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 

AFT 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 

A340-300 ENHANCED 

56293 INDICATING / RECORDING SYSTEMS - ACMS -INSTALL A WIRELESS GROUND 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 - ADVANCED 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 

ABSOLUTE 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 LAVATORY

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 the 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 AIR COOLING, TEMPERATURE 

CONTROL 

21.50.00 AIR 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. 
A340 MRB REPORT - Systems and Powerplant 

Issue : July 2010 3. EXPLANATION OF SYSTEMS AND POWERPLANT SECTION FORMAT

MSI 

REFERENCE 

TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

ZIP 

REFERENC

1 2 3 4 5 6 

1- This column indicates the MSI reference number and is directly obtained from the Airbus ATA Breakdown and Nomenclature R

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 

- 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, 9E This information can be used to clarify whether the task is to detect a failure (8B, 9B) or to detect degradation (5B, 6B, 7B, 8C, 

3- This column identifies the MSI title (which is in accordance with the Airbus ATA Breakdown) and the description of each task id

Report development process. The term "No task selected" indicates that the MSI has been subjected to a full MSG-3 analysis but no applicable and effective 

The term "-task deleted-" indicates that during the development process a task had been proposed which was eventually delet

amalgamation or ISC decision. Renumbering of tasks was avoided in order to minimise impact on cross reference data in oper

schedules. 
A340 MRB REPORT - Systems and Powerplant 

Issue : July 2010 

 The term "-reserved-" indicates that the task number has been allocated to an A330 MRB Report task. This ensures that corres

tasks 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 dependin

failure : - 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 pSuch tasks arise from either a specific MRB requirement (e.g. escape slide sampling) or have been determined as necessary tType 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 FECFECs (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 Inte

check. 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 CeRequirement (CMR) status. Such tasks are highlighted in this section by the notation "NOTE 24" in the interval column. The coinstructions are given in the approved document "A340 Certification Maintenance Requirements" reference 955.3019/92 which this 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) 
A340 MRB REPORT - Systems and Powerplant 

Issue : July 2010 

6- The scheduled maintenance task derived from MSG-3 analysis is considered adequately covered by the referenced Zonal task

noted 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 are giv

ALL Task 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 ROOM 

INSTALLED 

Self-explanatory 

A340-300 

PRE 44051 

Task applicable to A340-300 without modification 44051 embodied. 

A340-500 

POST 44051 

Task applicable to A340-500 with modification 44051 embodied. 

POST 44051 POST 44061 POST 44085 

Task applicable to all A340 with modification 44051 and 44061 and 44085 embodied. i.e. only to Aircraft with all modifications embodied. 

POST 45040 

OR 

POST 45056 

Task applicable to all A340 with modification 45040 or 45056 embodied i.e. to Aircraft with one of the modification or both modifications embodied. 

PRE 45040 PRE 45056 

Task applicable to all A340 without both modification 45051 and 45085 embodied at the same time i.e. without any if these modifications embodied 

A340-200 

OR 

A340-300 

PRE 49144 

Task applicable to all A340-300 without modification 49144 embodied and all A340-200 
A340 MRB REPORT - Systems and Powerplant 

Issue : July 2010 

A340-300 

POST 49144 

OR 

A340-500 

OR 

A340-600 

Task applicable to all A340-300 with modification embodied and to all A340-500 and A340-600 

POST 44040 

PRE 44057 

Task applicable to all A340 with modification 44040 and without modification 44057 embodied at the same time. 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.00.00 ENHANCED ZONAL  20.0.121 AVIONICS COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE AVIONICS - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF 710VU AND 740VU IN THE - I: 144 MO  AVIONICS COMPARTMENT, (EWIS).  20.0.131 FORWARD CARGO COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).  R GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).  20.0.137 BAY BEHIND FWD CARGO COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD - I: 72 MO  CARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  20.0.141 CENTER WING BOX  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE - I: 144 MO  THE 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-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.145 * * * * * C O N T I N U E * * * * *  R RS 01 CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN - I: 144 MO  FLOOR (ONLY IF CONTAMINATED), (EWIS).  20.0.151 AFT CARGO COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R RS 04 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 05 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).  R GVI 06 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).  R GVI 07 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).  R GVI 08 GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THE - I: 72 MO  ACT, EXTERNAL SURFACE ONLY.(EWIS)  NOTE: TASK COULD BE PERFORMED AT THE OPPORTUNITY OF  ACT R/I  20.0.155 REAR CENTER TANK  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.155 * * * * * C O N T I N U E * * * * *  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE - I: 144 MO  THE REAR CENTER TANK (AS FAR AS VISIBLE), (EWIS).  20.0.161 BULK CARGO COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).  R GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).  20.0.211 COCKPIT  R RS 01 CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY IF - I: 144 MO  CONTAMINATED), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE - I: 144 MO  COCKPIT AT LEVEL OF LATERAL FLOOR STRUCTURE BETWEEN  FR.1 TO FR.11, (EWIS).  20.0.221 FWD CABIN UTILITY AREA  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  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  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.221 * * * * * C O N T I N U E * * * * *  SEATS AND WITH EWIS CONNECTIONS BETWEEN SEAT  AND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.  R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN UTILITY - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MO  IN THIS AREA, (EWIS).  20.0.223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT  R RS 01 CLEANING OF EWIS AND CIRCUIT BRAKERS "5001 VE" - I: 144 MO  INSTALLED IN THE FWD CABIN UTILITY AREA OVERHEAD  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BRAKERS "5001VE" - I: 144 MO  AND "G, AND P" ROUTES INSTALLED IN THE FWD CABIN  UTILITY AREA OVERHEAD COMPARTMENT (ONLY IF  CONTAMINATED), (EWIS).  20.0.231 FWD CABIN  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  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.  R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE FWD CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  20.0.233 FWD CABIN OVERHEAD COMPARTMENT  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.233 * * * * * C O N T I N U E * * * * *  R RS 01 CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).  N GVI 03 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 144 MO  INSTALLED IN THE FORWARD CABIN OVERHEAD  COMPARTMENT, (EWIS).  N GVI 04 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 144 MO  INSTALLED IN THE FWD CABIN OVERHEAD COMPARTMENT,  (EWIS).  20.0.241 MID CABIN UTILITY AREA  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  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, ONLY.  R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS).  20.0.243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MO  OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED).  (EWIS).  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.243 * * * * * C O N T I N U E * * * * *  R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MO  OVERHEAD COMPARTMENT AREA (ONLY IF CONTAMINATED),  (EWIS).  N RS 03 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN UTILITY OVERHEAD  COMPARTMENT AREA, (EWIS).  N RS 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN UTILITY OVERHEAD  COMPARTMENT AREA, (EWIS).  20.0.251 MID CABIN  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  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.  R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MO  INSTALLED IN THIS AREA, RH ONLY, (EWIS).  R RS 04 CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  R RS 05 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS).  N GVI 06 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MO  INSTALLED IN THIS AREA, RH ONLY, (EWIS).  N GVI 07 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MO  INSTALLED IN THIS AREA, RH ONLY, (EWIS).  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.253 MID CABIN OVERHEAD COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  N GVI 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT  AREA. (EWIS).  N GVI 05 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA,  (EWIS).  N GVI 06 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT AREA,  (EWIS).  20.0.261 AFT CABIN  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTION, - I: 72 MO  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.  R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MO  (ONLY IF ONTAMINATED), (EWIS).  R RS 04 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.263 AFT CABIN OVERHEAD COMPARTMENT  R RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  R RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).  N GVI 04 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MO  THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).  N GVI 05 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MO  THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).  N GVI 06 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED IN - I: 144 MO  THE AFT CABIN OVERHEAD COMPARTMENT AREA, (EWIS).  20.0.271 AFT CABIN UTILITY AREA  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  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.  R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MO  IN THIS AREA, (EWIS).  20.0.273 AFT CABIN UNTILITY AREA OVERHEAD COMPARTMENT  R RS 01 CLEANING OF EWIS AND CIRCUIT BRAKERS "5005 VE" - I: 144 MO  INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEAD  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.273 * * * * * C O N T I N U E * * * * *  R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BRAKERS - I: 144 MO  "5005 VE" AND "P" ROUTE INSTALLED IN THE AFT CABIN  UTILITY AREA OVERHEAD COMPARTMENT, (EWIS).  20.0.315 TAIL CONE APU AND ACCESSORY COMPARTMENT  R GVI 01 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 54 MO  INSTALLED IN THE TAIL CONE FIREWALL AND APU AREA,  (EWIS).  20.0.319 HORIZONTAL STABILIZER CENTER BOX  R GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).  R GVI 03 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).  20.0.333 HORIZONTAL STABILIZER LATERAL BOX  R GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 3 TO  RIB 4 LH / RH (EWIS)  R SDI 02 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO  RIB 19LH / 20RH (EWIS)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.333 * * * * * C O N T I N U E * * * * *  R SDI 03 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO  RIB 13LH / 20RH (EWIS)  R GVI 04 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 13 TO  RIB 20LH (EWIS)  R SDI 05 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TO  RIB 20 LH/RH (EWIS)  R GVI 06 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) (EWIS)  R GVI 07 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  LATERAL BOX EWIS (AS FAR AS VISIBLE) (EWIS)  20.0.346 HORIZONTAL STABILIZER SPAR BOX VENT TANK  R GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  SPAR BOX VENT TANK EWIS (AS FAR AS VISIBLE) (EWIS)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.346 * * * * * C O N T I N U E * * * * *  R GVI 02 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MO  SPAR BOX VENT TANK EWIS (AS FAR AS VISIBLE) (EWIS)  20.0.541 INNER FUEL TANK  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER - I: 144 MO  FUEL TANK (AS FAR AS VISIBLE)(EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER - I: 144 MO  FUEL TANK (AS FAR AS VISIBLE)(EWIS).  20.0.542 OUTER/INNER FUEL TANK  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS IN THE OUTER FUEL - I: 144 MO  TANK (RIB 23 TO RIB 33)(AS FAR AS VISIBLE)(EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF EWIS IN THE INNER FUEL - I: 144 MO  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).  20.0.543 OUTER FUEL TANK  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE OUTER - I: 144 MO  FUEL TANK (AS FAR AS VISIBLE)(EWIS).  20.0.550 VENT SURGE TANK  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE VENT - I: 144 MO  SURGE 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-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 20.0.571 * * * * * C O N T I N U E * * * * *  R GVI 01 GENERAL VISUAL INSPECTION OF FUEL PUMP EWIS (AS FAR - I: 144 MO  AS VISIBLE)(EWIS).  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.00.00 AIR CONDITIONING  21.21.00 CABIN AIR DISTRIBUTION AND RECIRCULATION  VC 01 VISUAL CHECK OF MIXER UNIT 9 I: 4 C  02 TASK DELETED  DS 03 DISCARD RECIRCULATION FILTER ELEMENTS (PALL). 7 I: 5600 FH  NOTE 15  04 TASK RESERVED  05 TASK RESERVED  DS 06 DISCARD VIDEO CONTROL CENTER AIR FILTER ELEMENTS 9 I: 1 A  NOTE 1  OP 07 OPERATIONAL CHECK OF "STAND ALONE" SMOKE DETECTION 9 I: 2 C  SYSTEM VIA "SMOKE TEST" BUTTON  OP 08 OPERATIONAL CHECK OF VCC FAN DEACTIVATION BY USING 9 I: 2 C  THE FAN OFF SWITCH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.21.00 * * * * * C O N T I N U E * * * * *  R OP 09 OPERATIONAL CHECK TO VERIFY AUTOMATIC AND MANUAL 9 I: 2 C  CLOSING OF BULK CREW REST COMPARTMENT ISOLATION NOTE 24  VALVES  OP 10 OPERATIONAL CHECK TO VERIFY PROPER FUNCTION OF RETURN 8 I: 20000 FH  TO CABIN AURAL AND VISUAL COMMAND  DS 11 DISCARD ODOR RECIRCULATION FILTER ELEMENTS. 7 I: 2400 FH  NOTE 15  DS 12 DISCARD RECIRCULATION FILTER ELEMENTS (LE BOZEC - 7 I: 4000 FH  DONALDSON). NOTE 15  21.23.00 LAVATORY/GALLEY VENTILATION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.23.00 * * * * * C O N T I N U E * * * * *  DS 01 DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 7 I: 1200 FH  NOTE 1  02 TASK RESERVED  21.25.00 AIR CONDITIONING COMPARTMENT VENTILATION  OP 01 OPERATIONAL CHECK OF ABNORMAL VENTILATION WARNING 9 I: C  DI 02 DETAILED INSPECTION OF TURBOFAN SUPPLY DUCT 9 I: 4 C  GVI 03 GENERAL VISUAL INSPECTION OF PICCOLO TUBES 9 I: 2 C ZL-19 ZL-19 ZL-19 ZL-19 GVI 04 GENERAL VISUAL INSPECTION OF NACA AIR INLETS AND 9 I: C  PICCOLO TUBES IN HYDRAULIC COMPARTMENT  21.26.00 AVIONICS EQUIPMENT VENTILATION  OP 01 OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION 9 I: C  OP 02 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 C  (THIS TASK COVERS TASKS 73.25.00/02-C5 AND  73.25.00/01-R5)  OP 03 OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL 9 I: 2 C  OP 04 OPERATIONAL CHECK OF COOLING EFFECT DETECTOR (AEVC 8 I: 10000 FH  SYSTEM TEST)  GVI 05 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-12 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.26.00 * * * * * C O N T I N U E * * * * *  INSULATION ZL-12 ZL-12 RS 06 CLEANING OF RELAY BOX VU PANELS GRIDS 9 I: 2 C  21.27.00 AVIONICS EQUIPMENT GROUND COOLING  OP 01 OPERATIONAL CHECK OF FAULT WARNING 9 I: 2 C  GVI 02 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-12 INSULATION ZL-12 ZL-12 OP 03 OPERATIONAL CHECK OF GRU START 9 I: 2 C  21.28.00 LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING  (FWD, AFT AND BULK)  OP 01 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 3200 FH  ISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN NOTE 24A  CASE OF SMOKE WARNING.  (THIS TASK COVERS TASK 26.16.00/02).  OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF COLD 8 I: 3200 FH  AIR VALVE IN CASE OF SMOKE WARNING NOTE 24A  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.28.00 * * * * * C O N T I N U E * * * * *  OP 03 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FH  LOWER DECK MOBILE CREW REST ISOLATION VALVES IN NOTE 24  CASE OF SMOKE WARNING.  (THIS TASK COVERS TASK 26.18.00/05)  OP 04 OPERATIONAL CHECK OF HARD WIRED BACKUP TO VERIFY 9 I: 4 C  CLOSING OF LOWER DECK MOBILE CREW REST ISOLATION  VALVES  OP 05 OPERATIONAL CHECK OF HARD WIRED BACKUP OF VENTILATION 9 I: 4 C  CONTROLLER (TO VERIFY CLOSING OF ISOLATION VALVES AND  COLD AIR VALVE)  DS 06 DISCARD FILTER ELEMENT OF BULK VIDEO COMPARTMENT 9 I: 2400 FH  NOTE 1  OP 07 OPERATIONAL CHECK OF AUTOMATIC AND MANUAL SHUT OFF OF 9 I: 2 C  BULK VIDEO COMPARTMENT VENTILATION AND ELECTRICAL  POWER AND CHECK NON RETURN VALVE IS IN CLOSED  POSITION  21.31.00 PRESSURE CONTROL AND MONITORING  OP 01 OPERATIONAL CHECK OF MANUAL MODE 8 I: 20000 FH  OP 02 OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN 9 I: 2 C  DITCHING CONFIGURATION  OP 03 OPERATIONAL CHECK OF OUTFLOW VALVE OPENING (50%) BY 9 I: 2 C  EMERGENCY RAM AIR SWITCH  OP 04 OPERATIONAL CHECK OF LANDING FIELD ELEVATION SELECTOR 9 I: 2 C  BY MEANS OF INITIATED TEST (VIA MCDU)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.31.00 * * * * * C O N T I N U E * * * * *  FC 05 FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P 6,9 I: 24000 FH  PROTECTION OF SAFETY VALVES OR  6 YE  NOTE 24  06 TASK DELETED  OP 07 OPERATIONAL CHECK OF NEGATIVE PRESSURE RELIEF VALVE 9 I: 4 C  OP 08 OPERATIONAL CHECK OF POSITION INDICATION OF SAFETY 9 I: 4 C  VALVES  RS 09 REMOVE SAFETY VALVE FOR RESTORATION. 9 I: 50000 FH  OR  12 YE  21.50.00 AIR COOLING TEMPERATURE CONTROL  RS 01 CLEAN FLIGHT DECK TEMPERATURE SENSORS 7 I: C  OP 02 OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM 9 I: 2 C  OPENING  DI 03 DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS 9 I: 4 C  FOR CONDITION AND OPERATION  DI 04 DETAILED INSPECTION OF LP GROUND AIR CHECK VALVE 9 I: 24000 FH  FLAPPERS FOR CONDITION AND OPERATION.  VC 05 VISUAL CHECK OF PACK AIR SUPPLY DUCTS, CLAMPS AND 9 I: 24000 FH  BELLOWS (BETWEEN PACK OUTLET AND MIXER UNIT)  DI 06 DETAILED INSPECTION OF PACK DOWNSTREAM CHECK VALVES 6,9 I: 24000 FH  FLAPPERS FOR CONDITION AND OPERATION  GVI 07 GENERAL VISUAL INSPECTION OF TRIM AIR DUCTS BETWEEN 9 I: 4 C ZL-13 FLOW CONTROL VALVES AND HOT AIR MANIFOLDS ZL-13 ZL-13 ZL-19 ZL-19 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.50.00 * * * * * C O N T I N U E * * * * *  ZL-19 ZL-19 FC 08 REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK 9 I: 2 C  NOTE 1  RS 09 CLEANING OF CABIN TEMPERATURE SENSORS, SENSE LINES 7 I: 2 A  AND INLETS NOTE 1  DS 10 DISCARD CABIN TEMPERATURE SENSOR FILTERS 7 I: 1 A  NOTE 1  DI 11 DETAILED INSPECTION OF EMERGENCY RAM AIR AND LP 9 I: 4 C  GROUND AIR CONNECTION FLAPPERS FOR CONDITION AND  OPERATION  DS 12 DISCARD FLOW CONTROL VALVE FILTERS 9 I: 2000 FC  NOTE 1  GVI 13 GENERAL VISUAL INSPECTION OF HEATSHIELDS FOR 8 I: 20000 FH  CONDITION AND VISIBLE DAMAGE  RS 14 CLEANING AND DETAILED INSPECTION FOR EROSION OF PACK 7 I: 2 C  WATER INJECTOR NOZZELS.  DI 15 DETAILED INSPECTION OF EMERGENCY RAM AIR CHECK VALVE, 9 I: 4 C  SKIN VALVE FLAPPERS FOR CONDITION AND OPERATION.  21.70.00 HUMIDIFICATION SYSTEM  N DS 01 DISCARD WATER FILTER ELEMENT. 7 I: 48 MO  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 21.70.00 * * * * * C O N T I N U E * * * * *  N RS 02 REMOVE DUCT SENSOR UNIT FOR RESTORATION. 7 I: 24 MO  N RS 03 REMOVE STEAM GENERATING UNIT FOR RESTAURATION. 7 I: 10 YE  N DS 04 DISCARD STEAM HOSE. 7,9 I: 24 MO  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 22.00.00 AUTO FLIGHT  22.10.00 AUTOPILOT/FLIGHT DIRECTOR  OP 01 OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION 9 I: 2 C  OP 02 OPERATIONAL CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING 9 I: 4 C  DEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS  22.30.00 AUTOTHRUST  OP 01 OPERATIONAL CHECK OF A/THR ISOLATION FROM ENGINE 9 I: 4 C  CONTROL  22.60.00 FLIGHT ENVELOPE  NO TASK SELECTED  22.70.00 FLIGHT MANAGEMENT  OP 01 OPERATIONAL CHECK OF BACK-UP NAVIGATION FUNCTION 9 I: C  OP 02 OPERATIONAL CHECK OF MCDU 3 TRANSFER 9 I: C  OP 03 OPERATIONAL CHECK OF MCDU ANNUNCIATORS 9 I: C  OP 04 OPERATIONAL CHECK OF FM SOURCE SWITCHING 9 I: 2 C  22.90.00 AUTOFLIGHT SYSTEM BITE  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AUTO FLIGHT SECTION: C-22 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 23.00.00 COMMUNICATIONS  23.11.00 HF SYSTEM (MOD 40068, 40069)  NO TASK SELECTED  23.12.00 VHF SYSTEM  NO TASK SELECTED  23.24.00 AIRCRAFT COMMUNICATIONS ADDRESSING & REPORTING SYSTEM (ACARS)  (MOD 40065)  NO TASK SELECTED  23.28.00 SATELLITE COMMUNICATION  NO TASK SELECTED  23.33.00 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)  OP 01 OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION 9 I: 2 C  FROM FLIGHT DECK (IF INSTALLED) AND CABIN  DS 02 DISCARD IFE-RACK FILTERS. 9 I: 2400 FH  R RS 03 CLEANING OF VENTILATION GRIDS AND VENTILATOR HOUSING 9 I: 10000 FH  (IF INSTALLED) FROM IFE COMPONENTS INSTALLED  IN THE CABIN (VCC/RCC)  23.39.01 SATELLITE TV TRANSCEIVER SYSTEM TAILWIND (TW560) AND  PANASONIC (IDTV)  R DS 01 DISCARD ALL FILTER ELEMENTS ON TAILWIND SYSTEM. 7 I: A  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 23.39.02 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION BY BOEING (CBB).  OP 01 OPERATIONAL CHECK OF CONNEXION BY BOEING SYSTEM 9 I: 4 C  POWER OFF PROCEDURE.  OP 02 OPERATIONAL CHECK OF COOLING LOSS DETECTION OF 9 I: 4 C  CONNEXION BY BOEING SYSTEM.  23.42.00 COCKPIT TO GROUND CREW CALL SYSTEM  NO TASK SELECTED  23.51.00 AUDIO MANAGEMENT (INTEGRATING/FLIGHT INTERPHONE/SELCAL/CALL)  OP 01 OPERATIONAL CHECK OF OXYGEN MASK MICROPHONE 9 I: C  OP 02 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING 9 I: C  (COVERED BY MSI 23-71-00, TASK NO1)  OP 03 OPERATIONAL CHECK OF CAPTAIN AND F/O ACP SWITCHING TO 9 I: 2 C  THIRD ACP  23.61.00 STATIC DISCHARGER  FC 01 CHECK RESISTANCE FROM THE DISCHARGER TO THE BASE 9 I: C  (RETAINER) AND FROM THE BASE (RETAINER) TO THE  AIRCRAFT STRUCTURE  GVI 02 GENERAL VISUAL INSPECTION OF STATIC DISCHARGER. 9 I: C  23.71.00 COCKPIT VOICE RECORDER  OP 01 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING 9 I: C  (THIS TASK COVERS TASK 23.51.00/02)  OP 02 OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING 9 I: C  TIME DELAY RELAY  DS 03 DISCARD ULB BATTERY 9 I: VR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 23.71.00 * * * * * C O N T I N U E * * * * *  OP 04 OPERATIONAL CHECK OF THE ULB 9 I: VR  23.72.00 COCKPIT DOOR SURVEILLANCE SYSTEM (CDSS)  NO TASK SELECTED  23.73.00 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)  R OP 01 OPERATIONAL CHECK OF CABIN SIGNS VIA MCDU 9 I: 2 A  NOTE 26  OP 02 OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU 9 I: 1 C  NOTE 26  R OP 03 OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, 9 I: 2 C  DEUS-A CUT OFF FUNCTION  OP 04 OPERATIONAL CHECK OF EVAC FUNCTION 9 I: 2 C  R OP 05 OPERATIONAL CHECK OF HOT BATTERY BUS POWERED CIDS 9 I: 20000 FH  OPERATION  06 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 23.73.00 * * * * * C O N T I N U E * * * * *  07 TASK DELETED  OP 08 OPERATIONAL CHECK OF LDL/LDF SIGNS VIA MCDU 9 I: 4 C  NOTE 26  R OP 09 OPERATIONAL CHECK OF EMERGENCY CABIN ALERT SYSTEM 9 I: 2 C  (ECAS)  N OP 10 OPERATIONAL CHECK OF BATTERY POWERED CIDS PA 9 I: 20000 FH  OPRERATION.  23.75.00 TAXI AID CAMERA SYSTEM (TACS)  OP 01 OPERATIONAL CHECK OF THE VIDEO DISCONNECTION SWITCH 9 I: C  (999VU) FUNCTION  23.81.00 RADIO MANAGEMENT  OP 01 OPERATIONAL CHECK OF RMP LIGHT 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  OP 02 OPERATIONAL CHECK OF RADIO NAVIGATION BACK-UP MODE 9 I: C  * * * * * E N D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 24.00.00 ELECTRICAL POWER  24.20.00 AC GENERATION  OP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FH  (THIS TASK COVERS TASKS 24.50.00/01 AND 24.60.00/01) NOTE 24  OP 02 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FH  SUPPLY NOTE 24  (THIS TASK COVERS TASK 24.30.00/01)  03 TASK DELETED  OP 04 OPERATIONAL CHECK OF LIGHTS. 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  DS 05 DRAIN IDG OIL SYSTEM, DISCARD FILTER ELEMENT(S) 7 I: A  AND REPLENISH  FC 06 CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT 9 I: 2100 FH  OP 07 OPERATIONAL CHECK OF AC GENERATION SIDE 1 AND SIDE 2 9 I: C  ISOLATION  OP 08 OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS 9 I: C  OP 09 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION MANUAL 9 I: C  SWITCHING  OP 10 OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC 8 I: 18 MO  CONNECTION NOTE 24B  OP 11 OPERATIONAL CHECK OF EMERGENCY GENERATOR MANUAL 8 I: 18 MO  CONNECTION NOTE 24  OP 12 OPERATIONAL CHECK OF CSM/G DISCONNECTION WITH 8 I: 18 MO  SIMULATED ENGINES FLAMED OUT CONDITION AND SLATS NOTE 24B  EXTENDED  RS 13 CLEAN IDG OIL COOLER 7 I: 4 C  OP 14 OPERATIONAL CHECK OF IDG DISCONNECT FUNCTION 9 I: 4 C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 24.20.00 * * * * * C O N T I N U E * * * * *  OP 15 OPERATIONAL CHECK OF GENERATOR SHUT-DOWN WHEN ENGINE 9 I: 60 MO  FIRE HANDLE IS OPERATED  (COVERED BY MSI 26-21-00, TASK NO3).  16 TASK DELETED  OP 17 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION 9 I: C  AUTOMATIC SWITCHING  18 TASK DELETED  24.30.00 DC GENERATION  OP 01 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FH  SUPPLY (COVERED BY MSI 24-20-00, TASK NO2). NOTE 24  02 TASK DELETED  R RS 03 REMOVE BATTERIES (1, 2, APU) FOR OVERHAUL 6 I: VR  OP 04 OPERATIONAL CHECK OF DC MAIN GENERATION SWITCHING 9 I: 1 C  NOTE 24B  OP 05 OPERATIONAL CHECK OF DC ESSENTIAL GENERATION 9 I: C  SWITCHING  OP 06 OPERATIONAL CHECK OF DC BAT BUS AND DC ESS BUS 8 I: 800 FH  ISOLATION  24.40.00 EXTERNAL POWER  01 TASK DELETED  ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 24.50.00 AC ELECTRICAL LOAD DISTRIBUTION  OP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FH  (COVERED BY MSI 24-20-00, TASK NO1). NOTE 24  OP 02 OPERATIONAL CHECK OF COMMERCIAL LOAD SHEDDING 9 I: C  OP 03 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MO  (THIS TASK COVERS TASK 24.60.00/02)  OP 04 OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN 9 I: 2 C  EMERGENCY CONFIGURATION  05 TASK RESERVED  06 TASK RESERVED  24.54.00 ELECTRICAL LOAD MANAGEMENT SYSTEM  OP 01 OPERATIONAL CHECK OF THE ELMU OUTPUTS ACTIVATION BY 9 I: 2 C  MCDU  24.60.00 DC ELECTRICAL LOAD DISTRIBUTION  OP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FH  (COVERED BY MSI 24-20-00, TASK NO1). NOTE 24  OP 02 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MO  (COVERED BY MSI 24-50-00, TASK NO3).  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.00.00 EQUIPMENT/FURNISHINGS  25.11.00 COCKPIT SEATS  DI 01 DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT 8 I: 6 YE  ATTACHMENT  FC 02 FUNCTIONAL CHECK OF HORIZONTAL/VERTICAL MECHANICAL 6,9 I: C  CONTROL CABLE ADJUSTMENT OF COCKPIT SEATS  25.21.00 PASSENGER COMPARTMENT SEATS  GVI 01 GENERAL VISUAL INSPECTION OF SEAT TO FLOOR 8 I: 36 MO  ATTACHMENT.  GVI 02 GENERAL VISUAL INSPECTION OF LOWER SEAT STRUCTURE, 8 I: 36 MO  BAGGAGE RESTRAINT BAR, BACKREST AND BACKREST SUPPORT.  OP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MO  BELT ATTACHMENTS  R OP 04 OPERATIONAL CHECK OF ELECTRONIC CIRCUIT OF THE 8 I: VR  INFLATABLE RESTRAINT SYSTEM.  RS 05 REMOVE SEAT BELT SYSTEM FOR RESTORATION OF AIRBAG 7,8 I: VR  AND DISCARD BATTERY, HOSE, SQUIB AND GAS STORAGE  ACCORDING TO CMM  25.22.00 CABIN ATTENDANT SEATS  GVI 01 GENERAL VISUAL INSPECTION OF SEAT ATTACHMENT POINTS. 8 I: 36 MO  GVI 02 GENERAL VISUAL INSPECTION OF SEAT STRUCTURE. 8 I: 36 MO  OP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MO  BELT ATTACHMENTS  25.23.44 LININGS AND FURNISHINGS (DADO PANELS)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.23.44 * * * * * C O N T I N U E * * * * *  VC 01 VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS 8 I: 18 MO  IN CABIN ARE CLOSED  OP 02 OPERATIONAL CHECK OF CABIN DECOMPRESSION PANELS 9 I: 4 C  OPENING  25.24.00 OVERHEAD STOWAGE COMPARTMENTS  NO TASK SELECTED  25.27.00 DOOR AREA HEATING SYSTEM  R OP 01 OPERATIONAL CHECK OF THE DOOR AREA HEATING SYSTEM BY 9 I: 2 C  USING THE TEST BUTTON ON EACH CONTROL UNIT.  25.30.00 BUFFET AND GALLEY  DS 01 DISCARD GALLEY AIR EXTRACTION FILTER ELEMENT 9 I: 1400 FH  02 TASK DELETED  DI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 C  POINTS  (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-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.30.00 * * * * * C O N T I N U E * * * * *  OP 05 OPERATIONAL CHECK OF EMERGENCY EXIT HATCH FROM BOTH 8 I: 18 MO  SIDES  25.34.00 GALLEY COOLING  RS 01 CLEAN AIR CHILLER CONDENSER AIR FILTER. 7 I: 1400 FH  NOTE 1  RS 02 CLEAN REMOTE CHILLER CONDENSER AIR FILTER. 7 I: 1400 FH  NOTE 1  RS 03 CLEAN GAC "AIR OVER" FILTER. 7 I: 1400 FH  NOTE 1  RS 04 CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES 7 I: 1400 FH  IN THE GALLEY CABINET. NOTE 1  25.38.00 LIFT SYSTEM  OP 01 OPERATIONAL CHECK OF THE CAGE STOP FUNCTION. 9 I: 40 MO  DI 02 DETAILED INSPECTION OF TOOTH BELTS, BELT PULLEYS, 7,9 I: 80 MO  ATTACHMENT POINTS AND FLOOR PAN.  OP 03 OPERATIONAL CHECK OF LIFT SYSTEM SENSORS, USING THE 9 I: 80 MO  MAINTENANCE PANEL ON THE CONTROL UNIT.  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.40.00 LAVATORIES  R DI 01 DETAILED INSPECTION OF WASTE COMPARTMENT FOR FIRE 9 I: 1 C  CONTAINMENT CAPABILITY. OR  NR  NOTE 8  R OP 02 OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP 9 I: 1 C  OR  NR  NOTE 8  DI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 C  POINTS  (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  25.47.00 LOWER DECK LAVATORIES  01 TASK RESERVED  02 TASK RESERVED  25.51.00 LOWER DECK CARGO LOADING SYSTEM  R OP 01 OPERATIONAL CHECK OF POWER DRIVE UNITS (NOTE 11) 9 I: C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * C O N T I N U E * * * * *  R DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FH  R DI 03 REMOVE CREW REST ROOM CONTAINER LATCHES AT C53.7 8 I: 34000 FH  FOR DETAILED INSPECTION.  R GVI 04 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES 9 I: A ZL-13 ZL-13 ZL-15 R GVI 05 GENERAL VISUAL INSPECTION OF OVERRIDEABLE Y-DOOR SILL 9 I: A ZL-13 LATCHES ZL-13 ZL-15 R GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS 9 I: A ZL-13 ZL-13 ZL-15 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * C O N T I N U E * * * * *  R GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS 9 I: A ZL-13 INCLUDING TRANSPORT ROLLER. (NOTE11) ZL-13 ZL-15 R DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 300 FC  WEAR AND DAMAGE. (NOTE 11)  R GVI 09 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS (NOTE 9 I: 4 A ZL-13 11) ZL-13 ZL-15 R GVI 10 GENERAL VISUAL INSPECTION OF XZ-LATCHES (NOTE 11) 8 I: 3200 FH ZL-13 ZL-13 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * 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-13 C53.2 (NOT FOR A340-500), C53.8 (A340-500 ONLY), ZL-13 C57.1 (WITH MOD 49689), C65 AND C68 (NOTE 11) ZL-15 R GVI 12 GENERAL VISUAL INSPECTION OF FIXED, RETRACTABLE AND 9 I: 4 A ZL-13 OVERRIDEABLE YZ-LATCHES (NOTE 11) ZL-13 ZL-15 R GVI 13 GENERAL VISUAL INSPECTION OF Y-GUIDE ROLLERS, 9 I: C ZL-13 AUTOMATIC Z-GUIDE, GUIDE RAILS, YZ-LATCH GUIDE ZL-13 ROLLERS, XY-ENTRANCE GUIDE ASSEMBLIES, Y-GUIDES AND ZL-15 Y-GUIDE ACTUATION MECHANISMS (A340-200 OR A340-300  ONLY)(AND X-GUIDES WITH MOD40208) (NOTE 11)  R DI 14 REMOVE ACT LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FH  15 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * C O N T I N U E * * * * *  GVI 16 GENERAL VISUAL INSPECTION OF ROLLER KITS. 9 I: A ZL-13 ZL-15 R GVI 17 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-13 ZL-13 ZL-15 GVI 18 GENERAL VISUAL INSPECTION OF PALLET STOP. 9 I: 4 A ZL-13 N OP 19 OPERATIONAL CHECK OF BRAKING ROLLER. 9 I: 2 C  N 20 TASK RESERVED  25.51.01 ADVANCED LOWER DECK CARGO LOADING SYSTEM  N OP 01 OPERATIONAL CHECK OF SWIVEL NOSE AT XZ-LATCHES EG 9 I: 4 C  (ENTRANCE GUIDE) AND SWIVEL NOSES AT OVERRIDEABLE  CENTER LATCHES. (NOTE 11)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.01 * * * * * C O N T I N U E * * * * *  N DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FH  N 03 TASK RESERVED  N OP 04 OPERATIONAL CHECK OF BRAKING ROLLER AND SWIVEL 9 I: 2 C  CASTER. (NOTE 11)  N GVI 05 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES AND 9 I: A ZL-13 OVERRIDEABLE ARO DEVICES. ZL-15 N GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS, BALL MATS 9 I: A ZL-13 AND BALL STRIPS. ZL-15 N GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS, TRANSPORT 9 I: A ZL-13 ROLLERS. (NOTE 11) ZL-15 N DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 1500 FC  WEAR AND DAMAGE. (NOTE 11) OR  18 MO  N GVI 09 GENERAL VISUAL INSPECTION OF OVERRIDEABLE CENTER 9 I: 4 A ZL-13 LATCHES AND SPLITTER. (NOTE 11) ZL-15 N GVI 10 GENERAL VISUAL INSPECTION OF XZ-LATCHES. (NOTE 11) 8 I: 3200 FH  N GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AND 9 I: 4 A ZL-13 XZ-LATCHES EG (ENTRANCE GUIDE). (NOTE 11) ZL-15 N GVI 12 GENERAL VISUAL INSPECTION OF FIXED YZ-LATCHES AND 9 I: 4 A ZL-13 YZ-LATCHES WITH TRANSPORT ROLLER (MOD 56837). ZL-15 (NOTE 11)  N GVI 13 GENERAL VISUAL INSPECTION OF YZ LATCH-GUIDE ROLLERS, 9 I: C ZL-13 LATERAL ENTRANCE GUIDE, Y-GUIDE 42 L, SCUFF PLATE ZL-15 ROLLER, SIDE GUIDES, ENTRANCE ROLLER, DOOR SILL LATCH  SUPPORT ROLLER AND OVERROLLABLE GUIDE (MOD 56837).  (NOTE 11)  N GVI 14 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-13 ZL-15 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.51.01 * * * * * C O N T I N U E * * * * *  N GVI 15 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS AND 9 I: 4 A ZL-13 SWIVEL CASTERS. (NOTE 11) ZL-15 25.52.00 LOWER DECK AFT AND FORWARD CARGO COMPARTMENT  VC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING 8 I: 8 DY  STRIPS, PROTECTION PLATES, CENTER LINE COVER PLATES  AND ACCESS DOORS (NOTE 11).  VC 02 VISUAL CHECK OF DECOMPRESSION PANELS (NOTE 11) 8 I: 8 DY  R VC 03 VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE 9 I: A  ROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OF  CLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY.  (NOTE 11)  N OP 04 OPERATIONAL CHECK OF AIR STOP VALVES FOR HEATED 9 I: 4 C  DRAINAGE SYSTEM.  N GVI 05 GENERAL VISUAL INSPECTION OF THE DRAINAGE SYSTEM 9 I: 4 C ZL-13 INSTALLATION. ZL-15 ZL-15 ZL-16 ZL-16 N VC 06 VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR 9 I: A  EVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN AS  NECESSARY.  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-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.54.00 * * * * * C O N T I N U E * * * * *  VC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS 8 I: 8 DY  AND ACCESS DOOR AT C73.  (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  VC 02 VISUAL CHECK OF DECOMPRESSION PANELS. 8 I: 8 DY  (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  GVI 03 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-16 (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  R DI 04 DETAILED INSPECTION OF DIVIDER NETS, NET 9 I: C  ATTACHMENT POINTS, NET CONNECTING DEVICES AND TENSION  BUCKLES.  (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.54.00 * * * * * C O N T I N U E * * * * *  R DI 05 DETAILED INSPECTION OF NET SCREENS, NET SCREEN 9 I: C  ATTACHMENT POINTS AND TENSION BUCKLES.  (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  R DI 06 DETAILED INSPECTION OF SCREEN DECOMPRESSION 9 I: C  TARPAULINS.  (NOTE: IF PBCRC IS INSTALLED, TASK TO BE PERFORMED  IN REMAINING AREA)  25.61.00 COCKPIT ESCAPE FACILITIES  VC 01 VISUAL CHECK OF EMERGENCY ESCAPE ROPE AND ROPE 8 I: 6 YE  ATTACHMENT  25.62.00 CABIN ESCAPE FACILITIES  FC 01 REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST 6 I: NR  OR  VR  R RS 02 RESTORATION OF LIFE RAFTS BY REMOVAL AND REPLACEMENT 8 I: VR  WITH OVERHAULED.  R OP 03 OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT - I: NR  OR  VR  NOTE 10  DS 04 DISCARD SQUIB 8 I: VR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.62.00 * * * * * C O N T I N U E * * * * *  OP 05 OPERATIONAL CHECK OF THE SRPSU VIA MCDU 8 I: 20000 FH  OP 06 BATTERY CAPACITY CHECK OF THE SRPSU VIA MCDU 8 I: 6 MO  OP 07 OPERATIONAL CHECK OF THE ELECTRICAL CIRCUIT INCLUDING 8 I: 20000 FH  SQUIB NOTE 24B  25.65.32 EMERGENCY LOCATOR TRANSMITTER (PORTABLE)  R RS 01 REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER 9 I: VR  (ELT(S)) FOR WORKSHOP CHECK.  25.65.34 EMERGENCY VHF TRANSCEIVER  FC 01 REMOVE EMERGENCY VHF TRANSCEIVER FOR SHOP INSPECTION 9 I: VR  OR  24 MO  25.65.35 EMERGENCY LOCATOR TRANSMITTER SYSTEM  R OP 01 OPERATIONAL CHECK OF AUTOMATIC FIXED 8 I: 18 MO  EMERGENCY LOCATOR TRANSMITTER (ELT(AF))  SYSTEM BY MANUAL ACTIVATION.  R RS 02 REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER 8 I: VR  (ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDING  BATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELT  ACTIVATION.  25.65.51 MEGAPHONE  DS 01 DISCARD MEGAPHONE BATTERIES 9 I: VR  OP 02 OPERATIONAL CHECK OF MEGAPHONE 9 I: C  25.66.52 LIFE VEST  R RS 01 RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT 9 I: VR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.66.52 * * * * * 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 MO  AND BUNK STRUCTURE.  GVI 02 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-22 ATTACHMENT POINTS OF THE CREW REST ROOM (REST ROOM ZL-22 REMOVED). ZL-22 25.75.00 CREW REST ROOM (UNDERFLOOR)  OP 01 OPERATIONAL CHECK OF EMERGENCY EXIT HATCH OPENING 8 I: 18 MO  FROM INSIDE AND FROM OUTSIDE  DI 02 DETAILED INSPECTION OF BED BELTS AND BELT ATTACHMENTS 8 I: 36 CRR MO  ON CREW REST BUNKS  03 TASK DELETED  VC 04 VISUAL CHECK OF CARGO COMPARTMENT CEILING WELL, 8 I: 6 YE  INTERFACE LININGS AND OF THE OUTSIDE OF THE CONTAINER  GVI 05 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-25 ATTACHMENT POINTS OF THE STAIRHOUSE (STAIRHOUSE ZL-25 REMOVED). ZL-25 ZL-25 OP 06 OPERATIONAL CHECK OF DOOR HINGE AND LOCK 9 I: 36 CRR MO  OP 07 OPERATIONAL CHECK OF FULL BCRC KICK THROUGH PANEL 8 I: 40000 FH  FROM BOTH SIDES  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 25.75.00 * * * * * C O N T I N U E * * * * *  VC 08 VISUAL CHECK OF BCRC LINING AND MAINTENANCE ACCESS 8 I: 6 YE  PANELS  DI 09 DETAILED INSPECTION OF FULL BCRC FLIGHT CREW SEAT 8 I: 36 MO  BELT, SEAT ATTACHMENT AND STRUCTURE  VC 10 VISUAL CHECK OF DECOMPRESSION PANEL 8 I: 800 FH  GVI 11 GENERAL VISUAL INSPECTION OF MAIN AND EMERGENCY HATCH 8 I: 6 YE  SEALS  GVI 12 GENERAL VISUAL INSPECTION OF THE LADDER ASSEMBLY 6 I: 2 C  VC 13 VISUAL CHECK OF HATCH SEAL, DOOR SEALS AND BELLOW 8 I: 36 MO  SEALS.  25.76.00 TIRE DEBRIS RETENTION SYSTEM  GVI 01 GENERAL VISUAL INSPECTION OF TYRE DEBRIS RETENTION 9 I: A ZL-14 SYSTEM  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.00.00 FIRE PROTECTION  26.11.00 MAIN LANDING GEAR FIRE AND OVERHEAT DETECTION  OP 01 BITE TEST OF THE FDU THROUGH MCDU 8 I: 800 FH  26.12.00 ENGINE FIRE AND OVERHEAT DETECTION  NO TASK SELECTED  26.13.00 APU FIRE AND OVERHEAT DETECTION  OP 01 OPERATIONAL CHECK OF APU FIRE AND OVERHEAT DETECTION 9 I: 8000 FH  LOOPS  (COVERED BY MSI 26.22.00, TASK NO1)  26.15.00 AVIONICS COMPARTMENT SMOKE DETECTION  OP 01 OPERATIONAL CHECK OF AVIONICS COMPARTMENT SMOKE 9 I: 4 A  DETECTION BY PTT NOTE 5  RS 02 REMOVE AVIONICS SMOKE DETECTION PICCOLO TUBES FOR 8 I: 36 MO  CLEANING  03 TASK DELETED  26.16.00 LOWER DECK CARGO COMPARTMENT SMOKE DETECTION  OP 01 OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE 9 I: 4 A  DETECTION BY PTT NOTE 5  OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 9 I: C  CARGO 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-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.16.00 * * * * * C O N T I N U E * * * * *  26.17.00 LAVATORY SMOKE DETECTION  01 TASK DELETED  26.18.00 AUXILIARY AREAS SMOKE DETECTION  OP 01 OPERATIONAL CHECK OF LDMCR 9 I: 2 A  SMOKE DETECTION BY PTT NOTE 25  RS 02 REMOVE AND CLEAN LDMCR SMOKE 6 I: 72 CRR MO  DETECTORS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.18.00 * * * * * C O N T I N U E * * * * *  OP 03 OPERATIONAL CHECK OF LDMCR STAIRHOUSE SMOKE DETECTION 9 I: C  SYSTEM BY MCDU  OP 04 OPERATIONAL CHECK OF FCRC SMOKE DETECTION SYSTEM 9 I: C  BY MCDU  OP 05 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FH  LDMCR ISOLATION VALVE (IN CASE OF  FIRE IN LDMCR STAIRHOUSE OR CREW REST ROOM)  (COVERED BY MSI 21-28-00, TASK NO 3)  OP 06 OPERATIONAL CHECK OF LDMCR 9 I: 18 CRR MO  SMOKE DETECTORS WITH AEROSOL  07 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.18.00 * * * * * C O N T I N U E * * * * *  OP 08 OPERATIONAL CHECK OF SDCU/CIDS 8 I: 18 MO  TO VERIFY AUTOMATIC CLOSING  OF BCRC ISOLATION VALVE (IN CASE OF FIRE)  OP 09 OPERATIONAL CHECK OF BCRC STAIRHOUSE 9 I: C  SMOKE DETECTION SYSTEM BY MCDU  OP 10 OPERATIONAL CHECK OF VCC SMOKE DETECTION BY MCDU. 8 I: 18 MO  RS 11 REMOVE VCC PICCOLO TUBES FOR CLEANING. 7 I: 18000 FH  OP 12 OPERATIONAL CHECK OF IFES SMOKE DETECTION BY MCDU. 8 I: 18 MO  RS 13 REMOVE IFES PICCOLO TUBES FOR CLEANING. 7 I: 18000 FH  RS 14 REMOVE AND CLEAN LDF AFT (DCR) SMOKE DETECTOR. 8 I: 72 CRR MO  OP 15 OPERATIONAL CHECK OF LDF AFT (DCR) SMOKE DETECTION BY 8 I: 1400 CRR  PTT. FH  OP 16 OPERATIONAL CHECK OF LDF AFT (DCR) SMOKE DETECTOR 8 I: 18 CRR MO  WITH AEROSOL.  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.18.00 * * * * * C O N T I N U E * * * * *  RS 17 REMOVE AND CLEAN LDF AFT - AREA AROUND STAIRS SMOKE 6 I: 4 C  DETECTOR.  OP 18 OPERATIONAL CHECK OF FCC SMOKE DETECTION BY MCDU. 9 I: C  N RS 19 REMOVE AND CLEAN PICCOLO TUBES OF FCC RACK SMOKE 8 I: 18000 FH  DETECTION.  N OP 20 OPERATIONAL CHECK OF ALNAV2 CENTER RACK IV SMOKE 9 I: 18 MO  DETECTION BY MCDU  N RS 21 REMOVE AND CLEAN PICCOLO TUBES OF ALNAV2 CENTER RACK 8 I: 17000 FH  IV SMOKE DETECTION.  26.18.01 BULK AVIONICS COMPARTMENT SMOKE DETECTION  RS 01 REMOVE AND CLEAN BULK AVIONICS SMOKE DETECTOR PICCOLO 8 I: 36 MO  TUBES  OP 02 OPERATIONAL CHECK OF THE BULK AVIONICS COMPARTMENT 9 I: C  SMOKE DETECTION SYSTEM VIA MCDU  26.21.00 ENGINE FIRE EXTINGUISHING  OP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING SYSTEM 9 I: 1 A  NOTE 5  OP 02 OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER BOTTLE 9 I: C  LOW PRESSURE INDICATING CIRCUIT  OP 03 OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW 8 I: 18 MO  FUNCTION  (THIS TASK COVERS TASKS 24.20.00/15, 28.24.00/02 AND  36.00.00/04)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.21.00 * * * * * C O N T I N U E * * * * *  FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,9 I: NR OR VR  PRESSURE SWITCH SETTING NOTE 8  05 TASK DELETED  06 TASK DELETED  FC 07 FUNCTIONAL CHECK OF FIRING CIRCUIT CONTINUITY 9 I: 2 C  FC 08 FUNCTIONAL CHECK OF DISTRIBUTION PIPING FOR LEAKAGE 8 I: 12000 FH  AND OBSTRUCTION  DS 09 DISCARD CARTRIDGE 9 I: VR  26.22.00 APU FIRE EXTINGUISHING  OP 01 OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM 9 I: 2 A  (THIS TASK COVERS TASK 26.13.00/01)  OP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA 9 I: 4800 FH  MCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF,  6WF)(THIS TASK COVERS TASKS 49.62.00/03 FOR A340-200  OR A340-300 AND 49.62.00/04 FOR A340-500 OR A340-600)  OP 03 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 9 I: C  TRIGGER CIRCUIT  04 TASK DELETED  FC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 7,9 I: VR  PRESSURE SWITCH SETTING OR  NR  NOTE 8  06 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.22.00 * * * * * C O N T I N U E * * * * *  OP 07 OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 9 I: 2 C  DI 08 DETAILED INSPECTION OF DISTRIBUTION PIPING FOR CRACKS 8 I: 14000 FH  OP 09 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 36 MO  OP 10 OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION 8 I: 36 MO  (THIS TASK COVERS TASKS 28.29.00/01 AND 49.62.00/04  FOR A340-200 OR A340-300 AND 49.62.00/03 FOR A340-500  OR A340-600)  DS 11 DISCARD CARTRIDGE 8 I: VR  26.23.00 LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND  BULK)  OP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW 9 I: C  PRESSURE INDICATION CIRCUIT BY PTT  DS 02 DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT 8 I: 15 MO  FC 03 REMOVE BOTTLE FOR WEIGHT CHECK 8 I: 8000 FH  OP 04 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 10000 FH  FC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST 6,9 I: VR  OR  NR  NOTE 8  FC 06 FUNCTIONAL CHECK OF PRESSURE REDUCER 8 I: 14000 FH  NOTE 24  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.23.00 * * * * * C O N T I N U E * * * * *  07 TASK DELETED  08 TASK DELETED  FC 09 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND 8 I: 14000 FH  OBSTRUCTION  10 TASK DELETED  DS 11 DISCARD CARTRIDGE UNIT 8 I: VR  DI 12 DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND 8 I: 14000 FH  CHECK VALVE NOTE 24  FC 13 FUNCTIONAL CHECK OF FLOW METERING COMPACT UNIT (FMCU) 8 I: 14000 FH  DI 14 DETAILED INSPECTION OF FLOW METERING COMPACT UNIT 8 I: 14000 FH  (RESTRICTOR, HALON FILTER AND CHECK VALVE).  DS 15 DISCARD AND REPLACE WATER ADSORBING FILTER IN FLOW 8 I: 15 MO  METERING COMPACT UNIT (FMCU).  26.24.00 PORTABLE FIRE EXTINGUISHER  FC 01 REMOVE BOTTLES FOR WEIGHT CHECK 9 I: VR  NOTE 26  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.24.00 * * * * * C O N T I N U E * * * * *  FC 02 REMOVE BOTTLES FOR HYDROSTATIC TEST 9 I: VR  OR  NR  NOTE 8  03 TASK DELETED  GVI 04 GENERAL VISUAL INSPECTION OF PORTABLE FIRE 9 I: 1000 FH  EXTINGUISHER ATTACHMENT  26.25.00 LAVATORY FIRE EXTINGUISHING  OP 01 CHECK PRESSURE OF EXTINGUISHING AGENT 9 I: C  FC 02 REMOVE BOTTLE FOR WEIGHT CHECK 9 I: 4 C  26.28.00 AUXILIARY AREAS FIRE EXTINGUISHING (CREW REST ROOM-  UNDERFLOOR)  01 TASK DELETED  OP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 8 I: 12000 CRR  CIRCUIT IN THE LDMCR FH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  DS 03 DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE 8 I: VR  IN THE LDMCR  FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,8 I: VR  PRESSURE SWITCH SETTING IN THE LDMCR OR  NR  NOTE 8  OP 05 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES FOR 8 I: 72 CRR MO  OBSTRUCTION IN THE LDMCR.  OP 06 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY 8 I: 800 CRR  IN THE LDMCR FH  OP 07 OPERATIONAL CHECK OF THE MANUAL FIRE EXTINGUISHING 9 I: 36 CRR MO  CIRCUIT IN THE LDMCR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  OP 08 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MO  IN THE LDMCR  OP 09 OPERATIONAL CHECK OF FIRE EXTINGUISHING CIRCUIT IN 8 I: 36 MO  THE BCRC  FC 10 FUNCTIONAL CHECK OF PRESSURE REDUCER IN THE BCRC 8 I: 36 MO  DI 11 DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND 8 I: 36 MO  CHECK VALVE IN THE BCRC.  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  12 TASK DELETED  DS 13 DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT 8 I: 15 MO  IN THE BCRC  OP 14 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES FOR 8 I: 36 MO  OBSTRUCTION IN THE BCRC.  15 TASK DELETED  OP 16 OPERATIONAL CHECK OF THE PRESSURE 9 I: 2 C  INDICATING CIRCUIT IN THE BCRC  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  OP 17 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY IN THE BCRC. 8 I: 700 FH  FC 18 REMOVE BOTTLE FOR HYDROSTATIC TEST IN THE LDF AFT DCR 8 I: VR OR NR  AND CHECK OF PRESSURE SWITCH SETTING. NOTE 8  OP 19 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MO  IN THE LDF AFT DCR.  OP 20 OPERATIONAL CHECK OF LDF AFT DCR 8 I: 36 CRR MO  FIRING CIRCUIT CONTINUITY.  DS 21 DISCARD CARTRIDGE UNIT LDF AFT DCR 8 I: VR  OP 22 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES 8 I: 72 CRR MO  FOR OBSTRUCTION IN LDF AFT DCR.  OP 23 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY IN THE 8 I: 700 CRR  LDF AFT DCR. FH  DS 24 DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE IN THE 8 I: VR  BCRC  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  FC 25 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF THE 6,9 I: VR  PRESSURE SWITCH SETTING IN THE BCRC. OR NR  NOTE 8  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.00.00 FLIGHT CONTROLS  27.14.00 AILERON AND HYDRAULIC ACTUATION  OP 01 OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY 8 I: 10000 FH  BITE NOTE 24  (THIS TASK COVERS TASK 29.10.00/12)  VC 02 CHECK AILERON SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FH  POSITION  FC 03 CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FH  EXCESSIVE PLAY AND GENERAL CONDITION  LU 04 LUBRICATION OF AILERON HINGE BEARINGS 9 I: 7500 FH  OR  18 MO  LU 05 LUBRICATION OF AILERON SERVO CONTROL ROLLER BEARINGS 8 I: 7500 FH  OR  18 MO  OP 06 OPERATIONAL CHECK OF FCPC AND FCSC AILERON SERVO 9 I: C  LOOPS. (COVERED BY MSI 27-90-00 TASK 6)  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.21.00 RUDDER MECHANICAL CONTROL  01 TASK DELETED  02 TASK DELETED  OP 03 OPERATIONAL CHECK OF YAW DAMPER SERVO ACTUATOR 9 I: C  STANDBY SERVO LOOP  VC 04 CHECK POINTER OF CABLE TENSION REGULATOR WITHIN 9 I: 2 C  LIMITS  OP 05 OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL 9 I: 2 C  OP 06 OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL 9 I: 2 C  LIMITATION UNITS STANDBY CHANNEL  VC 07 VISUAL CHECK OF RUDDER MECHANICAL CONTROL IN THE FIN 8 I: 20000 FH  DI 08 DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL 6,9 I: 4 C  (EXCLUDING FIN)  OP 09 OPERATIONAL CHECK OF AP ARTIFICIAL FEEL SPRING ROD 9 I: 4 C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.21.00 * * * * * C O N T I N U E * * * * *  10 TASK DELETED  FC 11 FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS 8 I: 42 MO  SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR OR  WORKSHOP CHECK 20000 FH  OP 12 OPERATIONAL CHECK OF CENTERING MECHANISM 8 I: 34000 FH  OP 13 OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE 8 I: 3200 FH  NOTE 24A  14 TASK DELETED  VC 15 VISUAL CHECK TO CONFIRM INTEGRITY OF CONTROL ROD 8 I: 20000 FH  (ITEM 220 IN IPC 272147-1A) IN PTLU LINKAGE NOTE 24A  LU 16 LUBRICATION OF RUDDER PEDALS ADJUSTMENT MECHANISM 6 I: C  17 TASK DELETED  DI 18 DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT 6 I: 4 C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.21.00 * * * * * C O N T I N U E * * * * *  OP 19 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY 9 I: 2 C  CHANNEL  (THIS TASK COVERS TASK 27.90.00/18)  OP 20 OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL 9 I: 4 C  27.24.00 RUDDER HYDRAULIC ACTUATION  LU 01 LUBRICATION OF RUDDER HINGE BEARING NO4 9 I: 7500 FH  OR  18 MO  R OP 02 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH 8 I: 800 FH  INDIVIDUAL HYDRAULIC SYSTEMS (THIS TASK COVERS TASK  29.10.00/08)  OP 03 OPERATIONAL CHECK OF RUDDER SERVO CONTROL JAMMING 9 I: 2 C  DEVICE  FC 04 CHECK RUDDER SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 34000 FH  EXCESSIVE PLAY AND GENERAL CONDITION  05 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.24.00 * * * * * C O N T I N U E * * * * *  LU 06 LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER 8 I: 7500 FH  BEARING (RUDDER SIDE) OR  18 MO  LU 07 LUBRICATION OF RUDDER HINGE BEARING NO 6 9 I: 7500 FH  OR  18 MO  OP 08 OPERATIONAL CHECK OF RUDDER DAMPING MEASUREMENT BY 9 I: 1 C  BITE NOTE 24  09 TASK DELETED  FC 10 FUNCTIONAL CHECK OF THE INDIVIDUAL RUDDER 9 I: 10000 FH  SERVOCONTROLS NOTE 24A  27.34.00 ELEVATOR AND HYDRAULIC ACTUATION  OP 01 OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY 8 I: 10000 FH  BITE OR  18 MO  NOTE 24  FC 02 CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FH  EXCESSIVE PLAY AND GENERAL CONDITION  VC 03 CHECK ELEVATOR SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FH  POSITION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.34.00 * * * * * C O N T I N U E * * * * *  LU 04 LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING 8 I: 7500 FH  OR  18 MO  OP 05 OPERATIONAL CHECK OF FCPC AND FCSC STANDBY SERVO 9 I: C  LOOPS ON PITCH CONTROL  (COVERED BY MSI 27-90-00 TASK 9 OR 12 ACCORDING TO  A/C TYPE)  LU 06 LUBRICATION OF THE DIAGONAL BAR BEARING 9 I: 7500 FH  (ELEVATOR SUPPORT STRUT) OR  18 MO  27.40.00 TRIMMABLE HORIZONTAL STABILIZER (THS)  OP 01 OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL 8 I: 800 FH  HYDRAULIC SYSTEMS NOTE 24  LU 02 LUBRICATION OF THS ACTUATOR BALL SCREW NUT 8 I: 700 FH  NOTE 24B  SV 03 CHECK OIL LEVEL OF THS ACTUATOR GEARBOX 6,9 I: 8 A  OP 04 OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION 8 I: 5600 FH  DEVICE. NOTE 24  DI 05 CHECK MAGNETIC CHIP DETECTOR OF THS ACTUATOR GEARBOX 9 I: C  DI 06 DETAILED INSPECTION OF THS ACTUATOR FAIL SAFE NUT 8 I: 12000 FH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.40.00 * * * * * C O N T I N U E * * * * *  DI 07 DETAILED INSPECTION OF UPPER THS ACTUATOR ATTACHMENT 8 I: 12000 FH  (PRIMARY AND SECONDARY) AND NO-BACK HOUSING  DI 08 DETAILED INSPECTION OF LOWER THS ACTUATOR ATTACHMENT 8 I: 12000 FH  (PRIMARY AND SECONDARY).  LU 09 LUBRICATION OF THS MECHANICAL CONTROL CHAINS 6 I: 2 C  FC 10 CHECK MOVABLE INDEX ON THS CABLE TENSION COMPENSATOR 6 I: C  SCALE IS WITHIN LIMITS.  VC 11 CHECK WEAR INDICATOR OF THS ACTUATOR NO-BACK SYSTEM 8 I: 15000 FH  FC 12 CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT 8 I: 16000 FH  (PRIMARY AND SECONDARY LOAD PATH).  OP 13 OPERATIONAL CHECK OF THS ACTUATOR NO-BACK SYSTEM 8 I: 34000 FH  DI 14 DETAILED INSPECTION OF THS MECHANICAL CONTROL LOOP 6 I: 4 C  FC 15 FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE-OFF BRAKE 9 I: 4 C  (CHECK OF STATIC TORQUE)  VC 16 VISUAL CHECK OF THS ACTUATOR DRAIN COLLECTING 9 I: 2 A  CONTAINER ASSEMBLY INCLUDING HOSES  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.40.00 * * * * * C O N T I N U E * * * * *  OP 17 OPERATIONAL CHECK OF THSA ENHANCED RUNAWAY PROTECTION 9 I: C  (ERP).  (COVERED BY MSI 27.90.00, TASK NO 17)  OP 18 OPERATIONAL CHECK OF THSA CHECKABLE SHEAR PIN. 9 I: 10000 FH  27.50.00 FLAPS  LU 01 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 4 A  BEARINGS.  SV 02 TOP UP PCU TO CONFIRM FLUID LEVEL 6 I: C  DI 03 DETAILED INSPECTION OF TRANSMISSION ASSY 6 I: 60 MO  DI 04 DETAILED INSPECTION OF CRUISE ROLLERS, FLAP TRACKS 9 I: 60 MO  AND CARRIAGES, ROTARY ACTUATORS AND ATTACHMENTS  SV 05 DRAIN AND REFILL ROTARY ACTUATOR WITH SEMI-FLUID 6 I: 60 MO  DI 06 DETAILED INSPECTION OF TRACK 4 SENSORS 9 I: 60 MO  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.50.00 * * * * * C O N T I N U E * * * * *  DI 07 DETAILED INSPECTION OF INTERCONNECTION STRUT AND 8 I: 60 MO  ATTACHMENTS  FC 08 REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YE  (THIS TASK COVERS TASK 27.80.00/05)  SV 09 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 C  GVI 10 GENERAL VISUAL INSPECTION OF FLAP TRACK FAIRING 9 I: 4 C ZL-53 SUPPORT STRUTS AND LINKAGE ZL-53 LU 11 LUBRICATION OF FLAP CARRIAGE (2 TO 5) LEVER BEARINGS 9 I: 4 A  LU 12 LUBRICATION OF STEADY BEARINGS 6 I: C  LU 13 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 2 C  BEARINGS.  OP 14 OPERATIONAL CHECK OF FLAP WTB/POB PERFOMANCE TEST. 8 I: 6400 FH  27.64.00 SPOILER HYDRAULIC ACTUATION  LU 01 LUBRICATION OF ALL SPOILER LINKAGE BEARINGS PROVIDED 9 I: C  WITH GREASE NIPPLES  DI 02 DETAILED INSPECTION OF LINKAGE AND ATTACHMENT OF 9 I: 4 C  SPOILERS 1 TO 6  27.80.00 LIFT AUGMENTING (SLATS)  LU 01 LUBRICATION OF ALL SLAT TRACK ROLLER BEARINGS, PINION 6,9 I: 2800 FH  BEARINGS, RACK AND PINION TEETH AND SLAT  TRACK 2 AND 3 LEVER BEARINGS  SV 02 TOP UP PCU GEARBOX TO CONFIRM FLUID LEVEL 6 I: C  DI 03 DETAILED INSPECTION OF SLAT TRANSMISSION ASSY 6 I: 4 C  DI 04 DETAILED INSPECTION OF SLAT TRACKS AND ROLLERS, 9 I: 4 C  PINIONS AND CURVED RACK GEARS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.80.00 * * * * * C O N T I N U E * * * * *  FC 05 REMOVAL OF CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YE  (COVERED BY MSI 27-50-00, TASK 08)  SV 06 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 C  LU 07 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE A 6 I: 4 C  (TRACK 2-3).  LU 08 LUBRICATION OF STEADY BEARINGS 6 I: C  LU 09 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE B 6 I: 4 C  (TRACK 5-16)  OP 10 OPERATIONAL CHECK OF SLAT WTB/POB PERFOMANCE TEST. 8 I: 6400 FH  27.90.00 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)  OP 01 OPERATIONAL CHECK OF TAKEOVER AND PRIORITY FUNCTION 8 I: 18 MO  OP 02 OPERATIONAL CHECK OF FCPCS AND FCSCS YAW DAMPER SERVO 9 I: C  LOOPS.  03 TASK DELETED  OP 04 OPERATIONAL CHECK OF FCPC1 AND FCSC1 POWER SUPPLY 9 I: C  OP 05 OPERATIONAL CHECK OF FCPC2 AND THS ACTUATOR 9 I: 1 C  ELECTRICAL MOTOR 2 POWER SUPPLY NOTE 24A  OP 06 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S AILERON SERVO 9 I: C  LOOPS  (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-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.90.00 * * * * * C O N T I N U E * * * * *  OP 07 OPERATIONAL CHECK OF GREEN SERVOCONTROLS TRAVEL SPEED 8 I: 18 MO  LIMITATION WHEN RAT IS EXTENDED NOTE 24  OP 08 OPERATIONAL CHECK OF RETURN TO LOW SPEED 9 I: 4 C  CONFIGURATION OF RUDDER AND PEDAL TRAVEL LIMITATION  UNITS  OP 09 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S STANDBY SERVO 9 I: 15 MO  LOOPS ON PITCH CONTROL NOTE 24A  (THIS TASK COVERS TASK 27.34.00/05 FOR A340-200 OR  A340-300)  OP 10 OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY 9 I: C  11 TASK RESERVED  OP 12 OPERATIONAL CHECK OF FCPC ́S AND FCSC ́S STANDBY SERVO 9 I: 1 C  LOOPS ON PITCH CONTROL NOTE 24B  (THIS TASK COVERS TASK 27.34.00/05 FOR A340-500 OR  A340-600)  OP 13 OPERATIONAL CHECK OF LIGHTS 9 I: 2 A  (COVERED BY MSI 33-14-00)  OP 14 OPERATIONAL CHECK OF THE BACK UP CONTROL MODULE AND 8 I: 5000 FH  BACK UP POWER SUPPLY (BCM/BPS)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 27.90.00 * * * * * C O N T I N U E * * * * *  OP 15 OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP 9 I: C  OP 16 OPERATIONAL CHECK OF RUDDER ELECTRICAL BACK UP 8 I: 5000 FH  OP 17 OPERATIONAL CHECK OF THSA ENHANCED RUNAWAY PROTECTION 9 I: C  (ERP)  (THIS TASK COVERS TASK 27.40.00/17)  OP 18 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY 9 I: 2 C  CHANNEL (COVERED BY MSI 27-21-00 TASK NO 19)  19 TASK RESERVED  20 TASK RESERVED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.00.00 FUEL  28.11.00 TANKS  OP 01 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DY  FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS NOTE 1  OP 02 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 2 MO  FROM TRIM TANK AND TRIM VENT SURGE TANK NOTE 1  OP 03 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, 9 I: C  USING INDIVIDUAL MOTORS, TO PROVE CORRECT ACTUATOR  OPERATION AND COCKPIT INDICATION  OP 04 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE 8 I: 6 YE  TO PROVE THAT NEITHER VALVE HAS JAMMED IN THE OPEN  POSITION AND TO VERIFY CORRECT OPERATION OF THE P/BSW  OP 05 OPERATIONAL CHECK OF ALL COLLECTOR CELL CLACK VALVES 9 I: 8 C  TO ENSURE FULL AND FREE MOVEMENT  06 TASK DELETED  07 TASK DELETED  08 TASK RESERVED  09 TASK RESERVED  OP 10 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, 9 I: 4 C  USING INDIVIDUAL MOTORS TO PROVE CORRECT ACTUATOR  OPERATION AND COCKPIT INDICATION  OP 11 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DY  FROM THE REAR CENTER TANK NOTE 1  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.11.00 * * * * * C O N T I N U E * * * * *  OP 12 OPERATIONAL CHECK OF THE INNER TANK 2/3 CLACK VALVES 9 I: 8 C  TO ENSURE FULL AND FREE MOVEMENT  OP 13 OPERATIONAL CHECK OF THE INNER TANK 2/3 CLACK VALVES 8 I: 6 YE  TO ENSURE THAT THEY HAVE NOT FAILED OPEN  GVI 14 GENERAL VISUAL INSPECTION OF WATER DRAIN VALVE PIPES 9 I: 8 C ZL-54 FOR SECURITY AND INTEGRITY ZL-54 28.12.00 TANK VENTING SYSTEM  VC 01 VISUAL CHECK OF THE APERTURE LEADING TO WING AND TRIM 9 I: 2 C  SURGE TANK FLAME ARRESTORS (INSIDE THE NACA INTAKES)  FOR BLOCKAGE  VC 02 VISUAL CHECK OF THE WING AND TRIM VENT SURGE TANK 9 I: 1 C  OVERPRESSURE PROTECTORS (BURST DISCS) FOR INTEGRITY NOTE 5  28.14.00 TRIM PIPE SHROUD DRAINAGE  01 TASK DELETED  02 TASK DELETED  FC 03 FUNCTIONAL CHECK OF TRIM PIPE SHROUD DRAIN LINE AND C 8 I: 36 MO  ONNECTORS WITHIN PRESSURIZED FUSELAGE (COVERED BY MSI  28.27.00 TASK NO 3)  28.16.00 FUEL RECIRCULATION FOR COOLING  NO TASK SELECTED  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.17.00 WATER SCAVANGE  01 TASK DELETED  28.18.00 IGNITION PREVENTION  DI 01 DETAILED INSPECTION OF THE WING AND TRIM TANK BONDING 9 I: 8 C  LEADS (SFAR88)  GVI 02 GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND 9 I: 8 C  PROBE ATTACHMENTS (SFAR88)  GVI 03 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS 9 I: 8 C  (SFAR88)  DI 04 DETAILED INSPECTION OF THE HEATSHIELDS BELOW THE 8 I: 6 YE  CENTER TANK (SFAR88)  VC 05 VISUAL CHECK OF CENTER TANK FOR LEAKS (SFAR88) 8 I: 700 FH  GVI 06 GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD 9 I: 4 C  CARGO BAY INSULATION MATS (SFAR88)  GVI 07 GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE 9 I: 8 C  CENTER TANK (SFAR88)  GVI 08 GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND 9 I: 8 C  TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS  (SFAR88)  GVI 09 GENERAL VISUAL INSPECTION OF TRIM TANK EXTERNAL 9 I: 8 C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.18.00 * * * * * 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 C  ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL  SUPPLY CABLE (SFAR88)  28.21.00 MAIN FUEL PUMP SYSTEM  OP 01 OPERATIONAL CHECK TO VERIFY ISOLATION OF STANDBY PUMP 8 I: 10000 FH  4 CONTROL WHEN MAIN PUMP1 IS RUNNING IN ELECTRICAL NOTE 24A  EMERGENCY CONFIGURATION  OP 02 OPERATIONAL CHECK TO VERIFY THAT RELAY 27QA HAS NOT 8 I: 15000 FH  FAILED IN THE ENERGISED POSITION  OP 03 OPERATIONAL CHECK OF STANDBY PUMP AUTOMATIC CONTROL. 9 I: C  OP 04 OPERATIONAL CHECK TO ENSURE THAT STANDBY PUMP 4 8 I: 18 MO  OPERATES WHEN MAIN PUMP 1 IS SWITCHED OFF WITH THE  AIRCRAFT IN AN ELECTRICAL EMERGENCY CONFIGURATION  05 TASK RESERVED  OP 06 OPERATIONAL CHECK TO ENSURE THAT THE MAIN FUEL PUMP 8 I: 18 MO  NO.3 OPERATES WHEN THE MAIN PUMP NO.2 IS SWITCHED OFF  WITH THE AIRCRAFT IN AN ELECTRICAL EMERGENCY  CONFIGURATION  OP 07 OPERATIONAL CHECK TO VERIFY ISOLATION OF MAIN FUEL 8 I: 10000 FH  PUMP 3 WHEN MAIN FUEL PUMP 2 IS RUNNING IN ELECTRICAL NOTE 24B  EMERGENCY CONFIGURATION  28.22.00 APU FUEL PUMP SYSTEM  01 TASK DELETED  02 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.22.00 * * * * * C O N T I N U E * * * * *  OP 03 OPERATIONAL CHECK OF FWD APU FUEL FEED PUMP 9 I: C  ACTIVATION CIRCUIT VIA LANDING GEAR LGCIU1 (5GA1)  RELAY 12QC AND MAIN BOOSTER PUMP CONTACTORS  (10QA1- 10QA4, 11QA4)  OP 04 OPERATIONAL CHECK OF AFT APU FUEL PUMP FIRE STOP 9 I: C  CIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS 5WF, 6WF  GVI 05 GENERAL VISUAL INSPECTION OF APU FUEL SHROUD LINE AND 9 I: 4 C ZL-31 FUEL/AIR SEPARATOR FOR INTEGRITY AND ABSENCE OF ZL-31 LEAK PATHS.  06 TASK RESERVED  OP 07 OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO 9 I: 2800 FH  DRAIN ANY ACCUMULATED WATER  GVI 08 GENERAL VISUAL INSPECTION OF APU FUEL LINE SHROUD AND 8 I: 6 YE  CONNECTORS  GVI 09 GENERAL VISUAL INSPECTION OF APU FUEL LINE SHROUD 8 I: 36 MO  DRAIN LINE AND CONNECTORS  OP 10 OPERATIONAL CHECK TO VERIFY THAT RELAY 15QC HAS NOT 8 I: 36 MO  FAILED IN ENERGIZED POSITION.  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.23.00 CROSSFEED SYSTEM  OP 01 OPERATIONAL CHECK OF CROSSFEED VALVES 1 AND 4 TO 9 I: 2 C  PROVE THAT NEITHER VALVE HAS JAMMED IN CLOSED  POSITION  02 TASK RESERVED  03 TASK RESERVED  OP 04 OPERATIONAL CHECK OF THE CROSSFEED VALVES INDICATION 9 I: 1 C  NOTE 24B  OP 05 OPERATIONAL CHECK OF THE CROSSFEED VALVES USING THE 9 I: 2 C  INDIVIDUAL MOTORS NOTE 24B  OP 06 OPERATIONAL CHECK OF THE EMERGENCY ELECTRICAL CONTROL 8 I: 800 FH  CROSSFEED VALVES FUNCTION  28.24.00 ENGINE LP FUEL SHUT-OFF  OP 01 OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL 9 I: 2 C  MOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT AND OR  CORRECT COCKPIT INDICATION 5000 FC  NOTE 24B  OP 02 OPERATIONAL CHECK OF THE FIRE CONTROL P/B SW 8 I: 18 MO  SUB-FUNCTIONS  (COVERED BY MSI 26.21.00, TASK NO3)  N OP 03 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL 8 I: 6500 FC  SUPPLY TO ASSOCIATED ENGINE OR  12 YE  28.25.00 REFUEL/DEFUEL SYSTEM  DI 01 DETAILED INSPECTION OF REFUEL COUPLING FOR DAMAGE OR 9 I: 3500 FC  EVIDENCE OF WEAR  02 TASK RESERVED  03 TASK RESERVED  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.26.00 MAIN TRANSFER SYSTEM  GVI 01 GENERAL VISUAL INSPECTION OF RCT TRANSFER LINE SHROUD 8 I: 36 MO  AND DRAIN LINE CONNECTORS  28.27.00 TRIM TANK TRANSFER SYSTEM  R OP 01 OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES 9 I: 2 C  FOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH NOTE 24  R 02 TASK DELETED  R FC 03 FUNCTIONAL CHECK OF TRIM TANK TRANSFER LINE SHROUD 8 I: 36 MO  CONNECTORS (THIS TASK COVERS TASK 28.14.00/03)  28.28.00 ADDITIONAL CENTER TANK TRANSFER SYSTEM  OP 01 OPERATIONAL CHECK OF THE LEAK MONITOR FOR EVIDENCE OF 9 I: 500 FH  FUEL LEAKAGE NOTE 21  OP 02 OPERATIONAL CHECK OF THE INTERSPACE OVERBOARD DRAIN 9 I: 60 MO  SYSTEM NOTE 21  OP 03 OPERATE WATER DRAIN VALVES IN THE ACT(S) TO DRAIN 9 I: 42 DY  ACCUMULATED WATER (IF ACT(S) INSTALLED) OR NR  NOTE 1  NOTE 8  FC 04 FUNCTIONAL CHECK OF THE ACT INWARD RELIEF VALVE 9 I: 60 ACT MO  NOTE 21  NOTE 23  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.28.00 * * * * * C O N T I N U E * * * * *  OP 05 OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM 9 I: 60 MO  NOTE 18  NOTE 21  NOTE 24A  FC 06 FUNCTIONAL CHECK OF ACT PRESSURE REDUCING VALVE 9 I: 60 MO  NOTE 21  OP 07 OPERATIONAL CHECK OF INDIVIDUAL MOTORS OF THE 9 I: 60 MO  TRANSFER VALVE NOTE 21  DS 08 DISCARD ACT AIR INLET FILTER 6 I: 30 MO  NOTE 21  GVI 09 GENERAL VISUAL INSPECTION OF THE ACT HEAT SHIELD 8 I: 500 FC  NOTE 21  28.29.00 APU LP FUEL SHUT-OFF  OP 01 OPERATIONAL CHECK OF APU LP FUEL SHUT OFF VALVE USING 9 I: 2 C  EACH INDIVIDUAL MOTORS VIA APU FIRE EMERGENCY STOP  RELAYS 5WF, 6WF  (COVERED BY MSI 26-22-00, TASK NO10)  28.31.00 JETTISON SYSTEM  GVI 01 GENERAL VISUAL INSPECTION OF JETTISON PIPE FLEXIBLE 9 I: 2 C  HOSE FOR SECURITY AND CONDITION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 28.31.00 * * * * * C O N T I N U E * * * * *  GVI 02 GENERAL VISUAL INSPECTION OF ANTI-CORONA DEVICE FOR 9 I: 2 C  SECURITY OF ATTACHMENT AND FOR SATISFACTORY CONDITION  OP 03 OPERATIONAL CHECK TO VERIFY CORRECT RESPONSE OF 9 I: 4 C  JETTISON SYSTEM TO SELECTION OF JETTISON "ON"  28.42.00 QUANTITY INDICATING  NO TASK SELECTED  28.46.00 TANK LEVEL SENSING  01 TASK DELETED  OP 02 OPERATIONAL CHECK OF INNER TANK LOW LEVEL SENSORS AND 8 I: 10000 FH  ASSOCIATED WARNINGS  28.49.00 FUEL TEMPERATURE MEASUREMENT  OP 01 INTERROGATION OF FCMS GROUND REPORT PAGE FOR FAILURE 8 I: 10000 FH  OF OUTER TANK AND TRIM TANK TEMPERATURE SENSOR  28.51.00 FUEL CONTROL AND MONITORING  OP 01 INTERROGATION OF FCMS GROUND REPORT PAGE FOR FCMC 1 8 I: 10000 FH  (2) FAULT  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 29.00.00 HYDRAULIC POWER  29.10.00 MAIN HYDRAULIC POWER  FC 01 CHECK NITROGEN CHARGING PRESSURE ON HYDRAULIC POWER 9 I: 400 FH  ACCUMULATORS  VC 02 CHECK CLOGGING INDICATORS OF HIGH PRESSURE (HP), 9 I: A  RETURN, ENGINE DRIVEN PUMPS (EDP) CASE DRAIN,  RESERVOIR FILL AND AIR PRESSURIZATION UNIT (PUA)  FILTERS  SV 03 DRAINING OF WATER SEPARATORS 9 I: A  SV 04 SERVICING OF LEAKAGE RECOVERY TANKS 9 I: 2 A  OP 05 OPERATIONAL CHECK OF EDP DEPRESSURIZATION 9 I: C  DI 06 CHECK FOR CORRECT AIR PRESSURE BY READING GAUGES ON 6 I: C  EACH RESERVOIR  FC 07 FUNCTIONAL CHECK OF PRIORITY VALVE 6,9 I: 4 C  R OP 08 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH GREEN 8 I: 18 MO  HYDRAULIC SYSTEM PRESSURIZED  (COVERED BY MSI 27-24-00 TASK NO 2)  OP 09 OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT-OFF VALVES 8 I: 18 MO  OP 10 OPERATIONAL CHECK OF AUTOMATIC CONTROL OF FIRE 8 I: 18 MO  SHUT-OFF VALVE IN CASE OF LOW LEVEL ON GREEN  HYDRAULIC SYSTEM  FC 11 HYDRAULIC FLUID ANALYSIS 9 I: 2 C  OP 12 OPERATIONAL CHECK OF AILERON SERVOCONTROL WITH GREEN 9 I: 12500 FH  HYDRAULIC SYSTEM  (COVERED BY MSI 27-14-00 TASK NO 01)  FC 13 FUNCTIONAL CHECK OF GREEN LOW LEVEL WARNING SYSTEM 8 I: 12000 FH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 29.10.00 * * * * * 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 C  LEAK MEASUREMENT SOLENOID VALVE  FC 15 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 6 I: 4 C  YELLOW AND BLUE HYDRAULIC SYSTEMS  FC 16 REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK 8 I: 6 YE  GVI 17 GENERAL VISUAL INSPECTION OF SEAL DRAIN SYSTEM 9 I: 4 C ZL-14 ZL-14 ZL-19 ZL-19 ZL-19 FC 18 REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YE  FC 19 REMOVE SLAT PCU HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YE  OP 20 OPERATIONAL CHECK OF AUTOMATIC EDP DEPRESSURIZATION 9 I: C  THROUGHT FADEC (ECC) CONTROL  VC 21 VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN 9 I: A  VALVE POSITION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 29.10.00 * * * * * C O N T I N U E * * * * *  OP 22 OPERATIONAL CHECK OF AUTO CLOSURE OF FIRE SHUT OFF 8 I: 18 MO  VALVES IN CASE OF LOW LEVEL ON GREEN HYDRAULIC SYSTEM  AND ENGINE BURST SIGNAL  FC 23 FUNCTIONAL CHECK OF ENGINE BURST DETECTION 8 I: 18 MO  (THIS TASK COVERS TASK 29.20.00/09)  FC 24 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE IN 6 I: 10000 FH  GREEN SYSTEM  (COVERED BY MSI 29-20-00 TASK NO 08)  29.20.00 AUXILIARY HYDRAULIC POWER  OP 01 OPERATIONAL CHECK OF GREEN, YELLOW AND BLUE ELECTRIC 9 I: 4 A  PUMPS  OP 02 OPERATIONAL CHECK OF AUTOMATIC START OF GREEN AND 9 I: 4 A  YELLOW ELECTRIC PUMPS  OP 03 OPERATIONAL CHECK OF AUTOMATIC RAT DEPLOYMENT 8 I: 18 MO  04 TASK DELETED  DI 05 DETAILED INSPECTION OF RAT IN DEPLOYED POSITION 8 I: 18 MO  FC 06 OPERATIONAL CHECK OF MANUAL RAT DEPLOYMENT FOLLOWED 8 I: 18 MO  BY FUNCTIONAL CHECK OF RAT OPERATION AND INSPECTION NOTE 24  OF FILTER ELEMENT BY REFERENCE TO DIFFERENTIAL  PRESSURE INDICATOR.  FC 07 FUNCTIONAL CHECK OF GREEN AND BLUE LOW LEVEL WARNING 8 I: 12000 FH  SYSTEM (THIS TASK COVERS TASK 29.10.00/13)  FC 08 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 8 I: 10000 FH  GREEN 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-29 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 29.20.00 * * * * * C O N T I N U E * * * * *  FC 09 FUNCTIONAL CHECK OF ENGINE BURST DETECTION 8 I: 18 MO  (COVERED BY MSI 29-10-00 TASK NO 23)  10 TASK RESERVED  N DI 11 DETAILED INSPECTION RAT CASE DRAIN BOTTLE 9 I: 72 MO  N SV 12 SERVICING OF RAT CASE DRAIN BOTTLE 9 I: 10000 FH  OR  18 MO  29.30.00 INDICATING  OP 01 CROSS CHECK FLUID LEVEL ON EACH RESERVOIR, ON ECAM 9 I: 2 A  HYDRAULIC PAGE AND GROUND SERVICE PANEL INDICATOR  OP 02 OPERATIONAL CHECK OF OVERHEAT DETECTION SYSTEM 9 I: C  OP 03 OPERATIONAL CHECK OF RESERVOIRS LOW AIR PRESSURE 9 I: C  WARNING  * * * * * E N D * * * * *  ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 30.00.00 ICE AND RAIN PROTECTION  30.11.00 WING ICE PROTECTION  DI 01 DETAILED INSPECTION OF TELESCOPIC DUCTS, FLEXIBLE 9 I: 2 C  SLAT INTERCONNECTION SLEEVES AND, IN WING LEADING  EDGE, ANTI-ICING DUCT COUPLINGS, CLAMPS AND  ATTACHMENT POINTS  30.21.04 ENGINE AIR INTAKE ICE PROTECTION  DI 01 DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY 6 I: C  DUCTS AND ASSOCIATED HARDWARE IN CORE AND FAN  COMPARTMENTS  OP 02 OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE PROTECTION 9 I: 2 C  FAULT WARNING  GVI 03 GENERAL VISUAL INSPECTION OF INLET COWL ANTI-ICE 9 I: 4 C ZL-41 SUPPLY DUCT (BETWEEN SWIRL NOZZLE AND AFT BULKHEAD)  30.21.05 ENGINE AIR INTAKE ICE PROTECTION  GVI 01 GENERAL VISUAL INSPECTION OF THE NOSE COWL ANTI ICE 9 I: C  DUCT  30.31.00 PROBE ICE PROTECTION  NO TASK SELECTED  30.42.00 WINDSHIELD ANTI-ICING AND DEFOGGING  NO TASK SELECTED  30.45.00 WINDSHIELD RAIN PROTECTION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 30.45.00 * * * * * C O N T I N U E * * * * *  01 TASK DELETED  02 TASK DELETED  30.46.00 ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTION  OP 01 OPERATIONAL CHECK OF ESCAPE SLIDE LOCKING MECHANISM 9 I: C  ICE PROTECTION  30.70.00 WATER LINES  NO TASK SELECTED  30.81.00 ICE DETECTION  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 31.00.00 INDICATING/RECORDING SYSTEMS  31.21.00 ELECTRICAL CLOCK  DS 01 DISCARD CLOCK BATTERY 9 I: VR  31.33.00 DIGITAL FLIGHT DATA RECORDING SYSTEM (DFDRS)  R DS 01 DISCARD ULB BATTERY. 9 I: VR  R OP 02 OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU. 9 I: 1 C  NOTE 8  R OP 03 OPERATIONAL CHECK OF THE ULB. 9 I: VR  31.36.00 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)  NO TASK SELECTED  31.36.01 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)  R DS 01 DISCARD ULB BATTERY 9 I: VR  R OP 02 OPERATIONAL CHECK FOR DFDR SYSTEM BY USING MCDU 9 I: 1 C  NOTE 8  R OP 03 OPERATIONAL CHECK OF ULB. 9 I: VR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 31.36.01 * * * * * C O N T I N U E * * * * *  N OP 04 OPERATIONAL CHECK OF WGL-QAR/DAR INTERLOCK AND 8 I: 24000 FH  TRANSMISSION LOGIC.  31.44.00 WEIGHT AND BALANCE SYSTEM (IF INSTALLED)  NO TASK SELECTED  31.50.00 CENTRAL WARNING SYSTEM  OP 01 OPERATIONAL CHECK OF ATTENTION GETTER LIGHTS 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1).  OP 02 OPERATIONAL CHECK OF AUTOLAND LIGHTS 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  OP 03 OPERATIONAL CHECK OF SLAT AND FLAP SENSOR CIRCUIT VIA 8 I: 34000 FH  MCDU  OP 04 OPERATIONAL CHECK OF DMC OUTPUT CIRCUITS TO FWC ́S 8 I: 34000 FH  31.60.00 ELECTRONIC INSTRUMENT SYSTEM  OP 01 OPERATIONAL CHECK OF PFD/ND AND ECAM/ND MANUAL 9 I: C  TRANSFER  OP 02 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 9 I: C  OP 03 OPERATIONAL CHECK OF CORRECT EFIS AND ECAM TRANSFER 9 I: 2 C  WHEN BUSBAR 105XP IS LOST  04 TASK DELETED  OP 05 OPERATIONAL CHECK OF EFIS OFFSIDE AND ECAM NON ACTIVE 8 I: 34000 FH  MONITORING CIRCUITS  31.60.01 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD TECHNOLOGY)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 31.60.01 * * * * * C O N T I N U E * * * * *  OP 01 OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL 9 I: C  TRANSFER  OP 02 OPERATIONAL CHECK OF BRIGHTNESS CONTROL THROUGH MCDU 9 I: C  OP 03 OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN 9 I: 2 C  BUSBAR 105XP IS LOST  OP 04 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 8 I: 18 MO  * * * * * E N D * * * * *  ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.00.00 LANDING GEAR  32.11.00 MAIN GEAR  LU 01 LUBRICATION OF MAIN GEAR 6,9 I: 500 FC  OR  4 MO  LU 02 LUBRICATION OF SHORTENING MECHANISM HINGE JOINTS 5 I: 500 FC  OR  4 MO  FC 03 CHECK OF SHOCK ABSORBER NITROGEN CHARGE PRESSURE 6 I: C  SV 04 SERVICE MLG SHOCK ABSORBER 6 I: 2 C  FC 05 CHECK MAIN GEAR TORQUE LINKS FOR EXCESSIVE PLAY 6 I: 2 C  RS 06 RESTORATION OF MAIN GEAR 5 I: NOTE 7  OP 07 REMOVE HYDRAULIC FUSE IN MLG BOGIE PITCH TRIMMER 9 I: 10 YE  SUPPLY LINE FOR OPERATIONAL CHECK IN WORKSHOP.  GVI 08 GENERAL VISUAL INSPECTION OF PITCH TRIMMER AND 6 I: A ZL-73 ASSOCIATED PIPING AND COMPONENTS  GVI 09 GENERAL VISUAL INSPECTION OF SHOCK ABSORBER SLIDING 6 I: A  MEMBER FOR SIGNS OF LEAKAGE AND NORMAL EXTENSION  10 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.11.00 * * * * * C O N T I N U E * * * * *  LU 11 LUBRICATION OF MLG 6,9 I: 500 FC  OR  4 MO  FC 12 FUNCTIONAL CHECK OF MLG TORQUE LINKS FOR EXCESSIVE 9 I: 2 C  PLAY  RS 13 REMOVE MLG FOR RESTORATION 5,9 I: NOTE 7  FC 14 FUNCTIONAL CHECK OF SHOCK ABSORBER NITROGEN CHARGE 8 I: 36 HRS  PRESSURE (ELAPSED)  SV 15 SERVICE MLG SHOCK ABSORBER 8 I: 36 MO  VC 16 VISUAL CHECK OF MLG SHOCK ABSORBER SLIDING TUBE FOR 8 I: 800 FH  SIGNS OF LEAKAGE AND NORMAL EXTENSION  LU 17 LUBRICATE SHORTENING MECHANISM HINGE JOINTS 5 I: 500 FC  OR  4 MO  OP 18 REMOVE HYDRAULIC FUSE IN MLG BOGIE PITCH TRIMMER 9 I: 10 YE  SUPPLY LINE FOR OPERATIONAL CHECK IN WORKSHOP  VC 19 VISUAL CHECK OF PITCH TRIMMER AND ASSOCIATED PIPING 9 I: A  AND COMPONENTS  32.15.00 CENTERLINE GEAR  FC 01 FUNCTIONAL CHECK OF SHOCK ABSORBER NITROGEN CHARGE 9 I: 36 HRS  PRESSURE BY READING BOTTOM AND TOP GAUGES (ELAPSED)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.15.00 * * * * * C O N T I N U E * * * * *  LU 02 LUBRICATION OF CENTERLINE GEAR. 6,8 I: 500 FC  OR  4 MO  FC 03 FUNCTIONAL CHECK CLG TORQUE LINKS FOR EXCESSIVE PLAY 9 I: 2 C  SV 04 SERVICE CLG SHOCK ABSORBER 9 I: 2 C  RS 05 REMOVE CENTERLINE GEAR FOR RESTORATION 9 I: NOTE 7  VC 06 VISUAL CHECK OF CENTERLINE SHOCK ABSORBER FOR SIGNS 9 I: A  OF LEAKAGE  07 TASK DELETED  OP 08 OPERATIONAL CHECK OF HYDRAULIC FUSE IN CLG PITCH 9 I: 10 YE  TRIMMER SUPPLY LINE  09 TASK DELETED  SV 10 SERVICE CLG SHOCK ABSORBER 8 I: 36 MO  FC 11 FUNCTIONAL CHECK OF CLG SHOCK ABSORBER NITROGEN 8 I: 36 HRS  CHARGE PRESSURE BY READING BOTTOM AND TOP GAUGES (ELAPSED)  RS 12 RESTORATION OF CENTERLINE GEAR 6,8 I: NOTE 7  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.15.00 * * * * * C O N T I N U E * * * * *  VC 13 VISUAL CHECK OF CLG SHOCK ABSORBER FOR SIGNS OF 8 I: 800 FH  LEAKAGE  FC 14 FUNCTIONAL CHECK CLG TORQUE LINKS FOR EXCESSIVE PLAY 8 I: 36 MO  32.21.00 NOSE GEAR  LU 01 LUBRICATION OF NOSE LANDING GEAR. 6 I: 500 FC  OR  4 MO  FC 02 CHECK NOSE GEAR SHOCK ABSORBER NITROGEN CHARGE 6 I: C  PRESSURE  FC 03 FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE 6 I: 2 C  PLAY  SV 04 SERVICE NLG SHOCK ABSORBER 6 I: 2 C  RS 05 REMOVE NOSE GEAR FOR RESTORATION 6 I: NOTE 7  (THIS TASK COVERS TASK 32.50.00/03).  GVI 06 GENERAL VISUAL INSPECTION OF NOSE GEAR FOR SIGNS OF 6 I: A  LEAKAGE AND NORMAL EXTENSION  07 TASK DELETED  32.30.00 EXTENSION AND RETRACTION POSITION AND WARNING  LU 01 LUBRICATION OF ALL GEAR UP-LOCKS, DOOR UP-LOCK UNITS 6,8 I: 500 FC  AND PINS AND DOOR HINGES OR  4 MO  02 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.30.00 * * * * * C O N T I N U E * * * * *  LU 03 LUBRICATE ALL GEAR DOWN LOCK PIVOT PINS 5,8 I: 500 FC  OR  4 MO  VC 04 VISUAL CHECK OF DOWNLOCK SPRINGS ON ALL LANDING GEARS 9 I: 2 A  05 TASK DELETED  OP 06 OPERATIONAL CHECK OF LANDING GEAR INDICATION CIRCUITS 9 I: C  TO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGS  OPERATE  07 TASK DELETED  OP 08 OPERATIONAL CHECK OF LANDING GEAR FREE-FALL SYSTEM 8 I: 8000 FH  FOR CORRECT OPERATION OF UP-LOCK RELEASE NOTE 24B  OP 09 OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK 9 I: 4 C  (AIRCRAFT ON WHEELS)  OP 10 OPERATIONAL CHECK OF GROUND DOORS CLOSURE INHIBIT 9 I: 4 C  FC 11 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE CLOSES 9 I: 4 C  AT 280 KTS  FC 12 FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION 8 I: 6 YE  GVI 13 GENERAL VISUAL INSPECTION OF LANDING GEAR HYDRAULIC 6 I: A ZL-71 SYSTEM FOR SIGNS OF EXTERNAL LEAKAGE ZL-73 ZL-75 ZL-75 14 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.30.00 * * * * * C O N T I N U E * * * * *  LU 15 LUBRICATE ALL LANDING GEAR UP-LOCK AND DOOR UP-LOCK 5 I: 500 FC  UNITS AND PINS AND DOOR HINGES OR  4 MO  FC 16 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE OPENS 8 I: 6 YE  BELOW 280 KTS  FC 17 FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION 8 I: 6 YE  NOTE 24B  FC 18 FUNCTIONAL CHECK OF LANDING GEAR EXTENSION 9 I: 4 C  FC 19 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE CLOSES 8 I: 6 YE  AT 280 KTS  32.40.00 WHEELS AND BRAKES  VC 01 CHECK HEAT PACK WEAR INDICATOR 9 I: 7 DY  (PARKING BRAKE APPLIED)  FC 02 CHECK TYRE PRESSURES 9 I: 3 DY  FC 03 PERFORM CROSS-CHECK OF TPIS AND TYRE PRESSURE GAUGE 9 I: A  READING  FC 04 FUNCTIONAL CHECK OF NORMAL AND ALTERNATE BRAKE RETURN 6,9 I: 2 A  ACCUMULATORS NITROGEN PRESSURES BY READING GAUGES  FC 05 CHECK FLUID LEVEL OF BRAKE LOW PRESSURE RESERVOIR 6 I: C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.40.00 * * * * * C O N T I N U E * * * * *  FC 06 FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON 9 I: A  ALTERNATE PARKING BRAKE ACCUMULATORS BY READING  GAUGES  GVI 07 GENERAL VISUAL INSPECTION OF TYRES 6,9 I: 36 HRS  (ELAPSED)  GVI 08 GENERAL VISUAL INSPECTION OF WHEELS 9 I: 36 HRS  (ELAPSED)  VC 09 VISUAL CHECK OF BRAKES FOR HYDRAULIC LEAKS 9 I: 36 HRS  (ELAPSED)  OP 10 OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE 9 I: 4 A  SV 11 DRAIN WATER ACCUMULATION IN THE DRAIN TUBE OF BRAKE 9 I: 4 A  DISTRIBUTION DUAL VALVE (BDDV)  FC 12 CHECK TYRE PRESSURES USING TPIS AND MCDU 6 I: 36 HRS  (ELAPSED)  OP 13 OPERATIONAL CHECK OF PARKING BRAKE CONTROL VALVE 9 I: C  MOTORS 1 AND 2  OP 14 OPERATIONAL CHECK OF THE NORMAL AND ALTERNATE BRAKE 9 I: 10 YE  MANIFOLD HYDRAULIC SAFETY VALVES  OP 15 REMOVE THE ALTERNATE BRAKE FUSE MANIFOLD HYDRAULIC 9 I: 10 YE  SAFETY VALVES FOR AN OPERATIONAL CHECK IN THE  WORKSHOP  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 32.40.00 * * * * * C O N T I N U E * * * * *  OP 16 OPERATIONAL CHECK OF THE AUTOBRAKE SELECTOR SWITCH 8 I: 800 FH  32.50.00 STEERING  LU 01 LUBRICATION OF NOSE LANDING GEAR ROTATING SLEEVE 6 I: 500 FC  OR  4 MO  FC 02 CHECK NITROGEN PRESSURE ON NOSE WHEEL STEERING 9 I: C  ACCUMULATOR  RS 03 REMOVE NOSE LANDING GEAR FOR RESTORATION 9 I: NOTE 7  (COVERED BY MSI 32-21-00, TASK NO5)  32.53.00 NOSE LANDING GEAR-STEERING ANGLE PROTECTION (MOD 43442)  OP 01 OPERATIONAL CHECK OF COCKPIT AND NLG WARNING LAMPS 9 I: A  FC 02 FUNCTIONAL CHECK OF OVERSTEER INDICATION SYSTEM 9 I: C  * * * * * E N D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 33.00.00 LIGHTS  33.14.00 ANNUNCIATOR LIGHT TEST AND DIMMING  OP 01 OPERATIONAL CHECK OF LIGHTS 9 I: 2 A  (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 LIGHTS  NO TASK SELECTED  33.48.00 ANTI-COLLISION/STROBE LIGHTING  NO TASK SELECTED  33.51.00 CABIN EMERGENCY LIGHTING  OP 01 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA MCDU 9 I: 2 A  OP 02 BATTERY CAPACITY CHECK VIA MCDU 9 I: 6 MO  NOTE 26  OP 03 OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM 9 I: 2 C  AUTOMATIC CONTROL CIRCUIT AND MANUAL ACTIVATION FROM  BOTH CONTROL PANELS AND CHECK ALL LIGHTS AND SIGNS  ILLUMINATED BY BATTERIES  04 TASK DELETED  OP 05 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA THE EPSU 9 I: 2 A  TEST PUSHBUTTON.  OP 06 REMOVE BATTERY FOR CAPACITY CHECK. 9 I: 6 MO  NOTE 26  * * * * * E N D * * * * *  ISSUE: JUL 01/10 LIGHTS SECTION: C-33 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 34.00.00 NAVIGATION  34.13.00 AIR DATA  OP 01 OPERATIONAL CHECK OF ADR SYSTEM LIGHT 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  OP 02 OPERATIONAL CHECK OF PITOT PROBES HEATING (115 VAC) 9 I: 2 C  AND ADR/AOA POWER SUPPLY (26 VAC) IN EMERGENCY  CONFIGURATION  RS 03 FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES 6 I: 24 MO  NOTE 1  FC 04 LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS 6 I: 2 C  N OP 05 OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY 8 I: 12000 FH  34.14.00 ATTITUDE, HEADING AND POSITION  OP 01 OPERATIONAL CHECK OF THE IR SYSTEM LIGHT 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  OP 02 OPERATIONAL CHECK OF ATT/HDG SWITCHING 9 I: C  OP 03 OPERATIONAL CHECK OF ADIRU 1, 2 AND 3 POWER SUPPLY IN 9 I: 2 C  EMERGENCY CONFIGURATION  34.21.00 ALTITUDE AND AIRSPEED STANDBY DATA  RS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MO  NOTE 1  FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 C  34.22.00 ATTITUDE AND HEADING STANDBY DATA  NO TASK SELECTED  34.22.20 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 NAVIGATION SECTION: C-34 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 34.22.20 * * * * * C O N T I N U E * * * * *  RS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MO  NOTE 1  FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 C  OP 03 OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY 8 I: 800 FH  34.35.00 HEAD-UP DISPLAY (HUD) (IF INSTALLED)  NO TASK SELECTED  34.36.00 INSTRUMENT LANDING SYSTEM (ILS)  NO TASK SELECTED  34.36.01 MULTI-MODE RECEIVER (MMR)  DS 01 DISCARD AND REPLACE THE 2 COAXIAL CABLES FROM GLIDE 6 I: 5000 FC  ANTENNA 2 LOCATED ON NLG  DI 02 DETAILED INSPECTION OF NLG, NLG BAY BONDING LEADS AND 6 I: 2 C  G/S HEAT ELASTOMETRIC TUBING  34.41.00 WEATHER RADAR SYSTEM  FC 01 REMOVE RADOME FOR RADIO ELECTRICAL TEST 9 I: 30 MO  34.42.00 RADIO ALTIMETER  OP 01 OPERATIONAL CHECK OF FAN 9 I: NOTE  NOTE:  -36 MONTHS FOR COLLINS RA (POST 41510)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 NAVIGATION SECTION: C-34 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 34.42.00 * * * * * 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 SELECTED  34.48.00 TERRAIN AWARNESS AND WARNING SYSTEM (INCLUDING (E)GPWS AND  T2CAS-TAWS)  R OP 01 OPERATIONAL CHECK OF GPWS LIGHT 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1).  R OP 02 OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM 9 I: 2 C  34.51.00 DISTANCE MEASURING EQUIPMENT (DME)  NO TASK SELECTED  34.52.00 ATC MODE S (SELECT)  OP 01 OPERATIONAL CHECK OF ATC SYSTEM LIGHT 9 I: 2 A  (COVERED BY MSI 33-14-00, TASK NO1)  OP 02 OPERATIONAL CHECK OF THE REMOTE ATC SYSTEM 8 I: 24000 FH  34.53.00 AUTOMATIC DIRECTION FINDER (ADF)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 NAVIGATION SECTION: C-34 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 34.53.00 * * * * * C O N T I N U E * * * * *  R OP 01 OPERATIONAL CHECK OF ADF 1 IN EMERGENCY CONFIGURATION 9 I: C  34.55.00 VOR/MARKER  R OP 01 OPERATIONAL CHECK OF VOR 1 IN EMERGENCY CONFIGURATION 9 I: C  34.58.00 SATELLITE NAVIGATION (IF INSTALLED)  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NAVIGATION SECTION: C-34 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.00.00 OXYGEN  35.10.00 CREW OXYGEN  R VC 01 VISUAL CHECK OF OXYGEN MASKS (OUT OF BOX WITH 9 I: 18 MO  INFLATED HARNESS)  R RS 02 CLEANING OF OXYGEN MASKS 8 I: 18 MO  OP 03 OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK 8 I: 18 MO  NOTE 5  R FC 04 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6,9 I: 72 MO  FUNCTIONAL CHECK OF CYLINDER PRESSURE GAUGE. OR NR  OR VR  R FC 05 REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK 8 I: 72 MO  N FC 06 REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL 8 I: 72 MO  CHECK.  N FC 07 CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN 8 I: 6500 FH  FILL PANEL AND GAUGES ON OXYGEN CYLINDERS. OR  24 MO  35.20.01 PASSENGER OXYGEN (CHEMICAL)  FC 01 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE 9 I: 4 C  DI 02 DETAILED INSPECTION OF OXYGEN MASKS 9 I: 4 C  NOTE 27  OP 03 OPERATIONAL CHECK OF MANUAL MASK RELEASE 8 I: 6 YE  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.20.01 * * * * * C O N T I N U E * * * * *  VC 04 VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS 8 I: 6 YE  OF DISCHARGE  DS 05 DISCARD CHEMICAL OXYGEN GENERATORS 8 I: VR  OP 06 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 C  INTERRUPTION  VC 07 VISUAL CHECK OF CRR CHEMICAL OXYGEN GENERATORS FOR 8 I: 6 YE  SIGNS OF DISCHARGE. NOTE 26  DS 08 DISCARD CRR CHEMICAL OXYGEN GENERATORS. 8 I: VR  NOTE 26  35.20.02 PASSENGER OXYGEN (GASEOUS)  FC 01 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6 I: NR OR VR  FUNCTIONAL CHECK OF PRESSURE REDUCER NOTE 8  NOTE 24A  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  VC 02 CROSS-CHECK OF QUANTITY INDICATIONS ON ECAM 8 I: 1400 FH  "DOOR/OXY"-PAGE, OXYGEN FILL PANEL AND OXYGEN  CYLINDERS  FC 03 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION 8 I: 18 MO  R OP 04 OPERATIONAL CHECK OF SYSTEM SHUT-OFF VALVES (MOD 8 I: 18 MO  40257)/ PRESSURE REGULATORS (MOD 48635/48728/55606)  OPENING  OP 05 OPERATIONAL CHECK OF MANUAL SYSTEM OPERATION 8 I: 18 MO  R OP 06 OPERATIONAL CHECK OF "SYS ON" LIGHT BY ANNUNCIATOR 9 I: 1600 FH  LIGHT TEST  (COVERED BY MSI 33-14-00 TASK NO1)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R OP 07 OPERATIONAL CHECK OF OXYGEN CONTAINER OPENING AND 8 I: 30 MO  VENT FUNCTION OF BLEED/VENT VALVE  R FC 08 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY 8 I: 30 MO  CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEM  VC 09 VISUAL CHECK OF OVERBOARD DISCHARGE LINE FOR DAMAGE 8 I: 60 MO  R DI 10 DETAILED INSPECTION OF OXYGEN MASK ASSEMBLIES 8 I: 6 YE  R OP 11 OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICES 8 I: 60 MO  IN OXYGEN MASK CONTAINERS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R FC 12 REMOVE RISER LINE SHUT-OFF VALVES FOR FUNCTIONAL 8 I: 60 MO  CHECK  R OP 13 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM 8 I: 60 MO  OP 14 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 C  INTERRUPTION  R FC 15 REMOVE PRESSURE RELIEF VALVE FOR FUNCTIONAL CHECK 9 I: 60 MO  R FC 16 REMOVE PRESSURE REGULATOR FOR PRESSURE REGULATING 8 I: 60 MO  AND LEAKAGE TEST IN THE SHOP  OP 17 OPERATIONAL CHECK OF CYLINDER VALVE SWITCH 9 I: 4 C  35.30.00 PORTABLE OXYGEN  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 35.30.00 * * * * * C O N T I N U E * * * * *  VC 01 VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION 8 I: 8 DY  OF PROTECTIVE BREATHING EQUIPMENT NOTE 26  VC 02 CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE 9 I: 8 DY  R FC 03 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 9 I: NR  OR  VR  R DS 04 DISCARD PROTECTIVE BREATHING EQUIPMENT 8 I: VR  NOTE 26  R VC 05 VISUAL CHECK OF OXYGEN CYLINDER ATTACHMENT 9 I: 72 MO  N DI 06 DETAILED VISUAL INSPECTION OF THE CONTINOUS FLOW 9 I: 24 MO  MASK  N FC 07 REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR 9 I: VR  HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OXYGEN OR  REGULATOR. NR  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 36.00.00 PNEUMATIC  36.00.00 PNEUMATIC  DI 01 REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION 6 I: 4800 FH  OP 02 OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE 9 I: 4000 FC  FC 03 FUNCTIONAL CHECK OF OVERPRESSURE VALVE 9 I: 2 C  OP 04 OPERATIONAL CHECK OF CLOSING SIGNAL TO TEMPERATURE 9 I: C  LIMITATION 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-52 VENTILATION SYSTEM FOR BLOCKAGE AND DAMAGE ZL-52 06 TASK RESERVED  R DI 07 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: C  SDI 08 SPECIAL DETAILED INSPECTION OF APU BLEED CHECK VALVE 8 I: 2500 FH  R DI 09 DETAILED INSPECTION OF THE APU ENVELOPE DUCT. 8 I: 72 MO  10 TASK DELETED  DI 11 REMOVE APU BLEED CHECK VALVE FOR DETAILED VISUAL 8 I: 3300 FC  INSPECTION.  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 36.00.00 * * * * * C O N T I N U E * * * * *  N DI 12 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: 10000 FC  N DS 13 DISCARD OF APU BLEED CHECK VALVE 8 I: 10000 FC  * * * * * E N D * * * * *  ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 38.00.00 WATER/WASTE  38.10.00 POTABLE  R RS 01 DISINFECTION OF POTABLE WATER SYSTEM. 9 I: 3 MO  NOTE 8  N DS 02 DISCARD WATER FILTER CARTRIDGE OF THE LAVATORIES 7,9 I: 3 MO  NOTE 8  N DS 03 DISCARD WATER FILTER CARTRIDGE OF THE GALLEYS 7,9 I: 3 MO  NOTE 8  38.31.00 TOILET SYSTEM  01 TASK DELETED  GVI 02 GENERAL VISUAL INSPECTION OF WASTE TANKS AND WASTE 9 I: 4 C ZL-17 DRAIN LINES ZL-17 ZL-17 DS 03 DISCARD WATER SEPARATOR. 9 I: 4 A  NOTE 1  RS 04 CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING 6 I: 350 FH  AGENT AND CRUSHED ICE. NOTE 1  D 05 TASK RESERVED  RS 06 CLEANING OF FILTER OF POLAR CAP ASSY 9 I: 4 A  NOTE 1  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 38.31.00 * * * * * C O N T I N U E * * * * *  D 07 TASK RESERVED  N RS 08 CLEANING OF LIQUID LEVEL SENSOR. 7 I: C  N RS 09 CLEANING OF RINSE NOZZELS. 9 I: 4 A  NOTE 1  N RS 10 CLEANING OF WASTE TANKS AND WASTE DRAIN LINES. 6,9 I: C  N RS 11 CLEANING OF REFERENCE PRESSURE LINE LIQUIDE LEVEL 7 I: 4 A  TRANSMITTER. NOTE 1  N RS 12 CLEANING OF ABSOLUTE PRESSURE SENSORS (HAPS, AAPS) 7 I: 4 A  NOTE 1  N 13 TASK RESERVED  38.32.00 WASTE WATER DRAIN  GVI 01 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN LINES 9 I: 4 C ZL-13 IN BILGE AREA FOR LEAKAGE. ZL-13 ZL-15 ZL-15 ZL-15 ZL-17 ZL-17 ZL-17 GVI 02 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN LINES 9 I: 8 C ZL-13 IN CARGO COMPARTMENTS FOR LEAKAGE. ZL-13 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 38.32.00 * * * * * C O N T I N U E * * * * *  ZL-15 ZL-15 ZL-15 ZL-16 ZL-16 RS 03 CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE 7 I: 600 FH  38.40.00 AIR SUPPLY  DI 01 DETAILED INSPECTION OF COMPRESSOR INLET FILTER 9 I: 2 C  DS 02 DISCARD SYSTEM FILTER ELEMENT 6,9 I: 4 C  DS 03 DISCARD COMPRESSOR OUTLET FILTER ELEMENT 9 I: 4 C  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 45.00.00 ONBOARD MAINTENANCE SYSTEM  45.10.00 CENTRAL MAINTENANCE SYSTEM (CMS)  01 TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ONBOARD MAINTENANCE SYSTEM SECTION: C-45 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 46.00.00 INFORMATION SYSTEMS  46.11.00 FLYSMART WITH AIRBUS  N RS 01 CALIBRATION OF BASE TRANSCEIVER STATION 7 I: VR  46.11.34 SIU (SERVER INTERFACE UNIT)  NO TASK SELECTED  46.21.00 ATIMS  NO TASK SELECTED  46.21.01 ATIMS FANS CONFIGURATIONS  R NO TASK SELECTED  46.55.00 ON-BOARD INFORMATION TERMINAL (OIT)  N NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 INFORMATION SYSTEMS SECTION: C-46 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 APU 331-350  49.00.00 AIRBORNE AUXILIARY POWER  49.12.00 APU MOUNTS  VC 01 VISUAL CHECK OF APU SUSPENSION SYSTEM INCLUDING 9 I: C  SHOCKMOUNT STRUCTURE AND BRACKETS  49.13.00 FIRE SEALS  GVI 01 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE 8 I: 20000 FH  WALLS INCLUDING FORWARD, AFT, UPPER, SIDE AND  COMPARTMENT DOORS  49.16.00 AIR INTAKE SYSTEM  GVI 01 GENERAL VISUAL INSPECTION OF DIVERTER AND FLUID 9 I: 2 C ZL-31 GUTTERS ZL-31 49.17.00 POWERPLANT DRAIN SYSTEM  01 TASK DELETED  GVI 02 GENERAL VISUAL INSPECTION OF DRAIN PIPES 9 I: C ZL-31 ZL-31 49.20.00 ENGINE  NO TASK SELECTED  49.23.00 LOAD COMPRESSOR  NO TASK SELECTED  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.26.00 ACCESSORY DRIVE GEARBOX  NO TASK SELECTED  49.30.00 FUEL DISTRIBUTION AND CONTROL  VC 01 VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR 9 I: 1500 AH  BUTTON ON FUEL FILTER  49.34.00 APU FUEL LOW PRESSURE WARNING  NO TASK SELECTED  49.40.00 IGNITION AND STARTING  NO TASK SELECTED  49.51.00 BLEED AND SURGE AIR  NO TASK SELECTED  49.52.00 ACCESSORY COOLING  NO TASK SELECTED  49.60.00 ENGINE CONTROLS  NO TASK SELECTED  49.62.00 EMERGENCY SHUTDOWN  OP 01 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 C  APU STOP SWITCH 1KL  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.62.00 * * * * * C O N T I N U E * * * * *  OP 02 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 C  APU STOP SWITCH 2KL  NOTE: IT IS RECOMMENDED THAT BOTH TASKS 1 AND 2 ARE  PERFORMED ALTERNATELY  OP 03 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT (APU 9 I: 2 C  FIRE STOP RELAY 5WF)  (COVERED BY MSI 26-22-00, TASK NO2)  OP 04 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT. (APU 9 I: 2 C  FIRE P/B SW)  (COVERED BY MSI 26-22-00, TASK NO10)  49.70.00 INDICATING  NO TASK SELECTED  49.80.00 EXHAUST  VC 01 VISUAL CHECK OF V-CLAMP AND EXHAUST DUCT 9 I: C  VC 02 VISUAL CHECK OF EXHAUST DUCT HEAT INSULATION 9 I: 2 C  DI 03 DETAILED INSPECTION OF SEALING RING COUPLING AND 9 I: 2 C  BELLOWS  49.90.00 OIL  VC 01 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON LUBE 9 I: 500 AH  FILTER.  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.90.00 * * * * * C O N T I N U E * * * * *  VC 02 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON 9 I: 500 AH  GENERATOR SCAVENGE FILTER  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-350-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 APU 331-600  49.00.00 AIRBORNE AUXILIARY POWER  49.12.00 APU MOUNTS  VC 01 VISUAL CHECK OF APU SUSPENSION SYSTEM INCLUDING 9 I: 5000 FH  SHOCKMOUNT STRUCTURE, BRACKETS AND VISIBLE PART OF  STRUCTURE ATTACHMENT FITTINGS  49.13.00 FIRE SEALS  GVI 01 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE 8 I: 20000 FH  SEALS, WALLS INCLUDING FORWARD, AFT, UPPER, SIDES AND  COMPARTMENT DOORS  49.16.00 AIR INTAKE SYSTEM  GVI 01 GENERAL VISUAL INSPECTION OF DIVERTER AND FLUID 9 I: 2 C ZL-31 GUTTERS ZL-31 GVI 02 GENERAL VISUAL INSPECTION OF AIR INLET PLENUM AND 9 I: 2 C ZL-31 AIR INTAKE DUCT  49.17.00 POWERPLANT DRAIN SYSTEM  01 TASK DELETED  GVI 02 GENERAL VISUAL INSPECTION OF DRAIN PIPES 9 I: C ZL-31 ZL-31 49.21.00 POWER SECTION  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.21.00 * * * * * C O N T I N U E * * * * *  DS 01 DISCARD TURBINE WHEELS 7 I: NOTE 4  49.23.00 LOAD COMPRESSOR  NO TASK SELECTED  49.26.00 ACCESSORY DRIVE GEARBOX  NO TASK SELECTED  49.30.00 ENGINE FUEL AND CONTROL  GVI 01 GENERAL VISUAL INSPECTION OF THE FUEL SYSTEM 9 I: C ZL-31 COMPONENTS, SEALS,LINES AND INTERFACE CONNECTIONS FOR  EVIDENCE OF LEAKAGE  49.34.00 APU FUEL LOW PRESSURE WARNING  NO TASK SELECTED  49.40.00 IGNITION AND STARTING  NO TASK SELECTED  49.51.00 BLEED AND SURGE AIR  NO TASK SELECTED  49.61.00 CONTROL AND MONITORING  NO TASK SELECTED  49.62.00 EMERGENCY SHUTDOWN  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.62.00 * * * * * C O N T I N U E * * * * *  OP 01 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 C  APU STOP SWITCH (1KL)  OP 02 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 C  APU STOP SWITCH (2KL)  NOTE: IT IS RECOMMENDED THAT BOTH TASKS 1 AND 2 ARE  PERFORMED ALTERNATELY  OP 03 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT (APU 9 I: 2 C  FIRE P/B SWITCH)  (COVERED BY MSI 26.22.00, TASK NO10)  OP 04 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT. (APU 9 I: 2 C  FIRE EMERGENCY STOP RELAY 5WF)  (COVERED BY MSI 26.22.00, TASK NO02)  49.70.00 INDICATING  NO TASK SELECTED  49.80.00 EXHAUST  VC 01 VISUAL CHECK OF V-CLAMP AND EXHAUST MUFFLER IN APU 9 I: C  COMPARTMENT  VC 02 VISUAL CHECK OF EXHAUST MUFFLER INSULATION 9 I: 2 C  DI 03 DETAILED INSPECTION OF SEALING RING GUIDE ASSY AND 9 I: 2 C  BELLOWS  VC 04 VISUAL CHECK OF MUFFLER FROM JET PIPE 9 I: C  49.90.00 OIL  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-H331-600-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 49.90.00 * * * * * 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-
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 52.00.00 DOORS  52.10.00 PASSENGER/CREW DOORS  LU 01 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 6,9 I: C  HANDLE  NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR  INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGER  COMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/02  OP 02 OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN 9 I: C  POSITION  NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR  INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGER  COMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/03  03 TASK DELETED  FC 04 FUNCTIONAL CHECK OF LOCKING MECHANISM 6,9 I: 2 C  NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. ANY DOOR  INFREQUENTLY USED SHALL BE MAINTAINED AS A  PASSENGER COMPARTMENT EMERGENCY EXIT.  REFER TO MSI 52-22-00/05  OP 05 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 C  IS OPENED FROM OUTSIDE  OP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 C  LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS  OPEN  GVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-83 ZL-83 ZL-83 VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 C  FITTINGS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: C-52 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 52.10.00 * * * * * C O N T I N U E * * * * *  FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MO  SLIDER.  52.22.00 PASSENGER COMPARTMENT EMERGENCY EXIT  OP 01 OPERATIONAL CHECK OF DOOR DAMPING, ESCAPE SLIDE 9 I: C  RELEASE MECHANISM DISARMING, AND TO ENSURE THAT DOOR  CANNOT BE LOWERED AND LOCKED WHEN OPEN  LU 02 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 8 I: 18 MO  HANDLE  OP 03 OPERATIONAL CHECK OF DOOR UNLOCKING/LOCKING AND DOOR 8 I: 18 MO  OPENING/CLOSING FROM INSIDE AND OUTSIDE AND DOOR  LATCHING IN FULLY OPEN POSITION  OP 04 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 C  IS OPENED FROM OUTSIDE  FC 05 FUNCTIONAL CHECK OF LOCKING MECHANISM 8 I: 36 MO  OP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 C  LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS  OPEN  GVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-83 VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 C  FITTINGS  FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MO  SLIDER.  NOTE: TASK NOT APPLICABLE FOR A340-600 OVERWING  EMERGENCY EXIT  52.31.00 FWD AND AFT CARGO COMPARTMENT DOOR  LU 01 LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING, 6,9 I: C  LATCHING AND INTERLOCK MECHANISMS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: C-52 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 52.31.00 * * * * * C O N T I N U E * * * * *  FC 02 FUNCTIONAL CHECK OF LATCHING AND LOCKING HANDLE 6,9 I: 4 C  FORCES, AND OF WEAR AND OVERCENTER POSITIONS OF  LATCHING, LOCKING AND INTERLOCK MECHANISMS  GVI 03 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-82 ZL-82 ZL-82 ZL-82 52.33.00 BULK CARGO COMPARTMENT DOOR  OP 01 OPERATIONAL CHECK OF DOOR BALANCE MECHANISM AND OF 9 I: C  DOOR LATCHING IN FULLY OPEN POSITION  GVI 02 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-82 ZL-82 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: C-52 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 52.33.00 * * * * * C O N T I N U E * * * * *  LU 03 LUBRICATION OF BULK CARGO COMPARTMENT DOOR COMPONENTS 6 I: C  52.36.00 CARGO COMPARTMENT DOOR HYDRAULIC SYSTEM  NO TASK SELECTED  52.41.11 AVIONICS COMPARTMENT FWD DOOR  GVI 01 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-81 ZL-81 52.51.11 COCKPIT DOOR  FC 01 FUNCTIONAL CHECK OF SPRING LOADED DOOR STOP MECHANISM 9 I: 2 C  DI 02 DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR 6,9 I: 2 C  LOCKING SYSTEM  OP 03 OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS 9 I: 2 C  FOR RAPID DECOMPRESSION, CHECK OF DOOR OPENING IN  CASE OF POWER OFF AND BY USING THE EMERGENCY CODE  R OP 04 OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE 8 I: 11000 FH  MECHANISM NOTE 24  R DI 05 DETAILED INSPECTION OF FLAP BELLOW 8 I: 36 MO  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: C-52 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 52.51.11 * * * * * C O N T I N U E * * * * *  OP 06 OPERATIONAL CHECK OF MANUAL SWITCH OVER 9 I: 2 C  N OP 07 OPERATIONAL CHECK OF FLAP RELEASE MECHANISM (MANUAL 8 I: 72 MO  OPENING).  N GVI 08 GENERAL VISUAL INSPECTION OF AIR CYLINDER OF 8 I: 72 MO  DECOMPRESSION PANEL.  52.70.00 DOOR WARNING  OP 01 OPERATIONAL CHECK OF DOOR WARNING SYSTEM 9 I: 4 C  FC 02 CHECK BATTERY CAPACITY OF AUTONOMOUS STANDBY POWER 9 I: 8 MO  SUPPLY UNIT (ASPSU)  OP 03 BITE TEST OF AUTONOMOUS STANDBY POWER SUPPLY UNIT 9 I: 4 A  (ASPSU)  OP 04 OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE 9 I: 2 C  WARNING SYSTEM  FC 05 OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING 9 I: 4 C  SYSTEM AND FUNCTIONAL CHECK OF ASSOCIATED PRESSURE  SWITCH  * * * * * E N D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: C-52 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 53.00.00 FUSELAGE  53.19.00 FUSELAGE DRAINS  VC 01 VISUAL CHECK OF DRAIN HOLES IN LOWER PART OF FR1 AND 9 I: C  FR80 (FROM INSIDE)  VC 02 VISUAL CHECK OF PISTON TYPE DRAIN VALVES IN LOWER 9 I: C  FUSELAGE SHELL (FROM OUTSIDE) AND IN FWD AND AFT  CARGO COMPARTMENT DOORS  OP 03 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT UPPER 9 I: C  AFT END OF CENTER WING BOX (FROM MAIN LANDING GEAR  BAY).  OP 04 OPERATIONAL CHECK OF DRAIN MAST/PIPES AFT OF FR80 9 I: 5 MO  OP 05 OPERATIONAL CHECK OF DRAIN HOLES IN UNPRESSURIZED 9 I: C  PART OF FUSELAGE (IN RADOME, FORWARD OF FR1, BEHIND  REAR PRESSURE BULKHEAD, IN BELLY FAIRING, TAIL CONE  AND IN CARGO COMPARTMENT DOORS).  VC 06 VISUAL CHECK OF HOLES OF PISTON TYPE DRAIN OR 9 I: 4 C  PRESSURE DRAIN VALVES AND PRESSURE SEAL DRAINS FROM  INSIDE (IN FUSELAGE BILGE AREA, AT UPPER AFT END OF  CENTER WING BOX, IN CARGO COMPARTMENT DOORS AND AT  RCT)  VC 07 VISUAL CHECK OF PRESSURE SEAL DRAINS AT RCT (FROM 9 I: 4 C  INSIDE)  OP 08 OPERATIONAL CHECK OF DRAIN GAPS BETWEEN "THS-CUTOUT 9 I: 10 MO  FAIRING" PANELS AND AT RUBBER SEAL  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE SECTION: C-53 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 53.19.00 * * * * * C O N T I N U E * * * * *  OP 09 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT BULK 9 I: 1 C  CARGO COMPARTMENT DOOR (FROM OUTSIDE).  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE SECTION: C-53 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 54.00.00 NACELLES/PYLONS  54.59.00 PYLON DRAINS  OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: C  F DRAIN SYSTEM  OP 02 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C, D 9 I: 2 C  AND F DRAIN SYSTEM  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 55.00.00 STABILIZERS  55.16.00 TRIMMABLE HORIZONTAL STABILIZER ATTACH FITTINGS  LU 01 LUBRICATION OF THS HINGE LINE BEARINGS 9 I: 7500 FH  OR  18 MO  LU 02 LUBRICATION OF UPPER AND LOWER FRAME ATTACHMENT 9 I: 7500 FH  BEARINGS OR  18 MO  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STABILIZERS SECTION: C-55 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 56.00.00 WINDOWS  56.12.00 SLIDING WINDOWS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINDOWS SECTION: C-56 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 57.00.00 WINGS  57.29.00 WING DRAINS (OUTER WING)  OP 01 OPERATIONAL CHECK OF DRAIN HOSES AND DESIGNATED 9 I: 4 C  DRAIN HOLES FOR CLOGGING  57.39.00 WING DRAINS (WING TIP)  OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 C  57.59.00 WING DRAINS (LEADING/TRAILING EDGE AND LEADING/TRAILING EDGE  DEVICES)  OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 C  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: C-57 
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  71.00.00 POWERPLANT  71.10.00 COWLING  GVI 01 GENERAL VISUAL INSPECTION OF INLET COWL LIP ASSEMBLY 6 I: 2 A  AND INNER BARREL FAN FLOW AREA  DI 02 DETAILED INSPECTION OF INLET COWL LIP ASSEMBLY AND 6 I: C  INNER BARREL FAN FLOW AREA  GVI 03 GENERAL VISUAL INSPECTION OF FAN COWL HINGES AND 9 I: C  ADJACENT STRUCTURE  GVI 04 GENERAL VISUAL INSPECTION OF FAN COWL LATCHES, 9 I: C  KEEPERS AND ADJACENT STRUCTURE  DI 05 DETAILED INSPECTION OF INLET COWL ATTACHMENT FEATURES 9 I: C  GVI 06 GENERAL VISUAL INSPECTION OF INLET COWL AFT BULKHEAD 9 I: C ZL-41 AND TITANIUM SHIELD  GVI 07 GENERAL VISUAL INSPECTION OF FAN COWL DOORS NEXTEL 9 I: C ZL-41 COVERING  GVI 08 GENERAL VISUAL INSPECTION OF FAN COWL DOOR FIRE SEALS 8 I: 18 MO  FC 09 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 9 I: C  71.70.00 POWERPLANT DRAINS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 71.70.00 * * * * * C O N T I N U E * * * * *  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  72.00.00 ENGINE  72.20.00 FAN SECTION  01 TASK DELETED  DI 02 DETAILED INSPECTION OF FAN BLADES AND SPINNER 6 I: 2 A  DI 03 DETAILED INSPECTION OF VISIBLE AREA OF ENGINE INLET 6 I: 2 A  AND FAN OUTLET FOR DAMAGE AND/OR MISSING ABRADABLE  MATERIAL  DI 04 DETAILED INSPECTION OF ATTACHMENT POINTS FOR AIR 9 I: 8 C  INTAKE COWL AND THRUST REVERSER "V" GROOVE  DI 05 DETAILED INSPECTION OF FORWARD ENGINE MOUNT FAN FRAME 9 I: 8 C  ATTACHMENT POINTS  DS 06 DISCARD LIFE LIMITED PARTS OF FAN SECTION 5 I: NOTE 4  DS 07 DISCARD FAN SHAFT 5 I: NOTE 4  RS 08 DETAILED INSPECTION AND RELUBRICATION OF FAN BLADE 6 I: 1000 FC  DOVETAILS, MIDSPAN SHROUDS, RETAINERS, SPACERS AND  FAN DISK DOVETAIL SLOTS  72.30.00 HP COMPRESSOR SECTION  DS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4  ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 72.40.00 COMBUSTION SECTION  SDI 01 BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINERS AND 9 I: 6000 FH  DOME AREA  72.50.00 TURBINE SECTION  01 TASK DELETED  SDI 02 BORESCOPE INSPECTION OF HPT NOZZLE FROM TWO PORTS ON 6 I: 6000 FH  FORWARD SIDE  SDI 03 BORESCOPE INSPECTION OF HPT BLADES 6 I: 500 FC  DI 04 DETAILED INSPECTION OF AFT MOUNT LUGS FOR STRUCTURAL 9 I: 8 C  INTEGRITY AND DEFORMATION  DS 05 DISCARD LIFE LIMITED PARTS OF HP AND LP TURBINE 5 I: NOTE 4  SDI 06 BORESCOPE INSPECTION OF LEADING EDGES OF LPT STAGE 1 - I: 1500 FC  BLADES.  72.60.00 ACCESSORY DRIVE SECTION  01 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 72.60.00 * * * * * C O N T I N U E * * * * *  DI 02 CHECK TRANSFER GEARBOX AND ACCESSORY GEARBOX SCAVENGE 6 I: C  SCREENS FOR DEBRIS  (COVERED BY MSI 79-20-00, TASK NO3).  GVI 03 GENERAL VISUAL INSPECTION OF TRANSFER GEARBOX AND 6 I: C ZL-41 ACCESSORY GEARBOX HOUSINGS FOR LEAKS  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  73.00.00 ENGINE FUEL AND CONTROL  73.00.00 ENGINE FUEL AND CONTROL GENERAL  DS 01 DISCARD FUEL FILTER ELEMENT 9 I: 4000 FH  OP 02 OPERATIONAL CHECK OF THRUST REVERSER DEPLOY SWITCHES 9 I: 5000 FC  OP 03 OPERATIONAL CHECK OF THRUST REVERSER SYSTEM VIA MCDU 9 I: 5000 FC  04 TASK DELETED  05 TASK DELETED  73.25.00 FUNCTIONAL INTERFACE  01 TASK DELETED  OP 02 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 C  (COVERED BY MSI 21-26-00, TASK NO2).  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  74.00.00 IGNITION  74.00.00 IGNITION  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 IGNITION SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  75.00.00 AIR  75.20.00 COOLING  NO TASK SELECTED  75.30.00 COMPRESSOR CONTROL  NO TASK SELECTED  75.40.00 NACELLE TEMPERATURE INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  76.00.00 ENGINE CONTROLS  76.00.00 ENGINE CONTROLS GENERAL  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  77.00.00 ENGINE INDICATING  77.00.00 ENGINE INDICATING GENERAL  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  78.00.00 EXHAUST  78.10.00 TURBINE EXHAUST SYSTEM  DI 01 DETAILED INSPECTION OF NOZZLE, MIXER AND CENTERBODY 9 I: C  FOR STRUCTURAL DAMAGE AND SECURITY OF ATTACHMENT  DI 02 DETAILED INSPECTION OF MIXER AND CENTERBODY 9 I: C  ATTACHMENT FEATURES  DI 03 DETAILED INSPECTION OF FIRE SEALS FOR DAMAGE AND 8 I: 18 MO  SECURITY OF ATTACHMENT  78.31.00 THRUST REVERSER CONTROL AND INDICATING  01 TASK DELETED  GVI 02 GENERAL VISUAL INSPECTION OF HYDRAULIC FLEXIBLE HOSES 6 I: C  OP 03 OPERATIONAL CHECK OF ACTUATOR SECONDARY LOCKS 8 I: 8000 FH  NOTE 24A  DS 04 REMOVE RESTRICTOR/CHECK VALVE IN ADDITIONAL RETURN 8 I: 34000 FH  LINE FOR WORKSHOP CHECK NOTE 24A  78.32.00 THRUST REVERSER STRUCTURE  GVI 01 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, 9 I: C  LATCHES AND STRUCTURE ADJACENT TO HINGES AND LATCHES  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 78.32.00 * * * * * C O N T I N U E * * * * *  GVI 02 GENERAL VISUAL INSPECTION OF "V" GROOVES ON FWD AND 9 I: C  ON AFT FACE OF THRUST REVERSER AND ADAPTER RING OF  ENGINE, FAN FRAME  GVI 03 GENERAL VISUAL INSPECTION OF MOVEABLE KICKER PLATE, 9 I: C  ADJACENT PIVOTING DOOR AND ACTUATOR AREA. (BLOCKER  DOORS DEPLOYED)  GVI 04 GENERAL VISUAL INSPECTION OF THRUST REVERSER 9 I: C ZL-41 STRUCTURE IN BLEED AND FLOW AIR PASSAGES  GVI 05 GENERAL VISUAL INSPECTION OF INNER BARREL FIRE 8 I: 18 MO  THERMAL BLANKETS  GVI 06 GENERAL VISUAL INSPECTION OF PIVOTING DOOR SEALS 9 I: C  78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  79.00.00 OIL  79.10.00 STORAGE  NO TASK SELECTED  79.20.00 DISTRIBUTION  01 TASK DELETED  DS 02 DISCARD PRIMARY FILTER 9 I: 4000 FH  DI 03 CHECK OF FWD SUMP, AFT SUMP ACCESSORY GEARBOX AND 6 I: C  TRANSFER GEARBOX SCAVENGE SCREENS  (THIS TASK COVERS TASK 72.60.00/02-C5)  OP 04 OPERATIONAL CHECK OF ELECTRICAL MAGNETIC CHIP 9 I: C  DETECTOR  79.31.00 OIL QUANTITY TRANSMITTER SYSTEM  NO TASK SELECTED  79.32.00 OIL TEMPERATURE INDICATING SYSTEM  NO TASK SELECTED  79.33.00 OIL PRESSURE INDICATING SYSTEM  NO TASK SELECTED  79.34.00 LOW OIL PRESSURE WARNING SYSTEM  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 79.34.00 * * * * * C O N T I N U E * * * * *  NO TASK SELECTED  79.35.00 OIL FILTER CLOGGING WARNING SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-CFM56-5-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 CFM56-5  80.00.00 STARTING  80.10.00 STARTING  DI 01 STARTER OIL LEVEL CHECK/REPLENISH AND CHECK OF 6 I: A  MAGNETIC CHIP DETECTOR FOR PARTICLES  SV 02 DRAIN AND REPLENISH STARTER OIL 6 I: 2400 FH  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STARTING SECTION: C-CFM56-5-8
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  71.00.00 POWERPLANT  71.13.00 FAN COWL  GVI 01 GENERAL VISUAL INSPECTION OF THE FAN COWL DOORS 9 I: C  /STRAKES FOR CONDITION  GVI 02 GENERAL VISUAL INSPECTION OF THE NEXTEL INNER SKIN 9 I: C  FOR DAMAGE  FC 03 FUNCTIONAL CHECK OF LATCHES TENSION 9 I: C  71.61.00 AIR INTAKE COWL  GVI 01 GENERAL VISUAL INSPECTION OF INNER AND OUTER SURFACES 9 I: C  OF AIR INTAKE COWL FOR DAMAGE AND DEFORMATION  GVI 02 GENERAL VISUAL INSPECTION OF AIR INTAKE COWL SEALS 9 I: C  FOR DAMAGE OR MISSING PARTS  71.71.00 POWERPLANT DRAINS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  72.00.00 ENGINE  72.22.00 GAS GENERATOR FAIRINGS  GVI 01 GENERAL VISUAL INSPECTION OF THE GAS GENERATOR 9 I: C ZL-41 FAIRINGS AND UPPER AND LOWER SPLITTER FAIRINGS FOR  SIGNIFICANT DAMAGE  72.31.00 LP COMPRESSOR MODULE  DI 01 DETAILED INSPECTION OF LP COMPRESSOR BLADES 6,9 I: 2 A  DS 02 DISCARD THE LP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4  RS 03 RE-APPLICATION OF ROOT COATINGS TO LP COMPRESSOR 6 I: 4000 FC  BLADES  LU 04 RE-LUBRICATION OF LP COMPRESSOR BLADE ROOT COATINGS 6 I: 1200 FC  72.32.00 IP COMPRESSOR MODULE  DS 01 DISCARD THE IP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4  (THIS TASK COVERS TASK 72.33.00/02-R5)  72.33.00 COMPRESSOR INTERMEDIATE MODULE  01 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 72.33.00 * * * * * C O N T I N U E * * * * *  DS 02 DISCARD THE IP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4  (COVERED BY MSI 72.32.00 TASK NO 01)  DI 03 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FH  BY MSI 79.30.00, TASK 2)  72.33.40 EXTERNAL GEARBOX DRIVE  DI 01 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FH  BY MSI 79.30.00, TASK 2)  72.34.00 LP COMPRESSOR CASING  GVI 01 GENERAL VISUAL INSPECTION OF THE FAN TRACK AND COLD 9 I: C  STREAM DUCT FOR SIGNIFICANT DAMAGE  GVI 02 GENERAL VISUAL INSPECTION OF THE SPLITTER FAIRING FOR 9 I: C  SIGNIFICANT DAMAGE  72.40.00 COMBUSTION SECTION  SDI 01 SPECIAL DETAILED BORESCOPE INSPECTION OF COMBUSTOR 9 T: 1000 FC  OR  9000 FH  I: 550 FC  OR  5000 FH  72.41.20 HP COMPRESSOR ASSEMBLY  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 72.41.20 * * * * * C O N T I N U E * * * * *  DS 01 DISCARD THE HP COMPRESSOR LIFE LIMITED PARTS 5 I: NOTE 4  72.41.50 HP TURBINE SECTION  SDI 01 SPECIAL DETAILED BORESCOPE INSPECTION OF THE HPT 6,9 T: 1000 FC  NOZZLE GUIDE VANES OR  9000 FH  I: 500 FC  OR  4500 FH  DS 02 DISCARD THE HP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4  SDI 03 SPECIAL DETAILED BORESCOPE INSPECTION OF THE HPT 6,9 T: 1000 FC  BLADES OR  9000 FH  I: 550 FC  OR  5000 FH  72.51.00 IP/LP TURBINE MODULE  DS 01 DISCARD THE IP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4  72.52.00 LP TURBINE MODULE  DS 01 DISCARD THE LP TURBINE LIFE LIMITED PARTS 5 I: NOTE 4  VC 02 VISUAL CHECK OF THE TAIL BEARING HOUSING SUPPORT 8 I: 4000 FC  STRUCTURE ATTACHMENT LUGS  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 72.61.00 EXTERNAL GEARBOX MODULE  DI 01 DETAILED INSPECTION OF THE MASTER EMCD (TASK COVERED 6 I: 130 FH  BY MSI 79.30.00, TASK 2)  72.62.00 EXTERNAL GEARBOX DRIVESHAFT AND SHROUD  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  73.00.00 ENGINE FUEL AND CONTROL  73.10.00 FUEL DISTRIBUTION  DS 01 DISCARD LP FUEL FILTER ELEMENT 6,9 I: 1600 FC  OR  10000 FH  73.20.00 ENGINE FUEL AND CONTROL  NO TASK SELECTED  73.25.00 FUNCTIONAL INTERFACE  OP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 C  (COVERED BY MSI 21-26-00, TASK NO2)  73.30.00 ENGINE FUEL INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  74.00.00 IGNITION  74.00.00 IGNITION  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 IGNITION SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  75.00.00 AIR  75.21.00 ACCESSORY/ZONE COOLING  GVI 01 GENERAL VISUAL INSPECTION OF COOLING AIR INLET, AIR 9 I: C ZL-40 OUTLET FOR DAMAGE AND BLOCKAGE ZL-41 75.22.00 ENGINE COOLING AND SEALING  NO TASK SELECTED  75.24.00 TURBINE CASE COOLING SYSTEM  NO TASK SELECTED  75.33.00 IP/HP COMPRESSOR AIRFLOW CONTROL  NO TASK SELECTED  75.41.00 NACELLE TEMPERATURE INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  76.00.00 ENGINE CONTROLS  76.00.00 ENGINE CONTROLS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  77.00.00 ENGINE INDICATING  77.00.00 ENGINE INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  78.00.00 EXHAUST  78.11.00 TURBINE EXHAUST  GVI 01 GENERAL VISUAL INSPECTION OF THE AIR WASHED SURFACE 9 I: C ZL-41 OF THE NOZZLE  GVI 02 GENERAL VISUAL INSPECTION OF THE AIR WASHED SURFACE 9 I: C  OF THE PLUGS  GVI 03 GENERAL VISUAL INSPECTION OF THE EXHAUST FIRE SEAL 8 I: 18 MO  FOR DAMAGE  78.31.00 THRUST REVERSER CONTROL AND INDICATING  GVI 01 GENERAL VISUAL INSPECTION OF HYDRAULIC TUBES AND 6 I: C ZL-41 ACTUATOR FOR DAMAGE  FC 02 FUNCTIONAL CHECK OF THE THRUST REVERSER PRIMARY 6 I: 2700 FC  LOCKS, TERTIARY LOCKS AND SYNCHRO SHAFTS NOTE 24B  78.32.00 THRUST REVERSER STRUCTURE  GVI 01 GENERAL VISUAL INSPECTION OF THE THRUST REVERSER 9 I: C ZL-41 INTERNAL AND EXTERNAL AERODYNAMIC SURFACES  GVI 02 GENERAL VISUAL INSPECTION OF THE FORWARD PRESSURE 9 I: C ZL-41 SEAL FOR DAMAGE OR MISSING SEGMENT  GVI 03 GENERAL VISUAL INSPECTION OF THE FIRE SEALS AND FIRE 8 I: 18 MO  SHIELDS, INCLUDING THE BLEED VALVE DUCT SEALS  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 78.32.00 * * * * * C O N T I N U E * * * * *  GVI 04 GENERAL VISUAL INSPECTION OF THRUST REVERSER 9 I: C  CASCADES, BLOCKER DOORS, LINKS AND HINGES FOR DAMAGE  GVI 05 GENERAL VISUAL INSPECTION OF THE THERMAL BLANKETS FOR 9 I: C  DAMAGE  FC 06 FUNCTIONAL CHECK OF THE BLOW OUT DOOR FOR CORRECT 9 I: 8000 FH  TENSION  78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  79.00.00 OIL  79.10.00 OIL STORAGE  NO TASK SELECTED  79.20.00 OIL DISTRIBUTION  RS 01 REMOVE, INSPECT, CLEAN AND MARK PRESSURE OIL FILTER 6 I: 3000 FH  NOTE: PRESSURE OIL FILTER LIFE SHALL NOT EXCEED 2  CLEANINGS  DS 02 DISCARD SCAVENGE OIL FILTER 6 I: 1600 FH  79.30.00 OIL INDICATING  RS 01 CLEANING AND FUNCTIONAL CHECK OF THE MASTER EMCD 6 I: 2500 FH  DI 02 DETAILED INSPECTION OF THE MASTER EMCD 6 I: 130 FH  (THIS TASK COVERS TASKS 72.33.00/03-R5,  72.33.40/01-R5, 72.61.00/01-R5)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-RR T500-7
MSI 

REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

REFE

A340 MRB REPORT – Systems and Powerplant Section

 RR T500  80.00.00 STARTING  80.11.00 PNEUMATIC STARTER AND VALVE SYSTEM  DI 01 DETAILED INSPECTION OF STARTER MCD 6,9 I: 800 FH  OR  300 FC  SV 02 STARTER OIL CHANGE 6,9 I: 800 FH  OR  300 FC  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STARTING SECTION: C-RR T500-8
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 per 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 REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

S.T = 60000 FH

= Aircraft Inspection

I= 17700 FH

10Yrs 15Yrs 20Yrs 2

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICA

572011-01-1 DI 13000 FC

OR

60000 FH

4700 FC

OR

17700 FH

GRP 

O

GRP 

572011-01-2 DI 13000 FC

OR

60000 FH

3700 FC

OR

13900 FH

GRP 

O

GRP 

572011-01-3 DI 13000 FC

OR

26000 FH

4100 FC

OR

8200 FH

GRP 

Example 1 : SSI 572011 

12 43A 11 43A 10 43A 9 43A 8 43A 7 43A 6 43A 5 43A 4 43A 3 43A 

2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

S.T = 60000 FH

= Aircraft Inspection

I= 13900 FH

I= 17700 FH

10Yrs 15Yrs 20Yrs 2

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICA

572011-01-1 DI 13000 FC

OR

60000 FH

4700 FC

OR

17700 FH

GRP 

O

GRP 

572011-01-2 DI 13000 FC

OR

60000 FH

3700 FC

OR

13900 FH

GRP 

O

GRP 

572011-01-3 DI 13000 FC

OR

26000 FH

4100 FC

OR

8200 FH

GRP 

Example 2 : SSI 572011 

12 43B 11 43B 10 43B 9 43B 8 43B 7 43B 

6 43B 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

S.T = 13000 FC

= Aircraft Inspection

100% T= 16600 FC

I= 7100 FC 

10Yrs 15Yrs 20Yrs 25Y

Example 3 : SSI 531144 

TASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL APPLIC

531144-01-1 SDI 13000 FC 16600 FC 7100 FC A34

A34

12 43B 11 43B 10 43B 9 43B 8 43B 7 43B 6 43B 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

I= 5000 FC 

= Aircraft Inspection

I= 5000 FC 

10Yrs 15Yrs 20Yrs 25Y

Example 4 : SSI 533135 

TASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL APPLICA

533135-01-1 DI 10 YE

OR

13000 FC

10 YE 10 YE

OR

5000 FC

A340

OR

A340

12 43B 11 43B 10 43B 9 43B 8 43B 7 43B 6 43B 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

T= 13000 FC

= Aircraft Inspection

Example 5 : SSI 533154 

NOTE: A/C 1 to 4 are Pre mod 41652

I= 8100 F

10Yrs 15Yrs 20Yrs 

TASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL 

533154-01-1 DI 13000 FC 8100 FC GRP 

PRE ORGRP PRE 

533154-01-2 DI 13000 FC 13000 FC GRP 

POSORGRP POSORGRP ORGRP 

12 43A 11 43A 10 43A 9 43A 8 43A 7 43A 6 43A 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

TASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL APPLICABIL

533154-01-1 DI 13000 FC 8100 FC GRP 42A

PRE 41652ORGRP 43APRE 41652

533154-01-2 DI 13000 FC 13000 FC GRP 42A

POST 41652ORGRP 43APOST 41652ORGRP 42BORGRP 43B

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 900 FC/Yr 5000 FH/Yr 

T= 13000 FC

= Aircraft Inspection

Example 6 : SSI 533154 

I= 8100 FC

10Yrs 15Yrs 20Yrs 25Yrs

NOTE: A/C 1 to 4 are Pre mod 41652

12 43B 11 43B 10 43B 9 43B 8 43B 

7 43B 6 43A 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 
A340 MRB REPORT 

 Issue : July 2010 

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 700 FC/Yr 5200 FH/Yr 

T= 41500 FH

= Aircraft Inspection

I= 18700 FH

Example 7: SSI 574109 

I= 20100 FH I= 20100 FH 

I= 18700 FH

T= 40600 FH

I= 20100 FH I= 201

10Yrs 15Yrs 20Yrs 

TASK REF Level SAMPLE THRESHOLD 100% THRESHOLD INTERVAL E

574109-01-1 DI 10 YE 20 YE

OR9500 FCOR41500 FH

10 YEOR4600 FCOR20100 FH

GOG

574109-01-2 DI 10 YE 20 YE

OR9300 FCOR40600 FH

10 YEOR4300 FCOR18700 FH

GOG

574109-01-3 DI 10 YE 20 YE

OR11900 FCOR23800 FH

10 YEOR4700 FCOR9400 FH

G

12 43B 11 43B 10 43B 9 43B 8 43B 7 43B 6 43B 5 43A 4 43A 3 43A 2 43A 1 43A A/C Grp 

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 AMM 53-00-00

CML 08-109 

4 Cosmoline on seat track crown AMM 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 AMM 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 A340 

Y : Model (2 for –200 / 3 for –300) 

Z : Various Weight Variants corresponding to a specific certified Type/Model 

EXAMPLES

GROUP 42A : A340-200 WV 000, 001, 002 

(1st WV Group of A340-200 Series) 

GROUP 43B : A340-300 WV 020, 021, 023, 024, 025, 026, 028, 029, 030 

(2nd WV group of A340-300 Series)
 A340 MRB REPORT - Structures 

Issue : July 2010 

10. EXPLANATION OF STRUCTURES SECTION FORMAT

 Detailed information is given below concerning the format of the inspection requirements provided on subsequent pages. 

TASK 

REFERENCE 

ACCESS ZONE TASK 

DESCRIPTION 

SAMPLE 

 THRESHOLD

INTERVAL 

100% 

THRESHOLD

INTERVAL 

TPS CPCP ZIP 

REFERENC

1 2 3 4 5 6 7 8 9 

1. This column indicates the SSI task number, e.g. 531109-01-01. It is composed of 10 digits as follows: 

XXXXXX – XX – XX 

The SSI number is represented by the six first digits, 531109.The first set of two digits are in accordance with the A340 ATA 100 breakdown, showing the major section where the SSI is located e.g 53 Fuselage. The second set of two digitsare also in accordance breakdown, showing the sub section where the SSI is located e.g 53-11 Fwd fuselage. The third set of two digitsare sequential num02, 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 

e.g.Detailed or Special Detailed. These two digits are also changed when the inspection areas are physically different (e.g. rib 8 or have 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 ide

e.g aircraft series, mod status, WV group etc ...The digits are also used to differentiate between minor access differences e.g. differ

2. This column indicates the access requirement to adequately perform the required maintenance task, i.e. all items listed must be re

Applicability index Sequence number 

SSI number 
 A340 MRB REPORT - Structures 

Issue : July 2010 

panels 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. Details of 

provided, where applicable. The SSI description states the boundaries of the inspection area. All items within this boundary are tcutouts, 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 Sam

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 

 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 Ty

The technical specification for corrosion preventive temporary protective compounds can be found in the Process and Material SpecVolume 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 given belo
 A340 MRB REPORT - Structures 

Issue : July 2010 

Applicability Task applicable to

ALL All A340 aircraft. A340-xxx -xxx series aircraft. PRE nnnnn All A340 PRE MOD nnnnn. 

i.e. A340 that do not have MOD nnnnn embodied. 

POST nnnnn All A340 POST MOD nnnnn.

i.e. A340 that do have MOD nnnnn embodied. 

POST nnnnn Sxxxxx All A340 POST MOD nnnnn (at least with mod proposal no. Sxxxxx embodied). POST nnnnn POST mmmmm 

All A340 POST MOD nnnnn and POST MOD mmmmm. i.e. A340 that do have MOD nnnnn and MOD mmmmm embodied. 

A340-200 

OR A340-300 PRE nnnnn 

All A340-200, 

Or, All A340-300 that do not have MOD nnnnn embodied. 

A340-200 

POST nnnnn OR POST mmmm 

All A340-200 that do have MOD nnnnn embodied,

Or, All A340-200 that do have MOD mmmm embodied. 

A340-200 

POST nnnnn OR A340-300 POST nnnnn PRE mmmmm 

All A340-200 that do have MOD nnnnn embodied,

Or, All A340-300 that do have MOD nnnnn embodied and do not have MOD mmmmm embodied. 

POST nnnnn (xx-yyyy) 

All A340 that do have 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.
 A340 MRB REPORT - Structures 

Issue : July 2010 

Applicability Task applicable to

GROUP XYZ All aircraft with weight variant group XYZ GROUP XYZ PRE nnnn 

All aircraft with weight variant group XYZ that do not have MOD nnnn embodied 

GROUP XYZ POST nnnn 

All aircraft with weight variant group XYZ that do have MOD nnnn embodied 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 282801-01-1 821 822 131 DETAILED INSPECTION OF ADDITIONAL CENTER T: 6 YE  ACT 132 TANK EXTERNAL STRUCTURE I: 6 YE  151 NOTE: INTERVAL AND THRESHOLD CORRESPOND TO THE ACT  152 (T: 6 ACT YE AND I:6 ACT YE)  282803-01-1 821 822 131 DETAILED INSPECTION OF ADDITIONAL CENTER TANK T: 12 YE  ACT 132 INTERNAL STRUCTURE. I: 12 YE  BLADDER TANK 151 NOTE: THRESHOLD AND INTERVAL CORRESPOND TO THE ACT  152 (T:12 ACT YE AND I:12 ACT YE)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: D-28 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321101-01-1 N/A 731 DETAILED INSPECTION OF MLG MAIN FITTING. T: 6 YE  741 I: 6 YE  321102-01-1 MLG FULLY EXTENDED 731 DETAILED INSPECTION OF MLG SLIDING PISTON. T: 6 YE  741 I: 6 YE  321103-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG UPPER PISTON. T: 10 YE  741 I: 10 YE  321104-01-1 N/A 731 DETAILED INSPECTION OF MLG BOGIE BEAM. T: 6 YE  741 I: 6 YE  321105-01-1 MLG PITCH TRIMMER 731 DETAILED INSPECTION OF MLG PITCH TRIMMER T: 6 YE  EXTENDED 741 I: 6 YE  321106-01-1 N/A 731 DETAILED INSPECTION OF MLG SIDESTAY ASSEMBLY. T: 6 YE  741 I: 6 YE  321107-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCK STAY ASSEMBLY. T: 6 YE  741 I: 6 YE  321108-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG AXLES. T: 10 YE  741 I: 10 YE  321109-01-1 N/A 731 DETAILED INSPECTION OF MLG TORQUE LINK, LOWER AND T: 6 YE  741 UPPER. I: 6 YE  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321110-01-1 N/A 731 DETAILED INSPECTION OF MLG ARTICULATING LINK, LOWER T: 6 YE  741 AND UPPER. I: 6 YE  321114-01-1 PINS 731 DETAILED INSPECTION OF BOGIE PIVOT PIN, SIDESTAY T: 10 YE  741 ASSY PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY I: 10 YE  ATTACH PINS, ARTICULATING LINKAGE PINS, PITCH  TRIMMER ATTACH PINS, FORWARD PINTLE PINS AND  SHORTENING LINKAGE PINS.  321124-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCKSTAY ACTUATOR. T: 6 YE  741 I: 6 YE  321125-01-1 MLG FULLY LOWERED 570 DETAILED INSPECTION OF MLG PINTLE PINS AT OUTER T: 10 YE  670 WING TRAILING EDGE I: 10 YE  321126-01-1 PIN 570 DETAILED INSPECTION OF MLG SHORTENING T: 10 YE  670 MECHANISM AT OUTER WING TRAILING I: 10 YE  EDGE EARTHING PIN  321127-01-1 PIN 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE  670 OUTER WING TRAILING EDGE I: 10 YE  321151-01-1 N/A 731 DETAILED INSPECTION OF MLG MAIN FITTING. T: 6 YE  741 I: 6 YE  321152-01-1 MLG FULLY EXTENDED 731 DETAILED INSPECTION OF MLG SLIDING PISTON. T: 6 YE  741 I: 6 YE  321153-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG UPPER PISTON. T: 10 YE  741 I: 10 YE  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321154-01-1 N/A 731 DETAILED INSPECTION OF MLG BOGIE BEAM. T: 6 YE  741 I: 6 YE  321155-01-1 MLG PISTON ROD 731 DETAILED INSPECTION OF MLG PITCH TRIMMER. T: 6 YE  EXTENDED 741 I: 6 YE  321156-01-1 N/A 731 DETAILED INSPECTION OF MLG SIDESTAY ASSEMBLY. T: 6 YE  741 I: 6 YE  321157-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCK PINS ASSEMBLY. T: 6 YE  741 I: 6 YE  321158-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG AXLES. T: 10 YE  741 I: 10 YE  321159-01-1 N/A 731 DETAILED INSPECTION OF MLG TORQUE LINK, LOWER AND T: 6 YE  741 UPPER. I: 6 YE  321160-01-1 N/A 731 DETAILED INSPECTION OF MLG ARTICULATING LINK, LOWER T: 6 YE  741 AND UPPER. I: 6 YE  321161-01-1 SHOCK ABSORBER 731 DETAILED INSPECTION OF MLG SHORTENING LINK ASSEMBLY, T: 10 YE  741 UPPER AND LOWER LINK I: 10 YE  321164-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF BOGIE PIVOT PIN, SIDESTAY T: 10 YE  741 ASSY PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY I: 10 YE  ATTACH PINS, ARTICULATING LINKAGE PINS, PITCH  TRIMMER ATTACH PINS, FORWARD PINTLE PINS AND  SHORTENING LINKAGE PINS.  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321174-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCKSTAY ACTUATOR T: 6 YE  741 I: 6 YE  321175-01-1 MLG 570 DETAILED INSPECTION OF MLG PINTLE PINS AT OUTER T: 10 YE  670 WING TRAILING EDGE. I: 10 YE  321176-01-1 PIN 570 DETAILED INSPECTION OF MLG SHORTENING T: 10 YE  670 MECHANISM AT OUTER WING TRAILING I: 10 YE  EDGE EARTHING PIN  321177-01-1 PIN 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE  670 OUTER WING TRAILING EDGE. I: 10 YE  321505-01-1 N/A 751 DETAILED INSPECTION OF CLG MAIN FITTING (CYLINDER). T: 6 YE  I: 6 YE  321506-01-1 AXLE SLEEVES 751 DETAILED INSPECTION OF CLG SLIDING MEMBER (PISTON). T: 6 YE  PISTON EXTENDED I: 6 YE  WHEELS  321507-01-1 753 754 755 751 DETAILED INSPECTION OF CLG DRAG STAY ASSEMBLY. T: 6 YE  756 I: 6 YE  321508-01-1 753 754 755 751 DETAILED INSPECTION OF CLG LOWER STABILIZER LINK. T: 6 YE  756 I: 6 YE  321509-01-1 753 754 755 751 DETAILED INSPECTION OF CLG UPPER STABILIZER LINK. T: 6 YE  756 I: 6 YE  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321510-01-1 753 754 755 751 DETAILED INSPECTION OF CLG FORWARD AND AFT LOCK T: 6 YE  756 LINKS. I: 6 YE  321511-01-1 PINS 751 DETAILED INSPECTION OF CLG ATTACHMENT PINS. T: 10 YE  I: 10 YE  321512-01-1 AXLE SLEEVES 751 DETAILED INSPECTION OF TORQUE LINKS. T: 6 YE  PISTON EXTENDED I: 6 YE  WHEELS  321551-01-1 CLG DOORS OPEN 751 DETAILED INSPECTION OF CLG MAIN FITTING. T: 6 YE  I: 6 YE  321552-01-1 CLG DOORS OPEN 751 DETAILED INSPECTION OF CLG SLIDING MEMBER. T: 6 YE  SLIDING MEMBER FULLY I: 6 YE  EXTENDED  321553-01-1 N/A 751 DETAILED INSPECTION OF CLG TORQUE LINKS T: 6 YE  I: 6 YE  321554-01-1 WHEEL WELL DOORS 751 DETAILED INSPECTION OF CLG DRAG STAY ASSEMBLY T: 6 YE  (UPPER AND LOWER) INCLUDING LOCKLINK. I: 6 YE  321557-01-1 PINS 751 DETAILED INSPECTION OF CLG PINS T: 10 YE  - MAIN FITTING PINTLE PINS (LH & RH) I: 10 YE  - TORQUE LINK PINS (UPPER & LOWER)  - 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-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 321558-01-1 N/A 751 DETAILED INSPECTION OF CLG BOGIE BEAM, T: 6 YE  BRAKE RODS AND AXLES I: 6 YE  321559-01-1 WHEEL WELL DOORS 751 DETAILED INSPECTION OF CLG TRIANGULATION ARMS. T: 6 YE  I: 6 YE  322101-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING (BARREL). T: 6 YE  I: 6 YE  322102-01-1 SLEEVES 711 DETAILED INSPECTION OF NLG SLIDING MEMBER. T: 6 YE  SLIDING MEMBER FULLY I: 6 YE  EXTENDED  WHEELS  322103-01-1 N/A 711 DETAILED INSPECTION OF NLG TORQUE LINKS. T: 6 YE  I: 6 YE  322104-01-1 713 714 715 711 DETAILED INSPECTION OF NLG DRAGSTAY UPPER ARM. T: 6 YE  716 I: 6 YE  322105-01-1 N/A 711 DETAILED INSPECTION OF NLG DRAGSTAY LOWER ARM. T: 6 YE  I: 6 YE  322106-01-1 N/A 711 DETAILED INSPECTION OF NLG DOWNLOCK LINK. T: 6 YE  I: 6 YE  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 322107-01-1 PIN 711 DETAILED INSPECTION OF NLG PINS: T: 10 YE  - MAIN FITTING (BARREL) HINGE PINS (LH AND RH). I: 10 YE  - TORQUE LINKS HINGE PINS (UPPER, MIDDLE AND LOWER)  - 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  716 I: 5 YE  DRAG STRUT  DISCONNECTED  PINTLE PIN  322151-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING. T: 6 YE  I: 6 YE  322152-01-1 SLEEVES 711 DETAILED INSPECTION OF NLG SLIDING MEMBER, T: 6 YE  SLIDING MEMBER FULLY INCLUDING INTEGRAL AXLE. I: 6 YE  EXTENDED  WHEELS  322153-01-1 N/A 711 DETAILED INSPECTION OF NLG TORQUE LINKS. T: 6 YE  I: 6 YE  322154-01-1 WHEEL WELL DOORS 711 DETAILED INSPECTION OF NLG DRAG STAY T: 6 YE  ASSEMBLY (UPPER AND LOWER) INCLUDING I: 6 YE  LOCKLINK.  322157-01-1 PINS 711 DETAILED INSPECTION OF NLG PINS T: 10 YE  - MAIN FITTING PINTLE PINS (LH & RH) I: 10 YE  - TORQUE LINK PINS (UPPER, APEX & LOWER)  - DRAG STAY PINS (UPPER PINTLE & APEX)  - DOWNLOCK HINGE PINS (UPPER MIDDLE LOWER)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 521101-01-1 N/A TASK DELETED  521103-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 T: 6 YE  (FWD PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE. I: 6 YE  521103-01-2 N/A TASK DELETED  521104-01-1 ESCAPE SLIDE 831 DETAILED INSPECTION OF DOOR 1 (FORWARD T: 6 YE 1  INSULATION 841 PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YE  LINING  521123-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 T: 6 YE  (FORWARD PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE  521123-01-2 N/A TASK DELETED  521124-01-1 ESCAPE SLIDE 831 DETAILED INSPECTION OF DOOR 1 (FORWARD T: 6 YE 1  INSULATION 841 PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YE  LINING  521201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 T: 6 YE  (MID PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE.  521201-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 521202-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 T: 6 YE 1  ESCAPE SLIDE 842 (MID PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  521203-01-1 N/A TASK DELETED  521203-01-2 N/A TASK DELETED  521221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 T: 6 YE  (MID PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE  521221-01-2 N/A TASK DELETED  521222-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 T: 6 YE 1  ESCAPE SLIDE 842 (MID PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  521301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 T: 6 YE  (AFT PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE  521301-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 521302-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 T: 6 YE 1  ESCAPE SLIDE 843 (AFT PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  521303-01-1 N/A TASK DELETED  521303-01-2 N/A TASK DELETED  521321-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 T: 6 YE  (AFT PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE  521321-01-2 N/A TASK DELETED  521322-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 T: 6 YE 1  ESCAPE SLIDE 843 (AFT PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  522121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF OVERWING EMERGENCY EXIT T: 12 YE  DOOR SKIN, EXTERNAL SURFACE I: 12 YE  522122-01-1 836 846 836 DETAILED INSPECTION OF OVERWING EMERGENCY EXIT DOOR, T: 6 YE 1  INSULATION 846 INTERNAL STRUCTURE. I: 6 YE  LINING  522201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE  (EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE.  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 522201-01-2 N/A TASK DELETED  522202-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1  ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  522203-01-1 N/A TASK DELETED  522203-01-2 N/A TASK DELETED  522221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE  (EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 6 YE  EXTERNAL SURFACE  522221-01-2 N/A TASK DELETED  522221-01-3 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 12 YE  (EMERGENCY/PASSENGER/CREW DOOR) SKIN, I: 12 YE  EXTERNAL SURFACE  522222-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1  ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), I: 6 YE  INSULATION INTERNAL STRUCTURE  LINING  523101-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE. I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 523101-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FC  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE. I: 3000 FC  523102-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO T: 12 YE 1  821CR 821DR COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YE  LINING  523103-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF T: 12000 FC  FORWARD CARGO COMPARTMENT DOOR (10 PLACES). I: 9000 FC  523104-01-1 132AR 132BR 132CR 132 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR T: 12 YE 1  132DR 132ER 132FR 821 HINGE ASSEMBLIES AT FR 20B TO FR25 (10 PLACES). I: 12 YE  132GR 132HR 132JR  132KR 132LR  523105-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FC  FITTING OF FORWARD CARGO COMPARTMENT DOOR AT I: 8300 FC  FR 22A.  523106-01-1 N/A TASK DELETED  523121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YE  N 523121-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FC  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 3000 FC  523122-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO T: 12 YE 1  LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 523123-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF FWD CARGO T: 12000 FC  COMPARTMENT DOOR (10 PLACES) I: 9000 FC  523124-01-1 132AR 132BR 132CR 132 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT T: 12 YE 1  132DR 132ER 132FR 821 DOOR HINGE ASSEMBLIES AT FR 20B TO FR 25 (10 PLACES). I: 12 YE  132GR 132HR 132JR  132KR 132LR  523125-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FC  FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A I: 8300 FC  523201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO T: 6 YE  COMPARTMENTS DOOR SKIN, EXTERNAL SURFACE. I: 6 YE  R 523201-01-2 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO T: 3000 FC  COMPARTMENTS DOOR SKIN, EXTERNAL SURFACE. I: 3000 FC  523202-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1  822CR 822DR DOOR, INTERNAL STRUCTURE. I: 6 YE  LINING  523203-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF LATCHING HOOKS OF AFT T: 12000 FC  CARGO COMPARTMENT DOOR (10 PLACES). I: 9000 FC  523204-01-1 152AR 152BR 152CR 152 DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR T: 12 YE 1  152DR 152ER 152FR 822 HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES). I: 12 YE  152GR 152HR 152JR  152KR 152LR  523205-01-1 822 822 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FC  FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A. I: 8300 FC  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 523221-01-1 N/A 800 GENERAL VISUAL INSPECTION OF T: 6 YE  AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL I: 6 YE  SURFACE  N 523221-01-2 N/A 800 GENERAL VISUAL INSPECTION OF T: 3000 FC  AFT CARGO COMPARTMENT DOOR SKIN, EXTERNAL I: 3000 FC  SURFACE  523222-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1  LINING DOOR, INTERNAL STRUCTURE. I: 6 YE  523223-01-1 822 822AR 822BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF AFT CARGO T: 12000 FC  COMPARTMENT DOOR (10 PLACES). I: 9000 FC  523224-01-1 152AR 152BR 152CR 152 DETAILED INSPECTION OF AFT CARGO COMPARTMENT T: 12 YE 1  152DR 152ER 152FR 822 DOOR HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES) I: 12 YE  152GR 152HR 152JR  152KR 152LR  523225-01-1 N/A TASK DELETED  R 523301-01-1 N/A 823 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 550 FC  DOOR SKIN, EXTERNAL SURFACE. I: 550 FC  523301-01-2 N/A 823 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE  DOOR SKIN, EXTERNAL SURFACE. I: 6 YE  523302-01-1 823 823 DETAILED INSPECTION OF BULK CARGO T: 12 YE 1  LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 523303-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK T: 12 YE 1  CARGO COMPARTMENT DOOR. I: 12 YE  523321-01-1 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO T: 6 YE  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YE  N 523321-01-2 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO T: 550 FC  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 550 FC  523322-01-1 823 823 DETAILED INSPECTION OF BULK CARGO T: 12 YE 1  LINING COMPARTMENT DOOR, INTERNAL STRUCTURE I: 6 YE  523323-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK T: 12 YE 1  CARGO COMPARTMENT DOOR. I: 12 YE  524101-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 524101-02-2 N/A 800 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT T: 6 YE  LOWER ACCESS DOOR SKIN, EXTERNAL SURFACE. I: 6 YE  524102-01-1 811 121 DETAILED INSPECTION OF AVIONICS COMPARTMENT T: 6 YE 1+2  DOOR FLOOR PANEL 122 LOWER ACCESS DOOR INTERNAL STRUCTURE, INCLUDING I: 6 YE  811 DOOR STOPS AND HINGE FITTINGS ON FUSELAGE.  524103-01-1 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 14300 FC  DOOR FLOOR PANEL 122 STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR I: 14300 FC  811 CROSS MEMBERS.  524121-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT T: 6 YE  ACCESS DOOR SKIN, EXTERNAL SURFACE. I: 6 YE  524121-02-1 N/A TASK DELETED  524122-01-1 811 121 DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER T: 6 YE 1+2  122 ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS I: 6 YE  811 AND HINGE FITTINGS ON FUSELAGE.  524201-01-1 195HB 195 GENERAL VISUAL INSPECTION OF ACCESS DOOR TO BLUE T: 3 YE  HYDRAULIC BAY, INTERNAL AND EXTERNAL SKINS I: 3 YE  524202-01-1 195HB 195 DETAILED INSPECTION OF HINGES OF ACCESS DOOR TO BLUE T: 6 YE 1  HYDRAULIC BAY. I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 524203-01-1 196PB 196 GENERAL VISUAL INSPECTION OF ACCESS DOOR TO YELLOW T: 3 YE  HYDRAULIC BAY, INTERNAL AND EXTERNAL SKINS I: 3 YE  524204-01-1 196PB 196 DETAILED INSPECTION OF HINGES OF ACCESS DOOR TO T: 6 YE 1  YELLOW HYDRAULIC BAY. I: 6 YE  528101-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, T: 3 YE  744 MAIN DOOR, EXTERNAL SKIN, LH/RH I: 3 YE  528102-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, T: 3 YE  744 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YE  528103-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 12 YE 1  744 MAIN DOOR, FORWARD AND AFT FITTINGS, LH/RH. I: 12 YE  528104-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 6 YE 1  744 MAIN DOOR, CENTER FITTING AND SURROUNDING AREA (300 I: 6 YE  MM AROUND), LH/RH.  NOTE: TPS APPLICATION REQUIRED ON FITTING ONLY  528104-01-2 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR T: 6 YE 1  744 MAIN DOOR CENTER FITTING AND SURROUNDING AREA (300 I: 6 YE  MM AROUND), LH/RH.  NOTE: TPS APPLICATION REQUIRED ON FITTING ONLY  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 528121-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR DOOR, T: 3 YE  744 EXTERNAL SKIN, LH/RH. I: 3 YE  528122-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR DOOR, T: 3 YE  744 INTERNAL SKIN, LH/RH. I: 3 YE  528123-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, T: 6 YE 1  744 FWD AND AFT HINGES, INCLUDING FITTINGS ON KEELBEAM, I: 6 YE  LH/RH.  528124-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOOR, AREA T: 3 YE  744 AROUND CENTER FITTING (300 MM AROUND) , LH/RH. I: 3 YE  528125-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, T: 6 YE 1  744 CENTER HINGE, INCLUDING FITTINGS ON KEELBEAM, I: 6 YE  LH/RH.  528126-01-1 N/A TASK DELETED  528201-01-1 N/A 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  714 FORWARD DOOR, EXTERNAL SKIN, LH/RH. I: 3 YE  528202-01-1 713 714 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  714 FORWARD DOOR, INTERNAL SKIN, LH/RH I: 3 YE  528203-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR T: 6 YE 1  714 FORWARD DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDING I: 6 YE  FITTINGS ON FUSELAGE, LH/RH  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 528204-01-1 715 716 715 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  716 AFT DOOR, EXTERNAL AND INTERNAL I: 3 YE  SKINS, LH/RH.  528221-01-1 N/A 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  714 FORWARD DOOR, EXTERNAL SKIN, LH/RH. I: 3 YE  528222-01-1 713 714 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  714 FORWARD DOOR, INTERNAL SKIN, LH/RH. I: 3 YE  528223-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1  714 DOORS, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS I: 6 YE  ON FUSELAGE, LH/RH.  528224-01-1 715 716 700 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YE  715 AFT DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH. I: 3 YE  716  528225-01-1 715 716 715 DETAILED INSPECTION OF NOSE LANDING GEAR, AFT DOOR, T: 6 YE 1  716 HINGES (NO4, NO5) INCLUDING FITTINGS ON FUSELAGE, I: 6 YE  LH/RH.  528301-01-1 N/A 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  754 MAIN DOOR, EXTERNAL SKIN, LH/RH. I: 3 YE  528302-01-1 753 754 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  754 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YE  528303-01-1 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1  754 MAIN DOOR FITTINGS, LH/RH. I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 528303-01-2 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 13000 FC  754 MAIN DOOR FITTINGS, LH/RH. I: 3950 FC  528304-01-1 755 756 755 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  756 AFT DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH. I: 3 YE  528305-01-1 755 756 755 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1  756 AFT DOOR, FORWARD FITTINGS LH/RH. I: 6 YE  528321-01-1 N/A 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  754 MAIN DOOR, EXTERNAL SKIN, LH/RH. I: 3 YE  528322-01-1 753 754 753 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  754 MAIN DOOR, INTERNAL SKIN, LH/RH. I: 3 YE  528323-01-1 753 754 753 DETAILED INSPECTION OF CENTER LANDING GEAR, MAIN T: 6 YE 1  754 DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS I: 6 YE  ON KEELBEAM, LH/RH.  528324-01-1 N/A 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  755 MAINTENANCE DOOR, EXTERNAL SKIN, LH/RH. I: 3 YE  756  528325-01-1 755 756 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  755 MAINTENANCE DOOR, INTERNAL SKIN, LH/RH. I: 3 YE  756  528326-01-1 755 756 755 DETAILED INSPECTION OF CENTER LANDING GEAR, T: 6 YE 1  756 MAINTENANCE DOOR ATTACHMENT AND LOCK FITTINGS, LH/RH. I: 6 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 528327-01-1 N/A 700 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 3 YE  752 LEG DOOR, INTERNAL AND EXTERNAL SKIN, LH/RH. I: 3 YE  528328-01-1 N/A 755 DETAILED INSPECTION OF CENTER LANDING GEAR, LEG T: 6 YE 1  756 DOOR FITTINGS, LH/RH. I: 6 YE  528329-01-1 N/A 752 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR, T: 6 YE  HINGED DOOR, EXTERNAL SKIN. I: 6 YE  528330-01-1 N/A 149 DETAILED INSPECTION OF CENTER LANDING GEAR, HINGED T: 6 YE 1  DOOR, INTERNAL STRUCTURE AND HINGES. I: 6 YE  528331-01-1 757 758 149 DETAILED INSPECTION OF CENTER LANDING GEAR, HINGED T: 6 YE 1  DOOR, TRIPOD AND ANGLE FITTING. I: 6 YE  528332-01-1 N/A TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531101-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT T: 6 YE 3  RADOME OPENED PRESSURE BULKHEAD ATTACHED TO FR.1. I: 6 YE  531102-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, T: 6 YE  EXTERNAL VISIBLE PORTION OF FRAMEWORK BETWEEN FR 3 I: 6 YE  AND FR 10, LH/RH  531103-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE  FR 10 AND FR 18 FROM CABIN FLOOR LEVEL TO STR 9 I: 6 YE  (FWD AND AFT), EXTERNAL SURFACE, LH/RH.  531104-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, T: 12 YE  EXTERNAL PORTIONS OF FRAMEWORK COVERED BY I: 12 YE  RETAINERS.  531105-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, T: 6 YE  EXTERNAL VISIBLE PORTIONS OF RETAINERS. I: 6 YE  531106-01-1 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FC  FR 9 AND FR 10A AT COCKPIT LATERAL WINDOW LOWER I: 10200 FC  CORNER AREA, EXTERNAL SURFACE, LH/RH.  531106-01-2 N/A TASK DELETED  R 531107-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE  FR 0 AND FR 10 FROM FLOOR LEVEL TO CROWN I: 3 YE  CENTERLINE, EXTERNAL SURFACE  531110-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 531111-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE  FR 10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 3 YE  CENTERLINE, EXTERNAL SURFACE, LH/RH.  531112-02-1 N/A TASK DELETED  531115-01-1 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 6 YE  INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YE  CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RH  531115-01-2 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 12 YE  INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YE  CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RH  531116-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE  AND JOINT SURFACES BETWEEN FR 0 AND I: 6 YE  FR 18/19 BELOW CABIN FLOOR LEVEL,  EXTERNAL SURFACE  531117-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  PANELS 122 STRUCTURE BETWEEN FR 1 AND FR 20, FROM CABIN FLOOR I: 12 YE  NOTE 1 LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL, INCLUDING  CABIN FLOOR SUPPORT STRUCTURE AND NLG BAY PANELS AND  BEAMS.  NOTE: TPS APPLICATION REQUIRED ONLY BETWEEN FR 10 AND  FR 20, EXCLUDING NLG BAY PANELS  531118-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531120-01-1 713 714 123 GENERAL VISUAL INSPECTION OF NLG BAY INTERNAL T: 6 YE 1+2  STRUCTURE, NOSE LANDING GEAR WELL PANELS I: 6 YE  531120-01-2 N/A TASK DELETED  531121-01-1 AVIONIC BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  PANEL 122 STRUCTURE BETWEEN FR 10 AND FR 20 BELOW AVIONICS I: 12 YE  COMPARTMENT FLOOR LEVEL  531122-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  PANEL 122 STRUCTURE BETWEEN FR 1 AND FR 10 BELOW AVIONICS I: 12 YE  COMPARTMENT FLOOR LEVEL  531123-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  122 STRUCTURE BELOW GALLEYS AND TOILETS FROM CABIN I: 6 YE  FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL  BETWEEN FR 10 AND FR 13A, LH/RH  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA  531124-01-1 713 714 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 13000 FC  SIDE PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR I: 9600 FC  BAY FORWARD PANEL TO NOSE LANDING GEAR BAY AFT  PANEL, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531124-01-2 713 714 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 13000 FC  SIDE PANEL TOP INNER RADIUS FROM NOSE LANDING GEAR OR  BAY FORWARD PANEL TO NOSE LANDING GEAR BAY AFT 26000 FH  PANEL, LH/RH. I: 11400 FC  OR  22800 FH  531125-01-1 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT T: 13000 FC  AVIONIC BAY FLOOR 122 TO BOTTOM SKIN FROM STR 48 TO STR 51, LH/RH. I: 5700 FC  PANELS  531125-01-2 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 13000 FC  AVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STR 48 TO STR 51, LH/RH. OR  PANELS 26000 FH  I: 5700 FC  OR  11400 FH  531126-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AFT T: 12 YE 1  716 SIDE PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, I: 12 YE  LH/RH.  531127-01-1 N/A TASK DELETED  531127-02-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FC  716 STRUT FITTING LUG BORE I: 13000 FC  531127-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FC  716 STRUT FITTING LUG BORE I: 13000 FC  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531127-02-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FC  716 STRUT FITTING LUG BORE I: 13000 FC  531127-02-4 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 13000 FC  716 STRUT FITTING LUG BORE OR  26000 FH  I: 13000 FC  OR  26000 FH  531129-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR T: 12 YE 1+2  716 FITTING. I: 12 YE  BOLTS  NLG ACTUATOR  DISCONNECTED  531129-02-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING T: 13000 FC  716 GEAR ACTUATOR FITTING. I: 4700 FC  BOLTS  NLG ACTUATOR  DISCONNECTED  531129-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 13000 FC  716 ACTUATOR FITTING. I: 11500 FC  BOLTS  NLG ACTUATOR  DISCONNECTED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531130-01-1 NOTE 1 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  122 STRUCTURE, FR 16A AT CABIN FLOOR LEVEL, LH/RH. I: 3750 FC  531131-01-1 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 122 FR16A JOINT AREA BETWEEN STRS 28 AND 30, LH/RH. I: 9800 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 531131-02-1  531131-02-1 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 122 STRUCTURE, FR 16A JOINT AREA BETWEEN STRS 28 AND 30, I: 9800 FC  LH/RH.  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 531131-01-1  531132-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  122 FR14 JOINT BETWEEN STRS 28 AND 30 LEVEL, LH/RH. I: 12900 FC  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531133-01-1 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 122 STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM I: 9800 FC  JUNCTION ON FR12A AT STR 26 LEVEL LH/RH.  531133-01-2 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 122 STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM I: 9800 FC  JUNCTION ON FR12A AT STR 26 LEVEL LH/RH.  531133-01-3 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 13000 FC  NOTE 1 122 BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON I: 13000 FC  FR12A AT STR 26 LEVEL LH/RH.  531135-01-1 N/A TASK DELETED  531136-01-1 CEILING PANELS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 222 STRUCTURE, FRS 12 AND 13 DOUBLER AREA AT CROWN I: 10100 FC  CENTERLINE.  531137-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR DRAG STRUT T: 12 YE 1  716 FITTING ATTACHMENTS TO UPPER AND FORWARD CANTED I: 12 YE  PANEL.  531138-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD PRESSURE T: 13000 FC  RADOME OPENED BULKHEAD FORWARD FACE, STRINGERS AND SKIN, I: 9200 FC  FROM Y =-50 TO Y = 50 ABOVE COCKPIT FLOOR LEVEL  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531139-01-1 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 212 STRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACE I: 9200 FC  VERTICAL BEAMS AND UPPER SHEET AT Y =-330,  Y = 0 AND Y = 330, ABOVE COCKPIT FLOOR LEVEL.  531140-01-1 N/A TASK DELETED  531141-01-1 LININGS 211 DETAILED INSPECTION OF LATERAL FR11, SPLICE T: 13000 FC  NOTE 1 212 ABOVE COCKPIT FLOOR LEVEL ATTACHMENT, INTERNAL I: 9080 FC  STRUCTURE, LH/RH.  531142-01-1 CEILING PANELS 211 DETAILED INSPECTION OF FR 10 UPPER CURVED T: 13000 FC  NOTE 1 212 MEMBER BETWEEN CROWN CENTERLINE AND UPPER LATERAL I: 5250 FC  SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  531142-02-1.  531142-02-1 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FR 10 UPPER T: 13000 FC  NOTE 1 212 CURVED MEMBER BETWEEN CROWN CENTERLINE AND UPPER I: 7800 FC  LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL  STRUCTURE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  531142-01-1.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531143-01-1 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 122 FLOOR BEAM AND CRUCIFORM FITTING AT FR 14, LH/RH. I: 4000 FC  VACUUM PIPES  531144-01-1 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 122 STRUCTURE, JUNCTION AREA BETWEEN FR 14 AND CRUCIFORM I: 7100 FC  TOILET FITTING, LH/RH.  R 531150-01-1 311VU 312VU 313VU 211 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1  314VU 811 212 BULKHEAD ABOVE FLOOR LEVEL, INCLUDING FR1, AS FAR AS I: 12 YE  ACCESS BETWEEN FR1 VISIBLE  AND FR2 FROM AVIONIC  BAY NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THE  NOTE 1 PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETE  AFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED  AND ELECTRONIC DEVICE REMOVED.  531151-01-1 AVIONICS FORWARD 121 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1  FLOOR PANELS 122 BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR PANELS, I: 6 YE  NOTE 1 INCLUDING FR 1 AND STRINGER CONNECTIONS.  WIRING BUNDLES  DISPLACED NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THE  PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETE  AFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTED  AND ELECTRONIC DEVICE REMOVED.  531152-01-1 LINING 211 DETAILED INSPECTION OF COCKPIT WINDOW FRAMES T: 12 YE T: 20 YE  NOTE 1 212 AND CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND I: 12 YE I: 12 YE  FORWARD).  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531154-01-1 N/A TASK DELETED  531154-01-2 INSULATION TO BE 211 DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING T: 13000 FC  DISPLACED AS 212 PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, I: 8100 FC  REQUIRED TO COMPLETE INTERNAL STRUCTURE, LH/RH.  THE INSPECTION  LININGS  NOTE 1  SLIDING WINDOWS  OPENED  531156-01-1 CEILING PANELS 211 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  FCRC (IF INSTALLED) 212 STRUCTURE ABOVE FLOOR LEVEL, FROM FR1 TO FR 17, I: 12 YE  GALLEYS AND TOILETS 221 EXCLUDING:  NOTE 1 222 - UPPER AFT FACE OF FORWARD PRESSURE BULKHEAD.  OVERHEAD PANELS 223 - WINDSHIELD AND WINDOW FRAMES SURROUNDINGS  SIDEWALL PANELS 224 BETWEEN FWD COCKPIT AND FR 10  - INTERNAL STRUCTURE AROUND DOOR 1 (FORWARD  PASSENGER/CREW DOOR)  531157-01-1 LINING 233 DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPER T: 13000 FC  NOTE 1 234 KEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL, I: 10170 FC  INTERNAL STRUCTURE, LH/RH.  531159-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  NOTE 1 222 STRUCTURE AROUND DOOR 1 (FORWARD PASSENGER/CREW I: 6 YE  DOOR), BETWEEN FR 13A AND FR 17 AND BETWEEN FLOOR  LEVEL AND STR 9 (AFT), LH/RH.  531161-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531162-01-1 831 841 211 SPECIAL DETAILED INSPECTION OF FR 7 AND T: 13000 FC  COCKPIT FLOOR PANELS 212 CROSS BEAM AT ATTACHMENT AREA I: 7800 FC  531162-01-2 831 841 211 SPECIAL DETAILED INSPECTION OF FR 7 AND T: 13000 FC  COCKPIT FLOOR PANELS 212 CROSS BEAM AT ATTACHMENT AREA I: 7500 FC  531170-01-1 COCKPIT FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF COCKPIT FLOOR STRUCTURE T: 12 YE  212 BETWEEN FR 1 AND FR 10 I: 12 YE  531171-01-1 CABIN FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2  212 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YE  221 TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 17  222  531172-01-1 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2  FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YE  GALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 17  222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.  531172-01-2 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2  FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YE  GALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 17  222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.  531173-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  122 BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM I: 6 YE  CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR  LEVEL, BETWEEN FR 13A AND FR 17, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531175-01-1 LINING 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 13000 FC  NOTE 1 232 JUNCTION BETWEEN FR 17 AND MACHINED STIFFENERS AT I: 8000 FC  STRS 14/18/22/24, LH/RH.  531175-01-2 LININGS 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 13000 FC  NOTE 1 232 JUNCTION BETWEEN FR 17 AND MACHINED STIFFENERS AT I: 8000 FC  STRS 14/18/22/24, LH/RH.  531176-01-1 FWD AVIONICS BAY 121 GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE T: 6 YE 1+2  DOOR OPENED BELOW BATTERIES BETWEEN FR 10A AND FR 11A AND I: 6 YE  NOTE 1 BETWEEN STR 41 AND STR 43, LH  531180-01-1 N/A TASK DELETED  531185-01-1 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 FORWARD PASSENGER / CREW DOOR CUTOUT AFT UPPER I: 8850 FC  CORNER, JUNCTION OF INTERNAL PLATE ON FR. 17, BETWEEN  STR.12 AND 13, LH/RH.  531186-01-1 N/A TASK DELETED  531187-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531188-01-1 N/A TASK DELETED  531189-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, I: 8850 FC  FORWARD UPPER LONGERON AT STRINGER 12 LEVEL, BETWEEN  FR. 13A AND FR.13B, LH/RH.  531192-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9 I: 8100 FC  FORWARD, AND FR 13 AFT FACE AND STR 12, LH/RH.  531192-01-2 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9 I: 8100 FC  FORWARD, AND FR 13 AFT FACE AND STR 12, LH/RH.  531194-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 MACHINED STIFFENERS 14 AND 22 BETWEEN FR 17 AND FR I: 8100 FC  18, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531194-01-2 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  NOTE 1 222 MACHINED STIFFENERS 14 AND 22 BETWEEN FR 17 AND FR I: 8100 FC  18, LH/RH.  531198-01-1 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 13000 FC  NOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 8850 FC  BETWEEN FR 13A AND FR 14 AND FR 16A AND FR 17, LH/RH.  531801-01-1 NOTE 1 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE T: 6 YE 3  PANELS BULKHEAD ATTACHED TO FR.1. I: 6 YE  RADOME OPENED  531802-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, T: 6 YE  EXTERNAL VISIBLE PORTION OF FRAMEWORK BETWEEN FR 3 I: 6 YE  AND FR 10, LH/RH  531803-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE  FR.10 AND FR.18 FROM CABIN FLOOR LEVEL TO STR 9 I: 6 YE  (FWD AND AFT), EXTERNAL SURFACE, LH/RH.  531804-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 12 YE  PORTION OF FRAMEWORK COVERED BY RETAINERS. I: 12 YE  531805-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 6 YE  VISIBLE PORTION OF RETAINERS. I: 6 YE  531807-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 6 YE  FR 0 AND FR 10 FROM FLOOR LEVEL TO CROWN CENTERLINE, I: 6 YE  EXTERNAL SURFACE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531810-01-1 N/A TASK DELETED  531811-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE  FR 10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 12 YE  CENTERLINE, EXTERNAL SURFACE, LH/RH.  531812-01-1 N/A TASK DELETED  531815-01-1 SCUFF PLATE 100 DETAILED INSPECTION OF FUSELAGE STRUCTURE OF DOOR 1 T: 12 YE  (FWD PASSENGER/CREW DOOR), CUTOUT UNDERNEATH THE I: 6 YE  SCUFF-PLATE, LH/RH.  531816-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND T: 6 YE  JOINT SURFACES BETWEEN FR 0 AND FR 18/19 BELOW I: 6 YE  CABIN FLOOR LEVEL, EXTERNAL SURFACE.  531816-01-2 N/A TASK DELETED  531817-01-1 811 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  NOTE 1 122 STRUCTURE BETWEEN FR 1 AND FR 20 FROM CABIN I: 12 YE  FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL,  INCLUDING CABIN FLOOR SUPPORT STRUCTURE AND  NLG BAY PANELS AND BEAMS.  NOTE: TPS APPLICATION REQUIRED ONLY  BETWEEN FR 10 AND FR 20, EXCLUDING NLG BAY PANELS.  531818-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531820-01-1 713 714 123 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY T: 6 YE 1+2  INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS I: 6 YE  531820-01-2 N/A TASK DELETED  531821-01-1 AVIONIC BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  PANELS 122 STRUCTURE BELOW AVIONICS COMPARTMENT FLOOR I: 12 YE  LEVEL BETWEEN FR.10 AND FR. 20, LH/RH.  531822-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2  PANELS 122 STRUCTURE BELOW AVIONICS COMPARTMENT FLOOR I: 12 YE  NOTE 1 LEVEL BETWEEN FR.1 AND FR.10, LH/RH.  531823-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  122 BELOW GALLEYS AND TOILETS FROM CABIN FLOOR LEVEL TO I: 6 YE  AVIONICS COMPARTMENT FLOOR LEVEL BETWEEN FR 10 AND  FR 13A, LH/RH.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA  531824-01-1 N/A TASK DELETED  531826-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY T: 12 YE 1  716 LATERAL PANELS AROUND DRAG STRUT AND NOSE LANDING I: 12 YE  GEAR ATTACHMENT FITTINGS, LH/RH.  531827-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR BAY, ANGLE T: 6 YE 1  716 FITTINGS LINKING FORWARD CANTED PANEL TO ROOF PANEL. I: 6 YE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531827-01-2 N/A TASK DELETED  531829-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AND NOSE T: 12 YE 1  716 LANDING GEAR DOORS ACTUATOR FITTINGS, LH/RH. I: 12 YE  BOLTS  DOORS ACTUATOR  DISCONNECTED  531835-01-1 N/A TASK DELETED  R 531850-01-1 311VU 312VU 313VU 211 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1  314VU 811 212 BULKHEAD ABOVE COCKPIT FLOOR LEVEL, INCLUDING FR 1, I: 12 YE  ACCESS BETWEEN FR1 AS FAR AS VISIBLE.  AND FR2 FROM AVIONIC NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF  BAY THE PRESSURE BULKHEAD (SEE SSI 53-18-51),THE  NOTE 1 COMPLETE AFT FACE (UPPER AND LOWER AREA)  HAS TO BE INSPECTED AND ELECTRONIC DEVICE REMOVED  531851-01-1 AVIONIC FWD FLOOR 121 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1  PANELS TO BE REMOVED 122 BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR I: 12 YE  INSULATION AND PANELS, INCLUDING FR.1 AND STRINGER CONNECTIONS.  WIRING BUNDLES TO BE NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF  DISPLACED PRESSURE BULKHEAD, THE COMPLETE AFT FACE (UPPER AND  LOWER AREA) HAS TO BE INSPECTED AND ELECTRONIC  DEVICE REMOVED (SEE SSI 53-18-50)  531852-01-1 LINING 211 DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND T: 12 YE T: 20 YE  NOTE 1 212 CLOSING PANELS, INTERNAL STRUCTURE (FR10 AND I: 12 YE I: 12 YE  FORWARD).  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531856-01-1 CEILING PANELS 210 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  FCRC (IF INSTALLED) 220 STRUCTURE ABOVE FLOOR LEVEL, FROM FR 1 TO FR 17, I: 12 YE  GALLEYS AND TOILETS 230 EXCLUDING :  (IF INSTALLED) - UPPER AFT FACE OF FORWARD PRESSURE BULKHEAD,  NOTE 1 - WINDSHIELD AND WINDOW FRAMES SURROUNDINGS BETWEEN  OVERHEAD PANELS FWD COCKPIT AND FR 10,  SIDEWALL PANELS - INTERNAL STRUCTURE AROUND DOOR 1 (FORWARD  PASSENGER/CREW DOOR)  531859-01-1 LININGS 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2  NOTE 1 222 AROUND DOOR 1 (FORWARD PASSENGER / CREW DOOR), I: 6 YE  BETWEEN FR13A AND FR17 AND BETWEEN FLOOR LEVEL AND  STR 9 AFT, LH/RH.  531870-01-1 831 841 211 GENERAL VISUAL INSPECTION OF COCKPIT FLOOR T: 12 YE  COCKPIT FLOOR PANELS 212 STRUCTURE BETWEEN FR.1 AND FR.10. I: 12 YE  531871-01-1 831 841 211 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2  CABIN FLOOR PANELS 212 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YE  221 TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.  222  531872-01-1 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2  FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YE  GALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.  (IF INSTALLED) 222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.  531872-01-2 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2  FCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YE  GALLEYS AND TOILETS 221 DOORS ENTRANCE AREA, FROM FR 10 TO FR 20.  (IF INSTALLED) 222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.  531873-01-1 811 821 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  NOTE 1 122 BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM I: 6 YE  CABIN FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR  LEVEL BETWEEN FR 13A AND FR 17, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 531876-01-1 FLOOR PANELS 121 DETAILED INSPECTION OF FUSELAGE STRUCTURE BELOW T: 6 YE 1+2  FWD AVIONICS BAY BATTERIES FROM FR10 TO 17 AND FROM STR 40 TO BOTTOM I: 6 YE  DOOR CENTERLINE AND NLG BAY LATERAL PANEL, LH.  NOTE 1  531880-01-1 N/A TASK DELETED  532101-01-1 N/A TASK DELETED  532101-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO I: 6 YE  BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP  JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING,  LH/RH.  532102-01-1 821 133 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  CARGO COMPARTMENT 134 STRUCTURE BETWEEN FR 20 AND FR 39.1 BELOW I: 6 YE  FLOOR PANELS CARGO COMPARTMENT FLOOR PANELS.  R 532103-01-1 821 131 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CARGO COMPARTMENT 132 STRUCTURE BETWEEN MAIN DECK FLOOR I: 12 YE  CEILING PANELS PANELS AND CARGO COMPARTMENT FLOOR FROM FR 20  LINING TO FR 39.1.  NOTE 1  R 532104-01-1 821 131 DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE T: 6 YE 1+2  CARGO COMPARTMENT 132 FROM MAIN DECK FLOOR TO CARGO COMPARTMENT I: 6 YE  LINING FLOOR, BELOW AND 0.75 M FWD AND AFT OF GALLEYS AND  NOTE 1 TOILETS, FROM FR 20 TO FR 39.1 LH/RH.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532105-01-1 821 134 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  BALLMATS STRUCTURE BELOW FORWARD CARGO COMPARTMENT DOOR I: 6 YE  CUT-OUT BETWEEN FR 19 AND FR 26 FROM CARGO  COMPARTMENT FLOOR TO STR 46 RH.  532107-01-1 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1+2  COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND I: 6 YE  FR 25 (10 PLACES)  532107-01-2 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 7500 FC  COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND I: 7500 FC  FR 25 (10 PLACES)  R 532107-02-1 821 134 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO T: 6 YE T: 20 YE  ECCENTRIC BOLTS COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND I: 6 YE I: 6 YE  FR 25  532108-01-1 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1  INSULATION 132 STRUCTURE AROUND FORWARD CARGO COMPARTMENT DOOR I: 12 YE  LINING CUT-OUT BETWEEN FR 19 AND FR 26 FROM STR 26 RH TO  CARGO COMPARTMENT FLOOR LEVEL.  532109-01-1 N/A TASK DELETED  532110-01-1 N/A TASK DELETED  532111-01-1 N/A TASK DELETED  532114-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532114-01-2 N/A TASK DELETED  532115-01-1 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1  COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL I: 6 YE  FRAMES (FR 20A AND FR 25A)  532115-01-2 N/A TASK DELETED  532116-01-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE  234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YE  PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 6 AND  CROWN CENTERLINE, LH/RH.  532116-02-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE  234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YE  PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 13 AND  CROWN CENTERLINE, LH/RH.  532116-03-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE  234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YE  PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 3 AND  CROWN CENTERLINE AND BETWEEN STR 7 TO STR 17, LH/RH.  532117-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 532117-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, I: 12 YE  LH/RH.  532118-01-1 N/A TASK DELETED  R 532119-01-1 832 842 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 232 STRUCTURE BETWEEN FR 17 AND FR 36, FROM STR 15 I: 12 YE  SIDEWALL LINING 241 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO  242 MAIN DECK FLOOR, LH/RH.  532120-01-1 832 842 233 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CEILING PANELS 234 STRUCTURE BETWEEN FR 17 AND FR 36 FROM STR 15 I: 12 YE  NOTE 1 243 TO CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 244  BINS  532121-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE  SURFACE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YE  CUT-OUT BETWEEN FR 32 AND FR 36, FROM STR 9 TO STR  26, LH/RH.  R 532122-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  AIR CONDITION DUCTS 132 STRUCTURE BELOW DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YE  NOTE 1 CUT-OUT BETWEEN FR 32 AND FR 36, FROM MAIN DECK FLOOR  SIDEWALL LINING DOWN TO STR 30, LH/RH.  R 532123-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1  NOTE 1 242 STRUCTURE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 12 YE  SIDEWALL/DOOR FRAME 243 CUT-OUT BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOOR  LINING 244 UP TO STR 9, LH/RH.  532124-01-1 832 842 100 DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW T: 12 YE  SCUFF PLATE 200 DOOR) CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH I: 6 YE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532124-02-1 N/A TASK DELETED  532124-02-2 N/A TASK DELETED  532124-02-3 N/A TASK DELETED  532125-01-1 N/A TASK DELETED  532125-01-2 N/A TASK DELETED  532125-01-3 N/A TASK DELETED  532128-01-1 N/A TASK DELETED  532129-01-1 N/A TASK DELETED  532130-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 532134-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2  FLOOR PANELS 232 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YE  GALLEYS AND TOILETS 241 DOOR ENTANCE AREAS, FROM FR 17 TO FR 36.  242  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN 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  FLOOR PANELS 232 BELOW AND 0.75M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YE  GALLEYS AND TOILETS 241 DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.  242  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  R 532135-01-1 831 841 231 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE  FLOOR PANELS 232 STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND TOILETS, I: 12 YE  241 AND DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.  242  532138-01-1 N/A TASK DELETED  532142-01-1 N/A TASK DELETED  532143-01-1 N/A TASK DELETED  532144-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532145-01-1 N/A TASK DELETED  532146-01-1 N/A TASK DELETED  532147-01-1 N/A TASK DELETED  532148-01-1 N/A TASK DELETED  532149-01-1 N/A TASK DELETED  532150-01-1 N/A TASK DELETED  532152-01-1 N/A TASK DELETED  532153-01-1 N/A TASK DELETED  532154-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532155-01-1 N/A TASK DELETED  532156-01-1 N/A TASK DELETED  532157-01-1 N/A TASK DELETED  532158-01-1 N/A TASK DELETED  532158-02-1 N/A TASK DELETED  532159-01-1 N/A TASK DELETED  532160-01-1 N/A TASK DELETED  532161-01-1 N/A TASK DELETED  532162-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532163-01-1 N/A TASK DELETED  532165-01-1 N/A TASK DELETED  532165-02-1 N/A TASK DELETED  N 532166-01-2 N/A 200 GENERAL VISUAL INPECTION OF FUSELAGE SKIN EXTERNAL T: 3 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO I: 3 YE  CROWN CENTER LINE.  532201-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE  EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 I: 6 YE  FROM STR 26 LH/RH TO BOTTOM CENTER LINE,  EXCLUDING AREA UNDERNEATH BELLY FAIRING.  532201-01-2 N/A TASK DELETED  532202-01-1 821 133 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 134 STRUCTURE BETWEEN FR 20 AND FR 39 BELOW CARGO I: 6 YE  CARGO COMPARTMENT COMPARTMENT FLOOR PANELS.  FLOOR PANELS  532203-01-1 821 131 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE  ACT (IF INSTALLED) 132 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN I: 12 YE  CARGO COMPARTMENT FLOOR AND CARGO COMPARTMENT FLOOR, FROM FR 20  LINING TO FR 39, LH/RH.  NOTE 1  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532204-01-1 821 131 DETAILED INSPECTION OF FUSELAGE SIDE SHELL INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 132 STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YE  CARGO COMPARTMENT CARGO COMPARTMENT FLOOR, BELOW AND 0.75 M FWD  INSULATION AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FR 20  LINING TO FR 39, LH/RH.  NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE  FITTED ABOVE THE AREA.  532205-01-1 132AZ 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  BALLMATS 134 BELOW FWD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  FR 19 AND FR 26 FROM CARGO COMPARTMENT FLOOR TO  STR 47, RH.  532207-01-1 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1+2  COMPARTMENT DOOR LOCK FITTINGS AND BUSHES I: 6 YE  AT 10 POSITIONS BETWEEN FR 20B AND FR 25.  532207-01-2 N/A TASK DELETED  532207-02-1 821 134 DETAILED INSPECTION OF FORWARD CARGO T: 6 YE T: 20 YE  ECCENTRIC BOLTS COMPARTMENT DOOR ECCENTRIC BOLTS AT I: 6 YE I: 6 YE  10 POSITIONS BETWEEN FR 20B AND FR 25.  532208-01-1 132AZ 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  INSULATION 132 AROUND FWD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  LINING FR 19 AND FR 26 FROM STR 26 TO CARGO COMPARTMENT  FLOOR, RH.  532215-01-1 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1  COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF I: 6 YE  LATERAL FRAMES (FR 20A AND FR 25A).  532215-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 532217-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, I: 12 YE  LH/RH.  532219-01-1 832 842 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 232 STRUCTURE BETWEEN FR 17 AND FR 37.11, FROM STR 15 I: 12 YE  SIDEWALL LINING 241 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO  242 PASSENGER CABIN FLOOR, LH/RH.  532220-01-1 832 842 233 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CEILING PANELS 234 STRUCTURE BETWEEN FR 17 AND FR 37.11, FROM I: 12 YE  NOTE 1 243 STR 15 TO CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 244  BINS  532221-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE  SURFACE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YE  CUT-OUT BETWEEN FR 37.7 AND FR 37.11, FROM STR 9 TO  STR 26, LH/RH.  532222-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1  ACT (IF INSTALLED) 132 BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YE  INSULATION BETWEEN FR 37.7 AND FR 37.11, FROM PASSENGER CABIN  LINING FLOOR TO CARGO COMPARTMENT FLOOR, LH/RH.  532223-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  INSULATION 242 AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 12 YE  LINING 243 BETWEEN FR 37.7 AND FR 37.11 FROM PASSENGER CABIN  244 FLOOR TO STR 9, LH/RH.  532224-01-1 832 842 100 DETAILED INSPECTION OF DOOR 2 T: 12 YE  SCUFF PLATE 200 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YE  UNDERNEATH SCUFF PLATE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 532234-01-1 821 831 841 131 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2  ACT (IF INSTALLED) 132 STRUCTURE BELOW AND 0,75 M AROUND GALLAYS AND I: 5 YE  CARGO COMPARTMENT 231 TOILETS, INCLUDING DOOR ENTRANCE AREAS FROM  CEILINGS 232 FR 20 TO FR 39.  FLOOR PANELS 241  GALLEYS AND TOILETS 242 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED  532234-01-2 821 831 841 131 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2  ACT (IF INSTALLED) 132 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YE  CARGO COMPARTMENT 231 TOILETS, INCLUDING DOOR ENTRANCE AREAS FROM  CEILINGS 232 FR 20 TO FR 39.  FLOOR PANELS 241  GALLEYS AND TOILETS 242 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  532235-01-1 831 841 231 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE  FLOOR PANELS 232 STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND I: 12 YE  241 TOILETS, AND DOOR ENTRANCE AREAS, FROM FR 20 TO  242 FR 39.  N 532266-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 3 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO I: 3 YE  CROWN CENTER LINE.  533001-01-1 196AB 196BB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FC  STRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON I: 5500 FC  ARCH MEMBER AT Y =-1445.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533001-01-3 196EB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FC  STRUCTURE AT FR 46, HAT-SECTION PROFILE JUNCTION ON I: 5500 FC  ARCH MEMBER AT Y =-1445.  533002-01-1 196AB 196BB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FC  FRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 10800 FC  LONGITUDINAL WEB AT Y =-493  533002-01-3 196GB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FC  FRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 10800 FC  LONGITUDINAL WEB AT Y =-493  533003-01-1 197AB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE, FR T: 13000 FC  197 53.2 WEB AT Y =-1042, Y =-728.7 AND Y = 728.7 BELOW I: 10800 FC  198 LONGITUDINAL WEB ATTACHMENT  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533004-01-1 197GB 198GB 197 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 13000 FC  198 STRUCTURE AFT OF FR 53.8, T-SECTION JUNCTION ON I: 5500 FC  LONGITUDINAL BEAM, LH/RH.  R 533005-01-1 191AB 191AT 191BB 191 DETAILED INSPECTION OF FUSELAGE SKIN AT T: 13000 FC  191CB 192AT 192BB 192 BELLY FAIRING SEALING LIP ATTACHMENT FROM FR 37.1 OR  192CB 197AT 197FB 197 TO FR 38 AND FROM FR 53.6 TO FR 56 75000 FH  197GB 197HB 198AT 198 I: 4750 FC  198GB 198HB OR  32300 FH  533006-01-1 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YE  148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 3 YE  197BB 197EB 197FB 149  197GB 197HB 198AT 197  198BB 198EB 198GB 198  198HB 734 744  753 754  533006-01-2 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YE  148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 6 YE  197BB 197EB 197FB 149  197GB 197HB 198AT 197  198BB 198EB 198GB 198  198HB 734 744  753 754  533007-01-1 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YE  191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB I: 3 YE  192BB 192CB  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533007-01-2 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YE  191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB I: 6 YE  192BB 192CB  533008-01-1 N/A 190 DETAILED INSPECTION OF BELLY FAIRING PANELS AND T: 3 YE  FASTENERS AT WING UPPER SURFACE TO FUSELAGE JUNCTION, I: 3 YE  FROM WING LEADING EDGE TO TRAILING EDGE, LH/RH.  533011-01-1 251PC 251QC 252PC 253 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  252QC 254 CIRCUMFERENTIAL JOINT AT FR 53.3 FROM STR 4 TO STR I: 13000 FC  NOTE 1 5, LH/RH (64 FASTENER POSITIONS).  OVERHEAD STOWAGE  BINS NOTE:  RIVETS TO BE REMOVED - ROTOTEST INSPECTION. FASTENER REMOVAL- 64 POSITIONS  - THIS TASK IS AN ALTERNATIVE TO TASK 533011-02-1  533011-02-1 251PC 251QC 252PC 253 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  252QC 254 CIRCUMFERENTIAL JOINT AT FR 53.3 FROM STR 4 TO STR 5, I: 3830 FC  NOTE 1 LH/RH (64 FASTENER POSITIONS).  OVERHEAD STOWAGE  BINS NOTE:  - X-RAY INSPECTION  - THIS TASK IS AN ALTERNATIVE TO TASK 533011-01-1  533019-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  CIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM I: 6000 FC  CENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 AND  STRG5) LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 533035-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 2.5 YE 1+2  BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 2.5 YE  A340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.47  (FOR A340-200) AND FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING,  FR.47 FROM Y=-2390 EXTERNAL SURFACE, LH/RH.  TO Y=2390  R 533035-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2  BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 6 YE  A340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.47  (FOR A340-200) AND FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING,  FR.47 FROM Y=-2390 EXTERNAL SURFACE, LH/RH.  TO Y=2390  R 533036-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 5 YE 1+2  BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 5 YE  FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLY  TO Y=2390. FAIRING, EXTERNAL SURFACE, LH/RH.  R 533036-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2  BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 6 YE  FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLY  TO Y=2390. FAIRING, EXTERNAL SURFACE, LH/RH.  N 533037-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 12 YE 1+2  BETWEEN FR.37.1 (FOR FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 I: 12 YE  A340-300) OR FR.34 (FOR A340-300) OR FR.34 (FOR A340-200) AND FR.56  (FOR A340-200) AND COVERED BY BELLY FAIRING, EXTERNAL SURFACE, EXCLUDING  FR.56 EXCLUDING AREA FROM Y=-2390 TO Y=2390, LH/RH.  PANELS FROM Y=-2390  TO Y=2390  533101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE NO  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 12 YE  TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533101-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 4000 FC  TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  533101-01-3 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING I: 5700 FC  TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  533101-01-4 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING OR  TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 26000 FH  I: 5200 FC  OR  10400 FH  533101-01-5 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 13000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO OR  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 65000 FH  I: 4000 FC  OR  27100 FH  533102-01-1 N/A TASK DELETED  R 533103-02-1 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 13000 FC  SKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR OR  19, LH/RH. 75000 FH  I: 7300 FC  OR  49500 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533104-01-1 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50MM AROUND T: 13000 FC  LIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 I: 6100 FC  OBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48  INSTALLED 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)  R 533104-01-2 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN STRINGER T: 13000 FC  LIGHTS, ANTENNAS AND 1LH AND 1RH 50 MM AROUND: OR  OBTURATORS WHERE - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 26000 FH  INSTALLED - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 I: 7200 FC  AND FR.49 AND BETWEEN FR.52 AND FR.53 OR  - AFIS ANTENNA CUTOUT BETWEEN FR.40 AND FR.40.1 (IF 14400 FH  INSTALLED).  533104-01-3 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 13000 FC  LIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 OR  OBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 65000 FH  INSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 5800 FC  STRINGER 1 LH AND STRINGER 1 RH OR  - AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND 39100 FH  FR.40.1  533105-01-1 N/A TASK DELETED  R 533106-01-1 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 13000 FC  FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE OR  SKIN BETWEEN STR 18 AND STR 22, FROM FRAME 38 TO 26000 FH  53.3, LH/RH. I: 8450 FC  OR  16900 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 533107-01-1 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  DUCTS 132 STRUCTURE, FR.39 TO 39.2, WEB HOLE (AREA JUST BELOW OR  LINING 137 STRINGER 28) AND FASTENERS AREA AT FRAMES JUNCTION 60000 FH  NOTE 1 138 (BELOW STRINGER 29 LEVEL), LH/RH. I: 10400 FC  OR  70600 FH  R 533107-01-2 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  DUCTS 132 STRUCTURE, FR.39 TO 39.2, WEB HOLE (AREA JUST BELOW OR  LINING 137 STRINGER 28) AND FASTENERS AREA AT FRAMES JUNCTION 26000 FH  NOTE 1 138 (BELOW STRINGER 29 LEVEL), LH/RH. I: 12700 FC  OR  25400 FH  533111-01-1 N/A TASK DELETED  R 533113-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 13000 FC  STRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 OR  TO ABOVE STR 24 LEVEL, LH/RH. 60000 FH  I: 9200 FC  OR  62300 FH  533113-01-2 N/A TASK DELETED  533113-01-3 N/A TASK DELETED  533114-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533114-01-2 N/A TASK DELETED  533115-01-1 N/A TASK DELETED  533115-01-2 N/A TASK DELETED  533115-01-3 N/A TASK DELETED  533116-01-1 N/A TASK DELETED  533117-01-1 191KB 192PB 193BB 191 DETAILED INSPECTION OF FR 40 PRESSURE BULKHEAD, AFT T: 12 YE 1  RH ONLY: AIR 192 FACE BELOW CENTER WING BOX. I: 12 YE  CONDITIONING PACK 193  533117-01-2 N/A TASK DELETED  533122-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF CENTER LANDING GEAR T: 6 YE 1+2  754 148 WELL, KEEL BEAM INTERNAL STRUCTURE AND PANELS I: 6 YE  149 BETWEEN FR 47 AND FR 53.2  533123-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 6 YE 1  148 PRESSURE DIAPHRAGMS AND PRESSURIZED FLOORS LOWER I: 6 YE  SURFACE, BETWEEN FR.47 AND FR.53.2.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533124-01-1 734 744 753 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 13000 FC  754 148 CENTER LANDING GEAR DOOR CUTOUT, "Z" STIFFENER AT I: 13000 FC  149 HINGE 3 LOCATION, LH/RH.  533125-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR T: 6 YE 1  754 148 53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENT I: 6 YE  AREA OF THE CENTER LANDING GEAR TRUNNION FITTINGS  533125-01-2 N/A TASK DELETED  R 533126-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND T: 6 YE 1  754 148 CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO I: 6 YE  149 AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.  533126-01-2 N/A TASK DELETED  533126-01-3 N/A TASK DELETED  533126-01-4 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533127-01-1 N/A TASK DELETED  533127-02-1 FAIRING PANELS 191 GENERAL VISUAL INSPECTION OF AREA AROUND AIR T: 6 YE 1  BETWEEN FR 39.1 AND 192 CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM I: 6 YE  FR 47 193 (6.0 IN) EXTERNAL SURFACE  195  196  533127-02-2 N/A TASK DELETED  533127-03-1 N/A TASK DELETED  533127-03-2 N/A TASK DELETED  533129-01-1 734 744 753 143 DETAILED INSPECTION OF KEEL BEAM INTERNAL AND T: 12 YE 1  754 149 EXTERNAL STRUCTURE, SKIN AND ADJACENT FUSELAGE I: 12 YE  FAIRING PANELS 191 STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE.  BETWEEN FR 40 AND FR 192  47 193  195  196  533130-01-1 753 754 149 DETAILED INSPECTION OF FORWARD AND AFT FACE T: 12 YE 1  OF ATTACH FITTING FOR CLG DOOR ACTUATOR AND CLG I: 12 YE  DRAG STRUT FITTING INCLUDING THEIR ATTACHMENT TO  KEEL BEAM TORQUE BOX.  533130-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533130-02-2 N/A TASK DELETED  533132-02-1 753 754 149 SPECIAL DETAILED INSPECTION OF CLG TRUNNION T: 13000 FC  FITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARD OR  FLANGES RADIUS, LH/RH. 22000 FH  I: 9300 FC  OR  22000 FH  R 533132-02-2 753 754 149 SPECIAL DETAILED INSPECTION OF CLG TRUNNION T: 13000 FC  FITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARD OR  FLANGES RADIUS, LH/RH. 22000 FH  I: 9550 FC  OR  19100 FH  533133-01-1 753 754 149 DETAILED INSPECTION OF CLG LATERAL REACTION T: 12 YE 1  FITTING AT FR 53.1, RH. I: 12 YE  533134-01-1 753 754 149 DETAILED INSPECTION OF ATTACH FITTING FOR CLG T: 12 YE 1  ACTUATOR ACTUATOR AND ITS ATTACHMENT TO THE CENTER LINE I: 12 YE  DISCONNECTED STIFFENER AT FR 53.2.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533134-02-1 N/A TASK DELETED  533135-01-1 734 744 753 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 12 YE 1  754 148 FITTINGS NO.1 THROUGH NO.6, DOOR ACTUATOR FITTINGS I: 12 YE  149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH.  533135-01-2 734 744 753 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 13000 FC  754 148 FITTINGS NO.1 THROUGH NO.6, DOOR ACTUATOR FITTINGS I: 5000 FC  149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH.  533136-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING T: 13000 FC  148 NO.1 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FC  533138-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  NOTE 1 146 STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y = 1959, OR  AT FR 48 LEVEL, LH/RH. 60000 FH  I: 13000 FC  R 533139-01-1 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FC  756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG OR  ACTUATOR FITTING UPPER END. 75000 FH  I: 5550 FC  OR  37600 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533139-01-2 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FC  756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG I: 8100 FC  ACTUATOR FITTING UPPER END.  R 533139-01-3 753 754 755 147 SPECIAL DETAILED INSPECTION OF VERTICAL BEAM T: 13000 FC  756 148 AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG OR  ACTUATOR FITTING UPPER END. 26000 FH  I: 8050 FC  OR  16100 FH  533140-01-1 743 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  148 INTERNAL STRUCTURE, FR 53.2 BULKHEAD FORWARD FACE, I: 6800 FC  ANGLE SPLICE AT STR 42, LH/RH.  533140-01-2 743 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  148 INTERNAL STRUCTURE, FR 53.2 BULKHEAD FORWARD FACE, I: 6000 FC  ANGLE SPLICE AT STR 42, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533141-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR 53.2 T: 12 YE 1  ACT (IF INSTALLED) 152 AND PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE I: 12 YE  CARGO FLOOR PANELS AND CARGO COMPARTMENT FLOOR PANEL.  LD-MCR (IF  INSTALLED)  LINING  NOTE 1  533142-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 12 YE 1  LINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 12 YE  NOTE 1 INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE AND  STR 40, FROM AFT FACE OF CARGO COMPARTMENT REAR PANEL  TO FR 40.  533143-01-1 822 153 DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND T: 6 YE 1+2  ACT (IF INSTALLED) 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR I: 6 YE  CARGO FLOOR PANELS LEVEL.  LD-MCR (IF  INSTALLED)  533144-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 6 YE 1+2  LINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 6 YE  NOTE 1 INTERNAL STRUCTURE BELOW STR 40, FROM FR 39.1 TO FR  40.  NOTE : APPLY AFTER INSPECTION IN ADDITION TO TYPE 1  TYPE 2 TEMPORARY PROTECTION SYSTEM ON FWD FACE  OF FR 40 AND ON FUSELAGE STRUCTURE FROM 25 CM  AFTER FR 39.2 TO FR 40  533145-01-1 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 13000 FC  198HB 197 BUTT JOINT AT STR 31 LEVEL FROM FR 53.3 TO FR 54, I: 6000 FC  198 LH/RH.  D 533145-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533146-01-1 N/A TASK DELETED  533147-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  LINING 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM STR 15 TO I: 12 YE  NOTE 1 253 CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 254  BINS  533148-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  LINING 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM STR 15 TO I: 12 YE  NOTE 1 CABIN FLOOR LEVEL, LH/RH.  533149-01-1 N/A TASK DELETED  533150-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 6 YE 1  GALLEYS AND TOILETS 252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 6 YE  FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA.  533150-02-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 12 YE 1  252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 12 YE  FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2.  NOTE :  - TEMPORARY PROTECTION SYSTEM APPLICATION MAY BE  LIMITED TO PRESSURIZED FLOORS AND PRESSURE DIAPHRAGM.  - TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITED ABOVE THIS AREA  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533152-01-1 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FC  ACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6000 FC  FAIRING LEVEL, LH/RH.  R 533152-01-2 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FC  ACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8  LD-MCR (IF FAIRING LEVEL, LH/RH. I: 6000 FC  INSTALLED)  533152-01-3 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FC  ACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6000 FC  FAIRING LEVEL, LH/RH.  R 533152-01-4 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 13000 FC  ACT (IF INSTALLED) 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8  LD-MCR (IF FAIRING LEVEL, LH/RH. I: 6000 FC  INSTALLED)  533154-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533154-01-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  GALLEYS AND TOILETS 146 STRUCTURE, RIVET ROWS AT SHEAR PANELS AND I: 13000 FC  LONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1,  LH/RH.  R 533154-01-3 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  GALLEYS AND TOILETS 146 STRUCTURE, RIVET ROWS AT SHEAR PANELS AND OR  LONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1, 26000 FH  LH/RH. I: 13300 FC  OR  26600 FH  533157-01-1 N/A TASK DELETED  R 533162-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING T: 13000 FC  148 GEAR BAY, LOWER FLANGE OF GANTRY Y = 1456, 40 OR  FASTENERS FORWARD AND AFT OF FR 48 DATUM, LH/RH. 60000 FH  I: 9000 FC  OR  61000 FH  533163-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 533164-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FC  148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR OR  BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 60000 FH  Y = 1959, LH/RH. I: 8800 FC  OR  59600 FH  R 533164-01-2 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FC  148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR OR  BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 26000 FH  Y = 1959, LH/RH. I: 9900 FC  OR  19800 FH  R 533164-01-3 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, CANTED T: 13000 FC  148 DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR OR  BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO 65000 FH  Y = 1959, LH/RH. I: 8300 FC  OR  56300 FH  533165-01-1 N/A TASK DELETED  533166-01-1 N/A TASK DELETED  533167-01-1 N/A TASK DELETED  533168-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533169-01-1 N/A TASK DELETED  533170-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2  GALLEYS AND TOILETS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 5 YE  AND FR 53.5  NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN 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  GALLEYS AND TOILETS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 6 YE  AND FR 53.5.  NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN 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  252 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YE  TOILETS, BETWEEN FR 36 AND FR 53.5.  533179-01-1 251MG 251SG 252MG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 13000 FC  252SG 146 STRUCTURE, FR 48 TO FR 53.1, VERTICAL LEG AT OR  GALLEYS AND TOILETS STRINGER PASSAGE LH/RH. 60000 FH  NOTE 1 I: 11100 FC  533180-01-1 N/A TASK DELETED  533180-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533181-01-1 N/A TASK DELETED  533181-01-2 N/A TASK DELETED  533184-01-1 N/A TASK DELETED  533186-01-1 N/A TASK DELETED  R 533190-01-1 834 844 261 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 12 YE 1  INSULATION 262 AROUND DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YE  LINING CUT-OUT, BETWEEN FR 53.4 AND FR 53.8 FROM MAIN DECK  FLOOR LEVEL TO STR 9, LH/RH.  R 533191-01-1 151EW 151GW 152EW 151 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1  152GW 822 152 BELOW DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YE  ACT (IF INSTALLED) CUT-OUT, BETWEEN FR 53.4 AND FR 53.8 FROM MAIN DECK  FLOOR PANELS FLOOR DOWN TO CARGO FLOOR LEVEL LH/RH.  INSULATION  LDL TOILETS AND  FURNISHING (IF  INSTALLED)  LDMCR (IF INSTALLED)  533192-01-1 N/A TASK DELETED  533193-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533193-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE  200 (INCLUDING DOOR 3 CUTOUT) BETWEEN FR 53.3 AND FR 54 I: 6 YE  FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTER  LINE, EXTERNAL SURFACE, LH/RH.  533194-01-1 N/A TASK DELETED  533194-01-2 N/A TASK DELETED  533194-01-3 N/A TASK DELETED  533194-01-4 N/A TASK DELETED  533194-01-9 N/A TASK DELETED  533195-01-1 834 844 100 DETAILED INSPECTION OF DOOR 3 CUT-OUT, STRUCTURE T: 12 YE  SCUFF PLATE UNDERNEATH SCUFF PLATE, LH/RH. I: 6 YE  533195-02-1 N/A TASK DELETED  533195-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533195-02-3 N/A TASK DELETED  533195-02-4 N/A TASK DELETED  533195-02-9 N/A TASK DELETED  533716-01-1 734 744 753 149 DETAILED INSPECTION OF KEEL BEAM, CENTER LANDING GEAR T: 12 YE 1+2  754 FITTING INTERNAL STRUCTURE, LH/RH. I: 12 YE  EXTERNAL AND  INTERNAL PLUGS  533717-01-1 192GB 193FB 193JB 193 DETAILED INSPECTION OF KEEL BEAM, SPLICE TO FR41, T: 12 YE 1+2  195GB INTERNAL SURFACE, LH/RH. I: 12 YE  LEFT AIR  CONDITIONING PACK  533718-01-1 197AB 197 DETAILED INSPECTION OF KEEL BEAM, SPLICE TO FR 53.3, T: 12 YE 1+2  198 INTERNAL SURFACE, LH/RH. I: 12 YE  533719-01-1 192EB 193CB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM, INTERFACE T: 6 YE T: 12 YE 1+2  LEFT AND RIGHT AIR 192 BETWEEN UPPER SPAR, ANGLE FITTINGS AND FORWARD LOWER I: 6 YE I: 12 YE  INLET SHELL PANEL FROM FR38.1 TO FR40.3, AS FAR AS VISIBLE,  LH/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  192KB 193CB 193FB 192 FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN I: 12 YE  LEFT RAM AIR INLET 193 OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533721-01-1 197EB 198EB 197 SPECIAL DETAILED INSPECTION OF KEEL BEAM, INTERFACE T: 6 YE T: 12 YE 1+2  198 BETWEEN UPPER SPAR, ANGLE FITTINGS AND AFT LOWER I: 6 YE I: 12 YE  SHELL PANEL FROM FR53.2 TO FR53.6, AS FAR AS VISIBLE,  LH/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  198 FR 53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND I: 12 YE  SKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH  533723-01-1 192EB 192GB 192LB 191 DETAILED INSPECTION OF KEEL BEAM- T-SECTION BEAM, T: 12 YE 1+2  192QB 195GB 195LB 192 LH/RH. I: 12 YE  734 744 195  AIR CONDITIONING 196  PACKS  HEATSHIELDS  R 533728-01-1 192EB 192GB 193CB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM INTERNAL T: 6 YE T: 12 YE 1+2  193FB 193GB 193JB 192 SURFACE, NUTPLATE BETWEEN RIB 2 AND RIB 7, LH/RH. I: 6 YE I: 12 YE  ACCESS THROUGH NOTE: TPS APPLICATION ONLY FOR 100 % TASK.  ELLIPTICAL HOLES ON  DAMPING PANELS  533729-01-1 143AB 753 754 143 DETAILED INSPECTION OF KEEL BEAM, INTERNAL SURFACE T: 12 YE 1+2  OF TORQUE BOX. I: 12 YE  533730-01-1 143AB 753 754 143 DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX T: 6 YE 1+2  EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH. I: 6 YE  533730-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533731-01-1 192GB 193FB 193LB 143 DETAILED INSPECTION OF KEEL BEAM, EXTERNAL SURFACE , T: 6 YE 1+2  195GB 753 754 192 FROM FR40.3 TO FR47, INCLUDING RODS AND ATTACHMENT I: 6 YE  LEFT AIR 195 FITTINGS AT RIB 6, 10,13 AND 16, LH/RH.  CONDITIONING PACK  LEFT RAM AIR INLET  533731-01-2 N/A TASK DELETED  533732-01-1 734 744 753 147 DETAILED INSPECTION OF KEEL BEAM EXTERNAL SURFACE T: 6 YE 1+2  754 148 FROM FR 47 TO FR 53.2, INCLUDING ATTACH FITTING FOR I: 6 YE  149 MLG DOOR ACTUATOR, LH/RH.  NOTE: TPS APPLICATION ONLY ON ATTACH FITTING  FOR MLG DOOR ACTUATOR  533732-01-2 N/A TASK DELETED  R 533735-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 2.5 YE 1+2  BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1 I: 2.5 YE  FR.47 FROM Y=-2360 AND FR 47 FROM Y=-2360 TO Y=2360, COVERED BY BELLY  TO Y=2360 FAIRING, EXTERNAL SURFACE, LH/RH.  R 533735-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2  BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR 37.1 I: 6 YE  FR.47 FROM Y=-2360 AND FR 47 FROM Y=-2360 TO Y=2360, COVERED BY BELLY  TO Y=2360 FAIRING, EXTERNAL SURFACE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 533736-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 5 YE 1+2  BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 5 YE  FR.56 FROM Y=-2360 AND FR.56 FROM Y=-2360 TO Y=2360, COVERED BY BELLY  TO Y=2360. FAIRING, EXTERNAL SURFACE, LH/RH.  R 533736-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2  BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 6 YE  FR.56 FROM Y=-2360 AND FR.56 FROM Y=-2360 TO Y=2360, COVERED BY BELLY  TO Y=2360. FAIRING, EXTERNAL SURFACE, LH/RH.  N 533737-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 12 YE 1+2  BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 I: 12 YE  FR.56 EXCLUDING AND FR.56 COVERED BY BELLY FAIRING, EXTERNAL SURFACE,  PANELS FROM Y=-2360 EXCLUDING AREA FROM Y=-2360 TO Y=2360.  TO Y=2360  533801-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE  200 FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO I: 12 YE  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.  533817-01-1 192GB 192LB 191 DETAILED INSPECTION OF AFT FACE OF FR40 PRESSURE T: 12 YE 1  192 BULKHEAD BELOW CENTER WING BOX. I: 12 YE  193  195  533823-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY UPPER T: 6 YE 1  148 PRESSURE PANELS, LOWER SURFACE, BETWEEN FR 47 AND I: 6 YE  FR 53.2  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533823-01-2 N/A TASK DELETED  533825-01-1 734 744 753 147 GENERAL VISUAL INSPECTION OF FWD FACE OF FR.53.2 T: 6 YE 1  754 148 PRESSURE BULKHEAD INCLUDING FOOTFRAME, I: 6 YE  149 FLAP-TRACK BRACKETS, UPPER SUPPORT BRACKET AND  CONNECTION PLATES LATERAL PANEL.  533825-01-2 N/A TASK DELETED  533828-01-1 734 744 753 147 DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT T: 6 YE 1  754 148 FITTING ON FR 53.2 I: 6 YE  149  533828-01-2 N/A TASK DELETED  533831-01-1 734 744 753 147 DETAILED INSPECTION OF FORWARD FACE OF FR 53.2 T: 6 YE 1  754 148 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9. I: 6 YE  149  533831-01-2 N/A TASK DELETED  533834-01-1 734 744 753 149 DETAILED INSPECTION OF ATTACH FITTING FOR CLG T: 12 YE 1  754 ACTUATOR AND UPLOCK BRACKET. I: 12 YE  ACTUATOR BOLT  ACTUATOR  DISCONNECTED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533841-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR53.2 AND T: 12 YE 1  ACT (IF INSTALLED) 152 PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND I: 12 YE  LDMCR (IF INSTALLED) CARGO COMPARTMENT FLOOR LEVEL, INCLUDING BEAMS AND  LINING INTERCOSTALS.  NOTE 1  533842-01-1 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 6 YE 1+2  AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 6 YE  DUCTS INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE AND  GALLEYS AND TOILETS STGR 41, FROM FR39 TO FR40.  LINING NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS  NOTE 1 FITTED ABOVE THE AREA  REAR PANEL OF FWD  CARGO COMPARTMENT  533842-01-2 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 12 YE  AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 12 YE  DUCTS INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE AND  LINING STGR 41, FROM FR39 TO FR40.  NOTE 1 NOTE: TASK APPLICABLE IF NO GALLEYS OR TOILETS  REAR PANEL OF FWD FITTED ABOVE THE AREA  CARGO COMPARTMENT  533843-01-1 822 153 DETAILED INSPECTION OF AFT FACE OF FR53.2 AND T: 6 YE 1+2  ACT 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR I: 6 YE  CARGO COMPARTMENT LEVEL.  FLOOR PANELS  LDMCR  533844-01-1 821 137 DETAILED INSPECTION OF FWD FACE OF FR40, PRESSURE T: 6 YE 1+2  AIR CONDITIONING 138 BULKHEAD, CENTER WING BOX FRONT SPAR, AND FUSELAGE I: 6 YE  DUCTS INTERNAL STRUCTURE BELOW STGR 41, FROM FR39 TO FR40.  LINING  NOTE 1 NOTE: TPS IS REQUIRED ONLY ON FWD FACE OF FR40 AND  REAR PANEL OF FWD ON FUSELAGE INTERNAL STRUCTURE FROM 25 CM AFTER  CARGO COMPARTMENT FR39.2 TO FR40.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533847-01-1 GALLEYS AND TOILETS 253 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  LINING 254 STRUCTURE BETWEEN FR 37.11 AND FR 53.4 (FOR -500), I: 12 YE  NOTE 1 FR 56.1 (FOR -600), ABOVE STR 15, LH/RH.  OVERHEAD STOWAGE  BINS  533848-01-1 GALLEYS AND TOILETS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  LINING 252 STRUCTURE BETWEEN FR 37.11 AND FR 53.4 (FOR -500), I: 12 YE  NOTE 1 FR 56.1 (FOR -600), BETWEEN STR 15 AND CABIN FLOOR  LEVEL, LH/RH.  533849-01-1 N/A TASK DELETED  533849-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE NO  STRUCTURE, LINER INSIDE RCT FROM FR.53.2 TO FR.53.7 I: 6 YE  (RCT5) OR TO FR.53.9 (RCT9), AS FAR AS VISIBLE  533850-01-1 822 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 6 YE 1+2  CABIN FLOOR PANELS 146 BETWEEN FR47 AND FR53.2, FROM CABIN FLOOR LEVEL TO I: 6 YE  FWD PANEL OF AFT HORIZONTAL PRESSURE PANEL.  CARGO COMPARTMENT NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS  GALLEYS AND TOILETS FITTED ABOVE THE AREA  533850-01-2 822 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 12 YE  CABIN FLOOR PANELS 146 BETWEEN FR47 AND FR53.2, FROM CABIN FLOOR LEVEL TO I: 12 YE  FWD PANEL OF AFT HORIZONTAL PRESSURE PANEL.  CARGO COMPARTMENT NOTE: TASK APPLICABLE IF NO GALLEYS OR TOILETS  FITTED ABOVE THE AREA  533852-01-1 197AB 155 DETAILED INSPECTION OF REAR CENTER TANK, LOWER T: 6 YE  FUSELAGE SKIN FROM FR 53.2 TO FR 53.8 , BETWEEN STR I: 6 YE  54 LH AND STR 54 RH, MANHOLE AND PUMP HOLE FITTINGS,  AND CRASH SKID  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533853-01-1 N/A TASK DELETED  533853-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK, T: 12 YE NO  FUEL PUMPS INTERNAL STRUCTURE, LOWER AREA BELOW STR 46 FROM FR I: 12 YE  LINER 53.2 TO FR 53.7 (FOR 5 FRAME BAY LENGTH) , TO FR.53.9  PIPING (FOR 7 FRAME BAY LENGTH), AND MAN HOLE CUT-OUT, AND  ANTI CRASH RODS, AS FAR AS VISIBLE  533854-01-1 FLOOR PANELS 151 DETAILED INSPECTION OF ANGLE BETWEEN FUSELAGE AND RCT T: 6 YE 1+2  GALLEYS AND TOILETS 152 OBLIQUE PANELS, BETWEEN FR.53.2 AND FR.53.7 (FOR 5 I: 6 YE  FRAME BAY LENGTH) AND FR.53.9 (FOR 7 FRAME BAY  LENGTH), FROM THE JUNCTION TO STGR 31.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA  533854-01-2 FLOOR PANELS 151 DETAILED INSPECTION OF ANGLE BETWEEN FUSELAGE AND RCT T: 12 YE 1+2  152 OBLIQUE PANELS, BETWEEN FR.53.2 AND FR.53.7 (FOR 5 I: 12 YE  FRAME BAY LENGTH) AND FR.53.9 (FOR 7 FRAME BAY  LENGTH), FROM THE JUNCTION TO STGR 31.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITTED IN THIS AREA  533855-01-1 822 151 DETAILED INSPECTION OF REAR CENTER TANK, AFT FACE OF T: 12 YE 1  INSULATION 152 FR.53.7 (FOR 5 FRAME BAY LENGTH), FR.53.9 (FOR 7 I: 12 YE  LINING FRAME BAY LENGTH), BETWEEN CABIN FLOOR STRUCTURE AND  CARGO COMPARTMENT FLOOR LEVEL.  533856-01-1 822 153 DETAILED INSPECTION OF REAR CENTER TANK, AFT FACE OF T: 6 YE 1+2  LININGS 154 FR.53.7 (FOR 5 FRAME BAY LENGTH), OF FR.53.9 (FOR 7 I: 6 YE  NOTE 1 FRAME BAY LENGTH), BELOW CARGO COMPARTMENT FLOOR  LEVEL.  533857-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533857-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK T: 12 YE NO  INTERNAL STRUCTURE ABOVE STR 46, EXCLUDING STRUTS I: 12 YE  ONLY  533858-01-1 N/A TASK DELETED  533858-01-2 153AZ 155AZ 197CB 155 DETAILED INSPECTION OF REAR CENTER TANK, COMPOSITE T: 12 YE NO  STRUTS (20 PLACES FOR 5 FRAME BAY LENGTH AND 21 I: 12 YE  PLACES FOR 7 FRAMES BAY LENGTH)  533859-01-1 N/A TASK DELETED  533859-01-2 153AZ 155AZ 197CB 155 GENERAL VISUAL INSPECTION OF REAR CENTER TANK, 3 FWD T: 12 YE NO  METALLIC STRUTS (FOR 7 FRAME BAY LENGTH) I: 12 YE  533870-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW T: 5 YE 1+2  GALLEYS AND TOILETS 252 AND 0.75M AROUND GALLEYS AND TOILETS, BETWEEN FR.39 I: 5 YE  AND  - FR53.2 (FOR-600),  - FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYS  LENGTH),  - FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYS  LENGTH).  NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533870-01-2 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW T: 6 YE 1+2  GALLEYS AND TOILETS 252 AND 0.75M AROUND GALLEYS AND TOILETS, BETWEEN FR.39 I: 6 YE  AND  - FR53.2 (FOR-600),  - FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYS  LENGTH),  - FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYS  LENGTH)  NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN 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  TO BE REMOVED 252 EXCLUDING AREAS BELOW AND 0.75M AROUND GALLEYS AND I: 12 YE  TOILETS, BETWEEN FR.39 AND  - FR53.2 (FOR-600),  - FR53.7 (FOR-500 POST 47021, WITH RCT 5 FRAME BAYS  LENGTH),  - FR53.9 (FOR-500 POST 47968, WITH RCT 7 FRAME BAYS  LENGTH).  533881-01-1 LINING PANELS TO BE 251 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2  REMOVED 252 AROUND OVERWING EMERGENCY DOOR FROM STRINGER 12 TO I: 12 YE  NOTE 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  REMOVED 262 DOOR 3 (EMERGENCY DOOR) CUT-OUT, BETWEEN FR53.3 AND I: 12 YE  NOTE 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  FLOOR PANELS 152 BETWEEN FR.53.2 AND FR.53.7 (FOR 5 FRAME BAY LENGTH), I: 6 YE  GALLEYS AND TOILETS AND FR.53.9 (FOR 7 FRAME BAY LENGTH), FROM CABIN  FLOOR LEVEL TO STRINGER 31  NOTE: TASK APPLICABLE IF TOILETS OR GALLEYS  ARE INSTALLED IN THIS AREA  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 533891-01-2 822 151 DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN, T: 12 YE 1+2  FLOOR PANELS 152 BETWEEN FR.53.2 AND FR.53.7 (FOR 5 FRAME BAY LENGTH), I: 12 YE  AND FR.53.9 (FOR 7 FRAME BAY LENGTH), FROM CABIN  FLOOR LEVEL TO STRINGER 31  NOTE:TASK APPLICABLE IF TOILETS OR GALLEYS  ARE NOT INSTALLED IN THIS AREA  533895-01-1 SCUFF PLATE 200 DETAILED INSPECTION OF DOOR 3 (EMERGENCY DOOR) T: 12 YE  CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH. I: 6 YE  534102-01-1 N/A TASK DELETED  534102-01-2 N/A TASK DELETED  534104-01-1 N/A TASK DELETED  534104-01-2 N/A TASK DELETED  534104-01-3 N/A TASK DELETED  534104-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534105-01-1 N/A TASK DELETED  534105-01-2 N/A TASK DELETED  534107-01-1 N/A TASK DELETED  534107-01-3 N/A TASK DELETED  534108-01-1 N/A TASK DELETED  534110-01-1 N/A TASK DELETED  534120-01-1 N/A TASK DELETED  534122-01-1 N/A TASK DELETED  534124-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 534124-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 12 YE  FR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH EXCLUDING I: 12 YE  AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL  SURFACE.  534125-01-1 N/A TASK DELETED  534126-01-1 N/A TASK DELETED  534126-02-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE  SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH I: 6 YE  TO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND  LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA  OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF  FR 54  534127-01-1 822 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.2 AND FR 73 BELOW CARGO I: 6 YE  CARGO COMPARTMENT 163 COMPARTMENT FLOOR PANELS.  FLOOR PANELS 164  INSULATION NOTE: IF LDL INSTALLED, INSPECTION AREA BETWEEN FR  LDMCR (IF INSTALLED) 54A AND FR 73.  R 534128-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  NOTE 1 172 STRUCTURE BETWEEN FR 73 AND FR 80 BELOW MAIN DECK I: 6 YE  FLOOR INCLUDING MAIN DECK FLOOR STRUCTURE  534130-01-1 N/A 100 GENERAL VISUAL INSPECTION OF T: 6 YE  200 FUSELAGE SKIN AT DOOR 4 (AFT PASSENGER/CREW DOOR) I: 6 YE  CUT-OUT BETWEEN FR 73 AND FR 76, FROM STR 9 TO STR 26  LH/RH, EXTERNAL SURFACE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534130-01-2 N/A TASK DELETED  534131-01-1 N/A TASK DELETED  534132-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT T: 12 YE  SCUFF PLATE 200 PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YE  UNDERNEATH SCUFF PLATE, LH/RH.  534132-02-1 N/A TASK DELETED  R 534133-01-1 833 843 271 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 12 YE 1  DOOR FRAME LININGS 272 AROUND DOOR 4 (AFT PASSENGER/CREW DOOR) BETWEEN FR I: 12 YE  INSULATION 72 AND FR 77 FROM MAIN DECK FLOOR LEVEL TO  LINING STR 9 LH/RH.  R 534134-01-1 162ZW 823 171 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1  NOTE 1 172 BELOW DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, I: 6 YE  BETWEEN FR 73 AND FR 76 FROM MAIN DECK FLOOR LEVEL  TO STR 30 LH/RH.  534135-01-1 N/A TASK DELETED  534136-01-1 N/A TASK DELETED  534137-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534137-01-3 N/A TASK DELETED  534138-01-1 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT T: 12 YE 1  INSULATION 154 CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND I: 12 YE  LINING FR 66, FROM STR 26 RH TO CARGO FLOOR LEVEL.  534139-01-1 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1  154 DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES I: 6 YE  (FR 59A AND FR 65) AS FAR AS VISIBLE  534139-01-2 N/A TASK DELETED  534140-01-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR T: 6 YE T: 20 YE  ECCENTRIC BOLTS AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN I: 6 YE I: 6 YE  FR 59A AND FR 65  R 534140-02-1 822 152 GENERAL VISUAL INSPECTION OF T: 6 YE 1+2  LOCK FITTINGS AND BUSHES FOR AFT I: 6 YE  CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN  FR 59A AND FR 65  534140-02-2 N/A TASK DELETED  534141-01-1 N/A TASK DELETED  534143-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534143-01-3 N/A TASK DELETED  534144-01-1 823 100 DETAILED INSPECTION OF BULK CARGO T: 12 YE  SCUFF PLATE COMPARTMENT DOOR CUT-OUT STRUCTURE I: 6 YE  UNDERNEATH SCUFF PLATE.  534144-02-1 N/A TASK DELETED  534144-02-2 N/A TASK DELETED  534145-01-1 823 162 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1  FLOOR PANELS AROUND BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  LINING FR 66 AND FR 70 FROM STR 31 TO STR 48, RH.  NOTE 1  534146-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1+2  DOOR STOP FITTINGS AT 10 POSITIONS AT FR 67 AND FR 69 I: 6 YE  534146-01-2 N/A TASK DELETED  534148-01-1 N/A TASK DELETED  534149-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1  DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 67 I: 6 YE  AND FR 69) AS FAR AS VISIBLE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534149-01-2 N/A TASK DELETED  534150-01-1 N/A TASK DELETED  534154-01-1 N/A TASK DELETED  534155-01-1 N/A TASK DELETED  534156-01-1 N/A TASK DELETED  534156-01-2 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE T: 6 YE 1+2  CARGO COMPARTMENT 154 BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT I: 6 YE  FLOOR PANELS BETWEEN FR 59 AND FR 67, FROM CARGO FLOOR LEVEL  INSULATION TO STR 47 RH  LINING  R 534157-01-1 833 843 261 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE  FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS, I: 12 YE  271 AND DOOR ENTRANCE AREAS FROM FR 53.5 TO FR 80.  272  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 534158-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1  ACT (IF INSTALLED) 152 STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND I: 12 YE  CARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 53.2 TO FR 73,  CEILING PANELS 162 INCLUDING MAIN DECK FLOOR STRUCTURE  LDL TOILETS AND 171  FURNISHING (IF 172  INSTALLED)  LDMCR (IF INSTALLED)  LINING  NOTE 1  R 534159-01-1 833 843 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2  FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS INCLUDING I: 5 YE  TOILETS AND GALLEYS 271 DOOR ENTRANCE AREAS FROM FR 53.5 TO FR 80.  272  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED  R 534159-01-2 833 843 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 1+2  FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS INCLUDING I: 6 YE  TOILETS AND GALLEYS 271 DOOR ENTRANCE AREAS, FROM FR 53.5 TO FR 80.  272  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  534160-01-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CEILING PANELS 264 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM STR 15 TO I: 12 YE  NOTE 1 273 CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 274  BINS  R 534161-01-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 262 STRUCTURE BETWEEN FR 53.5 AND FR 80 FROM STR 15 I: 12 YE  SIDEWALL LINING 271 (OVERHEAD STOWAGE BINS LOWER SURFACE)  272 TO MAIN DECK FLOOR, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 534162-01-1 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2  ACT (IF INSTALLED) 152 STRUCTURE FROM MAIN DECK FLOOR TO CARGO I: 6 YE  CARGO COMPARTMENT 161 COMPARTMENT FLOOR, BELOW AND 0.5M FWD AND AFT OF  CEILING PANELS 162 UPPER DECK GALLEYS AND TOILETS, FROM FR 53.5 TO  LAVATORY/GALLEY 171 FR 80, LH/RH  EXTRACTION DUCT (FR 172 NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE  78-79) FITTED ABOVE THE AREA  LDL TOILETS AND  FURNISHING (IF  INSTALLED)  LDMCR (IF INSTALLED)  LINING  LOWER DECK CARGO  COMPARTMENT  VENTILATION DUCT (FR  70-71)  NOTE 1  534163-01-1 833 843 151 DETAILED INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  FLOOR PANELS 152 STRUCTURE IN LDL AREA FROM FR 53,2 TO FR 54A AND I: 6 YE  INSULATION 153 FROM STR 37 TO BOTTOM CENTER LINE, LH/RH,  LDL CEILING 154 INCLUDING LDL UPPER AND LOWER ATTACHMENT POINTS.  LINING NOTE: TASK ONLY APPLICABLE IF LDL INSTALLED  TOILETS FURNISHING  534166-01-1 N/A TASK DELETED  534166-02-1 N/A TASK DELETED  N 534177-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE  FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER I: 3 YE  LINE, EXCLUDING AREA UNDER VERTICAL STABILIZER  FAIRING, EXTERNAL SURFACE.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 534224-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE  SURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TO STR 26, I: 12 YE  LH/RH, EXCLUDING AREA COVERED BY VERTICAL STABILIZER  FAIRING.  534226-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE  EXTERNAL SURFACE BETWEEN FR 54 AND FR 80 I: 6 YE  FROM STR 26 LH/RH TO BOTTOM CENTER LINE,  EXCLUDING AREA UNDERNEATH BELLY FAIRING.  534226-01-2 N/A TASK DELETED  534227-01-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.2 AND FR 73 BELOW I: 6 YE  CARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.  FLOOR PANELS 164  LDF FURNISHING AND  EQUIPMENT (IF  INSTALLED)  LDMCR (IF INSTALLED)  534227-02-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.7 AND FR 73 BELOW I: 6 YE  CARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.  FLOOR PANELS 164  LDF FURNISHING AND  EQUIPMENT (IF  INSTALLED)  LDMCR (IF INSTALLED)  534227-03-1 822 823 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  ACT (IF INSTALLED) 154 STRUCTURE BETWEEN FR 53.9 AND FR 73 BELOW I: 6 YE  CARGO COMPARTMENT 163 CARGO COMPARTMENT FLOOR PANELS.  FLOOR PANELS 164  LDF FURNISHING AND  EQUIPMENT (IF  INSTALLED)  LDMCR (IF INSTALLED)  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534228-01-1 161AZ 822 171 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  IF LDF (PARTIAL OR 172 STRUCTURE BETWEEN FR 73 AND FR 80 BELOW I: 6 YE  FULL BULK) PASSENGER CABIN FLOOR.  INSTALLED: 161 MQ NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3  NOTE 1 FOR THE COMPLETE AREA AND ADDITIONAL TPS TYPE II  BELOW STR 40, LH/RH.  534230-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN T: 6 YE  EXTERNAL SURFACE AROUND DOOR 4 (AFT PASSENGER/ I: 6 YE  CREW DOOR) CUT-OUT BETWEEN FR 73 AND FR 76,  FROM STR 9 TO STR 26 LH/RH.  534232-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT T: 12 YE  SCUFF PLATE 200 PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH I: 6 YE  SCUFF PLATE LH/RH.  534233-01-1 833 843 271 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  INSULATION 272 AROUND DOOR 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT I: 6 YE  LINING 273 BETWEEN FR 73 AND FR 76 FROM PASSENGER CABIN FLOOR  274 TO STR 9, LH/RH  534234-01-1 161AZ 823 171 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1  IF LDF (PARTIAL OR 172 BELOW DOOR 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT I: 6 YE  FULL BULK) BETWEEN FR 73 AND FR 76 FROM PASSENGER CABIN FLOOR  INSTALLED: 161 MQ TO STR 43, LH/RH  INSULATION  534238-01-1 822 152 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  INSULATION AROUND AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  LINING FR 59 AND FR 66, FROM STR 26 TO CARGO COMPARTMENT  FLOOR, RH.  534239-01-1 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1  DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES I: 6 YE  (FR 59A AND FR 65).  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534239-01-2 N/A TASK DELETED  534240-01-1 822 152 GENERAL VISUAL INSPECTION OF LOCK FITTINGS AND BUSHES T: 6 YE 1+2  154 FOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS I: 6 YE  BETWEEN FR 59A AND FR 65  534240-01-2 N/A TASK DELETED  534240-02-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO T: 6 YE T: 20 YE  ECCENTRIC BOLTS 154 COMPARTMENT DOOR AT 10 POSITIONS BETWEEN I: 6 YE I: 6 YE  FR 59A AND FR 65  534244-01-1 823 100 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR T: 12 YE  SCUFF PLATE CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. I: 6 YE  534245-01-1 823 162 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1  CARGO COMPARTMENT 164 AROUND BULK CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  FLOOR PANELS FR 66 AND FR 70 FROM STR 31 TO STR 48, RH.  IF LDF (FULL BULK) NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3 FOR  INSTALLED: LDF THE COMPLETE AREA AND ADDITIONAL TPS TYPE II BELOW  FURNISHING AND STR 40.  EQUIPMENT  INSULATION  LINING  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534246-01-1 823 162 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS OF T: 6 YE 1+2  BULK CARGO COMPARTMENT DOOR, AT 10 POSITIONS I: 6 YE  AT FR 67 AND FR 69.  534246-01-2 N/A TASK DELETED  534249-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO T: 6 YE 1  COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL I: 6 YE  FRAMES (FR 67 AND FR 69).  534249-01-2 N/A TASK DELETED  534256-01-1 822 154 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  BALLMATS BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  FR 59 AND FR 66, FROM CARGO COMPARTMENT FLOOR TO  STR 47, RH.  534257-01-1 833 843 261 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE  FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILTETS I: 12 YE  271 AND DOOR ENTRANCE AREAS FROM FR 53.7 TO FR 80.  272  534257-02-1 833 843 261 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE  FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YE  271 AND DOOR ENTRANCE AREAS FROM FR 53.9 TO FR 80.  272  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534257-03-1 833 843 251 GENERAL VISUAL INSPECTION OF PASSENGER CABIN FLOOR T: 12 YE  FLOOR PANELS 252 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YE  261 AND DOOR ENTRANCE AREAS FROM FR 53.2 TO FR 80.  262  271  272  534258-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YE  CARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 53.7 TO FR 73.  LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFT  LDF FURNISHING AND 171 OF FR 68, LH/RH.  EQUIPMENT (IF 172  INSTALLED)  LDMCR (IF INSTALLED)  NOTE 1  534258-02-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YE  CARGO COMPARTMENT 161 CARGO COMPARTMENT FLOOR FROM FR 63.9 TO FR 73.  LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFT  LDF FURNISHING AND 171 OF FR 68, LH/RH.  EQUIPMENT (IF 172  INSTALLED)  LDMCR (IF INSTALLED)  NOTE 1  534258-03-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE SIDE SHELL T: 12 YE 1  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 12 YE  CARGO COMPARTMENT 161 COMPARTMENT FLOOR FROM FR 53.2 TO FR 73.  LINING 162 NOTE: APPLICATION OF TPS TYPE I, GRADE 2 OR 3, AFT  LDF FURNISHING AND 171 OF FR 68, LH/RH.  EQUIPMENT (IF 172  INSTALLED)  LDMCR (IF INSTALLED)  NOTE 1  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534259-01-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.2  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 251 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 252 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED  INSTALLED: LDF 261  FURNISHINGAND 262  EQUIPMENT 271  272  534259-01-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDINM DOOR ENTRANCE AREAS, FROM FR 53.2  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 251 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 252 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  INSTALLED: LDF 261  FURNISHINGAND 262  EQUIPMENT 271  272  534259-02-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.7  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED  INSTALLED: LDF 271  FURNISHINGAND 272  EQUIPMENT  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534259-02-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTANCE AREAS, FROM FR 53.7  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  INSTALLED: LDF 271  FURNISHINGAND 272  EQUIPMENT  534259-03-1 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 5 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 5 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDING DOOR ENTRANCE AREAS, FROM FR 53.9  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED  INSTALLED: LDF 271  FURNISHINGAND 272  EQUIPMENT  534259-03-2 161AZ 822 823 151 DETAILED INSPECTION OF PASSENGER CABIN FLOOR T: 6 YE 1+2  833 843 152 STRUCTURE BELOW AND 0.75 M AROUND GALLEYS AND I: 6 YE  CARGO COMPARTMENT 161 TOILETS, INCLUDING DOORENTRANCE AREAS, FROM FR 53.9  CEILING PANELS 162 TO FR 80.  FLOOR PANELS 171  GALLEYS AND TOILETS 172 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  IF LDF (PARTIAL, 261 FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATED  FULL BULK OR AFT) 262 IN NOTE 7 IN MRBR SECTION D ARE INCORPORATED  INSTALLED: LDF 271  FURNISHINGAND 272  EQUIPMENT  534260-01-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CEILING PANELS 264 STRUCTURE BETWEEN FR 53.4 AND FR 80, FROM STR 15 TO I: 12 YE  NOTE 1 273 CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 274  BINS  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534260-02-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  CEILING PANELS 264 STRUCTURE BETWEEN FR 56.1 AND FR 80, FROM STR 15 TO I: 12 YE  NOTE 1 273 CROWN CENTER LINE, LH/RH.  OVERHEAD STOWAGE 274  BINS  534261-01-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 262 STRUCTURE BETWEEN FR 53.4 AND FR 80, FROM STR 15 I: 12 YE  SIDEWALL LINING 271 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO PASSENGER  272 CABIN FLOOR, LH/RH.  R 534261-02-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 262 INTERNAL STRUCTURE BETWEEN FR 56.1 AND FR 80, FROM I: 12 YE  SIDEWALL LINING 271 STR 15 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO  272 PASSENGER CABIN FLOOR, LH/RH.  534262-01-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YE  IF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWD  FULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FR  INSTALLED: LDF 171 53.2 TO FR 80, LH/RH  FURNISHINGAND 172  EQUIPMENT NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE  INSULATION FITTED ABOVE THE AREA  LDMCR (IF INSTALLED)  LINING  534262-02-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YE  IF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWD  FULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FR  INSTALLED: LDF 171 53.7 TO  FURNISHINGAND 172 FR 80, LH/RH (WITH RCT, 5 FRAME BAYS)  EQUIPMENT  INSULATION NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE  LDMCR (IF INSTALLED) FITTED ABOVE THE AREA  LINING  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 534262-03-1 161AZ 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL T: 6 YE 1+2  ACT (IF INSTALLED) 152 INTERNAL STRUCTURE BETWEEN PASSENGER CABIN FLOOR AND I: 6 YE  IF LDF (PARTIAL, 161 CARGO COMPARTMENT FLOOR/STR 43, BELOW AND 0.75M FWD  FULL BULK OR AFT) 162 AND AFT OF MAIN DECK GALLEYS AND TOILETS, FROM FR  INSTALLED: LDF 171 53.9 TO  FURNISHINGAND 172 FR 80, LH/RH (WITH RCT, 7 FRAME BAYS)  EQUIPMENT  INSULATION NOTE: TASK APPLICABLE IF GALLEYS AND TOILETS ARE  LDMCR (IF INSTALLED) FITTED ABOVE THE AREA  LINING  534267-01-1 833 843 261 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  INSULATION 262 AROUND DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YE  LINING CUT-OUT, BETWEEN FR 56 AND FR 56.4 FROM PASSENGER  CABIN FLOOR TO STR 9, LH/RH.  534268-01-1 822 151 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1  ACT (IF INSTALLED) 152 BELOW DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) I: 6 YE  CARGO COMPARTMENT CUT-OUT, BETWEEN FR 56 AND FR 56.4 FROM PASSENGER  INSULATION CABIN FLOOR CARGO COMPARTMENT FLOOR, LH/RH.  LDF FURNISHING AND  EQUIPMENT (IF  INSTALLED)  LDMCR (IF INSTALLED)  LINING  534270-01-1 N/A 200 GENERAL VISUAL INSPECTION OF T: 6 YE  FUSELAGE SKIN EXTERNAL SURFACE AROUND DOOR 3 I: 6 YE  (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT  BETWEEN 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  SCUFF PLATE 200 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, I: 6 YE  STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.  N 534277-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 3 YE  FR 54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER I: 3 YE  LINE, EXCLUDING AREA UNDER VERTICAL STABILIZER  FAIRING, EXTERNAL SURFACE.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 535101-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE T: 20 YE  INSULATION 272 FACE ABOVE MAIN DECK FLOOR LEVEL INCLUDING FR 80/82, I: 12 YE I: 12 YE  TOILETS AND GALLEYS RIM ANGLE AND ATTACHMENT TO SKIN.  R 535102-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE T: 6 YE 1+2  172 BULKHEAD FWD FACE BELOW MAIN DECK FLOOR LEVEL I: 6 YE  INCLUDING FR 80/82, RIM ANGLE ATTACHMENT AND  ATTACHMENT TO SKIN  R 535103-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE T: 20 YE  312 FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 I: 12 YE I: 12 YE  LH/RH AND CROWN CENTERLINE.  535103-01-2 N/A TASK DELETED  535103-02-1 N/A TASK DELETED  R 535104-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE T: 6 YE 1+2  312 BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN I: 6 YE  BETWEEN STR 26 LH/RH, AND BOTTOM CENTER LINE  535104-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 535105-01-1 N/A TASK DELETED  535106-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1  CEILING PANELS 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YE  NOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN  TOILETS 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  312 AND AFT ATTACH FITTINGS IN AREA OF ATTACHMENTS TO I: 6 YE  FUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RH  TO CROWN CENTER LINE AND AT FR 84, 85, 86 AND 87.  535108-01-1 N/A TASK DELETED  535109-01-1 N/A TASK DELETED  535110-01-1 312AR 311 DETAILED INSPECTION OF ATTACH FITTINGS FOR T: 12 YE T: 20 YE  312 HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 86 I: 12 YE I: 12 YE  AND FR 87.  R 535111-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE  CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YE  FROM FR 84 TO FR 85 AND BETWEEN STR 27 RH AND  STR 39 RH, EXTERNAL SURFACE.  535111-02-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE  CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YE  FROM FR 84 TO FR 85 AND BETWEEN STR 27 RH AND  STR 39 RH, EXTERNAL SURFACE.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 535112-01-1 N/A TASK DELETED  535113-01-1 N/A TASK DELETED  535114-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM T: 12 YE  FR 80/82 TO FR 101 FROM CROWN TO BOTTOM CENTER LINE, I: 12 YE  EXTERNAL SURFACE, AS FAR AS VISIBLE, LH/RH.  535115-01-1 N/A TASK DELETED  535116-01-1 321AL 323AL 323AR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 1  323BL 323BR 323 SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN I: 6 YE  TO FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD  FITTINGS  535117-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF REAR FUSELAGE INTERNAL T: 6 YE 1  312 STRUCTURE BETWEEN FR 80/82 AND FR 95 FROM CROWN TO I: 6 YE  313 BOTTOM CENTER LINE, LH/RH  314 NOTE: APPLY AFTER INSPECTION TYPE 1 GRADE 2 OR 3  TEMPORARY PROTECTION SYSTEM FROM FR 80/82  TO FR 91 BELOW STR 25 LH/RH, FROM FR 92 TO FR 95  BELOW STR 13 LH/RH AND IN AREA BETWEEN FR 86 AND  FR 88 BELOW STR 15  535118-01-1 312AR 313AL 311 DETAILED INSPECTION OF REAR FUSELAGE INTERNAL T: 12 YE T: 20 YE  312 STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT BETWEEN I: 6 YE I: 6 YE  FR 86 AND FR 91 FROM STR 15 TO STR 30 AND FR 91  ASSEMBLY FROM CROWN TO BOTTOM CENTER LINE INCLUDING  TAIL CONE ATTACHMENT FITTINGS, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 535121-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YE  GALLEYS AND TOILETS 272 FWD FACE ABOVE MAIN DECK FLOOR LEVEL. I: 12 YE  (IF INSTALLED) 273  NOTE 1 274  R 535122-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YE  IF LDF (PARTIAL OR 172 FWD FACE BELOW MAIN DECK FLOOR LEVEL I: 6 YE  FULL BULK)  INSTALLED: 833 843  161AZ  R 535123-01-1 312AR 311 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YE  312 AFT FACE FROM CROWN TO BOTTOM CENTER LINE. I: 12 YE  R 535124-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2  312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 6 YE  BOTTOM CENTER LINE  R 535129-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE  GALLEYS AND TOILETS 272 FACE ATTACHMENT TO RIM ANGLE, ABOVE MAIN DECK FLOOR I: 12 YE  (IF INSTALLED) 273 LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.  NOTE 1 274  R 535130-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2  IF LDF (PARTIAL OR 172 FACE ATTACHMENT TO RIM ANGLE, BELOW MAIN DECK FLOOR I: 6 YE  FULL BULK) LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN  INSTALLED: 833 843  161AZ  R 535131-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE  312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 12 YE  CROWN CENTER LINE  R 535201-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE T: 12 YE  NOTE 1 272 BULKHEAD FWD FACE ABOVE CABIN FLOOR LEVEL I: 12 YE  TOILETS AND GALLEYS  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 535202-01-1 161AZ 822 171 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YE  IF LDF (PARTIAL OR 172 FWD FACE BELOW CABIN FLOOR LEVEL I: 6 YE  FULL BULK)  INSTALLED: 833 843  161AZ  R 535203-01-1 312AR 311 GENERAL VISUAL INSPECTION OF REAR PRESSURE T: 12 YE  312 BULKHEAD AFT FACE FROM CROWN TO BOTTOM CENTER LINE I: 12 YE  535204-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2  312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 6 YE  BOTTOM CENTER LINE.  535206-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1  CEILING PANELS 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YE  NOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN  TOILETS 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  312 AND AFT ATTACH FITTINGS IN AREA OF ATTACHMENTS TO I: 6 YE  FUSELAGE SKIN, INTERNAL STRUCTURE FROM STR 6 LH/RH  TO 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  312 HORIZONTAL STABILIZER TRIM ACTUATOR BETWEEN FR 85 I: 12 YE I: 12 YE  AND FR 86.  535211-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE  CUT-OUT FOR TAIL COMPARTMENT ACCESS DOOR I: 6 YE  BETWEEN FR 84 AND FR 85 AND BETWEEN STR 27 RH AND  37 RH, EXTERNAL SURFACE.  535214-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM FR 80 T: 12 YE  TO FR 100 FROM CROWN TO BOTTOM CENTER LINE, EXTERNAL I: 12 YE  SURFACE, AS FAR AS VISIBLE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 535216-01-1 321AL 323DL 323DR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 1  323EL 323ER 325LL 323 SURFACE UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN I: 6 YE  325LR TO FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD  FITTINGS  535217-01-1 312AR 313BL 311 GENERAL VISUAL INSPECTION OF T: 6 YE 1+2  312 REAR FUSELAGE INTERNAL STRUCTURE BETWEEN FR 80 I: 6 YE  313 AND FR 95 FROM CROWN TO BOTTOM CENTER LINE, LH/RH  314 NOTE: TPS TYPE I + TYPE II APPLICATION IS FROM FR 80  TO FR 91 BELOW STRINGER 25 LH / RH, FROM FR 91  TO FR 95 BELOW STRINGER 11 LH / RH, AND TPS TYPE I,  GRADE 2 OR 3 APPLICATION IN AREA BETWEEN FR 86  AND 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  312 STRUCTURE AROUND HORIZONTAL STABILIZER CUTOUT LH/RH I: 6 YE I: 6 YE  BETWEEN FR 86 AND FR 91 FROM STR 15 TO STR 30, AND  AND FR 91 ASSEMBLY FROM CROWN TO BOTTOM CENTER LINE  INCLUDING TAIL CONE ATTACHMENT FITTINGS.  R 535219-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE  NOTE 1 272 FACE ATTACHMENT TO RIM ANGLE, ABOVE CABIN FLOOR I: 12 YE  TOILETS AND GALLEYS 273 LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.  274  R 535220-01-1 161AZ 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2  IF LDF (PARTIAL OR 172 FACE ATTACHMENT TO RIM ANGLE, BELOW CABIN FLOOR I: 6 YE  FULL BULK) LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKIN.  INSTALLED: 833 843  161AZ  R 535221-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE  312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 12 YE  CROWN CENTER LINE.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 535222-01-1 311BL 311CL 311DL 311 DETAILED INSPECTION OF REAR FUSELAGE SKIN EXTERNAL T: 10 YE 1+2  311EL 311FL 312BR 312 SURFACE UNDERNEATH THS-FAIRING, INCLUDING FAIRING I: 10 YE  312CR 312DR 312ER BRACKETS.  312FR 331AT 333AB  333AT 341AT 343AB  343AT  535223-01-1 312AR 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 10 YE  312 SUPPORT MEMBERS. I: 10 YE  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545101-01-1 N/A TASK DELETED  545102-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE T: 12 YE NO  463 ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT I: 12 YE  473 MOUNT FITTING.  483  545103-01-1 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON T: 13000 FC  463 PYRAMID, END OF ARMS AT ENGINE FORWARD MOUNT OR  473 FITTING. 60000 FH  483 I: 13000 FC  OR  60000 FH  545103-01-3 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON T: 13000 FC  463 PYRAMID, END OF ARMS AT ENGINE FORWARD MOUNT OR  473 FITTING. 26000 FH  483 I: 13000 FC  OR  26000 FH  545103-01-4 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID,END OF T: 13000 FC  REMOVAL 463 ARMS AT ENGINE FORWARD MOUNT FITTING OR  473 65000 FH  483 I: 13000 FC  OR  65000 FH  545104-01-1 N/A TASK DELETED  545104-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545104-01-6 N/A TASK DELETED  R 545104-01-7 415AL 416AR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 13000 FC  418AR 425AL 426AR 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN OR  427AL 428AR 435AL 473 RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 60000 FH  436AR 437AL 438AR 483 I: 4100 FC  445AL 446AR 447AL OR  448AR 27600 FH  R 545104-01-8 415AL 416AR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 13000 FC  418AR 425AL 426AR 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN OR  427AL 428AR 435AL 473 RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 65000 FH  436AR 437AL 438AR 483 I: 4100 FC  445AL 446AR 447AL OR  448AR 27600 FH  545108-01-1 N/A TASK DELETED  545110-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT T: 12 YE NO  418AR 425AL 426AR 463 ATTACHMENT BEAM AT RIB 3. I: 12 YE  427AL 428AR 435AL 473  436AR 437AL 438AR 483  445AL 446AR 447AL  448AR  545112-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  473AR 473BL 473BR 483 TIME AS TASK 545112-02-1  483AL 483AR 483BL  483BR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545112-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  473AR 473BL 473BR 483 TIME AS TASK 545112-01-1  483AL 483AR 483BL  483BR  545116-01-1 453CL 453CR 463CL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO  463CR 473CL 473CR 463 UPPER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YE  483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  483 TIME AS TASK 545116-02-1  545116-02-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO  463CR 473CL 473CR 463 UPPER SURFACE, BETWEEN RIB 8 AND RIB 11. I: 12 YE I: 12 YE  483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  483 TIME AS TASK 545116-01-1  545118-01-1 414 415AL 416AR 453 DETAILED INSPECTION OF PYLON LOWER SPAR T: 12 YE T: 20 YE NO  417AL 418AR 424 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 14. I: 12 YE I: 12 YE  425AL 426AR 427AL 473  428AR 434 435AL 483  436AR 437AL 438AR  444 445AL 446AR  447AL 448AR 454CL  464CL 474CL 484CL  545121-01-1 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE NO  452DR 452EL 462AL 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YE  462AR 462CL 462CR 473  462DL 462FR 472AL 483  472AR 472CL 472CR  472ER 472FL 482AL  482AR 482CR 482DL  482ER  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545121-01-2 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  452DR 452GL 462AL 463 SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YE  462AR 462CL 462CR 473  462GL 462HR 472AL 483  472AR 472CL 472CR  472HL 472JR 482AL  482AR 482CR 482GL  482HR  545121-01-3 452FL 452JL 452JR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  452KL 452KR 462AL 463 SURFACE, BETWEEN RIB 1 AND RIB 09. I: 12 YE  462AR 462CL 462CR 473  462DL 462FR 472AL 483  472AR 472CL 472CR  472ER 472FL 482JL  482JR 482KR 482ML  482MR  545124-01-1 452DR 452EL 452FR 453 DETAILED INSPECTION OF PYLON UPPER SPAR T: 12 YE NO  454AL 454AR 462DL 463 UPPER SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YE  462FR 462GR 462HL 473  464AL 464AR 472ER 483  472FL 472GL 472HR  474AL 474AR 482DL  482ER 482FL 484AL  484AR  545124-01-2 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO  454AL 454AR 462GL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YE  462GR 462HL 462HR 473  464AL 464AR 472GL 483  472HL 472HR 472JR  474AL 474AR 482FL  482GL 482HR 484AL  484AR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545124-01-3 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO  454AL 454AR 462DL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YE  462FR 462GR 462HL 473  464AL 464MR 472ER 483  472FL 472GL 472HR  474AL 474AR 482FL  482GL 482HR 484AL  484AR  545124-01-4 452KL 452KR 452MR 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO  454AL 454KR 462DL 463 SURFACE, BETWEEN RIB 09 AND RIB 11A. I: 12 YE  462FR 462GR 462HL 473  464AL 464AR 472ER 483  472FL 472GL 472HR  474AL 474MR 482ML  482MR 482NL 484ML  484MR  545126-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  464BR 474BL 474BR 463 UPPER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YE  484BL 484BR 473  483  545126-01-2 454BL 454BR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  464KR 474KL 474KR 463 SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YE  484BL 484BR 473  483  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545126-01-3 454BL 454MR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  464KR 474KL 474KR 463 SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YE  484NL 484NR 473  483  545130-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  473AR 473BL 473BR 483 TIME AS TASK 545130-02-1  483AL 483AR 483BL  483BR  545130-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  473AR 473BL 473BR 483 TIME AS TASK 545130-01-1  483AL 483AR 483BL  483BR  545131-01-1 453CL 453CR 463CL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  463CR 473CL 473CR 463 LOWER SURFACE, BETWEEN RIB 11 AND RIB 14. I: 12 YE I: 12 YE  483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  483 TIME AS TASK 545131-02-1  545131-02-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  463CR 473CL 473CR 463 LOWER SURFACE, BETWEEN RIB 8 AND RIB 11. I: 12 YE I: 12 YE  483CL 483CR 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME  483 TIME AS TASK 545131-01-1  545139-01-1 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 60000 FH  I: 5110 FC  OR  35400 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545139-01-2 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 60000 FH  I: 4130 FC  OR  28600 FH  545139-01-4 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 26000 FH  I: 6000 FC  OR  12000 FH  545139-01-5 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 65000 FH  I: 4190 FC  OR  28300 FH  545139-01-6 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 65000 FH  I: 2330 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO OR  TASK 545139-02-1 15700 FH  545139-02-1 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF ACCESS OR  DOORS (6 ACCESS DOORS PER PYLON). 65000 FH  I: 13000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO OR  TASK 545139-01-6 65000 FH  545142-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545142-01-2 N/A TASK DELETED  545143-01-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF T: 13000 FC  453BR 463AL 463AR 463 ACCESS DOOR CUTOUTS AND MATING SURFACES, RIB 3 AND OR  463BL 463BR 473AL 473 RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B PYLON) AND 60000 FH  473AR 473BL 473BR 483 BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 6000 FC  483AL 483AR 483BL OR  483BR 41600 FH  545143-01-2 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  453BR 463AL 463AR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACES, OR  463BL 463BR 473AL 473 RIB 3 AND RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B 26000 FH  473AR 473BL 473BR 483 PYLON) AND BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 6000 FC  483AL 483AR 483BL OR  483BR 12000 FH  545143-01-3 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 13000 FC  453BR 463AL 463AR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACES, OR  463BL 463BR 473AL 473 RIB 3 AND RIB 4 AND BETWEEN RIB 5 AND RIB 6 (O/B 65000 FH  473AR 473BL 473BR 483 PYLON) AND BETWEEN RIB 6 AND RIB 7 (I/B PYLON). I: 13000 FC  483AL 483AR 483BL OR  483BR 65000 FH  D 545146-01-1 N/A TASK DELETED  D 545146-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545146-01-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON LOWER SPAR AND T: 13000 FC  418AR 425AL 426AR 463 LATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4. OR  427AL 428AR 435AL 473 65000 FH  436AR 437AL 438AR 483 I: 10300 FC  445AL 446AR 447AL OR  448AR 453AL 453AR 65000 FH  463AL 463AR 473AL  473AR 483AL 483AR  545150-01-1 452CL 452DR 452EL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452FR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462DL 462FR 462GR 473 60000 FH  462HL 472CL 472CR 483 I: 2470 FC  472ER 472FL 472GL OR  472HR 482CR 482DL 16900 FH  482ER 482FL  545150-01-2 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462GL 462HL 462HR 473 60000 FH  462JR 472CL 472CR 483 I: 2180 FC  472GL 472HL 472HR OR  472JR 482CR 482FL 14900 FH  482GL 482HR  545150-01-3 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462GL 462HL 462HR 473 26000 FH  462JR 472CL 472CR 483 I: 3250 FC  472GL 472HL 472HR OR  472JR 482CR 482FL 6500 FH  482GL 482HR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545150-01-4 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462GL 462HL 462HR 473 65000 FH  462JR 472CL 472CR 483 I: 3180 FC  472GL 472HL 472HR OR  472JR 482CR 482FL 21500 FH  482GL 482HR  545150-01-5 452CL 452DR 452FR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452GL 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462GL 462GR 462HL 473 60000 FH  462HR 472CL 472CR 483 I: 2470 FC  472GL 472HL 472HR OR  472JR 482CR 482FL 16900 FH  482GL 482HR  545150-01-6 452JL 452KL 452KR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR FLANGE AT T: 13000 FC  452MR 462CL 462CR 463 JUNCTIONS WITH LATERAL PANELS FROM RIB 4 TO RIB 11. OR  462GL 462HL 462HR 473 60000 FH  462JR 472CL 472CR 483 I: 2470 FC  472GL 472HL 472HR OR  472JR 482CR 482FL 16900 FH  482GL 482HR  545166-01-1 N/A TASK DELETED  545166-01-2 N/A TASK DELETED  545168-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545168-01-2 N/A TASK DELETED  545170-01-1 452DR 452EL 452FR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  462DL 462FR 462GR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YE  472ER 472FL 472GL 473 PER PYLON).  482DL 482ER 482FL 483  BOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUT  ENGINE REMOVAL AS FAR AS VISIBLE  LINKS  SLEEVES  545170-01-2 452DR 452FR 452GL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  462GL 462GR 462HR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YE  472GL 472HL 472JR 473 PER PYLON).  482FL 482GL 482HR 483  BOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUT  ENGINE REMOVAL AS FAR AS VISIBLE  LINKS  SLEEVES  545170-01-3 452KL 452KR 452MR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  462DL 462FR 462GR 463 FITTING SLEEVES, LINK AND BOLTS AT RIB 8 (4 PLACES I: 12 YE  472ER 472FL 472GL 473 PER PYLON).  482ML 482MR 482NL 483  BOLTS NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUT  ENGINE REMOVAL AS FAR AS VISIBLE  LINKS  SLEEVES  D 545174-01-1 N/A TASK DELETED  D 545174-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545174-01-3 454BL 454MR 464KL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 13000 FC  464KR 474KL 474KR 463 FITTING LUG AND LINKS AT RIB 14. OR  484NL 484NR 473 65000 FH  483 I: 13000 FC  OR  65000 FH  D 545174-01-4 N/A TASK DELETED  D 545174-01-5 N/A TASK DELETED  545180-01-1 454FL 454FR 464FL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE  464FR 474FL 474FR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YE  484FL 484FR 473 PYLON).  BOLTS 483  ENGINE  LINKS  SLEEVES  545180-01-2 454FL 454FR 464JL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE  464JR 474JL 474JR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YE  484FL 484FR 473 PYLON).  BOLTS 483  ENGINE  LINKS  SLEEVES  545180-01-3 454NR 454QL 464JL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE  464JR 474JL 474JR 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YE  484PL 484PR 473 PYLON).  ENGINE 483  LINKS  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545180-02-1 N/A TASK DELETED  545180-02-2 454NR 454QL 464JL 453 SPECIAL DETAILED INSPECTION OF PYLON TO WING T: 13000 FC  464JR 474JL 474JR 463 ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 OR  484PL 484PR 473 PLACES PER PYLON). 26000 FH  BOLTS 483 I: 13000 FC  ENGINE OR  LINKS 26000 FH  SLEEVES  545182-01-1 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FC  453CR 463BL 463BR 463 8 WEB CUT-OUT. OR  463CL 463CR 473BL 473 60000 FH  473BR 473CL 473CR 483 I: 6000 FC  483BL 483BR 483CL OR  483CR 42200 FH  545182-01-2 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FC  453CR 463BL 463BR 463 8 WEB CUT-OUT. OR  463CL 463CR 473BL 473 65000 FH  473BR 473CL 473CR 483 I: 6000 FC  483BL 483BR 483CL OR  483CR 12000 FH  545182-01-3 453BL 453BR 453CL 453 DETAILED INSPECTION OF PYLON INTERNAL STRUCTURE, RIB T: 13000 FC  453CR 463BL 463BR 463 8 WEB CUT-OUT. OR  463CL 463CR 473BL 473 65000 FH  473BR 473CL 473CR 483 I: 13000 FC  483BL 483BR 483CL OR  483CR 65000 FH  545701-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545705-01-1 N/A TASK DELETED  545721-01-1 N/A TASK DELETED  545721-01-2 N/A TASK DELETED  545725-01-1 N/A TASK DELETED  545725-01-2 N/A TASK DELETED  545801-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO  463 THE ENGINE FORWARD MOUNT FITTING. I: 12 YE  473  483  545801-02-1 N/A TASK DELETED  545802-01-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO  463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING. I: 12 YE  473  483  545802-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545808-01-1 N/A TASK DELETED  545810-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT T: 12 YE NO  418AR 425AL 426AR 463 ATTACHMENT BEAM AT RIB 6. I: 12 YE  427AL 428AR 435AL 473  436AR 437AL 438AR 483  445AL 446AR 447AL  448AR  545810-01-2 N/A TASK DELETED  545812-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 UPPER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473  473AR 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 AS  TASK 545812-03-1.  545812-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473  473AR 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 TIME  ENGINE AS TASK 545812-03-1.  THRUST REVERSER  DEPLOYED  545812-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  473AR 473BL 473BR 483 TASKS 545812-01-1 OR 545812-02-1.  483AL 483AR 483BL  483BR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545816-01-1 453CL 453CR 453DL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR UPPER T: 12 YE T: 20 YE NO  453DR 463CL 463CR 463 SURFACE, BETWEEN RIB 8 AND RIB 14. I: 12 YE I: 12 YE  463DL 463DR 473CL 473  473CR 473DL 473DR 483  483CL 483CR 483DL  483DR  545818-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON LOWER SPAR LOWER T: 12 YE T: 20 YE NO  416AR 417AL 418AR 463 SURFACE, BETWEEN RIB 1 AND RIB 14. I: 12 YE I: 12 YE  424AL 424AR 425AL 473  426AR 427AL 428AR 483  434AL 434AR 435AL  436AR 437AL 438AR  444AL 444AR 445AL  446AR 447AL 448AR  452FR 452HL 462FR  462HL 472FR 472HL  482FR 482HL  545821-01-1 452AL 452AR 452CL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  452DR 462AL 462AR 463 SURFACE, BETWEEN RIB 1 AND RIB 6. I: 12 YE I: 12 YE  462CL 462CR 462DL 473  472AR 472BL 472CL 483  472CR 472DL 482AR  482BL 482CR 482DL  545824-01-1 452CR 452EL 452GR 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  452KL 454AL 454AR 463 SURFACE, BETWEEN RIB 6 AND RIB 9. I: 12 YE I: 12 YE  462CR 462DL 462EL 473  462GR 462JL 464AL 483  464AR 472ER 472FL  472GL 472HR 474AL  474AR 482CR 482EL  482GR 482JL 484AL  484AR  545826-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  464BR 474BL 474BR 463 SURFACE, BETWEEN RIB 9 AND RIB 14. I: 12 YE I: 12 YE  484BL 484BR 473  483  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545830-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON, UPPER SPAR T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 LOWER SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473  473AR 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 TIME  AS 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  453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 1 AND RIB 3. I: 12 YE I: 12 YE  463BL 463BR 473AL 473  473AR 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 TIME  ENGINE AS TASK 545830-03-1.  THRUST REVERSER  DEPLOYED  545830-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR LOWER T: 12 YE T: 20 YE NO  453BR 463AL 463AR 463 SURFACE, BETWEEN RIB 3 AND RIB 8. I: 12 YE I: 12 YE  463BL 463BR 473AL 473 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  473AR 473BL 473BR 483 TASKS 545830-01-1 OR 545830-02-1.  483AL 483AR 483BL  483BR  545831-01-1 453CL 453CR 453DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR LOWER T: 12 YE T: 20 YE NO  453DR 463CL 463CR 463 SURFACE, BETWEEN RIB 8 AND RIB 14. I: 12 YE I: 12 YE  463DL 463DR 473CL 473  473CR 473DL 473DR 483  483CL 483CR 483DL  483DR  545833-01-1 453AL 453AR 453BL 453 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 12 YE T: 20 YE NO  453BR 453CL 453CR 463 INTERNAL SURFACE, FROM RIB 1 TO RIB 3. I: 12 YE I: 12 YE  463AL 463AR 463BL 473  463BR 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 TIME  483AL 483AR 483BL AS TASK 545833-03-1.  483BR 483CL 483CR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545833-02-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, INTERNAL T: 12 YE T: 20 YE NO  453BR 453CL 453CR 463 SURFACE, FROM RIB 1 TO RIB 3. I: 12 YE I: 12 YE  463AL 463AR 463BL 473  463BR 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 TIME  483AL 483AR 483BL AS TASK 545833-03-1.  483BR 483CL 483CR  ENGINE  THRUST REVERSER  DEPLOYED  545833-03-1 453AL 453AR 453BL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, INTERNAL T: 12 YE T: 20 YE NO  453BR 453CL 453CR 463 SURFACE, FROM RIB 3 TO RIB 14. I: 12 YE I: 12 YE  463AL 463AR 463BL 473  463BR 463CL 463CR 483 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME  473AL 473AR 473BL AS TASK 545833-01-1 OR 545833-02-1.  473BR 473CL 473CR  483AL 483AR 483BL  483BR 483CL 483CR  545835-01-1 452DR 452EL 452FR 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, EXTERNAL T: 12 YE T: 20 YE NO  452GR 452KL 454AL SURFACE AS FAR AS VISIBLE AND EXTERNAL UPPER AREAS I: 12 YE I: 12 YE  454AR 462DR 462FR COVERED BY FAIRINGS.  464AL 464AR 464BL  472DR 472FR 482CR  482DR 482EL 482FR  482GR 482JL 484AL  484AR  545837-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON LATERAL PANELS, EXTERNAL T: 12 YE T: 20 YE NO  416AR 424AL 424AR 463 LOWER AREAS COVERED BY REVERSER COWLS AND NOZZLE. I: 12 YE I: 12 YE  425AL 426AR 434AL 473  434AR 435AL 436AR 483  444AL 444AR 445AL  446AR  545842-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 545858-01-1 N/A TASK DELETED  545860-01-1 N/A TASK DELETED  545870-01-1 452CR 452EL 452GR 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  462CR 462EL 462GR 463 FITTING SLEEVES, LINKS AND BOLTS AT RIB 8 (4 PLACES I: 12 YE  462JL 472CR 472EL 473 PER PYLON).  472GR 472JL 482CR 483  482EL 482GR NOTE: INSPECT THE O/B LINKS OF THE O/B PYLONS WITHOUT  BOLTS REMOVAL AS FAR AS VISIBLE  ENGINE  LINKS  SLEEVES  545880-01-1 454AL 454AR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  454BR 464AR 464BL 463 FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER I: 12 YE  464BR 464CL 474AL 473 PYLON).  474BL 474BR 474CR 483  484AL 484AR 484BL  484BR  BOLTS  ENGINE  LINKS  SLEEVES  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551001-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE  312 ASSEMBLY OF TRIM ACTUATING ARMS, SUPPORT FITTINGS AND I: 12 YE I: 12 YE  UPPER AND LOWER ATTACHMENT PLATES.  551002-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 TRIM ACTUATING ARM LUGS AND SUPPORT FITTING I: 15000 FC  LUGS.  551004-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE  312 ASSEMBLY OF HINGE FITTING AT RIB 3, UPPER AND LOWER I: 12 YE I: 12 YE  ATTACH FITTINGS, LH/RH.  551007-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 12 YE  SPAR AND BETWEEN FUSELAGE FAIRING LINES  551008-01-1 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN I: 8600 FC  FUSELAGE FAIRING LINES. OR  44500 FH  551008-01-2 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN I: 12300 FC  FUSELAGE FAIRING LINES. OR  24600 FH  551009-01-1 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  REARMOST UPPER 343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM I: 5300 FC  FAIRING SUPPORT FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE OR  FITTING FAIRING LINE, LH/RH. 27200 FH  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551009-01-2 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  REARMOST UPPER 343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE FROM I: 9800 FC  FAIRING SUPPORT FRONT TO REAR SPAR AND BETWEEN RIB 3 AND FUSELAGE OR  FITTING FAIRING LINE, LH/RH. 19600 FH  551010-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 CENTER BOX BOTTOM SKIN LOWER SURFACE FROM FRONT TO I: 12 YE  REAR SPAR AND BETWEEN FUSELAGE FAIRING LINES  551011-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 12 YE T: 20 YE  312 SPAR AFT FACE JOINT PLATE INBOARD OF RIB 3, LH/RH OR I: 12 YE  15000 FC  I: 12 YE  OR  15000 FC  551011-02-1 N/A TASK DELETED  551012-01-1 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE  312 CENTER BOX REAR SPAR AFT FACE BETWEEN RIB 3 LH AND I: 15000 FC I: 12 YE  RIB 3 RH, EXCLUDING INBOARD JOINT PLATES  551013-01-1 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE 1  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12 YE  334 LH/RH.  344  551013-01-2 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 10000 FC  334 LH/RH. OR  344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 51800 FH  TIME AS TASK 551013-02-1  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551013-01-3 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12900 FC  334 LH/RH. OR  344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 25800 FH  TIME AS TASK 551013-02-2  551013-02-1 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 10000 FC  334 LH/RH. OR  344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 51800 FH  TIME AS TASK 551013-01-2  551013-02-2 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 12900 FC  334 LH/RH. OR  344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME 25800 FH  TIME AS TASK 551013-01-3  551015-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE  312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 15000 FC I: 12 YE  RIB 3 RH  551016-01-1 N/A TASK DELETED  551016-01-3 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  312 CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD I: 15000 FC  OF RIB 3, LH/RH  551018-01-1 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  319BL 319BR 319CR CENTER BOX INTERNAL STRUCTURE I: 12 YE  DISCONNECT SCAVENGE  WATER SYSTEM PIPE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 551018-01-2 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  319BL 319DR 319ER CENTER BOX INTERNAL STRUCTURE I: 12 YE  551019-01-1 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  312 STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 5800 FC  ATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH OR  TO RIB 3 RH. 29700 FH  551019-01-2 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  312 STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 7500 FC  ATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH OR  TO RIB 3 RH. 15000 FH  551020-01-1 N/A 300 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES I: 15000 FC  OUTBOARD OF FUSELAGE FAIRINGS  551020-02-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE I: 6 YE  SPLICES OUTBOARD OF FUSELAGE FAIRINGS  551021-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  CENTER BOX BOTTOM SKIN LOWER SURFACE CHORDWISE I: 6 YE  SPLICES OUTBOARD OF FUSELAGE FAIRINGS  551022-01-1 331AT 331BT 333AB 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL T: 12 YE NO  333AL 333AT 341AT 343 BOX INTERNAL STRUCTURE BETWEEN RIB 3 AND RIB 4 I: 12 YE  341BT 343AB 343AR  343AT  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551024-01-1 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 12 YE  333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 15000 FC I: 12 YE  343AB 343AT RIB 4  551025-01-1 331AT 331BT 331CT 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  331DT 331ET 332AB 332 LATERAL BOX FRONT SPAR FORWARD FACE FROM RIB 4 I: 12 YE  332AT 333AB 333AT 341 TO END RIB AND EXTERNAL SURFACE OF END RIB  341AT 341BT 341CT 342  341DT 341ET 342AB  342AT 343AB 343AT  551026-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  LATERAL BOX TOP SKIN UPPER SURFACE FROM I: 6 YE  CHORDWISE SPLICE TO END RIB  551027-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 3 YE  LATERAL BOX BOTTOM SKIN LOWER SURFACE FROM I: 3 YE  CHORDWISE SPLICE LINE TO END RIB  551028-01-1 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 3000 FC  FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF OR  FUSELAGE FAIRINGS 16000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-1  551028-01-2 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 4100 FC  FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF OR  FUSELAGE FAIRINGS 22200 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-2  551028-01-3 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICE, I: 5100 FC  FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF OR  FUSELAGE FAIRINGS 10200 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-3  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551028-02-1 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 8000 FC  CHORDWISE SPLICE, FIVE( 5) REARMOST ROWS OF OR  FASTENERS OUTBOARD OF FUSELAGE FAIRINGS 43700 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-1  551028-02-2 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 12400 FC  CHORDWISE SPLICE, FIVE (5) REARMOST ROWS OF OR  FASTENERS OUTBOARD OF FUSELAGE FAIRINGS 67400 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-2  551028-02-3 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  343 STABILIZER CENTER BOX TOP SKIN UPPER SURFACE I: 15000 FC  CHORDWISE SPLICE, FIVE (5) REARMOST ROWS OF OR  FASTENERS OUTBOARD OF FUSELAGE FAIRINGS 30000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-3  551029-01-1 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  319BL 319BR 319CR CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT I: 15000 FC  DISCONNECT SCAVENGE TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3 RH  WATER SYSTEM PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME  AS TASK 551029-02-1  R 551029-01-2 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC  319BL 319DR 319ER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT I: 15000 FC  TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3 RH.  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME  AS TASK 551029-02-2  551029-02-1 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  319BL 319BR 319CR STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 15000 FC  DISCONNECT SCAVENGE ATTACHMENT TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3  WATER SYSTEM PIPE RH.  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME  AS TASK 551029-01-1  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 551029-02-2 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL T: 15000 FC  319BL 319DR 319ER STABILIZER CENTER BOX TOP SKIN INTEGRAL FLANGE AT I: 15000 FC  ATTACHMENT TO FRONT SPAR WEB FROM RIB 3 LH TO RIB 3  RH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 551029-01-2  551030-01-1 334AB 334BB 334CB 334 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  334DB 334EB 334FB 344 LATERAL BOX REAR SPAR AFT FACE FROM RIB 3 I: 6 YE  334GB 344AB 344BB OUTBOARD JOINT PLATE TO END RIB  344CB 344DB 344EB  344FB 344GB  551031-01-1 334BB 334CB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 6 YE 1  335BB 344BB 344CB 344 HINGE FITTINGS NO.2 AND 3 AND SUPPORT RIBS. I: 15000 FC I: 6 YE  344DB 345BB  551031-02-1 N/A TASK DELETED  551032-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 15000 FC T: 6 YE 1  344CT 344 ACTUATOR ATTACHMENT FITTING AND REACTION BAR AT I: 15000 FC I: 6 YE  RIBS 8 AND 9, LH AND RH.  551032-02-1 N/A TASK DELETED  551033-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 15000 FC T: 12 YE 1  334EB 334FB 334GB 344 FITTINGS NO.1, 4, 5, 6 AND 7 AND SUPPORT RIBS I: 15000 FC I: 12 YE  335AB 335CB 335DB  335EB 335FB 344AB  344BB 344DB 344EB  344FB 344GB 345AB  345CB 345DB 345EB  345FB  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551033-02-1 N/A TASK DELETED  R 551035-01-1 332AB 332AT 333BB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333CB 333DB 333EB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YE  333FB 333GB 343BB RIB, LH / RH  343CB 343DB 343EB  343FB 343GB 344GB  346AB  PEELABLE HOLE COVERS  R 551035-01-2 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND I: 12 YE  343DB 343EB 343FB RIB 13 LH / END RIB RH.  343GB 344GB 346AB  PEELABLE HOLE COVERS  R 551035-01-3 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333EB 333FB 333GB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YE  334AZ 334GB 343BB RIB, LH / RH  343CB 343DB 343EB  343FB 343GB 344GB  346AB  PEELABLE HOLE COVERS  N 551035-01-4 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND I: 12 YE  343DB 343EB 343FB RIB 13 LH / END RIB RH.  343GB 344GB 346AB  PEELABLE HOLE COVERS  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 551035-02-1 331ET 332AB 332AT 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333EL 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 13 AND END I: 12 YE  PEELABLE HOLE COVERS RIB LH  551053-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE  312 SCREW JACK FITTING. I: 12 YE I: 12 YE  551054-01-1 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE  312 REAR SPAR, AFT FACE, CENTRAL JOINING PLATE, I: 12 YE I: 12 YE  EXTERNAL SURFACE.  551055-01-1 313BL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE 1  312 REAR SUPPORT FITTING AT RIB 3, INCLUDING UPPER AND I: 12 YE I: 12 YE  LOWER ATTACH FITTINGS, LH/RH.  551056-01-1 331AT 331BT 331CT 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  331DT 331ET 331FT 332 FRONT SPAR, FORWARD FACE, FROM RIB 3 TO END RIB I: 12 YE  332AB 332AT 341AT 341 (RIB 21) AND EXTERNAL SURFACE OF END RIB, LH/RH.  341BT 341CT 341DT 342  341ET 341FT 342AB  342AT  551057-01-1 331CT 331DT 341CT 331 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE  341DT 341 FRONT SPAR, FORWARD FACE, JOINING PARTS AT RIB 10, I: 12 YE I: 12 YE  EXTERNAL SURFACE, LH/RH.  551058-01-1 334AB 334BB 334CB 334 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  334DB 334EB 334FB 344 REAR SPAR, AFT FACE, FROM RIB 3 TO END RIB (RIB 21), I: 12 YE  344AB 344BB 344CB LH/RH.  344DB 344EB 344FB  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551059-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 6 YE 1  344CT 344 ACTUATOR FITTING NO 1 AND 2, LH/RH. I: 6 YE  551060-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE 1  334EB 334FB 344AB 344 ELEVATOR HINGE FITTINGS NO 1 TO 8 AND SUPPORT RIB, I: 12 YE  344BB 344DB 344EB LH/RH.  344FB  551061-01-1 312AR 313BL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 UPPER AND LOWER SKIN, INBOARD OF FUSELAGE FAIRINGS I: 12 YE  (INSIDE FUSELAGE), EXTERNAL SURFACE.  551062-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 FRONT SPAR, FORWARD FACE, FROM RIB 3 LH TO RIB 3 RH. I: 12 YE  551063-01-1 313BL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 REAR SPAR, AFTER FACE, FROM RIB 3LH TO RIB 3RH. I: 12 YE  551064-01-1 311CZ 311DZ 312AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  312CZ 312DZ 313BL INTERNAL STRUCTURE, BETWEEN RIB 3LH AND RIB 3 RH. I: 12 YE  551065-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  TOP SKIN, UPPER SURFACE, OUTBOARD OF FUSELAGE I: 6 YE  FAIRINGS, LH/RH.  551066-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  BOTTOM SKIN, LOWER SURFACE, OUTBOARD OF FUSELAGE I: 6 YE  FAIRINGS, LH/RH.  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 551067-01-1 331AT 331AZ 333BB 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  333CB 333DB 333EB 343 INTERNAL STRUCTURE, BETWEEN RIB 3LH AND RIB 15LH, I: 12 YE  333FB 333GB 333HB 346 AND BETWEEN RIB 3RH AND RIB 16RH.  333JB 333KB 333LB  333MB 341AT 341AZ  343BB 343CB 343DB  343EB 343FB 343GB  343HB 343JB 343KB  343LB 346AB  551068-01-1 331ET 331FT 332AB 337 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  332AT 334EB 334FB 347 INTERNAL STRUCTURE, BETWEEN RIB 15 LH AND I: 12 YE  334FT 341FT 342AB END RIB (RIB 21LH), AND BETWEEN RIB 16 RH AND END RIB  342AT 344EB 344FB (RIB 21RH).  344FT  PEELABLE HOLE COVERS  551069-01-1 331AT 331AZ 333BB 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  333CB 333DB 333EB 343 INTERNAL STRUCTURE, BETWEEN RIB 3 AND RIB 20 LH / RH I: 12 YE  333FB 333GB 333HB 346  333JB 333KB 333LB  333MB 333NB 333PB  333QB 333RB 333SB  333TB 341AT 341AZ  343BB 343CB 343DB  343EB 343FB 343GB  343HB 343JB 343KB  343LB 343MB 343NB  343PB 346AB 346BB  346CB  551070-01-1 332AB 332AT 334FB 337 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  334FT 342AB 342AT 347 INTERNAL STRUCTURE, BETWEEN RIB 20 LH / RH AND END I: 12 YE  344FB 344FT RIB (RIB 21 LH / RH)  PEELABLE HOLE COVERS  R 552001-01-1 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR TOP T: 3 YE  AND BOTTOM SKIN PANELS INCLUDING TRAILING EDGE, I: 3 YE  EXTERNAL SURFACE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 552002-01-1 334BB 334CB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE T: 15000 FC T: 6 YE 1  335BB 344BB 344CB 345 FITTINGS NO.2 AND 3 AND ACTUATOR FITTINGS, LH AND I: 15000 FC I: 6 YE  344DB 345BB RH  552002-02-1 N/A TASK DELETED  552003-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR SPAR FORWARD T: 12 YE  334DB 334EB 334FB 345 FACE. I: 12 YE  334GB 335AB 335BB  335CB 335DB 335EB  335FB 344AB 344BB  344CB 344DB 344EB  344FB 344GB 345AB  345BB 345CB 345DB  345EB 345FB  552004-01-1 N/A 300 SPECIAL DETAILED INSPECTION OF ELEVATOR TOP AND T: 6 YE  BOTTOM SKIN PANELS IN AREA OF HINGE FITTINGS NO.2 I: 6 YE  AND 3 AND AREA OF ACTUATOR FITTINGS, EXTERNAL  SURFACE.  552005-01-1 334AB 334BB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE T: 15000 FC T: 12 YE 1  334EB 334FB 334GB 345 FITTINGS NO.1, 4, 5, 6 AND 7 I: 15000 FC I: 12 YE  335AB 335CB 335DB  335EB 335FB 344AB  344BB 344DB 344EB  344FB 344GB 345AB  345CB 345DB 345EB  345FB  552005-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 552051-01-1 334AB 334BB 334CB 335 GENERAL VISUAL INSPECTION OF ELEVATOR, FRONT SPAR T: 12 YE  334DB 334EB 334FB 345 FORWARD FACE. I: 12 YE  335AB 335BB 335CB  335DB 335EB 335FB  335GB 335HB 335JB  344AB 344BB 344CB  344DB 344EB 344FB  345AB 345BB 345CB  345DB 345EB 345FB  345GB 345HB 345JB  552052-01-1 334CB 334CT 335CB 335 DETAILED INSPECTION OF ELEVATOR, ACTUATOR FITTINGS T: 6 YE 1  335DB 335EB 344CB 345 NO 1 AND 2. I: 6 YE  344CT 345CB 345DB  345EB  552053-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR, HINGE FITTINGS T: 12 YE 1  334DB 334EB 334FB 345 NO 1 TO 8. I: 12 YE  335AB 335BB 335CB  335DB 335EB 335FB  335GB 335HB 335JB  344AB 344BB 344CB  344DB 344EB 344FB  345AB 345BB 345CB  345DB 345EB 345FB  345GB 345HB 345JB  552054-01-1 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR, TOP T: 6 YE  AND BOTTOM SKIN, EXTERNAL SURFACE. I: 6 YE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 552055-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR, INTERNAL STRUCTURE T: 12 YE  334DB 334EB 334FB 345 AS FAR AS VISIBLE. I: 12 YE  335AB 335BB 335CB  335DB 335EB 335FB  335GB 335HB 335JB  344AB 344BB 344CB  344DB 344EB 344FB  345AB 345BB 345CB  345DB 345EB 345FB  345GB 345HB 345JB  PEELABLE HOLE COVERS  553004-01-1 N/A TASK DELETED  553005-01-1 N/A TASK DELETED  553008-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  SKIN PANELS FROM FRONT TO REAR SPAR AND I: 6 YE  FROM FIN/FUSELAGE FAIRING TO TOP, EXTERNAL  SURFACE LH/RH.  553009-01-1 325AL 325BL 325CL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  325DL 325EL 325FL REAR SPAR AFT FACE INCLUDING SUPPORT FITTINGS I: 6 YE  325GL 325HL 325JL FOR RUDDER HINGE ARMS  325KL  553010-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  324AT 324BT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YE  FACE.  553011-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 6 YE  RIB 1 AND RIB 8, INCLUDING LOWER SURFACE OF RIB 1  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 553012-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, T: 6 YE  FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD I: 6 YE  FITTINGS.  553013-01-1 322BL 322CL 324AT 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  325DL 325EL 325FL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 8 AND I: 12 YE  325GL 325HL 325JL RIB 18.  325KL  PEELABLE HOLE COVERS  553014-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE 1  RIB 1 AND RIB 5, METALLIC REINFORCEMENTS AT I: 6 YE  THE MANHOLES.  553015-01-1 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1  325HL 325KL 326BL SUPPORT FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YE  326DL 326DR 326FL  326HL 326KL  553015-01-2 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1  325HL 325KL 326DL SUPPORT FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YE  326DR  553070-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  SKIN PANELS FROM FRONT TO REAR SPAR AND I: 6 YE  FROM FIN/FUSELAGE FAIRING TO TOP, EXTERNAL  SURFACE LH/RH.  553071-01-1 325LL 325NL 325SL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  325TL 325UL 325VL REAR SPAR AFT FACE. I: 6 YE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 553072-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  322EL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING I: 12 YE  RIB UPPER FACE.  553073-01-1 311AZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 6 YE  RIB 1 AND RIB 5 INCLUDING LOWER SURFACE OF RIB 1.  R 553074-01-1 311AZ 312AR 323DL 323 DETAILED INSPECTION OF VERTICAL STABILIZER, T: 6 YE  323EL 325LL FWD, CENTER AND AFT MAIN FITTINGS AND SIDELOAD I: 6 YE  FITTINGS.  553075-01-1 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  324CT 325NL 325SL 324 STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN I: 12 YE  325TL 325UL 325VL RIB 5 AND RIB 13A.  PEELABLE HOLE COVERS  553076-01-1 325LL 325NL 325SL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND T: 6 YE 1  325TL 325UL 325VL ACTUATOR SUPPORT FITTINGS. I: 6 YE  326ML 326NL 326PL  326RL 326SL  R 554001-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YE  EXTERNAL SURFACE LH/RH I: 6 YE  R 554003-01-1 324BT 325AL 325BL 326 SPECIAL DETAILED INSPECTION OF RUDDER FRONT SPAR T: 6 YE  325CL 325DL 325EL I: 6 YE  325FL 325GL 325HL  325JL 325KL 326AL  326BL 326CL 326DL  326EL 326FL 326GL  326HL 326JL 326KL  326LL  PEELABLE HOLE COVERS  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 554003-01-2 324BT 325AL 325BL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YE  325CL 325DL 325EL I: 6 YE  325FL 325GL 325HL  325JL 325KL 326DL  PEELABLE HOLE COVERS  D 554005-01-1 N/A TASK DELETED  D 554005-02-1 N/A TASK DELETED  554006-01-1 N/A TASK DELETED  554007-01-1 N/A TASK DELETED  554007-01-2 N/A TASK DELETED  554008-01-1 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1  325HL 325KL 326BL I: 6 YE  326BR 326DL 326DR  326FL 326FR 326HL  326HR 326KL 326KR  554008-01-2 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1  325HL 325KL 326DL I: 6 YE  326DR  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 554009-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  BOOSTER AREA, LH/RH. I: 6 YE  N 554010-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 3 YE  AREA OF FRONT SPAR AND RIB 0. I: 3 YE  N 554010-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  AREA OF FRONT SPAR AND RIB 0. I: 6 YE  N 554011-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  AREA OF HOISTING POINTS AND TRAILING EDGE SCREW LINE, I: 6 YE  LH/RH.  N 554012-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  ATTACH FITTING AREA, LH/RH. I: 6 YE  N 554012-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  ATTACH FITTING AREA, LH/RH. I: 6 YE  N 554013-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YE  INTERNAL STRUCTURE, LH/RH. I: 6 YE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 554014-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0. T: 6 YE  I: 6 YE  R 554070-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YE  EXTERNAL SURFACE LH/RH. I: 6 YE  R 554071-01-1 325LL 325LR 325NL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YE  325NR 325SL 325SR I: 6 YE  325TL 325TR 325UL  325UR 325VL 325VR  326AT 326ML 326NL  326PL 326RL 326SL  PEELABLE HOLE COVERS  D 554072-01-1 N/A TASK DELETED  R 554073-01-1 325LL 325NL 325SL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1  325TL 325UL 325VL I: 6 YE  326ML 326NL 326PL  326RL 326SL  N 554074-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  BOOSTER AREA, LH/RH. I: 6 YE  N 554075-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  AREA OF FRONT SPAR AND RIB 0. I: 6 YE  N 554076-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  AREA OF HOISTING POINTS AND TRAILING EDGE SCREW I: 6 YE  LINE, LH/RH.  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 554077-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  ATTACH FITTING AREA, LH/RH. I: 6 YE  N 554078-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YE  INTERNAL STRUCTURE, LH/RH. I: 6 YE  N 554079-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0. T: 6 YE  I: 6 YE  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 562101-01-1 830 840 221 DETAILED INSPECTION OF MAIN DECK WINDOW PANES T: 6 YE  222 INCLUDING PASSENGER/CREW DOOR AND EMERGENCY EXIT I: 6 YE  231 WINDOW PANES.  232  241  242  251  252  261  262  271  272  562102-01-1 830 840 221 DETAILED INSPECTION OF PASSENGER CABIN T: 6 YE  222 WINDOW PANES INCLUDING PASSENGER/CREW DOOR AND I: 6 YE  231 EMERGENCY EXIT WINDOW PANES.  232  241  242  251  252  261  262  271  272  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINDOWS SECTION: D-56 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571102-01-1 N/A TASK DELETED  571102-01-2 N/A TASK DELETED  571102-01-3 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 13000 FC  AIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER OR  DUCTS 38 LEVEL, LH/RH. 65000 FH  LINING I: 5530 FC  NOTE 1 OR  37300 FH  571103-01-1 N/A TASK DELETED  D 571103-01-2 N/A TASK DELETED  571103-02-1 N/A TASK DELETED  D 571103-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571105-01-1 734 744 143 DETAILED INSPECTION OF CENTER WING BOX, T: 12 YE 1  AIR CONDITIONING 191 LOWER SKIN LOWER SURFACE FROM FR.40 TO FR.47 I: 12 YE  PACKS 192 BETWEEN RIB 1 LH AND RIB 1 RH  FAIRING PANELS 193  BETWEEN FR 40 AND FR 195  47 196  HEATSHIELDS  571106-01-1 191HB 191QB 192HB 191 GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER T: 12 YE 1  192QB 192 SPLICE AT RIB 1 BETWEEN FR 40 AND FR 47 I: 12 YE  195  196  571107-01-1 N/A TASK DELETED  571107-01-2 N/A TASK DELETED  R 571107-01-3 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  196 BOX LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN OR  STRINGERS 20 AND 21, LH/RH 26000 FH  I: 4900 FC  OR  9850 FH  571108-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571108-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  60000 FH  I: 7300 FC  OR  51000 FH  R 571108-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  60000 FH  I: 5900 FC  OR  40000 FH  R 571108-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  26000 FH  I: 6700 FC  OR  13400 FH  571108-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 13000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  65000 FH  I: 6500 FC  OR  43900 FH  571114-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571114-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  744 142 BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS OR  27 AND 28 60000 FH  I: 12600 FC  OR  60000 FH  571114-01-3 N/A TASK DELETED  D 571114-01-4 N/A TASK DELETED  571114-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  744 142 BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS OR  27 AND 28 65000 FH  I: 6500 FC  OR  43900 FH  571116-01-1 N/A TASK DELETED  571116-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 571116-01-3 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  BOX LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA OR  BETWEEN STRINGERS 21 AND 22, AT Y =-567.5 26000 FH  I: 4900 FC  OR  9850 FH  571118-01-1 N/A TASK DELETED  571118-01-2 N/A TASK DELETED  571118-01-3 N/A TASK DELETED  571118-01-4 N/A TASK DELETED  R 571118-01-5 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  BETWEEN FR 44 AND FR 195 LOWER PANEL, HYDRAULIC CONNECTOR AREAS AT Y =-2230 OR  47 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 26000 FH  27 AND STR 28. I: 4900 FC  OR  9850 FH  571118-01-6 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571121-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  148 INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND I: 6000 FC  LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL  FROM Y =-1959 TO Y = 1959.  (9 ASSYS TO BE INSPECTED)  571121-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 13000 FC  148 INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND OR  LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL 26000 FH  FROM Y =-1959 TO Y = 1959. I: 6000 FC  (9 ASSYS TO BE INSPECTED) OR  12000 FH  571122-01-1 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  196 BOX EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR OR  LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM 60000 FH  Y = 953 TO Y = 1959, LH/RH. I: 5500 FC  OR  27500 FH  571122-01-2 N/A TASK DELETED  R 571122-01-3 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  196 BOX EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR OR  LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM 26000 FH  Y = 953 TO Y = 1959, LH/RH. I: 4650 FC  OR  9350 FH  571123-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571123-01-2 N/A TASK DELETED  571123-01-3 N/A TASK DELETED  R 571125-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  148 BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 OR  AND FR 47 LOWER CORNER FITTING, LH/RH 75000 FH  I: 3850 FC  OR  26000 FH  R 571125-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  148 BOX REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 OR  AND FR 47 LOWER CORNER FITTING, LH/RH 26000 FH  I: 4200 FC  OR  8400 FH  571125-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 13000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 OR  AND FR 47 LOWER CORNER FITTING, LH/RH 65000 FH  I: 3910 FC  OR  26400 FH  571126-01-1 N/A TASK DELETED  D 571126-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571126-01-3 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 13000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER 65000 FH  I: 9900 FC  OR  65000 FH  571129-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR  60000 FH  I: 12100 FC  OR  60000 FH  571129-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR  60000 FH  I: 8000 FC  OR  60000 FH  571129-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 CENTER SPAR, 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR  26000 FH  I: 9200 FC  OR  18400 FH  571129-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 13000 FC  744 142 30MM AROUND ACCESS CUTOUTS (2 PLACES). OR  65000 FH  I: 8200 FC  OR  55400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571130-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FC  744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OR  147 60000 FH  148 I: 5710 FC  OR  38500 FH  571130-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FC  744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OR  147 26000 FH  148 I: 7700 FC  OR  15400 FH  571130-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 13000 FC  744 142 SPAR, 30MM AROUND MANHOLE CUTOUTS (2 PLACES). OR  147 65000 FH  148 I: 8300 FC  OR  56000 FH  571131-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CENTER WING BOX, REAR T: 6 YE 1  148 SPAR, AFT FACE I: 6 YE  571133-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD OR  FITTING CONNECTIONS (63 PLACES) 60000 FH  I: 7300 FC  OR  45800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 571133-01-2 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD OR  FITTING CONNECTIONS (63 PLACES) 75000 FH  I: 4700 FC  OR  31900 FH  R 571133-01-3 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, T: 13000 FC  744 142 STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD OR  FITTING CONNECTIONS (63 PLACES) 26000 FH  I: 5450 FC  OR  10900 FH  571137-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR 40, LH/RH 60000 FH  I: 6000 FC  OR  42300 FH  571137-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR 40, LH/RH 26000 FH  I: 6000 FC  OR  12000 FH  571137-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR 40, LH/RH 65000 FH  I: 13000 FC  OR  65000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571138-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, LOWER L-FITTING AT CONNECTION OR  WITH LOWER SKIN PANEL AT KEEL BEAM LEVEL, LH/RH. 60000 FH  I: 6000 FC  OR  42300 FH  571140-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP T: 6 YE 1  GALLEYS AND TOILETS 146 SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL I: 6 YE  FUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA  571140-02-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP T: 12 YE 1  146 SKIN UPPER SURFACE, PORTAL FRAMES AND LATERAL I: 12 YE  FUSELAGE STRUCTURE BETWEEN FR 40 AND FR 47.  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITTED ABOVE THIS AREA  571141-01-1 N/A TASK DELETED  571144-01-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 13000 FC  192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR  195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 65000 FH  196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5090 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 34300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571145-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CWB, INTERNAL T: 13000 FC  744 142 STRUCTURE, RIB1 LOWER TEE FITTING INBOARD FLANGE, OR  SEALANT REMOVAL FASTENERS IN RADIUS AREA AT STR16, STR20, STR21 AND 65000 FH  AND STR25 TO STR29, LH/RH I: 5230 FC  OR  35300 FH  571146-01-1 N/A TASK DELETED  571146-01-2 N/A TASK DELETED  571146-01-3 N/A TASK DELETED  R 571146-02-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR  195 OF RIB 1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND 60000 FH  196 STR25 TO STR29, LH/RH. I: 9500 FC  OR  64100 FH  571146-02-2 N/A TASK DELETED  D 571146-02-3 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571148-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192 PANEL, KEEL BEAM FITTING 4 FIRST BORE HOLES AFT FRAME OR  40 DATUM, LH/RH. 60000 FH  I: 6000 FC  OR  45900 FH  571149-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE OR  FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH 60000 FH  I: 6000 FC  OR  38300 FH  571149-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 571149-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE OR  FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH 26000 FH  I: 7200 FC  OR  14400 FH  571149-01-4 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  192 BOX LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE OR  FROM FR 40 TO STR 1 LEVEL, LH/RH 26000 FH  I: 8000 FC  OR  16000 FH  571149-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 13000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FR 40 TO OR  STR 1 LEVEL, LH/RH 65000 FH  I: 6500 FC  OR  43700 FH  R 571152-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  744 142 BOX INTERNAL STRUCTURE,CENTER SPAR FITTING FLANGE, OR  RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 75000 FH  FASTENERS 3 TO 12, LH/RH. I: 5900 FC  OR  40000 FH  R 571153-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF OR  SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 26000 FH  WITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 6000 FC  RADIUS ON EACH SIDE OF GUSSET, LH/RH OR  12000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571153-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF OR  SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 65000 FH  WITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 12100 FC  RADIUS ON EACH SIDE OF GUSSET, LH/RH OR  82000 FH  R 571153-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF OR  SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 60000 FH  WITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 6000 FC  RADIUS ON EACH SIDE OF GUSSET, LH/RH OR  40700 FH  571154-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX T: 12 YE NO  744 142 INTERNAL STRUCTURE EXCLUDING STRUTS I: 12 YE  571157-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, OR  SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 60000 FH  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 13000 FC  OR  60000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571157-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 13000 FC  744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, OR  SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 65000 FH  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 13000 FC  OR  65000 FH  571158-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 13000 FC  192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN OR  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 60000 FH  I: 4520 FC  OR  22600 FH  571158-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 13000 FC  192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN OR  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 65000 FH  I: 4290 FC  OR  29000 FH  571159-01-1 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  146 BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPAR OR  VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 60000 FH  BEAMS). I: 8200 FC  OR  60000 FH  571159-01-2 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING T: 13000 FC  146 BOX PORTAL BEAMS AT CONNECTION WITH FRONT SPAR OR  VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 26000 FH  BEAMS). I: 11300 FC  OR  22600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571159-01-3 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 13000 FC  146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS). 65000 FH  I: 9200 FC  OR  61900 FH  571160-01-1 147AZ 148AZ 141 DETAILED INSPECTION OF CENTER WING BOX T: 12 YE  142 STRUTS (54 PLACES) I: 12 YE  571165-01-1 N/A TASK DELETED  571165-01-2 N/A TASK DELETED  571805-01-1 192EB 192GB 192JB 143 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN T: 12 YE 1  192LB 192NB 192QB 191 LOWER SURFACE FROM FR.40 TO FR.47 BETWEEN RIB 1 LH I: 12 YE  195GB 195HB 195JB 192 AND RIB 1 RH.  195LB 195NB 734 193  744 195  AIR CONDITIONING 196  PACKS  HEATSHIELDS  571806-01-1 191FB 192FB 192JB 191 GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER T: 12 YE 1  192NB 195JB 195NB 192 SPLICE AT RIB 1 BETWEEN FR.40 AND FR.47. I: 12 YE  195  196  571831-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CENTER WING BOX , REAR T: 6 YE 1  148 SPAR, AFT FACE. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 571831-02-1 N/A TASK DELETED  571840-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  GALLEYS AND TOILETS 146 FROM FR40 TO FR47, BETWEEN CABIN FLOOR LEVEL AND I: 6 YE  INSULATION CENTER WING BOX UPPER PANEL.  LINING  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS  FITTED ABOVE THE AREA  571840-01-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2  INSULATION 146 FROM FR40 TO FR47, BETWEEN CABIN FLOOR LEVEL AND I: 12 YE  LINING CENTER WING BOX UPPER PANEL.  NOTE : TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITTED ABOVE THIS AREA.  571854-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX INTERNAL T: 12 YE NO  744 142 STRUCTURE AND ACCESS DOORS, EXCLUDING STRUTS. I: 12 YE  571860-01-1 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUTS (90 T: 12 YE  744 142 PLACES). I: 12 YE  572001-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 60000 FH  PYLON FAIRING AND PYLON REINFORCING I: 7200 FC  OR  27200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572001-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 60000 FH  PYLON FAIRING AND PYLON REINFORCING I: 7600 FC  OR  28700 FH  572001-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 26000 FH  PYLON FAIRING AND PYLON REINFORCING I: 8200 FC  OR  16400 FH  572001-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY 65000 FH  PYLON FAIRING AND PYLON REINFORCING I: 10400 FC  OR  45200 FH  572002-01-1 464BL 464BR 464FL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  464FR 474BL 474BR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR  474FL 474FR 472 60000 FH  474 I: 9500 FC  OR  35900 FH  572002-01-11 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR  474KL 474KR 472 65000 FH  474 I: 5400 FC  OR  23700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572002-01-2 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR  474KL 474KR 472 60000 FH  474 I: 7200 FC  OR  27200 FH  572002-01-3 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR  474KL 474KR 472 26000 FH  474 I: 7800 FC  OR  15600 FH  R 572002-01-7 464JL 464JR 464KL 462 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  464KR 474JL 474JR 464 MASKED BY PYLON DIAPHRAGM IN BAY 10 TO 10A OR  474KL 474KR 472 60000 FH  474 NOTE 8  I: 9500 FC  OR  35900 FH  572003-01-1 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FC  464AR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR  474AL 474AR 472 60000 FH  474 I: 7200 FC  OR  27200 FH  572003-01-10 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FC  464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR  474AL 474MR 472 65000 FH  474 I: 21500 FC  OR  93400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572003-01-2 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FC  464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR  474AL 474MR 472 60000 FH  474 I: 7600 FC  OR  28700 FH  572003-01-3 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FC  464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR  474AL 474MR 472 26000 FH  474 I: 8200 FC  OR  16400 FH  572003-01-7 462GR 462HL 464AL 462 DETAILED INSPECTION OF OUTER WING LOWER SURFACE, T: 13000 FC  464MR 472GL 472HR 464 VISIBLE PORTION OF INBOARD PYLON REINFORCING PLATE OR  474AL 474MR 472 60000 FH  474 I: 7200 FC  OR  27200 FH  572003-02-1 462GR 462HL 464AL 462 GENERAL VISUAL INSPECTION OF OUTER WING LOWER T: 12 YE  464AR 472GL 472HR 464 SURFACE VISIBLE PORTION OF INBOARD PYLON REINFORCING I: 12 YE  474AL 474AR 472 PLATE  474  572003-02-2 462GR 462HL 464AL 462 GENERAL VISUAL INSPECTION OF OUTER WING LOWER T: 12 YE  464MR 472GL 472HR 464 SURFACE VISIBLE PORTION OF INBOARD PYLON REINFORCING I: 12 YE  474AL 474MR 472 PLATE  474  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572004-01-1 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FH  MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5100 FC  FAIRING AND PYLON FAIRING. OR  19200 FH  572004-01-2 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FH  MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5300 FC  FAIRING AND PYLON FAIRING. OR  20000 FH  572004-01-3 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 26000 FH  MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 5700 FC  FAIRING AND PYLON FAIRING. OR  11400 FH  572004-01-4 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 65000 FH  MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 I: 3700 FC  FAIRING AND PYLON FAIRING. OR  16300 FH  572005-01-1 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF THE OUTER T: 13000 FC  641CB 641 WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA OR  MASKED BY MAIN LANDING GEAR REINFORCING PLATE 60000 FH  INCLUDING ATTACHMENT TO REAR SPAR I: 5700 FC  OR  21500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572005-01-2 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER T: 13000 FC  641 WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA OR  MASKED BY MAIN LANDING GEAR REINFORCING PLATE 60000 FH  INCLUDING ATTACHMENT TO REAR SPAR I: 5700 FC  OR  21500 FH  572005-01-3 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FC  641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN OR  LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 60000 FH  TO REAR SPAR I: 5600 FC  OR  21100 FH  572005-01-4 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FC  641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN OR  LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 26000 FH  TO REAR SPAR I: 6000 FC  OR  12000 FH  572005-01-5 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF THE OUTER WING BOTTOM T: 13000 FC  641 SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN OR  LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT 65000 FH  TO REAR SPAR I: 9400 FC  OR  40900 FH  572006-01-1 N/A TASK DELETED  572006-01-2 N/A TASK DELETED  572006-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572006-01-4 N/A TASK DELETED  572006-01-5 N/A TASK DELETED  572006-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO  600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YE  60000 FH  I: 4200 FC  OR  15800 FH  572006-02-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO  600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YE  60000 FH  I: 4700 FC  OR  17700 FH  572006-02-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 6 YE NO  600 MAIN LANDING GEAR REINFORCING PLATE I: 6 YE  572006-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC  600 MAIN LANDING GEAR REINFORCING PLATE OR  26000 FH  I: 5400 FC  OR  10800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572006-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 13000 FC T: 6 YE NO  600 MAIN LANDING GEAR REINFORCING PLATE OR I: 6 YE  65000 FH  I: 9700 FC  OR  42300 FH  572007-01-1 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN OR  AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 60000 FH  PYLON FAIRING I: 11200 FC  OR  42300 FH  572007-01-2 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN OR  AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 60000 FH  PYLON FAIRING I: 10000 FC  OR  37800 FH  572007-01-3 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN OR  AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 26000 FH  PYLON FAIRING I: 10800 FC  OR  21600 FH  572007-01-4 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN OR  AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD 65000 FH  PYLON FAIRING I: 6300 FC  OR  27300 FH  572007-01-5 464GL 464GR 474GL 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE T: 20 YE  474GR 531AB 631AB 600 SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN I: 12 YE I: 12 YE  AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD  PYLON FAIRING  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572008-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA OR  COVERED BY FLAP TRACK 2 FAIRING 60000 FH  I: 5000 FC  OR  18900 FH  572008-01-2 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA OR  COVERED BY FLAP TRACK 2 FAIRING 26000 FH  I: 5400 FC  OR  10800 FH  572008-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA OR  COVERED BY FLAP TRACK 2 FAIRING 65000 FH  I: 5800 FC  OR  25300 FH  572008-02-1 531AB 631AB 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE  631 SKIN LOWER SURFACE FORWARD OF REAR SPAR IN AREA I: 12 YE  COVERED BY FLAP TRACK 2 FAIRING  572009-01-1 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 OR  INBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FH  FAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 2400 FC  25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), OR  STRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 9000 FH  2-3).  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-02-1  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572009-01-2 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 60000 FH  FAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 2800 FC  BAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR  (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 10500 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-02-2  572009-01-3 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 26000 FH  FAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 3200 FC  BAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR  (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 6400 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-02-3  572009-01-9 464GL 464GR 474GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  474GR 531AB 631AB 474 SURFACE AT STRINGER RUNOUTS, STRINGER 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 (RIB BAY 65000 FH  FAIRING 631 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER 25 (RIB I: 5500 FC  BAY 11-12), STRINGER 26 (RIB BAY 8-9), STRINGER 27 OR  (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 2-3). 24000 FH  572009-02-1 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 OR  INBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FH  FAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 5100 FC  25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), OR  STRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 19200 FH  2-3).  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-01-1  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572009-02-2 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 OR  INBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 60000 FH  FAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 6100 FC  25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), OR  STRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 23000 FH  2-3).  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-01-2  572009-02-3 464GL 464GR 474GL 464 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  474GR 531AB 631AB 474 SKIN LOWER SURFACE AT STRINGER RUNOUTS, STRINGER 1 OR  INBOARD FUEL PUMP 531 (RIB BAY 2-3), STRINGER 2 (RIB BAY 4-5), STRINGER 3 26000 FH  FAIRING 631 (RIB BAY 6-7), STRINGER 4 (RIB BAY 8-9), STRINGER I: 6800 FC  25 (RIB BAY 11-12), STRINGER 26 (RIB BAY 8-9), OR  STRINGER 27 (RIB BAY 4-5) AND STRINGER 28 (RIB BAY 13600 FH  2-3).  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  572009-01-3  572010-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE T: 20 YE NO  541DB 541EB 541FB 641 SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS I: 12 YE I: 12 YE  641AB 641BB 641CB DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND  641DB 641EB 641FB 11-12  572010-02-1 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR  641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 60000 FH  641DB 641EB 641FB 9-10 AND 11-12 I: 5800 FC  OR  21900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572010-02-2 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR  641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 60000 FH  641DB 641EB 641FB 9-10 AND 11-12 I: 6700 FC  OR  25300 FH  572010-02-3 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR  641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 26000 FH  641DB 641EB 641FB 9-10 AND 11-12 I: 7500 FC  OR  15000 FH  572010-02-4 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541DB 541EB 541FB 641 BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND OR  641AB 641BB 641CB ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 65000 FH  641DB 641EB 641FB 9-10 AND 11-12 I: 5700 FC  OR  24700 FH  572011-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR OR  BETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 60000 FH  PYLON FAIRING. I: 4700 FC  OR  17700 FH  572011-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR OR  BETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 60000 FH  PYLON FAIRING. I: 3700 FC  OR  13900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572011-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR OR  BETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 26000 FH  PYLON FAIRING. I: 4100 FC  OR  8200 FH  572011-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO CENTER SPAR OR  BETWEEN RIB 1 AND RIB 12, EXCLUDING AREA COVERED BY 65000 FH  PYLON FAIRING. I: 5900 FC  OR  25600 FH  572012-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 1 AND OR  RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 60000 FH  FRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5000 FC  COVERED BY PYLON FAIRING AND PYLON OR  REINFORCING PLATE. 18900 FH  572012-01-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 1 AND OR  RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 26000 FH  FRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5400 FC  COVERED BY PYLON FAIRING AND PYLON OR  REINFORCING PLATE. 10800 FH  572012-01-3 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 1 AND OR  RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM 65000 FH  FRONT SPAR TO REAR SPAR EXCLUDING AREAS I: 5700 FC  COVERED BY PYLON FAIRING AND PYLON OR  REINFORCING PLATE. 24900 FH  572012-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572012-03-1 FUEL PUMP FAIRINGS 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  600 LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN I: 6 YE  RIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR  EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLON  REINFORCING PLATE.  572013-01-1 464AL 464AR 464BL 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  464BR 464FL 464FR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR  464GL 464GR 464HL EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 60000 FH  474AL 474AR 474BL AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5000 FC  474BR 474FL 474FR OR  474GL 474GR 474HL 18900 FH  572013-01-2 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR  464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 26000 FH  474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5400 FC  474HL 474JL 474JR OR  474KL 474KR 474MR 10800 FH  572013-01-3 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR  464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 60000 FH  474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5000 FC  474HL 474JL 474JR OR  474KL 474KR 474MR 18900 FH  572013-01-4 464AL 464GL 464GR 464 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  464HL 464JL 464JR 474 SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, OR  464KL 464KR 464MR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND 65000 FH  474AL 474GL 474GR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE I: 5700 FC  474HL 474JL 474JR OR  474KL 474KR 474MR 24900 FH  572013-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572013-02-2 464AL 464AR 464GL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  464GR 464HL 464JL 474 LOWER SURFACE IN AREA COVERED BY INBOARD PYLON I: 12 YE  464JR 464KL 464KR FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING  474AL 474AR 474GL PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING  474GR 474HL 474JL PLATE  474JR 474KL 474KR  572013-02-3 464AL 464GL 464GR 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  464HL 464JL 464JR 474 LOWER SURFACE IN AREA COVERED BY INBOARD PYLON I: 12 YE  464KL 464KR 464MR FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING  474AL 474GL 474GR PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING  474HL 474JL 474JR PLATE  474KL 474KR 474MR  572014-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FH  FAIRINGS. I: 8900 FC  OR  33600 FH  572014-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 60000 FH  FAIRINGS. I: 8100 FC  OR  30600 FH  572014-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 26000 FH  FAIRINGS. I: 8700 FC  OR  17400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572014-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 OR  BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY 65000 FH  FAIRINGS. I: 6300 FC  OR  27300 FH  572015-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  600 SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF I: 6 YE  FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1  AND RIB 12  572015-02-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 60000 FH  RIB 12 I: 9100 FC  OR  34300 FH  572015-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 60000 FH  RIB 12 I: 7400 FC  OR  27900 FH  572015-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 26000 FH  RIB 12 I: 8100 FC  OR  16200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572015-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 65000 FH  RIB 12 I: 5200 FC  OR  22500 FH  572016-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES I: 6 YE  BETWEEN RIB 2 AND RIB 4.  572016-02-1 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES OR  BETWEEN RIB 2 AND RIB 4 60000 FH  I: 4100 FC  OR  15400 FH  572016-02-2 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES OR  BETWEEN RIB 2 AND RIB 4 60000 FH  I: 4400 FC  OR  16600 FH  572016-02-3 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES OR  BETWEEN RIB 2 AND RIB 4 26000 FH  I: 4800 FC  OR  9600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572016-02-4 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES OR  BETWEEN RIB 2 AND RIB 4 65000 FH  I: 6100 FC  OR  26500 FH  572017-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR  60000 FH  I: 8600 FC  OR  32500 FH  572017-01-2 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR  60000 FH  I: 8000 FC  OR  30200 FH  572017-01-3 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR  26000 FH  I: 8400 FC  OR  16800 FH  572017-01-4 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641 SKIN ROOT JOINT FITTINGS ON STR 13 AND STR 20 OR  65000 FH  I: 10600 FC  OR  46000 FH  572017-02-1 541AB 641AB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  641 SKIN ROOT JOINT FITTING ON STR 13 AND STR 20 I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572018-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  541FZ 641AB 641AZ I: 7300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 27500 FH  641EZ 641FZ  572018-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  541FZ 641AB 641AZ I: 7300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 27500 FH  641EZ 641FZ  572018-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  541FZ 641AB 641AZ I: 7700 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 29100 FH  641EZ 641FZ  572018-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 26000 FH  541FZ 641AB 641AZ I: 8200 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 16400 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572018-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 OR  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 65000 FH  541FZ 641AB 641AZ I: 10800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 47100 FH  641EZ 641FZ  572018-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541BZ 541CB 541CZ 641 STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 I: 12 YE  541DB 541DZ 541EZ AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20  541FZ 641AB 641AZ  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  572019-01-1 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 OR  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  I: 7300 FC  OR  27500 FH  572019-01-2 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 OR  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  I: 7300 FC  OR  27500 FH  572019-01-3 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 OR  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 60000 FH  I: 7700 FC  OR  29100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572019-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 OR  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 26000 FH  I: 8200 FC  OR  16400 FH  572019-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 OR  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 65000 FH  I: 10800 FC  OR  47100 FH  572019-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641EB 641FB 641GB 641 STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 I: 12 YE  AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20  572020-01-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  641AB 641AZ 641BZ 641 UPPER SURFACE INCLUDING STRINGERS AND BUTTSTRAPS I: 6 YE  BETWEEN RIB 1 AND RIB 3  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE  ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF  THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL  ENVIRONMENT  572021-01-1 464FL 464FR 464GL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  464GR 474FL 474FR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR  474GL 474GR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FH  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FC  OR  44200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572021-01-2 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR  474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FH  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 10900 FC  OR  41200 FH  572021-01-3 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR  474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 26000 FH  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FC  OR  23400 FH  572021-01-4 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR  474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 60000 FH  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 11700 FC  OR  44200 FH  572021-01-5 464GL 464GR 464JL 464 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  464JR 474GL 474GR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 OR  474JL 474JR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON 65000 FH  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING I: 6700 FC  OR  29400 FH  572021-02-1 464FL 464FR 464GL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE  464GR 474FL 474FR 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 I: 12 YE  474GL 474GR 531AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON  631AB 631 FAIRING AND FLAP TRACK 2 FAIRING  572021-02-2 464GL 464GR 464JL 464 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE  464JR 474GL 474JL 474 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 I: 12 YE  474JR 531AB 631AB 531 AND STR 20 IN AREAS COVERED BY INBOARD PYLON  631 FAIRING AND FLAP TRACK 2 FAIRING  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572022-01-1 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY OR  PER NTM 10-11, FROM STR 6 TO STR 7 60000 FH  I: 9800 FC  OR  37000 FH  572022-01-2 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY OR  PER NTM 10-11, FROM STR 6 TO STR 7 60000 FH  I: 5800 FC  OR  21900 FH  572022-01-3 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY OR  PER NTM 10-11, FROM STR 6 TO STR 7 26000 FH  I: 6300 FC  OR  12600 FH  572022-01-4 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY OR  PER NTM 10-11, FROM STR 6 TO STR 7 65000 FH  I: 13000 FC  OR  65000 FH  572023-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  600 AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 I: 6 YE  FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS  COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN  LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2  FAIRING  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572023-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OR  10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 60000 FH  COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5000 FC  LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 OR  FAIRING 18900 FH  572023-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OR  10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 26000 FH  COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5400 FC  LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 OR  FAIRING 10800 FH  572023-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN AT STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB OR  10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS 65000 FH  COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN I: 5800 FC  LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 OR  FAIRING 25300 FH  572025-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641AB 641BB 641CB 641 SKIN STRINGER JOINTS AT STR 11 BETWEEN RIBS 3 AND OR  NUT REMOVAL AS PER RIBS 4 AND STR 12 AND 14 BETWEEN RIBS 5 AND 6 60000 FH  NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7100 FC  TASK 572025-02-1 OR  27200 FH  572025-01-2 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  641AB 641BB 641CB 641 SKIN STRINGER JOINTS AT STR 11 BETWEEN RIBS 3 AND OR  NUT REMOVAL AS PER RIBS 4 AND STR 12 AND 14 BETWEEN RIBS 5 AND 6 60000 FH  NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7500 FC  TASK 572025-02-2 OR  28800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572025-02-1 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641AB 641BB 641CB 641 BOTTOM SKIN STRINGER JOINTS AT STR 11 BETWEEN OR  NUT REMOVAL AS PER RIBS 3 AND RIBS 4 AND STR 12 AND 14 BETWEEN 60000 FH  NTM RIBS 5 AND 6 I: 7100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572025-01-1 27200 FH  572025-02-2 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641AB 641BB 641CB 641 BOTTOM SKIN STRINGER JOINTS AT STR 11 BETWEEN OR  NUT REMOVAL AS PER RIBS 3 AND RIBS 4 AND STR 12 AND 14 BETWEEN 60000 FH  NTM RIBS 5 AND 6 I: 7500 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572025-01-2 28800 FH  572026-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR  541DB 541DZ 541EZ 60000 FH  541FZ 641AB 641AZ I: 5700 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 21500 FH  641EZ 641FZ  572026-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR  541DB 541DZ 541EZ 60000 FH  541FZ 641AB 641AZ I: 5500 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 20700 FH  641EZ 641FZ  572026-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR  541DB 541DZ 541EZ 26000 FH  541FZ 641AB 641AZ I: 5900 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 11800 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572026-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 OR  541DB 541DZ 541EZ 65000 FH  541FZ 641AB 641AZ I: 8800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 38100 FH  641EZ 641FZ  572026-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  541BZ 541CB 541CZ 641 SKIN STRINGER 18 BETWEEN RIB 1 AND RIB 9 I: 12 YE  541DB 541DZ 541EZ  541FZ 641AB 641AZ  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  572027-01-1 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  541DB 541DZ 541EZ 1 AND RIB 9 60000 FH  541FZ 641AB 641AZ I: 13300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50200 FH  641EZ 641FZ  572027-01-2 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  541DB 541DZ 541EZ 1 AND RIB 9 60000 FH  541FZ 641AB 641AZ I: 13300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50200 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572027-01-3 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  541DB 541DZ 541EZ 1 AND RIB 9 60000 FH  541FZ 641AB 641AZ I: 10900 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 41200 FH  641EZ 641FZ  572027-01-4 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  541DB 541DZ 541EZ 1 AND RIB 9 26000 FH  541FZ 641AB 641AZ I: 11700 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 23400 FH  641EZ 641FZ  572027-01-5 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  541DB 541DZ 541EZ 1 AND RIB 9 65000 FH  541FZ 641AB 641AZ I: 8600 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 37600 FH  641EZ 641FZ  572027-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN I: 12 YE  541DB 541DZ 541EZ RIB 1 AND RIB 9.  541FZ 641AB 641AZ  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572028-01-1 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572028-02-1 I: 5700 FC  OR  21500 FH  572028-01-2 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572028-02-2 I: 5500 FC  OR  20700 FH  572028-02-1 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 OR  NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  NTM TASK 572028-01-1 I: 5700 FC  OR  21500 FH  572028-02-2 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8 OR  NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  NTM TASK 572028-01-2 I: 5500 FC  OR  20700 FH  572029-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN OR  RIB 1 AND RIB 12 60000 FH  I: 4200 FC  OR  22300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572029-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN OR  RIB 1 AND RIB 12 26000 FH  I: 5300 FC  OR  10600 FH  572029-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN OR  RIB 1 AND RIB 12 65000 FH  I: 6100 FC  OR  28100 FH  572030-01-1 N/A TASK DELETED  572030-01-2 N/A TASK DELETED  572030-01-3 N/A TASK DELETED  572030-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN OR  RIB 9 AND RIB 11 65000 FH  I: 8900 FC  OR  41200 FH  572032-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572032-01-2 N/A TASK DELETED  572032-01-3 N/A TASK DELETED  572033-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT OR  SPAR TO REAR SPAR 60000 FH  I: 4200 FC  OR  22600 FH  572033-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT OR  SPAR TO REAR SPAR 60000 FH  I: 4600 FC  OR  24800 FH  572033-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT OR  SPAR TO REAR SPAR 26000 FH  I: 6100 FC  OR  12200 FH  572033-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT OR  SPAR TO REAR SPAR 65000 FH  I: 6300 FC  OR  29000 FH  572033-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT I: 6 YE  SPAR TO REAR SPAR.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572034-01-1 N/A TASK DELETED  572034-01-2 N/A TASK DELETED  572034-01-3 N/A TASK DELETED  572035-01-1 N/A TASK DELETED  572035-01-2 N/A TASK DELETED  572035-01-3 N/A TASK DELETED  572035-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE FROM STRINGERS 12 TO 19 AND FROM RIB OR  4 TO RIB 8 65000 FH  I: 13000 FC  OR  65000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572036-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO OR  REAR SPARS 60000 FH  I: 5100 FC  OR  21900 FH  572036-01-2 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 13000 FC  641AB 641AZ 641BZ 641 CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS OR  60000 FH  I: 5000 FC  OR  21700 FH  572036-01-3 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO OR  REAR SPARS 26000 FH  I: 6200 FC  OR  12400 FH  572036-01-4 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO OR  REAR SPARS 65000 FH  I: 9700 FC  OR  44700 FH  572036-02-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO I: 12 YE  REAR SPARS.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572037-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR 60000 FH  541FZ 641AB 641AZ I: 5500 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 29500 FH  641EZ 641FZ  572037-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR 60000 FH  541FZ 641AB 641AZ SPAR I: 8800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 47100 FH  641EZ 641FZ  572037-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR 26000 FH  541FZ 641AB 641AZ SPAR I: 10800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 21600 FH  641EZ 641FZ  572037-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR 65000 FH  541FZ 641AB 641AZ SPAR I: 9800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 45100 FH  641EZ 641FZ  572037-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM I: 12 YE  541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR.  541FZ 641AB 641AZ  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572038-01-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  641FB 641 REINFORCING PLATE LOWER SURFACE AT INNER PYLON I: 12 YE  572039-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR  7 TO RIB 9 AND FROM RIB 11 TO RIB 12 60000 FH  I: 4200 FC  OR  22300 FH  572039-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR  7 TO RIB 9 AND FROM RIB 11 TO RIB 12 60000 FH  I: 4200 FC  OR  22300 FH  572039-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR  7 TO RIB 9 AND FROM RIB 11 TO RIB 12 26000 FH  I: 5200 FC  OR  10400 FH  572039-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB OR  7 TO RIB 9 AND FROM RIB 11 TO RIB 12 65000 FH  I: 8900 FC  OR  41200 FH  572040-01-1 N/A TASK DELETED  572040-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572040-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB OR  11 AND RIB 13 26000 FH  I: 13000 FC  OR  26000 FH  572040-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB OR  11 AND RIB 13 65000 FH  I: 13000 FC  OR  65000 FH  572041-01-1 573DB 573FB 673DB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE  673FB 573 AFT FACE BETWEEN RIB 1 AND RIB 12. I: 12 YE  FLAPS EXTENDED 671  673  572043-01-1 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR  60000 FH  I: 7100 FC  OR  31200 FH  572043-01-2 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR  60000 FH  I: 5400 FC  OR  23800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572043-01-3 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR  26000 FH  I: 6000 FC  OR  12000 FH  572043-01-4 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  673 AFT FACE SPAR JOINT PLATE AT RIB 9 OR  65000 FH  I: 9400 FC  OR  42400 FH  572043-02-1 573FB 673FB 573 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE  673 AFT FACE SPAR JOINT PLATE AT RIB 9. I: 12 YE  572045-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE NO  641AB 641AZ 641BZ 641 FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YE  572046-01-1 N/A TASK DELETED  572046-01-2 N/A TASK DELETED  572046-01-3 N/A TASK DELETED  572046-02-1 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO  541DB 541EB 541FB 641 FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP I: 12 YE  641AB 641BB 641CB AND BOTTOM FLANGES.  641DB 641EB 641FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572047-01-1 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OR  641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 60000 FH  641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FC  SEALANT REMOVAL AS RIB 7 OR  PER NTM 60000 FH  572047-01-2 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OR  641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 26000 FH  641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FC  SEALANT REMOVAL AS RIB 7 OR  PER NTM 26000 FH  572047-01-3 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  541CB 541CZ 641AB 641 REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, OR  641BB 641BZ 641CB FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND 65000 FH  641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND I: 13000 FC  SEALANT REMOVAL AS RIB 7 OR  PER NTM 65000 FH  572047-02-1 541AB 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR T: 12 YE NO  541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD I: 12 YE  641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND  641CZ SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND  RIB 7.  572049-01-1 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 9 60000 FH  I: 10700 FC  OR  46800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572049-01-2 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 9 60000 FH  I: 8100 FC  OR  35700 FH  572049-01-3 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 9 26000 FH  I: 9100 FC  OR  18200 FH  572049-01-4 N/A 540 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  640 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 9 65000 FH  I: 11700 FC  OR  53000 FH  572050-01-1 N/A TASK DELETED  572050-01-2 N/A TASK DELETED  572050-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572050-01-4 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  FLAPS EXTENDED 573 AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 OR  671 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7 65000 FH  673 I: 13000 FC  OR  65000 FH  572051-01-1 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 OR  PER NTM 60000 FH  I: 5200 FC  OR  22700 FH  572051-01-2 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 OR  PER NTM 60000 FH  I: 5200 FC  OR  22700 FH  572051-01-3 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 OR  PER NTM 60000 FH  I: 13000 FC  OR  60000 FH  572051-01-4 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 OR  PER NTM 26000 FH  I: 13000 FC  OR  26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572051-01-5 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2 OR  PER NTM 65000 FH  I: 13000 FC  OR  65000 FH  572052-01-1 N/A TASK DELETED  572052-01-2 N/A TASK DELETED  572052-01-3 N/A TASK DELETED  572052-02-1 541BB 541CB 641BB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO  641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP I: 12 YE  AND BOTTOM FLANGES.  572054-01-1 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 OR  60000 FH  I: 4500 FC  OR  19700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572054-01-2 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 OR  60000 FH  I: 3300 FC  OR  14500 FH  572054-01-3 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 OR  60000 FH  I: 7000 FC  OR  30600 FH  572054-01-4 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 13000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5 OR  26000 FH  I: 7800 FC  OR  15600 FH  572061-01-1 521AB 521BB 521CB 521 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE  521DB 521EB 521FB 522 FORWARD FACE BETWEEN RIB 1 AND RIB 12 INCLUDING I: 6 YE  521GB 521HB 521JB 621 ALL CUTOUTS AND IN VICINITY OF FORWARD PYLON  522AB 522BB 522CB 622 ATTACHMENT FITTING IN REGION OF RIB BAY 10-10A  522DB 522EB 621AB AND BUILD DOOR  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB  572062-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  641 UPPER AND LOWER ROOT JOINT FITTINGS I: 12 YE I: 12 YE  572063-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572063-01-2 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 OR  641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 60000 FH  641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 7100 FC  REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING OR  INBOARD OF RIB 12 31000 FH  572063-01-3 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 OR  641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 60000 FH  641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 8100 FC  REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING OR  INBOARD OF RIB 12 35800 FH  572063-01-4 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 OR  641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, 26000 FH  641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN I: 12300 FC  REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING OR  INBOARD OF RIB 12 24600 FH  572063-02-1 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO  541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 I: 12 YE  641AB 641BB 641CB AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,  641DB 641EB 641FB BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN  REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING  INBOARD OF RIB 12.  572064-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572064-01-2 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR  60000 FH  I: 7100 FC  OR  31000 FH  572064-01-3 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR  60000 FH  I: 8100 FC  OR  35800 FH  572064-01-4 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR  26000 FH  I: 12300 FC  OR  24600 FH  572064-01-5 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  640 AFT FACE BETWEEN RIB 8 AND RIB 10 OR  65000 FH  I: 13000 FC  OR  65000 FH  572064-02-1 541EB 641EB 540 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO  640 AND AFT FACE BETWEEN RIB 8 AND RIB 10. I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572065-01-1 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12 OR  60000 FH  I: 6900 FC  OR  30300 FH  572065-01-2 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OR  60000 FH  I: 6600 FC  OR  28800 FH  572065-01-3 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OR  26000 FH  I: 9900 FC  OR  19800 FH  572065-01-4 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. OR  65000 FH  I: 13000 FC  OR  65000 FH  572065-01-5 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 12 YE T: 20 YE  622EB 622 FORWARD FACE SPAR JOINT PLATE AT RIB 12. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572066-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 12 60000 FH  I: 6900 FC  OR  30300 FH  572066-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 12 60000 FH  I: 6600 FC  OR  28800 FH  572066-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 12 26000 FH  I: 9900 FC  OR  19800 FH  572066-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  RIB 12 65000 FH  I: 13000 FC  OR  65000 FH  572067-01-1 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 60000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 12000 FC  OR  52600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572067-01-2 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 60000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 12400 FC  OR  54400 FH  572067-01-3 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 26000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 13000 FC  OR  26000 FH  572067-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 65000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS I: 5200 FC  OR  23600 FH  572067-02-1 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6 T: 12 YE NO  541FZ 641CB 641DB 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS I: 12 YE  641EZ 641FZ INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF  STRINGER CUTOUTS AND ACCESS CUTOUT  SURROUNDS.  572068-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572068-01-2 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 4800 FC  SURROUNDS OR  21000 FH  572068-01-3 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 26000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FC  SURROUNDS OR  10400 FH  572068-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 T: 13000 FC  541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 65000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FC  SURROUNDS OR  23600 FH  572068-02-1 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7 T: 12 YE NO  541FZ 641CB 641DB 641 FORWARD AND AFT OF THE CENTER SPAR AT SKIN I: 12 YE  641EZ 641FZ ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT  SURROUNDS.  572069-01-1 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FC  641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5400 FC  SURROUNDS OR  23900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572069-01-2 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FC  641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 60000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 6100 FC  SURROUNDS OR  26700 FH  572069-01-3 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FC  641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 26000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 7200 FC  SURROUNDS OR  14400 FH  572069-01-4 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND T: 13000 FC  641FZ 641 9 FORWARD AND AFT OF THE CENTER SPAR AT SKIN OR  ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, 65000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FC  SURROUNDS OR  23600 FH  572069-02-1 541DB 541FZ 641DB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 8 AND 9 T: 12 YE NO  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS I: 12 YE  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.  572071-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FC  541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR  541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 60000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 5500 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING OR  24300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572071-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FC  541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR  541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 60000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 6200 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE OR  BOLTING 27200 FH  572071-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FC  541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR  541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 26000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 7300 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE OR  BOLTING 14600 FH  572071-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS T: 13000 FC  541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND OR  541EZ 641AB 641AZ RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS),SPAR 65000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 13000 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE OR  BOLTING 65000 FH  572071-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 2,3,4 T: 12 YE NO  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A I: 12 YE  541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE  BOLTING.  572072-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572073-01-1 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FC  641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 60000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13000 FC  SURROUNDS OR  60000 FH  572073-01-2 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FC  641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 60000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13300 FC  SURROUNDS OR  58200 FH  572073-01-3 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FC  641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 26000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 13000 FC  SURROUNDS OR  26000 FH  572073-01-4 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 13000 FC  641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 65000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 5200 FC  SURROUNDS OR  23600 FH  572073-02-1 541FB 541GB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB T: 12 YE NO  641GB 641 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN I: 12 YE  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT  SURROUNDS  572074-01-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB T: 12 YE NO  641FB 641 10 FORWARD, RIB 10 A AND PYLON DIAPHRAGM. I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572075-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOX, RIB 1 EXTERNAL T: 12 YE T: 20 YE NO  641 SURFACE AND UPPER SURFACE OF TRIFORM FITTING, BETWEEN I: 12 YE I: 12 YE  FRONT SPAR AND REAR SPAR.  572081-01-1 N/A TASK DELETED  572081-01-2 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC NO  641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  NOTE: TASK APPLICABLE IF MOD 43021 CARRIED OUT BY 60000 FH  RETROFIT SOLUTION I: 7500 FC  OR  33100 FH  572081-01-3 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  60000 FH  I: 4800 FC  OR  21300 FH  572081-01-4 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 OR  26000 FH  I: 5500 FC  OR  11000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572081-01-5 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 OR  65000 FH  I: 5400 FC  OR  24300 FH  572081-01-6 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 12 YE T: 20 YE NO  641AZ 641 SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2 I: 12 YE I: 12 YE  572082-01-1 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FH  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 8500 FC  641BB 641CB 641DB CONDUIT HOLES. OR  641DZ 641EB 641EZ 37400 FH  641FB 641FZ  572082-01-2 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FH  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 8500 FC  641BB 641CB 641DB CONDUIT HOLES. OR  641DZ 641EB 641EZ 37400 FH  641FB 641FZ  572082-01-3 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 60000 FH  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 10800 FC  641BB 641CB 641DB CONDUIT HOLES. OR  641DZ 641EB 641EZ 47300 FH  641FB 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572082-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 26000 FH  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 16300 FC  641BB 641CB 641DB CONDUIT HOLES. OR  641DZ 641EB 641EZ 32600 FH  641FB 641FZ  572082-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 13000 FC  541CB 541DB 541DZ 641 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES OR  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA 65000 FH  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND I: 13000 FC  641BB 641CB 641DB CONDUIT HOLES. OR  641DZ 641EB 641EZ 65000 FH  641FB 641FZ  572082-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING CENTER SPAR T: 12 YE NO  541CB 541DB 541DZ 641 BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES I: 12 YE  541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA  541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND  641BB 641CB 641DB CONDUIT HOLES.  641DZ 641EB 641EZ  641FB 641FZ  572083-01-1 541AB 541BZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER T: 12 YE T: 20 YE NO  641BZ 641 SPAR ASSEMBLY AFT FACE BETWEEN RIB 1 AND RIB 2 I: 12 YE I: 12 YE  572084-01-5 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 13000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR11, STR14, STR18 TO STR20 65000 FH  AND AT STR23 TO STR28, LH/RH I: 7000 FC  OR  47400 FH  572085-01-1 191BT 191CT 192BT 191 GENERAL VISUAL INSPECTION OF OUTER WING BOX, T: 12 YE 1  192CT 192 CRUCIFORM FITTING, OUTBOARD FLANGE UPPER SURFACE AS I: 12 YE  FAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RH.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572091-01-1 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10 OR  NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  NTM TASK 572091-02-1 I: 7100 FC  OR  26800 FH  572091-01-2 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10 OR  NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  NTM TASK 572091-02-2 I: 7500 FC  OR  28300 FH  572091-02-1 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641FB 641 BOTTOM SKIN STRINGER 10 JOINT BETWEEN RIB 9 AND OR  NUT REMOVAL AS PER RIB 10 60000 FH  NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7100 FC  SEALANT REMOVAL AS TASK 572091-01-1 OR  PER NTM 26800 FH  572091-02-2 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641FB 641 BOTTOM SKIN STRINGER 10 JOINT BETWEEN RIB 9 AND OR  NUT REMOVAL AS PER RIB 10 60000 FH  NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7500 FC  SEALANT REMOVAL AS TASK 572091-01-2 OR  PER NTM 28300 FH  572092-01-1 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 60000 FH  I: 5700 FC  OR  21500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572092-01-2 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 60000 FH  I: 5500 FC  OR  20700 FH  572092-01-3 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 26000 FH  I: 5900 FC  OR  11800 FH  572092-01-4 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR 65000 FH  I: 8800 FC  OR  38100 FH  572092-02-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, I: 12 YE  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR  572093-01-1 N/A TASK DELETED  572093-01-2 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-02-2 I: 10400 FC  OR  39300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572093-01-3 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-02-3 I: 10400 FC  OR  39300 FH  572093-01-4 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-02-4 I: 9200 FC  OR  34700 FH  572093-01-5 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FH  TASK 572093-02-5 I: 9900 FC  OR  19800 FH  572093-01-6 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 13000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FH  TASK 572093-02-6 I: 5200 FC  OR  22500 FH  572093-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572093-02-2 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-01-2 I: 10400 FC  OR  39300 FH  572093-02-3 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-01-3 I: 10400 FC  OR  39300 FH  572093-02-4 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572093-01-4 I: 9200 FC  OR  34700 FH  572093-02-5 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FH  TASK 572093-01-5 I: 9900 FC  OR  19800 FH  572093-02-6 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FH  TASK 572093-01-6 I: 5200 FC  OR  22500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572093-03-1 541FB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641 JOINT OF STRINGER 15 TO CENTER SPAR. I: 12 YE  572094-01-1 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  9 AND RIB 12 60000 FH  I: 13300 FC  OR  50200 FH  572094-01-2 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  9 AND RIB 12 60000 FH  I: 13300 FC  OR  50200 FH  572094-01-3 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  9 AND RIB 12 60000 FH  I: 10900 FC  OR  41200 FH  572094-01-4 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  9 AND RIB 12 26000 FH  I: 11700 FC  OR  23400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572094-01-5 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB OR  9 AND RIB 12 65000 FH  I: 8600 FC  OR  37600 FH  572094-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB I: 12 YE  9 AND RIB 12.  572095-01-1 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR  60000 FH  I: 7300 FC  OR  27500 FH  572095-01-2 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR  60000 FH  I: 7300 FC  OR  27500 FH  572095-01-3 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR  60000 FH  I: 7700 FC  OR  29100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572095-01-4 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR  26000 FH  I: 8200 FC  OR  16400 FH  572095-01-5 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  641CB 641 BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7 OR  65000 FH  I: 8600 FC  OR  37600 FH  572101-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 60000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4500 FC  OR  17000 FH  572101-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 60000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4300 FC  OR  16200 FH  572101-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 26000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 4600 FC  OR  9200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572101-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 65000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 I: 8000 FC  OR  34900 FH  572102-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  60000 FH  I: 5800 FC  OR  21900 FH  572102-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  60000 FH  I: 5000 FC  OR  18900 FH  572102-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  26000 FH  I: 5700 FC  OR  11400 FH  572102-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  65000 FH  I: 13000 FC  OR  65000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572104-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 60000 FH  AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 5600 FC  PLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN OR  JOINTS AT RIB 27 AND RIB 39 21100 FH  572104-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 65000 FH  AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 8000 FC  PLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN OR  JOINTS AT RIB 27 AND RIB 39 34900 FH  572104-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 60000 FH  AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 4600 FC  PLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN OR  JOINTS AT RIB 27 AND RIB 39 17300 FH  572104-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING 26000 FH  AREAS COVERED BY PYLON REINFORCING, PYLON FAIRING, I: 4900 FC  PLASTRON FAIRING, FLAP TRACK 5 FAIRING AND SKIN OR  JOINTS AT RIB 27 AND RIB 39 9800 FH  572106-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 12 AND RIB 23 60000 FH  I: 7700 FC  OR  29100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572106-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 12 AND RIB 23 60000 FH  I: 8000 FC  OR  30200 FH  572106-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 12 AND RIB 23 26000 FH  I: 8600 FC  OR  17200 FH  572106-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 12 AND RIB 23 65000 FH  I: 5300 FC  OR  23200 FH  572107-01-1 560BB 560CB 560DB 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  660BB 660CB 660DB 600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 23 AND RIB 39 60000 FH  I: 7700 FC  OR  29100 FH  572107-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 23 AND RIB 39 60000 FH  I: 8000 FC  OR  30200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572107-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 23 AND RIB 39 26000 FH  I: 8600 FC  OR  17200 FH  572107-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  600 BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGERS OR  BETWEEN RIB 23 AND RIB 39 65000 FH  I: 5300 FC  OR  23200 FH  572108-01-1 454FL 454FR 484FL 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  484FR 532AB 533AB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YE  534AB 541GB 541HB 641 IN ALL BAYS BETWEEN RIB 12 AND RIB 27  541JB 541KB 541LB 642  541MB 541NB 541PB  541QB 541RB 541SB  542AB 542BB 542CB  542DB 560CB 632AB  633AB 634AB 641GB  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB 642AB 642BB  642CB 642DB 660CB  572108-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572108-01-3 454FL 454FR 484FL 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  484FR 532AB 533AB 542 AND LOWER MATING SURFACE AROUND ACCESS DOOR CUTOUTS I: 6 YE  534AB 541GB 541HB 641 IN ALL BAYS BETWEEN RIB 12 AND RIB 27  541JB 541KB 541LB 642  541MB 541NB 541PB  541QB 541RB 541SB  542AB 542BB 542CB  542DB 632AB 633AB  634AB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB  572108-02-1 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 60000 FH  541JB 541KB 541LB 642 I: 9000 FC  541MB 541NB 541PB OR  541QB 541RB 541SB 34000 FH  542AB 542BB 542CB  542DB 560CB 632AB  633AB 634AB 641GB  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB 642AB 642BB  642CB 642DB 660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572108-02-11 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 65000 FH  541JB 541KB 541LB 642 I: 5200 FC  541MB 541NB 541PB OR  541QB 541RB 541SB 22500 FH  542AB 542BB 542CB  542DB 632AB 633AB  634AB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB  572108-02-2 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 60000 FH  541JB 541KB 541LB 642 I: 11800 FC  541MB 541NB 541PB OR  541QB 541RB 541SB 44600 FH  542AB 542BB 542CB  542DB 632AB 633AB  634AB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572108-02-3 454FL 454FR 484FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  484FR 532AB 533AB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  534AB 541GB 541HB 641 CUTOUTS IN ALL BAYS BETWEEN RIB 12 AND RIB 27 26000 FH  541JB 541KB 541LB 642 I: 12800 FC  541MB 541NB 541PB OR  541QB 541RB 541SB 25600 FH  542AB 542BB 542CB  542DB 632AB 633AB  634AB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB  572109-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR I: 6 YE  550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN  550DB 550EB 550FB 650 RIBS 27 AND 39  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-1 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR  550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 60000 FH  550DB 550EB 550FB 650 RIBS 27 AND 39 I: 11400 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 43000 FH  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572109-02-2 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR  550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 60000 FH  550DB 550EB 550FB 650 RIBS 27 AND 39 I: 8200 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 30900 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-3 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR  550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 26000 FH  550DB 550EB 550FB 650 RIBS 27 AND 39 I: 9400 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 18800 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-4 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542HB 542JB 542KB 550 SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR OR  550AB 550BB 550CB 642 CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN 65000 FH  550DB 550EB 550FB 650 RIBS 27 AND 39 I: 5200 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 22500 FH  650AB 650BB 650CB  650DB 650EB 650FB  572110-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5 I: 10700 FC  OR  40400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572110-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5 I: 9700 FC  OR  36600 FH  572110-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 26000 FH  FAIRINGS 3, 4 AND 5 I: 10400 FC  OR  20800 FH  572110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 65000 FH  FAIRINGS 3, 4 AND 5 I: 7700 FC  OR  33500 FH  572110-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM I: 6 YE  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY  FLAP TRACK FAIRINGS 3, 4 AND 5.  572111-01-1 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK OR  632AB 632CB 633AB 534 FAIRINGS 3, 4 AND 5 60000 FH  633CB 634AB 634CB 632 I: 10700 FC  633 OR  634 40400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572111-01-2 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK OR  632AB 632CB 633AB 534 FAIRINGS 3, 4 AND 5 60000 FH  633CB 634AB 634CB 632 I: 9700 FC  633 OR  634 36600 FH  572111-01-3 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 OR  632AB 632CB 633AB 534 AND 5 26000 FH  633CB 634AB 634CB 632 I: 10400 FC  633 OR  634 20800 FH  572111-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 OR  632AB 632CB 633AB 534 AND 5 65000 FH  633CB 634AB 634CB 632 I: 8300 FC  633 OR  634 36200 FH  572111-02-1 532AB 532CB 533AB 532 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE  533CB 534AB 534CB 533 LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS I: 6 YE  632AB 632CB 633AB 534 3, 4 AND 5.  633CB 634AB 634CB 632  633  634  572112-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FH  FLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 10100 FC  PLASTRON FAIRING OR  38100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572112-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 60000 FH  FLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 9100 FC  PLASTRON FAIRING OR  34300 FH  572112-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 26000 FH  FLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 10100 FC  PLASTRON FAIRING OR  20200 FH  572112-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 65000 FH  FLAP TRACK FAIRINGS 5, OUTBOARD PYLON FAIRING AND I: 7700 FC  PLASTRON FAIRING OR  33500 FH  572112-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  600 LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT I: 12 YE  SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP  TRACK FAIRING 5, OUTBOARD PYLON FAIRING AND  PLASTRON FAIRING.  572113-01-1 452FR 454AL 454AR 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  454BL 454BR 454FL 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR  454FR 482FL 484AL 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FH  484AR 484BL 484BR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FC  484FL 484FR FITTING OR  38100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572113-01-2 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR  454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FH  484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 9100 FC  484PL 484PR FITTING OR  34300 FH  572113-01-3 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR  454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 26000 FH  484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FC  484PL 484PR FITTING OR  20200 FH  572113-01-4 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR  454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 60000 FH  484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 10100 FC  484PL 484PR FITTING OR  38100 FH  572113-01-5 452MR 454AL 454BL 452 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  454KR 454MR 454NR 454 SKIN LOWER SURFACE IN AREA COVERED BY OUTBOARD OR  454QL 482NL 484AR 482 PYLON FAIRING, BUT EXCLUDING AREA COVERED BY 65000 FH  484ML 484NL 484NR 484 OUTBOARD PYLON PICK-UP PLATE AND AFT ATTACHMENT I: 8300 FC  484PL 484PR FITTING OR  36200 FH  572113-02-1 452FR 454AL 454AR 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454BL 454BR 454FL 454 LOWER SURFACE IN AREA COVERED BY OUTBOARD PYLON I: 12 YE  454FR 482FL 484AL 482 FAIRING, BUT EXCLUDING AREA COVERED BY OUTBOARD PYLON  484AR 484BL 484BR 484 PICK-UP PLATE AND AFT ATTACHMENT FITTING.  484FL 484FR  572113-02-2 452MR 454AL 454BL 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454KR 454MR 454NR 454 LOWER SURFACE IN AREA COVERED BY OUTBOARD PYLON I: 12 YE  454QL 482NL 484AR 482 FAIRING, BUT EXCLUDING AREA COVERED BY OUTBOARD PYLON  484ML 484NL 484NR 484 PICK-UP PLATE AND AFT ATTACHMENT FITTING.  484PL 484PR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572114-01-1 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT OR  RIB 26 60000 FH  I: 5100 FC  OR  22300 FH  572114-01-2 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT OR  RIB 26 60000 FH  I: 5400 FC  OR  23600 FH  572114-01-3 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT OR  RIB 26 26000 FH  I: 6000 FC  OR  12000 FH  572114-01-4 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642DB 642 SKIN MASKED BY INTERNAL PYLON BRACKETS AT OR  RIB 26 65000 FH  I: 6700 FC  OR  29100 FH  572115-01-1 452FR 454AL 454AR 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454BL 454BR 482FL 454 LOWER SURFACE, VISIBLE PORTION OF OUTBOARD PYLON I: 12 YE  484AL 484AR 484BL 482 REINFORCING PLATE.  484BR 484  572115-01-2 452MR 454AL 454BL 452 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454KR 454MR 482NL 454 LOWER SURFACE, VISIBLE PORTION OF OUTBOARD PYLON I: 12 YE  484AR 484ML 484NL 482 REINFORCING PLATE.  484NR 484  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572116-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 OR  AND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 60000 FH  AS VISIBLE. I: 8200 FC  OR  30900 FH  572116-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 OR  AND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 60000 FH  AS VISIBLE. I: 7300 FC  OR  27500 FH  572116-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 OR  AND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 26000 FH  AS VISIBLE. I: 7900 FC  OR  15800 FH  572116-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 OR  AND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR 65000 FH  AS VISIBLE. I: 9100 FC  OR  39600 FH  572117-01-1 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR  632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 60000 FH  633CB 634AB 634CB 632 3, 4 AND 5 I: 10000 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 37800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572117-01-2 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR  632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 60000 FH  633CB 634AB 634CB 632 3, 4 AND 5 I: 9400 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 35500 FH  572117-01-3 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR  632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 26000 FH  633CB 634AB 634CB 632 3, 4 AND 5 I: 10100 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 20200 FH  572117-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  533CB 534AB 534CB 533 SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER OR  632AB 632CB 633AB 534 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 65000 FH  633CB 634AB 634CB 632 3, 4 AND 5 I: 12300 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 53600 FH  572119-01-1 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK I: 6 YE  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR,  BETWEEN RIB 12 AND RIB 23  572119-01-2 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK OR  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 60000 FH  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 7100 FC  BETWEEN RIB 12 AND RIB 23 OR  26800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572119-01-3 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK OR  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 60000 FH  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 7800 FC  BETWEEN RIB 12 AND RIB 23 OR  29400 FH  572119-01-4 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK OR  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 26000 FH  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 8900 FC  BETWEEN RIB 12 AND RIB 23 OR  17800 FH  572119-01-5 533AB 633AB 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK OR  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN 65000 FH  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, I: 9800 FC  BETWEEN RIB 12 AND RIB 23 OR  42400 FH  572120-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT OR  STRINGER 20 IN RIB BAY 22-23 60000 FH  I: 3800 FC  OR  14300 FH  572120-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT OR  STRINGER 20 IN RIB BAY 22-23 60000 FH  I: 3600 FC  OR  13600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572120-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT OR  STRINGER 20 IN RIB BAY 22-23 26000 FH  I: 11300 FC  OR  22600 FH  572120-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE IN AREA OF SKIN JOINT RUNOUT AT OR  STRINGER 20 IN RIB BAY 22-23 65000 FH  I: 5300 FC  OR  23100 FH  572121-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR  541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 60000 FH  541RB 541SB 641GB AND 20 I: 4900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 20000 FH  641PB 641QB 641RB  641SB  572121-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR  541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 60000 FH  541RB 541SB 641GB AND 20 I: 5000 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 20400 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572121-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR  541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 26000 FH  541RB 541SB 641GB AND 20 I: 5400 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 10800 FH  641PB 641QB 641RB  641SB  572121-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR  541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 65000 FH  541RB 541SB 641GB AND 20 I: 9600 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 41600 FH  641PB 641QB 641RB  641SB  572121-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING I: 12 YE  541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13  541RB 541SB 641GB AND 20.  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB  572122-01-1 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 60000 FH  550CB 550DB 550EB 650 I: 8400 FC  550FB 560CB 642AB OR  642BB 642CB 642FB 31700 FH  642GB 642HB 642JB  650AB 650BB 650CB  650DB 650EB 650FB  660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572122-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 60000 FH  550CB 550DB 550EB 650 I: 8800 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 33200 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572122-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 26000 FH  550CB 550DB 550EB 650 I: 9400 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 18800 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572122-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB OR  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 AND 18 65000 FH  550CB 550DB 550EB 650 I: 9600 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 41600 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572122-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB I: 12 YE  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 & 18.  550CB 550DB 550EB 650  550FB 560CB 642AB  642BB 642CB 642FB  642GB 642HB 642JB  650AB 650BB 650CB  650DB 650EB 650FB  660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572122-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB I: 12 YE  542JB 550AB 550BB 642 BAYS 26 TO 28 AND STRINGERS 15 & 18.  550CB 550DB 550EB 650  550FB 642AB 642BB  642CB 642FB 642GB  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572123-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  542HB 542JB 542KB 550 SKIN ACCESS DOORS BETWEEN RIB 27 AND RIB 39 I: 6 YE  550AB 550BB 550CB 642 INCLUDING NACA DUCT DOOR.  550DB 550EB 550FB 650  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  572124-01-1 542AB 560CB 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  660CB 642 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YE  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE  TO BE ADJUSTED BY INDIVIDUAL OPERATORS IN  CONSIDERATION OF THEIR OWN IN-SERVICE  EXPERIENCE AND OPERATIONAL ENVIRONMENT  572124-01-2 542AB 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  642 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YE  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE  TO BE ADJUSTED BY INDIVIDUAL OPERATORS IN  CONSIDERATION OF THEIR OWN IN-SERVICE  EXPERIENCE AND OPERATIONAL ENVIRONMENT  572125-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572125-01-2 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO  484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE  642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FC  OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572125-02-1 I: 12 YE  OR  12300 FC  OR  46400 FH  572125-01-3 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO  484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE  642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FC  OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572125-02-2 I: 12 YE  OR  11900 FC  OR  44900 FH  572125-01-4 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO  484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE  642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FC  OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FH  TASK 572125-02-3 I: 12 YE  OR  13000 FC  OR  26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572125-01-5 454FL 454FR 484FL 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO  484FR 542DB 542EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR I: 12 YE  642DB 642EB JOINTS ON STRINGERS 15 AND 18 13000 FC  OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FH  TASK 572125-02-4 I: 12 YE  OR  13000 FC  OR  65000 FH  572125-02-1 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR  642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 60000 FH  SEALANT REMOVAL AS I: 12300 FC  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-2 46400 FH  572125-02-2 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR  642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 60000 FH  SEALANT REMOVAL AS I: 11900 FC  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-3 44900 FH  572125-02-3 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR  642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 26000 FH  SEALANT REMOVAL AS I: 13000 FC  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-4 26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572125-02-4 454FL 454FR 484FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  484FR 542DB 542EB 642 BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB OR  642DB 642EB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18 65000 FH  SEALANT REMOVAL AS I: 13000 FC  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-5 65000 FH  572126-01-1 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO  642 SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YE I: 12 YE  572126-01-2 N/A TASK DELETED  572126-02-1 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  60000 FH  I: 6300 FC  OR  23800 FH  572126-02-2 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  60000 FH  I: 7600 FC  OR  28700 FH  572126-02-3 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  26000 FH  I: 8800 FC  OR  17600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572126-02-4 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  65000 FH  I: 10600 FC  OR  46000 FH  572127-01-1 550AB 650AB 550 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  650 UPPER SURFACE BETWEEN RIB 33 AND RIB 34. I: 6 YE  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE  TO BE ADJUSTED BY INDIVIDUAL OPERATORS IN  CONSIDERATION OF THEIR OWN IN-SERVICE  EXPERIENCE AND OPERATIONAL ENVIRONMENT  572128-01-1 542CB 560CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  660CB 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB OR  SEALANT REMOVAL AS BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 60000 FH  PER NTM I: 8800 FC  OR  38500 FH  572128-01-2 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB OR  PER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 60000 FH  I: 5300 FC  OR  23200 FH  572128-01-3 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB OR  PER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 26000 FH  I: 6000 FC  OR  12000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572128-01-4 542CB 642CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 642 BOTTOM SKIN AT HOT FUEL RECIRCULATION HOLE IN RIB OR  PER NTM BAY 25-26 BETWEEN FRONT SPAR AND STRINGER 12 65000 FH  I: 13000 FC  OR  65000 FH  572129-01-1 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23 OR  60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FC  TASK 572129-02-1 OR  23000 FH  572129-01-2 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23 OR  60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6000 FC  TASK 572129-02-2 OR  22600 FH  572129-02-1 541SB 641SB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND OR  PER NTM RIB 23 60000 FH  I: 6100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572129-01-1 23000 FH  572129-02-2 541SB 641SB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND OR  PER NTM RIB 23 60000 FH  I: 6000 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572129-01-2 22600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572130-01-1 542AB 560CB 642AB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  660CB 642 SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24 OR  60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8400 FC  TASK 572130-02-1 OR  31700 FH  572130-01-2 542AB 642AB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642 SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24 OR  60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8800 FC  TASK 572130-02-2 OR  33200 FH  572130-02-1 542AB 560CB 642AB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  660CB 642 BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND OR  SEALANT REMOVAL AS RIB 24 60000 FH  PER NTM I: 8400 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572130-01-1 31700 FH  572130-02-2 542AB 642AB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 642 BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND OR  PER NTM RIB 24 60000 FH  I: 8800 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572130-01-2 33200 FH  572131-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572131-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND OR  REAR SPAR BETWEEN RIB 12 AND RIB 27 60000 FH  I: 4200 FC  OR  22300 FH  572131-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27 26000 FH  I: 5300 FC  OR  10600 FH  572131-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27 65000 FH  I: 6100 FC  OR  28100 FH  572132-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 TO RIB 39 60000 FH  I: 4200 FC  OR  22300 FH  572132-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 27 TO RIB 39 26000 FH  I: 4900 FC  OR  9800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572132-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 27 TO RIB 39 65000 FH  I: 6100 FC  OR  28100 FH  572133-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT OR  SPAR TO REAR SPAR. 60000 FH  I: 4200 FC  OR  22300 FH  572133-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT OR  SPAR TO REAR SPAR 60000 FH  I: 4100 FC  OR  22000 FH  572133-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 26000 FH  I: 5300 FC  OR  10600 FH  572133-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 13000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 65000 FH  I: 6300 FC  OR  29000 FH  572133-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO  600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT I: 6 YE  SPAR TO REAR SPAR.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572134-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR 60000 FH  I: 7100 FC  OR  37900 FH  572134-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR 60000 FH  I: 6900 FC  OR  36500 FH  572134-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR 26000 FH  I: 8900 FC  OR  17800 FH  572134-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR 65000 FH  I: 6300 FC  OR  29000 FH  572134-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT I: 6 YE  SPAR TO REAR SPAR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572135-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 60000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 6300 FC  OR  33600 FH  572135-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 60000 FH  AT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 6300 FC  OR  33600 FH  572135-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 26000 FH  AT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 8200 FC  OR  16400 FH  572135-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT 65000 FH  AT STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 13000 FC  OR  65000 FH  572138-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR  60000 FH  I: 9800 FC  OR  51900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572138-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR  60000 FH  I: 9800 FC  OR  51900 FH  572138-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR  26000 FH  I: 13000 FC  OR  26000 FH  572138-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA. OR  65000 FH  I: 13000 FC  OR  65000 FH  572139-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  60000 FH  I: 10800 FC  OR  57500 FH  572139-01-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  60000 FH  I: 10800 FC  OR  57500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572139-01-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  26000 FH  I: 13000 FC  OR  26000 FH  572139-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  65000 FH  I: 13000 FC  OR  65000 FH  572140-01-1 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 60000 FH  541PB 541QB 541RB I: 11100 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 59300 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-01-2 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 60000 FH  541PB 541QB 541RB I: 7000 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 37100 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572140-01-3 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 26000 FH  541PB 541QB 541RB I: 8200 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 16400 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND STR 19 AND ALL STRINGER JOINTS 65000 FH  541PB 541QB 541RB I: 9800 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 45100 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-02-1 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  541HB 541JB 541KB 641 STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING I: 12 YE  541LB 541MB 541NB BUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGER  541PB 541QB 541RB JOINTS.  541SB 641EB 641FB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572141-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572141-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 60000 FH  542KB 550AB 550BB 650 I: 6100 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 32300 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  572141-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 26000 FH  542KB 550AB 550BB 650 I: 7600 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 15200 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  572141-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 13000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24 65000 FH  542KB 550AB 550BB 650 I: 13000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 65000 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572141-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  542DB 542EB 542FB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING I: 12 YE  542GB 542HB 542JB 642 BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT IN  542KB 550AB 550BB 650 RIB BAY 23-24.  550CB 550DB 550EB  550FB 560CB 642AB  642BB 642CB 642DB  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  660CB  572141-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  542DB 542EB 542FB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING I: 12 YE  542GB 542HB 542JB 642 BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT IN  542KB 550AB 550BB 650 RIB BAY 23-24.  550CB 550DB 550EB  550FB 642AB 642BB  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  572142-01-1 N/A TASK DELETED  572143-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572144-01-1 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  60000 FH  I: 4900 FC  OR  27000 FH  572144-01-2 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 13000 FC  642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27 OR  60000 FH  I: 4900 FC  OR  27000 FH  572144-01-3 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 13000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27 OR  26000 FH  I: 6900 FC  OR  13800 FH  572144-01-4 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 13000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27 OR  65000 FH  I: 13000 FC  OR  65000 FH  572144-02-1 542EB 642EB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YE  572145-01-1 542BB 542CB 542DB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  560CB 642BB 642CB 642 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YE  642DB 660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572145-01-2 542BB 542CB 542DB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  642BB 642CB 642DB 642 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YE  572147-01-1 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  641 MANUAL REFUELING APERTURE REINFORCING PLATE IN RIB I: 12 YE  BAY 22-23  572148-01-1 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR  60000 FH  I: 12300 FC  OR  46400 FH  572148-01-2 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR  60000 FH  I: 11900 FC  OR  44900 FH  572148-01-3 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR  26000 FH  I: 13000 FC  OR  26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572148-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS OR  65000 FH  I: 13000 FC  OR  65000 FH  572148-02-1 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  642EB 642 STRINGERS IN RIB BAYS 26 TO 28 INCLUDING BUTTSTRAPS. I: 12 YE  572149-01-1 560CB 660CB 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YE  AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 60000 FH  SPAR, BETWEEN RIBS 23 AND 39 I: 8500 FC  OR  32100 FH  572149-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YE  AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 60000 FH  SPAR, BETWEEN RIBS 23 AND 39 I: 8200 FC  OR  30900 FH  572149-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YE  AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 26000 FH  SPAR, BETWEEN RIBS 23 AND 39 I: 9400 FC  OR  18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572149-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 13000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YE  AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 65000 FH  SPAR, BETWEEN RIBS 23 AND 39 I: 9800 FC  OR  42400 FH  572151-01-1 560DB 574AT 574BB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE  574CB 574DB 574EB 674 AFT FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YE  574FB 574GB 574HB  574JB 574KB 574LB  574MB 574NB 660DB  674AT 674BB 674CB  674DB 674EB 674FB  674GB 674HB 674JB  674KB 674LB 674MB  674NB  572151-01-2 574AT 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE  574DB 574EB 574FB 674 AFT FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YE  574GB 574HB 574JB  574KB 574LB 574MB  574NB 674AT 674BB  674CB 674DB 674EB  674FB 674GB 674HB  674JB 674KB 674LB  674MB 674NB  572152-01-1 574AT 575AT 575BT 575 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE  591AB 591BB 591CB 675 AFT FACE BETWEEN RIB 27 AND RIB 39. I: 12 YE I: 12 YE  591DB 592AB 592BB  592CB 592DB 674AT  675AT 675BT 691AB  691BB 691CB 691DB  692AB 692BB 692CB  692DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572153-01-1 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  575 JOINT PLATE AT RIB 27. OR I: 12 YE  674 13000 FC  675 OR  60000 FH  I: 12 YE  OR  7100 FC  OR  31200 FH  572153-01-2 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  575 JOINT PLATE AT RIB 27. OR I: 12 YE  674 13000 FC  675 OR  60000 FH  I: 12 YE  OR  5400 FC  OR  23800 FH  572153-01-3 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  575 JOINT PLATE AT RIB 27. OR I: 12 YE  674 13000 FC  675 OR  26000 FH  I: 12 YE  OR  5400 FC  OR  10800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572153-01-4 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  575 JOINT PLATE AT RIB 27. OR I: 12 YE  674 13000 FC  675 OR  65000 FH  I: 12 YE  OR  9400 FC  OR  42400 FH  572154-01-1 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YE  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FC  541QB 541RB 541SB 642 OR  542AB 542BB 542CB 60000 FH  542DB 542EB 542GB I: 12 YE  560CB 641FB 641GB OR  641HB 641JB 641KB 7300 FC  641LB 641MB 641NB OR  641PB 641QB 641RB 32100 FH  641SB 642AB 642BB  642CB 642DB 642EB  642GB 660CB  572154-01-2 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YE  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FC  541QB 541RB 541SB 642 OR  542AB 542BB 542CB 60000 FH  542DB 542EB 542GB I: 12 YE  641FB 641GB 641HB OR  641JB 641KB 641LB 6200 FC  641MB 641NB 641PB OR  641QB 641RB 641SB 27400 FH  642AB 642BB 642CB  642DB 642EB 642GB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572154-01-3 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR I: 12 YE  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 13000 FC  541QB 541RB 541SB 642 OR  542AB 542BB 542CB 26000 FH  542DB 542EB 542GB I: 12 YE  641FB 641GB 641HB OR  641JB 641KB 641LB 6200 FC  641MB 641NB 641PB OR  641QB 641RB 641SB 12400 FH  642AB 642BB 642CB  642DB 642EB 642GB  N 572154-01-4 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND I: 12 YE I: 12 YE  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.  541QB 541RB 541SB 642  542AB 542BB 542CB  542DB 542EB 542GB  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  572155-01-1 542HB 542JB 542KB 542 DETAILED INSPECTION OF OUTER WING REAR SPAR T: 12 YE T: 20 YE NO  550AB 550BB 550CB 550 FORWARD FACE BETWEEN RIB 30 AND RIB 39. I: 12 YE I: 12 YE  550DB 550EB 550FB 642  642HB 642JB 642KB 650  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572156-01-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 60000 FH  PER NTM I: 7100 FC  OR  31200 FH  572156-01-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 60000 FH  PER NTM I: 5400 FC  OR  23800 FH  572156-01-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 26000 FH  PER NTM I: 5400 FC  OR  10800 FH  572156-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 65000 FH  PER NTM I: 11700 FC  OR  53000 FH  572158-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23 60000 FH  541RB 541SB 641GB I: 6900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 27900 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572158-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23 60000 FH  541RB 541SB 641GB I: 6900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 27900 FH  641PB 641QB 641RB  641SB  572158-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23 60000 FH  541RB 541SB 641GB I: 7300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 29400 FH  641PB 641QB 641RB  641SB  572158-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23 26000 FH  541RB 541SB 641GB I: 7800 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 15600 FH  641PB 641QB 641RB  641SB  572158-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23 65000 FH  541RB 541SB 641GB I: 6400 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 27900 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572158-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND I: 12 YE  541NB 541PB 541QB RIB 23.  541RB 541SB 641GB  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB  572159-01-1 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR  642CB 660CB 60000 FH  I: 6900 FC  OR  27900 FH  572159-01-2 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR  642CB 660CB 60000 FH  I: 6900 FC  OR  27900 FH  572159-01-3 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR  60000 FH  I: 7300 FC  OR  29400 FH  572159-01-4 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR  26000 FH  I: 7800 FC  OR  15600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572159-01-5 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26 OR  65000 FH  I: 6400 FC  OR  27900 FH  572159-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  560CB 642AB 642BB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. I: 12 YE  642CB 660CB  572159-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. I: 12 YE  572161-01-1 522EB 522FB 522GB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  522HB 522JB 522KB 523 FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. I: 6 YE I: 6 YE  522LB 522MB 522NB 622  522PB 522QB 522RB 623  522SB 522TB 523AB  523BB 523CB 523DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 622RB  622SB 622TB 623AB  623BB 623CB 623DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572161-01-2 522EB 522FB 522GB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  522HB 522JB 522KB 523 FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. I: 6 YE I: 6 YE  522LB 522MB 522NB 622  522PB 522QB 522RB 623  522SB 522TB 523AB  523BB 523CB 523DB  560AB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622QB  622RB 622SB 622TB  623AB 623BB 623CB  623DB 660AB  572162-01-1 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  623 FORWARD FACE SPAR JOINT PLATE AT RIB 27. OR  60000 FH  I: 6900 FC  OR  30300 FH  572162-01-2 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 13000 FC  623 FORWARD FACE SPAR JOINT PLATE AT RIB 27 OR  60000 FH  I: 6600 FC  OR  28800 FH  572162-01-3 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 13000 FC  623 FACE SPAR JOINT PLATE AT RIB 27. OR  26000 FH  I: 8900 FC  OR  17800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572162-01-4 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 13000 FC  623 FACE SPAR JOINT PLATE AT RIB 27. OR  65000 FH  I: 13000 FC  OR  65000 FH  572162-01-5 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  623 FACE SPAR JOINT PLATE AT RIB 27. I: 6 YE I: 6 YE  572163-01-1 523EB 523FB 523GB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 12 YE T: 20 YE  523HB 523JB 523KB 623 FORWARD FACE BETWEEN RIB 27 AND RIB 39. I: 6 YE I: 6 YE  523LB 523MB 523NB  623EB 623FB 623GB  623HB 623JB 623KB  623LB 623MB 623NB  572164-01-1 N/A TASK DELETED  572164-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE  541NB 541PB 541QB 641 FLANGES 13000 FC  541RB 541SB 542AB 642 OR  542BB 542CB 542DB 60000 FH  560CB 641GB 641HB I: 12 YE  641JB 641KB 641LB OR  641MB 641NB 641PB 4300 FC  641QB 641RB 641SB OR  642AB 642BB 642CB 18800 FH  642DB 660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572164-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE  541NB 541PB 541QB 641 FLANGES 13000 FC  541RB 541SB 542AB 642 OR  542BB 542CB 542DB 60000 FH  641GB 641HB 641JB I: 12 YE  641KB 641LB 641MB OR  641NB 641PB 641QB 4600 FC  641RB 641SB 642AB OR  642BB 642CB 642DB 20300 FH  572164-01-4 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE  541NB 541PB 541QB 641 FLANGES 13000 FC  541RB 541SB 542AB 642 OR  542BB 542CB 542DB 26000 FH  641GB 641HB 641JB I: 12 YE  641KB 641LB 641MB OR  641NB 641PB 641QB 6300 FC  641RB 641SB 642AB OR  642BB 642CB 642DB 12600 FH  572164-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE  541NB 541PB 541QB 641 FLANGES  541RB 541SB 542AB 642  542BB 542CB 542DB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572164-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR I: 12 YE  541NB 541PB 541QB 641 FLANGES 13000 FC  541RB 541SB 542AB 642 OR  542BB 542CB 542DB 65000 FH  641GB 641HB 641JB I: 12 YE  641KB 641LB 641MB OR  641NB 641PB 641QB 8100 FC  641RB 641SB 642AB OR  642BB 642CB 642DB 36500 FH  572165-01-1 N/A TASK DELETED  572165-01-2 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE  550AB 550BB 550CB 642 FLANGES 13000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 60000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 4300 FC  OR  18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572165-01-3 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE  550AB 550BB 550CB 642 FLANGES 13000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 60000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 4600 FC  OR  20300 FH  572165-01-4 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE  550AB 550BB 550CB 642 FLANGES 13000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 26000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 6300 FC  OR  12600 FH  572165-01-5 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE  550AB 550BB 550CB 642 FLANGES  550DB 550EB 550FB 650  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572165-01-6 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO  542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE  550AB 550BB 550CB 642 FLANGES 13000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 65000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 13000 FC  OR  65000 FH  572166-01-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 60000 FH  PER NTM I: 6900 FC  OR  30300 FH  572166-01-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 60000 FH  PER NTM I: 6600 FC  OR  28800 FH  572166-01-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 26000 FH  PER NTM I: 8900 FC  OR  17800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572166-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 FRONT SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT OR  SEALANT REMOVAL AS RIB 27 65000 FH  PER NTM I: 13000 FC  OR  65000 FH  572171-01-1 541HB 541JB 541KB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB T: 12 YE T: 20 YE NO  541LB 541MB 541NB 542 39, AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION I: 12 YE I: 12 YE  541PB 541QB 541RB 550 OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 AND 26  541SB 542AB 542BB 641  542CB 542DB 542EB 642  542FB 542GB 542HB 650  542JB 542KB 550AB  550BB 550CB 550DB  550EB 550FB 560CB  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB 642AB 642BB  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB 660CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572171-01-2 541HB 541JB 541KB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB T: 12 YE T: 20 YE NO  541LB 541MB 541NB 542 39, AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION I: 12 YE I: 12 YE  541PB 541QB 541RB 550 OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 AND 26  541SB 542AB 542BB 641  542CB 542DB 542EB 642  542FB 542GB 542HB 650  542JB 542KB 550AB  550BB 550CB 550DB  550EB 550FB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642FB  642GB 642HB 642JB  642KB 650AB 650BB  650CB 650DB 650EB  650FB  572172-01-1 542CB 542DB 560CB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 12 YE T: 20 YE NO  642CB 642DB 660CB 642 26 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YE I: 12 YE  572172-01-2 542CB 542DB 642CB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB T: 12 YE T: 20 YE NO  642DB 642 26 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YE I: 12 YE  572173-01-1 560AB 560BB 560CB 560 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 10 YE  560DB 660AB 660BB 660 LOWER SURFACE COVERED BY PLASTRON FAIRING I: 10 YE  660CB 660DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572173-02-1 560AB 560BB 560CB 560 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  560DB 660AB 660BB 660 SKIN LOWER SURFACE COVERED BY PLASTRON OR  660CB 660DB FAIRING 60000 FH  I: 10100 FC  OR  38100 FH  572174-01-1 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO  541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YE  641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FC  641NB 641SB 642AB 642 OR  60000 FH  I: 12 YE  OR  5400 FC  OR  23900 FH  572174-01-2 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO  541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YE  641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FC  641NB 641SB 642AB 642 OR  60000 FH  I: 12 YE  OR  6100 FC  OR  26700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572174-01-3 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO  541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YE  641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FC  641NB 641SB 642AB 642 OR  26000 FH  I: 12 YE  OR  7200 FC  OR  14400 FH  572174-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO  642EB 642 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YE  SEALANT REMOVAL AS CUTOUTS AND FORWARD FLAP TRACK BRACKETS 13000 FC  PER NTM OR  65000 FH  I: 12 YE  OR  13000 FC  OR  65000 FH  572180-01-1 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541KB 541LB 541MB 641 SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB OR  541NB 541PB 541QB 23 60000 FH  541RB 541SB 641GB I: 5000 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 20600 FH  641PB 641QB 641RB  641SB  572180-01-2 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  541KB 541LB 541MB 641 SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB OR  541NB 541PB 541QB 23 60000 FH  541RB 541SB 641GB I: 5500 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 22600 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572180-01-3 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23 OR  541NB 541PB 541QB 26000 FH  541RB 541SB 641GB I: 5900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 11800 FH  641PB 641QB 641RB  641SB  572180-02-1 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. I: 12 YE  541NB 541PB 541QB  541RB 541SB 641GB  641HB 641JB 641KB  641LB 641MB 641NB  641PB 641QB 641RB  641SB  572181-01-1 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  560CB 642AB 642BB 642 SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB OR  642CB 660CB 26 60000 FH  I: 5000 FC  OR  18900 FH  572181-01-2 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  642AB 642BB 642CB 642 SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB OR  26 60000 FH  I: 5500 FC  OR  20700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572181-01-3 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26 OR  26000 FH  I: 5900 FC  OR  11800 FH  572181-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26 OR  65000 FH  I: 7400 FC  OR  32000 FH  572181-02-1 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  560CB 642AB 642BB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. I: 12 YE  642CB 660CB  572181-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. I: 12 YE  572182-01-1 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR  550BB 550CB 550DB 642 39 60000 FH  550EB 550FB 642FB 650 I: 12800 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 48300 FH  650CB 650DB 650EB  650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572182-01-2 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR  550BB 550CB 550DB 642 39 60000 FH  550EB 550FB 642FB 650 I: 12500 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 47200 FH  650CB 650DB 650EB  650FB  572182-01-3 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR  550BB 550CB 550DB 642 39 26000 FH  550EB 550FB 642FB 650 I: 13000 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 26000 FH  650CB 650DB 650EB  650FB  572182-01-4 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  542JB 542KB 550AB 550 SKIN STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB OR  550BB 550CB 550DB 642 39 65000 FH  550EB 550FB 642FB 650 I: 7400 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 32000 FH  650CB 650DB 650EB  650FB  572182-02-1 542FB 542GB 542HB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. I: 12 YE  550BB 550CB 550DB 642  550EB 550FB 642FB 650  642GB 642HB 642JB  642KB 650AB 650BB  650CB 650DB 650EB  650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572183-01-1 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS 60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12800 FC  TASK 572183-02-1 OR  48300 FH  572183-01-2 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS 60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12500 FC  TASK 572183-02-2 OR  47200 FH  572183-01-3 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS 26000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FC  TASK 572183-02-3 OR  26000 FH  572183-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS 65000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7400 FC  TASK 572183-02-4 OR  32000 FH  572183-02-1 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND OR  SEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 60000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12800 FC  TASK 572183-01-1 OR  48300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572183-02-2 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND OR  SEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 60000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 12500 FC  TASK 572183-01-2 OR  47200 FH  572183-02-3 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND OR  SEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 26000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FC  TASK 572183-01-3 OR  26000 FH  572183-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  642EB 642 BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND OR  SEALANT REMOVAL AS 28 INCLUDING STRINGER JOINTS 65000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7400 FC  TASK 572183-01-4 OR  32000 FH  572183-03-1 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING I: 12 YE  STRINGER JOINTS.  572184-01-1 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572184-02-1 I: 6100 FC  OR  23000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572184-01-2 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60000 FH  TASK 572184-02-2 I: 6000 FC  OR  22600 FH  572184-01-3 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FH  TASK 572184-02-3 I: 6400 FC  OR  12800 FH  572184-01-4 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FH  TASK 572184-02-4 I: 13000 FC  OR  65000 FH  572184-02-1 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND OR  PER NTM RIB 21 60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FC  TASK 572184-01-1 OR  23000 FH  572184-02-2 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  SEALANT REMOVAL AS 641 BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND OR  PER NTM RIB 21 60000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6000 FC  TASK 572184-01-2 OR  22600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572184-02-3 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 26000 FH  TASK 572184-01-3 I: 6400 FC  OR  12800 FH  572184-02-4 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 13000 FC  SEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21 OR  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 65000 FH  TASK 572184-01-4 I: 13000 FC  OR  65000 FH  572201-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE  600 SKIN LOWER SURFACE BETWEEN RIB 1 AND RIB 12 I: 6 YE  FROM FRONT TO REAR SPAR EXCLUDING AREAS COVERED  BY INBOARD PYLON FAIRING AND REINFORCING PLATE,  MAIN LANDING GEAR REINFORCING PLATE AND FLAP  TRACK 2 FAIRING.  572202-01-1 PYLON FAIRINGS 460 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  470 SKIN LOWER SURFACE VISIBLE PORTION OF INBOARD I: 12 YE  PYLON REINFORCING PLATE AND LOWER SKIN UNDER  PYLON FAIRING.  572203-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE  600 SKIN MAIN LANDING GEAR REINFORCING PLATE LOWER I: 6 YE  SURFACE.  572204-01-1 FLAP TRACK FAIRINGS 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE  631 SKIN IN AREA COVERED BY FLAP TRACK 2 FAIRING. I: 6 YE  572205-01-1 541AB 541BB 542AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO  542BB 542CB 542DB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 12 YE I: 12 YE  641AB 641BB 642AB 641 IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 & 11-12.  642BB 642CB 642DB 642  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572206-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE  600 SURFACE AT MLI HOLES AND DRAIN HOLES AFT OF FRONT I: 6 YE  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.  572207-01-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN VISIBLE T: 6 YE NO  600 SURFACES OF FUEL PUMP APERTURES IN RIB BAYS I: 6 YE  3-4 AND 5-6.  572208-01-1 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  542AB 542AZ 542BZ 542 UPPER SURFACE, INCLUDING STRINGERS AND BUTTSTRAPS, I: 6 YE  542DB 641AB 641AZ 641 BETWEEN RIB 1 AND RIB 3 FROM FRONT SPAR TO REAR SPAR,  641BZ 642AB 642AZ 642 BETWEEN RIB 5 AND RIB 7 FROM CENTER SPAR TO REAR SPAR  642BZ 642DB AND BETWEEN RIB 11 AND 12 FROM FRONT SPAR TO CENTER  SPAR.  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE  ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF  THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL  ENVIRONMENT  572209-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541BZ 541CZ 542AB 542 STRINGERS BETWEEN RIB 1 & RIB 12, INCLUDING STRINGER I: 12 YE  542AZ 542BB 542BZ 641 JOINTS, BUTTSTRAPS, JOINT FITTINGS AND ROOT JOINT  542CB 542CZ 542DB 642 FITTINGS.  542DZ 542EZ 641AB  641AZ 641BB 641BZ  641CZ 642AB 642AZ  642BB 642BZ 642CB  642CZ 642DB 642DZ  642EZ  572231-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM I: 6 YE  FRONT TO REAR SPAR.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572232-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  541BZ 541CZ 542AB 542 STRINGERS BETWEEN RIB 1 AND RIB 12, INCLUDING I: 12 YE  542AZ 542BB 542BZ 641 STRINGER JOINTS, BUTTSTRAPS, JOINT FITTINGS AND ROOT  542CB 542CZ 542DB 642 JOINT FITTINGS.  542DZ 542EZ 641AB  641AZ 641BB 641BZ  641CZ 642AB 642AZ  642BB 642BZ 642CB  642CZ 642DB 642DZ  642EZ  572233-01-1 542BB 542CB 542CZ 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  542DB 542DZ 542EZ 642 REINFORCING PLATE LOWER SURFACE AT INNER PYLON. I: 12 YE  642BB 642CB 642CZ  642DB 642DZ 642EZ  572241-01-1 573BB 573FB 673BB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE  673FB 573 AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER I: 12 YE  FLAPS EXTENDED 671 AND LOWER ATTACHMENT ANGLES AND JOINT PLATE  673 AT RIB 9.  572244-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  641 FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YE  572245-01-1 541AB 541BB 542AB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO  542BB 542CB 542DB 542 FORWARD FACE BETWEEN RIB 1 AND RIB 12 INCLUDING TOP I: 12 YE  641AB 641BB 642AB 641 AND BOTTOM FLANGES AND BOLTING.  642BB 642CB 642DB 642  572261-01-1 521AB 521BB 521CB 521 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE  521DB 521EB 521FB 522 FORWARD FACE BETWEEN RIB 1 AND RIB 12. I: 6 YE  521GB 521HB 522AB 621  522BB 522CB 621AB 622  621BB 621CB 621DB  621EB 621FB 621GB  621HB 622AB 622BB  622CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572263-01-1 541AZ 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO  541CZ 542AB 542AZ 542 AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING TOP I: 12 YE  542BB 542BZ 542CB 641 AND BOTTOM FLANGES.  542CZ 542DB 542DZ 642  641AZ 641BB 641BZ  641CZ 642AB 642AZ  642BB 642BZ 642CB  642CZ 642DB 642DZ  572264-01-1 522EB 622EB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  622 FACE JOINT PLATE AT RIB 12. I: 12 YE I: 12 YE  572271-01-1 542AB 542AZ 542BZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6, T: 12 YE NO  642AB 642AZ 642BZ 642 FORWARD AND AFT OF CENTER SPAR, AT SKIN ATTACHMENTS I: 12 YE  (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.  572272-01-1 542AB 542BZ 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7, T: 12 YE NO  642BZ 642 FORWARD AND AFT OF CENTER SPAR, AT SKIN I: 12 YE  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT  SURROUNDS.  572273-01-1 542BB 542CB 542CZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 8 T: 12 YE NO  642BB 642CB 642CZ 642 AND 9, FORWARD AND AFT OF CENTER SPAR, AT SKIN I: 12 YE  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT  SURROUNDS. FORWARD FLAP TRACK BRACKET.  572274-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 2, T: 12 YE NO  541BZ 641AB 641AZ 641 3, 4 AND 5, FORWARD AND AFT OF CENTER SPAR, I: 12 YE  641BB 641BZ AT SKIN ATTACHMENTS (INCLUDING CLEATS),  SPAR 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  641AZ 641 UPPER SURFACE OF TRIFORM FITTING BETWEEN FRONT SPAR I: 6 YE I: 6 YE  AND REAR SPAR.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572276-01-1 542CB 542DB 542DZ 542 GENERAL VISUAL INSPECTION OF OUTER WING RIB 10 T: 12 YE NO  542EZ 642CB 642DB 642 FORWARD, RIB 10A AND PYLON DIAPHRAGM. I: 12 YE  642DZ 642EZ  572277-01-1 542AB 542AZ 542BB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 10 T: 12 YE NO  542BZ 542CB 542CZ 642 AFT, 11 AND 12, FORWARD AND AFT OF CENTER SPAR, I: 12 YE  542DB 542DZ 542EB AT SKIN ATTACHMENTS (INCLUDING CLEATS),  542EZ 642AB 642AZ SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS  642BB 642BZ 642CB AND ACCESS CUTOUT SURROUNDS.  642CZ 642DB 642DZ  642EB 642EZ  572281-01-1 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 10 YE T: 20 YE NO  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. I: 10 YE I: 10 YE  572282-01-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING CENTER T: 12 YE NO  541BZ 542AB 542AZ 542 SPAR BETWEEN RIB 2 AND RIB 11 FORWARD I: 12 YE  542BB 542BZ 542CB 641 AND AFT FACES INCLUDING SKIN ATTACHMENTS,  542CZ 542DB 542DZ 642 RIB ATTACHMENTS, AREA AROUND ACCESS HOLES,  542EZ 641AB 641AZ DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.  641BB 641BZ 642AB  642AZ 642BB 642BZ  642CB 642CZ 642DB  642DZ 642EZ  572283-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO  641 ASSEMBLY AFT FACE BETWEEN RIB 1 AND RIB 2. I: 12 YE I: 12 YE  572285-01-1 191BT 192BT 192CT 191 DETAILED INSPECTION OF OUTER WING BOX, T: 12 YE 1  195CT 192 CRUCIFORM FITTING OUTBOARD FLANGE UPPER SURFACE AS I: 12 YE  195 FAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RH.  572301-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE  600 SKIN LOWER SURFACE BETWEEN RIB 12 AND RIB 27 I: 6 YE  FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS  COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 AND  OUTBOARD PYLON FAIRING.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572302-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE  600 SKIN LOWER SURFACE BETWEEN RIB 27 AND RIB 41 I: 12 YE  FROM FRONT SPAR TO REAR SPAR.  572303-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  542HB 542JB 542KB 642 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YE  542LB 542MB 542NB IN ALL BAYS BETWEEN RIBS 12 AND 21 AND BETWEEN RIBS  642EB 642FB 642GB 21 AND 22 FWD.  642HB 642JB 642KB  642LB 642MB 642NB  572304-01-1 542PB 542QB 542SB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  543AB 543BB 543CB 543 AND I: 6 YE  543DB 543EB 543FB 550 LOWER SURFACE AROUND ACCESS DOOR CUTOUTS, INCLUDING  543GB 543HB 543JB 642 NACA DUCT, IN ALL BAYS BETWEEN RIBS 21 AND 22 AFT AND  543KB 543LB 543MB 643 BETWEEN RIBS 22 AND 41.  543NB 543PB 543QB 650  543RB 543SB 543TB  543UB 543VB 550AB  550BB 550CB 550DB  550EB 550FB 642PB  642QB 642SB 643AB  643BB 643CB 643DB  643EB 643FB 643GB  643HB 643JB 643KB  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB 650AB 650BB  650CB 650DB 650EB  650FB  572305-01-1 FLAP TRACK FAIRINGS 450 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  OUTBOARD PYLON 480 SKIN LOWER SURFACE IN AREAS COVERED BY FLAP I: 6 YE  FAIRINGS 532 TRACK FAIRINGS 3, 4, 5 AND OUTBOARD PYLON FAIRING.  533  534  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572306-01-1 PYLON FAIRINGS 450 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 12 YE NO  480 SKIN LOWER SURFACE AT FRONT SPAR VISIBLE I: 12 YE  PORTION OF OUTBOARD PYLON REINFORCING PLATE.  572307-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE  600 LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK I: 6 YE  CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN  HOLES AFT OF FRONT SPAR AND FORWARD OF REAR  SPAR BETWEEN RIBS 12 AND 41.  572308-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  542HB 542JB 542KB 642 STRINGERS BETWEEN RIB 12 AND RIB 23, INCLUDING I: 12 YE  542LB 542MB 542NB STRINGER JOINTS, BUTTSTRAPS AND JOINT FITTINGS.  542PB 542QB 542RB  542SB 642EB 642FB  642GB 642HB 642JB  642KB 642LB 642MB  642NB 642PB 642QB  642RB 642SB  572309-01-1 543AB 543BB 543CB 543 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  543DB 543EB 543FB 550 STRINGERS BETWEEN RIB 23 AND RIB 41, INCLUDING I: 12 YE  543GB 543HB 543JB 643 STRINGER JOINTS, BUTTSTRAPS AND JOINT FITTINGS.  543KB 543LB 543MB 650  543NB 543PB 543QB  543RB 543SB 543TB  543UB 543VB 550AB  550BB 550CB 550DB  550EB 550FB 643AB  643BB 643CB 643DB  643EB 643FB 643GB  643HB 643JB 643KB  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB 650AB 650BB  650CB 650DB 650EB  650FB  VENT PIPES DISPLACED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572310-01-1 542PB 542QB 542SB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ACCESS T: 12 YE T: 20 YE NO  543AB 543BB 543CB 543 DOORS BETWEEN RIBS 21 AND 22 AFT AND BETWEEN RIBS 22 I: 12 YE I: 12 YE  543DB 543EB 543FB 550 AND 41 INCLUDING NACA DUCT DOOR  543GB 543HB 543JB 642  543KB 543LB 543MB 643  543NB 543PB 543QB 650  543RB 543SB 543TB  543UB 543VB 550AB  550BB 550CB 550DB  550EB 550FB 642PB  642QB 642SB 643AB  643BB 643CB 643DB  643EB 643FB 643GB  643HB 643JB 643KB  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB 650AB 650BB  650CB 650DB 650EB  650FB  572311-01-1 543AB 543NB 643AB 543 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  643NB 643 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YE  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE  ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF  THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL  ENVIRONMENT  572312-01-1 550AB 650AB 550 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  650 UPPER SURFACE BETWEEN RIB 35 AND RIB 36. I: 6 YE  NOTE: TASK INTERVAL MAY BE INFLUENCED BY  MICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BE  ADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OF  THEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONAL  ENVIRONMENT  572331-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 12 AND RIB 41 I: 6 YE  FROM FRONT SPAR TO REAR SPAR.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572332-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  542HB 542JB 542KB 642 STRINGERS BETWEEN RIB 12 AND RIB 23 INCLUDING I: 12 YE  542LB 542MB 542NB BUTTSTRAPS AND ALL STRINGER JOINTS.  542PB 542QB 642EB  642FB 642GB 642HB  642JB 642KB 642LB  642MB 642NB 642PB  642QB  572333-01-1 543AB 543BB 543CB 543 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  543DB 543EB 543FB 550 STRINGERS BETWEEN RIB 23 AND RIB 41 INCLUDING I: 12 YE  543GB 543HB 543JB 643 BUTTSTRAPS AND ALL STRINGER JOINTS.  543KB 543LB 543MB 650  543NB 543PB 543QB  543RB 543SB 543TB  543UB 543VB 550AB  550BB 550CB 550DB  550EB 550FB 643AB  643BB 643CB 643DB  643EB 643FB 643GB  643HB 643JB 643KB  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB 650AB 650BB  650CB 650DB 650EB  650FB  VENT PIPES DISPLACED  572334-01-1 543NB 543PB 543QB 543 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  643NB 643PB 643QB 643 REINFORCING PLATE LOWER SURFACE AT OUTER PYLON. I: 12 YE  OUTBOARD PYLON  FAIRINGS  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572341-01-1 574AB 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE  574DB 574EB 574FB 674 FACE BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YE  574GB 574HB 574JB  574KB 574LB 574MB  574NB 674AB 674BB  674CB 674DB 674EB  674FB 674GB 674HB  674JB 674KB 674LB  674MB 674NB  572342-01-1 575AB 575BB 575CB 575 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE  575DB 575EB 675AB 675 FACE BETWEEN RIB 27 AND RIB 41. I: 12 YE I: 12 YE  675BB 675CB 675DB  675EB  572343-01-1 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE T: 20 YE  575 FACE SPAR JOINT PLATE AT RIB 27 I: 12 YE I: 12 YE  674  675  572345-01-1 542DB 542EB 542FB 542 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO  542GB 542HB 542JB 543 FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING I: 12 YE  542KB 542LB 542MB 642 TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT  542NB 542PB 542QB 643 RIB 27.  543AB 543BB 543CB  543DB 543EB 543FB  543GB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 642LB  642MB 642NB 642PB  642QB 643AB 643BB  643CB 643DB 643EB  643FB 643GB  VENT PIPES DISPLACED  FROM RIB 23 OUTBOARD  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572346-01-1 543HB 543JB 543KB 543 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  543LB 543MB 550AB 550 FACE BETWEEN RIB 30 AND RIB 41. I: 12 YE I: 12 YE  550BB 550CB 550DB 643  550EB 550FB 643HB 650  643JB 643KB 643LB  643MB 650AB 650BB  650CB 650DB 650EB  650FB  VENT PIPES DISPLACED  572361-01-1 522EB 522GB 522HB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  522KB 522MB 522PB 523 FACE BETWEEN RIB 12 AND RIB 26, AS FAR AS VISIBLE. I: 6 YE I: 6 YE  523AB 523BB 523CB 622  523DB 622EB 622GB 623  622HB 622KB 622MB  622PB 623AB 623BB  623CB 623DB  572362-01-1 523DB 623DB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  623 FACE SPAR JOINT PLATE AT RIB 26. I: 12 YE I: 12 YE  572364-01-1 523DB 523FB 523HB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  523KB 523MB 523PB 623 FACE BETWEEN RIB 26 AND RIB 41. I: 6 YE I: 6 YE  523QB 623DB 623FB  623HB 623KB 623MB  623PB 623QB  572365-01-1 542EB 542FB 542GB 542 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO  542HB 542JB 542KB 543 AFT FACE BETWEEN RIB 12 AND RIB 26 INCLUDING TOP AND I: 12 YE  542LB 542MB 542NB 642 BOTTOM FLANGES.  542RB 542SB 543NB 643  543PB 642EB 642FB  642GB 642HB 642JB  642KB 642LB 642MB  642NB 642RB 642SB  643NB 643PB  VENT PIPES DISPLACED  FROM RIB 23 OUTBOARD  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572366-01-1 543JB 543KB 543LB 543 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT T: 12 YE T: 20 YE NO  543MB 543QB 543RB 550 FACE BETWEEN RIB 26 AND 41 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE  543SB 543TB 543UB 643 FLANGES,  543VB 550AB 550BB 650  550CB 550DB 550EB  550FB 643JB 643KB  643LB 643MB 643QB  643RB 643SB 643TB  643UB 643VB 650AB  650BB 650CB 650DB  650EB 650FB  VENT PIPES DISPLACED  572371-01-1 542FB 542GB 542HB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 14 T: 12 YE NO  542JB 542KB 542LB 543 TO 41 AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND I: 12 YE  542MB 542NB 542PB 550 REGION OF STRINGER CUTOUTS EXCLUDING RIBS 18, 23 & 25  542QB 542RB 542SB 642  543AB 543BB 543CB 643  543DB 543EB 543FB 650  543GB 543HB 543JB  543KB 543LB 543MB  543NB 543PB 543QB  543RB 543SB 543TB  543UB 543VB 550AB  550BB 550CB 550DB  550EB 550FB 642FB  642GB 642HB 642JB  642KB 642LB 642MB  642NB 642PB 642QB  642RB 642SB 643AB  643BB 643CB 643DB  643EB 643FB 643GB  643HB 643JB 643KB  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB 650AB 650BB  650CB 650DB 650EB  650FB  VENT PIPES DISPLACED  FROM RIB 23 OUTBOARD  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572372-01-1 543BB 543CB 543PB 543 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 25 T: 12 YE NO  543QB 643BB 643CB 643 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET. I: 12 YE  643PB 643QB  OUTBOARD PYLON  FAIRINGS  VENT PIPES DISPLACED  FROM RIB 23 OUTBOARD  572373-01-1 542EB 542FB 542KB 542 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 13, T: 12 YE NO  542LB 542QB 542SB 543 18 AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGER I: 12 YE  543AB 543NB 642EB 642 CUTOUTS AND FORWARD FLAP TRACK BRACKETS.  642FB 642KB 642LB 643  642QB 642SB 643AB  643NB  572601-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE  671 LANDING GEAR SIDE STAY FITTING (RIB 2). I: 12 YE  572602-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE  671 LANDING GEAR FORWARD PINTLE FITTING (RIB 5). I: 12 YE  572603-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE  671 LANDING GEAR RETRACTION JACK FITTING. I: 12 YE  572604-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE  671 LANDING GEAR SUPPORT RIB 6. I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572605-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YE  FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FC  INTERFACE PLATE AND THRUST PADS). I: 12 YE  OR  4700 FC  572605-01-2 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YE  FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FC  INTERFACE PLATE AND THRUST PADS). I: 12 YE  OR  5600 FC  572605-01-5 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND OR I: 12 YE  FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, 13000 FC  INTERFACE PLATE AND THRUST PADS). I: 12 YE  OR  13000 FC  572606-01-1 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 T: 13000 FC  632CB 633CB 634CB 533 AND 5 AFT PICK-UP ASSEMBLY I: 13000 FC  534  632  633  634  572606-02-1 532CB 533CB 534CB 532 GENERAL VISUAL INSPECTION OF OUTER WING FLAP TRACKS T: 12 YE  632CB 633CB 634CB 533 3, 4 AND 5 AFT PICK-UP ASSEMBLY I: 12 YE  534  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572607-01-1 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE  532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YE  534AB 534CB 631AB 533 13000 FC  631CB 632AB 632CB 534 I: 12 YE  633AB 633CB 634AB 631 OR  634CB 632 9200 FC  633  634  572607-01-2 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE  532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YE  534AB 534CB 631AB 533 13000 FC  631CB 632AB 632CB 534 I: 12 YE  633AB 633CB 634AB 631 OR  634CB 632 7300 FC  633  634  572607-01-3 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE  532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTING. OR I: 12 YE  534AB 534CB 631AB 533 13000 FC  631CB 632AB 632CB 534 I: 12 YE  633AB 633CB 634AB 631 OR  634CB 632 9200 FC  633  634  572607-02-1 N/A TASK DELETED  572608-01-1 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  522CT 622AB 622AT 622 INNER PYLON INBOARD AND OUTBOARD FORWARD I: 13000 FC  622BB 622CT ATTACHMENT FITTINGS  ENGINE  LINKS  SLEEVES  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572609-01-1 523AB 523AT 523BB 523 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  523CT 523QB 623AB 623 OUTER PYLON INBOARD AND OUTBOARD FORWARD I: 13000 FC  623AT 623BB 623CT ATTACHMENT FITTINGS  623QB  ENGINE  LINKS  SLEEVES  572610-01-1 462GR 462HL 463CL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON SPIGOT T: 12 YE T: 20 YE NO  463CR 464AL 464AR 641 FITTING. I: 12 YE I: 12 YE  472GL 472HR 473CL  473CR 474AL 474AR  SPIGOT SLEEVE  572610-01-3 462GR 462HL 463CL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON SPIGOT T: 12 YE T: 20 YE NO  463CR 464AL 464MR 641 FITTING. I: 12 YE I: 12 YE  472GL 472HR 473CL  473CR 474AL 474MR  SPIGOT SLEEVE  572610-02-1 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FC  464AR 472GL 472HR 641 SPIGOT FITTING I: 13000 FC  474AL 474AR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572610-02-6 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FC  464MR 472GL 472HR 641 SPIGOT FITTING I: 13000 FC  474AL 474MR  572610-02-7 462GR 462HL 464AL 541 SPECIAL DETAILED INSPECTION OF OUTER WING INNER PYLON T: 13000 FC  464MR 472GL 472HR 641 SPIGOT FITTING OR  474AL 474MR 65000 FH  I: 11400 FC  OR  51500 FH  572611-01-1 452EL 452FR 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO  453CR 454AL 454AR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YE  482ER 482FL 483CL  483CR 484AL 484AR  SPIGOT SLEEVE  572611-01-2 452KL 452MR 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO  453CR 454AL 454KR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YE  482MR 482NL 483CL  483CR 484AR 484ML  SPIGOT SLEEVE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572611-01-3 452FR 452GL 453CL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO  453CR 454AL 454AR 642 PYLON SPIGOT FITTING. I: 12 YE I: 12 YE  482FL 482HR 483CL  483CR 484AL 484AR  SPIGOT SLEEVE  572611-02-1 452EL 452FR 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  454AR 482ER 482FL 642 OUTER PYLON SPIGOT FITTING I: 13000 FC  484AL 484AR  572611-02-2 452KL 452MR 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  454KR 482MR 482NL 642 OUTER PYLON SPIGOT FITTING I: 13000 FC  484AR 484ML  572611-02-3 452FR 452GL 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  454AR 482FL 482HR 642 OUTER PYLON SPIGOT FITTING I: 13000 FC  484AL 484AR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572611-02-4 452FR 452GL 454AL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  454AR 482FL 482HR 642 OUTER PYLON SPIGOT FITTING OR  484AL 484AR 65000 FH  I: 11400 FC  OR  51500 FH  572612-01-1 464BL 464BR 464FL 541 DETAILED INSPECTION OF OUTER WING INNER T: 12 YE T: 20 YE NO  464FR 474BL 474BR 641 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  474FL 474FR  PIPE SUPPORT BRACKET  REMOVED OR DISPLACED  572612-01-2 464JL 464JR 464KL 541 DETAILED INSPECTION OF OUTER WING INNER T: 12 YE T: 20 YE NO  464KR 474JL 474JR 641 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  474KL 474KR  PIPE SUPPORT BRACKET  REMOVED OR DISPLACED  572612-02-1 464BL 464BR 464FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  464FR 474BL 474BR 641 INNER PYLON AFT ATTACHMENT FITTING OR  474FL 474FR 60000 FH  PIPE SUPPORT BRACKET I: 13000 FC  REMOVED OR DISPLACED OR  60000 FH  572612-02-13 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING OR  474KL 474KR 65000 FH  PIPE SUPPORT BRACKET I: 13000 FC  REMOVED OR DISPLACED OR  65000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572612-02-2 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING OR  474KL 474KR 26000 FH  PIPE SUPPORT BRACKET I: 13000 FC  REMOVED OR DISPLACED OR  26000 FH  572612-02-3 464JL 464JR 464KL 541 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  464KR 474JL 474JR 641 INNER PYLON AFT ATTACHMENT FITTING OR  474KL 474KR 60000 FH  PIPE SUPPORT BRACKET I: 13000 FC  REMOVED OR DISPLACED OR  60000 FH  572613-01-1 N/A TASK DELETED  572613-01-3 454BL 454BR 454FL 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO  454FR 484BL 484BR 642 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  484FL 484FR  572613-01-4 454BL 454MR 454NR 542 DETAILED INSPECTION OF OUTER WING OUTER T: 12 YE T: 20 YE NO  454QL 484NL 484NR 642 PYLON AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  484PL 484PR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572613-02-1 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING OR  484FL 484FR 60000 FH  I: 13000 FC  OR  60000 FH  572613-02-2 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING OR  484FL 484FR 26000 FH  I: 13000 FC  OR  26000 FH  572613-02-3 454BL 454MR 454NR 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  454QL 484NL 484NR 642 OUTER PYLON AFT ATTACHMENT FITTING OR  484PL 484PR 60000 FH  I: 13000 FC  OR  60000 FH  572613-02-4 452BL 452BR 452FL 542 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  452FR 484BL 484BR 642 OUTER PYLON AFT ATTACHMENT FITTING OR  484FL 484FR 65000 FH  I: 13000 FC  OR  65000 FH  572614-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572614-02-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE  743 HINGED DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YE  572615-01-1 N/A TASK DELETED  572615-02-1 732 742 732 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR LEG T: 6 YE  742 FAIRING ATTACHMENT ASSEMBLIES TO LEG STRUCTURE. I: 6 YE  572616-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING LOWER T: 3 YE  600 SURFACE PLASTRON FAIRING ASSEMBLY (LOWER I: 3 YE  SURFACE)  N 572617-01-1 734 744 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE  671 SUPPORT RIB 6 BEARING LUGS. I: 12 YE  572651-01-1 732 742 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN T: 12 YE  671 LANDING GEAR SIDE STAY FITTING (RIB 2). I: 12 YE  572652-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE  671 FORWARD PINTLE FITTING (RIB 5). I: 12 YE  572653-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE  671 RETRACTION JACK FITTING, I: 12 YE  572654-01-1 732 742 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE  671 SUPPORT RIB 6. I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572655-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673FB 673 EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND I: 12 YE I: 12 YE  FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET,  INTERFACE PLATE AND THRUST PADS).  572656-01-1 532SB 533SB 534SB 574 GENERAL VISUAL INSPECTION OF OUTER WING FLAP T: 12 YE  632SB 633SB 634SB 674 TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. I: 12 YE  572657-01-1 531VT 531WB 532VT 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, T: 12 YE T: 20 YE  532WB 533VT 533WB 532 4 AND 5 FORWARD PICK-UP FITTINGS LUGS. I: 12 YE I: 12 YE  534VT 534WB 631VT 533  631WB 632VT 632WB 534  633VT 633WB 634VT 631  634WB 632  633  634  572660-01-1 462GR 462JL 464AL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON T: 12 YE T: 20 YE NO  464AR 472GR 472JL 641 SPIGOT FITTING. I: 12 YE I: 12 YE  474AL 474AR  SPIGOT SLEEVE  572661-01-1 452EL 452GR 454AL 542 DETAILED INSPECTION OF OUTER WING OUTER PYLON T: 12 YE T: 20 YE NO  482EL 482GR 484AL 642 SPIGOT FITTING. I: 12 YE I: 12 YE  SPIGOT SLEEVE  572662-01-1 464AL 464AR 464BL 541 DETAILED INSPECTION OF OUTER WING INNER PYLON T: 12 YE T: 20 YE NO  464BR 474AL 474AR 641 AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  474BL 474BR  572663-01-1 454AL 454AR 454BL 542 DETAILED INSPECTION OF OUTER WING OUTER PYLON T: 12 YE T: 20 YE NO  454BR 484AL 484AR 642 AFT ATTACHMENT FITTING. I: 12 YE I: 12 YE  484BL 484BR  572664-01-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE  743 HINGED DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 572665-01-1 732 742 732 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR T: 6 YE  742 LEG FAIRING ATTACHMENT ASSEMBLIES TO LEG STRUCTURE. I: 6 YE  573001-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FC  OR  60000 FH  I: 12 YE  OR  5500 FC  OR  28900 FH  573001-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FC  OR  60000 FH  I: 12 YE  OR  2900 FC  OR  15300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 573001-01-3 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FC  OR  60000 FH  I: 12 YE  OR  4200 FC  OR  22300 FH  573001-01-4 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FC  OR  26000 FH  I: 12 YE  OR  5100 FC  OR  10200 FH  573001-01-5 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 13000 FC  OR  65000 FH  I: 12 YE  OR  6900 FC  OR  31200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 573002-01-1 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FC  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR  60000 FH  I: 5500 FC  OR  29400 FH  573002-01-2 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FC  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR  60000 FH  I: 2900 FC  OR  15300 FH  573002-01-3 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FC  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR  60000 FH  I: 4200 FC  OR  22300 FH  573002-01-4 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FC  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR  26000 FH  I: 5100 FC  OR  10200 FH  573002-01-5 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN T: 13000 FC  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE OR  65000 FH  I: 6900 FC  OR  31200 FH  573002-02-1 N/A 500 GENERAL VISUAL INSPECTION OF WING TIP BOX TOP SKIN T: 6 YE NO  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 573003-01-1 WINGLET 535 DETAILED INSPECTION OF WINGTIP TO WINGLET T: 12 YE T: 20 YE  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET) I: 12 YE I: 12 YE  573003-02-1 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FC  635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND OR  WINGLET) 60000 FH  I: 6400 FC  OR  33900 FH  573003-02-2 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FC  635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND OR  WINGLET) 60000 FH  I: 6100 FC  OR  32400 FH  573003-02-3 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FC  635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND OR  WINGLET) 26000 FH  I: 7300 FC  OR  14600 FH  573003-02-4 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO T: 13000 FC  635 WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND OR  WINGLET) 65000 FH  I: 12700 FC  OR  57400 FH  573004-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE  635BZ 635 AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 573004-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 13000 FC  635BZ 635 AFT FITTING BOTTOM FLANGE TO SKIN ATTACHMENT. OR  65000 FH  I: 6700 FC  OR  30200 FC  573005-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WING WINGTIP TO T: 12 YE  635BB 635 WINGLET JOINT BOLTS. I: 12 YE  JOINT BOLTS  573006-01-1 N/A 500 GENERAL VISUAL INSPECTION OF WINGLET EXTERNAL SURFACE T: 5 YE NO  600 I: 5 YE  573051-01-1 535AT 535CZ 635AT 535 SPECIAL DETAILED INSPECTION OF OUTER WING WINGTIP TO T: 12 YE T: 20 YE  635CZ 635 MAIN WINGBOX JOINT AT RIB 41 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE  TRAILING EDGE SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND  SECTION BUTTSTRAPS.  573052-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING WINGTIP T: 6 YE  600 BOX TOP SKIN UPPER SURFACE AND BOTTOM SKIN I: 6 YE  LOWER SURFACE.  573053-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WINGTIP TO WINGLET T: 12 YE T: 20 YE  635BB 635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). I: 12 YE I: 12 YE  573054-01-1 535AB 535BB 635AB 535 SPECIAL DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE  635BB 635 AFT I: 12 YE I: 12 YE  FITTING BOTTOM FLANGE TO SKIN ATTACHMENT  573055-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF OUTER WING WINGTIP T: 12 YE T: 20 YE  635BB 635 TO WINGLET JOINT BOLTS. I: 12 YE I: 12 YE  JOINT BOLTS  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 573056-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING WINGLET T: 10 YE  600 EXTERNAL SURFACE. I: 10 YE  574101-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521GB 521JB 522CB 522 LEADING EDGE TRACK RIBS 1 TO 16. I: 12 YE I: 12 YE  522JB 522LB 522NB 523  522RB 522TB 523CB 621  523EB 523GB 523JB 622  523LB 523NB 621BB 623  621CB 621DB 621GB  621JB 622CB 622JB  622LB 622NB 622RB  622TB 623CB 623EB  623GB 623JB 623LB  623NB  574102-01-1 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR  522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 60000 FH  522RB 522TB 523CB 621 I: 11000 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 48000 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-2 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR  522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 60000 FH  522RB 522TB 523CB 621 I: 10400 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 45400 FH  622JB 622LB 622NB  622RB 622TB 623CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574102-01-3 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR  522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 26000 FH  522RB 522TB 523CB 621 I: 10400 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 20800 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-4 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  521GB 521JB 522CB 522 FIXED LEADING EDGE FORWARD UPPER ROLLER PIN HOLES OR  522JB 522LB 522NB 523 IN TRACK RIBS 1 TO TRACK RIBS 11. 65000 FH  522RB 522TB 523CB 621 I: 13000 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 65000 FH  622JB 622LB 622NB  622RB 622TB 623CB  574103-01-1 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE  522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC  522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR  522UB 523AB 523BB 622 60000 FH  560AB 621DB 621FB 623 I: 12 YE  621GB 622AB 622BB OR  622CB 622EB 622GB 4300 FC  622HB 622JB 622NB OR  622RB 622UB 623AB 18700 FH  623BB 660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574103-01-2 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE  522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC  522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR  522UB 523AB 523BB 622 60000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 5300 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 23100 FH  574103-01-3 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE  522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC  522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR  522UB 523AB 523BB 622 26000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 5300 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 10600 FH  574103-01-4 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE CUTOUTS IN ALL INTERMEDIATE RIBS OR I: 12 YE  522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND 13000 FC  522JB 522NB 522RB 621 SLAT HOLD DOWN RIBS. OR  522UB 523AB 523BB 622 65000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 5500 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 25100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574104-01-1 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FC  521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521JB 522AB 523 60000 FH  522BB 522CB 522DB 621 I: 13000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522LB 623 60000 FH  522MB 522NB 522PB  522QB 522RB 522SB  523AB 523BB 523CB  523DB 523EB 523FB  523GB 523HB 523JB  523LB 523MB 523NB  523PB 560AB 621AB  621BB 621CB 621DB  621EB 621FB 621GB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622LB 622MB  622NB 622PB 622QB  622RB 622SB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623LB  623MB 623NB 623PB  660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574104-01-2 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FC  521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521JB 522AB 523 60000 FH  522BB 522CB 522DB 621 I: 8900 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522LB 623 38800 FH  522MB 522NB 522PB  522QB 522RB 522SB  523AB 523BB 523CB  523DB 523EB 523FB  523GB 523HB 523JB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622LB 622MB 622NB  622PB 622QB 622RB  622SB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574104-01-3 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FC  521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521JB 522AB 523 26000 FH  522BB 522CB 522DB 621 I: 8900 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522LB 623 17800 FH  522MB 522NB 522PB  522QB 522RB 522SB  523AB 523BB 523CB  523DB 523EB 523FB  523GB 523HB 523JB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622LB 622MB 622NB  622PB 622QB 622RB  622SB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574104-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 13000 FC  521DB 521EB 521FB 522 EDGE TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521JB 522AB 523 65000 FH  522BB 522CB 522DB 621 I: 7800 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522LB 623 35200 FH  522MB 522NB 522PB  522QB 522RB 522SB  523AB 523BB 523CB  523DB 523EB 523FB  523GB 523HB 523JB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622LB 622MB 622NB  622PB 622QB 622RB  622SB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623LB 623MB  623NB 623PB  574105-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YE  522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 60000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 4400 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 19200 FH  623GB 623JB 623LB  623NB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574105-01-2 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YE  522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 26000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 6500 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 13000 FH  623GB 623JB 623LB  623NB  574105-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521GB 521JB 522CB 522 LEADING EDGE BOTTOM SPREADER PLATE ON TRACK RIB 1 OR I: 12 YE  522JB 522LB 522NB 523 TO TRACK RIB 16. 13000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 65000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 7400 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 33400 FH  623GB 623JB 623LB  623NB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574106-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR  521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 60000 FH  522CB 522DB 522EB 621 I: 13000 FC  522FB 522GB 522HB 622 OR  522JB 522KB 522LB 623 60000 FH  522MB 522NB 522PB  522QB 523AB 523BB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  560AB 621BB 621CB  621DB 621EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623KB  623LB 623MB 623NB  623PB 660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574106-01-2 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR  521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 60000 FH  522CB 522DB 522EB 621 I: 13000 FC  522FB 522GB 522HB 622 OR  522JB 522KB 522LB 623 60000 FH  522MB 522NB 522PB  522QB 523AB 523BB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622QB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574106-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR  521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 26000 FH  522CB 522DB 522EB 621 I: 13000 FC  522FB 522GB 522HB 622 OR  522JB 522KB 522LB 623 26000 FH  522MB 522NB 522PB  522QB 523AB 523BB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622QB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574106-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK OR  521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16. 65000 FH  522CB 522DB 522EB 621 I: 13000 FC  522FB 522GB 522HB 622 OR  522JB 522KB 522LB 623 65000 FH  522MB 522NB 522PB  522QB 523AB 523BB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622QB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574106-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521EB 521FB 521GB 522 LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK I: 12 YE I: 12 YE  521JB 522AB 522BB 523 RIB 1 TO TRACK RIB 16.  522CB 522DB 522EB 621  522FB 522GB 522HB 622  522JB 522KB 522LB 623  522MB 522NB 522PB  522QB 523AB 523BB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  560AB 621BB 621CB  621DB 621EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623KB  623LB 623MB 623NB  623PB 660AB  574107-01-1 521FB 521GB 521JB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YE  522DB 522EB 522FB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12.  522GB 522HB 522JB 621  522KB 522LB 522MB 622  522NB 522PB 522QB 623  523AB 523BB 523CB  523DB 523EB 560AB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 623AB  623BB 623CB 623DB  623EB 660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574107-01-3 521FB 521GB 521JB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  522AB 522BB 522CB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YE  522DB 522EB 522FB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12.  522GB 522HB 522JB 621  522KB 522LB 522MB 622  522NB 522PB 522QB 623  523AB 523BB 523CB  523DB 523EB 523FB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622LB 622MB 622NB  622PB 622QB 622RB  622SB 623AB 623BB  623CB 623DB 623EB  623FB  574107-02-1 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OR  522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 60000 FH  522GB 522HB 522JB 621 I: 9700 FC  522KB 522LB 522MB 622 OR  522NB 522PB 522QB 623 42300 FH  523AB 523BB 523CB  523DB 523EB 560AB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 623AB  623BB 623CB 623DB  623EB 660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574107-02-2 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OR  522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 60000 FH  522GB 522HB 522JB 621 I: 9100 FC  522KB 522LB 522MB 622 OR  522NB 522PB 522QB 623 39700 FH  523AB 523BB 523CB  523DB 523EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB  574107-02-3 521FB 521GB 521JB 521 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  522AB 522BB 522CB 522 FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR OR  522DB 522EB 522FB 523 JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12 26000 FH  522GB 522HB 522JB 621 I: 9400 FC  522KB 522LB 522MB 622 OR  522NB 522PB 522QB 623 18800 FH  523AB 523BB 523CB  523DB 523EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB  574108-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE  621 LEADING EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, I: 12 YE  MAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.  574109-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574109-01-2 N/A TASK DELETED  574109-01-3 N/A TASK DELETED  574109-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND OR  521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS 65000 FH  522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND I: 5200 FC  522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS. OR  522HB 522JB 522KB 623 23400 FH  522LB 522MB 522NB  522PB 522QB 523AB  523BB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523LB  523MB 523NB 523QB  621AB 621BB 621CB  621DB 621EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623LB  623MB 623NB 623QB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574109-01-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND I: 12 YE I: 12 YE  521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS  522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND  522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS.  522HB 522JB 522KB 623  522LB 522MB 522NB  522PB 522QB 523AB  523BB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523LB  523MB 523NB 523QB  560AB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623LB  623MB 623NB 623QB  660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574109-01-6 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  521DB 521EB 521FB 522 LEADING EDGE BOTTOM JOINT SPREADER PLATES AND I: 12 YE I: 12 YE  521GB 521JB 522AB 523 SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS  522BB 522CB 522DB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND  522EB 522FB 522GB 622 SLAT HOLD DOWN RIBS.  522HB 522JB 522KB 623  522LB 522MB 522NB  522PB 522QB 523AB  523BB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523LB  523MB 523NB 523QB  621AB 621BB 621CB  621DB 621EB 621FB  621GB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622QB 623AB  623BB 623CB 623DB  623EB 623FB 623GB  623HB 623JB 623LB  623MB 623NB 623QB  574110-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 60000 FH  I: 10400 FC  OR  39300 FH  574110-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 60000 FH  I: 11200 FC  OR  42300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574110-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 26000 FH  I: 11600 FC  OR  23200 FH  574110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 6 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9  574110-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC T: 6 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9 65000 FH  I: 13000 FC  OR  65000 FH  574111-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 60000 FH  I: 9400 FC  OR  49800 FH  574111-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 60000 FH  I: 10100 FC  OR  53500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574111-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 26000 FH  I: 11600 FC  OR  23200 FH  574111-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39 65000 FH  I: 7200 FC  OR  33200 FH  574111-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE NO  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 39  574112-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  623NB 623 LEADING EDGE HOLD DOWN RIB BETWEEN SLAT TRACK RIB I: 12 YE I: 12 YE  15 AND SLAT TRACK 16, AREA OF SLAT TRACK BRAKE  FITTING.  574114-01-1 560AB 660AB 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 60000 FH  26 TO RIB 39 I: 10400 FC  OR  39300 FH  574114-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 60000 FH  26 TO RIB 39 I: 11200 FC  OR  42300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574114-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26000 FH  26 TO RIB 39 I: 11600 FC  OR  23200 FH  574114-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED T: 13000 FC  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE OR  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 65000 FH  26 TO RIB 39 I: 13000 FC  OR  65000 FH  574114-02-1 560AB 660AB 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 12 YE  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB  26 TO RIB 39.  574114-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE NO  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE I: 12 YE  FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB  26 TO RIB 39.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574115-01-1 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE  560AB 622AB 622BB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC  622CB 623AB 623BB 623 AND RIB 24 TO RIB 26 OR  623CB 660AB 60000 FH  I: 12 YE  OR  4200 FC  OR  15800 FH  574115-01-2 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE  622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC  623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR  60000 FH  I: 12 YE  OR  3100 FC  OR  11700 FH  574115-01-3 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE  622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC  623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR  26000 FH  I: 12 YE  OR  4600 FC  OR  9200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574115-01-4 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  523AB 523BB 523CB 523 LEADING BOTTOM SKIN OVERHANG UPPER SURFACE OR I: 12 YE  622AB 622BB 622CB 622 FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 13000 FC  623AB 623BB 623CB 623 AND RIB 24 TO RIB 26 OR  65000 FH  I: 12 YE  OR  13000 FC  OR  65000 FH  574116-01-1 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE  521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC  522BB 522CB 522DB 621 HOLD DOWN RIBS OR  522EB 522FB 522GB 622 60000 FH  522HB 522JB 522KB 623 I: 12 YE  522LB 522MB 522NB OR  522PB 522QB 523AB 5500 FC  523BB 523CB 523DB OR  523EB 523FB 523GB 24000 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 560AB 621AB  621BB 621CB 621DB  621EB 621FB 621GB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622QB 623AB 623BB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  660AB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574116-01-2 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE  521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC  522BB 522CB 522DB 621 HOLD DOWN RIBS OR  522EB 522FB 522GB 622 60000 FH  522HB 522JB 522KB 623 I: 12 YE  522LB 522MB 522NB OR  522PB 522QB 523AB 3100 FC  523BB 523CB 523DB OR  523EB 523FB 523GB 13500 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622QB  623AB 623BB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574116-01-3 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE  521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC  522BB 522CB 522DB 621 HOLD DOWN RIBS OR  522EB 522FB 522GB 622 26000 FH  522HB 522JB 522KB 623 I: 12 YE  522LB 522MB 522NB OR  522PB 522QB 523AB 9400 FC  523BB 523CB 523DB OR  523EB 523FB 523GB 18800 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622QB  623AB 623BB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574116-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE  521GB 521JB 522AB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC RIBS) AND SLAT 13000 FC  522BB 522CB 522DB 621 HOLD DOWN RIBS OR  522EB 522FB 522GB 622 65000 FH  522HB 522JB 522KB 623 I: 12 YE  522LB 522MB 522NB OR  522PB 522QB 523AB 13000 FC  523BB 523CB 523DB OR  523EB 523FB 523GB 65000 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622QB  623AB 623BB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  574119-01-1 521BB 521GB 523GB 521 DETAILED INSPECTION OF OUTER WING FIXED T: 12 YE T: 20 YE  523JB 523LB 523NB 523 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT I: 12 YE I: 12 YE  621BB 621GB 623GB 621 STRAPS AT TRACKS RIBS 1 AND 2 AND TRACK  623JB 623LB 623NB 623 RIBS 13 TO 16  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574151-01-1 521BB 521CB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521HB 522CB 522EB 522 TRACK RIBS 1 TO 17. I: 12 YE I: 12 YE  522GB 522HB 522KB 523  522MB 522PB 523BB 621  523CB 523DB 523FB 622  523HB 523KB 523MB 623  523PB 523QB 621BB  621CB 621FB 621HB  622CB 622EB 622GB  622HB 622KB 622MB  622PB 623BB 623CB  623DB 623FB 623HB  623KB 623MB 623PB  623QB  574153-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING I: 12 YE I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.  522KB 522MB 522PB 621  522QB 522RB 522UB 622  523AB 523BB 523DB 623  523FB 523HB 523KB  523MB 523PB 523QB  621CB 621EB 621FB  622AB 622BB 622CB  622EB 622GB 622HB  622KB 622MB 622PB  622QB 622RB 622UB  623AB 623BB 623DB  623FB 623HB 623KB  623MB 623PB 623QB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574155-01-1 521BB 521CB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521HB 522BB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 17. I: 12 YE I: 12 YE  522EB 522GB 522HB 523  522KB 522MB 522QB 621  523BB 523CB 523DB 622  523FB 523HB 523KB 623  523MB 523PB 523QB  621BB 621CB 621FB  621HB 622BB 622CB  622EB 622GB 622HB  622KB 622MB 622QB  623BB 623CB 623DB  623FB 623HB 623KB  623MB 623PB 623QB  574156-01-1 522BB 522CB 522EB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  522GB 522HB 522KB 523 BOTTOM SUB SPAR JOINT STRAPS ON TRACK RIB 5 TO TRACK I: 12 YE I: 12 YE  522MB 522PB 523BB 622 RIB 14.  523CB 523DB 523FB 623  523HB 523KB 622BB  622CB 622EB 622GB  622HB 622KB 622MB  622PB 623BB 623CB  623DB 623FB 623HB  623KB  574157-01-1 521FB 521HB 522CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  522EB 522GB 522HB 522 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YE  522KB 522MB 522PB 523 RIB 3 TO TRACK RIB 12.  523BB 523CB 523DB 621  523FB 621FB 621HB 622  622CB 622EB 622GB 623  622HB 622KB 622MB  622PB 623BB 623CB  623DB 623FB  574158-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE  621 LEADING EDGE FAIRING SUPPORT INBOARD OF RAMP I: 12 YE  RIB, MAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574159-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 12 YE T: 20 YE  522AB 522BB 522CB 522 EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR I: 12 YE I: 12 YE  522EB 522GB 522HB 523 JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING  522KB 522MB 522PB 621 TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.  522RB 522UB 523AB 622  523BB 523DB 523FB 623  523HB 523KB 523MB  523PB 523QB 621CB  621EB 621FB 622AB  622BB 622CB 622EB  622GB 622HB 622KB  622MB 622PB 622RB  622UB 623AB 623BB  623DB 623FB 623HB  623KB 623MB 623PB  623QB  574160-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER I: 6 YE  SURFACE FORWARD OF FRONT SPAR FROM ROOT  TO INBOARD PYLON FAIRINGS.  574161-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 6 YE  600 LEADING EDGE TOP SKIN OVERHANG UPPER SURFACE I: 6 YE  FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 41.  574162-01-1 523MB 523PB 623MB 523 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  623PB 623 INTERMEDIATE RIB BETWEEN SLAT TRACK RIB 15 AND SLAT I: 12 YE I: 12 YE  TRACK 16, AREA OF SLAT TRACK BRAKE FITTING.  574164-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED T: 12 YE  600 LEADING EDGE BOTTOM SKIN OVERHANG LOWER I: 12 YE  SURFACE FORWARD OF FRONT SPAR FROM INBOARD  PYLON FAIRINGS TO WINGTIP, EXCLUDING AREA HIDDEN  BY OUTBOARD PYLON FAIRINGS.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574165-01-1 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  523AB 523BB 523CB 523 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF I: 12 YE I: 12 YE  523DB 622AB 622BB 622 FRONT SPAR BETWEEN RIBS 9 AND 11 AND BETWEEN RIBS 23  622CB 623AB 623BB 623 AND 26.  623CB 623DB  574166-01-1 521CB 521EB 521FB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  522AB 522BB 522CB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS I: 12 YE I: 12 YE  522EB 522GB 522HB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCTS) AND  522KB 522MB 522PB 621 SLAT HOLD DOWN RIBS.  522RB 522UB 523AB 622  523BB 523DB 523FB 623  523HB 523KB 523MB  523PB 523QB 621CB  621EB 621FB 622AB  622BB 622CB 622EB  622GB 622HB 622KB  622MB 622PB 622RB  622UB 623AB 623BB  623DB 623FB 623HB  623KB 623MB 623PB  623QB  574169-01-1 521BB 521CB 523HB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  523KB 523MB 523PB 523 TOP I: 12 YE I: 12 YE  523QB 621BB 621CB 621 SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK  623HB 623KB 623MB 623 RIBS 1 AND 2 AND TRACK RIBS 13 TO 17.  623PB 623QB  R 574301-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FC  611 3, VISIBLE PART OF ROLLER CONTACT AREA. OR  65000 FH  I: 9400 FC  OR  47000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574301-01-2 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FC  611 3, VISIBLE PART OF ROLLER CONTACT AREA. OR  26000 FH  I: 11200 FC  OR  22400 FH  R 574301-01-3 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND T: 13000 FC  611 3, VISIBLE PART OF ROLLER CONTACT AREA. OR  65000 FH  I: 4500 FC  OR  22500 FH  R 574303-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 12 YE  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  N 574303-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FC  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574303-02-2 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FC  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574303-02-3 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 13000 FC  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574304-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN T: 12 YE T: 20 YE NO  611 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574304-03-1.  R 574304-02-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FC  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  65000 FH  I: 8800 FC  OR  31900 FH  R 574304-02-2 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FC  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  26000 FH  I: 10500 FC  OR  21000 FH  R 574304-02-3 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 13000 FC  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  65000 FH  I: 5500 FC  OR  20000 FH  R 574304-03-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574304-01-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574305-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1 HOLD DOWN T: 12 YE T: 20 YE  611 BRACKET, LH/RH. I: 12 YE I: 12 YE  574306-01-1 N/A TASK DELETED  R 574306-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1 TRAILING EDGE T: 3 YE  611 LOWER FACE, 100 MM FORWARD OF AFT EDGE, LH/RH. I: 3 YE  R 574307-01-1 521DB 521GB 621DB 511 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 T: 12 YE T: 20 YE  621GB 611 ACTUATION LINK CONNECTION BOLTS LH/RH. I: 6 YE I: 6 YE  REMOVAL OF THE BOLTS  ONE AT A TIME.  SLAT FULLY EXTENDED  R 574308-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL T: 6 YE NO  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574353-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 12 YE NO  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574354-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN T: 12 YE T: 20 YE NO  611 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574354-01-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574356-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRAILING EDGE T: 3 YE NO  611 LOWER FACE, 100 MM FROM LEFT EDGE, LH/RH. I: 3 YE  R 574357-01-1 521CB 521FB 621CB 521 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 T: 12 YE T: 20 YE NO  621FB 621 ACTUATION LINK CONNECTION BOLTS, LH/RH. I: 6 YE I: 6 YE  REMOVAL OF THE BOLTS  ONE AT A TIME.  SLAT FULLY EXTENDED  574358-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL T: 6 YE NO  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574401-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FC  612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  R 574401-01-2 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FC  612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 6200 FC  OR  12400 FH  R 574401-01-3 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, T: 13000 FC  612 TRACKS 5 AND 6 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574401-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 12 YE T: 20 YE  612 6 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574403-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 12 YE  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574403-02-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FC  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574403-02-2 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FC  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  574403-02-3 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 13000 FC  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574404-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574404-03-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574404-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FC  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 8800 FC  OR  31900 FH  R 574404-02-2 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FC  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 26000 FH  I: 10500 FC  OR  21000 FH  R 574404-02-3 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 13000 FC  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 5500 FC  OR  20000 FH  R 574404-03-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574404-01-1.  R 574405-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2 HOLD DOWN T: 12 YE T: 20 YE  612 BRACKET, LH/RH. I: 12 YE I: 12 YE  574406-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2 TRAILING EDGE T: 3 YE  612 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 574407-01-1 522CB 522FB 622CB 522 DETAILED INSPECTION OF SLAT 2, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622FB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574451-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 12 YE T: 20 YE NO  612 6 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574453-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 TO 6 T: 12 YE NO  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574454-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574454-03-1.  R 574454-03-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO  612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  612 BRACKET, LH/RH. I: 12 YE I: 12 YE  R 574456-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRAILING EDGE T: 3 YE NO  612 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 574457-01-1 522CB 522EB 622CB 522 DETAILED INSPECTION OF SLAT 2, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622EB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574501-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE T: 20 YE  613 8, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574501-02-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FC  613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  R 574501-02-2 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FC  613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 3100 FC  OR  15500 FH  R 574501-02-3 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FC  613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 3700 FC  OR  7400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574501-02-4 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, T: 13000 FC  613 TRACKS 7 AND 8 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574503-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE  613 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  574503-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FC  613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574503-02-2 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FC  613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  574503-02-3 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 13000 FC  613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574504-01-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574504-03-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574504-02-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FC  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 8800 FC  OR  31900 FH  R 574504-02-2 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FC  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 26000 FH  I: 10500 FC  OR  21000 FH  R 574504-02-3 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 13000 FC  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 5500 FC  OR  20000 FH  R 574504-03-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574504-01-1.  R 574505-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 3 HOLD DOWN T: 12 YE T: 20 YE  612 BRACKET, LH/RH. I: 12 YE I: 12 YE  574506-01-1 N/A TASK DELETED  R 574506-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRAILING EDGE T: 3 YE  613 LOWER FACE, 100 MM FORWARD OF AFT EDGE, LH/RH. I: 3 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574507-01-1 N/A TASK DELETED  N 574507-01-2 522JB 522LB 622JB 522 DETAILED INSPECTION OF SLAT 3, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622LB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574551-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE T: 20 YE NO  613 8 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574553-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND T: 12 YE NO  613 8 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574554-01-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574554-03-1.  R 574554-03-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO  613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  613 BRACKET, LH/RH. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574556-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRAILING EDGE T: 3 YE NO  613 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YE  N 574557-01-1 522JB 522LB 622JB 522 DETAILED INSPECTION OF SLAT 3, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622LB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  N 574558-02-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, T: 6 YE NO  600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574601-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FC  614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  R 574601-01-2 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FC  614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 6200 FC  OR  12400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574601-01-3 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, T: 13000 FC  614 TRACKS 9 AND 10 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574601-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 12 YE T: 20 YE  614 10, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574603-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 & T: 12 YE NO  614 10 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  574603-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FC  614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574603-02-2 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FC  614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  574603-02-3 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND T: 13000 FC  614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUG, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574604-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN T: 12 YE T: 20 YE NO  614 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574604-03-1.  R 574604-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FC  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  65000 FH  I: 8800 FC  OR  31900 FH  R 574604-02-2 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FC  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  26000 FH  I: 10500 FC  OR  21000 FH  R 574604-02-3 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 13000 FC  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  65000 FH  I: 5500 FC  OR  20000 FH  R 574604-03-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574604-01-1.  R 574605-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN T: 12 YE T: 20 YE  614 BRACKET, LH/RH. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574606-01-1 N/A TASK DELETED  R 574606-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4 TRAILING EDGE T: 3 YE  614 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YE  N 574607-01-1 522NB 522RB 622NB 522 DETAILED INSPECTION OF SLAT 4, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622RB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574651-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 12 YE T: 20 YE NO  614 10 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574653-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 TO T: 12 YE NO  614 10 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574654-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN T: 12 YE T: 20 YE NO  614 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574654-01-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574655-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN T: 12 YE T: 20 YE NO  614 BRACKET, LH/RH. I: 12 YE I: 12 YE  R 574656-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRAILING EDGE T: 3 YE NO  614 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YE  N 574657-01-1 522MB 522PB 622MB 522 DETAILED INSPECTION OF SLAT 4, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  622PB 622 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574701-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE T: 20 YE  615 12, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  574701-02-1 N/A TASK DELETED  R 574701-02-2 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FC  615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574701-02-3 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FC  615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 6200 FC  OR  12400 FH  R 574701-02-4 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, T: 13000 FC  615 TRACKS 11 AND 12 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574703-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE  615 12 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  574703-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FC  615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574703-02-2 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FC  615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574703-02-3 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND T: 13000 FC  615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574704-01-1 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574704-03-1.  R 574704-02-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FC  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 8800 FC  OR  31900 FH  R 574704-02-2 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FC  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 26000 FH  I: 10500 FC  OR  21000 FH  R 574704-02-3 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 13000 FC  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 5500 FC  OR  20000 FH  R 574704-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574704-01-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574705-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5 HOLD DOWN T: 12 YE T: 20 YE  615 BRACKET, LH/RH. I: 12 YE I: 12 YE  574706-01-1 N/A TASK DELETED  574706-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5 TRAILING EDGE, T: 3 YE  615 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YE  N 574707-01-1 523CB 523FB 623CB 523 DETAILED INSPECTION OF SLAT 5, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623FB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574751-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE T: 20 YE NO  615 12 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574753-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 12 YE NO  615 12 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574754-01-1 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574754-03-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574754-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO  615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  615 BRACKET, LH/RH. I: 12 YE I: 12 YE  R 574756-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRAILING EDGE T: 3 YE NO  615 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YE  N 574757-01-1 523CB 523EB 623CB 523 DETAILED INSPECTION OF SLAT 5, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623EB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 OF UPPER AN LOWER SKIN, LH/RH. I: 6 YE  R 574801-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE T: 20 YE  616 14, VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574801-02-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FC  616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574801-02-2 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FC  616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 6200 FC  OR  12400 FH  R 574801-02-3 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, T: 13000 FC  616 TRACKS 13 AND 14 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574803-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE  616 14 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  574803-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FC  616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  574803-02-2 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FC  616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574803-02-3 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND T: 13000 FC  616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574804-01-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574804-03-1.  R 574804-02-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FC  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 8800 FC  OR  31900 FH  R 574804-02-2 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FC  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 6800 FC  OR  24600 FH  R 574804-02-3 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FC  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 26000 FH  I: 8100 FC  OR  16200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574804-02-4 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 13000 FC  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 5500 FC  OR  20000 FH  R 574804-03-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574804-01-1.  R 574805-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6 HOLD DOWN T: 12 YE T: 20 YE  616 BRACKET, LH/RH. I: 12 YE I: 12 YE  574806-01-1 N/A TASK DELETED  R 574806-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6 TRAILING EDGE T: 3 YE  616 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YE  N 574807-01-1 523GB 523JB 623GB 523 DETAILED INSPECTION OF SLAT 6, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623JB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574851-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE T: 20 YE NO  616 14 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574853-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 12 YE NO  616 14 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574854-01-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574854-03-1.  R 574854-03-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO  616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 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  616 BRACKET, LH/RH. I: 12 YE I: 12 YE  R 574856-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRAILING EDGE T: 3 YE NO  616 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YE  N 574857-01-1 523HB 523KB 623HB 523 DETAILED INSPECTION OF SLAT 6, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623KB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574901-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 12 YE T: 20 YE  617 16 ;VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574901-02-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FC  617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 5200 FC  OR  26000 FH  R 574901-02-2 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FC  617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 26000 FH  I: 6200 FC  OR  12400 FH  R 574901-02-3 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, T: 13000 FC  617 TRACKS 15 AND 16 ; VISIBLE PART OF ROLLER CONTACT OR  AREA, LH/RH. 65000 FH  I: 4500 FC  OR  22500 FH  R 574903-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 12 YE  617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK I: 6 YE  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.  574903-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FC  617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 3400 FC  OR  17000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 574903-02-2 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FC  617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 26000 FH  I: 4000 FC  OR  8000 FH  574903-02-3 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND T: 13000 FC  617 16 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK OR  LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 65000 FH  I: 2000 FC  OR  10000 FH  R 574904-01-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO  617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574904-02-1.  R 574904-02-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE  617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB I: 12 YE I: 12 YE  STATIONS, EXTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574904-01-1.  R 574904-02-2 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FC  617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 8800 FC  OR  31900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574904-02-3 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FC  617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 26000 FH  I: 10500 FC  OR  21000 FH  R 574904-02-4 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 13000 FC  617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB OR  STATIONS, EXTERNAL, LH/RH. 65000 FH  I: 5500 FC  OR  20000 FH  R 574905-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7 HOLD DOWN T: 12 YE T: 20 YE  617 BRACKET, LH/RH. I: 12 YE I: 12 YE  574906-01-1 N/A TASK DELETED  R 574906-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7 TRAILING EDGE T: 3 YE  617 LOWER FACE, 100 MM FORWARD OF AFT EDGE LH/RH. I: 3 YE  N 574907-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF SLAT 7, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623NB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574951-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 TO 17, T: 12 YE T: 20 YE NO  617 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 574953-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 TO 17 T: 12 YE NO  617 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS AND LINKS, LH/RH.  R 574954-01-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO  617 CONNECTIONS AT TRACK RIB STATIONS, INTERNAL, LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574954-02-1.  R 574954-02-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO  617 CONNECTIONS AT TRACK RIB STATIONS, EXTERNAL, LH/RH. I: 12 YE I: 12 YE  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574954-01-1.  R 574956-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRAILING EDGE, T: 3 YE NO  617 LOWER FACE, 100 MM FROM AFT EDGE,H/RH. I: 3 YE  N 574957-01-1 523MB 523QB 623MB 523 DETAILED INSPECTION OF SLAT 7, PINION AND RACK TEETH, T: 6 YE T: 20 YE NO  623QB 623 LH/RH. I: 6 YE I: 6 YE  SLAT FULLY EXTENDED NOTE:THIS INSPECTION IS LISTED FOR CPCP PURPOSE ONLY.  THE 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  600 SURFACE OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  575001-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YE  13000 FC  I: 12 YE  OR  5200 FC  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575001-01-2 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YE  13000 FC  I: 12 YE  OR  4500 FC  575001-01-3 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING OR I: 12 YE  13000 FC  I: 12 YE  OR  5400 FC  575002-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673BB 673DB 673FB 673 EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR SPAR I: 12 YE I: 12 YE  OR FALSE REAR SPAR AND SPOILER 1 HINGE FITTINGS.  575003-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 674 EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT I: 12 YE I: 12 YE  FITTING (5 PLACES) LUGS AND ATTACHMENT TO BOTTOM  SKIN OVERHANG.  575004-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS 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 FC  OVERHANG I: 12 YE  OR  5200 FC  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575004-01-2 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS 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 FC  OVERHANG I: 12 YE  OR  4500 FC  575004-01-3 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS 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 FC  OVERHANG I: 12 YE  OR  6300 FC  575005-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 674 EDGE SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS I: 12 YE I: 12 YE  AND OUTER LINK HINGE RIBS (16 PLACES)  575006-01-1 575AB 575CB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  675CB 675 EDGE INBOARD AND OUTBOARD AILERON JACK BRACKETS (4 I: 12 YE I: 12 YE  PLACES) AT LUG AND ATTACHMENT TO TOP AND BOTTOM  SKIN OVERHANGS (INTERNAL AND EXTERNAL)  575008-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 574 EDGE RIB 10 FLAP CRUISE ROLLERS SUPPORT I: 12 YE I: 12 YE  673  674  575009-01-1 573BB 573CB 573DB 573 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  573EB 573FB 573GB 673 EDGE RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, TOP I: 12 YE  673BB 673CB 673DB AND BOTTOM SKIN OVERHANGS AND OUTER FLAP CRUISE  673EB 673FB 673GB ROLLER SUPPORT ATTACHMENT TO TRAILING EDGE RIB 10  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575010-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  13000 FC  OR  60000 FH  I: 12 YE  OR  9100 FC  OR  34600 FH  575010-01-2 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  13000 FC  OR  60000 FH  I: 12 YE  OR  8700 FC  OR  32900 FH  575010-01-3 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  13000 FC  OR  26000 FH  I: 12 YE  OR  11700 FC  OR  23400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575010-01-4 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673BB 673DB 673FB 673 EDGE FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  13000 FC  OR  65000 FH  I: 12 YE  OR  7400 FC  OR  33600 FH  575011-01-1 N/A TASK DELETED  575011-01-2 N/A TASK DELETED  575011-01-3 N/A TASK DELETED  575011-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE NO  600 EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR I: 12 YE  BETWEEN RIB 1 AND RIB 14.  575012-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 60000 FH  FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 3100 FC  REAR SPAR JUST INBOARD OF GEAR RIB 6. OR  11800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575012-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 60000 FH  FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 7000 FC  REAR SPAR JUST INBOARD OF GEAR RIB 6. OR  26500 FH  575012-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 26000 FH  FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 9400 FC  REAR SPAR JUST INBOARD OF GEAR RIB 6. OR  18800 FH  575012-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY 65000 FH  FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF I: 4600 FC  REAR SPAR JUST INBOARD OF GEAR RIB 6. OR  20000 FH  575012-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 6 YE NO  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 6 YE  BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY  FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF  REAR SPAR JUST INBOARD OF GEAR RIB 6.  575013-01-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR OR  SPAR JUST INBOARD OF GEAR SUPPORT RIB 6 60000 FH  I: 10500 FC  OR  39900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575013-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR OR  SPAR JUST INBOARD OF GEAR SUPPORT RIB 6 26000 FH  I: 13000 FC  OR  26000 FH  575013-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 13000 FC  600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR OR  SPAR JUST INBOARD OF GEAR SUPPORT RIB 6 65000 FH  I: 8900 FC  OR  38700 FH  575013-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM T: 6 YE NO  600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR I: 6 YE  SPAR JUST INBOARD OF GEAR SUPPORT RIB 6  575014-01-1 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  670 TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED OR  BY MLG REINFORCING 60000 FH  I: 9200 FC  OR  34800 FH  575014-01-2 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED OR  BY MLG REINFORCING 60000 FH  I: 10700 FC  OR  40800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575014-01-3 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED OR  BY MLG REINFORCING 26000 FH  I: 13000 FC  OR  26000 FH  575014-01-4 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  670 TRAILING EDGE BOTTOM SKIN AFT OR REAR SPAR COVERED OR  BY MLG REINFORCING 65000 FH  I: 13000 FC  OR  65000 FH  575015-01-1 454HL 464HL 532AB 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE NO  533AB 534AB 632AB 464 EDGE BOTTOM SKIN LOWER SURFACE AFT REAR SPAR FROM I: 12 YE  633AB 634AB 500 RIB 12 TO RIB 39.  532  533  534  600  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575016-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YE  UNDER FLAP TRACK 2 FAIRING. 13000 FC  OR  60000 FH  I: 12 YE  OR  5600 FC  OR  21400 FH  575016-01-2 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YE  UNDER FLAP TRACK 2 FAIRING. 13000 FC  OR  60000 FH  I: 12 YE  OR  3200 FC  OR  12400 FH  575016-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YE  UNDER FLAP TRACK 2 FAIRING. 13000 FC  OR  26000 FH  I: 12 YE  OR  5600 FC  OR  11200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575016-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  631 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR I: 12 YE  UNDER FLAP TRACK 2 FAIRING. 13000 FC  OR  65000 FH  I: 12 YE  OR  11800 FC  OR  51100 FH  575016-02-1 N/A TASK DELETED  575017-01-1 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE OR  CUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 60000 FH  JUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 4800 FC  OR  18200 FH  575017-01-2 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE OR  CUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 60000 FH  JUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 2700 FC  OR  10500 FH  575017-01-3 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE OR  CUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 26000 FH  JUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 5200 FC  OR  10400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575017-01-4 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING T: 13000 FC  673 TRAILING EDGE BOTTOM SKIN 50 MM AROUND MANHOLE OR  CUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR 65000 FH  JUST OUTBOARD OF GEAR SUPPORT RIB 6. I: 13000 FC  OR  65000 FH  575017-02-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 6 YE NO  673 EDGE BOTTOM SKIN 50MM AROUND MANHOLE CUTOUT, I: 6 YE  INTERNAL AND EXTERNAL, AFT OR REAR SPAR JUST  OUTBOARD OF GEAR SUPPORT RIB 6.  575018-01-1 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  192CT 672 EDGE ATTACHMENT OF SHROUD BOX OR  FLAPS EXTENDED 60000 FH  I: 6800 FC  OR  26000 FH  575018-01-2 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  192CT 672 EDGE ATTACHMENT OF SHROUD BOX OR  FLAPS EXTENDED 26000 FH  I: 9200 FC  OR  18400 FH  575018-02-1 147AT 148AT 191CT 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 10 YE  192CT 672 EDGE ATTACHMENT OF SHROUD BOX. I: 10 YE  FLAPS EXTENDED  575019-01-1 147AT 148AT 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 10 YE  671 EDGE ATTACHMENT OF OVERWING PANEL. I: 10 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575022-01-1 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12300 FC  ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN  OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO  HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575022-01-2 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12300 FC  ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN  OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO  HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575022-01-3 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 10600 FC  ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN  OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO  HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575022-01-6 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  675BB 675 EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT I: 12 YE I: 12 YE  ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN  OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO  HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575023-01-1 N/A TASK DELETED  575023-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575023-01-5 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  675DB 675 EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT I: 12 YE I: 12 YE  ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN  OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO  HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575025-01-1 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  531 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  600 FROM RIB 8 TO RIB 12 60000 FH  631 I: 5200 FC  OR  19700 FH  575025-01-2 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  531 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  600 FROM RIB 8 TO RIB 12 60000 FH  631 I: 3700 FC  OR  14200 FH  575025-01-3 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  FROM RIB 8 TO RIB 12 26000 FH  I: 5000 FC  OR  10000 FH  575025-01-9 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING T: 13000 FC  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  FROM RIB 8 TO RIB 12 65000 FH  I: 4600 FC  OR  20000 FH  575025-02-1 531AB 631AB 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 12 YE  FROM RIB 8 TO RIB 12.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575051-01-1 N/A TASK DELETED  575053-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, T: 12 YE T: 20 YE  FLAPS EXTENDED 148 DRIVE LINK, DRIVE LEVER, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YE  575053-01-2 N/A TASK DELETED  R 575054-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR T: 12 YE T: 20 YE  FLAPS EXTENDED 148 BOX, FORK ASSY, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YE  575055-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, T: 12 YE T: 20 YE  148 ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), I: 12 YE I: 12 YE  INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.  575055-01-2 N/A TASK DELETED  575057-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575059-01-1 AFT FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, T: 12 YE T: 20 YE  FAIRINGS 532 4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH I: 12 YE I: 12 YE  FLAPS EXTENDED 533 TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK  534 AND TRAVELLING BEAM AT TRACK NO.4.  631  632  633  634  575059-01-2 N/A TASK DELETED  R 575061-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, T: 12 YE T: 20 YE  532 4 AND 5, CARRIAGE ASSEMBLIES. I: 12 YE I: 12 YE  533  534  631  632  633  634  575061-01-2 N/A TASK DELETED  575063-01-1 N/A TASK DELETED  575063-01-2 FLAP TRACK FAIRING 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO. 2, 3, 4 T: 12 YE  REMOVED 532 AND 5 LOWER FLANGES, STRAP AND ANGLES. I: 12 YE  533  534  631  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575065-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO  532 NO.2, 3, 4 AND 5, INTERNAL STRUCTURE. I: 12 YE I: 12 YE  533  534  631  632  633  634  R 575067-01-1 FWD FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2,3,4 T: 12 YE T: 20 YE  FAIRINGS 532 AND 5, FORWARD ATTACHMENT SPIGOTS,EXTERNAL STRUCTURE. I: 12 YE I: 12 YE  533  534  631  632  633  634  575067-01-2 N/A TASK DELETED  R 575067-02-1 FS BOLTS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO  FWD FLAP TRACK 532 NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS, I: 12 YE I: 12 YE  FAIRINGS 533 INTERNAL STRUCTURE.  534  631  632  633  634  575067-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575069-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO  532 NO.2, 3, 4 AND 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE  533  534  631  632  633  634  575069-01-2 N/A TASK DELETED  R 575074-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOX T: 12 YE T: 20 YE  FLAPS EXTENDED 148 SUPPORT, FORK ASSEMBLY, DRIVE STRUT AND I: 12 YE I: 12 YE  CARRIAGE.  R 575075-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, ATTACHMENT T: 12 YE T: 20 YE  148 TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING I: 12 YE I: 12 YE  SUPPORT STRUTS WITH ATTACHMENT FITTING.  R 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  FAIRINGS 532 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH I: 12 YE I: 12 YE  FLAPS EXTENDED 533 TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT  534 LINK AND TRAVELING BEAM AT TRACK NO.4.  631  632  633  634  R 575081-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, T: 12 YE T: 20 YE  532 CARRIAGE ASSEMBLIES. I: 12 YE I: 12 YE  533  534  631  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575083-01-1 FLAP TRACK FAIRINGS 531 FLAP TRACK BEAM NO.2, 3, 4 AND 5 LOWER FLANGES, T: 12 YE  532 STRAP AND ANGLES. I: 12 YE  533  534  631  632  633  634  R 575085-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, T: 12 YE T: 20 YE NO  532 3, 4 AND 5, INTERNAL STRUCTURE. I: 12 YE I: 12 YE  533  534  631  632  633  634  R 575087-01-1 FS BOLT 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 T: 12 YE T: 20 YE NO  FWD FLAP TRACK 532 AND 5, FORWARD ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE  FAIRINGS 533  534  631  632  633  634  R 575087-02-1 FS BOLT 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS T: 12 YE T: 20 YE NO  FWD FLAP TRACK 532 NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE  FAIRINGS 533  534  631  632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575089-01-1 FLAP TRACK FAIRINGS 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 T: 12 YE T: 20 YE  532 AND 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE  533  534  631  632  633  634  575101-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 EDGE SPOILER 1 ACTUATOR SUPPORT FITTING. I: 12 YE I: 12 YE  575102-01-1 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING T: 12 YE T: 20 YE  673FB 673 EDGE RIBS 1-6, COMPRISING ATTACHMENTS TO REAR I: 12 YE I: 12 YE  SPAR OR FALSE REAR SPAR AND SPOILER 1 HINGE  FITTINGS.  575103-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING I: 12 YE I: 12 YE  (5 PLACES) LUGS AND ATTACHMENT TO REAR SPAR AND  TOP AND BOTTOM SKIN OVERHANGS.  575105-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS AND I: 12 YE I: 12 YE  OUTER LINK HINGE RIBS (18 RIBS).  575106-01-1 575AB 575CB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675CB 675 INBOARD AND OUTBOARD AILERON JACK BRACKETS I: 12 YE I: 12 YE  (4 PLACES) AT LUG AND ATTACHMENT TO TOP AND  BOTTOM SKIN OVERHANGS (INTERNAL AND EXTERNAL).  575108-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 574 RIB 10 FLAP CRUISE ROLLERS SUPPORT. I: 12 YE I: 12 YE  673  674  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575109-01-1 573BB 573FB 673BB 573 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  673FB 673 EDGE RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, I: 12 YE  TOP AND BOTTOM SKIN OVERHANGS AND OUTER FLAP  CRUISE ROLLER SUPPORT ATTACHMENT TO TRAILING  EDGE RIB 10.  575110-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. I: 12 YE I: 12 YE  575111-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  600 EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR I: 12 YE  BETWEEN RIB 1 AND RIB 14.  575112-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 6 YE  600 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR I: 6 YE  SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA  COVERED BY FLAP TRACK 2 FAIRING.  575115-01-1 FLAP TRACK 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  PYLON FAIRINGS 464 EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR I: 12 YE  500 SPAR FROM RIB 12 TO RIB 41.  532  533  534  600  632  633  634  575116-01-1 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR I: 12 YE I: 12 YE  UNDER FLAP TRACK 2 FAIRING.  575117-01-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO  673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL I: 6 YE  AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF  GEAR RIB 6.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575118-01-1 732 742 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  FLAPS EXTENDED 672 EDGE ATTACHMENT OF SHROUD BOX. I: 12 YE  575119-01-1 732 742 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING T: 12 YE  FLAPS EXTENDED 671 EDGE ATTACHMENT OF OVERWING PANEL. I: 12 YE  575122-01-1 575AB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE- T: 12 YE T: 20 YE  675 INNER AILERON HINGES 1-3 AND THE TOP AND BOTTOM SKIN I: 12 YE I: 12 YE  OVERHANGS UPPER AND LOWER SURFACES AT THESE  LOCATIONS.  575123-01-1 575CB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE- T: 12 YE T: 20 YE  675 OUTER AILERON HINGES 1-3 AND THE TOP AND BOTTOM SKIN I: 12 YE I: 12 YE  OVERHANGS UPPER AND LOWER SURFACES AT THESE  LOCATIONS.  575126-01-1 575BB 675BB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675 INNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS I: 12 YE I: 12 YE  AND THE TOP AND BOTTOM SKINS UPPER AND LOWER  SURFACES 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  675 OUTER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS I: 12 YE I: 12 YE  AND THE TOP AND BOTTOM SKINS UPPER AND LOWER  SURFACES AT THE ATTACHMENTS TO THE POSTS.  575401-01-1 N/A TASK DELETED  575401-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL T: 6 YE  600 SURFACE OF UPPER AND LOWER SKIN. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575401-02-1 N/A TASK DELETED  575402-01-1 N/A TASK DELETED  R 575403-01-1 581AB 681AB 734 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  744 681 SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL I: 12 YE I: 12 YE  AND EXTERNAL.  575403-01-2 N/A TASK DELETED  R 575403-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO  744 681 INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, I: 12 YE I: 12 YE  SPEED TAPES INTERNAL.  N 575404-01-1 FLAPS EXTENDED 581 GENERAL VISUAL INSPECTION OF INBOARD FLAP TRAILING T: 6 YE  681 EDGE. I: 6 YE  N 575404-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 6 YE  681 EDGE. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 575404-03-2 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 12 YE  681 EDGE. I: 12 YE  R 575405-01-1 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  631CB 681 SUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVE I: 12 YE I: 12 YE  FLAPS EXTENDED STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE  ARM ATTACHMENT BRACKET.  575405-01-2 N/A TASK DELETED  R 575405-01-3 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  631CB 681 SUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVE I: 12 YE I: 12 YE  FLAPS EXTENDED STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE  ARM ATTACHMENT BRACKET.  R 575405-02-1 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO  631CB 681 INTERNAL SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575405-02-2 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO  631CB 681 INTERNAL SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  R 575407-01-1 FLAPS EXTENDED 581 DETAILED INSPECTION OF INBOARD FLAP, OUTER T: 12 YE T: 20 YE NO  RUBBER SEALS 681 END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT I: 12 YE I: 12 YE  ATTACHMENT BRACKET.  R 575409-01-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  SPEED TAPES 681 STRUCTURE. I: 12 YE I: 12 YE  R 575451-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, T: 6 YE  600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN. I: 6 YE  575451-01-2 N/A TASK DELETED  R 575453-01-1 581AB 681AB 734 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE  744 681 FITTING AT TRACK NO.1 AND TRUNION, INTERNAL AND I: 12 YE I: 12 YE  EXTERNAL.  R 575453-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, T: 12 YE T: 20 YE NO  744 681 INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNION, I: 12 YE I: 12 YE  PLUGS INTERNAL.  SPEED TAPES  N 575454-01-1 FLAPS EXTENDED 581 GENERAL VISUAL INSPECTION OF INBOARD FLAP TRAILING T: 6 YE  681 EDGE. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 N 575454-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP T: 12 YE  681 TRAILING EDGE. I: 12 YE  R 575455-01-1 531SB 531VT 631SB 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE  631VT 681 FITTING AT TRACK NO.2 AND EXTERNAL DRIVE STRUT I: 12 YE I: 12 YE  FLAPS EXTENDED BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM  SPEED TAPES ATTACHMENT BRACKET.  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME  AS 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  631VT 681 INTERNAL SUPPORT FITTING AT TRACK NO. 2. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  575457-01-1 FLAPS EXTENDED 581 DETAILED INSPECTION OF INBOARD FLAP, OUTER T: 12 YE T: 20 YE  RUBBER SEALS 681 END-RIB INCLUDING ROLLER AND INTERCONNECTION STRUT I: 12 YE I: 12 YE  ATTACHMENT BRACKET.  R 575459-01-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  SPEED TAPES 681 STRUCTURE. I: 12 YE I: 12 YE  575501-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YE  600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN I: 6 YE  N 575501-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YE  600 EXTERNAL SURFACES OF UPPER AND LOWER SKIN. I: 6 YE  R 575503-01-1 532AT 532CB 632AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE  632CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.3, AND I: 12 YE I: 12 YE  FLAPS EXTENDED EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINK  TO CARRIAGE WITH ASSOCIATED ATTACHMENT FITTING  AND GUIDE ARM ATTACHMENT FITTING.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575503-01-2 N/A TASK DELETED  R 575503-02-1 532AT 532CB 632AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  632CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.3. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  575503-02-2 N/A TASK DELETED  R 575505-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE  633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.4, AND I: 12 YE I: 12 YE  FLAPS EXTENDED EXTERNAL FWD SUPPORT LINK AND AFT SUPPORT LINK  ATTACH FITTING.  575505-01-2 N/A TASK DELETED  R 575505-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE  633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.4. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  575505-02-2 N/A TASK DELETED  R 575507-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE  633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.5, AND I: 12 YE I: 12 YE  FLAPS EXTENDED EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TO  CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE  ARM ATTACH FITTING.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575507-01-2 N/A TASK DELETED  R 575507-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO.5. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  575507-02-2 N/A TASK DELETED  575509-01-1 FLAPS EXTENDED 583 DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 12 YE T: 20 YE  RUBBER SEALS 683 SURFACE OF INNER END RIB INCLUDING ROLLER AND I: 12 YE I: 12 YE  INTERCONNECTION STRUT ATTACHMENT BRACKET.  575509-01-2 N/A TASK DELETED  575509-02-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  RUBBER SEALS 683 INTERNAL STRUCTURE OF INNER END RIB. I: 12 YE I: 12 YE  SPEED TAPES  575509-02-2 N/A TASK DELETED  R 575551-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, T: 6 YE  600 EXTERNAL SURFACE OF UPPER AND LOWER SKIN RH/LH. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 R 575553-01-1 532SB 532VT 632SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  632VT 683 SUPPORT FITTING AT TRACK NO. 3, AND EXTERNAL DRIVE I: 12 YE I: 12 YE  FLAPS EXTENDED STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE  WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH  FITTING.  R 575553-02-1 532SB 532VT 632SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  632VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 3. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  R 575555-01-1 533SB 533VT 633SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  633VT 683 SUPPORT FITTING AT TRACK NO. 4, AND EXTERNAL FWD I: 12 YE I: 12 YE  FLAPS EXTENDED SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.  R 575555-02-1 533SB 533VT 633SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  633VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 4. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  R 575557-01-1 533SB 533VT 633SB 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  633VT 683 SUPPORT FITTING AT TRACK NO. 5, AND EXTERNAL DRIVE I: 12 YE I: 12 YE  FLAPS EXTENDED STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITH  ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH  FITTING.  R 575557-02-1 533SB 533VT 633SB 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  633VT 683 INTERNAL SUPPORT FITTING AT TRACK NO. 5. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  575559-01-1 FLAPS EXTENDED 583 DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 12 YE T: 20 YE  RUBBER SEALS 683 SURFACE OF INNER END RIB INCLUDING ROLLER AND I: 12 YE I: 12 YE  INTERCONNECTION STRUT ATTACHMENT BRACKET.  575559-02-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  RUBBER SEALS 683 INTERNAL STRUCTURE OF INNER END RIB. I: 12 YE I: 12 YE  SPEED TAPES  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 575561-01-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO  PLUGS 683 INTERNAL STRUCTURE. I: 12 YE I: 12 YE  SPEED TAPES  576101-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, T: 6 YE  690 UPPER AND LOWER SKINS, EXTERNAL SURFACE. I: 6 YE  576103-01-1 ONLY OUTBOARD 592 DETAILED INSPECTION OF OUTBOARD AILERON END T: 12 YE T: 20 YE  AILERON DEFLECTED 692 RIBS, EXTERNAL SURFACE. I: 12 YE I: 12 YE  576104-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON T: 12 YE T: 20 YE  592AB 592BB 592CB 692 FITTINGS (7 PLACES). I: 12 YE I: 12 YE  592DB 675BT 675CB  675DB 692AB 692BB  692CB 692DB  576106-01-1 JACK FITTING FAIRING 592 DETAILED INSPECTION OF OUTBOARD AILERONS, T: 14600 FC  692 FIRST LINE OF FASTENERS ON OUTER JACK FITTING I: 5100 FC  FLANGE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  576106-02-1  576106-02-1 JACK FITTING FAIRING 592 SPECIAL DETAILED INSPECTION OF OUTBOARD T: 14600 FC  692 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 14600 FC  FITTING FLANGE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  576106-01-1  576111-01-1 N/A 500 DETAILED INSPECTION OF INBOARD AILERON, T: 6 YE  600 UPPER AND LOWER SKINS, EXTERNAL SURFACE. I: 6 YE  576113-01-1 INBOARD AILERON ONLY 591 DETAILED INSPECTION OF INBOARD AILERON END T: 12 YE T: 20 YE  DEFLECTED 691 RIBS, EXTERNAL SURFACE. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 576114-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON T: 12 YE T: 20 YE  591AB 591BB 591CB 691 FITTINGS (7 PLACES). I: 12 YE I: 12 YE  591DB 675AB 675AT  675BB 691AB 691BB  691CB 691DB  576116-01-1 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD T: 13000 FC  691 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 6200 FC  FITTING FLANGE, LH/RH  576116-01-2 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD T: 14600 FC  691 AILERONS, FIRST LINE OF FASTENERS ON OUTER JACK I: 14600 FC  FITTING FLANGE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  576116-02-1.  576116-02-1 JACK FITTING FAIRING 591 DETAILED INSPECTION OF INBOARD AILERONS, T: 14600 FC  691 FIRST LINE OF FASTENERS ON OUTER JACK FITTING I: 5100 FC  FLANGE, LH/RH.  NOTE : THIS TASK IS AN ALTERNATIVE TO TASK  576116-01-2.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 576151-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, UPPER AND T: 6 YE  592 LOWER SKINS, EXTERNAL SURFACE. I: 6 YE  690  576153-01-1 ONLY OUTBOARD 592 DETAILED INSPECTION OF OUTBOARD AILERON END RIBS, T: 12 YE T: 20 YE  AILERON DEFLECTED 692 EXTERNAL SURFACE. I: 12 YE I: 12 YE  576154-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS T: 12 YE T: 20 YE  592AB 592BB 592CB 692 (7 PLACES). I: 12 YE I: 12 YE  592DB 675BT 675CB  675DB 692AB 692BB  692CB 692DB  576161-01-1 N/A 590 DETAILED INSPECTION OF INBOARD AILERON, UPPER AND T: 6 YE  690 LOWER SKINS, EXTERNAL SURFACE. I: 6 YE  576163-01-1 ONLY INBOARD AILERON 591 DETAILED INSPECTION OF INBOARD AILERON END RIBS, T: 12 YE T: 20 YE  DEFLECTED 691 EXTERNAL SURFACE. I: 12 YE I: 12 YE  576164-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON FITTINGS T: 12 YE T: 20 YE NO  591AB 591BB 591CB 691 (7 PLACES). I: 12 YE I: 12 YE  591DB 675AB 675AT  675BB 691AB 691BB  691CB 691DB  R 577001-01-1 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO.1, T: 6 YE  SPOILERS DEPLOYED 682 UPPER AND LOWER SKIN, EXTERNAL SURFACE, LH/RH. I: 6 YE  R 577003-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO.1, HINGE T: 12 YE T: 20 YE  SPOILERS DEPLOYED 682 AND ACTUATOR ATTACHMENT FITTINGS. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 577003-01-2 N/A TASK DELETED  577003-02-1 N/A TASK DELETED  R 577051-01-1 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO. 1 AND 2, T: 6 YE  SPOILERS DEPLOYED 584 UPPER AND LOWER SKIN, EXTERNAL SURFACE. I: 6 YE  682  684  R 577053-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO.1 AND NO.2, HINGE T: 12 YE T: 20 YE  SPOILERS DEPLOYED 584 AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES). I: 12 YE I: 12 YE  682  684  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 711151-01-1 415AL 416AR 425AL 411 DETAILED INSPECTION OF INLET COWL ATTACHMENT AND T: 6 YE NO  426AR 435AL 436AR 421 SURROUNDING STRUCTURE (15 CM AROUND THE A1 FLANGE). I: 6 YE  445AL 446AR 431  441  711311-02-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL HINGE FITTINGS T: 6 YE NO  426AR 435AL 436AR 416 AND SURROUNDING STRUCTURE (15 CM AROUND HINGES) I: 6 YE  445AL 446AR 425  426  435  436  445  446  711312-01-2 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL LATCHES AND T: 6 YE NO  426AR 435AL 436AR 416 SURROUNDING STRUCTURE 15 CM AROUND LATCHES I: 6 YE  445AL 446AR 425  426  435  436  445  446  711351-01-1 N/A TASK DELETED  711352-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL LATCH T: 6 YE NO  426AR 435AL 436AR 416 FITTINGS AND SURROUNDING STRUCTURE I: 6 YE  445AL 446AR 425 (15 CM AROUND FITTINGS).  426  435  436  445  446  712101-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 712101-01-2 N/A TASK DELETED  712101-02-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT T: 12 YE NO  FORWARD ENGINE MOUNT 423 INSTALLATION . I: 12 YE  DISASSEMBLED 433  443  712151-01-1 415AL 416AR 417AL 413 DETAILED INSPECTION OF TRENT 500-ENGINE FORWARD MOUNT T: 12 YE NO  418AR 425AL 426AR 423 INSTALLATION. I: 12 YE  427AL 428AR 435AL 433  436AR 437AL 438AR 443  445AL 446AR 447AL  448AR  ENGINE  ENGINE MOUNT  DISASSEMBLED  712152-01-1 N/A TASK DELETED  712153-01-1 N/A TASK DELETED  712201-01-1 N/A TASK DELETED  712201-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 712201-02-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION. T: 12 YE NO  DISASSEMBLED 423 I: 12 YE  ENGINE 433  443  712251-01-1 415AL 416AR 417AL 413 DETAILED INSPECTION OF TRENT 500-ENGINE REAR MOUNT T: 12 YE NO  418AR 425AL 426AR 423 INSTALLATION. I: 12 YE  427AL 428AR 435AL 433  436AR 437AL 438AR 443  445AL 446AR 447AL  448AR  ENGINE  REAR ENGINE MOUNT  712252-01-1 N/A TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 722301-02-1 415AL 416AR 417AL 412 GENERAL VISUAL INSPECTION OF FAN CASE V-GROOVE INNER T: 6 YE NO  418AR 425AL 426AR 422 RADIUS I: 6 YE  427AL 428AR 435AL 432  436AR 437AL 438AR 442  445AL 446AR 447AL  448AR  723151-01-1 415AL 416AR 417AL 412 DETAILED INSPECTION OF TRENT 500- LP COMPRESSOR REAR T: 6 YE NO  418AR 425AL 426AR 422 FANCASE V GROOVE. I: 6 YE  427AL 428AR 435AL 432 NOTE : TASK TO BE PERFORMED AT THE SAME TIME AS TASK  436AR 437AL 438AR 442 783255-01-1  445AL 446AR 447AL  448AR  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: D-72 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 783205-02-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER J-RING RADIUS T: 6 YE NO  418AR 425AL 426AR 418 I: 6 YE  427AL 428AR 435AL 427  436AR 437AL 438AR 428  445AL 446AR 447AL 437  448AR 438  447  448  783207-01-1 415AL 416AR 425AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 6 YE NO  426AR 435AL 436AR 418 12 O ́CLOCK BEAM AND FORWARD FRAME JUNCTION I: 6 YE  445AL 446AR 427  THRUST REVERSER 428  DEPLOYED 437  438  447  448  783208-01-1 415AL 416AR 425AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 6 YE NO  426AR 435AL 436AR 418 6 O ́CLOCK BEAM AND FORWARD FRAME JUNCTION I: 6 YE  445AL 446AR 427  THRUST REVERSER 428  DEPLOYED 437  438  447  448  783209-01-1 415AL 416AR 425AL 417 DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME T: 6 YE NO  426AR 435AL 436AR 418 LOWER AND UPPER FITTINGS I: 6 YE  445AL 446AR 427  428  437  438  447  448  ISSUE: JUL 01/10 EXHAUST SECTION: D-78 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 783211-02-1 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER COWL T: 6 YE NO  418AR 425AL 426AR 418 HINGE FITTINGS AND SURROUNDING STRUCTURE (15 CM I: 6 YE  427AL 428AR 435AL 427 AROUND FITTINGS)  436AR 437AL 438AR 428  445AL 446AR 447AL 437  448AR 438  HINGE ACCESS PANEL 447  448  783212-01-2 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER COWL LATCH T: 6 YE NO  418AR 425AL 426AR 418 ASSEMBLY AND SURROUNDING STRUCTURE (15 CM AROUND I: 6 YE  427AL 428AR 435AL 427 FITTINGS)  436AR 437AL 438AR 428  445AL 446AR 447AL 437  448AR 438  447  448  783251-01-1 417EL 418ER 427EL 417 DETAILED INSPECTION OF THRUST REVERSER HINGE LUGS AND T: 6 YE NO  428ER 437EL 438ER 418 SURROUNDING STRUCTURE (15 CM AROUND HINGE LUGS). I: 6 YE  447EL 448ER 427  428  437  438  447  448  783251-01-2 N/A TASK DELETED  783252-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER 6 O ́CLOCK BEAM T: 6 YE NO  417FL 418AR 425AL 418 LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING I: 6 YE  426AR 427AL 427FL 427 STRUCTURE (15 CM AROUND LATCH FITTINGS).  428AR 435AL 436AR 428  437AL 437FL 438AR 437  445AL 446AR 447AL 438  447FL 448AR 447  448  ISSUE: JUL 01/10 EXHAUST SECTION: D-78 
A340 MRB REPORT – Structures Section

TASK ACCESS ZONE 

REFERENCE

TASK DESCRIPTION SAMPLE THRESHOLD

INTERVAL 

C

100% 

THRESHOLD

INTERVAL 

TPS

 783253-01-1 414AL 414AR 415AL 414 DETAILED INSPECTION OF THRUST REVERSER AFT CORE COWL T: 6 YE NO  416AR 417AL 417FL 424 LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING I: 6 YE  418AR 424AL 424AR 434 STRUCTURE (15 CM AROUND LATCH FITTING).  425AL 426AR 427AL 444  427FL 428AR 434AL  434AR 435AL 436AR  437AL 437FL 438AR  444AL 444AR 445AL  446AR 447AL 447FL  448AR  783254-01-1 415AL 416AR 417CL 417 DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME T: 6 YE NO  417DL 417EL 418CR 418 AND TRANSCOWL ACTUATOR FITTINGS AND ITS ATTACHMENTS I: 6 YE  418DR 418ER 425AL 427 (6 PLACES ON EACH HALF).  426AR 427CL 427DL 428  427EL 428CR 428DR 437  428ER 435AL 436AR 438  437CL 437DL 437EL 447  438CR 438DR 438ER 448  445AL 446AR 447CL  447DL 447EL 448CR  448DR 448ER  783254-01-2 N/A TASK DELETED  783255-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER J RING (V T: 6 YE NO  417FL 418AR 425AL 418 BLADE). I: 6 YE  426AR 427AL 427FL 427 NOTE : TASK TO BE PERFORMED AT THE SAME TIME AS TASK  428AR 435AL 436AR 428 723151-01-1  437AL 437FL 438AR 437  445AL 446AR 447AL 438  447FL 448AR 447  448  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: D-78 
 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, flashlight 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, ladders 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 MRBR and 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 manufacturer 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 considered 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 REPORT 

Issue : July 2010 6. EXPLANATION OF ZONAL SECTION FORMAT

Detailed information is given below concerning the format of the inspection requirements provided on subsequent pages. 

TASK 

REFERENCE 

ACCESS ZONE DESCRIPTION INTERVAL MSI / SSI 

REFERENCE 

 1 2 3 4 5 6 

1- This column indicates the zonal task number, e.g. ZL 151-01-1. It is composed of 9 digits as follows:

 ZL XXX – XX – XX 

The Zone number is represented by the three first digits, ZL 151-01-01. The first digit, ZL151-01-01, is in accordance with the breakdown, showing the major section where the zone is located e.g 100 Lower Half of Fuselage. The second digit, ZL151-01

with the A340 ATA 100 breakdown, showing the sub section where the zone is located e.g 150 Aft Cargo Compartment. The tshows 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 151-0

content inspections at different intervals . The Applicability Index is composed of one digit. It follows the Sequential Number and is separated by a dash, ZL 151-0

applicability e.g aircraft model/mod status etc ...This digit is also used to differentiate between access differences e.g. differ

and differences in reference information. 

Applicability index: Identifies successive variants of the task Sequence number: Indicates separate tasks within in the same zone 

Zone number: Indicates the zone number 

ZL: Abbreviation for Zonal 
 A340 MRB REPORT 

Issue : July 2010 

2- 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 rem(ii) It defines the configuration of the aircraft, if necessary 

e.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 sim

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 prov

the Inspection area e.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 APU331-350  60 stands for APU331-600  C5 stands for CFM56-5 engine  R5 stands for RRT500 engine  7- This column indicates the A/C model/Mod status/engine type to which this requirement is applicable 
 A340 MRB REPORT 

This page intentionally left blank
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-100-01-1 N/A 100 LOWER HALF OF FUSELAGE I: C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 ZL-100-01-2 N/A 100 LOWER HALF OF FUSELAGE I: C MSI N SSI 5 SSI 5 SSI 5 SSI 5 R ZL-110-01-1 110AL 110 RADOME (EWIS) I: 2 C MSI N SSI N R ZL-121-01-1 132AZ 821 121 AVIONICS COMPARTMENT (EWIS) I: C MSI N 122  SSI N R ZL-121-01-2 121AL 121BL 121CL 121 AVIONICS COMPARTMENT (EWIS) I: C MSI N 121DL 121EL 132AZ 122  821 SSI N R ZL-121-02-1 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 2 121DF 121EF 121FF 122 MSI 2 121GF 121HF 121KF  122CF 122DF 122FF SSI N 122GF 122HF 122JF  122LF 122MF 122NF  122PF 131AW 131BW  132AZ 132CW 821  NOTE 1  R ZL-121-02-2 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 2 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-121-02-2 * * * * * C O N T I N U E * * * * *  121DF 121EF 121FF 122 MSI 2 121GF 121HF 121JF  121KF 121LF 122AF SSI N 122AZ 122BF 122CF  122DF 122EF 122FF  122GF 122HF 122JF  131AW 131BW 132AZ  132CW 821  NOTE 1  R ZL-121-02-3 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 2 121DF 121EF 121GF 122 MSI 2 121HF 121JF 121KF  121LF 122AF 122AZ SSI N 122BF 122CF 122DF  122EF 122FF 122GF  122HF 122JF 131AW  131BW 132AZ 132CW  821  NOTE 1  R ZL-123-01-1 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI N SSI N R ZL-123-01-2 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI N SSI N R ZL-131-01-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: A MSI 2 132 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-131-01-1 * * * * * C O N T I N U E * * * * *  MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 SSI N R ZL-131-01-2 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: A MSI 2 132 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 SSI N R ZL-131-02-1 131BC 131FC 131KC 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI N 131KW 131MC 131PC 132  131QW 131RC 131TC SSI N 131VC 132QW 132SW  132UW 821  R ZL-131-02-2 131AA 131CX 131DA 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI N 131DM 131NA 131PM 132  131QA 131SA 131TM SSI N 131UA 131WA 131YA  132AZ 132CX 132EW  132PM 132RM 132VM  132ZM 821  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-131-02-3 131AA 131CX 131DA 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI N 131DM 131GA 131HM 132  131JA 131LA 131NA SSI N 131PM 131QA 131SA  131TM 131UA 131WA  132AZ 132CX 132EW  132HM 132KM 132MM  132PM 132RM 132TM  132VM 821  R ZL-131-03-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 NOTE 1 132  SIDEWALL AND CEILING SSI 5 PANELS FROM FR20 TO  FR 39.2  R ZL-131-03-2 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 NOTE 1 132  SIDEWALL AND CEILING SSI 5 PANELS FROM FR 20 TO  BETWEEN FR 39/FR  39.1  R ZL-133-01-1 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 FLOOR PANELS FROM FR 134 MSI 3 20 TO FR 39  NOTE 1 SSI N R ZL-133-01-2 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 3 FLOOR PANELS FROM FR 134  20 TO FR 39 SSI N NOTE 1  R ZL-137-01-1 131BX 131CG 131CX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 131DG 131DX 132CG 138  132CX 132DG 132DX SSI N 821  R ZL-137-01-2 131BX 131CX 131DX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-137-01-2 * * * * * C O N T I N U E * * * * *  131JK 131LK 131MK 138 SSI N 132CX 132DX 132JK  132LK 132MK 821  R ZL-137-01-3 131BX 131CX 131DX 137 BAY BEHIND FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 131MH 131TH 131VH 138  132CX 132DX 132MH SSI N 132TH 132VH 132WH  821  R ZL-141-01-1 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI N 744 142  SSI 5 R ZL-141-01-2 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI N 744 142  SSI 5 R ZL-143-01-1 734 744 143 AREA BETWEEN KEEL BEAMS (EWIS) I: 8 C MSI N SSI N R ZL-145-01-1 834 844 145 ZONE UNDER CABIN FLOOR (EWIS) I: 8 C MSI N FLOOR PANELS FROM FR 146  40 TO FR 53.2 SSI N R ZL-147-01-1 734 744 147 MLG WELL AND HYDRAULIC COMPARTMENT (EWIS) I: A MSI 2 148 MSI 2 SSI N R ZL-147-01-2 734 744 147 MLG WELL AND HYDRAULIC COMPARTMENT (EWIS) I: A MSI 2 148  SSI N ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-149-01-1 753 754 149 CENTER LINE GEAR WELL (EWIS) I: C MSI N SSI N R ZL-149-01-2 753 754 149 CENTER LINE GEAR WELL (EWIS) I: C MSI N SSI N R ZL-149-02-1 149AB 149CB 753 149 CENTER LINE GEAR WELL (EWIS) I: 8 C MSI N 754  SSI N R ZL-151-01-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: A MSI 2 152 MSI 2 (IF LD-MCR OR LDF AND/OR DCR AND/OR ACT(S) MSI 2 INSTALLED , AS FAR AS VISIBLE) MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 MSI 2 SSI N R ZL-151-02-1 151BC 151BW 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151HC 151JW 151KC 152  151PC 151TW 152BW SSI N 152DW 152EW 152GW  152JW 152LW 822  LD-MCR (IF  INSTALLED)  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-151-02-2 151BW 151BY 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151HC 151JW 151KC 152  151PC 151TW 152AX SSI N 152BW 152BX 152DW  152JW 152LW 822  ACT(S)  LD-MCR (IF  INSTALLED)  R ZL-151-02-3 151BQ 151HM 151NA 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151RA 151RM 151UA 152  151WA 151YA 151YM SSI N 152BQ 152CQ 152NA  152PW 152RA 152UA  152UW 152VM 152WA  152XM 152YA 822  LD-MCR (IF  INSTALLED)  R ZL-151-02-4 151AA 151BW 151CA 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151EA 151GA 151HM 152  151JA 151LA 151NA SSI N 151RA 151RM 152AA  152BM 152BW 152CA  152CW 152EA 152FM  152GA 152HM 152JA  152KM 152LA 152MM  152NA 152PW 152RA  152UW 822  LD-MCR OR LDF  FURNISHING AND/OR  DCR (IF INSTALLED)  R ZL-151-03-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 ACT(S) AND/OR LD-MCR 152  (IF INSTALLED) SSI N LDL FURNISHING  NOTE 1  SIDEWALL AND CEILING  PANELS FROM FR 53.2  TO FR 66  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-151-03-2 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 LD-MCR (IF 152  INSTALLED) SSI N NOTE 1  SIDEWALL AND CEILING  PANELS FROM FR 53.7  TO FR 66  R ZL-151-03-3 822 000 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 LD-MCR OR LDF 151  FURNISHING AND/OR 152 SSI N DCR (IF INSTALLED)  NOTE 1  SIDEWALL AND CEILING  PANELS FROM FR 53.2  TO FR 66  R ZL-153-01-1 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 FLOOR PANELS FROM FR 154 MSI 3 53.2 TO FR 66  LD-MCR AND/OR ACT(S) SSI N (IF INSTALLED)  NOTE 1  R ZL-153-01-2 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 FLOOR PANELS FROM FR 154 MSI 3 53.7 TO FR 66  LD-MCR (IF SSI N INSTALLED)  NOTE 1  R ZL-153-01-3 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 3 FLOOR PANELS FROM FR 154  53.2 TO FR 66 SSI N LD-MCR OR LDF  FURNISHING AND/OR  DCR (IF INSTALLED)  NOTE 1  R ZL-155-01-1 153AZ 155AZ 197CB 155 REAR CENTER TANK (EWIS) I: 8 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-155-01-1 * * * * * C O N T I N U E * * * * *  FUEL PUMPS AND PIPES SSI 5 LINERS TO BE REMOVED SSI 5 R ZL-161-01-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: A MSI 2 162  (IF BCRC OR WASTE CHUTE CONTAINER INSTALLED, AS FAR SSI N AS VISIBLE)  R ZL-161-02-1 161AC 161BC 161CW 161 BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI N 161EC 162LW 162RW 162  162SW 162TW 162WW SSI N 822  R ZL-161-02-2 161FQ 161MY 161NQ 161 BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI N 161NY 161QY 161SY 162  162FY 162HY 162JY SSI N 162KY 162LY 833  843  R ZL-161-03-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 NOTE 1 162  SIDEWALL AND CEILING SSI N PANELS FROM FR 65 TO  FR 73  R ZL-161-03-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 BCRC FURNISHINGS OR 162  WASTE CHUTE (IF SSI N INSTALLED)  NOTE 1  SIDEWALL AND CEILING  PANELS FROM FR 65 TO  FR 73  R ZL-163-01-1 164AR 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-163-01-1 * * * * * C O N T I N U E * * * * *  FLOOR PANELS FROM FR 164 SSI N 65 TO FR 73  NOTE 1  R ZL-163-01-2 164AR 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 BCRC FURNISHINGS OR 164  WASTE CHUTE (IF SSI N INSTALLED)  FLOOR PANELS FROM FR  65 TO FR 73  NOTE 1  R ZL-171-01-1 162ZW 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI N 172  SSI N R ZL-171-01-2 161AZ 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI N 172  SSI N R ZL-171-01-3 161AZ 161MQ 171AL 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI N 833 843 172  SSI N R ZL-171-02-1 162ZW 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 3 FLOOR PANELS FROM FR 172 MSI 3 73 TO FR 80  NOTE 1 SSI 5 ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-171-02-2 161AZ 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 3 FLOOR PANELS FROM FR 172 MSI 3 73 TO FR 80  NOTE 1 SSI 5 R ZL-171-02-3 161AZ 161MQ 171AL 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 3 833 843 172 MSI 3 FLOOR PANELS FROM FR  73 TO FR 80 SSI 5 NOTE 1  R ZL-191-01-1 191FB 191KB 192JB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI N 192PB 192  SSI N R ZL-191-01-2 191BB 191DB 192BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI N 192DB 192JB 192PB 192  SSI N R ZL-191-02-1 191AB 191AT 191BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 2 191BT 191CB 191CT 192  191DB 191EB 191FB SSI N 191HB 191KB 191QB  192AT 192BB 192BT  192CB 192CT 192GB  192HB 192JB 192MB  192NB 192PB 192QB  R ZL-191-02-2 191AB 191AT 191BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 2 191BT 191CB 191CT  191DB 191FB 192AT SSI N 192BB 192BT 192CB  192CT 192DB 192FB  192GB 192HB 192JB  192MB 192NB 192PB  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-191-02-2 * * * * * C O N T I N U E * * * * *  192QB  R ZL-193-01-1 193BB 193DB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 2 SSI N R ZL-193-01-2 193BB 193DB 193HB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 2 SSI N R ZL-193-02-1 193AB 193BB 193CB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 2 193DB  SSI N R ZL-193-02-2 193AB 193BB 193CB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 2 193DB 193FB 193HB  SSI N R ZL-195-01-1 734 744 195 HYDRAULIC COMPARTMENT AND FAIRINGS (AS FAR AS I: A MSI 2 196 VISIBLE) (EWIS)  SSI N R ZL-195-02-1 195AB 195BB 196AB 195 HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) I: 2 C MSI 2 196BB 196 MSI 2 SSI N R ZL-195-02-2 195CT 195GB 195JB 195 HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) I: 2 C MSI 2 195NB 195PB 195QB 196 MSI 2 734 744  SSI N R ZL-197-01-1 734 744 197 REAR FAIRINGS (EWIS) I: A MSI N 198  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-197-01-1 * * * * * C O N T I N U E * * * * *  SSI N R ZL-197-02-1 197EB 198EB 197 REAR FAIRINGS (EWIS) I: 4 C MSI N 198  SSI N R ZL-197-02-2 197AB 197AT 197FB 197 REAR FAIRINGS (EWIS) I: 4 C MSI N 197GB 197HB 198AB 198  198AT 198FB 198GB SSI N 198HB  * * * * * E N D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-200-01-1 N/A 200 UPPER HALF OF FUSELAGE I: 2 C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-200-01-2 N/A 200 UPPER HALF OF FUSELAGE I: 2 C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-211-01-1 211JW 211KW 212JW 211 COCKPIT (EWIS) I: 2 C MSI N 212KW 831 841 212  SSI N R ZL-211-02-1 211AC 211AW 211BC 211 COCKPIT (EWIS) I: 8 C MSI N 211BW 211CC 211CW 212  211DC 211DW 211EC SSI 5 211EW 211FC 211FW SSI 5 211GC 211GW 211HC  211HW 211JC 211JW  211KC 211KW 211LC  211LW 211MC 211MW  211PW 212BC 212CC  212CW 212DC 212DW  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-211-02-1 * * * * * C O N T I N U E * * * * *  212EW 212FC 212FW  212GC 212GW 212HC  212HW 212JC 212JW  212KW 212LW 212MW  212NC 212NW 212QW  831 841  FLOOR PANELS FROM FR  1 TO FR 11  NOTE 1  R ZL-211-02-2 211AC 211AW 211BC 211 COCKPIT (EWIS) I: 8 C MSI N 211BW 211CC 211CW 212  211DC 211DW 211EC SSI 5 211EW 211FC 211FW SSI 5 211GC 211GW 211HC  211HW 211JC 211JW  211KC 211KW 211LC  211LW 211MC 211MW  211PW 212BC 212CC  212CW 212DC 212DW  212EW 212FC 212FW  212GC 212GW 212HC  212HW 212JC 212JW  212KW 212LW 212MW  212NC 212NW 212QW  831 841  FLOOR PANELS FROM FR  1 TO FR 11  NOTE 1  R ZL-221-02-1 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 2 DOOR FRAME LININGS 222  FCRC (IF INSTALLED) SSI 5 FLOOR PANELS FROM FR  11 TO FR 17  GALLEYS AND TOILETS  NOTE 1  SEATS AND  FURNISHINGS  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-221-02-2 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 2 DOOR FRAME LININGS 222  FCRC (IF INSTALLED) SSI 5 FLOOR PANELS FROM FR  11 TO FR 17  GALLEYS AND TOILETS  NOTE 1  SEATS AND  FURNISHINGS  R ZL-223-01-1 221AZ 221BZ 222AZ 223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N 222BZ 831 841 224  CEILING PANELS FROM SSI 5 FR 11 TO FR 17  FCRC  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  R ZL-223-01-2 221AZ 221BZ 222AZ 223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 2 222BZ 831 841 224  CEILING PANELS SSI 5 FCRC  GALLEYS AND TOILETS  FROM FR 11 TO FR 17  (IF INSTALLED)  NOTE 1  ZL-231-01-1 N/A TASK DELETED MSI N SSI N R ZL-231-02-1 831 841 231 FWD CABIN (EWIS) I: 8 C MSI N GALLEYS AND TOILETS 232  (IF INSTALLED) SSI 5 NOTE 1 SSI 5 SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 17 TO  FR 31  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-231-02-2 831 841 231 FWD CABIN (EWIS) I: 8 C MSI N GALLEYS AND TOILETS 232  (IF INSTALLED) SSI 5 NOTE 1 SSI 5 SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 17 TO  FR 37.7  R ZL-233-01-1 831 841 233 FWD CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 234  GALLEYS AND TOILETS SSI 5 (IF INSTALLED)  NOTE 1  OVERHEAD STOWAGE  BINS FROM FR 17 TO  FR 31  R ZL-233-01-2 831 841 233 FWD CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 234  GALLEYS AND TOILETS SSI 5 (IF INSTALLED)  NOTE 1  OVERHEAD STOWAGE  BINS FROM FR 17 TO  FR 37.7  ZL-241-01-1 N/A TASK DELETED MSI N SSI N R ZL-241-02-1 832 842 241 MID CABIN UTILITY AREA (EWIS) I: 8 C MSI N DOOR FRAME LININGS 242  FLOOR PANELS FROM FR SSI 5 31 TO FR 36 SSI 5 GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  SEATS AND  FURNISHINGS  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-241-02-2 832 842 241 MID CABIN UTILITY AREA (EWIS) I: 8 C MSI N DOOR FRAME LININGS 242  FLOOR PANELS FROM FR SSI 5 37.7 TO FR 37.11 SSI 5 GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  SEATS AND  FURNISHINGS  R ZL-243-01-1 832 842 243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS FROM 244  FR 31 TO FR 36 SSI 5 GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  R ZL-243-01-2 832 842 243 MID CABIN UTILITY AREA OVERHEAD COMPARTMEN (EWIS) I: 8 C MSI N CEILING PANELS FROM 244  FR 37.7 TO FR 37.11 SSI 5 GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  ZL-251-01-1 N/A TASK DELETED MSI N SSI N R ZL-251-02-1 832 842 251 MID CABIN (EWIS) I: 8 C MSI 2 NOTE 1 252  SEATS, FURNISHINGS SSI 5 GALLEYS, TOILETS AND  STAIRHOUSE (IF  INSTALLED)  SIDEWALL AND FLOOR  PANELS FROM FR 36 TO  FR 53.5  R ZL-251-02-2 832 842 251 MID CABIN (EWIS) I: 8 C MSI 2 252  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-251-02-2 * * * * * C O N T I N U E * * * * *  GALLEYS, TOILETS AND SSI 5 STAIRHOUSE (IF SSI 5 INSTALLED)  NOTE 1  SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 37.11  TO FR 53.4  R ZL-251-02-3 832 842 251 MID CABIN (EWIS) I: 8 C MSI 2 GALLEYS, TOILETS AND 252  STAIRHOUSE (IF SSI 5 INSTALLED) SSI 5 NOTE 1 SSI 5 SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 37.11  TO FR 56.1  R ZL-253-01-1 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 2 CEILING PANELS 254  OVERHEAD STOWAGE SSI 5 BINS FROM FR 36 TO  FR 53.5  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  R ZL-253-01-2 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 254  OVERHEAD STOWAGE SSI 5 BINS  GALLEYS AND TOILETS  FROM FR 37.11 TO FR  53.4 (IF INSTALLED)  NOTE 1  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-253-01-3 832 842 253 MID CABIN OVERHEAD COMPARTMEN (EWIS) I: 8 C MSI N CEILING PANELS 254  OVERHEAD STOWAGE SSI 5 BINS FROM FR 37.11  TO FR 56.1  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  ZL-261-01-1 N/A TASK DELETED MSI N SSI N R ZL-261-02-1 834 844 261 AFT CABIN (EWIS) I: 8 C MSI N DOOR FRAME LININGS 262  GALLEYS AND TOILETS SSI 5 (IF INSTALLED) SSI 5 NOTE 1  SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 53.5  TO FR 72  R ZL-261-02-2 834 844 261 AFT CABIN (EWIS) I: 8 C MSI N DOOR FRAME LININGS 262  GALLEYS AND TOILETS SSI 5 (IF INSTALLED) SSI 5 NOTE 1 SSI 5 SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 53.4  TO FR 72  R ZL-261-02-3 834 844 261 AFT CABIN (EWIS) I: 8 C MSI N DOOR FRAME LININGS 262  GALLEYS AND TOILETS SSI 5 (IF INSTALLED) SSI 5 NOTE 1  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-261-02-3 * * * * * C O N T I N U E * * * * *  SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 56.1  TO FR 72  R ZL-263-01-1 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 264  OVERHEAD STOWAGE SSI 5 BINS  GALLEYS AND TOILETS  FROM FR 53.5 TO FR  72 (IF INSTALLED)  NOTE 1  R ZL-263-01-2 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 264  OVERHEAD STOWAGE SSI 5 BINS  GALLEYS AND TOILETS  FROM FR 53.4 TO FR  72 (IF INSTALLED)  NOTE 1  R ZL-263-01-3 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 264  OVERHEAD STOWAGE SSI 5 BINS FROM FR 56.1 TO  FR 72  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  ZL-271-01-1 N/A TASK DELETED MSI N SSI N R ZL-271-02-1 833 843 271 AFT CABIN UTILITY AREA (EWIS) I: 8 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-271-02-1 * * * * * C O N T I N U E * * * * *  DOOR FRAME LININGS 272 SSI 5 FLOOR PANELS FROM FR SSI 5 72 TO FR 80 SSI 5 GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  SEATS AND  FURNISHINGS  R ZL-271-02-2 833 843 271 AFT CABIN UTILITY AREA (EWIS) I: 8 C MSI N DOOR FRAME LININGS 272  FLOOR PANELS FROM FR SSI 5 72 TO FR 80 SSI 5 GALLEYS AND TOILETS SSI 5 (IF INSTALLED) SSI 5 NOTE 1 SSI 5 SEATS AND  FURNISHINGS  SIDEWALL LINING  R ZL-273-01-1 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N 272AZ 272BZ 272CZ 274  833 843 SSI 5 CEILING PANELS FROM SSI 5 FR 72 TO FR 80  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  R ZL-273-01-2 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N 272AZ 272BZ 272CZ 274  833 843 SSI 5 CEILING PANELS FROM  FR 72 TO FR 80  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  R ZL-273-01-3 271AZ 271BZ 271CZ 272 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-273-01-3 * * * * * C O N T I N U E * * * * *  272AZ 272BZ 272CZ 274 SSI 5 833 843  CEILING PANELS FROM  FR 72 TO FR 80  GALLEYS AND TOILETS  (IF INSTALLED)  NOTE 1  * * * * * E N D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-300-01-1 N/A 300 STABILIZERS AND FUSELAGE REAR SECTION I: 2 C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-300-01-2 N/A 300 STABILIZERS AND FUSELAGE REAR SECTION I: 2 C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-311-01-1 312AR 313AL 311 REAR FUSELAGE SECTION (EWIS) I: C MSI 2 312 MSI 4 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-311-01-2 312AR 313BL 311 REAR FUSELAGE SECTION (EWIS) I: C MSI 4 TRANSFER PUMP 312 MSI 4 COVER/SEALING CASE  SSI 5 SSI 5 SSI 5 R ZL-313-01-1 313AL 313 TAIL CONE APU AIR INTAKE AREA (EWIS) I: C MSI 2 314 MSI 4 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-313-01-1 * * * * * C O N T I N U E * * * * *  SSI N R ZL-313-01-2 313BL 313 TAIL CONE APU AIR INTAKE AREA (EWIS) I: C MSI 4 314  SSI N R ZL-315-01-1 315AL 316AR 315 TAIL CONE APU AND ACCESSORY COMPARTMENT (EWIS) I: C MSI 4 316 MSI 4 MSI 4 SSI N R ZL-317-01-1 317AL 317 TAIL CONE APU EXHAUST AREA (EWIS) I: C MSI 4 SSI N R ZL-317-01-2 317BL 317 TAIL CONE APU EXHAUST AREA (EWIS) I: C MSI 4 SSI N ZL-319-01-1 N/A TASK DELETED MSI N SSI N R ZL-319-02-1 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL) (EWIS) I: 8 C MSI N 319AR 319BL 319BR  319CR SSI 5 DISCONNECT SCAVENGE  WATER SYSTEM PIPE  R ZL-319-02-2 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL) (EWIS) I: 8 C MSI N 319AR 319BL 319DR  319ER SSI N ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-319-02-3 311CZ 311DZ 312AR 319 HORIZONTAL STABILIZER SPAR BOX INSIDE FUSELAGE I: 8 C MSI N 312CZ 312DZ 313BL (INTERNAL) (EWIS)  SSI 5 R ZL-321-01-1 321AL 321 DORSAL FIN (EWIS) I: 8 C MSI N SSI N R ZL-322-01-1 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI N SSI 5 R ZL-322-01-2 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI N 322EL  SSI 5 R ZL-323-01-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 4 C MSI N SSI 5 R ZL-323-01-2 311AZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 4 C MSI N SSI 5 R ZL-323-02-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI N 322AL 322BL 322CL  323AL 323BL 325AL INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 5 325BL 325CL 325DL FITTINGS  325EL 325FL 325GL  325HL 325JL 325KL  PEELABLE HOLE COVERS  R ZL-323-02-2 311AZ 312AR 322AL 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI N 322BL 322CL 322EL  323DL 323EL 325LL INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 5 325NL 325SL 325TL FITTINGS  325UL 325VL  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-323-02-2 * * * * * C O N T I N U E * * * * *  PEELABLE HOLE COVERS  R ZL-324-01-1 324AT 324BT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI N SSI 5 R ZL-324-01-2 324CT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI N SSI 5 SSI 5 R ZL-325-01-1 325DL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI N SSI N R ZL-325-01-2 325NL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI N SSI N R ZL-325-02-1 325AL 325BL 325CL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 325DL 325EL 325FL  325GL 325HL 325JL SSI 5 325KL  R ZL-325-02-2 325LL 325NL 325SL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 325TL 325UL 325VL  SSI 5 R ZL-326-01-1 326DL 326 RUDDER (EWIS) I: C MSI N (AREA OF BEARINGS 2, 3 AND 4) SSI N R ZL-326-01-2 325NL 326ML 326NL 326 RUDDER (EWIS) I: C MSI N 326PL  (AREA OF BEARINGS 2, 3, 4 AND 5) SSI N ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-326-02-1 326BL 326DL 326FL 326 RUDDER (EWIS) I: 4 C MSI N 326HL 326KL  (AREA OF BEARINGS 1 TO 7) SSI N R ZL-326-02-2 325BL 325FL 325HL 326 RUDDER (EWIS) I: 4 C MSI N 325KL 326DL  (AREA OF BEARINGS 1 TO 7) SSI N R ZL-326-03-1 325AL 325BL 325DL 326 RUDDER (EWIS) I: 8 C MSI N 325FL 325HL 325KL  326AL 326BL 326BR (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI N 326CL 326DL 326DR VISIBLE)  326EL 326FL 326FR  326GL 326HL 326HR  326JL 326KL 326KR  326LL  R ZL-326-03-2 325AL 325BL 325CL 326 RUDDER (EWIS) I: 8 C MSI N 325CR 325DL 325EL  325ER 325FL 325GL (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI N 325GR 325HL 325JL VISIBLE)  325JR 325KL 326AT  326DL 326DR  R ZL-326-03-3 324CT 325LL 325LR 326 RUDDER (EWIS) I: 8 C MSI N 325NL 325NR 325SL  325SR 325TL 325TR (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS FAR AS SSI N 325UL 325VL 325VR VISIBLE)  326AT 326ML 326NL  326PL 326RL 326SL  R ZL-326-04-1 325NL 325SL 325TL 326 RUDDER (EWIS) I: 4 C MSI N 325UL 325VL 326ML  326NL 326PL 326RL (IN AREA OF BEARINGS 1 TO 8) SSI N 326SL  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-331-01-1 331AT 331BT 331CT 331 HORIZONTAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI N 331DT 331ET 333AB 341  333AT 341AT 341BT SSI 5 341CT 341DT 341ET SSI 5 343AB 343AT  R ZL-331-01-2 331AT 331BT 331CT 331 HORIZONTAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI N 331DT 331ET 331FT 341  341AT 341BT 341CT SSI 5 341DT 341ET 341FT  R ZL-332-01-1 332AB 332AT 342AB 332 HORIZONTAL STABILIZER TIP (EWIS) I: 8 C MSI N 342AT 342  SSI 5 R ZL-332-01-2 332AB 332AT 342AB 332 HORIZONTAL STABILIZER TIP (EWIS) I: 8 C MSI N 342AT 342  SSI 5 R ZL-333-01-1 331AT 331BT 333AB 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI N 333AL 333AT 341AT 343  341BT 343AB 343AR (RIB 3 TO RIB 4). SSI N 343AT  R ZL-333-01-2 331ET 332AB 332AT 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI N 333EL 343  (RIB 13 TO END RIB LH). SSI 5 R ZL-333-02-1 331AT 331AZ 333BB 333 HORIZONTAL STABILIZER SPAR BOX FUEL TANK (EWIS) I: 8 C MSI N 333CB 333DB 333EB 343  333FB 333GB 333HB (FROM RIB 3 TO RIB 15LH/14RH). SSI 5 333JB 333KB 333LB  333MB 341AT 341AZ  343BB 343CB 343DB  343EB 343FB 343GB  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-333-02-1 * * * * * C O N T I N U E * * * * *  343HB 343JB 343KB  343LB  R ZL-333-02-2 331AT 331AZ 333BB 333 HORIZONTAL STABILIZER SPAR BOX FUEL TANK (EWIS) I: 8 C MSI N 333CB 333DB 333EB 343  333FB 333GB 333HB (FROM RIB 3 TO RIB 20 LH, RIB 17 RH). SSI 5 333JB 333KB 333LB  333MB 333NB 333PB  333QB 333SB 333TB  341AT 341AZ 343BB  343CB 343DB 343EB  343FB 343GB 343HB  343JB 343KB 343LB  343MB 343NB 343PB  R ZL-334-01-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: C MSI N 344AB 344BB 344CB 344  (FUSELAGE FAIRING TO RIB 10) SSI N R ZL-334-01-2 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: C MSI N 334CT 344AB 344BB 344  344CB 344CT (FROM FUSELAGE FAIRING TO RIB 10) SSI N R ZL-334-02-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 334DB 334EB 334FB 344  334GB 344AB 344BB (FUSELAGE FAIRING TO RIB 21) SSI 5 344CB 344DB 344EB  344FB 344GB  R ZL-334-02-2 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 334DB 334EB 334FB 344  344AB 344BB 344CB (FROM FUSELAGE FAIRING TO RIB 21) SSI 5 344DB 344EB 344FB  R ZL-335-01-1 334BB 334CB 334DB 335 ELEVATOR (EWIS) I: C MSI N 335BB 344BB 344CB 345  344DB 345BB (AREA BETWEEN RIBS 8 AND 9) SSI N ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-335-02-1 334AB 334BB 334CB 335 ELEVATOR (EWIS) I: 8 C MSI N 334DB 334EB 334FB 345  334GB 335AB 335BB (LEADING EDGE AS FAR AS VISIBLE) SSI N 335CB 335DB 335EB  335FB 344AB 344BB  344CB 344DB 344EB  344FB 344GB 345AB  345BB 345CB 345DB  345EB 345FB  R ZL-335-02-2 334AB 334BB 334CB 335 ELEVATOR (EWIS) I: 8 C MSI N 334DB 334EB 334FB 345  335AB 335BB 335CB (LEADING EDGE AS FAR AS VISIBLE) SSI 5 335DB 335EB 335FB  335GB 335HB 335JB  344AB 344BB 344CB  344DB 344EB 344FB  345AB 345BB 345CB  345DB 345EB 345FB  345GB 345HB 345JB  R ZL-335-03-1 334CB 335CB 335DB 335 ELEVATOR (EWIS) I: C MSI N 335EB 344CB 345CB 345  345DB 345EB (AREA BETWEEN RIB 9 AND 10) SSI N R ZL-337-01-1 331ET 331FT 332AB 337 HORIZONTAL STABILIZER SPAR BOX DRY BAY (EWIS) I: 8 C MSI N 332AT 334EB 334FB 347  334FT 341FT 342AB (FROM RIB 15LH/16RH TO RIB 21 LH/RH) SSI 5 342AT 344EB 344FB  344FT  PEELABLE HOLE COVERS  R ZL-337-01-2 332AB 332AT 334ET 337 HORIZONTAL STABILIZER SPAR BOX DRY BAY (EWIS) I: 8 C MSI N 334FB 342AB 342AT 347  344ET 344FB (FROM RIB 20 TO RIB 21 LH/RH). SSI 5 PEELABLE HOLE COVERS  R ZL-346-01-1 346AB 346 HORIZONTAL STABILIZER SPAR BOX VENT TANK (EWIS) I: 8 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-346-01-1 * * * * * C O N T I N U E * * * * *  (FROM RIB 14RH TO RIB 16RH) SSI 5 R ZL-346-01-2 346AB 346BB 346CB 346 HORIZONTAL STABILIZER SPAR BOX VENT TANK (EWIS) I: 8 C MSI N (FROM RIB 17 RH TO RIB 20 RH). SSI 5 * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-400-01-1 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI N SSI N ZL-400-01-2 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI 7 SSI N R ZL-411-01-1 411AR 421AR 431AR 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI 3 441AR 421  431 SSI N 441  R ZL-411-02-1 411AR 411AZ 411BZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI N 411CZ 411DZ 415AL 421  416AR 421AR 421AZ 431 SSI N 421BZ 421CZ 421DZ 441  425AL 426AR 431AR  431AZ 431BZ 431CZ  431DZ 435AL 436AR  441AR 441AZ 441BZ  441CZ 441DZ 445AL  446AR  ZL-411-04-1 N/A ENGINE AIR INTAKE AND INTAKE LIP MSI N TASK DELETED SSI N R ZL-411-04-2 411AL 411AR 411AZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI N 411BZ 415AL 416AR 421  421AL 421AR 421AZ 431 SSI N 421BZ 425AL 426AR 441  431AL 431AR 431AZ  431BZ 435AL 436AR  441AL 441AR 441AZ  441BZ 445AL 446AR  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-412-01-1 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 7 426AR 435AL 436AR 422 MSI 7 445AL 446AR 432 MSI 7 442  SSI N R ZL-412-04-1 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 7 426AR 435AL 436AR 422  445AL 446AR 432 SSI N 442  R ZL-413-01-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI N 418AR 425AL 426AR 423  427AL 428AR 435AL 433 SSI N 436AR 437AL 438AR 443  445AL 446AR 447AL  448AR  R ZL-413-04-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI 7 417FL 418AR 425AL 423  426AR 427AL 427FL 433 SSI N 428AR 435AL 436AR 443  437AL 437FL 438AR  445AL 446AR 447AL  447FL 448AR  R ZL-414-01-1 417AL 418AR 427AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI N 428AR 437AL 438AR 424  447AL 448AR 434 SSI N 444  R ZL-414-04-1 415AL 416AR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI N 417FL 418AR 425AL 424  426AR 427AL 427FL 434 SSI N 428AR 435AL 436AR 444  437AL 437FL 438AR  445AL 446AR 447AL  447FL 448AR  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-415-01-1 415AL 415BL 416AR 415 FAN COWL (EWIS) I: 2 C MSI N 416BR 416CR 425AL 416  425BL 426AR 426BR 425 SSI 7 426CR 435AL 435BL 426  436AR 436BR 436CR 435  445AL 445BL 446AR 436  446BR 446CR 445  446  R ZL-415-04-1 415AL 415CL 416AR 415 FAN COWL (EWIS) I: 2 C MSI N 416BR 416CR 425AL 416  425CL 426AR 426BR 425 SSI N 426CR 435AL 435CL 426  436AR 436BR 436CR 435  445AL 445CL 446AR 436  446BR 446CR 445  446  R ZL-417-01-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 7 417BL 417CL 417DL 418  417EL 418AR 418BR 427 SSI 7 418CR 418DR 418ER 428 SSI 7 425AL 426AR 427AL 437 SSI 7 427BL 427CL 427DL 438  427EL 428AR 428BR 447  428CR 428DR 428ER 448  437AL 437BL 437CL  437DL 437EL 438AR  438BR 438CR 438DR  438ER 445AL 446AR  447AL 447BL 447CL  447DL 447EL 448AR  448BR 448CR 448DR  448ER  THRUST REVERSER  DEPLOYED  R ZL-417-04-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 7 417BL 417CL 417DL 418 MSI 7 417EL 417FL 418AR 427 MSI 7 418BR 418CR 418DR 428 MSI 7 418ER 425AL 426AR 437  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-417-04-1 * * * * * C O N T I N U E * * * * *  427AL 427BL 427CL 438 SSI N 427DL 427EL 427FL 447  428AR 428BR 428CR 448  428DR 428ER 435AL  436AR 437AL 437BL  437CL 437DL 437EL  437FL 438AR 438BR  438CR 438DR 438ER  445AL 446AR 447AL  447BL 447CL 447DL  447EL 447FL 448AR  448BR 448CR 448DR  448ER  THRUST REVERSER  DEPLOYED  R ZL-419-01-1 415AL 416AR 417AL 419 EXHAUST PLUG (EWIS) I: 2 C MSI N 417FL 418AR 425AL 429  426AR 427AL 427FL 439 SSI N 428AR 435AL 436AR 449  437AL 437FL 438AR  445AL 446AR 447AL  447FL 448AR  R ZL-451-01-1 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI N 451CR 461BL 461BR 461  461CL 461CR 471BL 471 SSI N 471BR 471CL 471CR 481  481BL 481BR 481CL  481CR  R ZL-451-04-1 451AR 451BL 451BR 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI N 451CL 461AR 461BL 461  461BR 461CL 471AR 471 SSI N 471BL 471BR 471CL 481  481AR 481BL 481BR  481CL  R ZL-452-01-1 452AL 452AR 452AZ 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-452-01-1 * * * * * C O N T I N U E * * * * *  452BL 452BZ 452CL 462 SSI 5 452CZ 452DR 452EL 472 SSI 5 452FR 462AL 462AR 482 SSI 5 462BL 462CL 462CR SSI 5 462DL 462EL 462FR  462GR 462HL 472AL  472AR 472BL 472CL  472CR 472DL 472ER  472FL 472GL 472HR  482AL 482AR 482AZ  482BL 482BZ 482CR  482CZ 482DL 482ER  482FL  R ZL-452-01-2 452AL 452AR 452AZ 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI N 452BL 452BZ 452CL 462  452CZ 452DR 452FR 472 SSI 5 452GL 462AL 462AR 482 SSI 5 462BL 462CL 462CR SSI 5 462EL 462GL 462GR SSI 5 462HL 462HR 472AL  472AR 472BL 472CL  472CR 472DL 472GL  472HL 472HR 472JR  482AL 482AR 482AZ  482BL 482BZ 482CR  482CZ 482FL 482GL  482HR  ZL-452-01-3 N/A TASK DELETED MSI N SSI N R ZL-452-01-4 452DZ 452EZ 452FL 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI N 452HL 452JL 452JR 462  452KL 452KR 452MR 472 SSI 5 462AL 462AR 462BL 482 SSI 5 462CL 462CR 462DL SSI 5 462EL 462FR 462GR SSI 5 462HL 472AL 472AR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-452-01-4 * * * * * C O N T I N U E * * * * *  472BL 472CL 472CR  472DL 472ER 472FL  472GL 472HR 482DZ  482JL 482JR 482KL  482KR 482ML 482MR  482NL  R ZL-452-04-1 452AL 452AR 452BL 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI N 452BR 452CL 452CR 462  452DL 452DR 452EL 472 SSI 5 452ER 452FL 452FR 482 SSI 5 452GL 452GR 452HL  452JL 462AL 462AR  462BL 462BR 462CL  462CR 462DL 462DR  462EL 462ER 462FL  462FR 462GL 462GR  462HL 462JL 472AL  472AR 472BL 472BR  472CL 472CR 472DL  472DR 472EL 472ER  472FL 472FR 472GL  472GR 472HL 472JL  482AL 482AR 482BR  482CR 482DL 482DR  482EL 482ER 482FL  482FR 482GL 482GR  482HL 482JL  R ZL-453-01-1 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI N 453BR 453CL 453CR 463  463AL 463AR 463BL 473 SSI N 463BR 463CL 463CR 483  473AL 473AR 473BL  473BR 473CL 473CR  483AL 483AR 483BL  483BR 483CL 483CR  R ZL-453-04-1 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI N 453BR 453CL 453CR 463  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-453-04-1 * * * * * C O N T I N U E * * * * *  453DL 453DR 453EL 473 SSI N 453ER 463AL 463AR 483  463BL 463BR 463CL  463CR 463DL 463DR  473AL 473AR 473BL  473BR 473CL 473CR  473DL 473DR 483AL  483AR 483BL 483BR  483CL 483CR 483DL  483DR 483EL 483ER  R ZL-454-01-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI N 454BR 454EL 454ER 464  454FL 454GL 454JL 474 SSI N 454JR 454KL 464AL 484  464AR 464BL 464BR  464EL 464ER 464FL  464GL 464HL 474AL  474AR 474BL 474BR  474EL 474ER 474FL  474GL 474HL 484AL  484AR 484BL 484BR  484EL 484ER 484FL  484GL 484JL 484JR  484KL  R ZL-454-01-2 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI N 454BR 454EL 454ER 464  454FL 454GL 454JL 474 SSI N 454JR 454KL 464AL 484  464EL 464ER 464GL  464HL 464JL 464KL  464KR 464MR 474AL  474EL 474ER 474GL  474HL 474JL 474KL  474KR 474MR 484AL  484AR 484BL 484BR  484EL 484ER 484FL  484GL 484JL 484JR  484KL  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-454-01-3 454AL 454BL 454EL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI N 454ER 454JL 454JR 464  454KL 454KR 454MR 474 SSI N 454QL 454SL 464AL 484  464EL 464ER 464GL  464HL 464JL 464KL  464KR 464MR 474AL  474EL 474ER 474GL  474HL 474JL 474KL  474KR 474MR 484EL  484ER 484JL 484JR  484KL 484KR 484ML  484NL 484NR 484PL  484QL  R ZL-454-02-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI N 454BR 454CL 454DL 464  454EL 454ER 454FL 474 SSI 5 454FR 454GL 454GR 484 SSI 5 454HL 454JL 454JR SSI 5 454KL 464AL 464AR SSI 5 464BL 464BR 464CL SSI 5 464DL 464EL 464ER SSI 5 464FL 464FR 464GL SSI 5 464GR 464HL 474AL  474AR 474BL 474BR  474CL 474DL 474EL  474ER 474FL 474FR  474GL 474GR 474HL  484AL 484AR 484BL  484BR 484CL 484DL  484EL 484ER 484FL  484FR 484GL 484GR  484HL 484JL 484JR  484KL  R ZL-454-02-2 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI N 454BR 454CL 454DL 464  454EL 454ER 454FL 474 SSI 5 454FR 454GL 454GR 484 SSI 5 454HL 454JL 454JR SSI 5 454KL 464AL 464CL SSI 5 464DL 464EL 464ER SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-454-02-2 * * * * * C O N T I N U E * * * * *  464GL 464GR 464HL  464JL 464JR 464KL  464KR 464MR 474AL  474CL 474DL 474EL  474ER 474GL 474GR  474HL 474JL 474JR  474KL 474KR 474MR  484AL 484AR 484BL  484BR 484CL 484DL  484EL 484ER 484FL  484FR 484GL 484GR  484HL 484JL 484JR  484KL  R ZL-454-02-3 454AL 454BL 454CL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI N 454DL 454EL 454ER 464  454HL 454JL 454JR 474 SSI 5 454KL 454KR 454MR 484 SSI 5 454NR 454PR 454QL SSI 5 454SL 464AL 464CL SSI 5 464DL 464EL 464ER SSI 5 464GL 464GR 464HL  464JL 464JR 464KL  464KR 464MR 474AL  474CL 474DL 474EL  474ER 474GL 474GR  474HL 474JL 474JR  474KL 474KR 474MR  484CL 484DL 484EL  484ER 484HL 484JL  484JR 484KL 484KR  484ML 484NL 484NR  484PL 484PR 484QL  484QR  R ZL-454-03-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 2 C MSI N 454BR 464AL 464AR 464  464BL 464BR 464CL 474 SSI N 464FL 474AL 474AR 484  474BL 474BR 474CR  474ER 484AL 484AR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-454-03-1 * * * * * C O N T I N U E * * * * *  484BL 484BR  R ZL-454-04-1 454AL 454AR 454BL 454 LOWER AND REAR PYLON FAIRING (EWIS) I: 4 C MSI N 454BR 454CL 454CR 464  454DL 454DR 464AL 474 SSI 5 464AR 464BL 464BR 484 SSI 5 464CL 464CR 464DL  464EL 464FL 474AL  474AR 474BL 474BR  474CL 474CR 474DL  474DR 474ER 484AL  484AR 484BL 484BR  484CL 484CR 484DL  484DR  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-500-01-1 FLAPS EXTENDED 500 WING LOWER SURFACE (EWIS) I: C MSI N SLATS EXTENDED 600  (INCLUDING SLATS AND FLAPS, EXCLUDING AREA COVERED BY SSI 5 PLASTRON FAIRING) SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-500-01-1 * * * * * C O N T I N U E * * * * *  SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-500-01-2 FLAPS EXTENDED 500 WING LOWER SURFACE (EWIS) I: C MSI N SLATS EXTENDED 600  (INCLUDING SLATS AND FLAPS) SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-500-02-1 FLAPS EXTENDED 500 WING UPPER SURFACE (EWIS) I: 2 C MSI N SLATS EXTENDED 600  SPOILERS EXTENDED (INCLUDING SLATS, FLAPS AND SPOILERS) SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-500-02-2 FLAPS EXTENDED 500 WING UPPER SURFACE (EWIS) I: 2 C MSI N SLATS EXTENDED 600  SPOILERS EXTENDED (INCLUDING SLATS, FLAPS AND SPOILERS) SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-500-02-2 * * * * * C O N T I N U E * * * * *  SSI 5 SSI 5 SSI 5 SSI 5 R ZL-521-01-1 521AB 521BB 521CB 521 INBOARD FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI 3 521DB 521FB 521GB 621  521JB 621AB 621BB SSI 5 621CB 621DB 621FB SSI 5 621GB 621JB  SLATS EXTENDED  R ZL-521-01-2 521AB 521BB 521CB 521 INBOARD FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI 3 521DB 521EB 521FB 621  521GB 521HB 521JB SSI 5 621AB 621BB 621CB SSI 5 621DB 621EB 621FB  621GB 621HB 621JB  SLATS EXTENDED  R ZL-522-01-1 522AB 522AT 522BB 522 CENTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI N 522BT 522CB 522CT 622  522EB 522HB 522JB SSI 5 522LB 522NB 522QB  522RB 522TB 522UB  622AB 622AT 622BB  622BT 622CB 622CT  622EB 622HB 622JB  622LB 622NB 622QB  622RB 622TB 622UB  SLATS EXTENDED  R ZL-522-01-2 522AB 522AT 522BB 522 CENTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI N 522BT 522CB 522CT 622  522EB 522GB 522HB SSI 5 522KB 522MB 522PB  622AB 622AT 622BB  622BT 622CB 622CT  622EB 622GB 622HB  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-522-01-2 * * * * * C O N T I N U E * * * * *  622KB 622MB 622PB  SLATS EXTENDED  R ZL-523-01-1 523AB 523AT 523BB 523 OUTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI N 523BT 523CB 523CT 623  523EB 523GB 523JB SSI N 523LB 523NB 623AB  623AT 623BB 623BT  623CB 623CT 623EB  623GB 623JB 623LB  623NB  SLATS EXTENDED  R ZL-523-01-2 523AB 523AT 523BB 523 OUTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI N 523BT 523CB 523DB 623  523FB 523HB 523KB SSI N 523MB 523PB 523QB  623AB 623BB 623BT  623CB 623DB 623FB  623HB 623KB 623MB  623PB 623QB  SLATS EXTENDED  R ZL-531-01-1 531CB 532CB 533CB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 2 C MSI N 534CB 631CB 632CB 532  633CB 634CB 533 SSI N FLAPS EXTENDED 534  631  632  633  634  R ZL-531-01-2 531SB 532SB 533SB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 2 C MSI N 534SB 631SB 632SB 532  633SB 634SB 533 SSI N FLAPS EXTENDED 534  631  632  633  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-531-01-2 * * * * * C O N T I N U E * * * * *  634  R ZL-531-02-1 531AB 531CB 532AB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 4 C MSI 2 532CB 533AB 533CB 532  534AB 534CB 631AB 533 SSI 5 631CB 632AB 632CB 534 SSI 5 633AB 633CB 634AB 631 SSI 5 634CB 632 SSI 5 FLAPS EXTENDED 633 SSI 5 634 SSI 5 R ZL-531-02-2 531KB 531SB 532KB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 4 C MSI 2 532SB 533KB 533SB 532  534KB 534SB 631KB 533 SSI 5 631SB 632KB 632SB 534 SSI 5 633KB 633SB 634KB 631 SSI 5 634SB 632 SSI 5 FLAPS EXTENDED 633  634  R ZL-535-01-1 535AB 535BB 635AB 535 WING TIP (EWIS) I: 4 C MSI N 635BB 635  SSI N R ZL-535-01-2 535AB 535AT 535BB 535 WING TIP (EWIS) I: 4 C MSI N 535CZ 635AB 635AT 635  635BB 635CZ SSI N R ZL-541-01-1 541AB 541BB 541BZ 541 INNER FUEL TANK (EWIS) I: 4 C MSI N 541CB 541CZ 641AB 641 NOTE 3  641BB 641BZ 641CB (RIB 1 TO RIB 7) SSI 5 641CZ  R ZL-541-02-1 541AB 541AZ 541BB 541 INNER FUEL TANK (EWIS) I: 8 C MSI 2 541BZ 541CB 541CZ 641  541DB 541DZ 541EB (RIB 1 TO RIB 23) SSI 5 541EZ 541FB 541FZ SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-541-02-1 * * * * * C O N T I N U E * * * * *  541GB 541GZ 541HB SSI 5 541JB 541KB 541LB SSI 5 541MB 541NB 541PB SSI 5 541QB 541RB 541SB SSI 5 641AB 641AZ 641BB SSI 5 641BZ 641CB 641CZ SSI 5 641DB 641DZ 641EB SSI 5 641EZ 641FB 641FZ SSI 5 641GB 641GZ 641JB SSI 5 641KB 641LB 641MB SSI 5 641NB 641PB 641QB SSI 5 641RB 641SB 642HB SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-541-03-1 541AB 541AZ 541BB 541 INNER FUEL TANK NO 2/3 (EWIS) I: 8 C MSI N 541BZ 541CZ 641AB 641  641AZ 641BB 641BZ (RIB 1 TO RIB 6 REAR OF CENTER SPAR) SSI 5 641CZ (RIB 1 TO RIB 11 FORWARD OF CENTER SPAR) SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-542-01-1 542AB 542BB 542CB 542 OUTER FUEL TANK (EWIS) I: 8 C MSI 2 542DB 542EB 542FB 642  542GB 542HB 542JB (RIB 23 TO RIB 33) SSI 5 542KB 560DB 642AB SSI 5 642BB 642CB 642DB SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-542-01-1 * * * * * C O N T I N U E * * * * *  642EB 642FB 642GB SSI 5 642HB 642JB 642KB SSI 5 660DB SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-542-02-1 542AB 542AZ 542BB 542 INNER FUEL TANK 1/4 (EWIS) I: 4 C MSI N 542BZ 542CB 542CZ 642  542DB 542DZ 542EB (RIB 6-11 AFT OF CENTER SPAR TO RIB 23) SSI 5 542EZ 542FB 542FZ (RIB 11-23) SSI 5 542GB 542GZ 542HB SSI 5 542JB 542KB 542LB SSI 5 542MB 542NB 542PB SSI 5 542QB 542RB 542SB SSI 5 642AB 642AZ 642BB SSI 5 642BZ 642CB 642CZ SSI 5 642DB 642DZ 642EB SSI 5 642EZ 642FB 642FZ SSI 5 642GB 642GZ 642HB SSI 5 642JB 642KB 642LB SSI 5 642MB 642NB 642PB SSI 5 642QB 642RB 642SB SSI 5 SSI 5 SSI 5 R ZL-543-01-1 543AB 543BB 543CB 543 OUTER FUEL TANK (EWIS) I: 8 C MSI N 543DB 543EB 543FB 643  543GB 543HB 543JB (RIB 23 TO RIB 35) SSI 5 543KB 543LB 543MB SSI 5 543NB 543PB 543QB SSI 5 543RB 543SB 543TB SSI 5 543UB 543VB 643AB SSI 5 643BB 643CB 643DB SSI 5 643EB 643FB 643GB SSI 5 643HB 643JB 643KB SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-543-01-1 * * * * * C O N T I N U E * * * * *  643LB 643MB 643NB  643PB 643QB 643RB  643SB 643TB 643UB  643VB  R ZL-550-01-1 550AB 550BB 550CB 550 VENT SURGE TANK (EWIS) I: 8 C MSI N 550DB 550EB 550FB 650  650AB 650BB 650CB (RIB 33 TO RIB 39) SSI 5 650DB 650EB 650FB SSI 5 SSI 5 SSI 5 SSI 5 R ZL-550-02-1 550AB 550BB 550CB 550 VENT SURGE TANK RIB 35-41 (EWIS) I: 8 C MSI N 550DB 550EB 550FB 650  650AB 650BB 650CB GENERAL VISUAL INSPECTION OF SURGE TANK WING BOX SSI 5 650DB 650EB 650FB RIBS 35 TO 45. SSI 5 SSI 5 R ZL-571-01-1 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI N 671  SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-571-01-2 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI N 671  SSI N R ZL-572-01-1 572BB 572CB 572EB 572 SHROUD BOX (EWIS) I: 4 C MSI N 672BB 672CB 672EB 672  SSI N R ZL-572-01-2 572BB 572CB 572EB 572 SHROUD BOX (EWIS) I: 4 C MSI N 672BB 672CB 672EB 672  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-572-01-2 * * * * * C O N T I N U E * * * * *  SSI 5 SSI 5 SSI 5 R ZL-573-01-1 573CB 573DB 573GB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 673CB 673DB 673GB 673  FLAPS EXTENDED SSI 5 SSI 5 R ZL-573-01-2 573CB 573DB 573FB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 573GB 673CB 673DB 673  673FB 673GB SSI N FLAPS EXTENDED  R ZL-574-01-1 574AT 674AT 574 CENTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N FLAPS EXTENDED 674  (RIB 12 TO RIB 27) SSI N R ZL-574-01-2 574AT 574BT 674AT 574 CENTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 674BT 674  FLAPS EXTENDED SSI N R ZL-575-01-1 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 575BT 575CB 575DB 675  575EB 675AB 675AT (RIB 27 TO RIB 39) SSI N 675BB 675BT 675CB  675DB 675EB  R ZL-575-01-2 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 575BT 575CB 575DB 675  575EB 675AB 675AT SSI N 675BB 675BT 675CB  675DB  R ZL-591-01-1 575AB 575BB 591AB 591 INBOARD AILERON (EWIS) I: 2 C MSI N 591BB 591CB 591DB 691  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-591-01-1 * * * * * C O N T I N U E * * * * *  675AB 675BB 691AB SSI N 691BB 691CB 691DB  R ZL-592-01-1 575CB 575DB 592AB 592 OUTBOARD AILERON (EWIS) I: 2 C MSI N 592BB 592CB 592DB 692  675CB 675DB 692AB SSI N 692BB 692CB 692DB  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-633-01-1 N/A TASK DELETED MSI N SSI N ZL-633-02-1 N/A TASK DELETED MSI N SSI N ZL-633-03-1 N/A TASK DELETED MSI N SSI N * * * * * E N D * * * * *  ISSUE: JUL 01/10 RH WING SECTION: E-600 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-700-01-1 N/A TASK DELETED MSI N SSI N ZL-700-01-2 N/A TASK DELETED MSI N SSI N R ZL-711-01-1 713 714 711 NOSE LANDING GEAR (EWIS) I: A MSI 3 SSI N R ZL-713-01-1 713 714 713 NOSE LANDING GEAR MAIN DOORS (EWIS) I: A MSI N 714  SSI 5 SSI 5 R ZL-713-01-2 713 714 713 NOSE LANDING GEAR MAIN DOORS (EWIS) I: A MSI N 714  SSI 5 SSI 5 R ZL-715-01-1 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI N 716  SSI 5 R ZL-715-01-2 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI N 716  SSI 5 R ZL-731-01-1 731 741 734 LH AND RH MAIN LANDING GEAR (EWIS) I: A MSI 3 744 MSI 3 SSI 5 R ZL-732-01-1 734 744 732 MAIN LANDING GEAR- LEG DOORS (EWIS) I: A MSI N 742  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-732-01-1 * * * * * C O N T I N U E * * * * *  SSI 5 R ZL-732-01-2 734 744 732 MAIN LANDING GEAR- LEG DOORS (EWIS) I: A MSI N 742  SSI 5 R ZL-733-01-1 N/A 733 MAIN LANDING GEAR- HINGE DOOR (EWIS) I: A MSI N 743  SSI 5 R ZL-733-01-2 N/A 733 MAIN LANDING GEAR- HINGE DOOR (EWIS) I: A MSI N 743  SSI 5 R ZL-734-01-1 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI N 744  SSI 5 SSI 5 R ZL-734-01-2 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI N 744  SSI 5 SSI 5 R ZL-751-01-1 753 754 751 CENTER LINE LANDING GEAR (EWIS) I: A MSI 3 SSI N R ZL-751-01-2 753 754 755 751 CENTER LINE LANDING GEAR (EWIS) I: A MSI 3 756  SSI N R ZL-753-01-1 753 754 753 CENTER LINE GEAR MAIN AND LEG DOORS (EWIS) I: A MSI N 754  SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-753-01-1 * * * * * C O N T I N U E * * * * *  SSI 5 R ZL-753-01-2 753 754 755 752 CENTER LINE GEAR MAIN, LEG DOORS AND MAINTENANCE DOOR I: A MSI N 756 753 (EWIS)  754 SSI 5 755 SSI 5 756 SSI 5 R ZL-755-01-1 755 756 755 CENTER LINE GEAR AFT DOORS (EWIS) I: A MSI N 756  SSI 5 R ZL-755-02-1 755 756 755 CENTER LINE GEAR AFT DOORS (EWIS) I: A MSI N 756  SSI 5 SSI 5 SSI 5 * * * * * E N D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-800-01-1 N/A 800 DOORS I: C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 ZL-800-01-2 N/A 800 DOORS I: C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 ZL-800-01-3 N/A 800 DOORS I: C MSI N SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 SSI 5 R ZL-811-01-1 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 5 SSI 5 R ZL-811-01-2 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 5 SSI N ISSUE: JUL 01/10 DOORS SECTION: E-800 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-821-01-1 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEAL; SSI 5 DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SSI 5 SILL)  R ZL-821-01-2 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 5 DOOR FRAMES AT FUSELAGE, DOOR SEALS AND VISIBLE PART  OF DOOR SILL)  R ZL-821-02-1 132AR 132BR 132CR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI N 132DR 132ER 132FR  132GR 132HR 132JR SSI N 132KR 132LR 821  821AR 821BR 821CR  821DR  R ZL-821-03-1 821 821AR 821BR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI N 821CR 821DR  INSULATION SSI N R ZL-822-01-1 822 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 5 DOOR FRAMES AT FUSELAGE, DOOR SEALS AND VISIBLE PART  OF DOOR SILL)  R ZL-822-01-2 822 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 5 DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR  SILL)  R ZL-822-02-1 152AR 152BR 152CR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI N 152DR 152ER 152FR  152GR 152HR 152JR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) SSI N 152KR 152LR 822  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-822-02-1 * * * * * C O N T I N U E * * * * *  822AR 822BR 822CR  822DR  R ZL-822-03-1 822 822AR 822BR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI N 822CR 822DR  INSULATION SSI N R ZL-823-01-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE SSI 5 FRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL)  R ZL-823-01-2 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE SSI 5 FRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL)  R ZL-823-02-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI N INSULATION  SSI N R ZL-823-02-2 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI N INSULATION  SSI N R ZL-831-01-1 831 841 831 FWD PASSENGER / CREW DOORS (EWIS) I: C MSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-831-01-1 * * * * * C O N T I N U E * * * * *  841 (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI N AND SCUFF PLATES)  R ZL-831-02-1 831 831AZ 831BZ 831 FWD PASSENGER / CREW DOOR (EWIS) I: 8 C MSI N 831CZ 831DZ 831EZ 841  831FZ 831GZ 831HZ SSI N 831JZ 841 841AZ  841BZ 841CZ 841DZ  841EZ 841FZ 841GZ  841HZ 841JZ  INSULATION  R ZL-832-01-1 832 842 832 MID PASSENGER / CREW DOORS (EWIS) I: C MSI 5 842  (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI N AND SCUFF PLATES)  ZL-832-01-2 N/A MID PASSENGER / CREW DOOR MSI N TASK DELETED SSI N R ZL-832-02-1 832 832AZ 832BZ 832 MID PASSENGER / CREW DOOR (EWIS) I: 8 C MSI N 832CZ 832DZ 832EZ 842  832FZ 832GZ 832HZ SSI N 832JZ 842 842AZ  842BZ 842CZ 842DZ  842EZ 842FZ 842GZ  842HZ 842JZ  INSULATION  R ZL-833-01-1 833 843 833 AFT PASSENGER / CREW DOORS (EWIS) I: C MSI 5 843  (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI N AND SCUFF PLATES)  ISSUE: JUL 01/10 DOORS SECTION: E-800 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 R ZL-833-02-1 833 833AZ 833BZ 833 AFT PASSENGER / CREW DOORS (EWIS) I: 8 C MSI N 833CZ 833DZ 833EZ 843  833FZ 833GZ 833HZ SSI N 833JZ 843 843AZ  843BZ 843CZ 843DZ  843EZ 843FZ 843GZ  843HZ 843JZ  INSULATION  R ZL-834-01-1 834 844 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: C MSI 5 844  (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS SSI N AND SCUFF PLATES)  ZL-834-01-2 N/A EMERGENCY EXIT MSI N TASK DELETED SSI N R ZL-834-02-1 834 834AZ 834BZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI N 834CZ 834DZ 834EZ 844  834FZ 834GZ 834HZ SSI N 834JZ 844 844AZ  844BZ 844CZ 844DZ  844EZ 844FZ 844GZ  844HZ 844JZ  INSULATION  R ZL-834-02-2 834 834KZ 834LZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI N 834MZ 834NZ 834PZ 844  834QZ 844 844KZ SSI N 844LZ 844MZ 844NZ  844PZ 844QZ  INSULATION  R ZL-834-02-3 834 834RZ 834SZ 834 EMERGENCY EXIT - DOORS 3 (EWIS) I: 8 C MSI N 834TZ 834UZ 834VZ 844  844 844RZ 844SZ SSI N 844TZ 844UZ 844VZ  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
A340 MRB REPORT – Zonal Section

TASK ZONE

REFERENCE

ACCESS DESCRIPTION INTERVAL M

REF

 ZL-834-02-3 * * * * * C O N T I N U E * * * * *  INSULATION  R ZL-836-01-1 836 846 836 OVERWING EXIT (EWIS) I: C MSI N 846  (INCLUDING DOOR STOPS ON FUSELAGE SIDE, DOOR SEALS) SSI N R ZL-836-02-1 836 836AZ 836BZ 836 OVERWING EXIT (EWIS) I: 8 C MSI N 836CZ 836DZ 836EZ 846  836FZ 846 846AZ SSI N 846BZ 846CZ 846DZ  846EZ 846FZ  INSULATION  * * * * * E N D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
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 REPORT 

Issue : July 2010 

200 

800 

(A340-600) 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR ZONES : A340 -200

100 LOWER HALF OF FUSELAGE 

(BELOW CABIN FLOOR) INCLUDING RADOME TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR0 - STA6382 

TO FR80/82 - STA56347 

200 UPPER HALF OF FUSELAGE 

(ABOVE CABIN FLOOR) TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR1 - STA7662 

TO FR80/82 - STA56347 

300 STABILIZER AND FUSELAGE REAR 

SECTION FROM REAR OF AFT PRESSURE BULKHEAD 

FR80/82 - STA56347 

TO FR106 - STA64998 

TOP OF RUDDER - STA65772 ELEVATOR - STA65803 

400 POWER PLANT NACELLES AND 

PYLONS 

500 LEFT WING 600 RIGHT WING 700 LANDING GEARS AND LANDING 

GEAR DOORS 

800 PASSENGER/CREW DOORS, 

CARGO COMPARTMENT DOORS AND EMERGENCY EXITS 

MAJOR ZONES : A340 -300

100 LOWER HALF OF FUSELAGE 

(BELOW CABIN FLOOR) INCLUDING RADOME TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR0 - STA6382 

TO FR80/82 - STA60614 

200 UPPER HALF OF FUSELAGE 

(ABOVE CABIN FLOOR) TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR1 - STA7662 

TO FR80/82 - STA60614 

300 STABILIZER AND FUSELAGE REAR 

SECTION FROM REAR OF AFT PRESSURE BULKHEAD 

FR80/82 - STA60614 

TO FR106 - STA69265 

TOP OF RUDDER - STA70040 ELEVATOR - STA70070 

400 POWER PLANT NACELLES AND 

PYLONS 

500 LEFT WING 600 RIGHT WING 700 LANDING GEARS AND LANDING 

GEAR DOORS 

800 PASSENGER/CREW DOORS, 

CARGO COMPARTMENT DOORS AND EMERGENCY EXITS 

MAJOR ZONES : A340 -500

100 LOWER HALF OF FUSELAGE 

(BELOW CABIN FLOOR) INCLUDING RADOME TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR0 - STA6382 

TO FR80/82 - STA64327 

200 UPPER HALF OF FUSELAGE 

(ABOVE CABIN FLOOR) TO FORWARD FACE OF AFT PRESSURE BULKHEAD 

FR1 - STA7662 

TO FR80/82 - STA64327 

300 STABILIZER AND FUSELAGE REAR 

SECTION FROM REAR OF AFT PRESSURE BULKHEAD 

FR80/82 - STA64327 

TO FR100 - STA71772 

TOP OF RUDDER - STA71772 ELEVATOR - STA71772 

400 POWER PLANT NACELLES AND 

PYLONS 

500 LEFT WING 600 RIGHT WING 700 LANDING GEARS AND LANDING 

GEAR DOORS 

800 PASSENGER/CREW DOORS, 

CARGO COMPARTMENT DOORS AND EMERGENCY EXITS 

MAJO

100 LOWER 

(BELOW INCLUDFORWAPRESS

FR

TO FR

200 UPPER 

(ABOVFORWAPRESS

FR

TO FR

300 STABIL

SECTIOPRESS

FR

TO FR

TOEL

400 POWE

PYLON

500 LEFT W600 RIGHT 700 LANDIN

GEAR 

800 PASSE

CARGO AND EM
A340 MRB REPORT 

Issue : July 2010 
A340 MRB REPORT 

Issue : July 2010 

A340-200/300
A340 MRB REPORT 

Issue : July 2010 
A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-300

110 RADOME (NOSE CONE TO FR 1) 

- STA6382,5 TO - STA7662,5 

120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

130 LOWER DECK FORWARD CARGO 

COMPARTMENT : AFT PARTITION OF AVIONICS COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX 

FR20 - STA14458,5 

TO FR40 - STA30372,1 

140 WING CENTER BOX, AIR COND, 

HYD COMPARTMENT : FORWARD PRESSURE BULKHEAD OF WING CENTER BOX TO FORWARD PRESSURE BULKHEAD OF AFT CARGO COMPARTMENT 

FR40 - STA30372,1 

TO FR53,2 - STA39930,9 

150 LOWER DECK AFT CARGO 

COMPARTMENT : FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AFT CARGO COMPARTMENT 

FR53,2 - STA39930,9 

TO BETWEEN FR65 - STA52134,5 AND FR66 - STA52664,5 

160 LOWER DECK BULK CARGO 

COMPARTMENT : AFT PARTITION, OF AFT CARGO COMPARTMENT TO AFT PARTITION OF BULK CARGO COMPARTMENT 

BETWEEN FR65 - STA52134,5 AND FR66 - STA52664,5 TO FR73 - STA53674,5 

170 AFT CABIN UNDERFLOOR 

COMPARTMENT : AFT PARTITION OF BULK CARGO COMPARTMENT TO AFT PRESSURE BULKHEAD 

FR73 - STA56374,4 

TO FR80/82 - STA60614,5 

190 BELLY FAIRING, AIR 

CONDITIONING COMPARTMENT, HYDRAULIC COMPARTMENT 

BETWEEN FR37,2 - STA26651,9 AND FR37,3 - STA27185,3 TO FR57,2 - STA46824,3 

210 COCKPIT FROM FORWARD 

PRESSURE BULKHEAD TO COCKPIT PARTITION 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

220 FORWARD CABIN UTILITY AREA 

AFT OF COCKPIT PARTITION TO FRONT OF FORWARD CABIN 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

MAJOR SUB ZONES A340-200

110 RADOME (NOSE CONE TO FR 1) 

- STA6382,5 TO - STA7662,5 

120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

130 LOWER DECK FORWARD CARGO 

COMPARTMENT : AFT PARTITION OF AVIONICS COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX 

FR20 - STA14458,5 

TO FR40 - STA28247,5 

140 WING CENTER BOX, AIR COND, 

HYD COMPARTMENT : FORWARD PRESSURE BULKHEAD OF WING CENTER BOX TO FORWARD PRESSURE BULKHEAD OF AFT CARGO COMPARTMENT 

FR40 - STA28247,5 

TO FR53,2 - STA37797,3 

150 LOWER DECK AFT CARGO 

COMPARTMENT : FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AFT CARGO COMPARTMENT 

FR53,2 - STA37797,3 

TO BETWEEN FR65 - STA47867,3 AND FR66 - STA48397,3 

160 LOWER 

COMPAOF AFT TO AFT CARGO 

BETWEAND FRTO FR

170 AFT CA

COMPAOF BULTO AFT 

FR

TO FR

190 BELLY 

CONDITHYDRA

BETWEAND FRTO FR

210 COCKP

PRESSCOCKP

FR

TO BETAND FR

220 FORWA

AFT OF FRONT 

BETWEAND FRTO FR
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-300

230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

240 MID CABIN UTILITY AREA AFT OF 

FORWARD CABIN TO FRONT OF MID CABIN 

FR31 - STA22408,5 

TO FR36 - STA25058,5 

250 MID CABIN AFT OF MID CABIN 

UTILITY AREA TO FRONT OF AFT CABIN 

FR36 - STA25058,5 

TO FR53,5 - STA39387,3 

260 AFT CABIN AFT OF MID CABIN TO 

FRONT OF AFT CABIN UTILITY AREA 

FR53,5 - STA39387,3 

TO FR72 - STA51577,3 

270 AFT CABIN UTILITY AREA AFT OF 

AFT CABIN TO FRONT OF AFT PRESSURE BULKHEAD 

FR72 - STA51577,3 

TO FR80/82 - STA56347,3 

310 FUSELAGE REAR SECTION AFT OF 

AFT PRESSURE BULKHEAD 

FR80/82 - STA56347,3 

TO FR106 - STA64998,3 

320 VERTICAL STABILIZER AND 

RUDDER 

330 TRIMMABLE HORIZONTAL 

STABILIZER, L SIDE AND L ELEVATOR 

340 TRIMMABLE HORIZONTAL 

STABILIZER, R SIDE AND R ELEVATOR 

710 NOSE GEAR AND DOORS 730 L MAIN LANDING GEAR AND 

DOORS 

740 R MAIN LANDING GEAR AND 

DOORS 

750 CENTERLINE GEAR AND DOORS 810 FORWARD AVIONICS 

COMPARTMENT DOOR 

820 CARGO COMPARTMENT DOORS 830 L PASSENGER/CREW DOORS AND 

EMERGENCY EXITS 

840 R PASSENGER/CREW DOORS AND 

EMERGENCY EXITS 

MAJOR SUB ZONES A340-200

230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

240 MID CABIN UTILITY AREA AFT OF 

FORWARD CABIN TO FRONT OF MID CABIN 

FR31 - STA22408,5 

TO FR36 - STA25058,5 

250 MID CABIN AFT OF MID CABIN 

UTILITY AREA TO FRONT OF AFT CABIN 

FR36 - STA25058,5 

TO FR53,5 - STA41520,9 

260 AFT CABIN AFT OF MID CABIN TO 

FRONT OF AFT CABIN UTILITY AREA 

FR53,5 - STA41520,9 

TO FR72 - STA55844,5 

270 AFT CABIN UTILITY AREA AFT OF 

AFT CABIN TO FRONT OF AFT PRESSURE BULKHEAD 

FR72 - STA55844,5 

TO FR80/82 - STA60614,5 

310 FUSELAGE REAR SECTION AFT OF 

AFT PRESSURE BULKHEAD 

FR80/82 - STA60614,5 

TO FR106 - STA69265,5 

320 VERTIC

RUDDE

330 TRIMMA

STABILELEVAT

340 TRIMMA

STABILELEVAT

710 NOSE G730 L MAIN 

DOORS 

740 R MAIN 

DOORS 

750 CENTE810 FORWA

COMPA

820 CARGO 830 L PASS

EMERG

840 R PASS

EMERG
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-500

110 RADOME (NOSE CONE TO FR 1) 

- STA6382,5 TO - STA7662,5 

120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

130 LOWER DECK FORWARD CARGO 

COMPARTMENT : AFT PARTITION OF AVIONICS COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX 

FR20 - STA14458,5 

TO FR40 - STA30372,1 

140 WING CENTER BOX, AIR COND, 

HYD COMPARTMENT : FORWARD PRESSURE BULKHEAD OF WING CENTER BOX TO FORWARD PRESSURE BULKHEAD OF AFT CARGO COMPARTMENT 

FR40 - STA30372,1 

TO FR53,2 - STA39930,9 

150 LOWER DECK AFT CARGO 

COMPARTMENT : FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AFT CARGO COMPARTMENT 

FR53,2 - STA39930,9 

TO BETWEEN FR65 - STA52134,5 AND FR66 - STA52664,5 

160 LOWER DECK BULK CARGO 

COMPARTMENT : AFT PARTITION, OF AFT CARGO COMPARTMENT TO AFT PARTITION OF BULK CARGO COMPARTMENT 

BETWEEN FR65 - STA52134,5 AND FR66 - STA52664,5 TO FR73 - STA53674,5 

170 AFT CABIN UNDERFLOOR 

COMPARTMENT : AFT PARTITION OF BULK CARGO COMPARTMENT TO AFT PRESSURE BULKHEAD 

FR73 - STA56374,4 

TO FR80/82 - STA60614,5 

190 BELLY FAIRING, AIR 

CONDITIONING COMPARTMENT, HYDRAULIC COMPARTMENT 

BETWEEN FR37,2 - STA26651,9 AND FR37,3 - STA27185,3 TO FR57,2 - STA46824,3 

210 COCKPIT FROM FORWARD 

PRESSURE BULKHEAD TO COCKPIT PARTITION 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

220 FORWARD CABIN UTILITY AREA 

AFT OF COCKPIT PARTITION TO FRONT OF FORWARD CABIN 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

MAJOR SUB ZONES A340-600

110 RADOME (NOSE CONE TO FR 1) 

- STA6382,5 TO - STA7662,5 

120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

130 LOWER DECK FORWARD CARGO 

COMPARTMENT : AFT PARTITION OF AVIONICS COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX 

FR20 - STA14458,5 

TO FR40 - STA28247,5 

140 WING CENTER BOX, AIR COND, 

HYD COMPARTMENT : FORWARD PRESSURE BULKHEAD OF WING CENTER BOX TO FORWARD PRESSURE BULKHEAD OF AFT CARGO COMPARTMENT 

FR40 - STA28247,5 

TO FR53,2 - STA37797,3 

150 LOWER DECK AFT CARGO 

COMPARTMENT : FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AFT CARGO COMPARTMENT 

FR53,2 - STA37797,3 

TO BETWEEN FR65 - STA47867,3 AND FR66 - STA48397,3 

160 LOWER 

COMPAOF AFT TO AFT CARGO 

BETWEAND FRTO FR

170 AFT CA

COMPAOF BULTO AFT 

FR

TO FR

190 BELLY 

CONDITHYDRA

BETWEAND FRTO FR

210 COCKP

PRESSCOCKP

FR

TO BETAND FR

220 FORWA

AFT OF FRONT 

BETWEAND FRTO FR
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-500

230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5 

TO FR37.7 - STA23998,5 

240 MID CABIN UTILITY AREA AFT OF 

FORWARD CABIN TO FRONT OF MID CABIN 

FR37.7 - STA23998,5 

TO FR37.11 - STA26118.5 

250 MID CABIN AFT OF MID CABIN 

UTILITY AREA TO FRONT OF AFT CABIN 

FR37.11 - STA23998,5 

TO FR53,4 - STA43110.9 

260 AFT CABIN AFT OF MID CABIN TO 

FRONT OF AFT CABIN UTILITY AREA 

FR53,4 - STA43110.9 

TO FR72 - STA59031.3 

270 AFT CABIN UTILITY AREA AFT OF 

AFT CABIN TO FRONT OF AFT PRESSURE BULKHEAD 

FR72 - STA59031,3 

TO FR80/82 - STA64327.3 

310 FUSELAGE REAR SECTION AFT OF 

AFT PRESSURE BULKHEAD 

FR80/82 - STA64327.3 

TO FR100 - STA717723 

320 VERTICAL STABILIZER AND 

RUDDER 

330 TRIMMABLE HORIZONTAL 

STABILIZER, L SIDE AND L ELEVATOR 

340 TRIMMABLE HORIZONTAL 

STABILIZER, R SIDE AND R ELEVATOR 

710 NOSE GEAR AND DOORS 730 L MAIN LANDING GEAR AND 

DOORS 

740 R MAIN LANDING GEAR AND 

DOORS 

750 CENTERLINE GEAR AND DOORS 810 FORWARD AVIONICS 

COMPARTMENT DOOR 

820 CARGO COMPARTMENT DOORS 830 L PASSENGER/CREW DOORS AND 

EMERGENCY EXITS 

840 R PASSENGER/CREW DOORS AND 

EMERGENCY EXITS 

MAJOR SUB ZONES A340-600

230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5 

TO FR37.7 - STA29298.5 

240 MID CABIN UTILITY AREA AFT OF 

FORWARD CABIN TO FRONT OF MID CABIN 

FR37.7 - STA29398,5 

TO FR37.11 - STA26118,5 

250 MID CABIN AFT OF MID CABIN 

UTILITY AREA TO FRONT OF AFT CABIN 

FR37.11 - STA226118,5 

TO FR56.1 - STA53187,1 

260 AFT CABIN AFT OF MID CABIN TO 

FRONT OF AFT CABIN UTILITY AREA 

FR56,1 - STA53187,1 

TO FR72 - STA66464,9 

270 AFT CABIN UTILITY AREA AFT OF 

AFT CABIN TO FRONT OF AFT PRESSURE BULKHEAD 

FR72 - STA66464,9 

TO FR80/82 - STA71760,9 

310 FUSELAGE REAR SECTION AFT OF 

AFT PRESSURE BULKHEAD 

FR80/82 - STA71760,9 

TO FR100 - STA79205,6 

320 VERTIC

RUDDE

330 TRIMMA

STABILELEVAT

340 TRIMMA

STABILELEVAT

710 NOSE G730 L MAIN 

DOORS 

740 R MAIN 

DOORS 

750 CENTE810 FORWA

COMPA

820 CARGO 830 L PASS

EMERG

840 R PASS

EMERG
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

A340-200/-300

A340-500-600
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-300

410 ENGINE 1 (LEFT OUTBOARD 

ENGINE), ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

420 ENGINE 2 (LEFT INBOARD ENGINE) 

ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

450 ENGINE 1 PYLON 460 ENGINE 2 PYLON 510 SLATS 520 FIXED LEADING EDGE 530 FLAP TRACK FAIRINGS AND WING 

TIP 

540 FUEL TANK 

RIB1 - STA0 

TO RIB33 - STA21905 

550 VENT SURGE TANK 

RIB33 - STA21905 

TO RIB39 - STA25566 

570 AFT SECTION OF WING AND 

TRAILING EDGE FIXED STRUCTURE 

580 FLAPS AND SPOILERS 590 AFT OUTBOARD SECTION OF 

WING TRAILING EDGE 

MAJOR SUB ZONES A340-200

430 ENGINE 3 (RIGHT INBOARD 

ENGINE), ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

440 ENGINE 4 (RIGHT OUTBOARD 

ENGINE) ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

470 ENGINE 3 PYLON 480 ENGINE 4 PYLON 610 SLATS 620 FIXED LEADING EDGE 630 FLAP TRACK FAIRINGS AND WING 

TIP 

640 FUEL TANK 

RIB1 - STA0 

TO RIB33 - STA21905 

650 VENT SURGE TANK 

RIB33 - STA21905 

TO RIB39 - STA25566 

670 AFT SECTION OF WING AND 

TRAILING EDGE FIXED STRUCTURE 

 680 FLAPS  690 AFT OU

WING T
MAJOR 

SUB 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

SUB 

ZONES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

SUB 

ZONES

DESCRIPTION/BOUNDARIES DE

A340 MRB REPORT 

Issue : July 2010 

MAJOR SUB ZONES A340-500/600

410 ENGINE 1 (LEFT OUTBOARD 

ENGINE), ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

420 ENGINE 2 (LEFT INBOARD ENGINE) 

ENGINE AIR INTAKE, FAN AND ACCESSORY GEAR BOX, THRUST REVERSER, EXHAUST NOZZLE AND COWLS 

450 ENGINE 1 PYLON 460 ENGINE 2 PYLON 510 SLATS 520 FIXED LEADING EDGE 530 FLAP TRACK FAIRINGS AND WING 

TIP 

540 FUEL TANK 

RIB1 - STA0 

TO RIB35 - STA27826 

550 VENT SURGE TANK 

RIB35 - STA27826 

TO RIB41 - STA32358 

570 AFT SECTION OF WING AND 

TRAILING EDGE FIXED STRUCTURE 

580 FLAPS AND SPOILERS 590 AFT OUTBOARD SECTION OF 

WING TRAILING EDGE 
A340 MRB REPORT 

Issue : July 2010 

A340-200/-300
A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-200

121/122 AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

 123 NOSE GEAR WELL 

FR11 - STA10127,5 

TO FR17 - STA13153,5 

131/132 LOWER DECK FORWARD CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA27178,5 AND FR39,2 - STA27708,5 

133/134 UNDERFLOOR COMPARTMENT OF 

LOWER DECK FORWARD CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO LOWER SIDE OF CARGO COMPARTMENT FLOOR (STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - STA14458,5 

TO FR39,1 - STA27178,5 AND FR39,1 - STA27708,5 

137/138 COMPARTMENT BETWEEN AFT 

PARTITION OF LOWER DECK FORWARD CARGO COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE (STR26 L/R) 

FR39,1 - STA27178,5 

AND FR39,2 - STA27708,5 

TO FR39 - STA26648,5 AND FR40 - STA28245,5 

141/142 WING CENTER BOX 

FR40 - STA28245,5 

AND FR47 - STA33538,5 

 143 AREA BETWEEN KEEL BEAMS 

UNDER WING CENTER BOX TO BOTTOM FUSELAGE BETWEEN FR44 AND FR45 

STA 32042,6 

TO FR49 STA 34603,2 

145/146 PRESSURIZED ZONE BETWEEN 

WING CENTER BOX, MAIN GEAR WELL AND CABIN FLOOR 

FR40 - STA28247,5 

TO FR53,2 - STA37797,3 

147/148 MAIN GEAR WELL AND 

HYDRAULIC COMPARTMENT 

FR47 - STA33538,5 

TO FR53,2 - STA37797,3 

 149 CENTERLINE GEAR WELL 

BETWEEN KEEL BEAMS UNDER ZONE 143 BETWEEN FR44 AND FR45 

STA 32042,6 

TO FR49 STA 34603,2 AND BETWEEN KEEL BEAMS 

FR49 STA 34603,2 

TO FR53,2 STA 37797,3 

 Sub zones A340- 300

121/122 AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

 123 NOSE GEAR WELL 

FR11 - STA10127,5 

TO FR17 - STA13153,5 

131/132 LOWER DECK FORWARD CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA29312,1 AND FR39,2 - STA28842,1 

133/134 UNDERFLOOR COMPARTMENT OF 

LOWER DECK FORWARD CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO LOWER SIDE OF CARGO COMPARTMENT FLOOR (STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - STA14458,5 

TO FR39,1 - STA29312,1 AND FR39,1 - STA29842,1 

137/138 COMPARTMENT BETWEEN AFT 

PARTITION OF LOWER DECK FORWARD CARGO COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE (STR26 L/R) 

FR39,1 - STA29312,1 

AND FR39,2 - STA29842,1 

TO FRAND FR

141/142 WING C

FR

AND FR

 143 AREA B

UNDER BOTTOBETWE

ST

TO FR

145/146 PRESS

WING CWELL A

FR

TO FR

147/148 MAIN G

HYDRA

FR

TO FR

 149 CENTE

BETWEZONE 1BETWE

ST

TO FRAND BE

FR

TO FR
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DE

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-200

151/152 LOWER DECK AFT CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 IN CYLINDRICAL SECTION) 

FR53,2 - STA37797,3 

TO FR65 - STA47867,3 AND FR66 - STA48397,3 

153/154 UNDERFLOOR COMPARTMENT OF 

LOWER DECK AFT CARGO COMPARTMENT : FROM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR53,2 - STA37797,3 

TO FR65 - STA47867,3 AND FR66 - STA48397,3 

161/162 LOWER DECK BULK CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR65 - STA47867,3 

AND FR66 - STA48397,3 TO FR73 - STA52107,3 

163/164 UNDERFLOOR COMPARTMENT OF 

LOWER DECK BULK CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR65 - STA47867,3 

AND FR66 - STA48397,3 TO FR73 - STA52107,3 

171/172 AFT CABIN UNDERFLOOR 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE (STR26 L/R) 

FR73 - STA52107,3 

TO FR80 - STA56347,3 

 191 DRY BAY AND FAIRINGS : 

BETWEEN FR31 AND FR37,1 STA23681,5 TO BETWEEN FR44 AND FR45 STA32042,6 

 192 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

BETWEEN FR37 AND FR37,1 STA23681,5 TO BETWEEN F44 AND FR45 STA32042,6 

 193 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

FR40 STA28247,51 

BETWEEN FR44 AND FR45 STA32042,6 

195/196 HYDRAULIC COMPARTMENT AND 

FAIRINGS : 

BETWEEN FR44 AND FR45 STA32042,6 TO FR47 STA33538,5 

197/198 REAR FAIRINGS : 

FR53,2 STA37797,3 

TO FR56 STA43097,3

Sub zones A340-300

151/152 LOWER DECK AFT CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 IN CYLINDRICAL SECTION) 

FR53,2 - STA39930,9 

TO FR65 - STA52134,5 AND FR66 - STA52664,5 

153/154 UNDERFLOOR COMPARTMENT OF 

LOWER DECK AFT CARGO COMPARTMENT : FROM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR53,2 - STA39930,9 

TO FR65 - STA52134,5 AND FR66 - STA52664,5 

161/162 LOWER DECK BULK CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR65 - STA52134,5 

AND FR66 - STA52664,5 TO FR73 - STA56374,5 

163/164 UNDERFLOOR COMPARTMENT OF 

LOWER DECK BULK CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR

AND FRTO FR

171/172 AFT CA

COMPASIDE OFLOOR (STR26 

FR

TO FR

 191 DRY BA

BETWESTA258AND FR

 192 AIR CO

COMPA

BETWESTA258FR45 S

 193 AIR CO

COMPA

FR

BETWESTA341

195/196 HYDRA

FAIRIN

BETWESTA341

197/198 REAR F

FR

TO FR
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DE

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-200

211/212 COCKPIT 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

221/222 FORWARD CABIN UTILITY AREA : 

FROM STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

223/224 FORWARD CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

231/232 FORWARD CABIN : FROM STR15 

L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

233/234 FORWARD CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

241/242 MID CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR31 - STA22408,5 

TO FR36 - STA25058,5 

243/244 MID CABIN UTILITY AREA : 

OVERHEAD COMPARTMENT FROM CROWN CENTER LINE TO STR15 L/R 

FR31 - STA22408,5 

TO FR36 - STA25058,5 

251/252 MID CABIN : FROM STR15 L/R TO 

PAX COMPARTMENT FLOOR UPPER SIDE (STR26 L/R IN CYLINDRICAL SECTION) 

FR39.6 - STA25056,5 

TO FR53,5 - STA39387,3 

253/254 MID CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR36 - STA25058,5 

TO FR53,5 - STA39387,3 

261/262 AFT CABIN : FROM STR15 L/R TO 

UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR53,5 - STA39387,3 

TO FR72 - STA51577,3 

Sub zones A340-300

211/212 COCKPIT 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

221/222 FORWARD CABIN UTILITY AREA : 

FROM STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

223/224 FORWARD CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

231/232 FORWARD CABIN : FROM STR15 

L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

233/234 FORWARD CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR17 - STA13153,5 

TO FR31 - STA22408,5 

241/242 MID CA

STR15 COMPAL/R IN C

FR

TO FR

243/244 MID CA

OVERHFROM STR15 

FR

TO FR

251/252 MID CA

PAX COUPPER CYLIND

Frr

TO FR

253/254 MID CA

COMPACENTE

FR

TO FR

261/262 AFT CA

UPPER COMPAL/R IN C

FR

TO FR
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DE

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-200

263/264 AFT CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR53,5 - STA39387,3 

TO FR72 - STA51577,3 

271/272 AFT CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION ) 

FR72 - STA51577,3 

TO FR80 - STA56347,3 

273/274 AFT CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR72 - STA51577,3 

TO FR80 - STA56347,3 

311/312 REAR FUSELAGE SECTION 

FR80/82 - STA56347,3 

TO BETWEEN FR91/92 STA60851,3 

313/314 TAIL CONE APU AIR INTAKE AREA 

BETWEEN FR91/92 - STA60851,3 TO FR95 - STA61779,3 

315/316 TAIL CONE APU AND ACCESSORY 

COMPT DELIMITED BY FIREWALLS 

FR95 - STA61779,3 

TO FR101 - STA63664,3 

 317 TAIL CONE APU EXHAUST AREA 

FR101 - STA63664,3 

TO FR106 - STA64998,3 

 321 DORSAL FIN  322 VERTICAL STABILIZER LEADING 

EDGE 

 323 VERTICAL STABILIZER SPAR BOX  324 VERTICAL STABILIZER TIP  325 VERTICAL STABILIZER TRAILING 

EDGE 

 326 RUDDER 

Sub zones A340-300

263/264 AFT CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR53,5 - STA41520,9 

TO FR72 - STA55844,5 

271/272 AFT CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION ) 

FR72 - STA55844,5 

TO FR80 - STA60614,5 

273/274 AFT CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR72 - STA55844,5 

TO FR80 - STA60614,5 

311/312 REAR F

FR

TO BET

313/314 TAIL CO

BETWETO FR

315/316 TAIL CO

COMPT 

FR

TO FR

 317 TAIL CO

FR

TO FR

 321 DORSA 322 VERTIC

EDGE 

 323 VERTIC 324 VERTIC 325 VERTIC

EDGE 

 326 RUDDE
A340 MRB REPORT 

Issue : July 2010 

A340-500

155 
A340 MRB REPORT 

Issue : July 2010 

A340-600

251 252

836 846
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DES

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-500

121/122 AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

 123 NOSE GEAR WELL 

FR11 - STA10127,5 

TO FR17 - STA13153,5 

131/132 LOWER DECK FORWARD CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA29301,9 AND FR39,2 - STA30361,9 

133/134 UNDERFLOOR COMPARTMENT OF 

LOWER DECK FORWARD CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO LOWER SIDE OF CARGO COMPARTMENT FLOOR (STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA29301,9 

 AND FR39,2 - STA30361,9 137/138 COMPARTMENT BETWEEN AFT 

PARTITION OF LOWER DECK FORWARD CARGO COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE 

 (STR26 L/R) 

 FR39,1 - STA29301,9 AND FR39,2 - STA30361,9 TO FR39 - STA29301,9 AND FR40 - STA36191,9 

141/142 WING CENTER BOX 

FR40 - STA30891,9 

AND FR47 - STA37796,1 

 143 AREA BETWEEN KEEL BEAMS 

UNDER WING CENTER BOX TO BOTTOM FUSELAGE BETWEEN FR44 AND FR45 

STA 36202,1 

TO FR49 STA 38856,2 

145/146 PRESSURIZED ZONE BETWEEN 

WING CENTER BOX, MAIN GEAR WELL AND CABIN FLOOR 

FR40 - STA30891,9 

TO FR53,2 - STA42050,9 

147/148 MAIN GEAR WELL AND 

HYDRAULIC COMPARTMENT 

FR47 - STA37796,1 

TO FR53,2 STA42050,9 

 149 CENTERLINE GEAR WELL 

BETWEEN KEEL BEAMS UNDER ZONE 143 BETWEEN FR44 AND FR45 

STA 36732,1 

TO FR49 STA 38856,8 AND BETWEEN KEEL BEAMS 

FR49 - STA 38856,8 

TO FR53,2 - STA 4250,9 

Sub zones A340- 600

121/122 AVIONICS COMPARTMENT 

FR1 - STA7662,5 

TO FR20 - STA14458,5 

 123 NOSE GEAR WELL 

FR11 - STA10127,5 

TO FR17 - STA13153,5 

131/132 LOWER DECK FORWARD CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA35131,9 AND FR39,2 - STA35661,9 

133/134 UNDERFLOOR COMPARTMENT OF 

LOWER DECK FORWARD CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO LOWER SIDE OF CARGO COMPARTMENT FLOOR (STR41 L/R IN CYLINDRICAL SECTION) 

FR20 - ST14448,5 

TO FR39,1 - STA35131,9 AND FR39,2 - STA35661,9 

137/138 COMPARTMENT BETWEEN AFT 

PARTITION OF LOWER DECK FORWARD CARGO COMPARTMENT TO FORWARD PRESSURE BULKHEAD OF WING CENTER BOX : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE 

 (STR26 

 FRAND FRTO FRAND FR

141/142 WING C

FR

AND FR

 143 AREA B

UNDER BOTTOBETWE

ST

TO FR

145/146 PRESS

WING CWELL A

FR

TO FR

147/148 MAIN G

HYDRA

FR

TO FR

 149 CENTE

BETWEZONE 1BETWE

ST

TO FRAND BE

FR

TO FR
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DES

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-500

151/152 LOWER DECK AFT CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 IN CYLINDRICAL SECTION) 

FR53,7 - STA44370,9 

TO FR65 - STA55321,3 AND FR66 - STA55851,3 

153/154 UNDERFLOOR COMPARTMENT OF 

LOWER DECK AFT CARGO COMPARTMENT : FROM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR53,7 - STA44370,9 

TO FR65 - STA55321,3 AND FR66 - STA55851,3 

 155 REAR CENTER TANK 

FR 53.2 -STA42050.9 FR 53.7 -STA44700.9 OR FR53.9 -STA45760.9 

161/162 LOWER DECK BULK CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

 FR65 - STA44370,9 AND FR66 - STA55851,3 TO FR73 - STA59561,3 

163/164 UNDERFLOOR COMPARTMENT OF 

LOWER DECK BULK CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

 FR65 - STA44370,9 AND FR66 - STA55851,3 TO FR73 - STA59561,3 

171/172 AFT CABIN UNDERFLOOR 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE (STR26 L/R) 

FR73 - STA59561,3 

TO FR80 - STA63197,3 

 191 DRY BAY AND FAIRINGS : 

BETWEEN FR37.11 AND FR40.1 STA26118.5 TO STA31421.3 

 192 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

BETWEEN FR37.11 TO F44 STA26118.5 TO STA 36202.5 

 193 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

FR37.13 TO FR44 STA27178.5 TO STA 36202,5 

195/196 HYDRAULIC COMPARTMENT AND 

FAIRINGS : 

BETWEEN FR40.1 AND FR47 TO STA31421.3 TO STA37796.1 

197/198 REAR FAIRINGS : 

FR44 STA36202.1 

TO FR47 STA37796.1
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DES

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-600

151/152 LOWER DECK AFT CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 IN CYLINDRICAL SECTION) 

FR53,2 - STA47350,9 

TO FR65 - STA62754,9 

 AND FR66 - STA63284,3 153/154 UNDERFLOOR COMPARTMENT OF 

LOWER DECK AFT CARGO COMPARTMENT : FROM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR53,2 - STA47350,9 

TO FR65 - STA62754,9 AND FR66 - STA63284,3 

161/162 LOWER DECK BULK CARGO 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO UPPER SIDE OF CARGO COMPARTMENT FLOOR (STR26 L/R TO STR41 L/R IN CYLINDRICAL SECTION) 

 FR65 - STA62754,9 AND FR66 - STA63284,9 TO FR73 - STA66994,9 

163/164 UNDERFLOOR COMPARTMENT OF 

LOWER DECK BULK CARGO COMPARTMENT : FROM BOTTOM CENTER LINE TO CARGO COMPARTMENT FLOOR LOWER SIDE (STR41 L/R IN CYLINDRICAL SECTION) 

FR65 - STA62754,9 AND FR66 - STA63284,9 TO FR73 - STA66994,9 

171/172 AFT CABIN UNDERFLOOR 

COMPARTMENT : FROM LOWER SIDE OF PAX COMPARTMENT FLOOR TO BOTTOM CENTER LINE (STR26 L/R) 

FR73 - STA66994,9 

 TO FR80 - STA71234,9  191 DRY BAY AND FAIRINGS : 

BETWEEN FR37.11 TO 40.1 STA31416.5 TO STA 36721.9 

 192 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

BETWEEN FR37 AND FR37,11 TO FR44 STA31416.1 TO STA 36721.9 

 193 AIR CONDITIONING 

COMPARTMENT AND FAIRINGS : 

 FR37.13 STA32476.5 TO FR44 

STA41502.1 

195/196 HYDRAULIC COMPARTMENT AND 

FAIRINGS : 

BETWEEN FR40.1 AND FR47 STA36721.1 TO FR4743624.1 

197/198 REAR FAIRINGS : 

FR53,2 STA47350.9 

 TO FR56.2 STA53717.1
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DES

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-500

211/212 COCKPIT 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

221/222 FORWARD CABIN UTILITY AREA : 

FROM STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

223/224 FORWARD CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

231/232 FORWARD CABIN : FROM STR15 

L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR17 - STA13153,5 

TO FR37.7 - STA23998,5 

233/234 FORWARD CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR17 - STA13153,5 

TO FR37.7 - STA23998,5 

241/242 MID CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR37.7 - STA23998,5 

TO FR37.11 - STA26118,5 

243/244 MID CABIN UTILITY AREA : 

OVERHEAD COMPARTMENT FROM CROWN CENTER LINE TO STR15 L/R 

FR37.7 - STA23998,5 

TO FR37.11 - STA26118,5 

251/252 MID CABIN : FROM STR15 L/R TO 

PAX COMPARTMENT FLOOR UPPER SIDE (STR26 L/R IN CYLINDRICAL SECTION) 

FR37.11 - STA26118,5 

TO FR53,4 - STA43110,9 

253/254 MID CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR37.11 - STA26118,5 

TO FR53,4 - STA43110,9 

261/262 AFT CABIN : FROM STR15 L/R TO 

UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

 FR53,4 - STA43110,9 TO FR72 - STA59031.3 

Sub zones A340-600

211/212 COCKPIT 

FR1 - STA7662,5 

TO BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 

221/222 FORWARD CABIN UTILITY AREA : 

FROM STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

223/224 FORWARD CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

BETWEEN FR11 - STA10187,5 AND FR11A - STA10427,5 TO FR17 - STA13153,5 

231/232 FORWARD CABIN : FROM STR15 

L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION) 

FR17 - STA13153,5 

TO FR37.7 - STA29298,5 

233/234 FORWARD CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR17 - STA13153,5 

TO FR37.7 - STA29298,5 

241/242 MID CA

STR15 COMPAL/R IN C

FR

TO FR

243/244 MID CA

OVERHFROM STR15 

FR

TO FR

251/252 MID CA

PAX COUPPER CYLIND

FR

TO FR

253/254 MID CA

COMPACENTE

FR

TO FR

261/262 AFT CA

UPPER COMPAL/R IN C

FR

TO FR
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DES

A340 MRB REPORT 

Issue : July 2010 

Sub zones A340-500

263/264 AFT CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

 FR53,4 - STA43110,9 TO FR72 - STA59031.3 

271/272 AFT CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION ) 

FR72 - STA59031.3 

TO FR80 - STA63801.3 

273/274 AFT CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR72 - STA59031.3 

TO FR80 - STA63801.3 

311/312 REAR FUSELAGE SECTION 

FR80/82 - STA63197,3 

TO BETWEEN FR91/92 STA68233.3 

313/314 TAIL CONE APU AIR INTAKE AREA 

BETWEEN FR91/92 - STA68233.3 TO FR94 - STA69223.3 

315/316 TAIL CONE APU AND ACCESSORY 

COMPT DELIMITED BY FIREWALLS 

FR94 - STA69223.3 

TO FR98 - STA71323,3 

 317 TAIL CONE APU EXHAUST AREA 

FR98 - STA71323,3 

TO FR100 - STA72220.7 

 321 DORSAL FIN  322 VERTICAL STABILIZER LEADING 

EDGE 

 323 VERTICAL STABILIZER SPAR BOX  324 VERTICAL STABILIZER TIP  325 VERTICAL STABILIZER TRAILING 

EDGE 

 326 RUDDER 

Sub zones A340-600

263/264 AFT CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR56,1 - STA53187,7 

 TO FR72 - STA66464,9 271/272 AFT CABIN UTILITY AREA : FROM 

STR15 L/R TO UPPER SIDE OF PAX COMPARTMENT FLOOR (STR26 L/R IN CYLINDRICAL SECTION ) 

FR72 - STA66464.9 

TO FR80 - STA71234.3 

273/274 AFT CABIN UTILITY AREA 

OVERHEAD COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

FR72 - STA66464.9 

TO FR80 - STA71234.3 

311/312 REAR F

FR

TO BET

313/314 TAIL CO

BETWETO FR

315/316 TAIL CO

COMPT 

FR

TO FR

 317 TAIL CO

FR

TO FR

 321 DORSA 322 VERTIC

EDGE 

 323 VERTIC 324 VERTIC 325 VERTIC

EDGE 

 326 RUDDE
A340 MRB REPORT 

Issue : July 2010 

A340-200/-300
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DE

A340 MRB REPORT 

Issue : July 2010 

CFM ENGINE 1 (L OUTBOARD)

411 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

412 FAN AND ACCESSORY GEAR BOX 415 L FAN COWL 416 R FAN COWL 417 L THRUST REVERSER 418 R THRUST REVERSER 413 HOT SECTION 414 EXHAUST NOZZLE 451 PYLON LEADING EDGE 452 UPPER FWD PYLON 453 LOWER PYLON 454 LOWER AND REAR PYLON 

FAIRINGS 

CFM ENGINE 2 (L INBOARD)

421 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

422 FAN AND ACCESSORY GEAR BOX 425 L FAN COWL 426 R FAN COWL 427 L THRUST REVERSER 428 R THRUST REVERSER 423 HOT SECTION 424 EXHAUST NOZZLE 461 PYLON LEADING EDGE 462 UPPER FWD PYLON 463 LOWER PYLON 464 LOWER AND REAR PYLON  FAIRINGS 

CFM ENGINE 3 (R INBOARD)

431 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

432 FAN AND ACCESSORY GEAR BOX 435 L FAN COWL 436 R FAN COWL 437 L THRUST REVERSER 438 R THRUST REVERSER 433 HOT SECTION 434 EXHAUST NOZZLE 471 PYLON LEADING EDGE 472 UPPER FWD PYLON 473 LOWER PYLON 474 LOWER AND REAR PYLON  FAIRINGS 

CFM EN

441 ENGINE 

INTAKE 

442 FAN AN445 L FAN C446 R FAN C447 L THRU448 R THRU443 HOT SE444 EXHAU481 PYLON 482 UPPER 483 LOWER 484 LOWER 

FAIRING
A340 MRB REPORT

Issue : July 2010 

431 441

432 442

435/436 445/446

433 433

437/438 447/448

434 444

439 449

471 481

472 482

473 483

474 484

411 421

412 422

415/416 425/426

413 423

417/418 427/428

414 424

419 429

451 461

452 462

453 463

454 464

A340-500/600 PYLONS AND ENGINES 1 AND 2 

A340-500/600 PYLONS AND ENGINES 3 AND 4 
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DE

A340 MRB REPORT 

Issue : July 2010 

A340-500/600

RR- ENGINE 1 (L OUTBOARD)

411 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

412 FAN AND ACCESSORY GEAR BOX 415 L FAN COWL 416 R FAN COWL 417 L THRUST REVERSER 418 R THRUST REVERSER 

 419 EXHAUST PLUG 

413 HOT SECTION 414 EXHAUST NOZZLE 451 PYLON LEADING EDGE 452 UPPER FWD PYLON 453 LOWER PYLON 454 LOWER AND REAR PYLON 

FAIRINGS 

A340-500/600

RR- ENGINE 2 (L INBOARD)

421 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

422 FAN AND ACCESSORY GEAR BOX 425 L FAN COWL 426 R FAN COWL 427 L THRUST REVERSER 428 R THRUST REVERSER 

 429 EXHAUST PLUG 

423 HOT SECTION 424 EXHAUST NOZZLE 461 PYLON LEADING EDGE 462 UPPER FWD PYLON 463 LOWER PYLON 465 LOWER AND REAR PYLON  FAIRINGS 

A340-500/600

RR-ENGINE 3 (R INBOARD)

431 ENGINE AIR INTAKE AND AIR 

INTAKE LIP 

432 FAN AND ACCESSORY GEAR BOX 435 L FAN COWL 436 R FAN COWL 437 L THRUST REVERSER 438 R THRUST REVERSER 

 439 EXHAUST PLUG 

433 HOT SECTION 434 EXHAUST NOZZLE 471 PYLON LEADING EDGE 472 UPPER FWD PYLON 473 LOWER PYLON 474 LOWER AND REAR PYLON 

 FAIRINGS 

RR EN

 441 ENGINE 

 INTAKE 

442 FAN AN445 L FAN C446 R FAN 447 L THRU448 R THRU449 EXHAU443 HOT SE444 EXHAU481 PYLON 482 UPPER 483 LOWER 484 LOWER 

FAIRIN
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

 TRIMMABLE HORIZONTAL 

STABILIZER CENTER SPAR BOX FUEL TANK 

HORIZONTAL TAIL (LH)

331 TRIMMABLE HORIZONTAL 

STABILIZER LEADING EDGE 

332 TRIMMABLE HORIZONTAL 

STABILIZER TIP 

333 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX 

334 TRIMMABLE HORIZONTAL 

STABILIZER TRAILING EDGE 

335 ELEVATOR 337 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX DRY BAY 

RIB19 TO RIB21 

HORIZONTAL TAIL (RH)

341 TRIMMABLE HORIZONTAL 

STABILIZER LEADING EDGE 

342 TRIMMABLE HORIZONTAL 

STABILIZER EDGE 

343 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX 

344 TRIMMABLE HORIZONTAL 

STABILIZER TRAILING EDGE 

345 ELEVATOR 346 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX VENT TANK 

347 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX DRY BAY 

RIB20 TO RIB21 

A340-200/300
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

 TRIMMABLE HORIZONTAL 

STABILIZER CENTER SPAR BOX FUEL TANK 

HORIZONTAL TAIL (LH)

331 TRIMMABLE HORIZONTAL 

STABILIZER LEADING EDGE 

332 TRIMMABLE HORIZONTAL 

STABILIZER TIP 

333 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX 

334 TRIMMABLE HORIZONTAL 

STABILIZER TRAILING EDGE 

335 ELEVATOR 337 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX DRY BAY 

RIB19 TO RIB21 

HORIZONTAL TAIL (RH)

341 TRIMMABLE HORIZONTAL 

STABILIZER LEADING EDGE 

342 TRIMMABLE HORIZONTAL 

STABILIZER EDGE 

343 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX 

344 TRIMMABLE HORIZONTAL 

STABILIZER TRAILING EDGE 

345 ELEVATOR 346 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX VENT TANK 

347 TRIMMABLE HORIZONTAL 

STABILIZER SPAR BOX DRY BAY 

RIB20 TO RIB21 

A340-500/600

Horizontal tail unit zones , left and rig
A340 MRB REPORT 

Issue : July 2010 

A340-200/300
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

A340-200/300

511 SLAT 1 512 SLAT 2 513 SLAT 3 514 SLAT 4 515 SLAT 5 516 SLAT 6 517 SLAT 7 521 INBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB 1 - STA0 

TO RIB9 - STA5676 

522 CENTER FIXED LEADING EDGE 

STRUCTURE 

RIB9 - STA5676 

TO RIB24 - STA16009 

523 OUTBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB24 - STA16009 

TO RIB39 - STA25566 

531 FLAP TRACK 2 FAIRING 532 FLAP TRACK 3 FAIRING 

533 FLAP TRACK 4 FAIRING 534 FLAP TRACK 5 FAIRING 535 WING TIP 541 INNER TANK 

RIB1 - STA0 

TO RIB23 - STA15298 

542 OUTER TANK 

RIB23 - STA15298 

TO RIB33 - STA21905 

550 VENT SURGE TANK 

RIB33 - STA21905 

TO RIB39 - STA25566 

562 PLASTRON FAIRING 571 MLG WELL 572 SHROUD BOX 573 INNER TRAILING EDGE FIXED 

STRUCTURE 

RIB6 

TO RIB12 

574 CENTER TRAILING EDGE FIXED 

STRUCTURE 

RIB12 

TO RIB27 

575 OUTER TRAILING EDGE FIXED 

STRUCTURE 

RIB27 

TO RIB39 

581 INBOARD FLAP 1 582 SPOILER 1 583 OUTBOARD FLAP 2 584 SPOILER 2 585 SPOILER 3 586 SPOILER 4 587 SPOILER 5 588 SPOILER 6 591 INBOARD AILERON 592 OUTBOARD AILERON 
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

A340-200/300

611 SLAT 1 612 SLAT 2 613 SLAT 3 614 SLAT 4 615 SLAT 5 616 SLAT 6 617 SLAT 7 621 INBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB 1 - STA0 

TO RIB9 - STA5676 

622 CENTER FIXED LEADING EDGE 

STRUCTURE 

RIB9 - STA5676 

TO RIB24 - STA16009 

623 OUTBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB24 - STA16009 

TO RIB39 - STA25566 

631 FLAP TRACK 2 FAIRING 632 FLAP TRACK 3 FAIRING 

633 FLAP TRACK 4 FAIRING 634 FLAP TRACK 5 FAIRING 635 WING TIP 641 INNER TANK 

RIB1 - STA0 

TO RIB23 - STA15298 

642 OUTER TANK 

RIB23 - STA15298 

TO RIB33 - STA21905 

650 VENT SURGE TANK 

RIB33 - STA21905 

TO RIB39 - STA25566 

662 PLASTRON FAIRING 671 MLG WELL 672 SHROUD BOX 673 INNER TRAILING EDGE FIXED 

STRUCTURE 

RIB6 

TO RIB12 

674 CENTER TRAILING EDGE FIXED 

STRUCTURE 

RIB12 

TO RIB27 

675 OUTER 

STRUC

RI

TO RI

681 INBOAR682 SPOILE683 OUTBO684 SPOILE685 SPOILE686 SPOILE687 SPOILE688 SPOILE691 INBOAR692 OUTBO
A340 MRB REPORT

Issue : July 2010 

A340-500/600 
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

A340-500/600

511 SLAT 1 512 SLAT 2 513 SLAT 3 514 SLAT 4 515 SLAT 5 516 SLAT 6 517 SLAT 7 521 INBOARD FIXED LEADING EDGE  STRUCTURE 

RIB 1 - STA0 

TO RIB9 - STA6778 

522 CENTER FIXED LEADING EDGE  STRUCTURE 

RIB9 - STA6778 

TO RIB24 - STA19156 

523 OUTBOARD FIXED LEADING EDGE  STRUCTURE 

RIB24 - STA19156 

TO RIB41 - STA32358 

531 FLAP TRACK 2 FAIRING 532 FLAP TRACK 3 FAIRING 

533 FLAP TRACK 4 FAIRING 534 FLAP TRACK 5 FAIRING 535 WING TIP 541 INNER TANK 

RIB1 - STA0 

TO RIB 6 - STA4375 TO RIB 11 - STA 9092 

542 OUTER TANK 

RIB23 - STA18492 

TO RIB35 - STA27826 

550 VENT SURGE TANK 

RIB35 - STA27826 

TO RIB41 - STA32358 

571 MLG WELL 572 SHROUD BOX 573 INNER TRAILING EDGE FIXED 

STRUCTURE 

RIB6 

TO RIB12 

574 CENTER TRAILING EDGE FIXED 

STRUCTURE 

RIB12 

TO RIB27 

575 OUTER TRAILING EDGE FIXED 

STRUCTURE 

RIB27 

TO RIB41 

581 INBOARD FLAP 1 582 SPOILER 1 583 OUTBOARD FLAP 2 584 SPOILER 2 585 SPOILER 3 586 SPOILER 4 587 SPOILER 5 588 SPOILER 6 591 INBOARD AILERON 592 OUTBOARD AILERON 
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

A340-500/600

611 SLAT 1 612 SLAT 2 613 SLAT 3 614 SLAT 4 615 SLAT 5 616 SLAT 6 617 SLAT 7 621 INBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB 1 - STA0 

TO RIB9 - STA5676 

622 CENTER FIXED LEADING EDGE 

STRUCTURE 

RIB9 - STA5676 

TO RIB24 - STA16009 

623 OUTBOARD FIXED LEADING EDGE 

STRUCTURE 

RIB24 - STA16009 

TO RIB39 - STA25566 

631 FLAP TRACK 2 FAIRING 

632 FLAP TRACK 3 FAIRING 

633 FLAP TRACK 4 FAIRING 634 FLAP TRACK 5 FAIRING 635 WING TIP 641 INNER TANK 

RIB1 - STA0 

TO RIB23 - STA15298 

642 OUTER TANK 

RIB23 - STA15298 

TO RIB33 - STA21905 

650 VENT SURGE TANK 

RIB33 - STA21905 

TO RIB39 - STA25566 

662 PLASTRON FAIRING 671 MLG WELL 672 SHROUD BOX 673 INNER TRAILING EDGE FIXED 

STRUCTURE 

RIB6 

TO RIB12 

674 CENTER TRAILING EDGE FIXED 

STRUCTURE 

RIB12 

TO RIB27 
SPECIF 

ZONES DESCRIPTION/BOUNDARIES 

SPECIF 

ZONES

SPECIF

DESCRIPTION/BOUNDARIES ZONES DESCRIPTION/BOUNDARIES

A340 MRB REPORT 

Issue : July 2010 

675 OUTER TRAILING EDGE FIXED 

STRUCTURE 

RIB27 

TO RIB39 

681 INBOARD FLAP 1 682 SPOILER 1 683 OUTBOARD FLAP 2 684 SPOILER 2 685 SPOILER 3 686 SPOILER 4 687 SPOILER 5 688 SPOILER 6 691 INBOARD AILERON 692 OUTBOARD AILERON 
SPECIF

ZONES DE

A340 MRB REPORT 

Issue : July 2010 

NOSE L

 711 NOSE G 712 LEG DO713/174 MAIN D715/716 AFT DO

MAIN L

 731 L MAIN  732 MLG - L 733 MLG -H 734 MLG - M

MAIN L

 741 R MAIN  742 MLG- L 743 MLG –H 744 MLG- M

CENTE

 751 CENTE 752 LEG DO753/754 CLG -M755/756 CLG- A

Landing Gear 
SPECIF

ZONES DE

A340 MRB REPORT 

Issue : July 2010 

811 FORWA

COMPAFR8 TO 

821 LOWER 

COMPAFR20A A

822 LOWER 

COMPAFR59A A

823 LOWER 

COMPAFR67 A

831 L FWD 

BETWE

832 L MID P

BETWE

833 L AFT P

BETWE

834 L EMER

FR53,5 

841 R FWD 

BETWE

842 R MID P

BETWE

843 R AFT P

BETWE

844 R EMER

FR53,5 
SPECIF

ZONES DE

A340 MRB REPORT 

Issue : July 2010 

811 FORWA COMPA FR8 TO 821 LOWER 

COMPAFR20A 

822 LOWER 

COMPAFR59A 

823 LOWER 

COMPAFR67 A

831 L FWD 

BETWE

832 L MID P

BETWE

833 L AFT P

BETWE

834 L EMER

FR53,5 

841 R FWD 

BETWE

842 R MID P

BETWE

843 R AFT P

BETWE

844 R EMER

FR53,5 
SPECIF

ZONES DE

A340 MRB REPORT 

Issue : July 2010 

811 

811 FORWA COMPA FR8 TO 821 LOWER 

COMPAFR20A 

822 LOWER 

COMPAFR59A 

823 LOWER 

COMPAFR67 A

831 L FWD 

BETWE

832 L MID P

BETWE

833 L AFT P

BETWE

834 L EMER

FR56.1A 

836 OVERW

FR41A 

841 R FWD 

BETWE

842 R MID P

BETWE

843 R AFT P

BETWE

844 R EMER

FR56.1A 

846 OVERW

FR41A 

846 

836 

836

846
 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 confirm 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. 
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 1 522 

622 

522AB 522BB 462DL 622AB 622BB 472 ER 

4C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the following harnesses end fittings, from rib 10A : - 7021VP, 7001VC- A, 7021VC- A, 7025VC- A, 10HA2, LH s- 7024VP, 7002VC- A, 7022VC- A, 7026VC- A, 10HA3, RH 

 20- 00- 01- 2 523 

623 

523AB 452EL 623AB 482ER 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the following harnesses end fittings, from rib 29: - 10HA1, 7003VC- A, 7013VC- A, 7015VC- A, 7023VC- A, 7A, LH side - 10HA4, 7004VC- A, 7014VC- A, 7016VC- A, 7024VC- A, 7

A, RH side

 20- 00- 01- 3 633 RAT extended 2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the connectors located on the RAT 

 R 20- 00- 01- 4 523 

623 

523NB 575DB 535AB 535CZ 623NB 675DB 635AB 635CZ 

C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

GVI of elements fitted on the following harnesses end fittingwing tip to rib 39: - 7621VB, 7623VB, 7625VB, 7627VB, LH side - 7622VB, 7624VB, 7626VB, 7628VB, RH side

 20- 00- 01- 5 533 

633 

533AB 574CB 574DB 574EB 574FB 533CB 633AB 674CB 674DB 674EB 674FB 633CB Flaps extended 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

GVI of elements fitted on the following harnesses end fittingrib19 to rib 14 : - 7633VB LH side - 7634VB RH side
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 6 531 

631 

531CB 573CB 573BB 573DB631CB 673CB 673BB 673DBFlaps extended 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

DET inspection of elements fitted on the following harnesses fittings, from rib 6 to fuselage : - 7651VB, 7681VB, 7683VB, LH side - 7652VB, 7682VB, 7684VB, RH side

 20- 00- 01- 7 571 

671 

Removal of fuel pump front fairing 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

GVI of the following braided conduit end fittings, from rib 6 tfuselage : - 100QA1- A, 101QA1- A, 100QA2- A, 101QA2- A, LH side - 100QA3- A, 101QA3- A, 100QA4- A, 101QA4- A, RH side

 20- 00- 01- 8 RESERVED  20- 00- 01- 9 531 

631 

531CB 573CB 573BB 573DB 631CB 673CB 673BB 673DBFlaps extended 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

DET inspection of elements fitted on the following harnesses fittings, from rib 6 to fuselage: - 7652VB, 7646VB, 7634VB, RH side - 7651VB, 7645VB, 7633VB, LH side

 20- 00- 01- 10 522 

622 

522AB 622AB 

4C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the following harnesses end fittings, from rib 10A : - 7001VC- A, 7021VC- A, 7025VC- A, LH side - 7008VC- A, 7022VC- A, 7026VC- A, RH side
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 11 523 

623 

523AB 623AB 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the following harnesses end fittings, from rib 29: ***** CONTINUED ***** - 7003VC- A, 7013VC- A, 7015VC- A, 7023VC-A, 7029VC-A7033VC-A LH side - 7004VC- A, 7014VC- A, 7016VC- A, 7024VC- A, 7034VC-A side

 20- 00- 01- 12 523 

623 

575DB 575EB 523RB 535AB 575CZ 535CB 675EB 623RB 675DB 635AB 635CZ 635CB Slats extended 

C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

GVI of elements fitted on the following harnesses end fittingwing tip to rib 41: - 7621VB, 7623VB, 7625VB, 7627VB, LH side - 7622VB, 7624VB, 7626VB, 7628VB, RH side

 20- 00- 01- 13 533 

633 

573FB 573BB 573CB 573DB673BB 673CB 673DB 673FBFLAP TRACK FAIRING 2 Flaps extended 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

 DET of elements fitted on the following harnesses end fittinrib 11 to fuselage : - 7633VB, 7645VB, 7639VB, 7651VB LH side - 7634VB, 7646VB,7640VB, 7652VB RH side 

 20- 00- 01- 14 191/192 

197/198 

Wing fillet fairings 521AB 621AB 

4C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Functional check of the following wing pressure seal bonding

 3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3743721VP, 3735VP, 3737VP, 3743VP
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 15 191/192 

197/198 

Wing fillet fairings 521AB 621AB 

4C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Functional check of the following wing pressure seal bonding

 3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3743721VP, 3735VP, 3737VP, 3743VP, 3204VP, 3207VP, 32083209VP

 20- 00- 02- 1 311 

312 

312AR 2C SECTION 19 BRAIDED CONDUIT 

Security check of the following harnesses end fittings at Fr. - 1CS- G, 1CS- H 

 20- 00- 03- 1 193 193AB 2C BELLY FAIRING BRAIDED CONDUIT 

GVI of elements fitted on the following harnesses end fittingFr. 39 to Fr. 40.2 : - 1541VB, 1543VB

R 20- 00- 03- 2 192 192EB 192QB 192GB 143AB 

193CB 193FB 193KB 195LB 191BB 

2C BELLY FAIRING BRAIDED CONDUIT 

GVI of elements fitted on the following harnesses end fittingFr. 37 to Fr. 49 : - 1541VB, 1543VB, 1542VB, 1544VB

R 20- 00- 03- 3 191 

192 198 

191CB 198GB 192CB 4C BELLY FAIRING BRAIDED CONDUIT 

Functional check of the following belly fairing pressure seal 3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VP

 20- 00- 03- 4 193 

195 197 198 

191CB, 192CB, 197EB 198GB 

4C BELLY FAIRING BRAIDED CONDUIT 

Functional check of the following belly fairing pressure seal 3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VP, 3203203VP
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 04- 1 RESERVED  20- 00- 05- 1 734 

744 

N/ A 2C MAIN LANDING GEAR BRAIDED CONDUIT 

Security check of the end fittings at MLG braided conduit 

 20- 00- 05- 2 734 

744 

N/ A 2C MAIN LANDING GEAR BRAIDED CONDUIT 

DET inspection of elements fitted on the route 2M from uniointerface bracket on strut at MLG braided conduit 

D 20- 00- 05- 3 TASK DELETED  20- 00- 06- 1 713 

714 

N/ A 2C NOSE LANDING GEAR 

Security check of the following harnesses end fittings at NLG conduit : - 1605VC- A, 1607VC- A, 2GH, 1GH

 20- 00- 06- 2 713 

714 

N/ A 2C NOSE LANDING GEAR 

Security check of the following harnesses end fittings at NLG conduit : - 1605VC- A, 1607VC- A
 A340 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Requ

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 07- 1 323 A340-200/-300: 

325BL 325DL 312AR 

2C VERTICAL FIN 

GVI of fly by wire protection installation at vertical fin: 5994VB 5995VB 5996VB 5997VB 

 20- 00- 07- 2 323 A340-200/-300: 

325BL 325DL 312AR A340-500/-600: 312AR 311AZ 325SL 325NL 313BL 

2C VERTICAL FIN 

GVI of fly by wire protection installation at vertical fin 5989VB 5994VB 5995VB 5996VB 5997VB 6989VB 6994VB 
 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 TEMPERATURE 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 - TEMPERATURE 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 – INTRODUCE 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 - ADAPT 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 - ADAPT 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 FLIGHT 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 – INTRODUCE 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 – INTRODUCE 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-ACTIVATE 

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 - ACTIVATE 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 GEAR
 A340 MRB REPORT 

Issue: 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 applicableHowever, where there is no source document, ‘MRBR APX 11’ is stated as a reference. ‘MRBR APX 11’ is also stated as an additional referebeen 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 be integrsubsequent revision. 

Item/ Component 

Part Number 

Comments / Reason Task Applicability Threshold/ 

Interval 

Source d

Shortening Mechanism Adjustable Link 

201479001 Inspection for cracks 

on eye ends 

Detailed Inspection of Adjustable Link Upper and Lower Eye Ends 

Pre Mod 49358 (A340-32-4173) 

Threshold: 3 YE Interval: 700FH 

A3

(MPD 

MLG Uplock Roller 

201275759 201489624 201489308 

Evidence of stress corrosion found on MLG Uplock Roller 

Inspection of MLG Uplock Roller for evidence of corrosion 

Pre Mod 50959 (A340-32-4202) 

Threshold: 5 YE or 25,000FH Interval: 5 YE or 25,000FH

A3

Bogie Pivot Pin 

201269612 201489621 201454925 201489751 

Prevention of Chrome Damage 

Reduced Lubrication interval 

All 250FC or 4MO S

(M-D 

MR

(MPD 

Braked Axle 

201272644 201272649 

Evidence of corrosion found on Axle 

Detailed Inspection of Axle Outer Diameter 

All 1C 

or at opportunity of Brake change 

S

MR

(MPD 

MLG Bogie Pivot Pin 

201269612 201489621 201454925 201489751 

In-service issue regarding chrome loss and corrosion 

In-service data collection on Bogie Pivot Pin inspection 

All At opportunity of 

Bogie Pivot Pin removal 

Vendo

A

MR

MLG Bellcrank 

20148300/301 20148353/354 20158306/307 20158300/301 

In-service issue regarding introducing grease to the Bellcrank 

Detailed Procedure for Lubricating the Bellcrank

All 250FC or 4 MO Vendo

A

MR

SM 8 Pin 201275789 

201478617 

In-service issue:  bush migration 

Reduced Lubrication interval 

All 250FC or 4MO MR

(MRBR 

SM 9 Pin 201275790 

201478616 

In-service issue:  bush migration 

Reduced Lubrication interval 

All 250FC or 4MO MR

(MRBR 
 A340 MRB REPORT 

Issue: July, 2010 Page: APX 11.3b) MLG modifications recommended to be accomplished prior to a 10 year TBO 

Airbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended product improvement mod

Gear overhaul. The benefit to the operator will be an improved operational reliability of the post mod parts and a lower level of degradation a

Vendor Service Bulletin Reference 

Airbus Service Bulletin Reference 

Mod Number 

Threshold/ Interval 

Description Introduced as 

Standard in 

Production From MSN: 

A33/34-32-171 A340-32-4173 49358 3 years from 

EIS 

Introduce new adjustable link assembly (201254 Series – Basic Gear) 

MSN 435 

A33/34-32-172 A340-32-4173 49358 3 years from 

EIS 

Introduce new adjustable link assembly (201489 Series – Growth Gear) 

MSN 435 

A33/34-32-197 A340-32-4178 49664 4 years from 

EIS 

New Shortening Mechanism connecting link (201254 Series – Basic Gear) 

MSN 454 

A33/34-32-198 A340-32-4178 49664 4 years from 

EIS 

New Shortening Mechanism connecting link (201489 Series – Growth Gear) 

MSN 454 
 A340 MRB REPORT 

Issue: July, 2010 Page: APX 11.4c) MLG modifications recommended to be accomplished at the 10 year overhaul Based on in-service data, Airbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended at first overhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to second overhaul. 

Vendor Service Bulletin Reference

Airbus Service Bulletin Reference 

Mod Number 

Description Introduced as 

Standard in 

Production 

From MSN: 

Com

A33/34-32-153 A340-32-4153 47523 New Aluminum Piston with Nickel under Chrome 

Oxide coating (201254 Series – Basic Gear) 

MSN 315 All in-

A33/34-32-154 A340-32-4153 47523 New Aluminum Piston with Nickel under Chrome 

Oxide coating (201489 Series – Growth Gear) 

MSN 315 All in-

A33/34-32-175 A340-32-4166 48246 New Bushes in Bogie Beam & Slider 

(201254 Series – Basic Gear) 

MSN 366 Bushe

stand

A33/34-32-176 A340-32-4166 48246 New Bushes in Bogie Beam & Slider 

(201489 Series – Growth Gear) 

MSN 366 Bushe

stand

A33/34-32-190 A340-32-4181 49777 Improved corrosion protection for Retraction Link & 

‘W’ Pin (201254 Series – Basic Gear)

MSN 454 Impro

applie

A33/34-32-191 A340-32-4181 49777 Improved corrosion protection for Retraction Link & 

‘W’ Pin (201489 Series – Growth Gear)

MSN 454 Impro

applie

A33/34-32-193 A340-32-4180 49806 New Axle with Additional Corrosion Protection 

(201254 Series – Basic Gear)

MSN 459 Appli

A33/34-32-194 A340-32-4180 49806 New Axle with Additional Corrosion Protection 

(201489 Series – Growth Gear)

MSN 459 Appli

A33/34-32-195 A340-32-4202 50959 Modified Uplock Roller assembly & new bolts 

(201254 Series – Basic Gear) 

MSN 527 Bas

over

A33/34-32-196 A340-32-4202 50959 Modified Uplock Roller assembly & new bolts 

(201489 Series – Growth Gear) 

MSN 527 Repla
 A340 MRB REPORT 

Issue: 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 

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhaul 

satisfacto

sampling 

Retraction Link 

201489311/12 Required for 

10 year TBO 

justification 

Two additional 

8-year samples 

(samples 

performed at 7.5 

years would be 

acceptable) 

Post Mod 

48066 

First Retraction Link 

available for sampling will 

be from January 2009 

8 Y

(based on 

sa

Retraction Actuator 

114256002-030 114256002-040 

Required for 

10 year TBO 

justification 

Additional 

sample to be performed at 

opportunity of 

Overhaul 

All Additional Retraction 

Actuator will be 

available 

for sampling from end of 

2008 

8 Y

(10-year 

based on s

* 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. As suchoverhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and complete overhaRetrospective compliance is currently not required for retraction actuators not having been overhauled. However, this is under review Once completed, sampling results will be communicated to the MRB/ISC for review. 
 A340 MRB REPORT 

Issue: 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 interv

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhaul 

satisfacto

sampling 

Main Gear Assembly 

201252001/002 

or 

201490001/002 

Required to 

justify 

20,000FC 

TBO interval 

One sample All Proposal is to sample 

MLG from MSN 428. 

Sample available by May 

2009 

17,

* 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 11.73 A340-200/300 NOSE LANDING GEARa) NLG required Inspection and Lubrication Tasks There are currently no required NLG inspections tasks affecting TBO intervals. b) NLG modifications recommended to be accomplished prior to a 10 year TBO There 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 overhaul Based on in-service data, Airbus and Messier-Dowty advise A340-200/300 operators to consider accomplishing the following recommended at first overhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to second overhaul. 

Vendor Service Bulletin Reference

Airbus Service Bulletin Reference 

Mod Number 

Description Introduced as 

Standard in 

Production 

From MSN:

Com

D23581-32-053 A340-32-4244 54793 Introduction of a New Shock Absorber Tube and 

Modification of the Material of the diaphragm 

MSN 793 Rep

the Tub
 A340 MRB REPORT 

Issue: 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 indivi

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhau

Retraction Actuator 

D23352000 series 

Required for 

10 year TBO 

justification 

Data from two 

Retraction 

Actuators at a 10 

year Overhaul 

and/or from two 

Fleet Leaders 

All Retraction Actuator will be 

available for sampling by 

end of 2008 

10 Y

To be justifie

from Overha

Fleet l

 Note: At the time of the sampling program, the NLG Retraction Actuator was considered by the industry as an “on-condition” item. As such, 

 functionally tested at overhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and co

Retrospective compliance is currently not required for Retraction Actuators not having been overhauled. However, this is under review Once completed, sampling results will be communicated to the MRB/ISC for review. 
 A340 MRB REPORT 

Issue: 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/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhaul 

satisfactor

sampling n

Nose Gear Assembly 

D23285001 D23285051 D23285101 D23285151 D23581100 

Required to 

justify 

20,000FC 

TBO interval 

One sample All Proposal is to sample 

NLG from MSN 428. 

Sample available by May 

2009. 

17,00

* 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 REPORT 

Issue: July, 2010 Page: APX 11.11d) A340-200/300 CLG Shock Strut Assembly 8 year sample details 

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhaul 

satisfactory 

achi

CLG Shock Strut Assembly 

37100 series Required to 

justify 10 

Year and 

12,000FC 

TBO interval 

Two 8 year 

calendar 

samples 

‘F’ Standard 

(Mod 46880) 

1st CLG sampled from 

MSN 025 at Lufthansa 

Technik in March 2008. 

2nd CLG sampled from 

MSN 058 at M-D, Toronto 

in August 2008. 

Completed sample reports 

to be available by 

December 2008 

8 Year

* 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 
 

Page Intentionally left blank