7633VB, 7645VB, 7639VB, 7651VB LH side- 7634VB, 7646VB,7640VB, 7652VB RH sideA340 -500/-60020- 00- 01- 14 191/192197/198Wing fillet fairings521AB 621AB4C WING ELECTRICAL WIRING PROTECTION ELEMENTSFunctional check of the following wing pressure seal bondings:3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503VP,3505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3744VP,3721VP, 3735VP, 3737VP, 3743VPA340 -200/-300PRE MOD 53665A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 820- 00- 01- 15 191/192197/198Wing fillet fairings521AB 621AB4C WING ELECTRICAL WIRING PROTECTION ELEMENTSFunctional check of the following wing pressure seal bondings:3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503VP,3505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3744VP,3721VP, 3735VP, 3737VP, 3743VP, 3204VP, 3207VP, 3208VP,3209VPA340 -500/-600PRE MOD 5366520- 00- 02- 1 311312312AR 2C SECTION 19 BRAIDED CONDUITSecurity check of the following harnesses end fittings at Fr. 87 :- 1CS- G, 1CS- HA340 -200/-30020- 00- 03- 1 193 193AB 2C BELLY FAIRING BRAIDED CONDUITGVI of elements fitted on the following harnesses end fittings, fromFr. 39 to Fr. 40.2 :- 1541VB, 1543VBA340 -200/-300R 20- 00- 03- 2 192 192EB 192QB 192GB 143AB193CB 193FB 193KB 195LB191BB2C BELLY FAIRING BRAIDED CONDUITGVI of elements fitted on the following harnesses end fittings, fromFr. 37 to Fr. 49 :- 1541VB, 1543VB, 1542VB, 1544VBA340 -500/-600R 20- 00- 03- 3 191192198191CB 198GB 192CB4C BELLY FAIRING BRAIDED CONDUITFunctional check of the following belly fairing pressure seal bonding:3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VPA340 -200/-300PRE MOD 5366520- 00- 03- 4 193195197198191CB, 192CB, 197EB198GB4C BELLY FAIRING BRAIDED CONDUITFunctional check of the following belly fairing pressure seal bonding:3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VP, 3201VP,3203VPA340 -500/-600PRE MOD 53665A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 920- 00- 04- 1 RESERVED20- 00- 05- 1 734744N/ A 2C MAIN LANDING GEAR BRAIDED CONDUITSecurity check of the end fittings at MLG braided conduitALL20- 00- 05- 2 734744N/ A 2C MAIN LANDING GEAR BRAIDED CONDUITDET inspection of elements fitted on the route 2M from union plate tointerface bracket on strut at MLG braided conduitALLD 20- 00- 05- 3 TASK DELETED20- 00- 06- 1 713714N/ A 2C NOSE LANDING GEARSecurity check of the following harnesses end fittings at NLG braidedconduit :- 1605VC-A, 1607VC-A, 2GH, 1GHPRE 4888220- 00- 06- 2 713714N/ A 2C NOSE LANDING GEARSecurity check of the following harnesses end fittings at NLG braidedconduit :- 1605VC-A, 1607VC-APOST 48882A340MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 1020- 00- 07- 1 323 A340-200/-300:325BL 325DL 312AR2C VERTICAL FINGVI of fly by wire protection installation at vertical fin:5994VB 5995VB 5996VB 5997VBPRE 4914420- 00- 07- 2 323 A340-200/-300:325BL 325DL 312ARA340-500/-600:312AR 311AZ 325SL 325NL313BL2C VERTICAL FINGVI of fly by wire protection installation at vertical fin5989VB 5994VB 5995VB 5996VB 5997VB 6989VB 6994VB 6996VBA340-200/300POST 49144ORA340-500/600

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 1 APPENDIX 10

MODIFICATION REFERENCE LIST



# This appendix provides the title of all modification numbers that are mentioned in the MRB report.

This is not a list of all modifications that have been assessed using MSG-3 methodology and thus

the absence of a modification does not necessarily imply that it has not been addressed.

MOD

NUMBER MOD TITLE

40063 AIR CONDITIONING-AVIONICS COMPARTMENT- DEFINE GROUND COOLING

UNIT INSTALLATION

40097 AIR CONDITIONING-DEFINE TEM PERATURE CONTROL OF FORWARD CARGO

COMPARTMENT

40123 FUSELAGE-CENTER FUSELAGE REINFORCE STRUCTURE

40219 AIR CONDITIONING - INTRODUCE OZONE CATALYTIC CONVERTERS

40243 WATER/WASTE-POTABLE WATER SYSTEM INTRODUCE INDEPENDANT

PRESSURIZATION

40255 NAVIGATION-ATC-INSTALL MODE S AND ANTENNAS DIVERSITY

40256 NAVIGATION - TCAS - INSTALL ALLIED SIGNAL TCAS II SYSTEM

40257 OXYGEN-PASSENGER OXYGEN-INSTALL SYSTEM PROVISIONS FOR FIVE

OXYGEN CYLINDERS GASEOUS SYSTEM

40260 EQUIPMENT/FURNISHINGS-CREW REST COMPARTMENT-INSTALL SYSTEM

PROVISIONS

40335 ICE AND RAIN PROTECTION-INSTALL GIRT BAR FITTING HEATING SYSTEM FOR

ENTRY DOORS

40336 EQUIPMENT/FURNISHINGS-EMERGENCY- DELETE EVAC SYSTEM

40347 FUSELAGE-NOSE FORWARD FUSELAGE MODIFY DOOR NR 1 SURROUND

40379 EQUIPMENT/FURNISHINGS-INSTALL PROVISIONS FOR AN UNDERFLOOR CREW

REST CONTAINER (BFE)

40391 GENERAL-INTRODUCE MINOR IMPROVEMENTS FROM A/C 29

40501 NAVIGATION-GPS-INSTALL WIRING PROVISIONS FOR A DUAL SYSTEM

40556 FUSELAGE-STUCTURE-IMPROVE FATIGUE PROPERTIES AT BUTT JOINTS

FRAME 58 AND 72, STRINGER P13-P'13

40597 WINGS-AILERON MAIN STRUCTURE-REINFORCE ACTUATOR ATTACHMENT

FITTING ON INNER AILERON

40610 WINGS-STRUCTURE-REDEFINE THE USE OF COLD WORKING

40611 EQUIPMENT/FURNISHINGS-UNDERFLOOR CREW REST ROOM-ADAPT

PROVISIONS FOR ST2 VERSIONS

40701 FLIGHT CONTROLS-FLAPS-INSTALL KAMATICS FLAP TRACK ROLLER

BEARINGS

40838 HYDRAULIC POWER-GREEN HYDRAULIC POWER-PROTECT GREEN

HYDRAULIC CIRCUIT AGAINST OUTER WING STRUCTURAL DAMAGE

40843 STABILIZER-VERTICAL STABILIZER-FINBOX- REINFORCE CFRP STRUCTURE

PARTS-SERIAL SOLUTION

40904 STABILIZERS-RUDDER-IMPROVED GFRP/CFRP COMPONENTS

41045 FUSELAGE - REAR FUSELAGE – IMPROVE SURROUNDING PANEL IN AREAS OF

CARGO DOOR CUT OUT CORNERS

41114 WINGS - OUTER WING MAIN STRUCTURE - MODIFY RIB 6 (AFT) TO DELETE

BUILD DOOR

41225 ENGINE-INTRODUCE CFM 56-C3 ENGINE

41300 WINGS-GENERAL-DEFINE A340 GROWTH VERSION

41323 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION-INSTALL LE

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 2 MOD

NUMBER MOD TITLE

BOZEC RECIRCULATION FILTERS

41371 NACELLES/PYLONS - PYLONS - MODIFY SEALS ON PYLON/WING FAIRINGS

41383 LANDING GEAR - MLG - BRAKING - FIT 3B STANDARD BSCU

41410 FUSELAGE-CENTRE FUSELAGE-CREATE ADDITIONAL ACCESS DOOR IN THE

FAIRING

41460 WINGS-WINGTIP STRUCTURE-INTRODUCE MINOR IMPROVEMENTS

41471 STABILIZERS-HORIZONTAL STABILIZER- MODIFY FRONT SPAR

41486 FLIGHT CONTROLS-RUDDER-INSTALL ON SECOND TRAVEL LMITER UNIT

41510 NAVIGATION-RADIO ALTIMETER-INSTALL COLLINS RADIO ALTIMETER SYSTEM

41535 DOORS-MAIN GEAR DOORS-REINFORCE CENTRAL HINGE

41600 FUEL-TRIM TRANSFER SYSTEM-FIT FORWARD TRANSFER PUMP IN THE TRIM

HORIZONTAL STABILIZER

41652 FUSELAGE-STRUCTURE-INTRODUCE A340 COMMONALITY ITEMS

41675 FUSELAGE-NOSE FORWARD FUSELAGE- REINFORCE STRINGER 12 AT FR 18

41714 GENERAL-ADAPTATION OF MSN 032 033 034 TO ALK1 VERSION

41833 COMMUNICATIONS-SATELLITE COMMUNICATIONS - INSTALL ALLIED

SIGNAL/DASSAULT ELECTRONIC HIGH RATE SECT.ANTENNA SYST.

41848 FUSELAGE - CENTER FUSELAGE – DEFINE STRUCTURAL REPERCUSSIONS

FOR GROWTH VERSIONS (SECT 15A)

41856 FUSELAGE - FORWARD FUSELAGE – DEFINE STRUTURAL REPERCUSSIONS

FOR GROWTH VERSIONS (SECT.13/14)

42069 FUSELAGE-FORWARD FUSELAGE-INTRODUCE ADDITIONAL ACCOUSTIC

INSULATION

42191 FUEL-FCMS-FIT FCMC WITH CHANGES FOR A330 TYPE CERTIFICATION AND

MINOR CHANGES A340

42226 ENGINE - INSTALL CFM 56-5C4 ENGINE

42274 WINGS-TRAILING EDGE-CHANGE TOP SKIN BOLTING IN CRITICAL AREAS TO

INTERFERENCE FIT (ADAPTATION SOLUTION)

42283 NACELLES/PYLONS - PYLONS - INTRODUCE AERODYNAMICALLY IMPROVED

PYLON FOR A340 GROWTH VERSIONS

42350 DOORS - PAX/EMERGENCY EXIT DOORS - IMPROVE STOP FITTINGS

42351 FUSELAGE-CENTER FUSELAGE-REINFORCE DOOR FRAMEWORK FOR TYPE

"A" DOOR

42352 FUSELAGE-CENTER FUSELAGE-REINFORCE DOOR FRAMEWORK-REINFORCE

DOOR FRAMEWORK FOR TYPE A DOOR (SERIAL SOLUTION)

42383 OXYGEN-PAX OXYGEN STORAGE-INTRODUCE MODIFIED TYPE 1 CONTAINER

42478 COMMUNICATIONS - CIDS - INTRODUCE CIDS VERSION 113

42481 FUSELAGE-GENERAL-IMPROVE UPPER PARTS OF FR 12 AND 13

42547 WINGS-STRUCTURE-INTRODUCE NEW INNER REAR SPAR MACHINING

42605 FUSELAGE-CENTER FUSELAGE-REINFORCE CENTER L/G DOOR JOINT

42606 FUSELAGE-CENTER FUSELAGE-REINFORCE VERTICAL BEAM IN ACTUATOR

FITTING AREA

42607 FUSELAGE - GENERAL – REINFORCE STRINGER 39 BETWEEN FR 53.2/FR 53.3

42612 FUEL-TANKS-INSTALL ONE ADDITIONALL CENTRE TANK

42704 WATER/WASTE - POTABLE - INSTALL FILTER FOR WATER SUPPLY IN EACH

LAVATORY.

42829 FUSELAGE - SECTION 11/12 – REINFORCE FRAME 10 LATERAL PART

42855 FUEL-GENERAL-INCREASE FUEL CAPACITY

42890 FUEL - APU FUEL PUMP SYSTEM – INTRODUCE SHORTENED SUCTION LINE IN

AIR SEPARATOR

42921 FUSELAGE - REAR FUSELAGE – INSTALL ADDITIONAL ACCESS DOOR FOR

DRAINAGE OF AIR SEPARATOR (RETROFIT SOLUTION)

42953 INDICATING/RECORDING SYSTEMS - ELECTRICAL CLOCK - INSTALL SMITH P/N

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 3 MOD

NUMBER MOD TITLE

2610-13

43021 A/S PART OF RETRO- SOLUTION IS COVERED UNDER MOD 43272

43069 LIGHTS - EMERGENCY LIGHTING SYSTEM -INSTALL MODIFIED EPSU

43165 ELECTRIC AND ELECTRONIC COMMON INSTALLATION – DELETE CONNECTORS

FROM INNER FLAPS

43142 INDICATING/RECORDING SYSTEMS –DEFINE PIN-PROGRAMMING FOR DLH2

VERSION

43183 NACELLES/PYLONS - GENERAL - MODIFY WING/PYLON FITTINGS

43260 NAVIGATION - RADIO ALTIMETER – INSTALL ALLIED SIGNAL QUANTUM LINE P/N

066.50007-0202 - (SFE)

43283 WINGS - STRUCTURE - FIT INTERFERENCE BOLTS AT STRINGERS 13 & 20

LOWER

43303 WINGS - INBOARD AND OUTBOARD FLAP - CHANGE MANUFACTURING

PROCESS OF CARRIAGE PARTS TRACK 1-5

43319 COMMUNICATION - PAX ADDRESS SYSTEM - CONNECT PA TO BATTERY BUS

BAR

43352 FUSELAGE - BELLY FAIRING – REINFORCE FR37-4 SUBSTRUCTURE

43363 STABILIZERS - VERTICAL STABILIZER CHANGE MANUFACTURING PROCEDURE

OF FIN BOX ATTACHMENT FITTINGS

43442 LANDING GEAR - NLG - INSTALL A WARNING SYSTEM IN COMPLIANCE WITH

JAR 25-745

43451 FUSELAGE -GENERAL-BELLY FAIRINGS-MODIFY THE ATTACHMENTS OF

STIFFENER 29 AT YL = - 1445 AND OF THE LOWER WEB AT FR 53.8

43463 WATER/WASTE - TOILET SYSTEM – INSTALL MODIFIED WASTE SEPARATOR

43491 STABILIZERS - HORIZONTAL STABILIZER - MOVE L/H LATERAL BOX BOUNDARY

OF THE TRIM TANK FROM RIB 19 TO 20

43560 COMMUNICATIONS – SATCOM - INSTALL SATCOM LOW GAIN ANTENNA

SYSTEM TOYOCOM

43577 FUSELAGE-CENTER FUSELAGE-MODIFY LOWER KEEL FITTING AND FORWARD

LOWER SHELL CONNECT.(RETROFIT SOLUTION VIA SB ONLY)

43652 COMMUNICATIONS - SATCOM – INSTALL TOP MOUNTED HIGH GAIN SATCOM

ANTENNA CANADIAN MARCONI

43683 FLIGHT CONTROLS - THSA – INTRODUCE COLLECTABLE DRAIN CONTAINER

43692 WINGS -STRUCTURE- FIT FATIGUE ENHANCED IRS ROOT JOINT AND NR 3 SKIN

PANEL TOP TO A340-300B FOR COMMONALITY

43727 FUSELAGE - FAIRING - EINFORCE LOWER WEB AND DOOR WEB JUNCTION AT

FR47 AT Y =-493 AND AT FR53.2

43750 AIR CONDITIONING - COCKPIT AND CABIN TEMPERATURE CONTROL -

INTRODUCE A SIX AREA TEMPERATURE CONTROL SYSTEM

43852 FUSELAGE - SECTION 15/21 – REINFORCE LONGITUDINAL SUPPORT BEAM AT

Y = +/- 1456 (PRODUCTION SOLUTION)

43865 WINGS - CENTER WING - MODIFY REAR SPAR

43904 FUSELAGE - CENTER FUSELAGE – UPPER FRAMES CHANGES AT THE

STRINGER HOLES (RETROFIT SOLUTION)

43956 COMMUNICATIONS - SATCOM - INSTALL BALL LOW GAIN ANTENNA AND

SPLITTER/COMBINER

44002 FUEL - TANKS - DEFINE SINGLE ACT INSTALLATION TO SUIT A340-200

44005 FUEL - TANKS - INSTALL A SECOND ADDITIONAL CENTRE TANK

44058 COMMUNICATION - CIDS – INTRODUCE IMPROVED NS/FSB SIGNS

44100 NAVIGATION - WEATHER RADAR SYSTEM - ACTIVATE DUAL PREDICTIVE

WINDSHEAR RADAR SYSTEM, COLLINS

44205 FUSELAGE - REAR FUSELAGE - DEFINE COMMOM STRUCTURE FOR SECTION

19

44245 WINGS - STRUCTURE - FIT NEW BOTTOM STRINGERS 10, 11, 12, 13, 14, 18 AND

19 AS CONTINUOUS STRINGERS

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 4 MOD

NUMBER MOD TITLE

44258 FUSELAGE - SECTION 12 STRUCTURE – FRAME OF PASSENGER DOOR NR 1 –

REINFORCE FRAME 16A LOWER AREA

44360 WING - CENTER WING - MODIFY FR40 AND FRONT SPAR

44385 FLIGHT CONTROLS - CONTROL INPUTS AND POWER SUPPLY - PROVIDE A

SECOND ELECTRICAL POWER SUPPLY TO FCPC3

44440 WINGS - CENTER WING - MODIFY LOWER KEEL FITTING AND FWD LOWER

SHELL CONNECTION

44442 FLIGHT CONTROLS - RUDDER TRAVEL LIMITATION UNIT - INSTALL NEW

STANDARD EQUIPMENT

44482 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION -

DEACTIVATE RAIN REPELLENT SYSTEM

44604 FUEL - APU FUEL PUMP SYSTEM – PREVENT AN ELECTRICAL ESS NETWORK

'OVERLOAD' (A340)

44620 COMMUNICATIONS-SATCOM-INSTALL BALL AEROSPACE HIGH GAIN ANTENNA

SYSTEM

44676 WINGS - LEADING EDGE - FIT TWO PART LOWER ACCESS PANEL AT TRACK

RIB 10

44729 AIR CONDITIONING - TEMPER ATURE CONTROL - RELOCATE CABIN

TEMPERATURE SENSOR

44754 NAVIGATION - WEATHER RADAR SYSTEM - ACTIVATE ALLIED SIGNAL

PREDICTIVE WINDSHEAR FUNCTION

44818 STABILIZERS - HORIZONTAL STABILIZER - REAR SPAR OF LATERAL BOX -

PROVIDE AN INSPECTION ACCESS

44826 FUSELAGE - FORWARD FUSELAGE- MODIFY ACOUSTIC INSULATION

44950 FUSELAGE - NOSE FORWARD FUSELAGE - INSTALL NEW GENERATION OF

RADOME USING QUARTZ MATERIAL

45022 NAVIGATION - RADIO ALTIMETER - INSTALL NEW THOMPSON ERT 540 RADIO

ALTIMETER STANDARD

45081 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION -

INTRODUCE NEW RECIRCULATION FILTER ELEMENTS

45293 FUSELAGE - FORWARD FUSELAGE - REINFORCE PAX DOOR II CUT-OUT

CORNER AREAS

45300 LANDING GEAR - CENTER LANDING GEAR - INSTALL "Y" LINK ON THE LH SIDE

THE CENTERLINE GEAR

45326 WINGS - INBOARD FLAP – INTRODUCE SIMPLIFIED SUPPORT 1 ASSEMBLY

45415 WINGS - STRUCTURE - REPLACE CLEARANCE FIT BOLTS WITH INTERFERENCE

FIT BOLTS AT CENTRE SPAR/STRINGER 15 JOINT

45503 COMMUNICATIONS - SATCOM – IMPROVE ALLIED SIGNAL/DASSAULT ANTENNA

INSTALLATION

45512 FLIGHT CONTROLS - AILERON – IN TRODUCE SERVO CONTROLS TO ECP-9 STD

45535 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION – TREAT

WINDSHIELD WITH PPG WATERPHOBIC COATING

45556 EQUIPMENT/FURNISHINGS-PAX COMPARTMENT- IMPROVE LAVATORY

MODULES

45578 FLIGHT CONTROLS - THSA – ADAPT COLLECTABLE DRAIN CONTAINER TO NEW

SECT. 19

45670 EQUIPMENT/FURNISHINGS - DOOR AREA FLOOR PANEL HEATING -

INTRODUCE HEATING ELEMENTS FOR PAX DOORS 1, 2, 3, 4

45739 WINGS - TRAILING EDGE – REPLACE CLEARANCE FIT BOLTS BY

INTERFERENCE FIT BOLTS

45749 FUSELAGE - CENTER FUSELAGE – REINFORCE FR40/ST18 JUNCTION

45968 FUSELAGE - GENERAL - INTRODUCE MINOR IMPROVEMENTS IN A/S PART

46025 FUSELAGE - REAR FUSELAGE SECT. 16 - REINFORCE LOWER SKIN PANEL FOR

INSTALL. OF VHF2 ANTENNA

46110 WINGS - STRUCTURE - PANEL NO.3 TOP -EXTEND LIFE OF REAR SPAR

FLANGE/TOP SKIN BOLT HOLES BETWEEN RIBS 2-7

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 5 MOD

NUMBER MOD TITLE

46111 WINGS - STRUCTURE - PANEL NO.3 TOP -EXTEND LIFE OF REAR SPAR

FLANGE/TOP SKIN BOLT HOLES BETWEEN RIBS 9-11

46135 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - INTRODUCE AN AIR FILTER

IN LAVATORY AIR EXTRACTION HOUSING

46141 WINGS - MAIN STRUCTURE - INNER REAR SPAR - COLD WORK WIRE HARNESS

SLOT RIB 4-5

46190 FUSELAGE - CENTER FUSELAGE – MODIFY CLG MOUNTING FITTING Y+/-450

46231 EQUIPMENT/FURNISHINGS - DOOR AREA FLOOR PANEL HEATING -

INTRODUCE HEATING ELEMENTS FOR PAX DOORS 1, 2, 3, 4

46241 WINGS - TRAILING EDGE – REPLACE CLEARANCE FIT BOLTS BY

INTERFERENCE FIT BOLTS

46307 FUSELAGE - CENTER FUSELAGE – REINFORCE FR40/ST18 JUNCTION

46386 AIR CONDITIONING - AVIONICS EQUIPMENT GROUND COOLING - IMPROVE

GRU LOGICS

46441 FUSELAGE - GENERAL - INTRODUCE MINOR IMPROVEMENTS IN A/S PART

46636 FUSELAGE - REAR FUSELAGE SECT. 16 - REINFORCE LOWER SKIN PANEL FOR

INSTALL. OF VHF2 ANTENNA

46730 WINGS - STRUCTURE - PANEL NO.3 TOP -EXTEND LIFE OF REAR SPAR

FLANGE/TOP SKIN BOLT HOLES BETWEEN RIBS 2-7

46772 WINGS - STRUCTURE - PANEL NO.3 TOP -EXTEND LIFE OF REAR SPAR

FLANGE/TOP SKIN BOLT HOLES BETWEEN RIBS 9-11

46849 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - INTRODUCE AN AIR FILTER

IN LAVATORY AIR EXTRACTION HOUSING

46900 WINGS - MAIN STRUCTURE - INNER REAR SPAR - COLD WORK WIRE HARNESS

SLOT RIB 4-5

46972 FUSELAGE - CENTER FUSELAGE – MODIFY CLG MOUNTING FITTING Y+/-450

46975 EQUIPMENT/FURNISHINGS -PASSENGER COMPT. SEATS - INTRODUCE IN-SEAT

POWER SUPPLY SYSTEM (ISPSS) 15V DC (VENDOR K.I.D.)

46996 E/F-PASSENGER COMPARTMENT SEATS - INTRODUCE IN-SEAT POWER

SUPPLY SYSTEM (ISPSS) 15V (VENDOR P.L. PORTER)

47019 GENERAL - ELECTRIC AND ELECTRONIC COMMON INSTALLATION - ADAPT

DEFINITION FOR A340-500/600

47021 FUSELAGE - CENTER FUSELAGE – ADAPT SECTION 15/21 FOR A340-500

47041 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER (THS) - DEFINE

NEW THSA FOR A340-500/600

47050 DOORS - PAX AND EMERGENCY EXIT DOORS - DEFINE REPERCUSSIONS FOR

OVERWING EMERG. EXIT DOORS FOR A340-600

47057 COMMUNICATIONS - GENERAL - ADAPT ATA 23 CABIN SYSTEMS FOR A340-

500/600

47063 AIR CONDITIONING - GENERAL - ADAPT BASIC DEFINITION FOR A340-500/600

47086 WATER/WASTE - GENERAL - DEFINE THE BASIC SYSTEM FOR A340-500/600

47159 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION-INSTALL LE

BOZEC RECIRCULATION FILTERS FOR A340-600

47197 EQUIPMENT/FURNISHINGS - CREW REST ROOM - INSTALL SYST PROV FOR

UNDERFLOOR BULK CREW REST COMPARTMENT (7 BED SOLUTION)

47210 LANDING GEAR - ALTERNATE BRAKING - INSTALL BRAKE DUAL DISTRIBUTION

VALVE WITH MODIFIED COVER

47244 NAVIGATION-STANDBY NAVIGATION SYSTEMS- INSTALL SEXTANT AVIONICS

INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)

47245 NAVIGATION - ADF - NOT TO INSTALL ADF RECEIVERS AND ASSOCIATED

ANTENNAS

47297 ENGINE FUEL AND CONTROL - CONTROLLING - INSTALL FADEC SOFTWARE

STD C3G

47372 WINGS - T/E AND TRAILING EDGE DEVICES - INSTALL NEW KAMATICS SELFLUBRIFICATING TRACK ROLLERS AT TRACK 1-5

47433 FLIGHT CONTROLS - AILERON AND HYDRAULIC ACTUATION - INTRODUCE

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 6 MOD

NUMBER MOD TITLE

ROLLER BEARING ON AILERON SERVOCONTROL

47482 NAVIGATION - ADF-INSTALL ADF1 RECEIVER 900 SERIES COLLINS P/N 822-

0299-020 (A340-600/500)

47524 INDICATING/RECORDING SYSTEMS-ELECTRONIC INSTRUMENT SYSTEM -

INSTALL NEW DISPLAY SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES)

47549 EQUIPMENT/FURNISHINGS - CREW REST ROOM (UNDERFLOOR) - DELETE

AUTOMATIC FIRE EXTINGUISHING SYSTEM INSIDE LDMCR

47625 HYDRAULIC POWER - MAIN HYDRAULIC POWER - A DAPT AIR PRESSURIZATION

UNIT

47674 FLIGHT CONTROLS -ELEVATOR AND HYDRAULIC ACTUATION -INTRODUCE ROD

EYE END ROLLER

BEARING ON ELEVATOR SERVOCONTROL

47798 WINGS - INBOARD FLAP - OPTIMIZE INBOARD FLAP DESIGN

47883 E/F - CREW REST ROOM - INSTALL SYSTEM PROVISIONS FOR A FIXED CREW

REST IN THE BULK COMPARTMENT

47928 INDICATING/RECORDING SYSTEMS – EIS - INSTALL DISPLAY UNITS WITH

VIDEO CAPACITY

47968 FUEL - TANKS - INSTALL A SEVEN-FRAME REAR CENTER TANK

48221 FLIGHT CONTROLS - AILERON AND HYDRAULIC ACTUATION - INTRODUCE

SERVO CONTROLS TOECP-11 STD

48239 LIGHTS - CABIN EMERGENCY LIGHTING - REPLACE FLOOR PATH MARKING BY

PHOTOLUMINISCENT FLOOR PATH MARKING SYSTEM

48437 WINGS - MAIN STRUCTURE - INTRODUCE NEW MATERIAL FOR WING TOP

SKINS AND STRINGERS

48442 FUSELAGE - REAR FUSELAGE - INCREASE OUTER DOUBLER FOR VHF2

ANTENNA IN SECTION 16

48451 EQUIPMENT/FURNISHINGS-PAX COMPARTMENT- DEFINE GALLEY COOLING

SYSTEM WITH LIQUID COOLANT

48634 FUSELAGE - REAR FUSELAGE - COLDWORK CARGO DOOR FRAME TO

INCREASE THE FATIGUE BEHAVIOUR

48635 OXYGEN PASSENGER OXYGEN - INSTALLATION OF A GASEOUS OXYGEN

SYSTEM FOR A340-500

48728 OXYGEN PASSENGER OXYGEN - INSTALLATION OF A GASEOUS OXYGEN

SYSTEM FOR A340-600

48744 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION-INTRODUCE

ODOR RECIRCULATION FILTER ELEMENTS (A340-600)

48769 NACELLES/PYLONS - GENERAL - REDUCE THICKNESS OF TITANIUM LATERAL

PANELS

48823 COMMUNICATIONS - GENERAL - A DAPT ATA 23 CABIN SYSTEMS FOR ENHANCED

CABIN A330/A340-300

48980 FUSELAGE - GENERAL - REAR FUSELAGE INTRODUCE CFRP PRESSURE BULKHEAD

FRAME

49008 WINGS - INBOARD FLAP - INTRODUCE A3456 INBOARD FLAP FOR A330/A340 BASIC

AIRCRAFT

49144 FLIGHT CONTROLS - ELECTRICAL FLIG HT CONTROL SYSTEM (EFCS) - INSTALL

RUDDER FLY-BY WIRE ON A330/A340

49194 FUSELAGE - FORWARD FUSELAGE - REINFORCESECTION 11/12

49202 FUSELAGE - CENTER FUSELAGE - REINFORCE SECTION 15/21

49203 NACELLES/PYLONS - PYLONS - REINFORCE PRIMARY STRUCTURE

49205 DOORS - CARGO - REMOVE BULK CARGO DOOR (IMPROVED SOLUTION)

49288 DOORS - CARGO - REMOVE BULK CARGO DOOR (NORMAL SOLUTION)

49353 WINGS - TRAILING EDGE - INTRODUCE REVISED MAIN LANDING GEAR BUSHES AT

AFT ATTACHMENT FITTING

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 7 MOD

NUMBER MOD TITLE

49404 FUSELAGE - CENTER FUSELAGE - REINFORCE AREA OF FRAME 40.3 TO 45, STR 26

TO 29 FOR MAINTENANCE TASK IMPROVEMENT

49444 FLIGHT CONTROLS - FLAPS - REPLACE FLAP TRACK ROLLER BY SELF

LUBRICATING ROLLERBEARINGS MANUFACTURED BY KAMATICS

49520 AIR CONDITIONING - CENTER FUSELAGE - INSTALL HEATSHIELDS IN BELLY

FAIRING TO SEGREGATE AIR SYSTEM

49657 EQUIPMENT/FURNISHINGS - CREW REST ROOM - INSTALL A CUSTOMIZED LDF IN

AFT LOWER DECK COMPARTMENT FOR DLH05

49769 NAVIGATION - ATC - INSTALL REMOTE ATC CONTROL BOX

49705 WATER/WASTE - WASTE WATER DRAIN - INSTALL A NEW DRAIN ASSY FOR A340-

500/600 AND ENHANCED CABIN

49951 WATER/WASTE - POTABLE - INSTALL A NEW POTABLE WATER FILTER IN EACH

LAVATORY

50014 EQUIPMENT/FURNISHINGS - COCKPIT - INSTALL AN ARMOURED COCKPIT DOOR

50088 WATER/WASTE - POTABLE - INSTALL INFRA RED WATER FAUCETS TOGETHER WITH

CHOOSEABLE DRAIN ASSY.

50108 EQUIPMENT/FURNISHING - CREW REST ROOM - DEFINE PARTIAL BCRC

PROVISIONS FOR ENHANCEMENT PROGRAM

50138 FLIGHT CONTROLS - SLATS – INTRO DUCE ROTARY ACTUATOR WITH IMPROVED

TORQUE LIMITER PERFORMANCE

50156 COMMUNICATIONS - CIDS - INSTALL COCKPIT CREW TO CABIN CREW ALERTING

SYSTEM

50157 COMMUNICATIONS - CIDS - INSTALL CABIN CREW TO COCKPIT CREW ALERTING

SYSTEM

50161 INDICATING/RECORDING SYSTEM - EIS - INSTALL NEW EIS2 STANDARD L3-1

(DMC, DU AND DISKS)

50213 AIR CONDITIONING - FLOW CONTROL AND INDICATING - INTRODUCE IMPROVED

FCV WITH FILTER

50217 FUSELAGE - CENTER FUSELAGE KEEL BEAM - REPLACE NUT STRIPS

50436 FLIGHT CONTROLS -FLAPS -REPLACE FLAP TRACK ROLLER BEARINGS ALTERNATE

EQPT MANUFACTURED BY TORRINGTON

50453 NAVIGATION - DDRMI - INSTALL UPDATED DDRMI WITH NEW TRANSFORMER

50471 FLIGHT CONTROLS - SLATS – INTRO DUCE ROTARY ACTUATOR WITH IMPROVED

TORQUE LIMITER ASSEMBLY

50675 FUSELAGE - FAIRINGS - USE OF TITANIUM ON 31 BELLY FAIRING PART

50676 OIL - GENERAL - INHIBIT ELECTRICAL MASTER CHIP DETECTOR (EMCD) FUNCTION

FOR RR T500 FIRST ENGINE

50723 DOORS - COCKPIT DOOR RELEASE SYSTEM - OVERRIDE ELECTRICAL SYSTEM

50745 FUSELAGE - DEFINE FATIGUE MAINTENANCE TASKS BASED ON FATIGUE

TEST/TEARDOWN/ IN SERVICE FINDINGS

50860 NAVIGATION - ADF - INSTALL ADF1 900 COLLINS RECEIVER

50990 FUSELAGE - CENTER FUSELAGE - INSTALL LINERS BETWEEN RCT FORWARD AND

REAR PRESSURE BULKHEAD (7 INTER-FRAMES)

51066 FUSELAGE - GENERAL - BELLY FAIRING - CHANGE PART MATERIAL

51336 AIR CONDITIONNING - AVIONICS EQUIPMENT GROUND COOLING - DE- A CTIVATE

THE GROUND REFRIGERATION UNIT (GRU)

51337 AIR CONDITIONNING - AVIONICS EQUIPMENT GROUND COOLING - REMOVE THE

GROUND REFRIGERATION UNIT (GRU)

51344 FUSELAGE - CENTER FUSELAGE - INSTALL LINERS BETWEEN RCT FORWARD AND

REAR PRESSURE BULKHEADS (5 INTER-FRAMES)

51454 EQUIPMENT/FURNISHINGS – CARGO COMPARTMENTS - IMPROVE ULD SUPPORT IN

THE AREA OF YZ-LATCHES - A340-500

# A340 MRB REPORT

Issue : July 2010 Page : APX 10. 8 MOD

NUMBER MOD TITLE

51992 EQUIPMENT/FURNISHINGS - CREW REST ROOM - INSTALL FIXED BULK CREW

REST COMPT. (PBCRC) PARTIAL USE FOR IBE06 VERSION

52634 EQUIPMENT/FURNISHINGS - CREW REST ROOM - INSTALL UNDERFLOOR FULL

BULK CREW REST COMPARTMENT

52635 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION - INTRODUCE

ODOR RECIRCULATION FILTER ELEMENTS (A340-500)

52911 FUSELAGE - CENTER FUSELAGE - REINFORCE STTRUCTURE TO IMPROVE FATIGUE

MAINTENANCE TASK

53033 WATER/WASTE - TOILET SYSTEM - INTRODUCE NEW WASTE TANKS

53123 DOORS - COCKPIT DOOR RELEASE SYSTEM- ELECTRICAL BACK- UP SYSTEM

53220 EQUIPMENT/FURNISHINGS - CREW REST ROOM (UNDERFLOOR) - INSTALL A BULK

CREW REST COMPARTMENT FOR THA04 VERSION

53522 NAVIGATION - ATC/MODE S - DEACTIVATE RATC FUNCTION

53622 NAVIGATION - SWITCHING AND INDICATING - REMOVE DDRMI INDICATORS

54128 COMMUNICATIONS - SATELLITE TV/DATA TRANSCEIVER SYSTEM (INCL.

TERRESTRIAL TV) - INSTALL TAILWIND 560 SYSTEM MOD CLOSURE : STAGE 3

54173 STABILISERS-HORIZONTAL STABILISER - INCREASE CAPACITY OF FUEL TANK

54880 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED

THSA (P/N 47172-500) FOR SB ONLY

54881 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED

THSA (P/N 47147-700) FOR SB ONLY

54882 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED

THSA (P/N 47175-500)

55652 WINGS - TRAILING EDGE AND TRAILING EDGEDEVICES-CHANGE SEMI MATERIALS

FOR PARTSOF FLAP TRACK 2, 3, 4 AND 5.

55780 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE MODIFIED

THSA (P/N 47172-510)

56234 PNEUMATIC - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - INTRODUCE

NEW CRISSAIR APU CHECK VALVE

55606 OXYGEN - PASSENGER OXYGEN - INSTALL A GASEOUS OXYGEN SYSTEM

FOR A340-300 ENHANCED

56234 PNEUMATIC - APU BLEED AIR SUPPLY AND CROSSBLEED SYSTEMS - INTRODUCE

NEW CRISSAIR APU CHECK VALVE

56284 ENGINE - GENERAL - A CTIVATE ELECTRONIC MAGNETIC CHIP DETECTOR (EMCD)

FUNCTION ON IN-SERVICE RRT700 ENGINES

56418 FUSELAGE - BELLY FAIRING - CHANGE PART MATERIAL (RETROFIT SOLUTION)

# This page is intentionally left blank

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.1 APPENDIX 11

LANDING GEAR OVERHAUL / RESTORATION INTERVAL REQUIREMENTS

1. INTRODUCTION

2. A340-200/300 MAIN LANDING GEAR

3. A340-200/300 NOSE LANDING GEAR

4. A340-200/300 CENTRE LANDING GEAR

5. LANDING GEAR SAMPLING POLICY

1. INTRODUCTION

This Appendix summarises the requirements to justify the Time Between Overhaul (TBO) interval for

restoration of the A340-200/300 Nose Landing Gear (NLG), Centre Landing Gear (CLG) and Main

Landing Gear (MLG).

The interval selected for restoration of A340-200/300 MLG and NLG is 10 years or 17,000FC,

whichever occurs first.

The interval selected for restoration of A340-200/300 CLG is 10 years or 12,000FC, whichever occurs

first.

The above intervals are dependent on the Inspection and Lubrication requirements stated in Paragraph

a) of Sections 2, 3 & 4.

Any new or modified requirements in this Appendix are not retrospective. They are to be applied from

receipt of MRBR Rev 11. If operators wish to deviate from these requirements, they must consult with

Airbus and Messier-Dowty to determine the impact on the overhaul and work with their own

airworthiness authorities for approval.

Airbus and Messier-Dowty have reviewed all A340-200/300 Landing Gear ‘recommended’ Vendor

Service Bulletins that introduce new or modified parts, and have a significant impact on the Landing

Gear. Airbus and Messier-Dowty recommend that they are considered by A340-200/300 operators for

accomplishment, either prior to overhaul or at overhaul. The aim of embodiment is to improve

operational reliability and minimize component degradation and replacement/repair cost at overhaul.

The criteria used to determine the selection of these ‘recommended’ VSB’s included:

• Improved corrosion resistance (protective coating/base metal);

• Improved lubrication;

• Significant economical and/or operational impact if not performed;

• In service data and overhaul findings;

• VSB’s that are not mandated by AD or ALS Pt1 limitations;

• Latest VSB’s that have superseded earlier versions.

The ‘recommended’ VSB’s that have been selected are listed in Sections 2, 3 and 4, Paras b) and c).

Items requiring additional Sampling are listed in Sections 2 & 3 Paras d) and e), and Section 4, Para d).

The Landing Gear Sampling Policy is stated in Section 5.

The requirements stated in Sections 2, 3 & 4 are temporary. Following a working group review, they are

expected to be superseded by new or revised tasks in MRBR rev 12.

2. A340-200/300 MAIN LANDING GEARA340 MRB REPORTIssue: July, 2010 Page: APX 11.2a) MLG Required Inspection and Lubrication Tasks.The following inspection and lubrication tasks are required to be performed to achieve the overhaul intervals stated above. Where applicable, a source document is stated.However, where there is no source document, ‘MRBR APX 11’ is stated as a reference. ‘MRBR APX 11’ is also stated as an additional reference, where a new interval hasbeen introduced compared to the existing source document.These tasks will be assessed through the MSG3 analyses, discussed in a dedicated Landing Gear working group meeting and may beintegrated into the MRBR in asubsequent revision.Item/ComponentPartNumberComments / Reason Task Applicability Threshold/IntervalSource documents AircraftconfigurationShorteningMechanismAdjustable Link201479001 Inspection for crackson eye endsDetailed Inspection ofAdjustable Link Upperand Lower Eye EndsPre Mod 49358(A340-32-4173)Threshold: 3 YEInterval: 700FHISBA340-32-4171(MPD 321100-22-1)Weight OnWheelsMLGUplockRoller201275759201489624201489308Evidence of stresscorrosion found onMLG Uplock RollerInspection of MLGUplock Roller forevidence of corrosionPre Mod50959(A340-32-4202)Threshold: 5 YEor 25,000FHInterval: 5 YE or25,000FHISBA340-32-4220Weight OnWheelsBogiePivot Pin201269612201489621201454925201489751Prevention of ChromeDamageReduced LubricationintervalAll 250FC or 4MO SIL 32-114(M-D SL A33/34-A6)MRBR APX 11(MPD 321000-04-1)Weight OnWheelsBrakedAxle201272644201272649Evidence of corrosionfound on AxleDetailed Inspection ofAxle Outer DiameterAll 1Cor at opportunityof Brake changeSIL 32-088MRBR APX 11(MPD 324100-05-1)Weight offWheelsMLG BogiePivot Pin201269612201489621201454925201489751In-service issueregarding chromeloss and corrosionIn-service data collectionon Bogie Pivot PininspectionAll At opportunity ofBogie Pivot PinremovalVendor Service LetterA33-34/A26MRBR APX 11Weight OffWheelsMLGBellcrank20148300/30120148353/35420158306/30720158300/301In-service issueregarding introducinggrease to theBellcrankDetailedProcedure forLubricating theBellcrankAll 250FC or 4 MOVendor Service LetterA33-34/A27MRBR APX 11Weight OnWheelsSM 8 Pin201275789201478617In-service issue:bush migrationReduced LubricationintervalAll 250FC or 4MO MRBR APX 11(MRBR task 32.11.00/01)Weight OnWheelsSM 9 Pin 201275790201478616In-service issue:bush migrationReduced LubricationintervalAll 250FC or 4MO MRBR APX 11(MRBR task 32.11.00/01)Weight OnWheelsA340 MRB REPORTIssue: July, 2010 Page: APX 11.3b) MLG modifications recommended to be accomplished prior to a 10 year TBOAirbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended product improvementmodifications prior to Main LandingGear overhaul. The benefit to the operator will be an improved operational reliability of the post mod parts and a lower levelof degradation at overhaul.Vendor ServiceBulletinReferenceAirbusService BulletinReferenceModNumberThreshold/IntervalDescriptionIntroduced asStandard inProductionFrom MSN:CommentsA33/34-32-171 A340-32-4173 49358 3 years fromEISIntroduce new adjustable link assembly(201254 Series – Basic Gear)MSN 435 Inspection task applicablefor pre mod statusA33/34-32-172 A340-32-4173 49358 3 years fromEISIntroduce new adjustable link assembly(201489 Series – Growth Gear)MSN 435 Inspection task applicablefor pre mod statusA33/34-32-197 A340-32-4178 49664 4 years fromEISNew Shortening Mechanism connectinglink(201254 Series – Basic Gear)MSN 454 There is no Inspection taskapplicable for pre mod, asstress corrosion is noteasily detectable Requiresjackingfor replacement.A33/34-32-198 A340-32-4178 49664 4 years fromEISNew Shortening Mechanism connectinglink(201489 Series – Growth Gear)MSN 454 There is no Inspection taskapplicable for pre mod, asstress corrosion is noteasily detectable Requiresjacking for replacement.A340 MRB REPORTIssue: July, 2010 Page: APX 11.4c) MLG modifications recommended to be accomplished at the 10 year overhaulBased on in-service data, Airbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended product improvement modificationsat first overhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a lower level of degradation atsecond overhaul.VendorServiceBulletinReferenceAirbus ServiceBulletinReferenceModNumberDescription Introduced asStandard inProductionFrom MSN:CommentsA33/34-32-153 A340-32-4153 47523 New Aluminum Piston with Nickel under ChromeOxide coating (201254 Series – Basic Gear)MSN 315 All in-service parts post mod.A33/34-32-154 A340-32-4153 47523 New Aluminum Piston with Nickel under ChromeOxide coating (201489 Series – Growth Gear)MSN 315 All in-service parts post mod.A33/34-32-175 A340-32-4166 48246 New Bushes in Bogie Beam & Slider(201254 Series – Basic Gear)MSN 366 Bushes replaced with lateststandard at overhaulA33/34-32-176 A340-32-4166 48246 New Bushes in Bogie Beam & Slider(201489 Series – Growth Gear)MSN 366 Bushes replaced with lateststandard at overhaulA33/34-32-190 A340-32-4181 49777 Improved corrosion protection for Retraction Link &‘W’ Pin(201254 Series–Basic Gear)MSN 454 Improved protective coatingapplied at overhaulA33/34-32-191 A340-32-4181 49777 Improved corrosion protection for Retraction Link &‘W’ Pin(201489 Series–Growth Gear)MSN 454 Improved protective coatingapplied at overhaulA33/34-32-193 A340-32-4180 49806 New Axle with Additional Corrosion Protection(201254 Series–Basic Gear)MSN 459 Application of top coat paint overSermetalA33/34-32-194 A340-32-4180 49806 New Axle with Additional Corrosion Protection(201489 Series–Growth Gear)MSN 459 Application of top coat paint overSermetalA33/34-32-195 A340-32-4202 50959 Modified Uplock Roller assembly & new bolts(201254 Series – Basic Gear)MSN 527 Basic Main Fitting replaced atoverhaul to include new UplockRoller Assembly.A33/34-32-196 A340-32-4202 50959 Modified Uplock Roller assembly & new bolts(201489 Series – Growth Gear)MSN 527 Replaced with new Uplock Rollerassembly at overhaulA340 MRB REPORTIssue: July, 2010 Page: APX 11.5d) A340-200/300 MLG items requiring further sampling and/or data from recent overhauls to justify 10 year TBO interval on individual partsItem/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul requirement ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationRetractionLink201489311/12 Required for10 year TBOjustificationTwo additional8-year samples(samplesperformed at 7.5years would beacceptable)Post Mod48066First Retraction Linkavailable for sampling willbe from January 20098 YEARS*(based on previous 5 yearsample)Weight OnWheelsRetractionActuator114256002-030114256002-040Required for10 year TBOjustificationAdditionalsample to beperformed atopportunity ofOverhaulAll Additional RetractionActuator will beavailablefor sampling from end of20088 YEARS*(10-year TBO low riskbased on samples to date)Weight OnWheels* Note: 8 year restoration limit refers to the parts as listed, not to the assembly or the aircraft on which they are installed.At the time of the sampling program, the MLG Retraction Actuator was considered by the industry as an “on-condition” item. Assuch, it was only functionally tested atoverhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and complete overhaul.Retrospective compliance is currently not required for retraction actuators not having been overhauled. However, this is underreview by Airbus and Messier-Dowty.Once completed, sampling results will be communicated to the MRB/ISC for review.A340 MRB REPORTIssue: July, 2010 Page: APX 11.6e) A340-200/300 MLG items requiring further sampling and/or data from recent overhauls to justify 20,000FC TBO interval.Item/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul requirement ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationMain GearAssembly201252001/002or201490001/002Required tojustify20,000FCTBO intervalOne sample All Proposal is to sampleMLG from MSN 428.Sample available by May200917,000FC* Aircraft onjacks – offwing task* Note:17,000FC restoration limit refers to the parts as listed, and not necessarily to the aircraft on which they are installed.Once completed, sampling results will be communicated to the MRB/ISC for review.A340 MRB REPORTIssue: July, 2010 Page: APX 11.73 A340-200/300 NOSE LANDING GEARa) NLG required Inspection and Lubrication TasksThere are currently no required NLG inspections tasks affecting TBO intervals.b) NLG modifications recommended to be accomplished prior to a 10 year TBOThere are currently no NLG modifications recommended to be accomplished prior to a 10 year TBO.c) NLG modifications recommended to be accomplished at the 10 year overhaulBased on in-service data, Airbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended product improvement modificationsat first overhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a lower level of degradation atsecond overhaul.Vendor ServiceBulletinReferenceAirbusServiceBulletinReferenceModNumberDescription Introduced asStandard inProductionFrom MSN:CommentsD23581-32-053 A340-32-4244 54793 Introduction of a New Shock Absorber Tube andModification of the Material of the diaphragmMSN 793 Replaced at overhaul withthe new Shock AbsorberTube and DiaphragmA340 MRB REPORTIssue: July, 2010 Page: APX 11.8d) A340-200/300 NLG items requiring sampling and/or data from recent overhauls to justify 10 year TBO interval on individual partsItem/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval AircraftmaintenanceconfigurationRetractionActuatorD23352000seriesRequired for10 year TBOjustificationData from twoRetractionActuators at a 10year Overhauland/or from twoFleet LeadersAll Retraction Actuator will beavailable for sampling byend of 200810 YEARSTo be justified using datafrom Overhaul and/or fromFleet leadersWeight OnWheelsNote:At the time of the sampling program, the NLG Retraction Actuator was considered by the industry as an “on-condition” item. Assuch, it was onlyfunctionally tested at overhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore requiresampling and complete overhaul.Retrospective compliance is currently not required for Retraction Actuators not having been overhauled. However, this is underreview by Airbus and Messier- Dowty.Once completed, sampling results will be communicated to the MRB/ISC for review.A340 MRB REPORTIssue: July, 2010 Page: APX 11.9e) A340-200/300 NLG items requiring further sampling and/or data from recent overhauls to justify 20,000FC TBO interval.Item/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationNose GearAssemblyD23285001D23285051D23285101D23285151D23581100Required tojustify20,000FCTBO intervalOne sample All Proposal is to sampleNLG from MSN 428.Sample available by May2009.17,000FC* Aircraft onjacks – offwing task* Note:17,000FC restoration limit refers to the parts as listed, and not necessarily to the aircraft on which they are installed.Once completed, sampling results will be communicated to the MRB/ISC for review.

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.10 4. A340-200/300 CENTRE LANDING GEAR

a) CLG required Inspection and Lubrication Tasks.

There are currently no required CLG inspection or lubrication tasks affecting TBO intervals.

b) CLG modifications recommended to be accomplished prior to a 10 year TBO

There are currently no CLG modifications recommended to be accomplished prior to a 10 year TBO.

c) CLG modifications recommended to be accomplished at the 10 year overhaul

There are currently no CLG modifications recommended to be accomplished at a 10 year overhaul.A340 MRB REPORTIssue: July, 2010 Page: APX 11.11d) A340-200/300 CLG Shock Strut Assembly 8 year sample detailsItem/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval ifsatisfactory sampling notachieved.AircraftmaintenanceconfigurationCLGShock StrutAssembly37100 series Required tojustify 10Year and12,000FCTBO intervalTwo 8 yearcalendarsamples‘F’ Standard(Mod 46880)1stCLG sampled fromMSN 025 at LufthansaTechnik in March 2008.2ndCLG sampled fromMSN 058 at M-D, Torontoin August 2008.Completed sample reportsto be available byDecember 20088 Years TBO* Aircraft onjacks – offwing task* Note:8 years restoration limit refers to the parts as listed, and not necessarily to the aircraft on which they are installed.Once completed, sampling results will be communicated to the MRB/ISC for review.

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.12 5. LANDING GEAR SAMPLING POLICY

The sampling aim is to justify the restoration interval.

Note: Unless otherwise notified by AIRBUS, operators may assume for maintenance planning

purposes that the restoration interval for gears/components is:

-10 years or 17,000FC, whichever occurs first, for the A340-200/300 MLG and NLG.

-10 years or 12,000FC, whichever occurs first, for A340-200/300 CLG.

-10 years or 8,500FC, whichever occurs first, for A340-500/600 MLG, NLG and CLG.

The sampling program, managed by AIRBUS, will continue until sufficient data has been compiled to

enable submittal of a final report, with recommendations, to the A340 MRB/ISC.

A main gear comprises:

- main fitting

- shock absorber assembly

- bogie beam (including axles)

- articulation links

- torque links

- sidestay assembly (including downlock mechanism & springs)

- shortening mechanism

- retraction actuator.

For a complete list of MLG Life Limited Parts refer to A340 ALS Pt 1.

A nose gear comprises:

- main fitting

- shock absorber assembly

- torque links

- axle

- drag stay assembly (including downlock mechanism & springs)

- retraction actuator

For a complete list of NLG Life Limited Parts refer to A340 ALS Pt 1.

A centerline gear comprises:

- main fitting

- sliding tube with axle (A340-200/300)

- bogie beam (including axles) (A340-500/600)

- shock absorber assembly

- torque links

- drag stay assembly (including downlock mechanism & springs)

- retraction actuator

For a complete list of CLG Life Limited Parts (A340-500/600 only) refer to A340 ALS Pt 1.

Note: For A340-200/300 CLG there are no Life Limited Parts listed in A340 ALS Pt 1.

AIRBUS will notify the MRB of all planned sampling inspections sufficiently well in advance to enable

them to attend or to delegate representation. Throughout the program, AIRBUS will forward all

teardown reports and recommendations to the MRB for scrutiny.

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.13 A340-200/300 Sampling

- Main Landing Gear:

Calendar sampling complete, excluding the parts referenced in Section 2, Para d) that still require

sampling and/or validation by using overhaul data.

Flight Cycle sample required at 17,000FC to validate any further increase in Flight Cycle TBO interval,

reference Section 2, Para e).

- Nose Landing Gear:

Calendar sampling complete, excluding the parts referenced in Section 3, Para d) that still require

sampling and/or validation by using overhaul data.

Flight Cycle sample required at 17,000FC to validate any further increase in Flight Cycle TBO interval,

reference Section 3, Para e).

- Centre Landing Gear Shock Strut Assembly:

Two CLG Shock Strut Assemblies to be sampled that have been in service 8 calendar years, reference

Section 4, Para d).

Data from the completed CLG calendar samples, to be extrapolated to justify 12,000FC TBO interval.

- Center Landing Gear Drag Stay Assembly:

Calendar sampling complete.

Data has already been extrapolated from previous CLG Drag Stay samples, to justify a 10 years and a

12,000FC TBO interval.

- Center Landing Gear Retraction Actuator:

Previous sampling of CLG Retraction Actuators after 10 years in-service to inspect them for corrosion,

has supported the inclusion of CLG Retraction Actuator within the 10 year CLG Overhaul (ref

Restoration VSB 37001-32-001), and also meets MRBR CLG restoration requirement.

Wear data from the 10 year overhauls, to be extrapolated to justify 12,000FC TBO interval.

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.14 A340-500/600 Sampling Proposal

One NLG, MLG and CLG gear set sample will be taken from each of four different climatic regions,

Temperate, Sub-tropical, Tropical, and Desert.

Each sample should be the first gear in each region that has been in service between 7.5 and 8

calendar years. 4 reserve gears will also be selected as a back-up.

- 4 NLG legs

- 8 MLG legs

- 4 CLG legs

For nominated sample aircraft refer to Table A, below. Each sample will be the subject of a commercial

agreement between Airbus/Messier-Dowty and the relevant operator.

The first gear set in each region from a second operator to achieve the target TBO, i.e. 10 years, will

also be sampled. 4 reserve gears will also be selected as a back-up.

- 4 NLG legs

- 8 MLG legs

- 4 CLG legs

For nominated sample aircraft refer to Table B, below. Each sample will be the subject of a commercial

agreement between Airbus/Messier-Dowty and the relevant operator.

Additionally, aircraft will also be nominated to sample Flight Cycle usage and validate the target TBO,

i.e. 8,500FC. For nominated sample aircraft refer to Table C, below. Each sample will be the subject of

a commercial agreement between Airbus/Messier-Dowty and the relevant operator.

The complete aircraft set of gears will be overhauled for each sample aircraft.

Sampling shall consist of a complete disassembly of each gear and special detailed inspections of all

Life Limited Parts (LLP’s) contained within that gear.

All parts removed in order to gain access to the LLP’s shall also be inspected.

Sampling Reports, once completed, shall be presented to the MRB/ISC for review.

Table A : A340-500/600 sample aircraft to perform 7.5 to 8 year MLG, NLG and CLG samples

MSN Model Operator Aircraft

Delivery Date Sample Region Sample Date

383 340-642 Virgin Atlantic 26/07/2002 First Temperate 26/01/2010 - 26/07/2010

391 340-642 Virgin Atlantic 05/10/2002 First Temperate

Reserve 05/03/2010 – 05/10/2010

453 340-642 Cathay Pacific 29/11/2002 First Sub-Tropical 29/05/2010 – 29/11/2010

436 340-642 Hainan Airlines 19/12/2002 First Sub-Tropical

Reserve 19/06/2010 – 19/12/2010

495 340-541 Qatar 15/09/2003 First Desert 15/03/2011 – 15/09/2011

471 340-541 Emirates 23/10/2003 First Desert

Reserve 23/10/2011 – 23/04/2012

478 340-541 Singapore A/L 19/12/2003 First Tropical 19/06/2011 – 19/12/2011

492 340-541 Singapore A/L 31/12/2003 First Tropical

Reserve 31/06/2011 – 31/12/2011

# A340 MRB REPORT

Issue: July, 2010 Page: APX 11.15 Table B : A340-500/600 sample aircraft to perform MLG, NLG and CLG samples at target Calendar

TBO

MSN Model Operator Aircraft

Delivery Date Sample Region Sample Date

517 340-642 Lufthansa 25/11/2003 Second Temperate 25/11/2013

482 340-642 Lufthansa 23/12/2003 Second Temperate

Reserve 23/12/2013

417 340-642 South African A/L 20/12/2002 Second Sub-Tropical 20/12/2012

410 340-642 South African A/L 24/12/2002 Second Sub-Tropical

Reserve 24/12/2012

457 340-541 Emirates 22/11/2003 Second Desert 22/11/2013

485 340-541 Emirates 29/11/2003 Second Desert

Reserve 29/11/2013

624 340-541 Thai Airways 06/04/2005 Second Tropical 06/04/2015

628 340-541 Thai Airways 29/04/2005 Second Tropical

Reserve 29/04/2015

Table C : A340-500/600 sample aircraft to perform MLG, NLG and CLG samples to validate target

Flight Cycle TBO

MSN Model Operator Aircraft

Delivery Date Sample Date Predicted FC

at 10 Year TBO

488 340-642 China Eastern 30/06/2003 30/06/2013 7000FC

457 340-541 Emirates 22/11/2003 22/11/2013 6350FC

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