Maintenance Review Board 

Report

Airbus A330 

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 intentionally left blank 
A330 MRB REPORT

Issue : July 2010 ROR Page : 1 

RECORD OF REVISIONS

REV. 

NO. 

ISSUE 

DATE 

DATE 

INSERTED 

BY REV. 

NO. 

ISSUE 

DATE 

DATE 

INSERTED 

BY 

0 14 OCT 93 

1 10 JUN 94 

2 23 DEC 94 

3 16 OCT 96 

4 07 APR 97 

5 31 MAR 98 

6 31 DEC 98 

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 intentionally left blank 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 1

SUMMARY OF CHANGES INCORPORATED INTO 

A330 MRB REPORT REVISION 12 

GENERAL

The A330 MRB REPORT revision 12 (Sep 2009) is issued to: 

- Add A330-200 Freighter requirements 

- 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 GROUPs 32E and 33E updated. New WV GROUP 32F added 

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 A1 

Paragraph 1 A330-200F models added. 

Page A2 

Paragraph 3 “A330-200F” added. 

Paragraph 5 “(including EWIS)” added 

SECTION B

Page B1 

Rule 8: “Damage Tolerant” added for clarification 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 2

Rule 18: Reworded to add EWIS compliance notes. 

 

SECTION C

Page C-INTRO-1 1. GENERAL. Note (d): “PW 4164/4168” changed to “PW 4000”. 

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

34.48.00, 38.10.01, 46.11.00, 52.36.00. 

Page C-INTRO-3 Paragraph 1 (l) Reworded to add EWIS compliance notes.

Page C-INTRO-4 Paragraph 2 NOTE 10: Following note added: 

“For A330-200F applicable for FWD Passenger/Crew Door only.” 

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 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)." 

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)." 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 3

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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)." 

IN APPLICABILITY: "A330-200F" ADDED 

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 20.0.161/01 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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.161/02 R 

DESCRIPTION CHANGED FROM: "WIRING ROUTES INSTALLED 

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

"ROUTES INSTALLED IN THE BULK CARGO COMPARTMENT, 

(EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.161/03 N NEW TASK ADDED 

C-20 20.0.161/04 N NEW TASK ADDED 

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)." 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 4

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-20 20.0.221/01 R 

IN TASK TITLE: "/ COURIER COMPARTMENT" ADDED 

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 SEATS AND A/C AND 

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 

SEAT TO SEAT CONNECTION," 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 

C-20 20.0.221/02 R 

IN TASK TITLE: "/ COURIER COMPARTMENT" ADDED 

DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN 

THE FWD CABIN UTILITY AREA (ONLY CONTAMINATED 

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

CABIN UTILITY AREA (ONLY IF 

CONTAMINATED), (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.221/03 R 

IN TASK TITLE: "/ COURIER COMPARTMENT" ADDED 

DESCRIPTION CHANGED FROM: "WIRING ROUTES INSTALLED 

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

THIS AREA, (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.221/04 N NEW TASK ADDED 

C-20 20.0.221/05 N NEW TASK ADDED 

C-20 20.0.221/06 N NEW TASK ADDED 

C-20 20.0.223/01 R 

TASK TITLE CHANGED FROM: "COPMPARTMENT", TO: 

"COMPARTMENT / COURIER OVERH EAD COMPARTMENT" 

DESCRIPTION CHANGED FROM: "ALL WIRING AND CIRCUIT 

BREAKERS "5001 VE" INSTALLED IN THE FWD CABIN 

ULITY AREA OVERHEAD COMPARTMENT (ONLY 

CONTAMINATED 

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

CIRCUIT BREAKERS "5001 VE" INSTALLED IN THE FWD 

CABIN ULITY AREA OVERHEAD COMPARTMENT (ONLY IF 

CONTAMINATED), (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 5

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-20 20.0.223/02 R 

TASK TITLE CHANGED FROM: "COPMPARTMENT", TO: 

"COMPARTMENT / COURIER OVERH EAD COMPARTMENT" 

DESCRIPTION CHANGED FROM: "INSTALLED IN THE 

FORWARD CABIN UTILITY AREA OVERHEAD COMPARTMENT, 

(EZAP).", TO: "AND 'G, AND P' ROUTES INSTALLED IN 

THE FWD CABIN UTILITY AREA OVERHEAD 

COMPARTMENT, (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.223/03 N NEW TASK ADDED 

C-20 20.0.223/04 N NEW TASK ADDED 

C-20 20.0.230/01 N NEW TASK ADDED 

C-20 20.0.230/02 N NEW TASK ADDED 

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.", 

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." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.233/03 N NEW TASK ADDED 

C-20 20.0.240/01 N NEW TASK ADDED 

C-20 20.0.240/02 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 6

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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 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 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," 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.243/01 R 

DESCRIPTION CHANGED FROM: "WIRING INSTALLED IN THE 

MID CABIN UTILITY AREA OVERHEAD COMPARTMENT AREA 

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

INSTALLED IN THE MID CABIN 

UTILITY AREA OVERHEAD COMPARTMENT AREA (ONLY IF 

CONTAMINATED), (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.243/03 N NEW TASK ADDED 

C-20 20.0.250/01 N NEW TASK ADDED 

C-20 20.0.250/02 N NEW TASK ADDED 

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", 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 AND/OR SEAT TO 

SEAT CONNECTION," 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 7

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.251/03 R 

DESCRIPTION CHANGED FROM: ""G" WIRING ROUTES 

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

ROUTES INSTALLED IN THIS AREA.(EWIS)" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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). 

." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.253/04 N NEW TASK ADDED 

C-20 20.0.260/01 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", TO: 

"EWIS CONNECTIONS, 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," 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.263/01 R 

DESCRIPTION CHANGED FROM: "ALL WIRING INSTALLED IN 

THE AFT CABIN OVERHEAD COMPARTMENT AREA (ONLY 

CONTAMINED WIRING), (EZAP).", TO: "EWIS INSTALLED 

IN THE AFT CABIN OVERHEAD 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.263/04 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 8

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-20 20.0.270/01 N NEW TASK ADDED 

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 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 EWIS 

CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEAT TO 

SEAT CONNECTION, ONLY." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

NOTE OR A330-300 NOTE" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.271/03 R 

DESCRIPTION CHANGED FROM: "WIRING ROUTES IN THIS 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-20 20.0.273/01 R 

DESCRIPTION CHANGED FROM: "ALL WIRING AND CIRCUIT 

BREAKERS "5005 VE" INSTALLED IN THE AFT CABIN 

UTILITY AREA OVERHEAD COMPARTMENT (ONLY 

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

AND CIRCUIT BREAKERS "5005 VE" INSTALLED IN THE 

AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (ONLY 

IF CONTAMINATED), (EWIS)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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)." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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)." 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 9

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-20 20.0.319/01 R 

DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS 

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

(EWIS)." 

APPLICABILITY CHANGED FROM: "PRE 41600", TO: 

"A330-200 PRE 41600 OR A330-300 PRE 41600" 

C-20 20.0.319/02 R 

DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS 

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

(EWIS)." 

APPLICABILITY CHANGED FROM: "POST 41600", TO: 

"A330-200 POST 41600 OR A330-300 POST 41600 OR 

A330-200F" 

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)." 

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)." 

APPLICABILITY CHANGED FROM: "PRE 43491", TO: 

"A330-200 PRE 43491 OR A330-300 PRE 43491" 

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)." 

APPLICABILITY CHANGED FROM: "POST 43491 PRE 

44818", TO: "A330-200 POST 43491 PRE 44818 OR 

A330-300 POST 43491 PRE 44818" 

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)." 

APPLICABILITY CHANGED FROM: "POST 43491 PRE 

44818", TO: "A330-200 POST 43491 PRE 44818 OR 

A330-300 POST 43491 PRE 44818" 

C-20 20.0.333/05 R 

DESCRIPTION CHANGED FROM: "WIRING (AS FAR AS 

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

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

20LH/RH, (EWIS)." 

APPLICABILITY CHANGED FROM: "POST 44818", TO: 

"A330-200 POST 44818 OR A330-300 POST 44818 OR 

A330-200F" 

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)." 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 10

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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 20.0.550/01 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 21.21.00/04 R APPLICABILITY CHANGED FROM: "POST 46203", TO: 

"A330-200 POST 46203" 

C-21 21.21.00/05 R APPLICABILITY CHANGED FROM: "POST 46201", TO: 

"A330-200 POST 46201" 

C-21 21.21.00/13 N NEW TASK ADDED 

C-21 21.21.00/14 N NEW TASK ADDED 

C-21 21.23.00/02 R APPLICABILITY CHANGED FROM: "POST 46203", TO: 

"A330-200 POST 46203" 

C-21 21.28.00/02 R IN APPLICABILITY: "A330-200F" ADDED 

C-21 21.28.00/03 R 

APPLICABILITY CHANGED FROM: "POST 40379 PRE 

56296", TO: "A330-200 POST 40379 PRE 56296 OR 

A330-300 POST 40379 PRE 56296" 

C-21 21.28.00/04 R 

DESCRIPTION CHANGED FROM: "HARD WIRED", TO: 

"HARDWIRED" 

APPLICABILITY CHANGED FROM: "POST 40379 PRE 

56296", TO: "A330-200 POST 40379 PRE 56296 OR 

A330-300 POST 40379 PRE 56296" 

C-21 21.28.00/06 R APPLICABILITY CHANGED FROM: "POST 46441", TO: 

"A330-200 POST 46441 OR A330-300 POST 46441" 

C-21 21.28.00/07 R APPLICABILITY CHANGED FROM: "POST 46441", TO: 

"A330-200 POST 46441 OR A330-300 POST 46441" 

C-21 21.50.00/09 R 

APPLICABILITY CHANGED FROM: "PRE 43750 PRE 44729", 

TO: "A330-200 PRE 43750 PRE 44729 OR A330-300 PRE 

43750 PRE 44729" 

C-21 21.50.00/10 R 

APPLICABILITY CHANGED FROM: "POST 43750 OR POST 

44729", TO: "A330-200 POST 43750 OR A330-200 POST 

44729 OR A330-300 POST 43750 OR A330-300 POST 

44729" 

C-21 21.50.00/16 N NEW TASK ADDED 

C-23 23.33.00/03 R 

DESCRIPTION CHANGED FROM: "FROM IFE COMPONENTS 

INSTALLED IN THE CABIN (VCC/RCC).", TO: "(IF 

INSTALLED) FROM IFE COMPONENTS INSTALLED IN THE 

CABIN (VCC/RCC)" 

C-23 23.39.01/01 R 

DESCRIPTION CHANGED FROM: "ELEMENTS.", TO: 

"ELEMENTS ON TAILWIND SYSTEM" 

APPLICABILITY CHANGED FROM: "POST 54762 OR POST 

54946", TO: "A330-200/300 IF TAILWIND SYSTEM 

INSTALLED" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 11

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-23 23.73.00/01 R 

APPLICABILITY CHANGED FROM: "PRE 44058 PRE 48823 

OR PRE 45556 PRE 48823", TO: "A330-200 PRE 45556 

OR A330-200 PRE 48823 OR A330-300 PRE 44058 PRE 

45556 OR A330-300 PRE 48823" 

C-23 23.73.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-23 23.73.00/03 R 

100% INTERVAL CHANGED FROM: "2C NOTE 26", TO: "2 

C" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-23 23.73.00/05 R 

100% INTERVAL CHANGED FROM: "16000 FH", TO: "20000 

FH" 

APPLICABILITY CHANGED FROM: "POST 40823", TO: 

"POST 40823 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-23 23.73.01/01 N NEW TASK ADDED 

C-23 23.73.01/02 N NEW TASK ADDED 

C-23 23.73.01/03 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 25.22.00/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300 OR A330-200F IF CAS INSTALLED" 

C-25 25.22.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300 OR A330-200F IF CAS INSTALLED" 

C-25 25.22.00/03 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300 OR A330-200F IF CAS INSTALLED" 

C-25 25.23.44/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-25 25.23.44/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-25 25.27.00/01 R 

APPLICABILITY CHANGED FROM: "POST 45670 PRE 47423 

PRE 51617", TO: "A330-200 POST 45670 PRE 47423 PRE 

51617 OR A330-200 POST 45670 PRE 56746 OR A330-300 

POST 45670 PRE 47423 PRE 

51617 OR A330-300 POST 45670 PRE 56746" 

C-25 25.51.00/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

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: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 12

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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: 

"A330-200 POST 40611" 

C-25 25.51.00/04 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/05 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/06 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/07 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

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: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/09 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

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-131-01-1; ZL-151-01-1" 

REMOVED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/11 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/12 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/13 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/17 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 55381 OR A330-300 PRE 55380" 

C-25 25.51.00/19 N NEW TASK ADDED 

C-25 25.51.00/20 N NEW TASK ADDED 

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 TASK ADDED 

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 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 13

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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.", 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 25.55.00/01 N NEW TASK ADDED 

C-25 25.55.00/02 N NEW TASK ADDED 

C-25 25.55.00/03 N NEW TASK ADDED 

C-25 25.55.00/04 N NEW TASK ADDED 

C-25 25.55.00/05 N NEW TASK ADDED 

C-25 25.56.00/01 N NEW TASK ADDED 

C-25 25.56.00/02 N NEW TASK ADDED 

C-25 25.56.00/03 N NEW TASK ADDED 

C-25 25.56.00/04 N NEW TASK ADDED 

C-25 25.56.00/05 N NEW TASK ADDED 

C-25 25.56.00/06 N NEW TASK ADDED 

C-25 25.56.00/07 N NEW TASK ADDED 

C-25 25.56.00/08 N NEW TASK ADDED 

C-25 25.56.00/09 N NEW TASK ADDED 

C-25 25.56.00/10 N NEW TASK ADDED 

C-25 25.56.00/11 N NEW TASK ADDED 

C-25 25.56.00/12 N NEW TASK ADDED 

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." 

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

"OR VR NOTE 10" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 14

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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: "DS", 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 25.65.51/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300 OR A330-200F IF MEGAPHONE INSTALLED" 

C-25 25.65.51/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300 OR A330-200F IF MEGAPHONE INSTALLED" 

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

OVERHAULED." ADDED 

C-25 25.75.00/05 R IN ZIP-REFERENCE(S): "ZL-253-01-1" 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-26 26.18.02 N NEW ENTRY "NO TASK SELECTED" 

C-26 26.19.00/01 N NEW TASK ADDED 

C-26 26.19.00/02 N NEW TASK ADDED 

C-26 26.23.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "POST 40041 

OR POST 44601" 

C-27 27.21.00/03 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/04 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/05 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/06 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 15

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-27 27.21.00/07 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/08 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/09 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/11 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/12 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/13 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.21.00/15 R 

APPLICABILITY CHANGED FROM: "POST 44442 PRE 

49144", TO: "A330-200 POST 44442 PRE 49144 OR 

A330-300 POST 44442 PRE 49144" 

C-27 27.21.00/18 R 

APPLICABILITY CHANGED FROM: "POST 49144", TO: 

"A330-200 POST 49144 OR A330-300 POST 49144 OR 

A330-200F" 

C-27 27.21.00/19 R 

APPLICABILITY CHANGED FROM: "POST 49144", TO: 

"A330-200 POST 49144 OR A330-300 POST 49144 OR 

A330-200F" 

C-27 27.21.00/20 R 

APPLICABILITY CHANGED FROM: "POST 49144", TO: 

"A330-200 POST 49144 OR A330-300 POST 49144 OR 

A330-200F" 

C-27 27.24.00/02 R 

IN DESCRIPTION: "(THIS TASK COVERS TASK 

29.10.00/08)" ADDED 

APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.24.00/03 R APPLICABILITY CHANGED FROM: "PRE 49144", TO: 

"A330-200 PRE 49144 OR A330-300 PRE 49144" 

C-27 27.24.00/06 R IN APPLICABILITY: "OR A330-200F" ADDED 

C-27 27.24.00/07 R IN APPLICABILITY: "OR A330-200F" ADDED 

C-27 27.24.00/08 R 

APPLICABILITY CHANGED FROM: "POST 49144", TO: 

"A330-200 POST 49144 OR A330-300 POST 49144 OR 

A330-200F" 

C-28 28.11.00/01 R IN APPLICABILITY: "A330-200F POST 58623 PRE 

200281" ADDED 

C-28 28.11.00/09 R IN APPLICABILITY: "A330-200F PRE 58623 OR 

A330-200F POST 200281" ADDED 

C-28 28.13.00/01 R IN APPLICABILITY: "A330-200F POST 58623 PRE 

200281" ADDED 

C-28 28.18.00/04 R IN APPLICABILITY: "A330-200F PRE 58623 OR 

A330-200F POST 200281" ADDED 

C-28 28.18.00/06 R IN APPLICABILITY: "A330-200F PRE 58623 OR 

A330-200F POST 200281" ADDED 

C-28 28.18.00/07 R IN APPLICABILITY: "A330-200F PRE 58623 OR 

A330-200F POST 200281" ADDED 

C-28 28.22.00/06 R IN APPLICABILITY: "A330-200F POST 58623 PRE 

200281" ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 16

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-28 28.23.00/03 R IN APPLICABILITY: "A330-200F POST 58623 PRE 

200281" ADDED 

C-28 28.24.00/03 N NEW TASK ADDED 

C-28 28.25.00/03 R IN APPLICABILITY: "A330-200F POST 58623 PRE 

200281" ADDED 

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

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

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

C-28 28.31.00/01 R IN APPLICABILITY: "A330-200F POST 45008" ADDED 

C-28 28.31.00/02 R IN APPLICABILITY: "A330-200F POST 45008" ADDED 

C-28 28.31.00/03 R IN APPLICABILITY: "A330-200F POST 45008" ADDED 

C-29 29.10.00/03 R APPLICABILITY CHANGED FROM: "PRE 47625", TO: 

"A330-200 PRE 47625 OR A330-300 PRE 47625" 

C-30 30.21.02 R TASK TITLE CHANGED FROM: "PW4164/PW4168)", TO: 

"PW4000)" 

C-30 30.46.00/01 R 

APPLICABILITY CHANGED FROM: "POST 40335 PRE 51642 

PRE 51617", TO: "A330-200 POST 40335 PRE 51642 PRE 

51617 OR A330-300 POST 40335 PRE 51642 PRE 51617" 

C-31 31.33.00/01 R 

IN DESCRIPTION: "(THIS TASK COVERS TASK 

31.36.01/01)" REMOVED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 48904 OR A330-300 PRE 48904"

C-31 31.33.00/02 R 

DESCRIPTION CHANGED FROM: "MCDU. (THIS TASK COVERS 

TASK 31.36.01/02)", TO: "THE MCDU." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 48904 OR A330-300 PRE 48904"

C-31 31.33.00/03 R 

IN DESCRIPTION: "(THIS TASK COVERS TASK 

31.36.01/03)" REMOVED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

PRE 48904 OR A330-300 PRE 48904" 

C-31 31.36.01/01 R 

IN DESCRIPTION: "(COVERED BY MSI 31.33.00, TASK 

01)" REMOVED 

APPLICABILITY CHANGED FROM: "POST 47606", TO: 

"POST 48904"

C-31 31.36.01/02 R 

DESCRIPTION CHANGED FROM: "MCDU (COVERED BY MSI 

31.33.00, TASK 02)", TO: "THE MCDU." 

APPLICABILITY CHANGED FROM: "POST 47606", TO: 

"POST 48904" 

C-31 31.36.01/03 R 

DESCRIPTION CHANGED FROM: "THE ULB (COVERED BY MSI 

31.33.00, TASK 03)", TO: "ULB" 

APPLICABILITY CHANGED FROM: "POST 47606", TO: 

"POST 48904" 

C-31 31.36.01/04 N NEW TASK ADDED 

C-33 33.51.00/05 R APPLICABILITY CHANGED FROM: "PRE 43069", TO: 

"A330-200 PRE 43069 OR A330-300 PRE 43069" 

C-33 33.51.00/06 R APPLICABILITY CHANGED FROM: "PRE 43069", TO: 

"A330-200 PRE 43069 OR A330-300 PRE 43069" 

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)" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 17

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

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 T2CAS-TAWS)" 

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 50860 POST 50453 PRE 53622", TO: 

"PRE 47245 PRE 53622 OR PRE 47245 POST 54662 OR 

PRE 50859 PRE 53622 OR PRE 

50859 POST 54662 OR POST 50860 PRE 53622 OR POST 

50860 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 35.10.00/04 R 

IN DESCRIPTION: "AND FUNCTIONAL CHECK OF OXYGEN 

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 35.10.00/08 N NEW TASK ADDED 

C-35 35.10.00/09 N NEW TASK ADDED 

C-35 35.10.00/10 N NEW TASK ADDED 

C-35 35.10.00/11 N NEW TASK ADDED 

C-35 35.10.00/12 N NEW TASK ADDED 

C-35 35.10.00/13 N NEW TASK ADDED 

C-35 35.10.00/14 N NEW TASK ADDED 

C-35 35.10.00/15 N NEW TASK ADDED 

C-35 35.10.00/16 N NEW TASK ADDED 

C-35 35.10.00/17 N NEW TASK ADDED 

C-35 35.10.00/18 N NEW TASK ADDED 

C-35 35.20.01/01 R 

APPLICABILITY CHANGED FROM: "PRE 40257 PRE 52485 

PRE 56322", TO: "A330-200 PRE 40257 PRE 52485 OR 

A330-300 PRE 40257 PRE 56322" 

C-35 35.20.01/02 R 

APPLICABILITY CHANGED FROM: "PRE 40257 PRE 52485 

PRE 56322", TO: "A330-200 PRE 40257 PRE 52485 OR 

A330-300 PRE 40257 PRE 56322" 

C-35 35.20.01/03 R 

APPLICABILITY CHANGED FROM: "PRE 40257 PRE 52485 

PRE 56322", TO: "A330-200 PRE 40257 PRE 52485 OR 

A330-300 PRE 40257 PRE 56322" 

C-35 35.20.01/04 R 

APPLICABILITY CHANGED FROM: "PRE 40257 PRE 52485 

PRE 56322", TO: "A330-200 PRE 40257 PRE 52485 OR 

A330-300 PRE 40257 PRE 56322" 

C-35 35.20.01/05 R 

APPLICABILITY CHANGED FROM: "PRE 40257 PRE 52485 

PRE 56322", TO: "A330-200 PRE 40257 PRE 52485 OR 

A330-300 PRE 40257 PRE 56322" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 18

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-35 35.20.02/01 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/02 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/03 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/04 R 

DESCRIPTION CHANGED FROM: "SYSTEM SHUT-OFF VALVES 

OPENING", TO: "THE SYSTEM SHUT-OFF VALVES 

(MOD.40257)/ PRESSURE REGULATORS (MOD.52485/56322) 

OPENING." 

APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/05 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/06 R 

100% INTERVAL CHANGED FROM: "2 A", TO: "1600 FH" 

APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/07 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/08 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/09 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/10 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/11 R 

APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257 PRE 52485 OR A330-300 POST 

40257 PRE 56322" 

C-35 35.20.02/12 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/13 R APPLICABILITY CHANGED FROM: "POST 40257", TO: 

"A330-200 POST 40257; A330-300 POST 40257" 

C-35 35.20.02/15 R 

APPLICABILITY CHANGED FROM: "POST 52485 OR POST 

56322", TO: "A330-200 POST 52485 OR A330-300 POST 

56322" 

C-35 35.20.02/16 R 

APPLICABILITY CHANGED FROM: "POST 52485 OR POST 

56322", TO: "A330-200 POST 52485 OR A330-300 POST 

56322" 

C-35 35.20.02/17 R 

APPLICABILITY CHANGED FROM: "POST 52485 OR POST 

56322", TO: "A330-200 POST 52485 OR A330-300 POST 

56322" 

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 36.00.00/06 R APPLICABILITY CHANGED FROM: "PW4164 OR PW4168 OR 

TRENT700", TO: "PW OR RR" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 19

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-36 36.00.00/07 R APPLICABILITY CHANGED FROM: "ALL", TO: "PRE 57418" 

C-36 36.00.00/12 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" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.10.00/02 N NEW TASK ADDED 

C-38 38.10.00/03 N NEW TASK ADDED 

C-38 38.10.01/01 N NEW TASK ADDED 

C-38 38.10.01/02 N NEW TASK ADDED 

C-38 38.10.01/03 N NEW TASK ADDED 

C-38 38.10.01/04 N NEW TASK ADDED 

C-38 38.10.01/05 N NEW TASK ADDED 

C-38 38.31.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/03 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/04 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/05 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/06 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/07 R 

DESCRIPTION CHANGED FROM: "COMPONENTS FOR WASTE 

TANK LEVEL MEASUREMENT.", TO: "REFERENCE PRESSURE 

LINE OF LIQUID LEVEL TRANSMITTER." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.31.00/08 N NEW ENTRY "TASK RESERVED" 

C-38 38.31.00/09 N NEW ENTRY "TASK RESERVED" 

C-38 38.31.00/10 N NEW ENTRY "TASK RESERVED" 

C-38 38.31.00/11 N NEW ENTRY "TASK RESERVED" 

C-38 38.31.00/12 N NEW ENTRY "TASK RESERVED" 

C-38 38.31.00/13 N NEW TASK ADDED 

C-38 38.31.01/01 N NEW TASK ADDED 

C-38 38.31.01/02 N NEW TASK ADDED 

C-38 38.31.01/03 N NEW TASK ADDED 

C-38 38.32.00/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.32.00/02 R 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.32.00/03 R 

APPLICABILITY CHANGED FROM: "POST 45556 OR POST 

49705 OR POST 50088", TO: "A330-200 POST 45556 OR 

A330-200 POST 49705 OR A330-200 POST 50088 OR 

A330-300 POST 45556 OR A330-300 POST 

49705 OR A330-300 POST 50088" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 20

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-38 38.40.00/01 R APPLICABILITY CHANGED FROM: "POST 40243", TO: 

"A330-200 POST 40243 OR A330-300 POST 40243" 

C-38 38.40.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-38 38.40.00/03 R APPLICABILITY CHANGED FROM: "POST 40243", TO: 

"A330-200 POST 40243 OR A330-300 POST 40243" 

C-46 46.11.00/01 N NEW TASK ADDED 

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

"CONFIGURATIONS" 

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

C-49 49.62.00/04 R 100% INTERVAL CHANGED FROM: "36 MO", TO: "2 C" 

C-52 52.10.00/01 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

C-52 52.10.00/02 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

C-52 52.10.00/04 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

C-52 52.10.00/10 N NEW TASK ADDED 

C-52 52.10.00/11 N NEW TASK ADDED 

C-52 52.10.00/12 N NEW TASK ADDED 

C-52 52.22.00/01 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/02 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/03 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/04 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/05 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/06 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/07 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/08 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.22.00/09 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

C-52 52.38.00/01 N NEW TASK ADDED 

C-52 52.38.00/02 N NEW TASK ADDED 

C-52 52.38.00/03 N NEW TASK ADDED 

C-52 52.38.00/04 N NEW TASK ADDED 

C-52 52.38.00/05 N NEW TASK ADDED 

C-52 52.38.00/06 N NEW TASK ADDED 

C-52 52.38.00/07 N NEW TASK ADDED 

C-52 52.51.11/01 R APPLICABILITY CHANGED FROM: "PRE 50014", TO: 

"A330-200 PRE 50014 OR A330-300 PRE 50014" 

C-52 52.51.11/02 R IN APPLICABILITY: "A330-200F IF COCKPIT DOOR 

INSTALLED" ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 21

SECTION TASK 

NUMBER 

Rev 

Code SUMMARY OF CHANGE 

C-52 52.51.11/03 R IN APPLICABILITY: "A330-200F IF COCKPIT DOOR 

INSTALLED" ADDED 

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 

C-53 53.19.00/10 N NEW TASK ADDED 

C-54 PW 

4000 54.59.00/01 R TASK TITLE CHANGED FROM: "4164/PW 4168)", TO: "4000)" 

 

SECTION D

Page D-INTRO-17 Weight Variant Table updated to add WV 059 and 060 to Group 32E, and WV 

054 deleted from Group 33E. New WV GROUP 32F added. 

 Following note added under WV table: 

 NOTE: Fatigue tasks for the A330-200F (WV GROUP 32F) will be included in 

 a later revision of the MRBR. 

Page D-INTRO-16 8. NOTES FOR SECTION D . New note 8 added: 

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

Page D-INTRO-20 Applicability Table updated to include A330-200F and to clarify that A330-200 is 

PAX only 

STRUCTURE SECTION

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-52 521201-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 521202-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 521301-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 521302-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 522201-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 522202-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523101-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523102-01-1 R IN ACCESS: "821" ADDED 

D-52 523103-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 22

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-52 523105-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523201-01-2 R IN ZONE: "822" ADDED AND "800" REMOVED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523202-01-1 R IN ACCESS: "822" ADDED 

D-52 523203-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523205-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523301-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 523801-01-1 N NEW TASK ADDED 

D-52 523802-01-1 N NEW TASK ADDED 

D-52 523803-01-1 N NEW TASK ADDED 

D-52 523804-01-1 N NEW TASK ADDED 

D-52 523805-01-1 N NEW TASK ADDED 

D-52 523806-01-1 N NEW TASK ADDED 

D-52 523807-01-1 N NEW TASK ADDED 

D-52 528104-01-2 R TPS: "APPLICATION OF TPS TYPE 1 GRADE 2 OR GRADE 

3" ADDED 

D-52 528203-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-52 528206-01-1 N NEW TASK ADDED 

D-52 528207-01-1 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 531115-01-1 R APPLICABILITY CHANGED FROM: "PRE 40347", TO: 

"A330-200 PRE 40347 OR A330-300 PRE 40347" 

D-53 531115-01-2 R APPLICABILITY CHANGED FROM: "POST 40347", TO: 

"A330-200 POST 40347 OR A330-200F OR A330-300 POST 

40347" 

D-53 531116-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 531144-01-3 R IN PREPARATION TASKS: "LINING; TOILET" ADDED AND 

"AIR DUCTS; VACUUM PIPES" REMOVED 

D-53 531150-01-1 R IN ACCESS: "811" ADDED 

IN PREPARATION TASKS: "INSULATION PANELS" 

REMOVED 

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 531151-01-1 R IN PREPARATION TASKS: "INSULATION PANELS" 

REMOVED

D-53 531167-01-1 N NEW TASK ADDED 

D-53 531168-01-1 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 23

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 531169-01-1 N NEW TASK 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" 

APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE"

D-53 532107-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532117-01-2 R DESCRIPTION CHANGED FROM: "26, TO CROWN 

CENTER 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532119-01-1 R DESCRIPTION CHANGED FROM: "BINS' LOWER 

SURFACE) TO 

PASSENGER CABIN", TO: "BINS LOWER SURFACE) TO 

MAIN 

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532120-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532121-01-1 R DESCRIPTION CHANGED FROM: "CUT-OUT", TO: 

"CUT-OUTS" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532123-01-1 R DESCRIPTION CHANGED FROM: "CABIN FLOOR UP TO", 

TO: 

"MAIN DECK FLOOR UPTO" 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300"

D-53 532124-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

DECK" 

APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

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

DECK" 

APPLICABILITY CHANGED FROM: "ALL NOTE", TO: 

"A330-200 NOTE OR A330-300 NOTE"

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

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300"
 A330 MRB REPORT

Issue : July 2010 SOC Page : 24

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 532137-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532137-02-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532142-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532145-02-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532152-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532159-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 532160-01-2 R APPLICABILITY CHANGED FROM: "POST 40255", TO: 

"A330-200 POST 40255 OR A330-300 POST 40255" 

D-53 532161-01-2 R APPLICABILITY CHANGED FROM: "POST 43560 OR POST 

43956", TO: "A330-200 POST 43560 OR A330-200 POST 

43956 OR A330-300 POST 43560 OR A330-300 POST 

43956" 

D-53 532162-01-2 R APPLICABILITY CHANGED FROM: "POST 44620 OR POST 

41833 OR POST 45503", TO: "A330-200 POST 44620 OR 

A330-200 POST 41833 OR A330-200 POST 45503 OR 

A330-300 POST 44620 OR A330-300 POST 

41833 OR A330-300 POST 45503" 

D-53 532163-01-1 R DESCRIPTION CHANGED FROM: "CUT6OUT", TO: "CUTOUT" 

APPLICABILITY CHANGED FROM: "POST 43652", TO: 

"A330-200 POST 43652 OR A330-300 POST 43652" 

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

D-53 532167-01-1 N NEW TASK ADDED 

D-53 532168-01-1 N NEW TASK ADDED 

D-53 532169-01-1 N NEW TASK ADDED 

D-53 532170-02-1 N NEW TASK ADDED 

D-53 532171-02-1 N NEW TASK ADDED 

D-53 532172-01-1 N NEW TASK ADDED 

D-53 532175-01-1 N NEW TASK ADDED 

D-53 532177-01-1 N NEW TASK ADDED 

D-53 532178-02-1 N NEW TASK ADDED 

D-53 532179-01-1 N NEW TASK ADDED 

D-53 532180-01-1 N NEW TASK ADDED 

D-53 532181-01-1 N NEW TASK ADDED 

D-53 533009-01-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "12900 FC", TO: 

"13900 FC OR 41700 FH" 

D-53 533009-01-2 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL: "OR 54200 FH" ADDED 

IN APPLICABILITY: "GROUP 33C PRE 49202 PRE 52911" 

REMOVED 

D-53 533009-01-3 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "10600 FC", TO: 

"11400 FC OR 34300 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 25

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 533009-01-4 N NEW TASK ADDED 

D-53 533009-02-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4310 FC", TO: 

"4600 

FC OR 13900 FH" 

D-53 533009-02-2 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "3610 FC", TO: 

"3600 

FC OR 18100 FH" 

IN APPLICABILITY: "GROUP 33C PRE 49202 PRE 52911" 

REMOVED

D-53 533009-02-3 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "3500 FC", TO: 

"3800 

FC OR 11400 FH" 

D-53 533009-02-4 N NEW TASK ADDED 

D-53 533010-01-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "3650 FC", TO: 

"3900 

FC OR 11700 FH" 

D-53 533010-01-2 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL: "OR 15300 FH" ADDED 

IN APPLICABILITY: "GROUP 33C PRE 49202" REMOVED 

D-53 533010-01-3 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "3000 FC", TO: 

"3200 

FC OR 9700 FH" 

D-53 533010-01-4 N NEW TASK ADDED 

D-53 533012-01-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7600 FC", TO: 

"8100 

FC OR 24400 FH" 

D-53 533012-02-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "2140 FC", TO: 

"2300 

FC OR 6900 FH"

D-53 533013-01-2 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"18000 FC OR 72000 FH" 

SAMPLE INTERVAL CHANGED FROM: "15200 FC OR 

59300 

FH", TO: "14700 FC OR 73900 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-53 533013-01-3 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"19000 FC" 

SAMPLE INTERVAL CHANGED FROM: "15000 FC OR 

58800 

FH", TO: "15500 FC OR 46500 FH"

D-53 533013-01-4 N NEW TASK ADDED 

D-53 533014-01-1 R SAMPLE INTERVAL CHANGED FROM: "21600 FH", TO: 

"20900 FH" 

D-53 533014-01-2 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 41000 

FH", TO: "7300 FC OR 36800 FH" 

D-53 533016-01-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4100 FC", TO: 

"4400 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 26

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

FC OR 13200 FH" 

D-53 533016-01-2 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4000 FC", TO: 

"4300 

FC OR 13000 FH"

D-53 533016-01-4 N NEW TASK ADDED 

D-53 533018-01-1 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4360 FC", TO: 

"4300 

FC OR 21800 FH" 

IN APPLICABILITY: "GROUP 33C PRE 49202" REMOVED

D-53 533018-01-2 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4300 FC", TO: 

"4600 

FC OR 13800 FH"

D-53 533018-01-3 N NEW TASK ADDED 

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

FR.37.1 AND FR.47 FROM Y=-2390 TO Y=2390" ADDED 

AND "FAIRING PANELS BETWEEN FR 37.1 AND FR 47" 

REMOVED 

DESCRIPTION CHANGED FROM: "BETWEEN FR 37.1 AND 

FR 

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

FROM Y=-2390 TO Y=2390," 

APPLICABILITY CHANGED FROM: "PRE 50675", TO: 

"A330-200 PRE 50675 OR A330-300 PRE 50675" 

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

FR.37.1 AND FR.47 FROM Y=-2390 TO Y=2390" ADDED 

AND "FAIRING PANELS BETWEEN FR 37.1 AND FR 47" 

REMOVED 

DESCRIPTION CHANGED FROM: "BETWEEN FR 37.1 AND 

FR 

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

FROM Y=-2390 TO Y=2390," 

APPLICABILITY CHANGED FROM: "POST 50675", TO: 

"A330-200 POST 50675 OR A330-200F OR A330-300 POST 

50675" 

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," 

APPLICABILITY CHANGED FROM: "PRE 50675", TO: 

"A330-200 PRE 50675 OR A330-300 PRE 50675" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 27

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

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 

COVERED BY BELLY FAIRING, EXTERNAL SURFACE, 

LH/RH", TO: "LOWER PART BETWEEN FR.47 AND FR.56 

FROM Y=-2390 TO Y=2390, COVERED BY 

BELLY FAIRING, EXTERNAL SURFACE, LH/RH." 

APPLICABILITY CHANGED FROM: "POST 50675", TO: 

"A330-200 POST 50675 OR A330-200F OR A330-300 POST 

50675" 

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

D-53 533104-01-3 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "4900 FC", TO: 

"5000 

FC OR 15000 FH"

D-53 533106-01-2 R SAMPLE INTERVAL CHANGED FROM: "7400 FC OR 22100 

FH", TO: "6800 FC OR 20600 FH" 

D-53 533107-01-7 R DESCRIPTION CHANGED FROM: "STRU FRAMES 39 TO 

39.2 

WEB HOLE AREA JUST BELOW STRINGER AND 

FASTENERS 

AREA AT FRAMES JUNCTION BELOW STRINGER 29 

LEVEL, 

LH/RH", TO: "STRUCTURE FRAMES 39 

TO 39.2 WEB HOLE AREA JUST BELOW STRINGER 28 

AND 

FASTENERS AREA AT FRAMES JUNCTION BELOW 

STRINGER 

29 LEVEL, LH/RH." 

D-53 533124-01-2 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"21300 FC" 

SAMPLE INTERVAL CHANGED FROM: "20000 FC", TO: 

"21300 FC" 

D-53 533126-01-2 R DESCRIPTION CHANGED FROM: "AREA AROUND CLG 

AND MLG 

CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL 

SURFACE", TO: "SKIN PANEL, AREA AROUND CLG AND 

MLG 

CUTOUT TO AN EXTENT OF 15.0 

CM (6.0 IN) EXTERNAL SURFACE." 

D-53 533138-01-3 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

78000 

FH", TO: "19800 FC OR 59500 FH"

D-53 533145-01-3 R SAMPLE INTERVAL CHANGED FROM: "7100 FC", TO: 

"7050 

FC"

D-53 533145-01-4 R SAMPLE INTERVAL CHANGED FROM: "6200 FC", TO: 

"6100 

FC" 

D-53 533147-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 28

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 533148-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533150-01-1 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-53 533152-01-2 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"20000 FC NOTE 8" 

D-53 533152-01-5 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"20000 FC NOTE 8" 

D-53 533155-01-1 R SAMPLE INTERVAL CHANGED FROM: "9700 FC OR 30000 

FH", TO: "12600 FC OR 63100 FH" 

IN APPLICABILITY: "GROUP 33A OR GROUP 33B OR 

GROUP 

33C OR GROUP 33D" REMOVED 

D-53 533155-01-2 N NEW TASK ADDED 

D-53 533155-01-3 N NEW TASK ADDED 

D-53 533156-01-1 R SAMPLE INTERVAL CHANGED FROM: "18800 FH", TO: 

"18300 FH" 

D-53 533164-01-3 R SAMPLE INTERVAL CHANGED FROM: "12600 FC OR 

36600 

FH", TO: "13700 FC OR 68500 FH" 

IN APPLICABILITY: "GROUP 33A OR GROUP 33B OR 

GROUP 

33C OR GROUP 33D" REMOVED 

D-53 533164-01-6 N NEW TASK ADDED 

D-53 533164-01-7 N NEW TASK ADDED 

D-53 533170-01-1 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-53 533170-01-2 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-53 533171-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533179-01-2 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"19000 FC" 

SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

44800 

FH", TO: "11800 FC OR 35400 FH"

D-53 533182-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533182-02-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533184-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533185-01-1 N NEW TASK ADDED 

D-53 533188-01-1 N NEW TASK ADDED 

D-53 533190-01-1 R DESCRIPTION CHANGED FROM: "CABIN FLOOR LEVEL 

TO 

STR 9, LH/RH", TO: "MAIN DECK FLOOR LEVEL TO STR 

9, LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300"

D-53 533191-01-1 R DESCRIPTION CHANGED FROM: "CABIN", TO: "MAIN 

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 29

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

OR A330-300" 

D-53 533193-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 533195-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534108-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534110-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534113-01-1 R DESCRIPTION CHANGED FROM: "JOINT IN FOLLOWING 

CRACK STOPPER AREAS : - AT STR 13 AND STR 22 

LH/RH, FROM FR 54 TO FR 72 - AT STR 17 AND", TO: 

"JOINTS IN FOLLOWING CRACK STOPPER AREAS 

: - AT STR 13 AND STR 22 LH/RH, FROM FR 54 TO FR 

72 - AT STR 17 AND STR" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534113-02-1 R DESCRIPTION CHANGED FROM: "JOINT IN FOLLOWING 

CRACK STOPPER AREAS : - AT STR 13 AND STR 22 

LH/RH, FROM FR 54 TO FR 72 - AT STR 17 AND 24 

LH/RH, FROM FR 76 TO FR 80, EXTERNAL 

SURFACE. NOTE : - INSPECTION REQUIRES INSPECTION

OF LAP JOINT LOWER RIVET ROW. -", TO: "JOINTS IN 

FOLLOWING CRACK STOPPER AREAS : - AT STR 13 AND 

STR 22 LH/RH, FROM FR 54 TO FR 72 

- AT STR 17 AND STR 24 LH/RH, FROM FR 76 TO FR 80, 

EXTERNAL SURFACE. NOTE:" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534115-01-1 R DESCRIPTION CHANGED FROM: "JOINT", TO: "JOINTS" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534115-02-1 R DESCRIPTION CHANGED FROM: "JOINT IN FOLLOWING 

CRACK STOPPER AREAS : - AT STR 5 LH/RH, FROM FR 

54 

TO FR 72, - AT STR 6 LH/RH, FROM FR 72 TO FR 80, 

EXTERNAL SURFACE. NOTE : - 

INSPECTION REQUIRES INSPECTION OF LAP JOINT 

LOWER 

RIVET ROW. -", TO: "JOINTS IN FOLLOWING CRACK 

STOPPER AREAS : - AT STR 5 LH/RH, FROM FR 54 TO FR 

72, - AT STR 6 LH/RH, FROM FR 72 

TO FR 80, EXTERNAL SURFACE. NOTE:" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534116-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534117-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 30

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 534122-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534124-01-1 R DESCRIPTION CHANGED FROM: "26 LH/RH TO CROWN 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

INCLUDING 

CABIN", TO: "MAIN DECK FLOOR INCLUDING MAIN DECK" 

D-53 534130-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534132-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

DECK" 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300"

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

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534138-01-1 R IN DESCRIPTION: "FR" ADDED 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300"

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" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

DECK" 

APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE"

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

DECK" 

APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE"

D-53 534160-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 31

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-53 534161-01-1 R DESCRIPTION CHANGED FROM: "BIN LOWER SURFACE) 

TO 

PASSENGER CABIN", TO: "BINS LOWER SURFACE) TO 

MAIN 

DECK" 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-53 534162-01-1 R IN PREPARATION TASKS: "ACT IF INSTALLED; CEILINGS" 

ADDED AND "CEILING PANELS" REMOVED 

DESCRIPTION CHANGED FROM: "PASSENGER CABIN", 

TO: 

"MAIN DECK" 

APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-53 534167-01-1 N NEW TASK ADDED 

D-53 534168-01-1 N NEW TASK ADDED 

D-53 534169-01-1 N NEW TASK ADDED 

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

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

DECK" 

APPLICABILITY CHANGED FROM: "PRE 48980", TO: 

"A330-200 PRE 48980 OR A330-300 PRE 48980" 

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

DECK" 

APPLICABILITY CHANGED FROM: "PRE 48980", TO: 

"A330-200 PRE 48980 OR A330-300 PRE 48980" 

D-53 535103-01-1 R APPLICABILITY CHANGED FROM: "PRE 48980", TO: 

"A330-200 PRE 48980 OR A330-300 PRE 48980" 

D-53 535104-01-1 R APPLICABILITY CHANGED FROM: "PRE 48980", TO: 

"A330-200 PRE 48980 OR A330-300 PRE 48980" 

D-53 535109-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

APPLICABILITY CHANGED FROM: "PRE 44205", TO: 

"A330-200 PRE 44205 OR A330-300 PRE 44205" 

D-53 535111-02-1 R APPLICABILITY CHANGED FROM: "POST 44205", TO: 

"A330-200 POST 44205 OR A330-300 POST 44205" 

D-53 535116-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

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-271-05-1; 

ZL-273-01-1; ZL-273-02-1" ADDED 

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 32

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

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; ZL-171-02-2" 

ADDED 

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

D-53 535123-01-1 R 100% THRESHOLD CHANGED FROM: "10 YE", TO: "6 YE" 

100% INTERVAL CHANGED FROM: "10 YE", TO: "6 YE" 

CPCP: "CPCP" ADDED 

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

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

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

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

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

D-53 535129-01-1 R IN PREPARATION TASKS: "GALLEYS AND TOILETS IF 

INSTALLED" ADDED AND "TOILETS AND GALLEYS" 

REMOVED 

DESCRIPTION CHANGED FROM: "CABIN FLOOR LEVEL, 

INCLUDING FR80", TO: "MAIN DECK FLOOR LEVEL, 

INCLUDING FR 80" 

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

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

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

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" 

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

D-53 535131-01-1 R IN PREPARATION TASKS: "IF LDF (PARTIAL OR FULL 

BULK) INSTALLED: 833 843 161AZ" REMOVED 

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

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

APPLICABILITY CHANGED FROM: "POST 48980", TO: 

"A330-200 POST 48980 OR A330-200F OR A330-300 POST 

48980" 

D-54 545101-02-1 R APPLICABILITY CHANGED FROM: "PRE 48298", TO: 

"A330-200 PRE 48298 OR A330-300 PRE 48298" 

D-54 545101-02-2 R APPLICABILITY CHANGED FROM: "PW POST 48298 OR 

RR 

POST 48298", TO: "A330-200 PW POST 48298 OR 

A330-200F PW OR A330-300 PW POST 48298 OR A330-200

RR POST 48298 OR A330-200F RR OR 

A330-300 RR POST 48298" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 33

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-54 545104-02-

10 

R IN PREPARATION TASKS: "FASTENERS" REMOVED 

SAMPLE INTERVAL CHANGED FROM: "14200 FC", TO: 

"11000 FC" 

IN APPLICABILITY: "GROUP 32E GE" REMOVED 

D-54 545104-02-

11 

R IN PREPARATION TASKS: "FASTENERS" REMOVED 

DESCRIPTION CHANGED FROM: "RIB2.(2 FASTENER 

LOCATIONS/PYLON)", TO: "RIB 2 (2 FASTENER 

LOCATIONS/PYLON)." 

SAMPLE INTERVAL CHANGED FROM: "14200 FC", TO: 

"11400 FC" 

D-54 545104-02-

15 

N NEW TASK ADDED 

D-54 545104-02-

16 

N NEW TASK ADDED 

D-54 545104-02-

17 

N NEW TASK ADDED 

D-54 545104-02-

18 

N NEW TASK ADDED 

D-54 545104-02-

19 

N NEW TASK ADDED 

D-54 545104-02-

20 

N NEW TASK ADDED 

D-54 545104-02-6 R IN PREPARATION TASKS: "FASTENERS" REMOVED 

SAMPLE INTERVAL CHANGED FROM: "15100 FC OR 

50000 

FH", TO: "11600 FC OR 34800 FH" 

IN APPLICABILITY: "GROUP 32A GE POST 48298 OR 

GROUP 32A RR POST 48298 OR GROUP 33C GE POST 

48298; GROUP 33D GE POST 48298" REMOVED 

D-54 545104-02-7 R IN PREPARATION TASKS: "FASTENERS" REMOVED 

SAMPLE INTERVAL CHANGED FROM: "15100 FC OR 

50000 

FH", TO: "11900 FC OR 35700 FH" 

IN APPLICABILITY: "GROUP 32A PW POST 48298" 

REMOVED 

D-54 545104-02-8 R IN PREPARATION TASKS: "FASTENERS" REMOVED 

SAMPLE INTERVAL CHANGED FROM: "15300 FC OR 

45900 

FH", TO: "11600 FC OR 34800 FH" 

IN APPLICABILITY: "GROUP 33E GE" REMOVED 

D-54 545104-02-9 R IN PREPARATION TASKS: "FASTENERS" REMOVED 

SAMPLE INTERVAL CHANGED FROM: "15300 FC OR 

45900 

FH", TO: "11900 FC OR 35700 FH" 

D-54 545106-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-54 545108-04-1 R APPLICABILITY CHANGED FROM: "RR PRE 48298 OR GE 

PRE 48298", TO: "A330-200 GE PRE 48298 OR A330-300 

GE PRE 48298 OR A330-200 RR PRE 48298 OR A330-300 

RR PRE 48298" 

D-54 545108-04-2 R APPLICABILITY CHANGED FROM: "PW PRE 48298", TO: 

"A330-200 PW PRE 48298 OR A330-300 PW PRE 48298" 

D-54 545111-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 34

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-54 545118-02-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-54 545119-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-54 545121-02-1 R DESCRIPTION CHANGED FROM: "AREA", TO: "AREA, AS 

FAR AS VISIBLE." 

D-54 545121-02-2 R DESCRIPTION CHANGED FROM: "AREA", TO: "AREA, AS 

FAR AS VISIBLE." 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-54 545122-01-1 R APPLICABILITY CHANGED FROM: "GE POST 42102 

S11772", TO: "A330-200 GE POST 42102 S11772 OR 

A330-300 GE POST 42102 S11772" 

D-54 545122-01-2 R APPLICABILITY CHANGED FROM: "PW POST 42102 

S11772", TO: "A330-200 PW POST 42102 S11772 OR 

A330-200F PW OR A330-300 PW POST 42102 S11772" 

D-54 545122-01-3 R APPLICABILITY CHANGED FROM: "RR POST 42102 

S11772", TO: "A330-200 RR POST 42102 S11772 OR 

A330-200F RR OR A330-300 RR POST 42102 S11772" 

D-54 545122-01-4 R APPLICABILITY CHANGED FROM: "GE POST 42102 

S11723", TO: "A330-200 GE POST 42102 S11723 AND 

PRE 42102 S11772 OR A330-300 GE POST 42102 S11723 

AND PRE 42102 S11772" 

D-54 545122-01-5 R APPLICABILITY CHANGED FROM: "PW POST 42102 

S11723", TO: "A330-200 PW POST 42102 S11723 AND 

PRE 42102 S11772 OR A330-300 PW POST 42102 S11723 

AND PRE 42102 S11772" 

D-54 545122-01-6 R APPLICABILITY CHANGED FROM: "RR POST 42102 

S11723", TO: "A330-200 RR POST 42102 S11723 AND 

PRE 42102 S11772 OR A330-300 RR POST 42102 S11723 

AND PRE 42102 S11772" 

D-54 545124-02-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-54 545124-02-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F OR A330-300 POST 

43271" 

D-54 545126-02-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-54 545126-02-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F OR A330-300 POST 

43271" 

D-54 545128-01-1 R APPLICABILITY CHANGED FROM: "PRE 42044", TO: 

"A330-200 PRE 42044 OR A330-300 PRE 42044" 

D-54 545128-01-2 R APPLICABILITY CHANGED FROM: "POST 42044", TO: 

"A330-200 POST 42044 OR A330-200F OR A330-300 POST 

42044" 

D-54 545135-01-1 R IN ACCESS: "454CR; 464CR" ADDED 

APPLICABILITY CHANGED FROM: "PRE 48298", TO: 

"A330-200 PRE 48298 OR A330-300 PRE 48298" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 35

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-54 545137-01-1 R APPLICABILITY CHANGED FROM: "GE PRE 48298", TO: 

"A330-200 GE PRE 48298 OR A330-300 GE PRE 48298" 

D-54 545137-01-2 R APPLICABILITY CHANGED FROM: "PW PRE 48298", TO: 

"A330-200 PW PRE 48298 OR A330-300 PW PRE 48298" 

D-54 545137-01-3 R APPLICABILITY CHANGED FROM: "RR PRE 48298", TO: 

"A330-200 RR PRE 48298 OR A330-300 RR PRE 48298" 

D-54 545138-01-6 R SAMPLE INTERVAL CHANGED FROM: "12000 FC OR 

41900 

FH", TO: "12800 FC OR 50000 FH" 

IN APPLICABILITY: "GROUP 33A GE OR GROUP 33B GE 

OR 

GROUP 33C GE OR GROUP 33D GE; GROUP 33A PW OR 

GROUP 33B PW OR GROUP 33C PW OR GROUP 33D PW"

REMOVED

D-54 545142-01-1 R DESCRIPTION CHANGED FROM: "AREA 30 MM AROUND 

CUTOUT BETWEEN RIB 13 AND RIB 14", TO: "INTERNAL 

AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND 

RIB 

14." 

D-54 545150-02-1 R SAMPLE INTERVAL CHANGED FROM: "8900 FC OR 31200 

FH", TO: "9000 FC OR 27100 FH" 

IN APPLICABILITY: "GROUP 32A GE; GROUP 32A RR" 

REMOVED 

D-54 545150-02-

10 

N NEW TASK ADDED 

D-54 545154-01-1 R APPLICABILITY CHANGED FROM: "PRE 48298 AND PRE 

50003 AND PRE 54399", TO: "A330-200 PRE 48298 AND 

PRE 50003 AND PRE 54399 OR A330-300 PRE 48298 AND 

PRE 50003 AND PRE 54399" 

D-54 545158-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-54 545166-02-

13 

N NEW TASK ADDED 

D-54 545166-02-5 R SAMPLE INTERVAL CHANGED FROM: "7600 FC OR 26600 

FH", TO: "8100 FC OR 24300 FH" 

IN APPLICABILITY: "GROUP 32A GE; GROUP 32A PW" 

REMOVED 

D-54 545168-02-

13 

N NEW TASK ADDED 

D-54 545168-02-5 R IN ACCESS: "452CL; 452CR; 454BL; 454BR; 462CL; 

462CR; 464BL; 464BR" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7600 FC OR 26600 

FH", TO: "8100 FC OR 24300 FH" 

IN APPLICABILITY: "GROUP 32A GE; GROUP 32A PW" 

REMOVED 

D-54 545174-01-2 R SAMPLE INTERVAL CHANGED FROM: "9900 FC OR 34600 

FH", TO: "10700 FC OR 32000 FH" 

IN APPLICABILITY: "GROUP 32A PW" REMOVED 

D-54 545174-01-3 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 25200 

FH", TO: "7700 FC OR 23200 FH" 

IN APPLICABILITY: "GROUP 32A RR" REMOVED 

D-54 545174-01-6 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 36

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-54 545174-01-7 N NEW TASK ADDED 

D-54 545174-03-1 R APPLICABILITY CHANGED FROM: "PRE 48298 AND PRE 

50003 AND PRE 54399", TO: "A330-200 PRE 48298 AND 

PRE 50003 AND PRE 54399 OR A330-300 PRE 48298 AND 

PRE 50003 AND PRE 54399" 

D-54 545174-03-2 R APPLICABILITY CHANGED FROM: "POST 48298", TO: 

"A330-200 POST 48298; A330-300 POST 48298; 

A330-200F" 

D-54 545180-03-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-54 545180-03-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F OR A330-300 POST 

43271" 

D-55 551008-01-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-55 551015-01-1 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-55 551015-01-3 N NEW TASK ADDED 

D-55 551018-01-3 N NEW TASK ADDED 

D-55 551018-01-4 N NEW TASK ADDED 

D-55 551019-01-3 N NEW TASK ADDED 

D-55 551024-01-1 N NEW TASK ADDED 

D-55 551024-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-55 551028-01-4 R APPLICABILITY CHANGED FROM: "A330-200", TO: 

"GROUP 

32A OR GROUP 32E OR GROUP 32F" 

D-55 551028-02-4 R APPLICABILITY CHANGED FROM: "A330-200", TO: 

"GROUP 

32A OR GROUP 32E OR GROUP 32F" 

D-55 551029-01-3 R APPLICABILITY CHANGED FROM: "PRE 41600", TO: 

"A330-200 PRE 41600 OR A330-300 PRE 41600" 

D-55 551029-01-4 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE 

WATER 

PIPE" REMOVED 

APPLICABILITY CHANGED FROM: "POST 41600", TO: 

"A330-200 POST 41600 OR A330-300 POST 41600 OR 

A330-200F" 

D-55 551029-02-3 R APPLICABILITY CHANGED FROM: "PRE 41600", TO: 

"A330-200 PRE 41600 OR A330-300 PRE 41600" 

D-55 551029-02-4 R IN PREPARATION TASKS: "DISCONNECT SCAVENGE 

WATER 

PIPE" REMOVED 

APPLICABILITY CHANGED FROM: "POST 41600", TO: 

"A330-200 POST 41600 OR A330-300 POST 41600 OR 

A330-200F"

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

REMOVED 

IN PREPARATION TASKS: "PEELABLE HOLE COVERS" 

ADDED 

APPLICABILITY CHANGED FROM: "PRE 43491", TO: 

"A330-200 POST 41471 PRE 43491 OR A330-300 POST 

41471 PRE 43491" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 37

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

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

ADDED 

APPLICABILITY CHANGED FROM: "POST 43491 PRE 

44818", TO: "A330-200 POST 43491 PRE 44818 OR 

A330-300 POST 43491 PRE 44818"

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

ADDED 

APPLICABILITY CHANGED FROM: "POST 44818", TO: 

"A330-200 POST 44818 OR A330-300 POST 44818 OR 

A330-200F"

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

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

ADDED 

IN APPLICABILITY: "A330-200 PRE 41471; A330-300 

PRE 41471" ADDED 

D-55 552001-01-2 R IN ZIP-REFERENCE(S): "ZL-300-01-1" ADDED 

D-55 553010-01-2 R IN ZIP-REFERENCE(S): "ZL-324-01-1" ADDED 

D-55 553020-01-1 R APPLICABILITY CHANGED FROM: "A330-200", TO: 

"A330-200 POST 48979 OR A330-200F" 

D-55 553021-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

D-55 553022-01-2 R IN ACCESS: "322EL" ADDED AND "322DL" REMOVED 

IN APPLICABILITY: "A330-200F" ADDED 

D-55 553023-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

D-55 553024-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

D-55 553025-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

D-55 553026-01-2 R IN APPLICABILITY: "A330-200F" ADDED 

D-55 554001-01-2 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 554005-01-2 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 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 38

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-55 554020-01-1 R IN DESCRIPTION: "INCLUDING TRAILING EDGE," 

REMOVED 

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

IN APPLICABILITY: "A330-200F" ADDED

D-55 554021-01-1 R IN DESCRIPTION: "FORWARD FACE AND INTERNAL 

STRUCTURE AS FAR AS VISIBLE." REMOVED 

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

D-55 554021-01-2 R IN DESCRIPTION: "FORWARD FACE AND INTERNAL 

STRUCTURE AS FAR AS VISIBLE." REMOVED 

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

IN APPLICABILITY: "A330-200F" ADDED 

D-55 554022-01-1 D TASK DELETED 

D-55 554023-01-1 R IN ZONE: "325" REMOVED 

IN DESCRIPTION: "AND ACTUATOR ATTACHMENTS." 

REMOVED 

D-55 554023-01-2 R IN ZONE: "325" REMOVED 

IN DESCRIPTION: "AND ACTUATOR ATTACHMENTS." 

REMOVED 

IN APPLICABILITY: "A330-200F" ADDED 

D-55 554024-01-1 N NEW TASK ADDED 

D-55 554025-01-1 N NEW TASK ADDED 

D-55 554026-01-1 N NEW TASK ADDED 

D-55 554027-01-1 N NEW TASK ADDED 

D-55 554028-01-1 N NEW TASK ADDED 

D-55 554029-01-1 N NEW TASK ADDED 

D-56 562101-01-2 R DESCRIPTION CHANGED FROM: "PASSENGER CABIN 

WINDOW 

PANES INCLUDING PASSENGER/CREW", TO: "MAIN DECK

WINDOW PANES INCLUDING 

PASSENGER/COURIER/CREW" 

D-57 571107-01-1 N NEW TASK ADDED 

D-57 571107-01-3 N NEW TASK ADDED 

D-57 571107-01-4 R SAMPLE INTERVAL CHANGED FROM: "5520 FC OR 19300 

FH", TO: "6200 FC OR 18600 FH" 

IN APPLICABILITY: "GROUP 32A; GROUP 33C OR GROUP 

33D" REMOVED 

D-57 571108-01-4 N NEW TASK ADDED 

D-57 571108-01-5 R SAMPLE INTERVAL CHANGED FROM: "8100 FC OR 24300 

FH", TO: "8400 FC OR 25200 FH" 

D-57 571108-01-6 R SAMPLE INTERVAL CHANGED FROM: "7300 FC OR 35800 

FH", TO: "7400 FC OR 37300 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571108-01-7 R SAMPLE INTERVAL CHANGED FROM: "7100 FC OR 35000 

FH", TO: "8150 FC OR 24500 FH" 

D-57 571114-01-5 R SAMPLE INTERVAL CHANGED FROM: "12500 FC OR 

37600 

FH", TO: "13000 FC OR 39000 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 39

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 571114-01-6 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "18000 FC OR 72000 FH" 

SAMPLE INTERVAL CHANGED FROM: "10700 FC OR 

50000 

FH", TO: "10900 FC OR 54500 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571114-01-7 R SAMPLE INTERVAL CHANGED FROM: "10400 FC OR 

50000 

FH", TO: "11900 FC OR 35800 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571116-01-2 N NEW TASK ADDED 

D-57 571116-01-3 N NEW TASK ADDED 

D-57 571116-01-4 R SAMPLE INTERVAL CHANGED FROM: "5520 FC OR 19300 

FH", TO: "6200 FC OR 18600 FH" 

IN APPLICABILITY: "GROUP 32A; GROUP 33C OR GROUP 

33D" REMOVED 

D-57 571118-01-6 N NEW TASK ADDED 

D-57 571118-01-7 R SAMPLE INTERVAL CHANGED FROM: "5520 FC OR 19300 

FH", TO: "6200 FC OR 18600 FH" 

IN APPLICABILITY: "GROUP 32A; GROUP 33C OR GROUP 

33D" REMOVED 

D-57 571118-01-8 N NEW TASK ADDED 

D-57 571122-01-4 R SAMPLE INTERVAL CHANGED FROM: "4580 FC OR 16000 

FH", TO: "4900 FC OR 14700 FH" 

D-57 571125-01-3 R SAMPLE INTERVAL CHANGED FROM: "5800 FC OR 20200 

FH", TO: "6150 FC OR 18500 FH" 

D-57 571125-01-4 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "18000 FC OR 72000 FH" 

SAMPLE INTERVAL CHANGED FROM: "4240 FC OR 14800 

FH", TO: "4000 FC OR 20000 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571125-01-5 R SAMPLE INTERVAL CHANGED FROM: "4100 FC OR 14500 

FH", TO: "4400 FC OR 13300 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571126-01-3 R SAMPLE INTERVAL CHANGED FROM: "13200 FC OR 

39500 

FH", TO: "13600 FC OR 41000 FH" 

D-57 571126-01-4 R DESCRIPTION CHANGED FROM: "CENT WING BOX, REAR

SPARE", TO: "CENTER WING BOX, REAR SPAR" 

SAMPLE INTERVAL CHANGED FROM: "11700 FC OR 

35200 

FH", TO: "10800 FC OR 54200 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571126-01-5 R DESCRIPTION CHANGED FROM: "CENT", TO: "CENTER" 

SAMPLE INTERVAL CHANGED FROM: "11400 FC OR 

34400 

FH", TO: "11900 FC OR 35700 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571129-01-4 R SAMPLE INTERVAL CHANGED FROM: "12000 FC OR 

34700 

FH", TO: "11500 FC OR 34600 FH"

D-57 571130-01-3 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 23800 

FH", TO: "6900 FC OR 20700 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 40

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 571140-01-1 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-57 571140-02-1 R APPLICABILITY CHANGED FROM: "NOTE", TO: "A330-200 

NOTE OR A330-300 NOTE" 

D-57 571140-02-2 N NEW TASK ADDED 

D-57 571144-01-1 R SAMPLE INTERVAL CHANGED FROM: "9500 FC OR 28500 

FH", TO: "9600 FC OR 28800 FH" 

D-57 571145-01-1 R SAMPLE INTERVAL CHANGED FROM: "22700 FH", TO: 

"22900 FH" 

D-57 571145-01-3 R SAMPLE INTERVAL CHANGED FROM: "8200 FC OR 40100 

FH", TO: "8150 FC OR 40700 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571145-01-6 R SAMPLE INTERVAL CHANGED FROM: "8000 FC OR 39300 

FH", TO: "9000 FC OR 27200 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571146-02-4 R SAMPLE INTERVAL CHANGED FROM: "9200 FC OR 27800 

FH", TO: "9600 FC OR 28800 FH" 

D-57 571146-02-5 R SAMPLE INTERVAL CHANGED FROM: "7700 FC OR 37800 

FH", TO: "7900 FC OR 39400 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571146-02-8 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 36800 

FH", TO: "8650 FC OR 25900 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571154-01-1 R IN ZIP-REFERENCE(S): "ZL-141-01-2" REMOVED 

D-57 571159-01-3 R DESCRIPTION CHANGED FROM: "SPARE", TO: "SPAR" 

SAMPLE INTERVAL CHANGED FROM: "8600 FC OR 25100 

FH", TO: "8350 FC OR 25000 FH" 

D-57 571159-01-4 R DESCRIPTION CHANGED FROM: "SPARE", TO: "SPAR" 

SAMPLE INTERVAL CHANGED FROM: "9900 FC OR 28800 

FH", TO: "8850 FC OR 44400 FH" 

IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 571159-01-5 R DESCRIPTION CHANGED FROM: "SPARE", TO: "SPAR" 

SAMPLE INTERVAL CHANGED FROM: "9800 FC OR 28400 

FH", TO: "9450 FC OR 28300 FH" 

IN APPLICABILITY: "GROUP 33C" ADDED 

D-57 571159-01-6 R DESCRIPTION CHANGED FROM: "SPARE", TO: "SPAR" 

D-57 571159-01-7 R DESCRIPTION CHANGED FROM: "SPARE", TO: "SPAR" 

D-57 572001-02-1 R SAMPLE INTERVAL CHANGED FROM: "5700 FC OR 22900 

FH", TO: "5100 FC OR 23400 FH" 

D-57 572001-02-3 R SAMPLE INTERVAL CHANGED FROM: "5500 FC OR 17200 

FH", TO: "5600 FC OR 16700 FH" 

D-57 572001-02-4 R SAMPLE INTERVAL CHANGED FROM: "5300 FC OR 16600 

FH", TO: "5400 FC OR 15900 FH" 

D-57 572002-01-8 R SAMPLE THRESHOLD CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "20000 FC OR 50000 FH NOTE 8" 

D-57 572003-01-

10 

R IN DESCRIPTION: "BOTTOM SKIN" ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 41

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572003-01-4 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "8500 FC OR 34100 

FH", TO: "6200 FC OR 28100 FH" 

D-57 572003-01-5 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

D-57 572003-01-6 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "8300 FC OR 26000 

FH", TO: "6700 FC OR 20000 FH" 

D-57 572003-01-7 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7900 FC OR 24700 

FH", TO: "6400 FC OR 19100 FH" 

D-57 572003-01-9 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

D-57 572003-02-2 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-57 572003-02-3 R IN DESCRIPTION: "BOTTOM SKIN" ADDED 

APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F POST 43271 OR 

A330-300 POST 43271" 

D-57 572004-02-3 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 24400 

FH", TO: "8100 FC OR 24000 FH" 

D-57 572005-01-8 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 24400 

FH", TO: "9700 FC OR 28700 FH" 

D-57 572005-01-9 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 24400 

FH", TO: "9700 FC OR 28700 FH" 

D-57 572007-01-5 R SAMPLE INTERVAL CHANGED FROM: "13300 FC OR 

41700 

FH", TO: "13800 FC OR 40800 FH" 

D-57 572008-01-4 R SAMPLE INTERVAL CHANGED FROM: "6700 FC OR 21000 

FH", TO: "6900 FC OR 20500 FH" 

D-57 572010-02-4 R SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 28100 

FH", TO: "6400 FC OR 29100 FH" 

D-57 572010-02-6 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 21300 

FH", TO: "6900 FC OR 20500 FH" 

D-57 572010-02-7 R SAMPLE INTERVAL CHANGED FROM: "6600 FC OR 20700 

FH", TO: "6700 FC OR 20000 FH" 

D-57 572012-02-1 R SAMPLE INTERVAL CHANGED FROM: "5300 FC OR 21300 

FH", TO: "4700 FC OR 21400 FH" 

D-57 572012-02-2 R SAMPLE INTERVAL CHANGED FROM: "6400 FC OR 20000 

FH", TO: "6300 FC OR 18800 FH" 

D-57 572012-02-3 R SAMPLE INTERVAL CHANGED FROM: "15900 FH", TO: 

"15000 FH" 

D-57 572012-02-4 R SAMPLE INTERVAL CHANGED FROM: "4900 FC OR 15300 

FH", TO: "4800 FC OR 14300 FH" 

D-57 572013-03-1 R SAMPLE INTERVAL CHANGED FROM: "7300 FC", TO: 

"6400 

FC"

D-57 572013-03-2 R SAMPLE INTERVAL CHANGED FROM: "6400 FC OR 20000 

FH", TO: "6300 FC OR 18700 FH" 

D-57 572013-03-3 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22500 

FH", TO: "7100 FC OR 21100 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 42

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572013-03-4 R SAMPLE INTERVAL CHANGED FROM: "6700 FC OR 21000 

FH", TO: "6600 FC OR 19600 FH" 

D-57 572013-04-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-57 572013-04-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F POST 43271 OR 

A330-300 POST 43271" 

D-57 572014-02-2 R SAMPLE INTERVAL CHANGED FROM: "8100 FC OR 25400 

FH", TO: "7900 FC OR 23300 FH" 

D-57 572015-02-1 R SAMPLE INTERVAL CHANGED FROM: "7600 FC OR 30500 

FH", TO: "6800 FC OR 31200 FH" 

D-57 572015-02-2 R SAMPLE INTERVAL CHANGED FROM: "6500 FC OR 20300 

FH", TO: "6600 FC OR 19600 FH" 

D-57 572015-02-3 R SAMPLE INTERVAL CHANGED FROM: "8000 FC OR 25000 

FH", TO: "8100 FC OR 23900 FH" 

D-57 572015-02-4 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 21300 

FH", TO: "6900 FC OR 20500 FH" 

D-57 572016-02-4 R SAMPLE INTERVAL CHANGED FROM: "3400 FC OR 13600 

FH", TO: "3100 FC OR 14200 FH" 

D-57 572016-02-5 R SAMPLE INTERVAL CHANGED FROM: "4500 FC OR 14100 

FH", TO: "4600 FC OR 13600 FH" 

D-57 572016-02-6 R SAMPLE INTERVAL CHANGED FROM: "3400 FC OR 10600 

FH", TO: "3500 FC OR 10400 FH" 

D-57 572016-02-7 D TASK DELETED 

D-57 572017-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "54900 FH", TO: 

"50000 FH" 

D-57 572017-01-

11 

R SAMPLE INTERVAL CHANGED FROM: "70900 FH", TO: 

"50000 FH" 

D-57 572018-01-

11 

R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22500 

FH", TO: "7300 FC OR 21600 FH" 

D-57 572018-01-

12 

N NEW TASK ADDED 

D-57 572018-01-5 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 31300 

FH", TO: "7100 FC OR 32300 FH" 

D-57 572018-01-6 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22500 

FH", TO: "7300 FC OR 21700 FH" 

D-57 572018-01-7 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 23500 

FH", TO: "10900 FC OR 31000 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C OR 

GROUP 

33D POST 48437",TO "GROUP 33C POST 48437 OR 

GROUP 

33D POST 48437" 

D-57 572019-01-

11 

R SAMPLE INTERVAL CHANGED FROM: "5500 FC OR 17200 

FH", TO: "5600 FC OR 16600 FH" 

D-57 572019-01-

12 

N NEW TASK ADDED 

D-57 572019-01-5 R SAMPLE INTERVAL CHANGED FROM: "6000 FC OR 24100 

FH", TO: "5400 FC OR 24900 FH" 

D-57 572019-01-6 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22500 

FH", TO: "7300 FC OR 21700 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 43

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572019-01-7 R SAMPLE INTERVAL CHANGED FROM: "5800 FC OR 18100 

FH", TO: "8100 FC OR 23200 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C OR 

GROUP 

33D POST 48437",TO "GROUP 33C POST 48437 OR 

GROUP 

33D POST 48437" 

D-57 572021-03-2 R SAMPLE INTERVAL CHANGED FROM: "10600 FC OR 

33200 

FH", TO: "10200 FC OR 30300 FH"

D-57 572021-04-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-57 572021-04-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F POST 43271 OR 

A330-300 POST 43271" 

D-57 572022-01-4 D TASK DELETED 

D-57 572022-01-5 D TASK DELETED 

D-57 572022-01-6 D TASK DELETED 

D-57 572022-01-7 D TASK DELETED 

D-57 572022-01-8 D TASK DELETED 

D-57 572022-01-9 D TASK DELETED 

D-57 572023-02-3 R SAMPLE INTERVAL CHANGED FROM: "4000 FC OR 16000 

FH", TO: "3600 FC OR 16500 FH" 

D-57 572023-02-4 R SAMPLE INTERVAL CHANGED FROM: "4100 FC OR 12800 

FH", TO: "4000 FC OR 12000 FH" 

D-57 572023-02-5 R SAMPLE INTERVAL CHANGED FROM: "3800 FC OR 11900 

FH", TO: "3900 FC OR 11600 FH" 

D-57 572023-02-6 R SAMPLE INTERVAL CHANGED FROM: "3600 FC OR 11200 

FH", TO: "3700 FC OR 11000 FH" 

D-57 572027-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 21600 

FH", TO: "6500 FC OR 19200 FH" 

D-57 572027-01-5 R SAMPLE INTERVAL CHANGED FROM: "7400 FC OR 29700 

FH", TO: "6200 FC OR 28300 FH" 

D-57 572027-01-6 R SAMPLE INTERVAL CHANGED FROM: "11100 FC OR 

34800 

FH", TO: "8600 FC OR 25600 FH" 

D-57 572030-01-4 D TASK DELETED 

D-57 572032-01-

11 

D TASK DELETED 

D-57 572032-01-4 R SAMPLE INTERVAL CHANGED FROM: "13400 FC OR 

48500 

FH", TO: "11800 FC OR 53700 FH" 

D-57 572032-01-6 N NEW TASK ADDED 

D-57 572032-01-7 R SAMPLE INTERVAL CHANGED FROM: "10800 FC OR 

29700 

FH", TO: "10000 FC OR 28500 FH"

D-57 572033-01-4 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 28100 

FH", TO: "6600 FC OR 30100 FH" 

D-57 572033-01-5 R SAMPLE INTERVAL CHANGED FROM: "8800 FC OR 27900 

FH", TO: "8600 FC OR 25500 FH" 

D-57 572033-01-6 R SAMPLE INTERVAL CHANGED FROM: "21100 FH", TO: 

"19700 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 44

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572033-01-7 R SAMPLE INTERVAL CHANGED FROM: "19200 FH", TO: 

"17800 FH" 

D-57 572036-01-4 D TASK DELETED 

D-57 572036-01-5 R SAMPLE INTERVAL CHANGED FROM: "8200 FC OR 26100 

FH", TO: "12700 FC OR 37700 FH" 

D-57 572039-01-4 R SAMPLE INTERVAL CHANGED FROM: "16900 FC OR 

60800 

FH", TO: "14600 FC OR 66500 FH"

D-57 572039-01-5 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

50900 

FH", TO: "16400 FC OR 48900 FH"

D-57 572039-01-6 R SAMPLE INTERVAL CHANGED FROM: "16100 FC OR 

50000 

FH", TO: "16300 FC OR 48500 FH"

D-57 572039-01-7 R SAMPLE INTERVAL CHANGED FROM: "14600 FC OR 

46200 

FH", TO: "14800 FC OR 44000 FH" 

D-57 572040-01-4 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"91100 FH" 

SAMPLE INTERVAL CHANGED FROM: "15900 FC OR 

50000 

FH", TO: "13500 FC OR 61500 FH"

D-57 572040-01-5 R SAMPLE INTERVAL CHANGED FROM: "11100 FC OR 

35300 

FH", TO: "11000 FC OR 32900 FH"

D-57 572040-01-6 R SAMPLE INTERVAL CHANGED FROM: "16200 FC OR 

50000 

FH", TO: "16100 FC OR 47800 FH" 

D-57 572040-01-7 R SAMPLE INTERVAL CHANGED FROM: "15200 FC OR 

50000 

FH", TO: "15100 FC OR 44900 FH" 

D-57 572043-01-

11 

R SAMPLE INTERVAL CHANGED FROM: "50800 FH", TO: 

"50000 FH" 

D-57 572043-01-4 R SAMPLE INTERVAL CHANGED FROM: "11600 FC OR 

41700 

FH", TO: "10300 FC OR 47600 FH"

D-57 572043-01-5 R SAMPLE INTERVAL CHANGED FROM: "6200 FC OR 20000 

FH", TO: "5800 FC OR 18500 FH" 

D-57 572043-01-6 R SAMPLE INTERVAL CHANGED FROM: "10800 FC OR 

34700 

FH", TO: "11100 FC OR 35600 FH" 

D-57 572043-01-7 R SAMPLE INTERVAL CHANGED FROM: "9100 FC OR 29300 

FH", TO: "9400 FC OR 30000 FH" 

D-57 572046-01-4 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 21900 

FH", TO: "5400 FC OR 24900 FH" 

D-57 572046-01-8 R SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "8000 FC OR 25100 FH"

D-57 572046-01-9 R SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "6900 FC OR 40600 FH"

D-57 572047-01-4 D TASK DELETED 

D-57 572047-01-7 R SAMPLE INTERVAL CHANGED FROM: "37700 FH", TO: 

"37300 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 45

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572047-01-8 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"100500 FH" 

SAMPLE INTERVAL CHANGED FROM: "50000 FH", TO: 

"60900 FH" 

D-57 572047-01-9 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"118200 FH" 

SAMPLE INTERVAL CHANGED FROM: "50000 FH", TO: 

"60900 FH" 

D-57 572048-01-1 N NEW TASK ADDED 

D-57 572048-01-2 N NEW TASK ADDED 

D-57 572048-01-3 N NEW TASK ADDED 

D-57 572048-01-4 N NEW TASK ADDED 

D-57 572049-01-4 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"92100 FH" 

SAMPLE INTERVAL CHANGED FROM: "17400 FC OR 

50000 

FH", TO: "15500 FC OR 71400 FH"

D-57 572049-01-5 R SAMPLE INTERVAL CHANGED FROM: "9300 FC OR 30000 

FH", TO: "8700 FC OR 27800 FH" 

D-57 572049-01-6 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"63900 FH" 

SAMPLE INTERVAL CHANGED FROM: "16300 FC OR 

50000 

FH", TO: "16700 FC OR 53400 FH" 

D-57 572049-01-7 R SAMPLE INTERVAL CHANGED FROM: "13700 FC OR 

43900 

FH", TO: "14100 FC OR 45000 FH"

D-57 572050-01-6 R SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 22600 

FH", TO: "7200 FC OR 23200 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33B", TO: 

"GROUP 33B PRE 48437" 

D-57 572051-01-6 R SAMPLE INTERVAL CHANGED FROM: "5600 FC OR 18000 

FH", TO: "5200 FC OR 16600 FH" 

D-57 572052-03-4 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 24000 

FH", TO: "7700 FC OR 24600 FH" 

D-57 572052-03-6 R SAMPLE INTERVAL CHANGED FROM: "7900 FC OR 22000 

FH", TO: "9200 FC OR 28700 FH" 

D-57 572054-01-6 D TASK DELETED 

D-57 572063-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "7300 FC OR 43000 FH" 

IN APPLICABILITY: "GROUP 33D POST 48437" REMOVED 

D-57 572063-01-

11 

N NEW TASK ADDED 

D-57 572063-01-5 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 25800 

FH", TO: "5500 FC OR 25600 FH" 

D-57 572063-01-6 R SAMPLE INTERVAL CHANGED FROM: "7300 FC OR 23300 

FH", TO: "6600 FC OR 21300 FH" 

D-57 572063-01-7 R SAMPLE INTERVAL CHANGED FROM: "6200 FC OR 20000 

FH", TO: "6100 FC OR 19700 FH" 

D-57 572063-01-8 R SAMPLE INTERVAL CHANGED FROM: "5800 FC OR 18600 

FH", TO: "5700 FC OR 18400 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 46

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572064-01-

10 

R DESCRIPTION CHANGED FROM: "10.", TO: "10,INCLUDING

TOP AND BOTTOM FLANGES" 

SAMPLE INTERVAL CHANGED FROM:"8300 FC 0R 48700 

FH"TO: "7300 FC OR 43000 FH 

D-57 572064-01-5 R DESCRIPTION CHANGED FROM: "10.", TO: "10, 

INCLUDING TOP AND BOTTOM FLANGES" 

SAMPLE INTERVAL CHANGED FROM: "8300 FC OR 29800 

FH", TO: "6900 FC OR 31700 FH" 

D-57 572064-01-7 R DESCRIPTION CHANGED FROM: "10.", TO: "10, 

INCLUDING TOP AND BOTTOM FLANGES." 

SAMPLE INTERVAL CHANGED FROM: "6700 FC OR 21500 

FH", TO: "8500 FC OR 26000 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C POST 48437" 

D-57 572064-01-8 R DESCRIPTION CHANGED FROM: "10.", TO: "10, 

INCLUDING TOP AND BOTTOM FLANGES." 

SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "10000 FC OR 31300 FH" 

D-57 572064-01-9 R DESCRIPTION CHANGED FROM: "10.", TO: "10, 

INCLUDING TOP AND BOTTOM FLANGES." 

SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "8600 FC OR 43400 FH"

D-57 572064-02-2 R DESCRIPTION CHANGED FROM: "10.", TO: "10, 

INCLUDING TOP AND BOTTOM FLANGES" 

D-57 572065-01-4 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

51300 

FH", TO: "14600 FC OR 46800 FH" 

D-57 572065-01-7 R IN APPLICABILITY: "GROUP 32F" ADDED 

D-57 572066-01-5 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

51300 

FH", TO: "14600 FC OR 46800 FH"

D-57 572067-01-5 R SAMPLE INTERVAL CHANGED FROM: "12500 FC OR 

39400 

FH", TO: "8100 FC OR 23000 FH" 

D-57 572067-01-6 D TASK DELETED 

D-57 572068-01-6 D TASK DELETED 

D-57 572069-01-

11 

R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"62800 FH" 

SAMPLE INTERVAL CHANGED FROM: "18600 FC OR 

50000 

FH", TO: "17100 FC OR 53700 FH" 

IN APPLICABILITY: "GROUP 33C POST 48437" ADDED 

D-57 572069-01-

12 

R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"117900 FH" 

SAMPLE INTERVAL CHANGED FROM: "50000 FH", TO: 

"86700 FH" 

D-57 572069-01-

13 

N NEW TASK ADDED 

D-57 572069-01-4 R IN APPLICABILITY: "GROUP 33C" REMOVED 

D-57 572069-01-5 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 24600 

FH", TO: "6700 FC OR 19000 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 47

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572069-01-6 R SAMPLE INTERVAL CHANGED FROM: "7100 FC OR 22500 

FH", TO: "6100 FC OR 17400 FH" 

D-57 572073-01-5 R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 21900 

FH", TO: "6400 FC OR 18200 FH" 

D-57 572081-01-

10 

D TASK DELETED 

D-57 572081-01-5 D TASK DELETED 

D-57 572082-01-

10 

R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"99800 FH" 

SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "23400 FC OR 137500 FH"

D-57 572082-01-5 D TASK DELETED 

D-57 572082-01-6 R SAMPLE INTERVAL CHANGED FROM: "9200 FC OR 29500 

FH", TO: "8400 FC OR 26900 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33A", TO: 

"GROUP 33A POST 40366 POST 42275" 

D-57 572082-01-7 R SAMPLE INTERVAL CHANGED FROM: "9200 FC OR 29500 

FH", TO: "8400 FC OR 26900 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33B", TO: 

"GROUP 33B POST 42550" 

D-57 572082-01-9 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"53200 FH" 

SAMPLE INTERVAL CHANGED FROM: "17000 FC OR 

50000 

FH", TO: "27200 FC OR 85200 FH"

D-57 572090-01-1 R SAMPLE INTERVAL CHANGED FROM: "6000 FC OR 24100 

FH", TO: "5200 FC OR 23600 FH" 

D-57 572090-01-3 R SAMPLE INTERVAL CHANGED FROM: "5900 FC OR 18500 

FH", TO: "5700 FC OR 16800 FH" 

D-57 572090-01-4 R SAMPLE INTERVAL CHANGED FROM: "5600 FC OR 17500 

FH", TO: "5400 FC OR 16100 FH" 

D-57 572090-02-1 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"90900 FH" 

SAMPLE INTERVAL CHANGED FROM: "14100 FC OR 

56700 

FH", TO: "12800 FC OR 58200 FH" 

D-57 572090-02-3 R SAMPLE INTERVAL CHANGED FROM: "13800 FC OR 

43200 

FH", TO: "14000 FC OR 41500 FH"

D-57 572090-02-4 R SAMPLE INTERVAL CHANGED FROM: "13100 FC OR 

41000 

FH", TO: "13400 FC OR 39600 FH"

D-57 572093-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "6600 FC OR 20700 

FH", TO: "6100 FC OR 18100 FH" 

D-57 572093-01-

11 

R SAMPLE THRESHOLD CHANGED FROM: "20000 FC", TO: 

"17000 FC" 

D-57 572093-01-

13 

R SAMPLE INTERVAL CHANGED FROM: "8400 FC OR 23500 

FH", TO: "8000 FC OR 22700 FH" 

IN APPLICABILITY: "GROUP 33C POST 48437" ADDED 

D-57 572093-01-

14 

R SAMPLE INTERVAL CHANGED FROM: "30400 FH", TO: 

"30300 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 48

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572093-01-6 R SAMPLE INTERVAL CHANGED FROM: "7100 FC OR 28500 

FH", TO: "5900 FC OR 26800 FH" 

D-57 572093-01-7 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 21300 

FH", TO: "6300 FC OR 18800 FH" 

D-57 572093-01-9 R SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 21900 

FH", TO: "6500 FC OR 19400 FH" 

D-57 572093-02-

10 

R SAMPLE INTERVAL CHANGED FROM: "6600 FC OR 20700 

FH", TO: "6100 FC OR 18100 FH" 

D-57 572093-02-

13 

R SAMPLE INTERVAL CHANGED FROM: "8400 FC OR 23500 

FH", TO: "8000 FC OR 22700 FH" 

IN APPLICABILITY: "GROUP 33C POST 48437" ADDED 

D-57 572093-02-

14 

R SAMPLE INTERVAL CHANGED FROM: "30400 FH", TO: 

"30300 FH" 

D-57 572093-02-6 R SAMPLE INTERVAL CHANGED FROM: "7100 FC OR 28500 

FH", TO: "5900 FC OR 26800 FH" 

D-57 572093-02-7 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 21300 

FH", TO: "6300 FC OR 18800 FH" 

D-57 572093-02-9 R SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 21900 

FH", TO: "6500 FC OR 19400 FH" 

D-57 572094-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 21600 

FH", TO: "6500 FC OR 19200 FH" 

D-57 572094-01-5 R SAMPLE INTERVAL CHANGED FROM: "7400 FC OR 29700 

FH", TO: "6200 FC OR 28300 FH" 

D-57 572094-01-6 R SAMPLE INTERVAL CHANGED FROM: "11100 FC OR 

34800 

FH", TO: "8600 FC OR 25600 FH"

D-57 572095-01-

10 

R IN DESCRIPTION: "SKIN" ADDED 

D-57 572095-01-

11 

R IN DESCRIPTION: "SKIN" ADDED 

D-57 572095-01-

12 

R IN DESCRIPTION: "SKIN" ADDED 

D-57 572095-01-5 R IN DESCRIPTION: "SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7600 FC OR 30500 

FH", TO: "6900 FC OR 31500 FH" 

D-57 572095-01-6 R IN DESCRIPTION: "SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22500 

FH", TO: "7300 FC OR 21700 FH" 

D-57 572095-01-7 R IN DESCRIPTION: "SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7300 FC OR 22800 

FH", TO: "7500 FC OR 22100 FH" 

D-57 572095-01-8 R IN DESCRIPTION: "SKIN" ADDED 

SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 21900 

FH", TO: "7100 FC OR 21100 FH" 

D-57 572095-01-9 R IN DESCRIPTION: "SKIN" ADDED 

D-57 572101-01-

12 

N NEW TASK ADDED 

D-57 572101-01-4 R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 27700 

FH", TO: "5600 FC OR 25500 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 49

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572101-01-6 R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 21600 

FH", TO: "6300 FC OR 18800 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C PRE 48437" 

D-57 572101-01-7 R SAMPLE INTERVAL CHANGED FROM: "6300 FC OR 18800 

FH", TO: "5500 FC OR 16300 FH" 

D-57 572104-01-

12 

N NEW TASK ADDED 

D-57 572104-01-4 R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 27700 

FH", TO: "5600 FC OR 25500 FH" 

D-57 572104-01-5 R SAMPLE INTERVAL CHANGED FROM: "7900 FC OR 24700 

FH", TO: "6800 FC OR 20200 FH" 

D-57 572104-01-6 R SAMPLE INTERVAL CHANGED FROM: "6900 FC OR 21600 

FH", TO: "6300 FC OR 18800 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C PRE 48437" 

D-57 572104-01-7 R SAMPLE INTERVAL CHANGED FROM: "6300 FC OR 18800 

FH", TO: "5500 FC OR 16300 FH" 

D-57 572108-02-4 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 28900 

FH", TO: "6600 FC OR 30000 FH" 

D-57 572108-02-6 R SAMPLE INTERVAL CHANGED FROM: "7000 FC OR 21900 

FH", TO: "7100 FC OR 21100 FH" 

D-57 572108-02-7 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 21300 

FH", TO: "6900 FC OR 26000 FH" 

D-57 572109-02-5 R SAMPLE INTERVAL CHANGED FROM: "11300 FC OR 

35400 

FH", TO: "10200 FC OR 30300 FH" 

D-57 572110-01-4 R SAMPLE INTERVAL CHANGED FROM: "11800 FC OR 

47400 

FH", TO: "9400 FC OR 43000 FH"

D-57 572110-01-5 D TASK DELETED 

D-57 572110-01-6 R SAMPLE INTERVAL CHANGED FROM: "11900 FC OR 

37300 

FH", TO: "10600 FC OR 31500 FH" 

D-57 572110-01-7 R SAMPLE INTERVAL CHANGED FROM: "11000 FC OR 

34500 

FH", TO: "9800 FC OR 29100 FH"

D-57 572111-01-4 D TASK DELETED 

D-57 572111-01-5 D TASK DELETED 

D-57 572111-01-6 R SAMPLE INTERVAL CHANGED FROM: "10300 FC OR 

32300 

FH", TO: "9200 FC OR 27400 FH"

D-57 572111-01-7 D TASK DELETED 

D-57 572116-02-2 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 23500 

FH", TO: "7200 FC OR 21400 FH" 

D-57 572117-01-5 R SAMPLE INTERVAL CHANGED FROM: "8700 FC OR 27200 

FH", TO: "8400 FC OR 25000 FH" 

D-57 572119-02-9 N NEW TASK ADDED 

D-57 572121-01-

12 

N NEW TASK ADDED 

D-57 572121-01-4 D TASK DELETED 

D-57 572121-01-5 D TASK DELETED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 50

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572121-01-6 R SAMPLE INTERVAL CHANGED FROM: "6500 FC OR 15200 

FH", TO: "8300 FC OR 23600 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C POST 48437" 

D-57 572121-01-7 D TASK DELETED 

D-57 572122-01-4 D TASK DELETED 

D-57 572122-01-5 D TASK DELETED 

D-57 572122-01-6 R SAMPLE INTERVAL CHANGED FROM: "6000 FC OR 18800 

FH", TO: "5300 FC OR 15800 FH" 

D-57 572122-01-7 D TASK DELETED 

D-57 572125-01-6 R SAMPLE INTERVAL CHANGED FROM: "12600 FC OR 

50000 

FH", TO: "9900 FC OR 45200 FH" 

D-57 572125-01-7 R SAMPLE INTERVAL CHANGED FROM: "14700 FC OR 

46100 

FH", TO: "13000 FC OR 38500 FH"

D-57 572125-01-8 R SAMPLE INTERVAL CHANGED FROM: "12700 FC OR 

39800 

FH", TO: "11200 FC OR 33200 FH"

D-57 572125-01-9 R SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

36000 

FH", TO: "10200 FC OR 30100 FH"

D-57 572125-02-4 R SAMPLE INTERVAL CHANGED FROM: "12600 FC OR 

50000 

FH", TO: "9900 FC OR 45200 FH" 

D-57 572125-02-5 R SAMPLE INTERVAL CHANGED FROM: "14700 FC OR 

46100 

FH", TO: "13000 FC OR 38500 FH"

D-57 572125-02-6 R SAMPLE INTERVAL CHANGED FROM: "12700 FC OR 

39800 

FH", TO: "11200 FC OR 33200 FH"

D-57 572125-02-7 R SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

36000 

FH", TO: "10200 FC OR 30100 FH"

D-57 572129-01-3 D TASK DELETED 

D-57 572129-02-3 D TASK DELETED 

D-57 572130-01-3 D TASK DELETED 

D-57 572130-02-3 D TASK DELETED 

D-57 572131-01-4 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"91700 FH" 

SAMPLE INTERVAL CHANGED FROM: "16400 FC OR 

50000 

FH", TO: "13600 FC OR 62400 FH"

D-57 572131-01-5 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

50000 

FH", TO: "16400 FC OR 48900 FH"

D-57 572131-01-6 R SAMPLE INTERVAL CHANGED FROM: "16300 FC OR 

50000 

FH", TO: "15800 FC OR 47100 FH"

D-57 572131-01-7 R SAMPLE INTERVAL CHANGED FROM: "15500 FC OR 

49100 

FH", TO: "15000 FC OR 44600 FH" 

D-57 572133-01-4 R SAMPLE INTERVAL CHANGED FROM: "6400 FC OR 27100 

FH", TO: "5800 FC OR 26300 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 51

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572133-01-5 R SAMPLE INTERVAL CHANGED FROM: "28400 FH", TO: 

"26600 FH" 

D-57 572133-01-7 R SAMPLE INTERVAL CHANGED FROM: "19800 FH", TO: 

"18500 FH" 

D-57 572134-02-

10 

N NEW TASK ADDED 

D-57 572138-01-

10 

N NEW TASK ADDED 

D-57 572138-01-4 R APPLICABILITY CHANGED FROM: "GROUP 32A OR 

GROUP 

33C OR GROUP 33D", TO: "GROUP 32A POST48437 OR 

GROUP 33C POST48437 OR GROUP 33D POST48437" 

D-57 572138-01-7 N NEW TASK ADDED 

D-57 572138-01-9 N NEW TASK ADDED 

D-57 572139-01-

10 

N NEW TASK ADDED 

D-57 572139-01-4 R APPLICABILITY CHANGED FROM: "GROUP 32A OR 

GROUP 

33C OR GROUP 33D POST 48437", TO: "GROUP 32A 

POST48437 OR GROUP 33C POST48437 OR GROUP 33D 

POST48437"

D-57 572139-01-9 N NEW TASK ADDED 

D-57 572140-01-4 R SAMPLE INTERVAL CHANGED FROM: "10400 FC OR 

37700 

FH", TO: "8700 FC OR 39600 FH"

D-57 572140-01-5 R SAMPLE INTERVAL CHANGED FROM: "9100 FC OR 28800 

FH", TO: "8900 FC OR 26400 FH" 

D-57 572141-01-4 R SAMPLE INTERVAL CHANGED FROM: "12800 FC OR 

46300 

FH", TO: "10000 FC OR 45300 FH" 

D-57 572141-01-5 R SAMPLE INTERVAL CHANGED FROM: "13200 FC OR 

41900 

FH", TO: "12600 FC OR 37600 FH" 

D-57 572141-01-8 R SAMPLE INTERVAL CHANGED FROM: "12000 FC OR 

38300 

FH", TO: "11000 FC OR 32600 FH"

D-57 572144-01-

10 

N NEW TASK ADDED 

D-57 572144-01-4 R APPLICABILITY CHANGED FROM: "GROUP 32A OR 

GROUP 

33C OR GROUP 33D POST 48437", TO: "GROUP 32A 

POST48437 OR GROUP 33C POST48437 OR GROUP 33D 

POST48437" 

D-57 572144-01-9 N NEW TASK ADDED 

D-57 572148-01-4 R SAMPLE INTERVAL CHANGED FROM: "12600 FC OR 

50000 

FH", TO: "9900 FC OR 45200 FH"

D-57 572148-01-5 R SAMPLE INTERVAL CHANGED FROM: "14700 FC OR 

46100 

FH", TO: "13000 FC OR 38500 FH" 

D-57 572148-01-6 R SAMPLE INTERVAL CHANGED FROM: "12700 FC OR 

39800 

FH", TO: "11200 FC OR 33300 FH" 

D-57 572148-01-7 R SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

36000 

FH", TO: "10200 FC OR 30100 FH"
 A330 MRB REPORT

Issue : July 2010 SOC Page : 52

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572149-01-

12 

N NEW TASK ADDED 

D-57 572153-01-

12 

R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"118100 FH" 

SAMPLE INTERVAL CHANGED FROM: "50000 FH", TO: 

"50800 FH" 

D-57 572153-01-4 R SAMPLE INTERVAL CHANGED FROM: "11600 FC OR 

41700 

FH", TO: "10300 FC OR 47600 FH" 

D-57 572153-01-5 R SAMPLE INTERVAL CHANGED FROM: "6200 FC OR 20000 

FH", TO: "5800 FC OR 18500 FH" 

D-57 572153-01-6 R SAMPLE INTERVAL CHANGED FROM: "10800 FC OR 

34700 

FH", TO: "11100 FC OR 35600 FH"

D-57 572153-01-8 R SAMPLE INTERVAL CHANGED FROM: "9100 FC OR 29300 

FH", TO: "9400 FC OR 30000 FH" 

D-57 572154-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "10300 FC OR 

33100 

FH", TO: "9700 FC OR 31200 FH"

D-57 572154-01-

12 

N NEW TASK ADDED 

D-57 572154-01-4 R SAMPLE INTERVAL CHANGED FROM: "11400 FC OR 

41300 

FH", TO: "9400 FC OR 43300 FH" 

D-57 572154-01-5 R SAMPLE INTERVAL CHANGED FROM: "8400 FC OR 26800 

FH", TO: "7800 FC OR 24900 FH" 

D-57 572154-01-6 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"62700 FH" 

SAMPLE INTERVAL CHANGED FROM: "10900 FC OR 

34900 

FH", TO: "17200 FC OR 54000 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C POST 48437 OR GROUP 33D POST 48437" 

D-57 572158-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "5900 FC OR 18500 

FH", TO: "5500 FC OR 16500 FH" 

D-57 572158-01-5 R SAMPLE INTERVAL CHANGED FROM: "6300 FC OR 25300 

FH", TO: "5300 FC OR 24300 FH" 

D-57 572158-01-6 R SAMPLE INTERVAL CHANGED FROM: "7400 FC OR 23200 

FH", TO: "6900 FC OR 20500 FH" 

D-57 572159-01-4 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 27300 

FH", TO: "5700 FC OR 26100 FH" 

D-57 572159-01-5 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 23500 

FH", TO: "8100 FC OR 23900 FH" 

D-57 572159-01-9 R SAMPLE INTERVAL CHANGED FROM: "6300 FC OR 19700 

FH", TO: "6000 FC OR 17700 FH" 

D-57 572162-01-5 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

51300 

FH", TO: "14600 FC OR 46800 FH"

D-57 572162-01-8 R IN APPLICABILITY: "GROUP 32F" ADDED 

D-57 572164-01-

11 

R SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "7500 FC OR 44300 FH" 

IN APPLICABILITY: "GROUP 33D POST 48437" REMOVED

D-57 572164-01- N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 53

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

12 

D-57 572164-01-5 R SAMPLE INTERVAL CHANGED FROM: "8800 FC OR 31800 

FH", TO: "7500 FC OR 34900 FH" 

D-57 572164-01-6 R SAMPLE INTERVAL CHANGED FROM: "7600 FC OR 24500 

FH", TO: "6900 FC OR 22300 FH" 

D-57 572164-01-7 R SAMPLE INTERVAL CHANGED FROM: "8400 FC OR 26900 

FH", TO: "8300 FC OR 26500 FH" 

D-57 572164-01-9 R SAMPLE INTERVAL CHANGED FROM: "8200 FC OR 26300 

FH", TO: "8100 FC OR 25900 FH" 

D-57 572165-01-

11 

N NEW TASK ADDED 

D-57 572166-01-5 R SAMPLE INTERVAL CHANGED FROM: "16000 FC OR 

50000 

FH", TO: "14600 FC OR 46800 FH"

D-57 572174-01-7 N NEW TASK ADDED 

D-57 572180-01-

11 

D TASK DELETED 

D-57 572180-01-4 D TASK DELETED 

D-57 572180-01-5 D TASK DELETED 

D-57 572180-01-6 R SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

36000 

FH", TO: "10300 FC OR 30600 FH"

D-57 572180-01-7 R SAMPLE INTERVAL CHANGED FROM: "8900 FC OR 24900 

FH", TO: "8400 FC OR 24000 FH" 

D-57 572181-01-4 D TASK DELETED 

D-57 572181-01-5 D TASK DELETED 

D-57 572181-01-6 R SAMPLE INTERVAL CHANGED FROM: "11500 FC OR 

36000 

FH", TO: "10300 FC OR 30600 FH" 

D-57 572181-01-7 D TASK DELETED 

D-57 572184-01-4 D TASK DELETED 

D-57 572184-01-5 D TASK DELETED 

D-57 572184-01-6 R SAMPLE INTERVAL CHANGED FROM: "6400 FC OR 20000 

FH", TO: "5600 FC OR 16600 FH" 

D-57 572184-01-7 D TASK DELETED 

D-57 572184-02-4 D TASK DELETED 

D-57 572184-02-5 D TASK DELETED 

D-57 572184-02-6 R SAMPLE INTERVAL CHANGED FROM: "6400 FC OR 20000 

FH", TO: "5600 FC OR 16600 FH" 

D-57 572184-02-7 D TASK DELETED 

D-57 572605-01-9 N NEW TASK ADDED 

D-57 572607-01-5 N NEW TASK ADDED 

D-57 572610-01-1 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

D-57 572610-01-2 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F POST 43271 OR 

A330-300 POST 43271" 

D-57 572612-01-2 R APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 54

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 572612-01-3 R APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-200F POST 43271 OR 

A330-300 POST 43271" 

D-57 572612-02-

11 

R SAMPLE INTERVAL CHANGED FROM: "11800 FC OR 

36900 

FH", TO: "11300 FC OR 35500 FH"

D-57 572612-02-

15 

R SAMPLE INTERVAL CHANGED FROM: "12800 FC OR 

35600 

FH", TO: "12300 FC OR 34300 FH"

D-57 572612-02-

17 

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

"9700 FC" 

D-57 572612-02-9 R SAMPLE INTERVAL CHANGED FROM: "10100 FC", TO: 

"9700 FC" 

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

D-57 573001-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 19300 

FH", TO: "5700 FC OR 18300 FH" 

D-57 573001-01-5 R SAMPLE INTERVAL CHANGED FROM: "6500 FC OR 23400 

FH", TO: "5300 FC OR 24400 FH" 

D-57 573001-01-7 R SAMPLE INTERVAL CHANGED FROM: "5900 FC OR 18700 

FH", TO: "5600 FC OR 18000 FH" 

D-57 573001-01-8 R SAMPLE INTERVAL CHANGED FROM: "6200 FC OR 19700 

FH", TO: "5800 FC OR 18700 FH" 

D-57 573002-01-5 R SAMPLE INTERVAL CHANGED FROM: "6500 FC OR 23400 

FH", TO: "5300 FC OR 24400 FH" 

D-57 573002-01-7 R SAMPLE INTERVAL CHANGED FROM: "5900 FC OR 18700 

FH", TO: "5600 FC OR 18000 FH" 

D-57 573002-01-8 R SAMPLE INTERVAL CHANGED FROM: "6200 FC OR 19700 

FH", TO: "5800 FC OR 18700 FH" 

D-57 573002-01-9 R SAMPLE INTERVAL CHANGED FROM: "6100 FC OR 19300 

FH", TO: "5700 FC OR 18300 FH" 

D-57 573003-02-

10 

R SAMPLE INTERVAL CHANGED FROM: "5500 FC OR 17300 

FH", TO: "5100 FC OR 16500 FH" 

D-57 573003-02-

11 

N NEW TASK ADDED 

D-57 573003-02-4 R SAMPLE INTERVAL CHANGED FROM: "5800 FC OR 21000 

FH", TO: "4700 FC OR 21900 FH" 

D-57 573003-02-5 R SAMPLE INTERVAL CHANGED FROM: "7200 FC OR 22900 

FH", TO: "6800 FC OR 21800 FH" 

D-57 573003-02-6 R SAMPLE INTERVAL CHANGED FROM: "5600 FC OR 17700 

FH", TO: "8200 FC OR 25800 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C POST 48437" 

D-57 573003-02-7 R SAMPLE INTERVAL CHANGED FROM: "8200 FC OR 25800 

FH", TO: "17000 FC OR 50000 FH" 

D-57 573003-02-8 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"99800 FH" 

SAMPLE INTERVAL CHANGED FROM: "7100 FC OR 41600 

FH", TO: "14900 FC OR 87500 FH" 

D-57 573004-01-4 N NEW TASK ADDED 

D-57 574103-02-9 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 55

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 574105-01-

12 

N NEW TASK ADDED 

D-57 574107-02-4 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"92400 FH" 

SAMPLE INTERVAL CHANGED FROM: "16200 FC OR 

50000 

FH", TO: "14100 FC OR 65200 FH" 

D-57 574107-02-5 R SAMPLE INTERVAL CHANGED FROM: "13500 FC OR 

42600 

FH", TO: "12500 FC OR 40000 FH" 

D-57 574110-02-9 N NEW TASK ADDED 

D-57 574114-03-1 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"114600 FH" 

SAMPLE INTERVAL CHANGED FROM: "15300 FC OR 

50000 

FH", TO: "12400 FC OR 56600 FH" 

D-57 574114-03-2 R SAMPLE INTERVAL CHANGED FROM: "6000 FC OR 18800 

FH", TO: "5500 FC OR 16400 FH" 

D-57 574114-03-3 R SAMPLE INTERVAL CHANGED FROM: "15200 FC OR 

47600 

FH", TO: "13900 FC OR 41000 FH"

D-57 574114-03-4 R SAMPLE INTERVAL CHANGED FROM: "13900 FC OR 

43600 

FH", TO: "12700 FC OR 37500 FH"

D-57 574116-01-

12 

N NEW TASK ADDED 

D-57 574301-01-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574303-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574304-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574304-03-2", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574304-03-2." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574304-03-2 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH 

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME 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 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 "REMOVAL OF THE BOLTS 

SUCCESSIVELY." REMOVED 

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

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

D-57 574401-01-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 56

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 574403-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574404-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574404-03-2", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574404-03-2." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574404-03-2 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH 

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

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

TASK MAY BE PERFORMED AT THE 

SAME TIME AS TASK 574404-01-1." 

D-57 574406-01-1 R DESCRIPTION CHANGED FROM: "EDGE,", TO: "EDGE" 

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

D-57 574501-02-4 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574503-01-1 R DESCRIPTION CHANGED FROM: "TO 8 ATTACHMENTS,", 

TO: 

"& 8 ATTACHMENTS" 

D-57 574503-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574504-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574504-02-3", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574504-02-3." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

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

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

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

TASK MAY BE PERFORMED AT THE 

SAME TIME AS TASK 574504-01-1."

D-57 574504-02-4 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH", TO:

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

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

D-57 574507-01-1 N NEW TASK ADDED 

D-57 574508-01-1 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH." 

D-57 574601-01-3 R DESCRIPTION CHANGED FROM: ";", TO: "," 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574601-02-1 R DESCRIPTION CHANGED FROM: ";", TO: "," 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 57

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 574603-01-2 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 574603-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574604-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574604-02-1", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574604-02-1." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

D-57 574604-02-1 R DESCRIPTION CHANGED FROM: "STATIONS, INTERNAL 

AND 

EXTERNAL, LH/RH. NOTE: THIS TASK MUST BE 

PERFORMED 

AT THE SAME TIME AS TASK 574604-01-1", TO: 

"STATIONS,EXTERNAL, LH/RH. NOTE: 

THIS TASK MAY BE PERFORMED AT THE SAME TIME AS 

TASK 574604-01-1."

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

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

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

OF ROLLER CONTACT AREA, LH/RH." 

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

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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 574703-02-3 R DESCRIPTION CHANGED FROM: "LH/RH", TO: "LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574704-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574704-03-1", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574704-03-1." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 58

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 574704-03-1 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH 

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

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

TASK MAY BE PERFORMED AT THE 

SAME TIME AS TASK 574704-01-1." 

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

D-57 574801-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

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

INCLUDING 

TRACK RIB LUGS, TRACK", TO: "ATTACHMENTS 

INCLUDING 

TRACK RIB LUGS,TRACK" 

D-57 574803-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574804-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574804-03-2", TO: "MAY BE 

PERFORMED AT THE SAME TIME AS TASK 574804-03-2." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574804-03-2 R DESCRIPTION CHANGED FROM: "EXTERNAL, LH/RH 

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

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

TASK MAY BE PERFORMED AT THE 

SAME TIME AS TASK 574804-01-1."

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

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

D-57 574901-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574903-01-1 R DESCRIPTION CHANGED FROM: "ATTACHMENTS,", TO: 

"ATTACHMENTS" 

D-57 574903-02-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 574904-01-1 R DESCRIPTION CHANGED FROM: "MUST BE PERFORMED 

AT 

THE SAME TIME AS TASK 574904-02-1", TO: "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: "EXTERNAL, LH/RH 

NOTE: 

THIS TASK MUST BE PERFORMED AT THE SAME TIME AS

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

TASK MAY BE PERFORMED AT THE 

SAME TIME AS TASK 574904-01-1." 

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

"EXTERNAL,LH/RH." 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 59

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

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

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

D-57 575001-01-7 N NEW TASK ADDED 

D-57 575004-01-7 N NEW TASK ADDED 

D-57 575010-01-

12 

N NEW TASK ADDED 

D-57 575011-01-

11 

R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"59500 FH" 

SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "19000 FC OR 56600 FH" 

D-57 575011-01-4 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"90700 FH" 

SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "17300 FC OR 78500 FH"

D-57 575011-01-6 R SAMPLE THRESHOLD CHANGED FROM: "50000 FH", TO: 

"59300 FH" 

SAMPLE INTERVAL CHANGED FROM: "20000 FC OR 

50000 

FH", TO: "19400 FC OR 57600 FH" 

D-57 575012-01-

10 

R SAMPLE INTERVAL CHANGED FROM: "8500 FC OR 23700 

FH", TO: "8000 FC OR 22900 FH" 

IN APPLICABILITY: "GROUP 33C POST 48437" ADDED 

D-57 575012-01-6 R APPLICABILITY CHANGED FROM: "GROUP 33C", TO: 

"GROUP 33C PRE 48437" 

D-57 575016-01-4 R SAMPLE INTERVAL CHANGED FROM: "9100 FC OR 36800 

FH", TO: "8300 FC OR 37700 FH" 

D-57 575016-01-6 R SAMPLE INTERVAL CHANGED FROM: "7800 FC OR 24700 

FH", TO: "8000 FC OR 23700 FH" 

D-57 575016-01-8 R SAMPLE INTERVAL CHANGED FROM: "7400 FC OR 23500 

FH", TO: "7600 FC OR 22500 FH" 

D-57 575017-01-4 R SAMPLE INTERVAL CHANGED FROM: "5500 FC OR 22200 

FH", TO: "5000 FC OR 22800 FH" 

D-57 575017-01-6 R SAMPLE INTERVAL CHANGED FROM: "5400 FC OR 17100 

FH", TO: "5500 FC OR 16300 FH" 

D-57 575017-01-7 R SAMPLE INTERVAL CHANGED FROM: "5100 FC OR 16200 

FH", TO: "5200 FC OR 15500 FH" 

D-57 575018-01-4 D TASK DELETED 

D-57 575019-01-1 R DESCRIPTION CHANGED FROM: "DETAILED", TO: 

"GENERAL 

VISUAL" 

D-57 575022-01-3 D TASK DELETED 

D-57 575022-01-5 D TASK DELETED 

D-57 575023-01-7 R SAMPLE THRESHOLD: "OR 50000 FH" ADDED 

SAMPLE INTERVAL: "OR 42800 FH" ADDED 

D-57 575023-01-8 N NEW TASK ADDED 

D-57 575025-01-4 R SAMPLE INTERVAL CHANGED FROM: "8100 FC OR 32600 

FH", TO: "7300 FC OR 33300 FH" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 60

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 575025-01-5 R SAMPLE INTERVAL CHANGED FROM: "7300 FC OR 23300 

FH", TO: "6600 FC OR 19700 FH" 

APPLICABILITY CHANGED FROM: "GROUP 33A POST 

42276 

OR GROUP 33A POST 42699 OR GROUP 33A POST 45739 

OR 

GROUP 33B POST 42276 OR GROUP 33B POST 42699 OR

GROUP 33B POST 45739", TO: 

"GROUP 33A OR GROUP 33B"

D-57 575025-01-6 R SAMPLE INTERVAL CHANGED FROM: "8000 FC OR 25100 

FH", TO: "8100 FC OR 24000 FH" 

D-57 575025-01-7 R SAMPLE INTERVAL CHANGED FROM: "8000 FC OR 22900 

FH", TO: "8400 FC OR 23900 FH" 

D-57 575025-01-8 R SAMPLE INTERVAL CHANGED FROM: "6800 FC OR 30600 

FH", TO: "7100 FC OR 32000 FH" 

D-57 575025-01-9 R SAMPLE INTERVAL CHANGED FROM: "7500 FC OR 23700 

FH", TO: "7600 FC OR 22700 FH" 

D-57 575053-01-1 R DESCRIPTION CHANGED FROM: "NO 1,", TO: "NO.1," 

APPLICABILITY CHANGED FROM: "PRE 45326", TO: 

"A330-200 PRE 45326 OR A330-300 PRE 45326" 

D-57 575054-01-1 R DESCRIPTION CHANGED FROM: "NO 1, GEAR BOX 

SUPPORT,", TO: "NO.1. GEAR BOX," 

APPLICABILITY CHANGED FROM: "POST 45326", TO: 

"A330-200 POST 45326 OR A330-200F POST 45326 OR 

A330-300 POST 45326" 

D-57 575055-01-1 R DESCRIPTION CHANGED FROM: "NO 1,", TO: "NO.1," 

D-57 575059-01-1 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 

TRAVELLING 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 TRAVELLING BEAM AT TRACK 

NO.4." 

D-57 575061-01-1 R DESCRIPTION CHANGED FROM: "NO 2,3,4 AND 5, 

CARRIAGE ASSEMBLIES", TO: "NO.2,3,4 AND 5, 

CARRIAGE ASSEMBLIES." 

D-57 575063-01-3 R APPLICABILITY CHANGED FROM: "POST 55652", TO: 

"A330-200 POST 55652 OR A330-200F POST 55652 OR 

A330-300 POST 55652" 

D-57 575065-01-1 R DESCRIPTION CHANGED FROM: "NO 2,3,4 AND 5, 

INTERNAL STRUCTURE", TO: "NO. 2,3,4 AND 5, 

INTERNAL STRUCTURE." 

D-57 575067-01-1 R IN PREPARATION TASKS: "FS BOLT" REMOVED 

DESCRIPTION CHANGED FROM: "NO 2,3,4 AND 5, 

FORWARD 

ATTACHMENT SPIGOTS, EXTERNAL STRUCTURE", TO: 

"NO.2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, 

EXTERNAL STRUCTURE."
 A330 MRB REPORT

Issue : July 2010 SOC Page : 61

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 575067-02-1 R DESCRIPTION CHANGED FROM: "NO 2,3,4 AND 5, 

FORWARD 

ATTACHMENT SPIGOTS, INTERNAL STRUCTURE", TO: 

"NO. 

2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, 

INTERNAL 

STRUCTURE." 

D-57 575069-01-1 R DESCRIPTION CHANGED FROM: "NO 2,3,4 AND 5, AFT 

ATTACHMENT SPIGOTS", TO: "NO.2,3,4 AND 5, AFT 

ATTACHMENT SPIGOTS." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

D-57 575401-01-1 R DESCRIPTION CHANGED FROM: "SKIN", TO: "SKIN." 

D-57 575403-01-1 R DESCRIPTION CHANGED FROM: "NO 1 AND TRUNNION, 

INTERNAL AND EXTERNAL NOTE: TASK MUST BE 

PERFORMED 

AT THE SAME TIME AS TASK 575403-02-1", TO: "NO.1 

AND TRUNNION, INTERNAL AND 

EXTERNAL."

D-57 575403-02-1 R DESCRIPTION CHANGED FROM: "NO 1 AND TRUNNION, 

INTERNAL NOTE: TASK MUST BE PERFORMED AT THE 

SAME 

TIME AS TASK 575403-01-1", TO: "NO.1 AND TRUNNION, 

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: "NO 2 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." 

APPLICABILITY CHANGED FROM: "PRE 49008", TO: 

"A330-200 PRE 49008 OR A330-300 PRE 49008" 

D-57 575405-01-3 R IN ACCESS: "531AT; 531CB; 631AT; 631CB" ADDED AND 

"531SB; 531VT; 631SB; 631VT" REMOVED 

IN PREPARATION TASKS: "SPEED TAPES" REMOVED 

DESCRIPTION CHANGED FROM: "NO 2 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." 

APPLICABILITY CHANGED FROM: "POST 49008", TO: 

"A330-200 POST 49008 OR A330-200F OR A330-300 POST 

49008" 

D-57 575405-02-1 R DESCRIPTION CHANGED FROM: "NO 2", TO: "NO.2." 

APPLICABILITY CHANGED FROM: "PRE 49008", TO: 

"A330-200 PRE 49008 OR A330-300 PRE 49008" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 62

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

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." 

APPLICABILITY CHANGED FROM: "POST 49008", TO: 

"A330-200 POST 49008 OR A330-200F OR A330-300 POST 

49008" 

D-57 575407-01-1 R DESCRIPTION CHANGED FROM: "BRACKET", TO: 

"BRACKET." 

TPS: "TPS MUST NOT BE APPLIED" ADDED 

D-57 575409-01-1 R DESCRIPTION CHANGED FROM: "STRUCTURE", TO: 

"STRUCTURE." 

D-57 575501-01-1 N NEW TASK ADDED 

D-57 575503-01-1 R DESCRIPTION CHANGED FROM: "NO 3, AND EXTERNAL 

DRIVE STRUT ATTACHMENT FITTING, SWING LINK TO 

CARRIAGE WITH ASSOCIATED ATTACH FITTING AND 

GUIDE 

ARM ATTACHMENT FITTING", TO: "NO.3, 

AND EXTERNAL DRIVE STRUT ATTACHMENT FITTING, 

SWING 

LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING

AND GUIDE ARM ATTACHMENT FITTING." 

D-57 575503-02-1 R DESCRIPTION CHANGED FROM: "NO 3", TO: "NO. 3." 

D-57 575505-01-1 R DESCRIPTION CHANGED FROM: "NO 4, AND EXTERNAL 

FWD 

SUPPORT LINK AND AFT SUPPORT LINK ATTACH 

FITTING", 

TO: "NO.4, AND EXTERNAL FWD SUPPORT LINK AND AFT

SUPPORT LINK ATTACH FITTING."

D-57 575505-02-1 R DESCRIPTION CHANGED FROM: "NO", TO: "NO." 

D-57 575507-01-1 R IN ACCESS: "533AT; 533CB; 633AT; 633CB" ADDED AND 

"534AT; 534CB; 634AT; 634CB" REMOVED 

IN PREPARATION TASKS: "SPEED TAPES" REMOVED 

DESCRIPTION CHANGED FROM: "NO 5, AND EXTERNAL 

DRIVE STRUT ATTACH FITTING, SWING LINK TO 

CARRIAGE 

WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM 

ATTACH FITTING", TO: "NO. 5, AND 

EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK 

TO 

CARRIAGE WITH ASSOCIATED ATTACH FITTING AND 

GUIDE 

ARM ATTACH FITTING."

D-57 575507-02-1 R IN ACCESS: "533AT; 533CB; 633AT; 633CB" ADDED AND 

"534AT; 534CB; 634AT; 634CB" REMOVED 

IN PREPARATION TASKS: "SPEED TAPES" ADDED 

DESCRIPTION CHANGED FROM: "NO", TO: "NO." 

D-57 576106-01-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 576106-02-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 576116-01-3 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 63

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGE 

D-57 576116-02-2 R APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

D-57 577001-01-2 R DESCRIPTION CHANGED FROM: "NO1, UPPER AND 

LOWER 

SKIN, EXTERNAL SURFACE.LH/RH", TO: "NO.1, UPPER 

AND LOWER SKIN, EXTERNAL SURFACE,LH/RH." 

D-57 577003-01-1 R DESCRIPTION CHANGED FROM: "NO 1, HINGE AND 

ACTUATOR ATTACHMENT FITTINGS (6 PLACES)", TO: 

"NO. 

1, HINGE AND ACTUATOR ATTACHMENT FITTINGS." 

D-71 711141-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711142-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711341-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711341-02-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711343-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711345-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 711347-02-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 712101-06-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-71 712201-03-1 R DESCRIPTION CHANGED FROM: "MOUNT.", TO: "MOUNT 

LOWER BEAM." 

D-71 712201-04-1 R DESCRIPTION CHANGED FROM: "MOUNT.", TO: "MOUNT 

LOWER BEAM." 

D-71 712201-05-1 R DESCRIPTION CHANGED FROM: "MOUNT.", TO: "MOUNT 

LOWER BEAM." 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-78 783201-01-1 R IN ACCESS: "415AL; 416AR; 425AL; 426AR" ADDED AND 

"415BL; 416BR; 425BL; 426BR" REMOVED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-78 783201-03-2 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

D-78 783202-01-1 R APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

SECTION E

Page E-INTRO-1 1 GENERAL: 2nd to 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 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 64

(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-100-01-2 R IN SSI-REFERENCE(S): "531167-01-1" ADDED 

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-121-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-123-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-125-01-1 N NEW TASK 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 AND "25.51.00/10" REMOVED 

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 N NEW TASK ADDED 

E-100 ZL-131-03-1 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; 25.55.00/03" 

ADDED 

E-100 ZL-137-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-141-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "A330-300", TO: "ALL" 

E-100 ZL-141-01-2 D TASK DELETED 

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-149-05-1 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 PREPARATION TASKS: "LD-MCR-IF INSTALLED" ADDED 

AND "LDMCR" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-151-02-2 R IN PREPARATION TASKS: "LD-MCR-IF INSTALLED" ADDED 

AND "LDMCR" REMOVED 

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-151-02-5 N NEW TASK ADDED 

E-100 ZL-151-03-1 R IN PREPARATION TASKS: "LD-MCR-IF INSTALLED" ADDED 

AND "LDMCR" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 65

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-100 ZL-153-01-1 R IN PREPARATION TASKS: "LDL - LAVATORIES AND 

FURNISHING" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

IN MSI-REFERENCE(S): "25.52.00/05; 25.55.00/03" 

ADDED 

IN APPLICABILITY: "A330-200F" ADDED 

E-100 ZL-153-01-2 R IN PREPARATION TASKS: "LAVATORIES AND FURNISHING 

," REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

IN MSI-REFERENCE(S): "25.52.00/05" ADDED 

E-100 ZL-161-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN DESCRIPTION: "(IF FLIGHT KIT CONTAINER 

INSTALLED, AS FAR AS VISIBLE)" ADDED 

IN MSI-REFERENCE(S): "38.32.00/02" ADDED AND 

"25.54.00/04; 25.54.00/05; 25.54.00/06" REMOVED 

E-100 ZL-161-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-100 ZL-161-02-2 N NEW TASK ADDED 

E-100 ZL-161-03-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-100 ZL-161-03-2 N NEW TASK ADDED 

E-100 ZL-163-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN MSI-REFERENCE(S): "25.52.00/05" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-100 ZL-163-01-2 N UEW TASK ADDED 

E-100 ZL-171-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-100 ZL-171-01-2 N NEW TASK ADDED 

E-100 ZL-171-02-1 R IN ACCESS: "162ZW" ADDED 

IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "535122-01-1" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-100 ZL-171-02-2 N NEW TASK ADDED 

E-100 ZL-191-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-191-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-193-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-193-02-1 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-197-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-100 ZL-197-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-200 ZL-200-01-1 R IN SSI-REFERENCE(S): "532166-01-2; 532167-01-1; 

532175-01-1; 534167-01-1; 534177-01-2" 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 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 66

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-200 ZL-221-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-221-03-1 N NEW TASK ADDED 

E-200 ZL-223-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-223-02-1 N NEW TASK ADDED 

E-200 ZL-231-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-231-03-1 N NEW TASK ADDED 

E-200 ZL-231-04-1 N NEW TASK ADDED 

E-200 ZL-231-05-1 N NEW TASK ADDED 

E-200 ZL-233-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-233-02-1 N NEW TASK ADDED 

E-200 ZL-241-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-241-03-1 N NEW TASK ADDED 

E-200 ZL-241-04-1 N NEW TASK ADDED 

E-200 ZL-241-05-1 N NEW TASK ADDED 

E-200 ZL-243-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-243-02-1 N NEW TASK ADDED 

E-200 ZL-251-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-251-03-1 N NEW TASK ADDED 

E-200 ZL-251-04-1 N NEW TASK ADDED 

E-200 ZL-251-05-1 N NEW TASK ADDED 

E-200 ZL-253-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN MSI-REFERENCE(S): "25.75.00/05" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-253-02-1 N NEW TASK ADDED 

E-200 ZL-261-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-261-03-1 N NEW TASK ADDED 

E-200 ZL-261-04-1 N NEW TASK ADDED 

E-200 ZL-261-05-1 N NEW TASK ADDED 

E-200 ZL-263-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-263-02-1 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 67

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-200 ZL-271-02-1 R IN PREPARATION TASKS: "DOOR FRAME LININGS, 

SIDEWALL AND FLOOR PANELS FROM FR 72 TO FR 80" 

ADDED AND "SIDEWALL AND FLOOR PANELS FROM FR 72 

TO 

FR 80" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "535121-01-1" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-271-03-1 N NEW TASK ADDED 

E-200 ZL-271-04-1 N NEW TASK ADDED 

E-200 ZL-271-05-1 N NEW TASK ADDED 

E-200 ZL-273-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "535121-01-1" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-200 ZL-273-02-1 N NEW TASK ADDED 

E-300 ZL-300-01-1 R IN SSI-REFERENCE(S): "552001-01-2; 554001-01-2; 

554014-01-1; 554020-01-1; 554029-01-1" ADDED 

E-300 ZL-311-01-1 R TASK TITLE CHANGED FROM: "SECTION", TO: "SECTIO 

(EWIS)" 

IN SSI-REFERENCE(S): "535123-01-1; 551015-01-3" 

ADDED 

E-300 ZL-313-01-1 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-319-02-1 R TASK TITLE CHANGED FROM: "(INTERNAL)", TO: 

"(INTERNAL)(EWIS)" 

IN SSI-REFERENCE(S): "551018-01-3" ADDED AND 

"551018-01-1" REMOVED 

APPLICABILITY CHANGED FROM: "PRE 41600", TO: 

"A330-200 PRE 41600 OR A330-300 PRE 41600" 

E-300 ZL-319-02-2 R IN ACCESS: "319AL; 319AR; 319BL" ADDED 

IN PREPARATION TASKS: "DISCONNECT SCAVENGE 

WATER 

SYSTEM PIPE" REMOVED 

TASK TITLE CHANGED FROM: "(INTERNAL)", TO: 

"(INTERNAL)(EWIS)" 

IN SSI-REFERENCE(S): "551018-01-4" ADDED AND 

"551018-01-2" REMOVED 

APPLICABILITY CHANGED FROM: "POST 41600", TO: 

"A330-200 POST 41600 OR A330-300 POST 41600 OR 

A330-200F" 

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-322-01-3 R IN TASK TITLE: "(EWIS)" ADDED 

IN APPLICABILITY: "A330-200F" ADDED 

E-300 ZL-323-01-1 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 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 68

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-300 ZL-323-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

IN APPLICABILITY: "A330-200F" ADDED 

E-300 ZL-324-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "553010-01-2" ADDED 

E-300 ZL-324-01-2 R IN TASK TITLE: "(EWIS)" ADDED 

IN APPLICABILITY: "A330-200F" 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 

IN APPLICABILITY: "A330-200F" 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-325-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

IN APPLICABILITY: "A330-200F" 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 

IN APPLICABILITY: "A330-200F" 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-326-02-3 R TASK TITLE CHANGED FROM: "RUDDER", TO: "RUDDE 

(EWIS)" 

E-300 ZL-326-02-4 R IN TASK TITLE: "(EWIS)" ADDED 

IN APPLICABILITY: "A330-200F" ADDED 

E-300 ZL-326-03-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-300 ZL-326-03-2 R IN ACCESS: "326AT" ADDED 

IN TASK TITLE: "(EWIS)" ADDED 

E-300 ZL-326-03-3 R IN TASK TITLE: "(EWIS)" ADDED 

E-300 ZL-326-03-4 R TASK TITLE CHANGED FROM: "VISIBLE)", TO: 

"VISIBLE)(EWIS)" 

IN APPLICABILITY: "A330-200F" ADDED 

E-300 ZL-331-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "551024-01-1" ADDED 

E-300 ZL-332-01-1 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 

APPLICABILITY CHANGED FROM: "POST 43491 PRE 

44818", TO: "A330-200 POST 43491 PRE 44818 0R 

A330-300 POST 43491 PRE 44818" 

E-300 ZL-334-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-300 ZL-334-02-1 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-400 ZL-411-03-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-411-03-2 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-411-04-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 69

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-400 ZL-412-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-412-02-2 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-412-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-413-02-1 R IN PREPARATION TASKS: "THRUST REVERSER 

DEPLOYED" 

REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE"

E-400 ZL-413-02-2 R IN PREPARATION TASKS: "THRUST REVERSER 

DEPLOYED" 

REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-413-02-3 R IN PREPARATION TASKS: "THRUST REVERSER 

DEPLOYED" 

REMOVED 

IN TASK TITLE: "(EWIS)" ADDED

E-400 ZL-414-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-414-02-2 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-414-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-415-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-415-02-2 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-415-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-417-02-1 R IN ACCESS: "415BL; 416BR; 425BL; 427BL" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-417-02-2 R IN ACCESS: "427AL" ADDED AND "427BL" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-417-02-3 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-451-02-1 R IN ACCESS: "451AL; 461AL" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-451-02-2 R IN ACCESS: "451AL; 461AL" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "GE", TO: "A330-200 GE 

OR A330-300 GE" 

E-400 ZL-451-02-3 R IN ACCESS: "451AL; 461AL" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-452-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-400 ZL-453-01-1 R IN ACCESS: "453AL; 453AR; 463AL; 463AR" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

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

E-400 ZL-453-01-2 N NEW TASK ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 70

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-400 ZL-454-05-1 R IN ACCESS: "454DR; 454EL; 454ER; 464DR; 464EL; 

464ER" REMOVED 

IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

E-400 ZL-454-05-2 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-300 POST 43271 OR 

A330-200F" 

E-400 ZL-454-06-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "PRE 43271", TO: 

"A330-200 PRE 43271 OR A330-300 PRE 43271" 

E-400 ZL-454-06-2 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "POST 43271", TO: 

"A330-200 POST 43271 OR A330-300 POST 43271 OR 

A330-200F" 

E-500 ZL-500-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "575404-01-1; 575501-01-1" 

ADDED 

E-500 ZL-500-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

IN SSI-REFERENCE(S): "572134-02-10; 575404-01-1" 

ADDED 

E-500 ZL-521-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-522-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-523-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-531-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-531-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-535-01-1 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-542-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-550-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-571-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-572-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-573-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-500 ZL-574-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

DESCRIPTION CHANGED FROM: "17)", TO: "27)" 

E-500 ZL-575-01-1 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-715-01-1 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-733-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-700 ZL-734-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

E-800 ZL-800-01-1 R IN SSI-REFERENCE(S): "523801-01-1" ADDED 

E-800 ZL-811-01-1 R IN TASK TITLE: "(EWIS)" ADDED 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 71

SECTION TASK 

NUMBER 

REV 

CODE SUMMARY OF CHANGES 

E-800 ZL-821-01-1 R IN TASK TITLE: "(EWIS)" 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 

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 

E-800 ZL-823-02-1 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 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-800 ZL-832-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-800 ZL-833-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-800 ZL-833-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-800 ZL-834-01-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "ALL", TO: "A330-200 

OR A330-300" 

E-800 ZL-834-02-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "TYPE A", TO: 

"A330-200 TYPE A OR A330-300 TYPE A" 

E-800 ZL-834-03-1 R IN TASK TITLE: "(EWIS)" ADDED 

APPLICABILITY CHANGED FROM: "TYPE 1", TO: 

"A330-200 TYPE I OR A330-300 TYPE I" 

E-800 ZL-835-01-1 N NEW TASK ADDED 

E-800 ZL-835-02-1 N NEW TASK ADDED 

E-800 ZL-835-03-1 N NEW TASK 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.” 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 72

APPENDIX 2

A330-200F illustrations added. 

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. 

APPENDIX 8

No change. 

APPENDIX 9

Page APX 9.4 10HA sensor references amended in description in task 20-00-01-1. 

535CZ and 635CZ deleted rom access in task 20-00-01-4. 

Page APX 9.8 “A330-200 POST 48979: 325SL 325NL 312AR” and “PRE 48979” deleted from access 

in task 20-00-07-1. 

Page APX 9.9 “311AZ 313BL” added to access in task 20-00-07-2. 

APPENDIX 10

The MODIFICATION REFERENCE LIST has been updated to include the following modifications: 

Mod 49144 number corrected from 49114. All other changes are introduction of new modifications. 

MOD 

NUMBER MOD TITLE 

40041 EQUIPMENT/FURNISHINGS-DEFINE BASIC LOWER CARGO COMPARTMENT 

40366 WINGS-STRUCTURE-INTRODUCE POST A330 COMMON WING BOX DEFINITION 

41471 STABILIZERS-HORIZONTAL STABILIZER- MODIFY FRONT SPAR 

42275 WINGS-STRUCTURE-FIT T PLATES TO CENTRE SPAR 

43719 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - INSTALL 

COMPARTMENT DRAINAGE 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 73

MOD 

NUMBER MOD TITLE 

44601 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - ADAPT BASIC 

ST6 DEFINITION TO ST7

45395 EQUIPMENT/FURNISHINGS-CARGO COMPART.- ADAPT HEATED DRAINAGE SYSTEM 

IN FWD ANDAFT C.C. FOR ST7 A/C

47798 WINGS - INBOARD FLAP - OPTIMIZE INBOARD FLAP DESIGN 

48904 INDICATING/RECORDING SYSTEM - ACMS - INSTALL SYSTEM PROVISIONS FOR 

THE COMBINED FDIU/DMU (FDIMU)

49144 FLIGHT CONTROLS - ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) - INSTALL 

RUDDER FLY-BY WIRE ON A330/A340

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

49610 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL T SHAPED 

CENTERLINE GUIDE FOR A330-200 

50156 COMMUNICATIONS - CIDS - INSTALL COCKPITCREW TO CABIN CREW ALERTING 

SYSTEM 

50157 COMMUNICATIONS - CIDS - INSTALL CABIN CREW TO COCKPIT CREW ALERTING 

SYSTEM 

50567 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL "T-SHAPED" 

CENTER LINE GUIDE FOR A330-300 

53368 NAVIGATION-ADIRS-INTRODUCE AIR DATA MONITORING FUNCTION 

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 

55381 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- ADAPT ADVANCED CARGO 

LOADING SYSTEM FOR A330-200 

55559 OXYGEN-CABIN ATTENDANTS PORTABLE DEVICE- INTRODUCE NEW STD 

LAYOUT LIGHT WEIGHT PORTABLE OXYGEN CYLINDER ASSEMBLY 

55776 WATER / WASTE - WASTE DISPOSAL - INSTALL A BIDET 

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

LINK DAR , 4GSM/GPRS , ARINC 600 

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

56835 E/F - CARGO COMPARTMENTS - INSTALL HEATED DRAINAGE IN FWD AND AFT 

C.C. FOR A330-200 - ADVANCED CLS

56837 E/F - LOWER DECK BULK CARGO COMPARTMENT- PROVIDE CAPABILITY FOR 

LD3 CONTAINERS- FOR A330-300/A340-300 - ADVANCED CLS 

56839 E/F-LWR DECK AFT C.C.-ADAPT STRUCTURAL AND SYST. PROVISIONS FOR AN 

UCRC (LD-MCR) FOR A330-200 - ADVANCED CLS

57371 EQUIPMENT/FURNISHING - CURTAINS AND PARTITIONS - INTRODUCE IMPROVED 

DECOMPRESSION PANEL IN COCKPIT DOOR

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

58204 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL A 

MAIN DECK CLS (BFE) - ANCRA

58215 WATER / WASTE - AIR SUPPLY - INSTALL AN AUXILIARY COMPRESSOR 

58552 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL OF 

MAIN DECK CLS (BFE) MULTIPLE CHOICE CONFIGURATION - AAR 

58623 FUEL-TANKS- REMOVE OF THE CENTRE TANK CAPABILITY 

58640 CABIN SYSTEM - ON-BOARD MOBILE TELEPHONY SYSTEM - DEFINE OMTS PART 

OF ALNA V2 
 A330 MRB REPORT

Issue : July 2010 SOC Page : 74

MOD 

NUMBER MOD TITLE 

200281 FUEL - TANKS - ADDITION OF CENTRE TANK CAPABILITY 

APPENDIX 11

No change 
 A330 MRB REPORT

 

Page intentionally left blank 
A330 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 A330 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 intentionally left blank
 A330 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 74 

TOC 1 to 1 

 

LEP 1 to 1 

A 1 to 3 

B 1 to 3 

C-INTRO 1 to 7 

 

C-20 1 to 7 

C-21 1 to 5 

C-22 1 to 1 

C-23 1 to 3 

C-24 1 to 3 

C-25 1 to 8 

C-26 1 to 8 

C-27 1 to 8 

C-28 1 to 7 

C-29 1 to 3 

C-30 1 to 2 

C-31 1 to 2 

C-32 1 to 4 

C-33 1 to 1 

C-34 1 to 4 

C-35 1 to 5 

C-36 1 to 1 

C-38 1 to 2 

C-45 1 to 1 

C-46 1 to 1 

C-49 1 to 3 

C-52 1 to 4 

C-53 1 to 1 

C-54 PW 4000 1 to 1 

C-54 CF6-80E 1 to 1 

C-54 T700 1 to 1 

C-55 1 to 1 

C-56 1 to 1 

C-57 1 to 1 

C-CF6-80E-71 1 to 1 

C-CF6-80E-72 1 to 1 

C-CF6-80E-73 1 to 1 

C-CF6-80E-74 1 to 1 

C-CF6-80E-75 1 to 1 

C-CF6-80E-76 1 to 1 

C-CF6-80E-77 1 to 1 

C-CF6-80E-78 1 to 2 

C-CF6-80E-79 1 to 1 

C-CF6-80E-80 1 to 1 

C-PW 4000-71 1 to 1 

C-PW 4000-72 1 to 2 

C-PW 4000-73 1 to 1 

C-PW 4000-74 1 to 1 

C-PW 4000-75 1 to 1 

C-PW 4000-76 1 to 1 

C-PW 4000-77 1 to 1 

C-PW 4000-78 1 to 1 

C-PW 4000-79 1 to 1 

C-PW 4000-80 1 to 1 

C-RR T700-71 1 to 1 

C-RR T700-72 1 to 3 

C-RR T700-73 1 to 1 

C-RR T700-74 1 to 1 

C-RR T700-75 1 to 1 

C-RR T700-76 1 to 1 

C-RR T700-77 1 to 1 

C-RR T700-78 1 to 2 

C-RR T700-79 1 to 1 

C-RR T700-80 1 to 1 

D-INTRO 1 to 21 

D-32 1 to 3 

D-52 1 to 5 

D-53 1 to 63 

D-54 1 to 38 

D-55 1 to 12 

D-56 1 to 1 

D-57 1 to 298 

D-71 1 to 5 

D-78 1 to 2 

E-INTRO 1 to 5 

 

E-100 1 to 7 

E-200 1 to 5 

E-300 1 to 7 

E-400 1 to 7 

E-500 1 to 6 

E-600 1 to 1 

E-700 1 to 1 

E-800 1 to 4 

F 1 to 2 

APX 1 1 to 1 

APX 2 1 to 19 

APX 3 1 to 1 

APX 4 1 to 1 

APX 5 1 to 29 

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 10 
This page intentionally left blank
 A330 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 A330 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 A330 Type Certificate Data Sheet (TCDS) under the 

number 00G050A0002/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 A330 models and 

powerplants as defined on the aircraft Type Certificate Data Sheet: 

- A330-20x with GE CF6-80E engines 

- A330-22x with PW 4000 engines 

- A330-24x with TRENT 700 engines 

- A330-30x with GE CF6-80E engines 

- A330-32x with PW4000 engines 

- A330-34x with TRENT 700 engines 

- A330-22xF with PW 4000 engines 

- A330-24xF with TRENT 700 engines 

 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 

A330-20x 

A330-22x 

A330-24x 

A330-30x 

A330-32x 

A330-34x 

A330-22xF 

A330-24xF 

A330-202, A330-203 

A330-223 

A330-243 

A330-301 

A330-321, A330-322, A330-323 

A330-341, A330-342, A330-343 

A330-220F 

A330-240F 

2. BASIS FOR STANDARDS AND PROCEDURES

The scheduled maintenance tasks and frequencies contained in this MRB Report have been 
 A330 MRB REPORT 

Issue : July 2010 Page : A2

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 

Program Development Policy and Procedures Handbook (PPH) - 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. 

3. AIRCRAFT UTILISATION ASSUMPTIONS 

The MRB Report for the A330 is based on the following aircraft utilisation assumptions: 

A330-200, A330-200F 

 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 

A330-300 

 With interval defined as 800FH: Flight cycle envelope = 133 FC to 800 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 2200 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 A330 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. 
 A330 MRB REPORT 

Issue : July 2010 Page : A3

 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 months 

4C – Check 6 Yrs 

8C – Check 12 Yrs 

For safety related tasks, the 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 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 MSG3 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 intentionally left blank 
 A330 MRB REPORT 

Issue : July 2010 Page : B1

SECTION B

 GENERAL RULES THAT APPLY TO ALL A330 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 A330 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 Section, to the validity of the General Visual Inspections of the Structures 

Section. 

- For Structures Section, to tasks derived from Damage Tolerance Evaluation as noted in 

Sect. D, Structures Section, 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 955.2074/93. 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.0089/97. This is the controlling document for all tasks identified as Damage Tolerant 

Airworthiness Limitation Items. 

9. Within this MRB Report the terms "test", "check" and "inspection" are not intended to imply a 
 A330 MRB REPORT 

Issue : July 2010 Page : B2

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. ETOPS Maintenance Standards identified during the Type Certification process were originally 

listed in the MRB Report Appendix 3. These Standards included ETOPS related tasks (which are 

also included in MRB Report Section C) and ETOPS specific tasks/intervals (which are included 

in the ETOPS CMP document but not in MRB Report Section C). In the March 2002 MRB Report 

revision, the Appendix 3 was suppressed since it no longer provided complete information 

necessary for maintenance program development. 

ETOPS Maintenance Standards identified by in-service experience are quoted only in the 

ETOPS CMP document. Operators should note that the ETOPS CMP, reference AI/EA5000, is 

the authoritative document for mandatory ETOPS Maintenance Standards. 

15. When two or more intervals are assigned to a task, and when not otherwise stated, the interval 

expiring first shall apply. 

16. 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. 

17. 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. 
 A330 MRB REPORT 

Issue : July 2010 Page : B3

18. 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 

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. 
 A330 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 powerplants 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 A330 Airworthiness Limitation Section – Part 1 

 - GE CF6-80E1 Engine Shop Manual Chapter 5 

- PW 4000 Engine Shop Manual Chapter 5 

 - RR Time Limits Manual, T-Trent-1RR 

(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. 
 A330 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)

38.10.01 POTABLE (for A330-200F) 38.10.01 POTABLE (for A330-200F) 

38.32.01 FREIGHTER WASTE WATER DRAIN 

38.41.01 FREIGHTER AIR SUPPLY SYSTEM 

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 
 A330 MRB REPORT 

Issue : July 2010 Page : C-INTRO-3

53.59.00

(k) During the review of an aircraft system for the purpose of modifying or verifying the 

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 18 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: 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. 

NOTE 3: -deletedNOTE 4: For interval refer to Chapter 5 of Engine Shop Manual (ESM) (GE and PW) or 

Time Limits Manual (RR). 

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
 A330 MRB REPORT 

Issue : July 2010 Page : C-INTRO-4

FWD Passenger/ 1 36 MTHS 

Crew Door 

MID Passenger/ 1 36 MTHS 

Crew Door 

AFT Passenger/ 1 36 MTHS 

Crew Door 

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. 

For A330-200F applicable for FWD Passenger/Crew Door only. 

NOTE 11: Crew rest room (underfloor) and/or ACTs not to be removed if installed. 

NOTE 12: - deleted - (transferred 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: Task may be undertaken at opportunity of thrust reverser removal. 

NOTE 17: - deleted -

NOTE 18: - reserved - 

NOTE 19: - reserved - 

NOTE 20: - deleted - 

NOTE 21: - reserved - 

NOTE 22: - reserved - 

NOTE 23: - reserved - 

NOTE 24: Refer to the A330 Certification Maintenance Requirements (CMR) document 

(reference 955.2074/93) for identification of specific requirements regarding 

handling of task interval. Instructions to locate the CMR Document are given 

in Appendix 1 of this MRB Report. Where the CMR interval for an MRB 

Report task is more restrictive, the CMR interval takes precedence. 

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. 

 

NOTE 26 For CRR(u) users only: 
 A330 MRB REPORT 

Issue : July 2010 Page : C-INTRO-5

 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. 
 A330 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. 
 A330 MRB REPORT - Systems and Powerplant

Issue : July 2010 

 The term "-reserved-" indicates that the task number has been allocated to an A340 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

 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 Ce

Requirement (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 "A330 Certification Maintenance Requirements" reference 955.2074/93. InstruDocument are given in Appendix 1 of 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) 
 A330 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 are not subject to tasks additional to those given in Section E. 

7- This column indicates the A/C configuration, model or engine type to which this requirement is applicable. Examples are given 

ALL Task applicable to all A330 aircraft, including A330-200F 

A330-200 Task applicable to all A330-200 only, excluding A330-200F 

A330-200 

OR 

A330-300 

Task applicable to all A330 aircraft excluding A330-200F 

A330-200F Task applicable to all A330-200F only 

PRE 49144 Task applicable to all A330 PRE 49144. 

i.e. Aircraft without modification 49144 embodied. 

POST 49144 Task applicable to: all A330 POST 49144. 

i.e. to Aircraft with modification 49144 embodied. 

IF CREW REST ROOM 

INSTALLED 

Self-explanatory 

A330-300 

PRE 44051 

Task applicable to A330-300 without modification 44051 embodied. 

A330-200 

POST 44051 

Task applicable to A330-200 (excluding A330-200F) with 

modification 44051 embodied. 

POST 44051 POST 44061 POST 44085 

Task applicable to all A330 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 A330 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 A330 without both modification 45051 and 45085 embodied at the same time i.e. without any if these modifications embodied 

POST 44040 

PRE 44057 

Task applicable to all A330 with modification 44040 and without modification 44057 embodied at the same time. 
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 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 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 GVI 02 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  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).  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
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 20.0.151 * * * * * C O N T I N U E * * * * *  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).  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 GVI 02 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MO  INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).  N RS 03 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MO  COMPARTMENT (ONLY IF CONTAMINATED).(EWIS).  N GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED - I: 144 MO  IN THE BULK CARGO COMPARTMENT. (EWIS)  20.0.211 COCKPIT  R RS 01 CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY - I: 144 MO  IF 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 / COURIER COMPARTMENT  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
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 20.0.221 * * * * * C O N T I N U E * * * * *  R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MO  ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEEN  SEATS AND A/C AND 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 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).  N RS 04 CLEANING OF EWIS INSTALLED IN THE COURIER COMPARTMENT - I: 144 MO  AREA (ONLY IF CONTAMINATED), (EWIS)  N GVI 05 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MO  IN THE COURIER COMPARTMENT AREA,(EWIS).  N GVI 06 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 COURIER COMPARTMENT AREA,(EWIS).  NOTE: TASK ONLY APPLICAPBLE IF SEATS WITH EWIS  CONNECTION BETWEEN SEAT AND A/C AND/OR SEAT TO SEAT  CONNECTIONS INSTALLED.  20.0.223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT / COURIER OVERH  EAD COMPARTMENT  R RS 01 CLEANING OF EWIS AND CIRCUIT BREAKERS "5001 VE" - I: 144 MO  INSTALLED IN THE FWD CABIN ULITY AREA OVERHEAD  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001 - I: 144 MO  VE" AND  ́G, AND P ́ ROUTES INSTALLED IN THE FWD  CABIN UTILITY AREA OVERHEAD COMPARTMENT, (EWIS).  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
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 20.0.223 * * * * * C O N T I N U E * * * * *  N RS 03 CLEANING OF ALL EWIS AND CIRCUIT BREAKERS "5001 VE" - I: 144 MO  INSTALLED IN THE COURIER OVERHEAD COMPARTMENT (ONLY  IF CONTAMINATED), (EWIS).  N GVI 04 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001 - I: 144 MO  VE" AND "G, AND P" ROUTES INSTALLED IN THE COURIER  OVERHEAD COMPARTMENT AREA, (EWIS).  20.0.230 FWD MAIN DECK CARGO COMPARTMENT  N RS 01 CLEANING OF EWIS INSTALLED IN THE FWD MAIN DECK CARGO - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MO  IN THE FWD MAIN DECK CARGO COMPARTMENT AREA. (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).  20.0.233 FWD CABIN OVERHEAD COMPARTMENT  R RS 01 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).  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
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A330 MRB REPORT – Systems and Powerplant Section

 20.0.240 FWD MID MAIN DECK CARGO COMPARTMENT  N RS 01 CLEANING OF ALL EWIS INSTALLED IN THE FWD MID MAIN - I: 144 MO  DECK CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED),  (EWIS).  N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MO  IN THE FWD MID MAIN DECK OVERHEAD CARGO COMPARTMENT  AREA, (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).  20.0.243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT  R RS 01 CLEANING OF ALL EWIS INSTALLED IN THE MID CABIN - I: 144 MO  UTILITY AREA OVERHEAD COMPARTMENT AREA  (ONLY IF CONTAMINATED), (EWIS).  N GVI 03 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN UTILITY AREA OVERHEAD  COMPARTMENT AREA, (EWIS)  20.0.250 MID MAIN DECK CARGO COMPARTMENT  N RS 01 CLEANING OF EWIS INSTALLED IN THE MID MAIN DECK CARGO - I: 144 MO  COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).  N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MO  IN THE MID MAIN DECK CARGO COMPARTMENT AREA, (EWIS).  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 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 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.(EWIS)  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).  .  N GVI 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MO  INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENT  AREA. (EWIS)  20.0.260 AFT MID MAIN DECK CARGO COMPARTMENT  N RS 01 CLEANING OF EWIS INSTALLED IN THE AFT MID MAIN DECK - I: 144 MO  CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED).(EWIS).  20.0.261 AFT 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 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 O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 20.0.261 * * * * * C O N T I N U E * * * * *  R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MO  (ONLY IF CONTAMINATED), (EWIS).  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).  N RS 04 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED - I: 144 MO  IN THE AFT CABIN OVERHEAD COMPARTMENT AREA (EWIS).  20.0.270 AFT MAIN DECK CARGO COMPARTMENT  N RS 01 CLEANING OF ALL EWIS INSTALLED IN THE AFT MAIN DECK - I: 144 MO  CARGO COMPARTMENT (ONLY IF CONTAMINATED), (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  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 IN THIS - I: 144 MO  AREA, (EWIS).  20.0.273 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 20.0.273 * * * * * C O N T I N U E * * * * *  R RS 01 CLEANING OF EWIS AND CIRCUIT BREAKERS "5005 VE" - I: 144 MO  INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEAD  COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).  R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5005 - I: 144 MO  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).  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).  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 20.0.333 * * * * * C O N T I N U E * * * * *  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).  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 20LH/RH, (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).  20.0.542 OUTER 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).  ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 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  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 

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A330 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 RESERVED  DS 03 DISCARD RECIRCULATION FILTER ELEMENTS (PALL). 7 I: 5600 FH  NOTE 15  R OP 04 OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC 9 I: 2 C  CLOSING OF ISOLATION VALVES OF THE STOWAGE  COMPARTMENT  R OP 05 OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC 8 I: 3200 FH  CLOSING OF ISOLATION VALVES OF THE CREW REST ROOM NOTE  (UNDERFLOOR) IN LOWER DECK LAVATORY CONFIGURATION.  NOTE: IF MOBILE CREW REST ROOM IS NOT FITTED WHEN  TASK BECOMES DUE IT MUST BE PERFORMED WHEN MCR IS  NEXT INSTALLED.  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 9 I: 2 C  USING THE FAN OFF SWITCH  09 TASK RESERVED  10 TASK RESERVED  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  N OP 13 OPERATIONAL CHECK TO VERIFY CLOSING OF ISOLATION 8 I: 3200 FH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 21.21.00 * * * * * C O N T I N U E * * * * *  VALVES OF THE MDCC.  N OP 14 OPERATIONAL CHECK OF MORV. 9 I: 34000 FH  OR  12 YE  21.23.00 LAVATORY/GALLEY VENTILATION  DS 01 DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 7 I: 1200 FH  NOTE 1  R DS 02 DISCARD FILTER ELEMENT 6 I: 1200 FH  NOTE 1  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 04 TASK RESERVED  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 73.25.00/01-G6,  73.25.00/01-PW, 73.25.00/01-RR)  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 

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A330 MRB REPORT – Systems and Powerplant Section

 21.26.00 * * * * * C O N T I N U E * * * * *  INSULATION  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  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 24  CASE OF SMOKE WARNING.  (THIS TASK COVERS TASK 26.16.00/02)  R OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 3200 FH  COLD AIR VALVE IN CASE OF SMOKE WARNING NOTE 24  R 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)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 21.28.00 * * * * * C O N T I N U E * * * * *  R OP 04 OPERATIONAL CHECK OF HARDWIRED 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)  R DS 06 DISCARD FILTER ELEMENT OF BULK VIDEO COMPARTMENT 9 I: 2400 FH  NOTE 1  R 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 

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A330 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-19 ZL-19 FC 08 REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK 9 I: 2 C  NOTE 1  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 21.50.00 * * * * * C O N T I N U E * * * * *  R RS 09 CLEANING OF CABIN TEMPERATURE SENSORS, SENSE LINES 7 I: 2 A  AND INLETS NOTE 1  R DS 10 DISCARD CABIN TEMPERATURE SENSOR FILTERS 7 I: 1 A  NOTE 1  11 TASK RESERVED  DS 12 DISCARD FLOW CONTROL VALVE FILTERS 7 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.  N RS 16 CLEANING OF COURIER AREA AND MDCC TEMPERATURE 7 I: 1600 FH  SENSORS, SENSE LINES & INLETS. NOTE 1  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21 
 MSI 

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A330 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 

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A330 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)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 23.39.01 * * * * * C O N T I N U E * * * * *  R DS 01 DISCARD ALL FILTER ELEMENTS ON TAILWIND SYSTEM 7 I: A  23.39.02 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION BY BOEING (CBB).  OP 01 OPERATIONAL CHECK OF CONNEXION BY BOEING SYSTEM POWER 9 I: 4 C  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  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 23.71.00 * * * * * C O N T I N U E * * * * *  (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  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  R 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  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 23.73.00 * * * * * C O N T I N U E * * * * *  06 TASK DELETED  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  OPERATION  23.73.01 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)  N OP 01 OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, AND 9 I: 20000 FH  DEUS-A CUT OFF FUNCTION  N OP 02 OPERATIONAL CHECK OF EVAC FUNCTION 9 I: 20000 FH  N OP 03 OPERATIONAL CHECK OF BATTERY POWERED CIDS PA 9 I: 20000 FH  OPERATION  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 

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A330 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 SCAVENGE FILTER ELEMENT 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 24  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  EXTENDED  RS 13 CLEAN IDG OIL COOLER 7 I: 4 C  OP 14 OPERATIONAL CHECK OF IDG DISCONNECT FUNCTION 9 I: 4 C  OP 15 OPERATIONAL CHECK OF GENERATOR SHUT-DOWN WHEN ENGINE 9 I: 60 MO  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 24.20.00 * * * * * C O N T I N U E * * * * *  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 RESERVED  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: C  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  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)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 24.50.00 * * * * * C O N T I N U E * * * * *  OP 04 OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN 9 I: 2 C  EMERGENCY CONFIGURATION  OP 05 OPERATIONAL CHECK OF LEFT AND RIGHT FUEL PUMP 2 8 I: 18 MO  SHEDDING IN LAND RECOVERY CONFIGURATION NOTE 24  OP 06 OPERATIONAL CHECK AFT APU PUMP SHEDDING IN LAND 8 I: 18 MO  RECOVERY CONFIGURATION  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 

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A330 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 ATTACHMENT 8 I: 36 MO  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 SEATBELT SYSTEM FOR RESTORATION OF AIRBAG AND 7,8 I: VR  DISCARD BATTERY, HOSE, SQUIB AND GAS STORAGE  ACCORDING TO CMM.  25.22.00 CABIN ATTENDANT SEATS  R GVI 01 GENERAL VISUAL INSPECTION OF SEAT ATTACHMENT POINTS. 8 I: 36 MO  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.22.00 * * * * * C O N T I N U E * * * * *  R GVI 02 GENERAL VISUAL INSPECTION OF SEAT STRUCTURE. 8 I: 36 MO  R 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)  R VC 01 VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS 8 I: 18 MO  IN CABIN ARE CLOSED  R 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  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.27.00 * * * * * C O N T I N U E * * * * *  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  AND 53.41.59).  04 TASK DELETED  05 TASK RESERVED  25.34.00 GALLEY COOLING  RS 01 CLEAN AIR CHILLER CONDENSER AIR FILTER. 7 I: 1400 FH  NOTE 1  02 TASK RESERVED  03 TASK RESERVED  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.34.00 * * * * * C O N T I N U E * * * * *  RS 04 CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES 7 I: 1400 FH  IN THE GALLEY CABINET. NOTE 1  25.40.00 LAVATORIES  DI 01 DETAILED INSPECTION OF WASTE COMPARTMENT FOR FIRE 9 I: NR  CONTAINMENT CAPABILITY. OR  1 C  NOTE 8  OP 02 OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP 9 I: NR  OR  1 C  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  AND 53.41.59).  04 TASK DELETED  25.47.00 LOWER DECK LAVATORIES  RS 01 CLEANING OF DRAIN OPENINGS 9 I: C  VC 02 VISUAL CHECK OF LDL RAPID DECOMPRESSION PANELS 8 I: 800 FH  25.51.00 LOWER DECK CARGO LOADING SYSTEM  R OP 01 OPERATIONAL CHECK OF POWER DRIVE UNITS 9 I: C  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 

RE

A330 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 FOR 8 I: 34000 FH  DETAILED INSPECTION.  R GVI 04 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES 9 I: A ZL-13 ZL-15 R GVI 05 GENERAL VISUAL INSPECTION OF OVERRIDEABLE Y-DOOR SILL 9 I: A ZL-13 LATCHES ZL-15 R GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS 9 I: A ZL-13 ZL-15 R GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS INCLUDING 9 I: A ZL-13 TRANSPORT ROLLER. ZL-15 NOTE 11  R DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 300 FC  WEAR AND DAMAGE. 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * C O N T I N U E * * * * *  R GVI 09 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS 9 I: 4 A ZL-13 NOTE 11 ZL-15 R GVI 10 GENERAL VISUAL INSPECTION OF XZ LATCHES 8 I: 3200 FH  NOTE 11  R GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AT C20, C39, 9 I: 4 A ZL-13 C53.2, C65 AND C68 ZL-15 NOTE 11  R GVI 12 GENERAL VISUAL INSPECTION OF FIXED, RETRACTABLE AND 9 I: 4 A ZL-13 OVERRIDEABLE YZ-LATCHES ZL-15 NOTE 11  R GVI 13 GENERAL VISUAL INSPECTION OF Y-GUIDE ROLLERS, 9 I: C ZL-13 AUTOMATIC Z-GUIDES, GUIDE RAILS, YZ-LATCH GUIDE ZL-15 ROLLERS, XY-ENTRANCE GUIDE ASSEMBLIES, Y-GUIDES AND  Y-GUIDE ACTUATION MECHANISMS (AND X-GUIDES WITH MOD  40208)  NOTE 11  14 TASK RESERVED  15 TASK DELETED  16 TASK RESERVED  R GVI 17 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.51.00 * * * * * C O N T I N U E * * * * *  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 OP 20 OPERATIONAL CHECK OF CENTERLINE GUIDE SWIVEL NOSES. 9 I: 4 C  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)  N DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FH  N DI 03 REMOVE LOWER DECK-MOBIL CREW REST CONTAINER LATCHES 8 I: 34000 FH  FOR DETAILED INSPECTION.  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.51.01 * * * * * C O N T I N U E * * * * *  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.51.01 * * * * * C O N T I N U E * * * * *  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)  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.51.01 * * * * * C O N T I N U E * * * * *  N GVI 14 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-13 ZL-15 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 FORWARD/AFT 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 8 I: 8 DY  NOTE 11  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)  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 25.52.00 * * * * * C O N T I N U E * * * * *  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  VC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS 8 I: 8 DY  AND ACCESS DOOR AT C73  VC 02 VISUAL CHECK OF DECOMPRESSION PANELS 8 I: 8 DY  GVI 03 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS 9 I: C ZL-16 R DI 04 DETAILED INSPECTION OF DIVIDER NETS, NET 9 I: C  ATTACHMENT POINTS, NET CONNECTING DEVICES AND TENSION  BUCKLES  R DI 05 DETAILED INSPECTION OF NET SCREENS, NET SCREEN 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.54.00 * * * * * C O N T I N U E * * * * *  ATTACHMENT POINTS AND TENSION BUCKLES  R DI 06 DETAILED INSPECTION OF SCREEN DECOMPRESSION 9 I: C  TARPAULINS  25.55.00 MAIN DECK CARGO COMPARTMENT (INCLUDING DRAINAGE AND BARRIER  WALL)  N DI 01 DETAILED INSPECTION OF BARRIER WALL, BARRIER WALL 8 I: 1000 FH  ATTACHMENTS, DECOMPRESSION PANEL, SMOKE CURTAIN AND OR  ACCESS DOOR SEALING. 3 MO  N GVI 02 GENERAL VISUAL INSPECTION OF MDCC LINING. 9 I: A ZL-23 ZL-24 ZL-25 ZL-26 ZL-27 N GVI 03 GENERAL VISUAL INSPECTION OF THE DRAINAGE SYSTEM 9 I: 4 C ZL-13 INSTALLATION. ZL-13 ZL-15 ZL-15 ZL-23 ZL-24 ZL-25 ZL-26 ZL-27 N GVI 04 GENERAL VISUAL INSPECTION OF THE PROTECTION ANGLE AT 9 I: A ZL-23 THE BARRIER WALL AND THE REAR BULK HEAD. ZL-27 N VC 05 VISUAL CHECK OF THE DRAIN FUNNELS WITHIN THE DRAIN 9 I: 1000 FH  PANS FOR CLOGGING OR OBSTRUCTION AND CLEAN AS  NECESSARY.  25.56.00 MAIN DECK CARGO LOADING SYSTEM  N OP 01 OPERATIONAL CHECK OF BRAKING ROLLER. 9 I: 36 MO  N GVI 02 GENERAL VISUAL INSPECTION OF XZ-LATCHES. 8 I: 3200 FH  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.56.00 * * * * * C O N T I N U E * * * * *  N DI 03 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FH  N OP 04 OPERATIONAL CHECK OF XZ-ENDSTOP SWIVEL NOSES. 9 I: 4 C  N GVI 05 GENERAL VISUAL INSPECTION OF BALL TRANSFER UNITS, 9 I: 1000 FH ZL-23 BALL MATS.  N GVI 06 GENERAL VISUAL INSPECTION OF LOADING BRIDGE. 9 I: 1000 FH ZL-23 N GVI 07 GENERAL VISUAL INSPECTION XZ-ENDSTOPS. 9 I: 4 A ZL-23 ZL-27 N GVI 08 GENERAL VISUAL INSPECTION OF GUIDING COMPONENTS. 9 I: 4 A ZL-23 ZL-24 ZL-25 ZL-26 ZL-27 N GVI 09 GENERAL VISUAL INSPECTION OF SPLITTER. 9 I: 4 A ZL-23 ZL-24 N GVI 10 GENERAL VISUAL INSPECTION OF ROLLER TRAYS, TRANSPORT 9 I: 1000 FH ZL-23 ROLLERS AND BRAKING ROLLERS. ZL-24 ZL-25 ZL-26 ZL-27 N GVI 11 GENERAL VISUAL INSPECTION OF FIXED YZ-LATCHES, 9 I: 4 A ZL-23 OVERRIDEABLE CENTER LATCHES, RETRACTABLE SIDE ZL-24 RESTRAINT ASSEMBLIES. ZL-25 ZL-26 ZL-27 N GVI 12 GENERAL VISUAL INSPECTION OF OVERRIDEABLE ANTI ROLL 9 I: 4 A ZL-23 OUT DEVICE.  25.61.00 COCKPIT ESCAPE FACILITIES  VC 01 VISUAL CHECK OF EMERGENCY ESCAPE ROPE AND ROPE 8 I: 6 YE  ATTACHMENT  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 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  04 TASK RESERVED  05 TASK RESERVED  06 TASK RESERVED  07 TASK RESERVED  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 EMERGENCY 8 I: 18 MO  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.65.35 * * * * * C O N T I N U E * * * * *  ACTIVATION.  25.65.51 MEGAPHONE  R DS 01 DISCARD MEGAPHONE BATTERIES 9 I: VR  R 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  WITH OVERHAULED.  25.74.00 CREW REST ROOM (CABIN)  DI 01 DETAILED INSPECTION OF SEAT BELTS, BELT ATTACHMENTS 8 I: 36 MO  AND LOWER 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).  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 25.75.00 * * * * * C O N T I N U E * * * * *  DI 02 DETAILED INSPECTION OF BED BELTS AND BELT 8 I: 36 CRR MO  ATTACHMENTS ON CREW REST BUNKS  03 TASK RESERVED  VC 04 VISUAL CHECK OF CARGO COMPARTMENT CEILING WELL, 8 I: 6 YE  INTERFACE LININGS AND OF THE OUTSIDE OF THE CONTAINER  R GVI 05 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-25 ATTACHMENT POINTS OF THE STAIRHOUSE (STAIRHOUSE ZL-25 REMOVED).  OP 06 OPERATIONAL CHECK OF DOOR HINGE AND LOCK 9 I: 36 CRR MO  07 TASK RESERVED  08 TASK RESERVED  09 TASK RESERVED  10 TASK RESERVED  11 TASK RESERVED  12 TASK RESERVED  VC 13 VISUAL CHECK OF HATCH SEAL, DOOR SEALS AND BELLOW 8 I: 36 MO  SEALS.  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 26.00.00 FIRE PROTECTION  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  26.17.00 LAVATORY SMOKE DETECTION  01 TASK DELETED  26.18.00 AUXILIARY AREAS SMOKE DETECTION  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.18.00 * * * * * C O N T I N U E * * * * *  OP 01 OPERATIONAL CHECK OF LDMCR SMOKE DETECTION BY PTT. 9 I: 2 A  NOTE 25  RS 02 REMOVE AND CLEAN LDMCR SMOKE DETECTORS. 6 I: 72 CRR MO  OP 03 OPERATIONAL CHECK OF LDMCR STAIRHOUSE SMOKE DETECTION 9 I: C  SYSTEM BY MCDU.  OP 04 OPERATIONAL CHECK OF FCRC SMOKE DETECTION SYSTEM BY 9 I: C  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 SMOKE DETECTORS WITH 9 I: 18 CRR MO  AEROSOL.  07 TASK DELETED  08 TASK RESERVED  09 TASK RESERVED  OP 10 OPERATIONAL CHECK OF VCC SMOKE DETECTION BY MCDU. 8 I: 18 MO  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.18.00 * * * * * C O N T I N U E * * * * *  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  14 TASK RESERVED  15 TASK RESERVED  16 TASK RESERVED  17 TASK RESERVED  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 8 I: 17000 FH  RACK IV SMOKE DETECTION  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 26.18.01 BULK AVIONICS COMPARTMENT SMOKE DETECTION (MOD 46441)  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  26.18.02 SMOKE DETECTION COURIER AREA  N NO TASK SELECTED  26.19.00 MAIN DECK CARGO COMPARTMENT SMOKE DETECTION  N OP 01 OPERATIONAL CHECK OF MAIN DECK CARGO COMPARTMENT 9 I: 3200 FH  SMOKE DETECTION BY PTT.  N OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF MDCC 9 I: 18 MO  ISOLATION VALVES.  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)  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.21.00 * * * * * C O N T I N U E * * * * *  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 TASK 49.62.00/03)  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  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 (THIS 8 I: 36 MO  TASK COVERS TASKS 28.29.00/01 AND 49.62.00/04)  DS 11 DISCARD CARTRIDGE 8 I: VR  26.23.00 LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT AND  BULK)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.23.00 * * * * * C O N T I N U E * * * * *  OP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW 9 I: C  PRESSURE INDICATION CIRCUIT BY PTT  R 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  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  13 TASK DELETED  14 TASK DELETED  15 TASK DELETED  26.24.00 PORTABLE FIRE EXTINGUISHER  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.24.00 * * * * * C O N T I N U E * * * * *  FC 01 REMOVE BOTTLES FOR WEIGHT CHECK 9 I: VR  NOTE 26  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 (IF INSTALLED) (CREW REST  ROOM - UNDERFLOOR)  01 TASK RESERVED  OP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 8 I: 12000 CRR  CIRCUIT IN THE LDMCR. FH  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  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.  OP 08 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MO  IN THE LDMCR.  09 TASK RESERVED  10 TASK RESERVED  11 TASK RESERVED  12 TASK DELETED  13 TASK RESERVED  14 TASK RESERVED  15 TASK DELETED  16 TASK RESERVED  17 TASK RESERVED  18 TASK RESERVED  19 TASK RESERVED  20 TASK RESERVED  21 TASK RESERVED  22 TASK RESERVED  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 26.28.00 * * * * * C O N T I N U E * * * * *  23 TASK RESERVED  24 TASK RESERVED  25 TASK RESERVED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 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 NO 6)  27.21.00 RUDDER MECHANICAL CONTROL  01 TASK DELETED  02 TASK DELETED  R OP 03 OPERATIONAL CHECK OF YAW DAMPER SERVO ACTUATOR 9 I: C  STANDBY SERVO LOOP  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.21.00 * * * * * C O N T I N U E * * * * *  R VC 04 CHECK POINTER OF CABLE TENSION REGULATOR WITHIN 9 I: 2 C  LIMITS  R OP 05 OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL 9 I: 2 C  R OP 06 OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL 9 I: 2 C  LIMITATION UNITS STANDBY CHANNEL  R VC 07 VISUAL CHECK OF RUDDER MECHANICAL CONTROL IN FIN 8 I: 20000 FH  R DI 08 DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL 6,9 I: 4 C  (EXCLUDING FIN)  R OP 09 OPERATIONAL CHECK OF AP ARTIFICIAL FEEL SPRING ROD 9 I: 4 C  10 TASK RESERVED  R FC 11 FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS 8 I: 42 MO  SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR OR  WORKSHOP CHECK 20000 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.21.00 * * * * * C O N T I N U E * * * * *  R OP 12 OPERATIONAL CHECK OF CENTERING MECHANISM 8 I: 34000 FH  R OP 13 OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE 8 I: 3200 FH  NOTE 24  14 TASK DELETED  R VC 15 VISUAL CHECK TO CONFIRM INTEGRITY OF CONTROL ROD 8 I: 20000 FH  (ITEM 220 IN IPC 272147-1A) IN PTLU LINKAGE NOTE 24  LU 16 LUBRICATION OF THE RUDDER PEDALS ADJUSTMENT MECHANISM 6 I: C  17 TASK DELETED  R DI 18 DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT 6 I: 4 C  R OP 19 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM 9 I: 2 C  STANDBY CHANNEL  (THIS TASK COVERS TASK 27.90.00/18)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.21.00 * * * * * C O N T I N U E * * * * *  R 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)  R 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  R LU 06 LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER 8 I: 7500 FH  BEARING (RUDDER SIDE) OR  18 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.24.00 * * * * * C O N T I N U E * * * * *  R LU 07 LUBRICATION OF RUDDER HINGE BEARING NO 6 9 I: 7500 FH  OR  18 MO  R 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  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  LU 04 LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING 8 I: 7500 FH  OR  18 MO  OP 05 OPERATIONAL CHECK OF FCPCS AND FCSCS STANDBY SERVO 9 I: C  LOOPS ON PITCH CONTROL (COVERED BY MSI 27-90-00  TASK NO 9)  06 TASK RESERVED  27.40.00 TRIMMABLE HORIZONTAL STABILIZER (THS)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.40.00 * * * * * C O N T I N U E * * * * *  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  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  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  17 TASK RESERVED  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.40.00 * * * * * C O N T I N U E * * * * *  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  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.50.00 * * * * * C O N T I N U E * * * * *  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, PINION AND RACK 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  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.80.00 * * * * * C O N T I N U E * * * * *  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 RESERVED  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 24  OP 06 OPERATIONAL CHECK OF FCPCS AND FCSCS AILERON SERVO 9 I: C  LOOPS  (THIS TASK COVERS TASK 27.14.00/06)  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 FCPCS AND FCSCS STANDBY SERVO 9 I: 15 MO  LOOPS ON PITCH CONTROL NOTE 24  (THIS TASK COVERS TASK 27.34.00/05)  OP 10 OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY 9 I: C  OP 11 OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2 9 I: 1 C  NOTE 24  12 TASK RESERVED  OP 13 OPERATIONAL CHECK OF LIGHTS 9 I: 2 A  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 27.90.00 * * * * * C O N T I N U E * * * * *  (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)  OP 15 OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP 9 I: C  OP 16 OPERATIONAL CHECK RUDDER ELECTRICAL BACK UP 8 I: 5000 FH  17 TASK RESERVED  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)  OP 19 OPERATIONAL CHECK OF POWER SUPPLY OF THE RTA2, RTLU 9 I: C  AND PTLU MOTOR 2  OP 20 OPERATIONAL CHECK OF PFTU-TRIM 2 NORMAL/BACK-UP 9 I: C  POWER SUPPLY  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 28.00.00 FUEL  28.11.00 TANKS  R OP 01 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DY  FROM 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 RESERVED  OP 08 OPERATIONAL CHECK OF STANDBY FUEL CELL CLACK VALVES 9 I: 8 C  TO ENSURE FULL AND FREE MOVEMENT  R OP 09 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DY  FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS NOTE 1  10 TASK RESERVED  11 TASK RESERVED  12 TASK RESERVED  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 28.11.00 * * * * * C O N T I N U E * * * * *  13 TASK RESERVED  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  28.13.00 CENTER BOX VENTING AND DRAINAGE  R OP 01 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: A  CENTER BOX (THIS TASK COVERS TASKS 28.22.00/06,  28.23.00/03 AND 28.25.00/03)  28.14.00 TRIM PIPE SHROUD DRAINAGE  01 TASK DELETED  02 TASK DELETED  FC 03 FUNCTIONAL CHECK OF TRIM PIPE SHROUD DRAIN LINE AND 8 I: 36 MO  CONNECTORS WITHIN PRESSURIZED FUSELAGE  (COVERED BY MSI MSI 28.27.00 TASK N03)  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)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 28.18.00 * * * * * C O N T I N U E * * * * *  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)  R 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  R GVI 06 GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD 9 I: 4 C  CARGO BAY INSULATION MATS (SFAR88)  R 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  ELECTRICAL WIRING AND CONNECTIONS (SFAR88)  GVI 10 GENERAL VISUAL INSPECTION OF WING FUEL PUMP 9 I: 8 C  ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 28.18.00 * * * * * C O N T I N U E * * * * *  SUPPLY CABLE (SFAR88)  28.21.00 MAIN FUEL PUMP SYSTEM  OP 01 OPERATIONAL CHECK TO VERIFY ISOLATION OF RIGHT NO.2 8 I: 4800 FH  MAIN FUEL PUMP WHEN LEFT NO.2 MAIN FUEL PUMP IS NOTE 24  RUNNING IN ELECTRICAL EMERGENCY CONFIGURATION AND TO  VERIFY LEFT NO.2 PUMP "OFF" FUNCTION IS OPERATIVE  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  04 TASK RESERVED  OP 05 OPERATIONAL CHECK TO ENSURE THAT THE RIGHT NO.2 MAIN 8 I: 18 MO  FUEL PUMP OPERATES WHEN THE LEFT NO.2 MAIN FUEL PUMP  IS SWITCHED OFF IN ELECTRICAL EMERGENCY CONFIGURATION  06 TASK RESERVED  07 TASK RESERVED  28.22.00 APU FUEL PUMP SYSTEM  01 TASK RESERVED  02 TASK DELETED  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  (60QA1, 60QA2, 61QA1, 61QA2).  OP 04 OPERATIONAL CHECK OF AFT APU FUEL PUMP FIRE STOP 9 I: C  CIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS (5WF AND  6WF)  GVI 05 GENERAL VISUAL INSPECTION OF APU FUEL FEED SHROUD 9 I: 4 C ZL-31 LINE AND FUEL/AIR SEPARATOR FOR INTEGRITY AND ABSENCE ZL-31 * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 28.22.00 * * * * * C O N T I N U E * * * * *  OF LEAKAGE PATH.  R OP 06 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: A  CENTER BOX  (COVERED BY MSI 28-13-00 TASK NO1)  OP 07 OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO 9 I: 2800 FH  DRAIN ANY ACCUMULATED WATER  08 TASK RESERVED  09 TASK RESERVED  OP 10 OPERATIONAL CHECK TO VERIFY THAT RELAY 15QC HAS NOT 8 I: 36 MO  FAILED IN ENERGIZED POSITION.  28.23.00 CROSSFEED SYSTEM  OP 01 OPERATIONAL CHECK OF CROSSFEED VALVE TO VERIFY THAT 8 I: 34000 FH  INDIVIDUAL ENGINE FUEL FEED SYSTEMS CAN BE OR  INTERCONNECTED 12 YE  OP 02 OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL 9 I: 2 C  MOTORS  R OP 03 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: A  CENTER BOX  (COVERED BY MSI 28.13.00 TASK NO1)  04 TASK RESERVED  05 TASK RESERVED  06 TASK RESERVED  28.24.00 ENGINE LP FUEL SHUT-OFF  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 28.24.00 * * * * * C O N T I N U E * * * * *  OP 01 OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL 9 I: 2 C  MOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT AND  CORRECT COCKPIT INDICATION  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(S) FOR DAMAGE 9 I: C  OR EVIDENCE OF WEAR  OP 02 OPERATIONAL CHECK TO PROVE THAT THERE IS NO FUEL 8 I: 34000 FH  TRANSFER FROM AFT TO FWD INNER TANK WHEN EMERGENCY OR  ISOLATION VALVE IS SELECTED CLOSED 12 YE  R OP 03 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: A  CENTER BOX  (COVERED BY MSI 28-13-00 TASK NO1)  28.26.00 MAIN TRANSFER SYSTEM  NO TASK SELECTED  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)  ISSUE: JUL 01/10 FUEL SECTION: C-28 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 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  R GVI 01 GENERAL VISUAL INSPECTION OF JETTISON PIPE FLEXIBLE 9 I: 2 C  HOSE FOR SECURITY AND CONDITION  R GVI 02 GENERAL VISUAL INSPECTION OF ANTI-CORONA DEVICE FOR 9 I: 2 C  SECURITY OF ATTACHMENT AND FOR SATISFACTORY CONDITION  R OP 03 OPERATIONAL CHECK TO VERIFY CORRECT RESPONSE OF 9 I: 4 C  JETTISON VALVES 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  01 TASK RESERVED  ISSUE: JUL 01/10 FUEL SECTION: C-28 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 28.51.00 FUEL CONTROL AND MONITORING  01 TASK RESERVED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUEL SECTION: C-28 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 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  R 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  OP 08 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH GREEN 8 I: 18 MO  HYDRAULIC SYSTEM PRESSURIZED.  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  (COVERED BY MSI 29-20-00 TASK NO 07)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 29.10.00 * * * * * C O N T I N U E * * * * *  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 SYSTEM  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-19 FC 18 REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YE  19 TASK RESERVED  20 TASK RESERVED  VC 21 VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN 9 I: A  VALVE POSITION  22 TASK RESERVED  23 TASK RESERVED  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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 29.20.00 * * * * * C O N T I N U E * * * * *  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, BLUE AND YELLOW LOW LEVEL 8 I: 12000 FH  WARNING 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)  09 TASK RESERVED  OP 10 OPERATIONAL CHECK OF THE AUTOMATIC START OF THE BLUE 9 I: C  ELECTRIC PUMP.  29.30.00 HYDRAULIC SYSTEM DATA ACQUISITION / INTERFACE AND 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 

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A330 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  30.21.01 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 GE CF6-80E1)  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)  30.21.02 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 PW4000)  R NO TASK SELECTED  30.21.03 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 RR TRENT 768/772)  NO TASK SELECTED  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 

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A330 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  R 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 

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A330 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 THE 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 OPERATIONEL CHECK FOR DFDR SYSTEM BY USING THE 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 

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A330 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)  OP 01 OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL 9 I: C  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 31.60.01 * * * * * C O N T I N U E * * * * *  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 

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A330 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  32.21.00 NOSE GEAR  LU 01 LUBRICATION OF NOSE 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  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 32.21.00 * * * * * C O N T I N U E * * * * *  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  LU 03 LUBRICATE ALL GEAR DOWN LOCK PIVOT PINS 5,8 I: 500 FC  OR  4 MO  VC 04 VISUAL CHECK OF DOWN LOCK SPRINGS ON ALL LANDING 9 I: 2 A  GEARS  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  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  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32 
 MSI 

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A330 MRB REPORT – Systems and Powerplant Section

 32.30.00 * * * * * C O N T I N U E * * * * *  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 14 TASK RESERVED  15 TASK RESERVED  16 TASK RESERVED  17 TASK RESERVED  18 TASK RESERVED  19 TASK RESERVED  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  VC 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  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 HR  GVI 08 GENERAL VISUAL INSPECTION OF WHEELS 9 I: 36 HR  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 32.40.00 * * * * * C O N T I N U E * * * * *  VC 09 VISUAL CHECK OF BRAKE FOR HYDRAULIC LEAKS 9 I: 36 HR  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).  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 GEAR FOR RESTORATION 9 I: NOTE 7  (COVERED BY MSI 32-21-00, TASK NO5)  32.53.00 NOSE LANDING GEAR-STEERING ANGLE PROTECTION  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 

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A330 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  R OP 05 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA THE EPSU 9 I: 2 A  TEST PUSHBUTTON.  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LIGHTS SECTION: C-33 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 33.51.00 * * * * * C O N T I N U E * * * * *  R 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 

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A330 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 

RE

A330 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)  NO TASK SELECTED  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)  - 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)  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 34.43.00 * * * * * C O N T I N U E * * * * *  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 

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A330 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.00.00 OXYGEN  35.10.00 CREW OXYGEN  R VC 01 VISUAL CHECK OF OXYGEN MASKS 9 I: 18 MO  (OUT OF BOX WITH INFLATED HARNESS)  RS 02 CLEAN 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 OXYGEN 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  N OP 08 OPERATIONAL CHECK OF OXYGEN CYLINDER HANDVALVE 8 I: 72 MO  SWITCHES.  N FC 09 FUNCTIONAL CHECK OF LOW PRESSURE SWITCH. 9 I: 40000 FH  OR  72 MO  N FC 10 FUNCTIONAL CHECK OF OXYGEN SYSTEM PRESSURE HOLDING 8 I: 72 MO  CHARACTERISTICS AND OPERATIONAL CHECK OF BLEED/VENT  VALVE.  N FC 11 FUNCTIONAL CHECK OF ALTITUDE PRESSURE SWITCH. 9 I: 72 MO  N OP 12 OPERATIONAL CHECK OF OXYGEN MANUAL ACTIVATION AND 8 I: 24 MO  CONTAINER DOOR OPENING.  N OP 13 OPERATIONAL CHECK OF THE CABIN OXYGEN SUPPLY OFF 8 I: 72 MO  INDICATION AND MONITORING FUNCTION.  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.10.00 * * * * * C O N T I N U E * * * * *  N OP 14 OPERATIONAL CHECK OF REGULATION/DISTRIUTION DEVICE 8 I: 60 MO  IN OXYGEN MASK CONTAINERS.  N DI 15 DETAILED INSPECTION OF CONTINOUS FLOW OXYGEN MASKS. 8 I: 72 MO  N OP 16 OPERATIONAL CHECK OF CABIN OXYGEN SYSTEM CONTROL AND 8 I: 48 MO  REDUNDANCY FUNCTIONS.  N FC 17 REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL 6,8 I: 60 MO  CHECK.  N OP 18 CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN 8 I: 2000 FH  FILL PANEL AND GAUGES ON OXYGEN CYLINDERS.  35.20.01 PASSENGER OXYGEN (CHEMICAL)  R FC 01 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE 9 I: 4 C  R DI 02 DETAILED INSPECTION OF OXYGEN MASKS 9 I: 4 C  NOTE 27  R 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.20.01 * * * * * C O N T I N U E * * * * *  R VC 04 VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS 8 I: 6 YE  OF DISCHARGE  R 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)  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R FC 01 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6 I: NR OR VR  FUNCTIONAL CHECK OF PRESSURE REDUCER NOTE 8  NOTE 24  R VC 02 CROSS-CHECK OF QUANTITY INDICATIONS ON ECAM 8 I: 1400 FH  "DOOR/OXY"-PAGE, OXYGEN FILL PANEL AND OXYGEN  CYLINDERS  R FC 03 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION 8 I: 18 MO  R OP 04 OPERATIONAL CHECK OF THE SYSTEM SHUT-OFF VALVES 8 I: 18 MO  (MOD.40257)/ PRESSURE REGULATORS (MOD.52485/56322)  OPENING.  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R 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).  R OP 07 OPERATIONAL CHECK OXYGEN CONTAINER OPENING AND VENT 8 I: 30 MO  FUNCTION OF BLEED/VENT VALVE NOTE 24  R FC 08 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY 8 I: 30 MO  CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEM NOTE 24  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R 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  NOTE 24  R OP 11 OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICES 8 I: 60 MO  IN OXYGEN MASK CONTAINERS  R FC 12 REMOVE RISER LINE SHUT-OFF VALVES FOR FUNCTIONAL 8 I: 60 MO  CHECK NOTE 24  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.20.02 * * * * * C O N T I N U E * * * * *  R OP 13 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM 8 I: 60 MO  NOTE 24  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  NOTE 24  R FC 16 REMOVE PRESSURE REGULATOR FOR PRESSURE REGULATING 8 I: 60 MO  AND LEAKAGE TEST IN THE SHOP NOTE 24  R OP 17 OPERATIONAL CHECK OF CYLINDER VALVE SWITCH 9 I: 4 C  35.30.00 PORTABLE OXYGEN  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  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 35.30.00 * * * * * C O N T I N U E * * * * *  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 INSPECTION OF THE OXYGEN CONTINOUS FLOW MASK 9 I: 24 MO  N FC 07 REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR 9 I: VR  HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OR  OXYGEN REGULATOR. NR  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OXYGEN SECTION: C-35 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 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: 6400 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.  R DI 06 REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION 6 I: 10000 FH  R DI 07 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: C  08 TASK RESERVED  09 TASK RESERVED  10 TASK RESERVED  11 TASK RESERVED  N DI 12 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: 10000 FC  * * * * * E N D * * * * *  ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 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  38.10.01 POTABLE WATER  N RS 01 DISINFECTION OF POTABLE WATER SYSTEM. 9 I: 3 MO  OR  NR  N DS 02 DISCARD WATER FILTER CARTRIDGE. 9 I: 3 MO  OR  NR  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 38.10.01 * * * * * C O N T I N U E * * * * *  N DS 03 DISCARD AIR MANIFOLD FILTER. 9 I: 40000 FH  N RS 04 RESTORATION, BY CLEANING OF COMPRESSOR AIR INLET 9 I: 25000 FH  FILTER. OR  72 MO  N DS 05 DISCARD COMPRESSOR OUTLET AIR FILTER. 9 I: 40000 FH  38.31.00 TOILET SYSTEM  01 TASK DELETED  R GVI 02 GENERAL VISUAL INSPECTION OF WASTE TANKS AND WASTE 9 I: 4 C ZL-17 DRAIN LINES  R DS 03 DISCARD WATER SEPARATOR. 9 I: 4 A  NOTE 1  R RS 04 CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING 6 I: 350 FH  AGENT AND CRUSHED ICE. NOTE 1  R RS 05 CLEANING OF LIQUID LEVEL SENSORS, WASTE TANKS AND 6,9 I: C  WASTE DRAIN LINES.  R RS 06 CLEANING OF FILTER OF POLAR CAP ASSY 9 I: 4 A  NOTE 1  R RS 07 CLEANING OF RINSE NOZZLES AND REFERENCE PRESSURE LINE 7,9 I: 4 A  OF LIQUID LEVEL TRANSMITTER. NOTE 1  N 08 TASK RESERVED  N 09 TASK RESERVED  N 10 TASK RESERVED  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 38.31.00 * * * * * C O N T I N U E * * * * *  N 11 TASK RESERVED  N 12 TASK RESERVED  N OP 13 OPERATIONAL CHECK OF BIDET ́S SPRAY NOZZLE. 9 I: 600 FH  NOTE 1  38.31.01 TOILET SYSTEM  N DI 01 DETAILED INSPECTION OF FLUSH NIPPLE CAP AND THE 9 I: 24 MO  OVERFLOW PORT CAP.  N DI 02 DETAILED INSPECTION OF WASTE CAP DRAIN VALVE. 6 I: 24 MO  N RS 03 CLEANING OF FILTER ELEMENT OF WASHBASIN SINK DRAIN 9 I: 2000 FH  ASSEMBLY. NOTE 1  38.32.00 WASTE WATER DRAIN  R GVI 01 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN 9 I: 4 C ZL-13 LINES IN BILGE AREA FOR LEAKAGE. ZL-15 ZL-15 ZL-17 R GVI 02 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN 9 I: 8 C ZL-13 LINES IN CARGO COMPARTMENTS FOR LEAKAGE. ZL-15 ZL-16 ZL-16 * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 38.32.00 * * * * * C O N T I N U E * * * * *  R RS 03 CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE 7 I: 600 FH  38.40.00 AIR SUPPLY  R DI 01 DETAILED INSPECTION OF COMPRESSOR INLET FILTER 9 I: 2 C  R DS 02 DISCARD SYSTEM FILTER ELEMENT 6,9 I: 4 C  R 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 

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A330 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 

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A330 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 

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A330 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 RESERVED  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  49.26.00 ACCESSORY DRIVE GEARBOX  NO TASK SELECTED  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-49 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 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  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)  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-49 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 49.62.00 * * * * * C O N T I N U E * * * * *  R 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.  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-49 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

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A330 MRB REPORT – Systems and Powerplant Section

 52.00.00 DOORS  52.10.00 PASSENGER/CREW DOORS  R 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  R 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  R 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  FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MO  SLIDER.  N LU 10 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 6,9 I: C  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 52.10.00 * * * * * C O N T I N U E * * * * *  HANDLE.  NOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. INTERVAL FOR  ANY DOOR INFREQUENTLTY USED IS 18 MO.  N OP 11 OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN 6,9 I: C  POSITION.  NOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. INTERVAL FOR  ANY DOOR INFREQUENTLTY USED IS 18 MO.  N FC 12 FUNCTIONAL CHECK OF LOCKING MECHANISM. 6,9 I: 2 C  NOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USED  REGULARLY DURING DAY TO DAY OPERATION. INTERVAL FOR  ANY DOOR INFREQUENTLTY USED IS 36 MO.  52.22.00 PASSENGER COMPARTMENT EMERGENCY EXIT  R 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  R LU 02 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 8 I: 18 MO  HANDLE  R 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  R OP 04 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 C  IS OPENED FROM OUTSIDE  R FC 05 FUNCTIONAL CHECK OF LOCKING MECHANISM 8 I: 36 MO  R OP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 C  LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR IS  OPEN  * * * * * 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 

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A330 MRB REPORT – Systems and Powerplant Section

 52.22.00 * * * * * C O N T I N U E * * * * *  R GVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-83 R VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 C  FITTINGS  R FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MO  SLIDER.  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  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 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 LU 03 LUBRICATION OF BULK CARGO COMPARTMENT DOOR COMPONENTS 6 I: C  52.36.00 CARGO COMPARTMENT DOOR HYDRAULIC SYSTEM  NO TASK SELECTED  52.38.00 MAIN DECK CARGO COMPARTMENT DOOR  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 52.38.00 * * * * * C O N T I N U E * * * * *  N LU 01 LUBRICATION OF DOOR HINGE. 9 I: 24 MO  N FC 02 FUNCTIONAL CHECK OF LATCHING AND LOCKING MECHANISM. 6,9 I: 72 MO  N VC 03 VISUAL CHECK OF DRAIN VALVES. 9 I: 72 MO  N GVI 04 GENERAL VISUAL INSPECTION OF GUIDE FITTING. 9 I: 24 MO ZL-83 N GVI 05 GENERAL VISUAL INSPECTION OF DOOR STOP BOLTS. 9 I: 24 MO ZL-83 N GVI 06 GENERAL VISUAL INSPECTION OF DOOR SEAL AND RETAINER 9 I: 24 MO ZL-83 PROFILE.  N LU 07 LUBRICATION OF LATCHING MECHANISM, LOCKING MECHANISM, 6,9 I: 18 MO  SEQUENCE SHAFT AND INTERLOCK MECHANISM.  52.41.11 AVIONICS COMPARTMENT FWD DOOR  GVI 01 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-81 52.51.11 COCKPIT DOOR  R FC 01 FUNCTIONAL CHECK OF SPRING LOADED DOOR STOP MECHANISM 9 I: 2 C  R DI 02 DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR 6,9 I: 2 C  LOCKING SYSTEM  R 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  * * * * * 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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 52.51.11 * * * * * C O N T I N U E * * * * *  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  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 

RE

A330 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 AND IN CARGO COMPARTMENT DOORS).  07 TASK RESERVED  08 TASK RESERVED  OP 09 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT BULK 9 I: C  CARGO COMPARTMENT DOOR (FROM OUTSIDE).  N VC 10 VISUAL CHECK OF DRAIN FUNNEL(S) IN BARRIER WALL. 9 I: 4 C  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE SECTION: C-53 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  54.00.00 NACELLES/PYLONS  54.59.00 PYLON DRAINS (PW 4000)  R OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 C  F AND OF HYDRAULIC AND FUEL PAN DRAIN SYSTEM  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 PW 400
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  54.00.00 NACELLES/PYLONS  54.59.00 PYLON DRAINS (GE CF6-80E1)  OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 C  F AND OF HYDRAULIC AND FUEL PAN DRAIN SYSTEM  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 CF6-80
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  54.00.00 NACELLES/PYLONS  54.59.00 PYLON DRAINS (RR TRENT 768/772)  OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 C  F DRAIN SYSTEM  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 T700 
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 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 

RE

A330 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 

RE

A330 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 DRAIN 9 I: 4 C  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 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  71.00.00 POWERPLANT  71.10.00 ENGINE COWLING  DI 01 DETAILED INSPECTION OF AIR INTAKE COWL INNER BARREL 9 I: C  ASSEMBLY  02 TASK DELETED  03 TASK DELETED  GVI 04 GENERAL VISUAL INSPECTION OF FIRESHIELD, FIRE SEALS 8 I: 18 MO  AND HEAT BLANKETS  FC 05 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 9 I: C  71.70.00 POWERPLANT DRAINS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  72.00.00 ENGINE  72.20.00 FAN SECTION  DI 01 DETAILED INSPECTION OF FAN BLADES AND SPINNER 6 I: 4500 FH  DS 02 DISCARD LIFE LIMITED PARTS OF LP COMPRESSOR 5 I: NOTE 4  DI 03 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FH  (COVERED BY MSI 79-20-00, TASK NO2)  72.30.00 HP COMPRESSOR SECTION  DS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4  DI 02 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FH  (COVERED BY MSI 79-20-00, TASK NO2)  72.40.00 COMBUSTION SECTION  NO TASK SELECTED  72.50.00 TURBINE SECTION  SDI 01 BORESCOPE INSPECTION OF STAGE 1 AND STAGE 2 HP 6 I: 500 FC  TURBINE BLADES  NOTE: OPERATOR SHOULD CONTACT THE OEM TO ADJUST THE  INTERVAL FOR LOW FLIGHT LENGTH  DS 02 DISCARD LIFE LIMITED PARTS OF HPT AND LPT ROTORS 5 I: NOTE 4  DI 03 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FH  (COVERED BY MSI 79-20-00, TASK NO2)  72.60.00 ACCESSORY DRIVE SECTION  DI 01 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FH  (COVERED BY MSI 79-20-00, TASK NO2)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  73.00.00 ENGINE FUEL AND CONTROL  73.00.00 ENGINE FUEL AND CONTROL GENERAL  DS 01 DISCARD FUEL FILTER 9 I: 6000 FH  02 TASK DELETED  03 TASK DELETED  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).  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  74.00.00 IGNITION  74.00.00 IGNITION GENERAL  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 IGNITION SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  75.00.00 AIR  75.00.00 AIR GENERAL  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  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-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  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-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  78.00.00 EXHAUST  78.11.00 COLLECTOR/NOZZLE  NO TASK SELECTED  78.31.00 THRUST REVERSER CONTROL/ACTUATION SYSTEM  RS 01 REMOVE AND REPACK ANGLE GEARBOX 6 I: 6000 FC  LU 02 LUBRICATE FLEXIBLE DRIVE SHAFTS 6 I: C  LU 03 LUBRICATE BALLSCREW ACTUATORS 6 I: 1000 FC  FC 04 HOLDING TORQUE CHECK OF THE CDU CONE BRAKE 9 I: 4 C  NOTE 24  DI 05 DETAILED INSPECTION OF TRANSCOWL INNER BONDMENT SEAL 9 I: 4 C  AND MATING SURFACES (FORWARD FAIRING AND AFT FRAME NOTE 24  ASSEMBLY)  FC 06 HOLDING TORQUE CHECK OF THE THRUST REVERSER 9 I: 7000 FH  ELECTROMECHANICAL BRAKE NOTE 24  FC 07 THRUST REVERSER DIRECTIONAL PILOT VALVE LEAK CHECK 9 I: 7000 FH  78.32.00 THRUST REVERSER ASSEMBLY  VC 01 VISUAL CHECK OF THE BLOCKER DOORS, HINGES AND 9 I: C  ADJACENT STRUCTURE WITH T/R DEPLOYED  VC 02 VISUAL CHECK OF FAN REVERSER DEFLECTORS WITH T/R 9 I: C  DEPLOYED  03 TASK DELETED  04 TASK DELETED  05 TASK DELETED  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 78.32.00 * * * * * C O N T I N U E * * * * *  GVI 06 GENERAL VISUAL INSPECTION OF REVERSER 8 I: 18 MO  FIRESHIELD/SEALS  GVI 07 GENERAL VISUAL INSPECTION OF FIRE PROTECTION COATING 8 I: 18 MO  GVI 08 GENERAL VISUAL INSPECTION OF FAN EXIT FLOWPATH 9 I: C ZL-41 SURFACES  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  79.00.00 OIL  79.11.00 OIL SYSTEM STORAGE  NO TASK SELECTED  79.20.00 DISTRIBUTION  DS 01 DISCARD OIL SCAVENGE FILTER ELEMENT 6 I: C  DI 02 CHECK THE MASTER CHIP DETECTOR FOR PARTICLES 6 I: 1000 FH  (THIS TASK COVERS TASKS 72.20.00/03-G6,  72.30.00/02-G6, 72.50.00/03-G6, 72.60.00/01-G6)  79.31.00 OIL QUANTITY INDICATING 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  NO TASK SELECTED  79.35.00 OIL FILTER CLOGGING WARNING SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-CF6-80E-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 CF6-80E  80.00.00 STARTING  80.00.00 ENGINE STARTING SYSTEM  SV 01 STARTER OIL CHANGE 6 I: 1600 FH  OR  800 FC  DI 02 STARTER OIL LEVEL CHECK 6 I: A  DI 03 INSPECTION OF STARTER CHIP DETECTOR 6 I: 1600 FH  OR  800 FC  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STARTING SECTION: C-CF6-80E-8
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  71.00.00 POWERPLANT  71.13.00 FAN COWL  DI 01 DETAILED INSPECTION OF AIR INTAKE COWL LIP AND INNER 9 I: C  SKIN  02 TASK DELETED  03 TASK DELETED  FC 04 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 8 I: 18 MO  71.70.00 POWERPLANT DRAINS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  72.00.00 ENGINE  72.31.00 LOW PRESSURE COMPRESSOR GROUP  DI 01 DETAILED INSPECTION OF FAN BLADES 6 I: 2100 FH  02 TASK DELETED  DS 03 DISCARD FAN HUB AND LPC DRUM ROTOR 5 I: NOTE 4  04 TASK TRANSFERED TO MSI 72.32.00/01  DI 05 DETAILED INSPECTION OF INLET CONE 6 I: 4 A  72.32.00 LPC/LPT COUPLING GROUP  DS 01 DISCARD LPC/LPT COUPLING 5 I: NOTE 4  72.33.00 FAN CASES GROUP  GVI 01 GENERAL VISUAL INSPECTION OF FAN CASE RUB STRIP FOR 9 I: 4 A ZL-40 DAMAGE  GVI 02 GENERAL VISUAL INSPECTION OF FAN CASE, ACOUSTIC 9 I: C ZL-41 LINERS AND FAN EXIT GUIDE VANES  72.34.00 INTERMEDIATE CASE GROUP  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: A  (COVERED BY MSI 79.20.00, TASK NO1)  72.35.00 HIGH PRESSURE COMPRESSOR GROUP  DS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4  72.41.00 DIFFUSER, COMBUSTION & TURBINE NOZZLE GROUP  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 72.41.00 * * * * * C O N T I N U E * * * * *  SDI 01 BORESCOPE INSPECTION OF INNER AND OUTER COMBUSTION 9 I: 700 FC  CHAMBER ASSEMBLIES AND FIRST STAGE VANES OR  2400 FH  DI 02 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: A  (COVERED BY MSI 79.20.00, TASK NO1)  72.52.00 HIGH PRESSURE TURBINE GROUP  SDI 01 BORESCOPE INSPECTION OF THE FIRST AND SECOND STAGE 6 I: 700 FC  HIGH PRESSURE TURBINE BLADES OR  2400 FH  DS 02 DISCARD LIFE LIMITED PARTS OF HP TURBINE 5 I: NOTE 4  72.53.00 LOW PRESSURE TURBINE GROUP  DS 01 DISCARD LIFE LIMITED PARTS OF LP TURBINE 5 I: NOTE 4  72.54.00 TURBINE EXHAUST SECTION  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: A  (COVERED BY MSI 79.20.00, TASK NO1)  72.61.00 MAIN GEARBOX SECTION  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: A  (COVERED BY MSI 79.20.00, TASK NO1)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  73.00.00 ENGINE FUEL AND CONTROL  73.10.00 FUEL DISTRIBUTION  DS 01 DISCARD FUEL FILTER ELEMENT 6 I: 5000 FH  73.20.00 FUEL CONTROL  NO TASK SELECTED  73.25.00 FADEC FUNCTIONAL INTERFACE  OP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 C  SYSTEM  (COVERED BY MSI 21.26.00 TASK NO2)  73.30.00 FUEL INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  74.00.00 IGNITION  74.00.00 ENGINE IGNITION  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 IGNITION SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  75.00.00 AIR  75.20.00 ACCESSORY COOLING SYSTEM  NO TASK SELECTED  75.30.00 COMPRESSOR CONTROL SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  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-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  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-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  78.00.00 EXHAUST  78.31.00 THRUST REVERSER CONTROL AND INDICATING SYSTEM  NO TASK SELECTED  78.32.00 THRUST REVERSER STRUCTURE  GVI 01 GENERAL VISUAL INSPECTION OF CASCADES AND BLOCKER 9 I: C ZL-41 DOOR ATTACHMENTS  GVI 02 GENERAL VISUAL INSPECTION OF TRANSLATING COWL FORWARD 9 I: C ZL-41 SEAL.  GVI 03 GENERAL VISUAL INSPECTION OF FIXED STRUCTURE SEALS 8 I: 18 MO  GVI 04 GENERAL VISUAL INSPECTION OF FIRE BLANKET 8 I: 18 MO  78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  79.00.00 OIL  79.10.00 OIL SYSTEM STORAGE  NO TASK SELECTED  79.20.00 ENGINE OIL SYSTEM DISTRIBUTION  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: A  (THIS TASK COVERS TASKS 72.34.00/01-PW,  72.41.00/02-PW, 72.54.00/01-PW, 72.61.00/01-PW)  79.30.00 ENGINE OIL SYSTEM INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-PW 4000-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 PW 4000  80.00.00 STARTING  80.00.00 ENGINE STARTING SYSTEM  01 TASK DELETED  SV 02 CHANGE STARTER OIL 6 I: 600 FH  DI 03 INSPECT STARTER CHIP DETECTOR FOR PARTICLES 6 I: 600 FH  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STARTING SECTION: C-PW 4000-8
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  71.00.00 POWERPLANT  71.12.00 FAN COWL  01 TASK DELETED  02 TASK DELETED  GVI 03 GENERAL VISUAL INSPECTION FOR THE PRESENCE AND 9 I: C ZL-41 SECURITY OF FAN COWL DOORS ZONE 1/AMBIENT SEALS  FC 04 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 8 I: 18 MO  71.61.00 AIR INTAKE COWL  GVI 01 GENERAL VISUAL INSPECTION OF THE AIRWASHED SURFACES 9 I: 4 A  FOR DISTORTION AND SECURITY OF INSTALLATION  GVI 02 GENERAL VISUAL INSPECTION FOR THE PRESENCE AND 9 I: C ZL-41 SECURITY OF NOSE COWL SEAL  71.71.00 POWERPLANT DRAINS  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  72.00.00 ENGINE  72.03.00 GAS GENERATOR FAIRINGS  GVI 01 GENERAL VISUAL INSPECTION FOR SIGNIFICANT FAIRING 9 I: C ZL-41 DAMAGE AND/OR MISSING PANELS  72.31.00 LP COMPRESSOR MODULE  DI 01 DETAILED INSPECTION OF LP COMPRESSOR BLADES 6 I: 2 A  DS 02 DISCARD LIFE LIMITED PARTS OF THE LP COMPRESSOR 5 I: NOTE 4  LU 03 RE-LUBRICATION OF LP COMPRESSOR BLADE ROOT COATINGS 6 I: 1200 FC  72.32.00 IP COMPRESSOR MODULE  DS 01 DISCARD LIFE LIMITED PARTS OF THE IP COMPRESSOR 5 I: NOTE 4  (THIS TASK COVERS TASK 72-33-00/01-RR)  72.33.00 COMPRESSOR INTERMEDIATE MODULE  DS 01 DISCARD LIFE LIMITED PARTS OF THE IP COMPRESSOR 5 I: NOTE 4  (COVERED BY MSI 72-32-00, TASK NO1)  DI 02 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FH  ABNORMAL DEPOSITS  (COVERED BY MSI 79-20-00, TASK NO1)  03 TASK DELETED  DI 04 DETAILED INSPECTION OF EMCD 6 I: 130 FH  (COVERED BY MSI 79-30-00, TASK NO2)  72.33.40 EXTERNAL GEARBOX DRIVE  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 72.33.40 * * * * * C O N T I N U E * * * * *  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FH  ABNORMAL DEPOSITS  (COVERED BY MSI 79-20-00, TASK NO1)  DI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FH  (COVERED BY MSI 79-30-00, TASK NO2)  72.34.00 LP COMPRESSOR CASING  GVI 01 GENERAL VISUAL INSPECTION OF THE FAN TRACK AND COLD 9 I: 1000 FH  STREAM DUCT, AS FAR AS VISIBLE FROM THE FRONT, FOR  SIGNIFICANT DAMAGE  GVI 02 GENERAL VISUAL INSPECTION OF THE SPLITTER FAIRING 9 I: 4 A  FOR SIGNIFICANT DAMAGE  72.41.00 COMBUSTION SECTION  SDI 01 BORESCOPE INSPECTION OF COMBUSTION LINER 9 I: 1500 FC  OR  6000 FH  72.41.20 HP COMPRESSOR SECTION  DS 01 DISCARD LIFE LIMITED PARTS OF THE HP COMPRESSOR 5 I: NOTE 4  72.41.50 HP TURBINE SECTION  SDI 01 BORESCOPE INSPECTION OF HP TURBINE NOZZLE GUIDE VANES 6 T: 2000 FC  OR  8500 FH  I: 1500 FC  OR  6000 FH  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 72.41.50 * * * * * C O N T I N U E * * * * *  SDI 02 BORESCOPE INSPECTION OF HP TURBINE BLADES 6 T: 2000 FC  OR  8500 FH  I: 1500 FC  OR  6000 FH  DS 03 DISCARD LIFE LIMITED PARTS OF THE HP TURBINE 5 I: NOTE 4  72.51.00 IP/LP TURBINE MODULE  DS 01 DISCARD LIFE LIMITED PARTS OF THE IP TURBINE 5 I: NOTE 4  72.52.00 LP TURBINE MODULE  DS 01 DISCARD LIFE LIMITED PARTS OF THE LP TURBINE 5 I: NOTE 4  72.61.00 EXTERNAL GEARBOX MODULE  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FH  ABNORMAL DEPOSITS  (COVERED BY MSI 79-20-00, TASK NO1)  DI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FH  (COVERED BY MSI 79-30-00, TASK NO2)  72.62.11 QUILLSHAFT AND SHROUD  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  73.00.00 ENGINE FUEL AND CONTROL  73.10.00 FUEL DISTRIBUSTION  DS 01 DISCARD LP FUEL FILTER ELEMENT 9 I: 6000 FH  73.20.00 FUEL CONTROL  NO TASK SELECTED  73.25.00 FADEC 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 FUEL INDICATING  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  74.00.00 IGNITION  74.00.00 IGNITION SYSTEM  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 IGNITION SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  75.00.00 AIR  75.21.00 ACCESSORY/ZONE COOLING  NO TASK SELECTED  75.22.00 ENGINE COOLING AND SEALING  NO TASK SELECTED  75.23.00 BEARING COMPARTMENT COOLING  NO TASK SELECTED  75.24.00 TURBINE CASE COOLING  NO TASK SELECTED  75.33.00 IP/HP COMPRESSOR AIRFLOW CONTROL  NO TASK SELECTED  75.41.00 NACELLE TEMPERATURE INDICATION  NO TASK SELECTED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 AIR SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  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 T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  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 T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  78.00.00 EXHAUST  78.11.00 EXHAUST COLLECTOR/NOZZLE  VC 01 VISUAL CHECK OF THE FIRE SEALS 8 I: 1600 FH  78.31.00 THRUST REVERSER CONTROL AND INDICATION  NO TASK SELECTED  78.32.00 THRUST REVERSER STRUCTURE  GVI 01 GENERAL VISUAL INSPECTION OF THE FAN EXIT FLOW PATH 9 I: C ZL-41 SURFACES  02 TASK DELETED  03 TASK DELETED  GVI 04 GENERAL VISUAL INSPECTION OF THE ZONE 1/AMBIENT FIRE 8 I: 18 MO  SEAL  VC 05 VISUAL CHECK OF THE INNER FIXED STRUCTURE FIRE SEALS 8 I: 18 MO  GVI 06 GENERAL VISUAL INSPECTION OF THE PIVOT DOOR 9 I: 6000 FH  DEFLECTOR PLATES, MOVEABLE PANELS AND MECHANISM  (THRUST REVERSER DEPLOYED)  GVI 07 GENERAL VISUAL INSPECTION OF FRONT FRAME AND INNER 9 I: 2 A  FIXED STRUCTURE THERMAL BLANKETS  OP 08 OPERATIONAL CHECK OF THE SECONDARY AND TERTIARY LOCKS 9 I: 2 C  (THIS TASK COVERS TASK 78.37.00/01-RR)  09 TASK DELETED  78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEM  OP 01 OPERATIONAL CHECK OF THE TERTIARY LOCKS 9 I: 2 C  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 78.37.00 * * * * * C O N T I N U E * * * * *  (COVERED BY 78.32.00, TASK NO8)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  79.00.00 OIL  79.10.00 OIL SYSTEM STORAGE  NO TASK SELECTED  79.20.00 OIL DISTRIBUTION  DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FH  ABNORMAL DEPOSITS  (THIS TASK COVERS TASK 72.33.00/02-RR,  72.33.40/01-RR, 72.61.00/01-RR)  RS 02 REMOVE, CLEAN AND REINSTALL PRESSURE OIL FILTER 6 I: 1600 FH  ELEMENT  DS 03 REMOVE, DISCARD AND REPLACE OIL SCAVENGE FILTER 9 I: 1600 FH  79.30.00 OIL INDICATING SYSTEM  RS 01 CLEANING AND FUNCTIONAL CHECK OF EMCD 6,9 I: 2500 FH  DI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FH  (THIS TASK COVERS TASKS 72.33.00/04-RR,  72.33.40/02-RR, 72.61.00/02-RR)  * * * * * E N D * * * * *  ISSUE: JUL 01/10 OIL SECTION: C-RR T700-7
 MSI 

 REFERENCE TASK MSI AND TASK DESCRIPTION FEC INTERVAL 

RE

A330 MRB REPORT – Systems and Powerplant Section

 RR T700  80.00.00 STARTING  80.11.00 PNEUMATIC STARTING  SV 01 STARTER OIL CHANGE AND INSPECTION OF STARTER CHIP 6,9 I: A  DETECTOR  SV 02 STARTER OIL REPLENISHMENT 6,9 I: 400 FH  * * * * * E N D * * * * *  ISSUE: JUL 01/10 STARTING SECTION: C-RR T700-8
A330 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, post 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. 
A330 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 as fully covered by the Zonal (ZIP) task 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 Section. 

 
A330 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 534148-01-2 

 Fatigue or corrosion tasks where accidental damage is likely, are not selected for 

 sampling. These tasks have a 100% threshold only. e.g. SSI 534146-01-1 

 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 534127-01-1 

 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 inspected at the 100% threshold. 

 e.g. 533106-01-1 

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. 545126-02-1 

 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. 574804-02-4 

 

 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 current inspection program continues to apply. 

 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 

operator's A330 aircraft. 

 The oldest aircraft are defined as the aircraft with the highest age in years since their initial 

manufacturer's delivery date. 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-4

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 33a aircraft 

and 1/5 of the oldest Group 33b 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 

 SSIs are shown on the following pages. 

 The Sampling Program aircraft should first be selected before the subsequent planning of the SSI 

 details. 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-5

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr 3000 FH/Yr 

S.T = 50000 FH 

= Aircraft Inspection

I= 6100 FC

10Yrs 15Yrs 20Yrs 2

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICA

572011-02-1 DI 20000 FC

OR

50000 FH

6100 FC

OR

24500 FH

GRP 

572011-02-2 DI 20000 FC

OR

50000 FH

5700 FC

OR

17800 FH

GRP 

O

GRP 

572011-02-3 DI 20000 FC

OR

50000 FH

6000 FC

OR

18800 FH

GRP 

Example 1 : SSI 572011 

12 32A 11 32A 10 32A 9 32A 8 32A 7 32A 6 32A 5 32A 4 32A 3 32A 2 32A 1 32A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-6

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr 3000 FH/Yr 

S.T = 50000 FH

= Aircraft Inspection

I= 5700 FC

I= 6100 FC

10Yrs 15Yrs 20Yrs 2

Example 2 : SSI 572011 

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICA

572011-02-1 DI 20000 FC

OR

50000 FH

6100 FC

OR

24500 FH

GRP 

572011-02-2 DI 20000 FC

OR

50000 FH

5700 FC

OR

17800 FH

GRP 

O

GRP 

572011-02-3 DI 20000 FC

OR

50000 FH

6000 FC

OR

18800 FH

GRP 

12 32B 11 32B 10 32B 9 32B 8 32B 7 32B 6 32B 5 32A 4 32A 3 32A 2 32A 1 32A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-7

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr 3000 FH/Yr 

= Aircraft Inspection

100% T= 25800 FC

10Yrs 15Yrs 20Yrs 25

Example 3 : SSI 531134 

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICAB

531134-01-1 SDI 20000 FC 35400 FC 7000 FC531134-01-2 SDI 20000 FC 25800 FC 3500 FC GRP 3

OR

GRP 3

GRP 3

OR

GRP 3

S.T = 20000 FC I = 3

12 32A 11 32A 10 32A 9 32A 8 32A 7 32A 6 32A 5 32A 4 32A 3 32A 2 32A 1 32A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-8

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 950 FC/Yr 3000 FH/Yr 

= Aircraft Inspection

I= 7500 FC

10Yrs 15Yrs 20Yrs 25

Example 4 : SSI 533135 

TASK REF Level

SAMPLE 

THRESHOL

100% 

THRESHOL

INTERVAL APPLICA

535103-01-1 DI 10 YE

OR

16500 FC

20 YE 10 YE

OR

7500 FC

A

S.T = 10 Yrs 100% T= 16500 FC

12 33B 11 33B 10 33B 9 33B 8 33B 7 33B 6 33B 5 33A 4 33A 3 33A 2 33A 1 33A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-9

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr 3000 FH/Yr 

T= 12100 FC

= Aircraft Inspection

Example 5 : SSI 533154 

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

I= 8100 FC

10Yrs 15Yrs 20Yrs 25Y

TASK REF Level SAMPLE 100% THRESHOLD INTERVAL APPL

533154-01-4 DI 12100 FC 8100 FC GRP 33A

PRE 416ORGRP 33BPRE 416

533154-01-5 DI 20000 FC 13300 FC GRP 33A

POST 41ORGRP 33BPOST 41ORGRP 32AORGRP 33C

I

12 33A 11 33A 10 33A 9 33A 8 33A 7 33A 6 33A 5 33A 4 33A 3 33A 2 33A 1 33A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-10

Yrs, FC, FH

= Sampling Program Aircraft

= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr

 3000 FH/Yr 

T= 20000 FC

= Aircraft Inspection

Example 6 : SSI 533154 

10Yrs 15Yrs 20Yrs 25Y

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

TASK REF Level SAMPLE 100% THRESHOLD INTERVAL APPLI

533154-01-4 DI 12100 FC 8100 FC GRP 33A

PRE 4165ORGRP 33BPRE 4165

533154-01-5 DI 20000 FC 13300 FC GRP 33A

POST 416ORGRP 33BPOST 416ORGRP 32AORGRP 33C

T= 12100 FC I= 8100 FC I= 

12 33B 11 33B 10 33B 9 33B 8 33B 7 33B 6 33A 5 33A 4 33A 3 33A 2 33A 1 33A A/C Grp 
A330 MRB REPORT 

 Issue : July 2010 Page : D-INTRO-11

Yrs, FC, FH

= Sampling Program Aircraft= Aircraft Delivery

Aircraft Utilisation: 1100 FC/Yr 3000 FH/Yr 

T= 10 Yrs

= Aircraft Inspection

I= 6200 FC

Example 7: SSI 574109 

T= 15800 FC

100% T= 20000 FC

I= 8200 FC

10Yrs 15Yrs 20Yrs 2

TASK REF Level SAMPLE THRESHOL 100% THRESHOL INTERVAL EF

574109-02-1 DI 10 YE 20 YE

OR20000 FCOR50000 FH

10 YEOR8200 FC

OR29500 FH

GR

574109-02-2 DI 10 YE 20 YE

OR15600 FCOR49200 FH

10 YEOR6200 FC

OR19500 FH

GRORGR

574109-02-3 DI 10 YE 20 YE

OR20000 FCOR50000 FH

10 YEOR7900 FC

OR24900 FH

GR

I= 8200 FC

I= 6200 

12 33A 11 33A 10 33A 9 33A 8 33A 7 33A 6 33A 5 32A 4 32A 3 32A 2 32A 1 32A A/C Grp 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-12 

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 occuring 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. 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-13 

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. 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-14 

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. Where a task has more than one limit, e.g. 

one in FC and another in calendar time, the limit expiring first shall apply. 

 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. 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-15 

 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 A330 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) 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-16 

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: - deleted 

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 A330 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. 

 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 

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 25-3167 

12 Seals at Cabin Attendant Seat /NTF SB 25-3275 
A330 MRB REPORT 

Issue : July 2010 Page : D-INTRO-17 

 “Applicability” column. Refer to the details below: 

WV GROUPS A/C Series Weight Variants 

GROUP 32A A330-200 020, 021, 022, 023, 024, 

025, 026, 027 

GROUP 32E A330-200 050, 051, 052, 053, 054, 

055, 056, 059, 060 

GROUP 32F A330-200F 000, 001, 

GROUP 33A A330-300 000, 001, 002, 003, 004 

GROUP 33B A330-300 010, 011, 012, 013, 014 

GROUP 33C A330-300 020, 024, 025, 026, 027 

GROUP 33D A330-300 022 

GROUP 33E A330-300 050, 051, 052, 053, 

NOTE: Fatigue tasks for the A330-200F (WV GROUP 32F) will be included in a later revision of the 

 MRBR. 

INTERPRETATION

GROUP X Y Z

X : Aircraft Type 3 for A330 

Y : Model (2 for –200 / 3 for –300) 

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

EXAMPLES

GROUP 32A : A330-200 WV 020, 021, 022, 023, 024, 025, 026, 027 

(1st WV Group of A330-200 Series) 

 GROUP 33B : A330-300 WV 010, 011, 012, 013, 014 

 (2nd WV group of A330-300 Series)
 A330 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. 531109-01-1. It is composed of 9 or 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 A330 ATA 100 bre

section where the SSI is located e.g 53 Fuselage. The second set of two digits are also in accordance with the A330 ATA 100 breaksection where the SSI is located e.g 53-11 Fwd fuselage. The third set of two digits are sequential numbers within the section e.g 0

 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 either one or two digits. Numbers 1 to 9 have one digit; numbers 10 and subsequent have 2 Number and is separated by a dash, 531109-01-1. It identifies different applicability e.g aircraft series, mod status, WV group etc differentiate between minor access differences e.g. different access panel numbers. 

Applicability index Sequence number 

SSI number
 A330 MRB REPORT - Structures 

Issue : July 2010 

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

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. 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
 A330 MRB REPORT - Structures 

Issue : July 2010 

Applicability Task applicable to

ALL All A330 aircraft. A330-200 -200 PAX series aircraft onlyA330-200F -200 Freighter series only PRE nnnnn All A330 PRE MOD nnnnn. 

i.e. A330 that do not have MOD nnnnn embodied. 

POST nnnnn All A330 POST MOD nnnnn.

i.e. A330 that do have MOD nnnnn embodied. 

POST nnnnn Sxxxxx All A330 POST MOD nnnnn (at least with mod proposal no. Sxxxxx embodied). POST nnnnn POST mmmmm 

All A330 POST MOD nnnnn and POST MOD mmmmm. i.e. A330 that do have MOD nnnnn and MOD mmmmm embodied. 

A330-200 

OR A330-300 PRE nnnnn 

All A330-200 PAXOr, All A330-300 that do not have MOD nnnnn embodied. 

A330-200 POST nnnnn OR POST mmmm 

All A330-200 PAX that do have MOD nnnnn embodied, Or, All A330-200 PAX that do have MOD mmmm embodied. 

A330-200 POST nnnnn OR A330-300 POST nnnnn PRE mmmmm 

All A330-200 PAX that do have MOD nnnnn embodied, Or, All A330-300 that do have MOD nnnnn embodied and do not have MOD mmmmm embodied. 

POST nnnnn (xx-yyyy) 

All A330 that do have MOD nnnnn embodied.

(xx-yyyy) is the Service Bulletin reference associated to the modification. 

GE All A330 equipped with GE CF6-80 E1 engines. 
 A330 MRB REPORT - Structures 

Issue : July 2010 

Applicability Task applicable to

PW All A330 equipped with PW 4000 engines. RR All A330 equipped with RR Trent 700 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.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 

A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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 MEMBER T: 6 YE  741 I: 6 YE  321103-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG STATIC 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  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 ASSY T: 10 YE  741 PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY ATTACH I: 10 YE  PINS, ARTICULATING LINKAGE PINS, PITCH TRIMMER ATTACH  PINS, FORWARD PINTLE PINS AND SHORTENING LINKAGE PINS  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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 WING T: 10 YE  670 TRAILING EDGE I: 10 YE  321126-01-1 PINS 570 DETAILED INSPECTION OF MLG SHORTENING MECHANISM AT T: 10 YE  670 OUTER WING TRAILING EDGE I: 10 YE  321127-01-1 PINS 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE  670 OUTER WING TRAILING EDGE I: 10 YE  322101-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING (BARREL) T: 6 YE  I: 6 YE  322102-01-1 WHEELS AND SLEEVES, 711 DETAILED INSPECTION OF NLG SLIDING MEMBER T: 6 YE  SLIDING MEMBER FULLY I: 6 YE  EXTENDED  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 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 322107-01-1 PINS 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  * * * * * E N D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 521101-01-1 N/A TASK DELETED  521103-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD T: 6 YE  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 PASSENGER/CREW T: 6 YE 1  INSULATION 841 DOOR), INTERNAL STRUCTURE I: 6 YE  LINING  R 521201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 (MID T: 6 YE  PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE I: 6 YE  521201-01-2 N/A TASK DELETED  R 521202-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW T: 6 YE 1  ESCAPE SLIDE 842 DOOR), INTERNAL STRUCTURE I: 6 YE  INSULATION  LINING  521203-01-1 N/A TASK DELETED  521203-01-2 N/A TASK DELETED  R 521301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 (AFT T: 6 YE  PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE I: 6 YE  521301-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 521302-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW T: 6 YE 1  ESCAPE SLIDE 843 DOOR), INTERNAL STRUCTURE I: 6 YE  INSULATION  LINING  521303-01-1 N/A TASK DELETED  521303-01-2 N/A TASK DELETED  R 522201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE  (EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL I: 6 YE  SURFACE  522201-01-2 N/A TASK DELETED  R 522202-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1  ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YE  INSULATION  LINING  522203-01-1 N/A TASK DELETED  522203-01-2 N/A TASK DELETED  523101-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YE  R 523101-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FC  COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 3000 FC  R 523102-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT T: 12 YE 1  821CR 821DR DOOR, INTERNAL STRUCTURE I: 6 YE  LINING  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 523103-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF FORWARD T: 12000 FC  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  R 523105-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FC  FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A I: 8300 FC  523106-01-1 N/A TASK DELETED  523201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE  DOOR SKIN, EXTERNAL SURFACE I: 6 YE  R 523201-01-2 N/A 822 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 3000 FC  DOOR SKIN, EXTERNAL SURFACE I: 3000 FC  R 523202-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, T: 12 YE 1  822CR 822DR INTERNAL STRUCTURE I: 6 YE  LINING  R 523203-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF LATCHING HOOKS OF AFT CARGO T: 12000 FC  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  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 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  523301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE  DOOR SKIN, EXTERNAL SURFACE I: 6 YE  R 523301-01-2 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 550 FC  DOOR SKIN, EXTERNAL SURFACE I: 550 FC  523302-01-1 823 823 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR, T: 12 YE 1  LINING INTERNAL STRUCTURE I: 6 YE  523303-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK CARGO T: 12 YE 1  COMPARTMENT DOOR I: 12 YE  N 523801-01-1 N/A 835 GENERAL VISUAL INSPECTION OF MAIN DECK CARGO DOOR T: 12 YE  SKIN, EXTERNAL SURFACE. I: 12 YE  N 523802-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR, INTERNAL T: 12 YE 3  LINING INSULATION STRUCTURE, EXCLUDING SIDE FRAMES AND ACTUATOR FRAME. I: 12 YE  N 523803-01-1 835 835 DETAILED INSPECTION OF ACTUATOR ATTACH FITTINGS T: 12 YE 1  LINING INSULATION INCLUDING RIVETING AND BUSH. I: 12 YE  N 523804-01-1 835 835 DETAILED INSPECTION OF LOCKING MECHANISM, ATTACH T: 12 YE  MCD ACCESS PANELS FITTINGS AND SUPPORT STRUCTURE OF MAIN DECK CARGO I: 12 YE  DOOR AT ALL FRAMES.  N 523805-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR T: 12 YE  LATCHING HOOKS AND BOLTS. I: 12 YE  N 523806-01-1 835 835 DETAILED INSPECTION OF PIANO HINGE FITTING AND HINGE T: 12 YE  PIN. I: 12 YE  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 523807-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR SIDE T: 12 YE  LINING INSULATION FRAMES AND STOP FITTINGS. I: 12 YE  524101-01-2 N/A TASK DELETED  524101-02-3 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 LOWER T: 6 YE 1+2  DOOR FLOOR PANEL 122 ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS I: 6 YE  811 AND HINGE FITTINGS ON FUSELAGE  524103-01-2 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  DOOR FLOOR PANEL 122 AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS I: 14300 FC  811  524103-01-3 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  DOOR FLOOR PANEL 122 AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS. I: 14300 FC  811  528101-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, MAIN T: 3 YE  744 DOOR, EXTERNAL SKIN, LH/RH I: 3 YE  528102-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, MAIN T: 3 YE  744 DOOR, INTERNAL SKIN, LH/RH I: 3 YE  528103-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, T: 12 YE 1  744 FORWARD AND AFT FITTINGS, LH/RH I: 12 YE  528104-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 528104-01-2 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, T: 6 YE 1  744 CENTER FITTING AND SURROUNDING AREA (300 MM AROUND), I: 6 YE  LH/RH  NOTE: TPS APPLICATION REQUIRED ON FITTING ONLY  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  R 528203-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1  714 DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON I: 6 YE  FUSELAGE, LH/RH  528203-01-2 N/A TASK DELETED  528204-01-1 715 716 715 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, AFT T: 3 YE  716 DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH I: 3 YE  N 528206-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1  714 DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON I: 6 YE  FUSELAGE, LH/RH  N 528207-01-1 715 716 715 DETAILED INSPECTION OF NOSE LANDING GEAR AFT DOOR, T: 6 YE 1  716 HINGES (NO 4 & NO 5) INCLUDING FITTINGS ON FUSELAGE, I: 6 YE  LH/RH  * * * * * E N D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: D-52 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531101-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE T: 6 YE 3  RADOME OPENED BULKHEAD ATTACHED TO FR 1 I: 6 YE  531102-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL T: 6 YE  VISIBLE PORTIONS OF FRAMEWORK BETWEEN FR 3 AND FR 10, I: 6 YE  LH/RH  531103-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 6 YE  10 AND FR 18 FROM CABIN FLOOR LEVEL TO STR 9 (FWD AND I: 6 YE  AFT), EXTERNAL SURFACE, LH/RH  531104-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 12 YE  PORTIONS OF FRAMEWORK COVERED BY RETAINERS I: 12 YE  531105-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 6 YE  VISIBLE PORTIONS OF RETAINERS I: 6 YE  531106-01-3 N/A TASK DELETED  531106-01-4 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 AND T: 20000 FC  FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, I: 10200 FC  EXTERNAL SURFACE, LH/RH.  531106-01-5 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN T: 17000 FC  BETWEEN FR.9 AND FR.10A AT COCKPIT LATERAL WINDOW I: 10200 FC  LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 531107-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE  0 AND FR 10 FROM FLOOR LEVEL TO CROWN CENTERLINE, I: 3 YE  EXTERNAL SURFACE  531110-02-2 N/A TASK DELETED  R 531111-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE  10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 3 YE  CENTERLINE, EXTERNAL SURFACE, LH/RH  531112-01-1 N/A TASK DELETED  531112-02-1 N/A TASK DELETED  R 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  R 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  R 531116-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND JOINT T: 6 YE  SURFACES BETWEEN FR 0 AND FR 18/19 BELOW CABIN FLOOR I: 6 YE  LEVEL, EXTERNAL SURFACE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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  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 AVIONICS BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2  PANEL 122 BETWEEN FR 10 AND FR 20 BELOW AVIONICS COMPARTMENT I: 12 YE  FLOOR LEVEL  531122-01-1 AVIONICS 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 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.  531124-01-3 N/A TASK DELETED  531124-01-4 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531124-01-6 713 714 123 DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER T: 17000 FC  RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT I: 17000 FC  PANEL, LH/RH  531125-01-3 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 20000 FC  AVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH I: 5700 FC  PANELS  531125-01-4 N/A TASK DELETED  531125-01-5 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 17000 FC  AVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH I: 17000 FC  PANELS  531126-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AFT SIDE T: 12 YE 1  716 PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, LH/RH I: 12 YE  531127-01-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 20000 FC  716 STRUT FITTING LUG BORE I: 20000 FC  531127-01-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 20000 FC  716 STRUT FITTING LUG BORE I: 20000 FC  531127-01-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 17000 FC  716 DRAG STRUT FITTING LUG BORE I: 17000 FC  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  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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INTERVAL 

 TPS

 531129-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 20000 FC  716 ACTUATOR FITTING I: 4700 FC  BOLTS  NLG ACTUATOR  DISCONNECTED  531129-02-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 17000 FC  716 ACTUATOR FITTING I: 11500 FC  BOLTS  NLG ACTUATOR  DISCONNECTED  531130-01-2 N/A TASK DELETED  531131-01-2 N/A TASK DELETED  531131-02-2 N/A TASK DELETED  531132-01-2 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  122 FRAME 14 JOINT BETWEEN STRINGERS 28 AND 30 LEVEL, I: 12900 FC  LH/RH  531132-01-3 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  122 FRAME 14 JOINT BETWEEN STRINGERS 28 AND 30 LEVEL, LH/ I: 17000 FC  531133-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531133-01-4 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 17000 FC  NOTE 1 122 BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON I: 17000 FC  FRAME 12A AT STRINGER 26 LEVEL, LH/RH  531134-01-1 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  DOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 7000 FC  SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.  531134-01-2 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  DOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 3500 FC  SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.  531134-01-3 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  DOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 3500 FC  SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.  531134-01-4 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  DOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 17000 FC  SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.  531135-01-2 N/A TASK DELETED  531136-01-2 N/A TASK DELETED  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 PANEL I: 12 YE  531138-01-2 NOTE 1 110 DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD T: 20000 FC  PANELS RADOME OPENED FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 I: 9200 FC  ABOVE COCKPIT FLOOR LEVEL.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531138-01-3 NOTE 1 110 DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD T: 17000 FC  PANELS RADOME OPENED FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 I: 9200 FC  ABOVE COCKPIT FLOOR LEVEL.  531139-01-2 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 212 FORWARD PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND I: 9200 FC  UPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT  FLOOR LEVEL.  531139-01-3 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 212 PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND UPPER I: 9200 FC  SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT FLOOR  LEVEL  531140-01-1 N/A TASK DELETED  531141-01-2 N/A TASK DELETED  531142-01-2 CEILING PANELS 211 DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER T: 20000 FC  NOTE 1 212 BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, I: 5250 FC  SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  531142-02-2  531142-01-3 CEILING PANELS 211 DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER T: 17000 FC  NOTE 1 212 BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, I: 5250 FC  SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  531142-02-3  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531142-02-2 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED T: 20000 FC  NOTE 1 212 MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL I: 7800 FC  SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  531142-01-2  531142-02-3 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED T: 17000 FC  NOTE 1 212 MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL I: 7800 FC  SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  531142-01-3  531143-01-2 N/A TASK DELETED  531143-01-3 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 122 FLOOR BEAM AND CRUCIFORM FITTING AT FR.14, LH/RH I: 4000 FC  VACUUM PIPES  531144-01-2 N/A TASK DELETED  R 531144-01-3 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  NOTE 1 122 STRUCTURE, JUNCTION AREA BETWEEN FRAME 14 AND I: 7100 FC  TOILET CRUCIFORM FITTING, LH/RH.  531146-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 212 LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 I: 8750 FC  UPPER MEMBER, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531146-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 212 LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 I: 8750 FC  UPPER MEMBER, LH/RH.  531149-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 212 ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING I: 8500 FC  TOP 3 NUTS ON CENTRE POST.  531149-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 212 ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, I: 8500 FC  INCLUDING TOP 3 NUTS ON CENTRE POST  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 A VISIBLE  ND 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.  R 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 AND T: 12 YE T: 20 YE  NOTE 1 212 CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND I: 12 YE I: 12 YE  FORWARD).  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531154-01-2 N/A TASK DELETED  531154-01-3 LINING 211 DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING T: 17000 FC  NOTE 1 212 PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, I: 8100 FC  SLIDING WINDOWS INTERNAL STRUCTURE, LH/RH.  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 FR 1 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 BETWEEN  SIDEWALL PANELS 224 FWD COCKPIT AND FR 10,  - INTERNAL STRUCTURE AROUND DOOR 1 (FORWARD  PASSENGER/CREW DOOR)  531157-01-2 LINING 233 DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPER T: 20000 FC  NOTE 1 234 KEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL, I: 10170 FC  INTERNAL STRUCTURE, LH/RH.  531158-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 212 JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 I: 15600 FC  AND 9 UPPER MEMBERS, LH/RH.  531158-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 212 JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 I: 15600 FC  AND 9 UPPER MEMBERS, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531159-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2  NOTE 1 222 AROUND DOOR 1 (FORWARD PASSENGER/CREW DOOR), BETWEEN I: 6 YE  FR 13A AND FR 17 AND BETWEEN FLOOR LEVEL AND STR 9  (AFT), LH/RH.  531161-01-2 N/A TASK DELETED  531162-01-3 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS BEAM T: 20000 FC  COCKPIT FLOOR PANELS 212 ATTACHMENT AREA. I: 7800 FC  531162-01-4 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS BEAM T: 20000 FC  COCKPIT FLOOR PANELS 212 ATTACHMENT AREA. I: 7500 FC  531162-01-5 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS T: 17000 FC  COCKPIT FLOOR PANELS 212 BEAM ATTACHMENT AREA I: 17000 FC  531166-01-1 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  122 STRUCTURE, UPPER CORNERS OF PORTAL FRAME, FROM FRAMES I: 6400 FC  11A TO 16A, LH/RH.  531166-01-2 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  122 STRUCTURE, UPPER CORNERS OF PORTAL FRAME, FROM FRAMES I: 6200 FC  11A TO 16A, LH/RH.  531166-01-3 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  122 UPPER CORNERS OF PORTAL FRAME, FROM FRAMES 11A I: 9300 FC  TO 16A, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 531167-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND T: 6 YE  JOINT SURFACE BETWEEN FR.0 AND FR.18/19 BELOW I: 6 YE  CABIN FLOOR LEVEL, EXTERNAL SURFACE, EXCLUDING  AREA COVERED BY NOSE FAIRING.  N 531168-01-1 125CL 125DL 125EL 125 GENERAL VISUAL INSPECTION OF NOSE FORWARD T: 6 YE 1  125FL 125GL 125HL 126 FUSELAGE LOWER SKIN AND FAIRING SUBSTRUCTURE, I: 6 YE  126CR 126FR AREA COVERED BY NOSE FAIRING BETWEEN FR.17 AND  FR.22 INCLUDING AFT FACE OF LOWER FR.17 FITTING,  AND AFT FITTINGS, LH/RH.  N 531169-01-1 125AL 125BL 125LL 125 GENERAL VISUAL INSPECTION OF NOSE FORWARD T: 6 YE 1  126BR 126CR 713 126 FUSELAGE LOWER SKIN AND FAIRING SUBSTRUCTURE, I: 6 YE  714 AREA COVERED BY NOSE FAIRING BETWEEN FR.10 AND  FR.17, INCLUDING NLG BAY LATERAL PANEL EXTERNAL  SURFACE, FLAT PANEL, FR.16A AND FORWARD FACE OF  LOWER FR.17 FITTING, LH/RH.  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.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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 CABIN I: 6 YE  FLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL,  BETWEEN FR 13A AND FR 17, LH/RH  531175-01-3 N/A TASK DELETED  531175-01-4 LINING 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 17000 FC  NOTE 1 232 JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT I: 8000 FC  STGR.14/18/22/24, LH/RH.  531176-01-1 FWD AVIONICS BAY 121 GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE BELOW T: 6 YE 1+2  DOOR OPENED BATTERIES BETWEEN FR 10A AND 11A AND BETWEEN STR 41 I: 6 YE  NOTE 1 AND STR 43, LH  531180-01-1 N/A TASK DELETED  531183-01-1 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  LININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 10400 FC  NOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.  TOILETS  531183-01-3 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  LININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 9600 FC  NOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.  TOILETS  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531183-01-4 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FC  LININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 9600 FC  NOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.  TOILETS  531184-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 20000 FC  STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP I: 11100 FC  JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A AND  FROM FR.14 TO FR.16A, LH/RH.  531184-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 17000 FC  STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP I: 11100 FC  JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A  AND FROM FR.14 TO FR.16A, LH/RH  531185-01-2 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 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.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 531186-01-2 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  LININGS 224 CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF I: 10400 FC  NOTE 1 FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.  TOILETS  531186-01-3 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  LININGS 224 CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF I: 9600 FC  NOTE 1 FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.  TOILETS  531187-01-2 N/A TASK DELETED  531187-01-3 N/A TASK DELETED  531187-01-4 N/A TASK DELETED  531188-01-2 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7600 FC  FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9  FWD LEVEL, LH/RH.  531188-01-3 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7000 FC  FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9  FWD LEVEL, LH/RH.  531188-01-4 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FC  200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7000 FC  FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9  FWD LEVEL, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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 TPS

 531189-01-2 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERON I: 8850 FC  AT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B,  LH/RH  531189-01-3 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  NOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER I: 15200 FC  LONGERON AT STRINGER 12 LEVEL, BETWEEN FR. 13A  AND FR.13B, LH/RH  531192-01-3 N/A TASK DELETED  531192-01-4 N/A TASK DELETED  531194-01-3 N/A TASK DELETED  531194-01-4 N/A TASK DELETED  531198-01-2 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 20000 FC  NOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 8850 FC  BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH  531198-01-3 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 17000 FC  NOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 15200 FC  BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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 TPS

 532101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM I: 6 YE  CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS,  EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH  532101-01-2 N/A TASK DELETED  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 CARGO I: 6 YE  FLOOR PANELS 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 PANELS AND CARGO I: 12 YE  CEILINGS PANELS COMPARTMENT FLOOR FROM FR 20 TO FR 39.1  LINING  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 FLOOR, I: 6 YE  LINING BELOW AND 0,75 M FWD AND AFT OF GALLEYS AND TOILETS,  NOTE 1 FROM FR 20 TO FR 39.1, LH/RH  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA.  532105-01-1 821 134 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  BALLMATS BELOW FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YE  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 FR I: 6 YE  25 (10 PLACES)  R 532107-01-2 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 7500 FC  COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR I: 7500 FC  25 (10 PLACES)  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TPS

 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 STRUCTURE T: 12 YE 1  INSULATION 132 AROUND FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 12 YE  LINING 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  532114-01-2 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 INTERNAL T: 12 YE  234 SURFACE UNDERNEATH ACOUSTIC INSULATION PANELS FROM I: 12 YE  FR 18 TO FR 26.4 BETWEEN STR 6 AND CROWN CENTERLINE,  LH/RH.  532116-01-2 N/A TASK DELETED  532116-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 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 CENTER LINE, LH/RH.  532116-03-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN INTERNAL T: 12 YE  234 SURFACE UNDERNEATH ACOUSTIC INSULATION PANELS FROM FR I: 12 YE  18 TO FR 26.4 BETWEEN STR 3 AND CROWN CENTERLINE AND  BETWEEN STR 7 TO STR 17, LH/RH.  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  532117-01-3 N/A TASK DELETED  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 MAIN DECK  242 FLOOR, LH/RH  R 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 TO I: 12 YE  NOTE 1 243 CROWN CENTER LINE, LH/RH  OVERHEAD STOWAGE 244  BINS  R 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-OUTS BETWEEN FR 32 AND FR 36, FROM STR 9 TO STR  26 LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TPS

 R 532122-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2  AIR CONDITION DUCTS 132 BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YE  NOTE 1 BETWEEN FR 32 AND FR 36, FROM MAIN DECK FLOOR DOWN  SIDEWALL LINING TO STR 30, LH/RH  R 532123-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1  NOTE 1 242 AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YE  SIDEWALL/DOOR FRAME 243 BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOOR UPTO  LINING 244 STR 9, LH/RH  R 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, I: 6 YE  LH/RH  532124-02-4 N/A TASK DELETED  532124-02-5 N/A TASK DELETED  532124-02-6 N/A TASK DELETED  532124-02-7 N/A TASK DELETED  532124-02-8 N/A TASK DELETED  532124-02-9 N/A TASK DELETED  532125-01-4 N/A TASK DELETED  532125-01-5 N/A TASK DELETED  532125-01-6 N/A TASK DELETED  532125-01-7 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 532125-01-8 N/A TASK DELETED  532125-01-9 N/A TASK DELETED  532126-01-1 N/A TASK DELETED  532127-01-1 N/A TASK DELETED  532128-01-1 N/A TASK DELETED  532129-01-2 N/A TASK DELETED  532129-01-3 N/A TASK DELETED  532130-01-2 N/A TASK DELETED  532130-01-3 N/A TASK DELETED  R 532134-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2  FLOOR PANELS 232 BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, I: 5 YE  GALLEYS AND 241 INCLUDING DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.  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.  R 532134-01-2 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 1+2  FLOOR PANELS 232 BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, I: 6 YE  GALLEYS AND 241 INCLUDING DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.  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.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 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  532136-01-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN T: 12 YE  234 UNDERNEATH ACOUSTIC INSULATION PANELS FROM FR 18 TO I: 12 YE  FR 32, BETWEEN STR 3 AND CROWN CENTER LINE, LH/RH AND  - BETWEEN STR 7 TO STR 17, LH/RH.  R 532137-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FC  JOINTS IN THE FOLLOWING CRACK STOPPER AREAS : I: 6500 FC  AT STR 5 LH/RH, FROM 18 TO FR 38, AT STR 13 AND STR  22 LH/RH, FROM FR 18 TO FR 31 AND FROM FR 37.1 TO FR  38, EXTERNAL SURFACE  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  532137-02-1  R 532137-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  LONGITUDINAL LAP JOINTS IN THE FOLLOWING CRACK I: 20000 FC  STOPPER AREAS :  AT STR 5 LH/RH, FROM 18 TO FR 38, AT STR 13 AND STR  22 LH/RH, FROM FR 18 TO FR 31 AND FROM FR 37.1 TO FR  38, EXTERNAL SURFACE  NOTE :  - INSPECTION REQUIRES INSPECTION OF LAP JOINT LOWER  RIVET ROW.  - THIS TASK IS AN ALTERNATIVE TO TASK 532137-01-1  532138-01-1 N/A TASK DELETED  532139-01-1 N/A TASK DELETED  R 532142-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNA T: 24000 FC  CUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTER I: 16000 FC  LINE, EXTERNAL SURFACE  532143-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 TPS

 532144-01-2 N/A TASK DELETED  R 532145-02-1 N/A 200 GENERAL VISUAL INSPECTION OF SKIN AT SHEAR TIE T: 22800 FC  ATTACHMENTS BETWEEN FR 19 AND FR 25, FR 26.1 AND FR I: 12000 FC  37, FR 37.2 AND FR 37.4, FROM STR 13 LH/RH TO CROWN  CENTER LINE, EXTERNAL SURFACE  532146-01-2 N/A TASK DELETED  532147-01-2 N/A TASK DELETED  532148-01-2 N/A TASK DELETED  532149-01-2 N/A TASK DELETED  532150-01-2 N/A TASK DELETED  532150-01-3 N/A TASK DELETED  532150-01-4 N/A TASK DELETED  532151-01-1 N/A TASK DELETED  R 532152-01-1 N/A 100 DETAILED INSPECTION OF FUSELAGE SKIN AT SHEAR TIE T: 20000 FC  200 ATTACHMENT BETWEEN FR 26 AND FR 37.1 FROM STR 13 TO OR  STR 31 LH/RH, EXTERNAL SURFACE 75000 FH  I: 8500 FC  OR  31900 FH  532153-01-2 N/A TASK DELETED  532153-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 532154-01-2 N/A TASK DELETED  532155-01-2 N/A TASK DELETED  532156-01-2 N/A TASK DELETED  532156-01-3 N/A TASK DELETED  532156-01-4 N/A TASK DELETED  532157-01-2 N/A TASK DELETED  532158-01-2 N/A TASK DELETED  532158-01-3 N/A TASK DELETED  R 532159-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND VHF 1 ANTENNA T: 24000 FC  CUT-OUT BETWEEN FR 22 AND FR 23, ON CROWN CENTER I: 12000 FC  LINE, EXTERNAL SURFACE  R 532160-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND ATC 1 + 2 ANTENNA T: 24000 FC  CUT-OUT BETWEEN FR 24 AND FR 25, AND BETWEEN STR 2 I: 12000 FC  AND STR 3, LH/RH, EXTERNAL SURFACE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 R 532161-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND SATCOM (LG) T: 24000 FC  ANTENNA CUT-OUT BETWEEN FR 26 AND FR 26.1 ON CROWN I: 12000 FC  CENTER LINE, EXTERNAL SURFACE  R 532162-01-2 831 841 233 DETAILED INSPECTION OF SKIN AROUND SATCOM (45 DEG) T: 24000 FC  ANTENNA 234 ANTENNA CUT-OUT BETWEEN FR 26.1 AND FR 26.3 AND I: 12000 FC  MAINTENANCE DOOR BETWEEN STR 12 AND STR 13, LH/RH, EXTERNAL SURFACE  OVERHEAD  STOWAGE-COMPARTMENT  DOOR  R 532163-01-1 ANTENNA REAR FAIRING 200 DETAILED INSPECTION OF SKIN AROUND SATCOM (HG) T: 24000 FC  COVER AND BRACKET ANTENNA CUT-OUT BETWEEN FR 26.2 AND FR 27, ON CROWN I: 12000 FC  CENTER LINE, EXTERNAL SURFACE  532164-01-1 N/A TASK DELETED  532165-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TPS

 532165-01-3 N/A TASK DELETED  532165-02-1 N/A TASK DELETED  N 532166-01-2 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  TO CROWN CENTER LINE.  N 532167-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE  SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO STR 6, I: 12 YE  LH/RH.  N 532168-01-1 831 841 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3  BARRIER WALL DOORS 232 STRUCTURE FROM BARRIER WALL (BETWEEN FR 19 AND FR 20) I: 12 YE  LINING 233 TO FR 36, FROM CROWN CENTER LINE TO MAIN DECK FLOOR,  NOTE 1 234 LH/RH.  241  242  243  244  N 532169-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3  BARRIER WALL DOORS 232 FROM BARRIER WALL (BETWEEN FR 19 AND FR 20)TO FR 36. I: 6 YE  FLOOR PANELS 241  242  N 532170-02-1 BARRIER WALL LINING 230 DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO T: 12 YE 3  SMOKE CURTAIN FUSELAGE, FITTING ASSEMBLIES. I: 12 YE  STOWAGE BINS (IF  FITTED)  N 532171-02-1 BARRIER WALL LINING 230 DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO T: 6 YE 3  PROTECTION ANGLES CARGO FLOOR, FITTING ASSEMBLIES. I: 6 YE  AND DOOR STEPS  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TPS

 N 532172-01-1 BARRIER WALL LINING 230 GENERAL VISUAL INSPECTION OF BARRIER WALL FRAMES AND T: 6 YE 3  STOWAGE BINS (IF BOX STRUCTURE. I: 6 YE  FITTED)  N 532175-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL T: 12 YE  200 STRUCTURE AROUND MAIN DECK CARGO DOOR CUT-OUT FROM I: 12 YE  FRAME 18 TO FRAME 31 AND FROM CROWN CENTERLINE TO  STRINGER 35.  N 532177-01-1 MDC DOOR 231 GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 3  STRUCTURE OF MAIN DECK CARGO DOOR LOCK FITTING I: 6 YE  ATTACHMENTS, SURROUNDING STRUCTURE AND LOWER LONGERON  FROM FRAME 20 TO FRAME 29 AND FROM STRINGER 26 TO  STRINGER 30.  N 532178-02-1 MDC DOOR 231 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE OF T: 6 YE 1  MAIN DECK CARGO DOOR LOCK FITTINGS FROM FRAME 20 TO I: 6 YE  FRAME 29 AND FROM STRINGER 26 TO STRINGER 30 AT 8  PLACES.  N 532179-01-1 MDC DOOR 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 3  233 STRUCTURE OF MAIN DECK CARGO DOOR CUT-OUT FRAMES 20 I: 6 YE  AND 29 FROM STRINGER 5 TO STRINGER 28.  N 532180-01-1 MDC COMPARTMENT 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3  LINING 233 STRUCTURE AROUND MAIN DECK CARGO DOOR CUT-OUT FROM I: 12 YE  FRAME 18 TO FRAME 31 AND FROM CROWN CENTERLINE TO  STRINGER 26.  N 532181-01-1 CC LINING 131 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 3  STRUCTURE BELOW MAIN DECK CARGO DOOR CUT-OUT FROM I: 6 YE  FRAME 18 TO FRAME 31 AND FROM STRINGER 26 TO STRINGER  35.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TPS

 533001-01-2 196AB 196BB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FC  STRUCTURE AT FRAME 46, HAT-SECTION PROFILE JUNCTION I: 5500 FC  ON ARCH MEMBER AT Y = 1445  533001-01-4 196EB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FC  STRUCTURE AT FRAME 46, HAT-SECTION PROFILE I: 5500 FC  JUNCTION ON ARCH MEMBER AT Y = 1445  533002-01-2 196AB 196BB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 20000 FC  FRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 13700 FC  LONGITUDINAL WEB AT Y = 493  533002-01-4 196GB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 20000 FC  FRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 13700 FC  LONGITUDINAL WEB AT Y = 493  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 533003-01-2 197AB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE, FRAME T: 20000 FC  197 53.2 WEB AT Y=-1042, Y=-728.7 AND Y=728,7 BELOW I: 13700 FC  198 LONGITUDINAL WEB ATTACHMENT  533004-01-2 197GB 198GB 197 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FC  198 STRUCTURE AFT OF FRAME 53.8, T-SECTION JUNCTION ON I: 5500 FC  LONGITUDINAL BEAM, LH/RH  533005-01-2 N/A TASK DELETED  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  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  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 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  R 533009-01-1 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  NOTE 1 254 LH/RH. I: 13900 FC  OVERHEAD STOWAGE NOTE : OR  BINS - ROTOTEST INSPECTION 41700 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-1  R 533009-01-2 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  NOTE 1 254 LH/RH. I: 10800 FC  OVERHEAD STOWAGE NOTE : OR  BINS - ROTOTEST INSPECTION 54200 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-2  R 533009-01-3 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  NOTE 1 254 LH/RH. I: 11400 FC  OVERHEAD STOWAGE NOTE : OR  BINS - ROTOTEST INSPECTION 34300 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-3  N 533009-01-4 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  NOTE 1 254 LH/RH. I: 11600 FC  OVERHEAD STOWAGE NOTE : OR  BINS - ROTOTEST INSPECTION 34900 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-4  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533009-02-1 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  OVERHEAD STOWAGE 254 LH/RH. I: 4600 FC  BINS NOTE : OR  - X-RAY INSPECTION 13900 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-1  R 533009-02-2 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  OVERHEAD STOWAGE 254 LH/RH. I: 3600 FC  BINS NOTE : OR  - X-RAY INSPECTION 18100 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-2  R 533009-02-3 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  OVERHEAD STOWAGE 254 LH/RH. I: 3800 FC  BINS NOTE : OR  - X-RAY INSPECTION 11400 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-3  N 533009-02-4 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN OR  NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FH  OVERHEAD STOWAGE 254 LH/RH. I: 3800 FC  BINS NOTE : OR  - X-RAY INSPECTION 11600 FH  - THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-4  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533010-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN OR  CENTERLINE TO STRINGER 17, LH/RH 50000 FH  I: 3900 FC  OR  11700 FH  R 533010-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN OR  CENTERLINE TO STRINGER 17, LH/RH 50000 FH  I: 3050 FC  OR  15300 FH  R 533010-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN OR  CENTERLINE TO STRINGER 17, LH/RH 50000 FH  I: 3200 FC  OR  9700 FH  N 533010-01-4 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN OR  CENTERLINE TO STRINGER 17, LH/RH 50000 FH  I: 3250 FC  OR  9800 FH  533011-01-2 N/A TASK DELETED  533011-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533012-01-1 261CC 262CC 263 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  NOTE 1 264 CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO OR  OVERHEAD STOWAGE 5, LH/RH. 50000 FH  BINS NOTE : I: 8100 FC  RIVETS - ROTOTEST INSPECTION 1MM OR  - THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-1 24400 FH  R 533012-02-1 261CC 262CC 263 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  NOTE 1 264 CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO OR  OVERHEAD STOWAGE 5, LH/RH. 50000 FH  BINS NOTE : I: 2300 FC  - X-RAY INSPECTION 5 MM OR  - THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-1 6900 FH  533013-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  NOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 20000 FC  AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH OR  78000 FH  R 533013-01-2 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 18000 FC  NOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION OR  AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH 72000 FH  I: 14700 FC  OR  73900 FH  R 533013-01-3 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 19000 FC  NOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 15500 FC  AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH OR  46500 FH  N 533013-01-4 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 19000 FC  NOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 15600 FC  AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH OR  46900 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533014-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 20000 FC  148 LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF OR  FRAME 47 DATUM, LH/RH 50000 FH  I: 6900 FC  OR  20900 FH  R 533014-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 20000 FC  148 LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF OR  FRAME 47 DATUM, LH/RH 50000 FH  I: 7300 FC  OR  36800 FH  533015-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, LOWER T: 20000 FC  148 FLANGE OF GANTRY Y=1959 AT FRAME 48 LEVEL, LH/RH I: 20000 FC  OR  78000 FH  533015-01-2 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 17000 FC  148 LOWER FLANGE OF GANTRY Y=1959 AT FRAME 48 LEVEL, LH/R OR  50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533016-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN OR  CENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, 50000 FH  EXTERNAL SURFACE, LH/RH I: 4400 FC  OR  13200 FH  R 533016-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN OR  CENTERLINE TO STR 3 AND FROM STR 5 TO STR 50000 FH  11, EXTERNAL SURFACE, LH/RH I: 4300 FC  OR  13000 FH  533016-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FC  CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN OR  CENTERLINE TO STR 3 AND FROM STR 5 50000 FH  TO STR 11, EXTERNAL SURFACE, LH/RH. I: 4360 FC  OR  13100 FH  N 533016-01-4 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FC  CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN OR  CENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, 50000 FH  EXTERNAL SURFACE, LH/RH. I: 4180 FC  OR  20900 FH  533017-01-1 N/A TASK DELETED  R 533018-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN OR  CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FH  EXTERNAL SURFACE, LH/RH I: 4300 FC  OR  21800 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533018-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN OR  CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FH  EXTERNAL SURFACE, LH/RH I: 4600 FC  OR  13800 FH  N 533018-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN OR  CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FH  EXTERNAL SURFACE, LH/RH. I: 4600 FC  OR  14000 FH  533019-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FC  CIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM I: 8000 FC  CENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 AND  STRG5) LH/RH  533019-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FC  CIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, OR  FROM CENTERLINE TO STRG8 50000 FH  (EXCLUDING AREA BETWEEN STRG3 AND STRG5) LH/RH I: 8000 FC  OR  40000 FH  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 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 2.5 YE  FR.47 FROM Y=-2390 AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY  TO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.  R 533035-01-2 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=-2390 AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY  TO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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 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=-2390 EXCLUDING AREA FROM Y=-2390 TO Y=2390, LH/RH.  TO Y=2390  533101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 12 YE NO  200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 12 YE  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  533101-01-5 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 20000 FC  200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 7860 FC  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  533101-01-6 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 20000 FC  200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 6340 FC  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  533101-01-7 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 20000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 6200 FC  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533101-01-8 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 17000 FC  200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO OR  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 50000 FH  I: 9200 FC  OR  27500 FH  533101-01-9 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 17000 FC  200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO OR  CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 50000 FH  I: 8800 FC  OR  43900 FH  533102-01-1 N/A TASK DELETED  533103-02-1 N/A TASK DELETED  R 533104-01-3 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 20000 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 50000 FH  INSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 5000 FC  STRINGER 1 LH AND STRINGER 1 RH OR  15000 FH  533104-01-4 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 20000 FC  LIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 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)  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533104-01-5 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 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 50000 FH  INSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 17000 FC  STRINGER 1 LH AND STRINGER 1 RH OR  - AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND 50000 FH  FR.40.1  533104-02-6 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 FC  LIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUTS BETWEEN FR.40.3 AND OR  OBTURATORS WHERE FR.41 50000 FH  INSTALLED - OBTURATOR CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 FC  - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 OR  AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN 40000 FH  STRINGER 1 LH AND STRINGER 1 RH  - AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND  FR.40.1  533104-02-7 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 FC  LIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUTS BETWEEN FR.40.3 AND OR  OBTURATORS WHERE FR.41 50000 FH  INSTALLED - OBTURATOR CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 FC  - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 OR  AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN 24000 FH  STRINGER 1 LH AND STRINGER 1 RH  - AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND  FR.40.1  533105-01-2 N/A TASK DELETED  R 533106-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 20000 FC  FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE OR  SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FH  53.3, LH/RH I: 6800 FC  OR  20600 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533106-01-3 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 20000 FC  FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE OR  SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FH  53.3, LH/RH I: 8000 FC  OR  44000 FH  533106-01-4 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 17000 FC  FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE OR  SKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FH  53.3, LH/RH I: 8000 FC  OR  24000 FH  533106-01-5 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 17000 FC  FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE OR  SKIN BETWEEN STRG. 18 AND STRG. 22, 50000 FH  FROM FRAME 38 TO 53.3, LH/RH I: 8000 FC  OR  40000 FH  533107-01-3 N/A TASK DELETED  533107-01-4 N/A TASK DELETED  533107-01-6 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  DUCTS 132 STRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUST OR  LINING 137 BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES 50000 FH  NOTE 1 138 JUNCTION BELOW STRINGER 29 LEVEL, LH/RH I: 11000 FC  OR  33000 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533107-01-7 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  DUCTS 132 STRUCTURE FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW OR  LINING 137 STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION 50000 FH  NOTE 1 138 BELOW STRINGER 29 LEVEL, LH/RH. I: 9900 FC  OR  49800 FH  533109-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FC  LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT I: 10200 FC  STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22  FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARD  AND AFT FRAME 45 LEVEL, LH/RH  533109-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 17000 FC  LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT I: 10200 FC  STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22  FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS  FORWARD AND AFT FRAME 45 LEVEL, LH/RH  533113-01-4 N/A TASK DELETED  533113-01-5 N/A TASK DELETED  533114-01-3 N/A TASK DELETED  533114-01-4 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533114-01-5 251XW 252XW 251 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  NOTE 1 252 STRUCTURE FRAME 47 WEB AT JUNCTION WITH STABILIZERS OR  STRINGER 20 TO 23, LH/RH 50000 FH  I: 17000 FC  OR  50000 FH  533115-01-4 N/A TASK DELETED  533115-01-5 N/A TASK DELETED  533115-01-6 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  533122-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CLG WELL; KEEL BEAM T: 6 YE 1  148 INTERNAL STRUCTURE AND PANELS BETWEEN FR 47 AND FR I: 6 YE  149 53.2  NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN  THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA.  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 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533124-01-2 734 744 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT CLG T: 21300 FC  148 DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH I: 21300 FC  149 NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN  THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA.  533124-01-3 734 744 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT CLG T: 17000 FC  148 DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH I: 17000 FC  149 NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT  IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA  533125-01-1 734 744 147 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2 T: 6 YE 1  148 PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF I: 6 YE  149 THE CLG TRUNNION FITTINGS  NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN  THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA.  533126-01-1 N/A TASK DELETED  R 533126-01-2 734 744 147 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND T: 6 YE 1  148 CLG AND MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) I: 6 YE  149 EXTERNAL SURFACE.  NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN  THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA.  533126-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533127-01-1 N/A TASK DELETED  533127-02-1 FAIRING PANELS 191 GENERAL VISUAL INSPECTION OF AREA AROUND T: 6 YE 1  BETWEEN FR 39.1 AND 192 AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 I: 6 YE  FR 47 193 CM (6.0 IN) EXTERNAL SURFACE  195  196  533127-02-2 N/A TASK DELETED  533127-03-1 N/A TASK DELETED  533129-01-1 734 744 143 DETAILED INSPECTION OF KEEL BEAM INTERNAL AND T: 12 YE 1  FAIRING PANELS 149 EXTERNAL STRUCTURE SKIN AND ADJACENT FUSELAGE I: 12 YE  BETWEEN FR 40 AND FR 191 STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE.  47 192  193  195  196  533135-01-1 734 744 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 12 YE 1  148 FITTINGS NO 1 THROUGH NO 6, DOOR ACTUATOR FITTINGS I: 12 YE  149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RH  NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED  TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN  THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL  COMMONALITY WITH THE A340 IN THIS AREA.  533136-01-2 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING NO 1 T: 20000 FC  148 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FC  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533136-01-3 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING NO T: 17000 FC  148 1 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FC  533137-01-1 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND T: 20000 FC  252MG 146 ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 16600 FC  FUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER AT  Y=2565, LH/RH  533137-01-2 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND T: 20000 FC  252MG 146 ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 20000 FC  FUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER AT  Y=2565, LH/RH  533137-01-3 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL T: 17000 FC  252MG 146 AND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 17000 FC  FUSELAGE SKIN PANEL TO FIRST HORIZONTAL  STIFFENER AT Y=2565, LH/RH  533138-01-2 N/A TASK DELETED  R 533138-01-3 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  NOTE 1 146 STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y = 1959, OR  AT FR 48 LEVEL, LH/RH. 50000 FH  I: 19800 FC  OR  59500 FH  533140-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 7100 FC  SPLICE AT STRINGER 42, LH/RH  533140-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 6400 FC  SPLICE AT STRINGER 42, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533140-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 5900 FC  SPLICE AT STRINGER 42, LH/RH  533141-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND T: 12 YE 1  CARGO FLOOR PANELS 152 PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND I: 12 YE  LD-MCR IF INSTALLED CARGO COMPARTMENT FLOOR LEVEL  OR POST 46678 LDL  TOILETS AND  FURNISHINGS  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  CARGO FLOOR PANELS 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR LEVEL I: 6 YE  LD-MCR IF INSTALLED  OR POST 46678 LDL  TOILETS AND  FURNISHINGS  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  R 533145-01-3 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FC  198HB 197 BUTT JOINT AT STRINGER 31 LEVEL FROM FRAME 53.3 TO I: 7050 FC  198 FRAME 54, LH/RH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

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 TPS

 R 533145-01-4 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FC  198HB 197 BUTT JOINT AT STRINGER 31 LEVEL FROM FRAME 53.3 TO I: 6100 FC  198 FRAME 54, LH/RH  533146-01-1 N/A TASK DELETED  R 533147-01-2 GALLEYS 253 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  LINING 254 STRUCTURE BETWEEN FR 36 AND FR 53.5 FROM STR 15 TO I: 12 YE  NOTE 1 CROWN CENTER LINE, LH/RH  OVERHEAD STOWAGE  BINS  TOILETS  R 533148-01-1 GALLEYS 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  TOILETS  533149-01-1 N/A TASK DELETED  R 533150-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 6 YE 1  GALLEYS 252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 6 YE  TOILETS FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533150-01-2 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:  - IF NO GALLEYS/TOILETS ARE INSTALLED TPS APPLICATION  MAY BE LIMITED TO PRESSURIZED FLOORS AND PRESSURE  DIAPHRAGM.  - TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITTED ABOVE THIS AREA.  533152-01-1 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 7100 FC  FAIRING LEVEL, LH/RH.  R 533152-01-2 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  LD-MCR IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8  FAIRING LEVEL, LH/RH. I: 7100 FC  533152-01-3 151HX 152HX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  LDL IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 7100 FC  FAIRING LEVEL, LH/RH.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533152-01-4 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6200 FC  FAIRING LEVEL, LH/RH.  R 533152-01-5 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  LD-MCR IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8  FAIRING LEVEL, LH/RH. I: 6200 FC  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533152-01-6 151HX 152HX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FC  LDL IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6200 FC  FAIRING LEVEL, LH/RH.  533154-01-4 N/A TASK DELETED  533154-01-5 N/A TASK DELETED  533154-01-6 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  GALLEYS 146 RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS I: 17000 FC  TOILETS JUNCTION, FROM FRAME 48 TO 53.1, LH/RH  R 533155-01-1 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH OR  50000 FH  I: 12600 FC  OR  63100 FH  N 533155-01-2 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. OR  50000 FH  I: 9700 FC  OR  29100 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 533155-01-3 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  NOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. OR  50000 FH  I: 13000 FC  OR  39100 FH  R 533156-01-1 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  LD-MCR IF INSTALLED 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS OR  OR POST 46678 LDL 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FH  TOILETS AND I: 6100 FC  FURNISHINGS OR  LINING 18300 FH  NOTE 1  533156-01-2 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  LD-MCR IF INSTALLED 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS OR  OR POST 46678 LDL 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FH  TOILETS AND I: 7300 FC  FURNISHINGS OR  LINING 41600 FH  NOTE 1  533156-01-3 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  LINING 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN OR  NOTE 1 STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FH  I: 7300 FC  OR  22700 FH  533156-01-4 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  LINING 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN OR  NOTE 1 STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FH  I: 7000 FC  OR  35000 FH  533157-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533161-01-1 251AX 251CX 251EX 251 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRU T: 20000 FC  252AX 252CX 252EX 252 SPLICING AREA AT FRAMES 53 TO 53.2 BETWEEN STRINGERS I: 20000 FC  NOTE 1 24 AND 26, LH/RH OR  77900 FH  533162-01-2 N/A TASK DELETED  R 533164-01-3 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED OR  DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FH  FROM Y=450 TO Y=1959, LH/RH I: 13700 FC  OR  68500 FH  533164-01-4 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED OR  DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 50000 FH  47 AND 48 FROM Y=450 TO Y=1959, LH/RH I: 12500 FC  OR  50000 FH  533164-01-5 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED OR  DIAPHRAGMS ON FLOOR BEAMS BETWEEN 50000 FH  FRAMES 47 AND 48 FROM Y=450 TO Y=1959, LH/RH I: 14900 FC  OR  44600 FH  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 533164-01-6 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED OR  DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FH  FROM Y=450 TO Y=1959, LH/RH. I: 12200 FC  OR  36800 FH  N 533164-01-7 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FC  148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED OR  DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FH  FROM Y=450 TO Y=1959, LH/RH. I: 14800 FC  OR  44400 FH  533165-01-2 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  533169-01-1 N/A TASK DELETED  R 533170-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2  GALLEYS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 5 YE  TOILETS 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.  R 533170-01-2 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 6 YE 1+2  GALLEYS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 6 YE  TOILETS 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.  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 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  533178-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  GALLEYS AND TOILETS 146 STRUCTURE FLOOR BEAM INBOARD FLANGE RADIUS AT Y=1959, I: 20000 FC  IF INSTALLED FROM FRAME 47 TO FRAME 48, LH/RH OR  NOTE 1 78000 FH  533178-01-2 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  GALLEYS AND TOILETS 146 STRUCTURE FLOOR BEAM INBOARD FLANGE RADIUS AT OR  IF INSTALLED Y=1959, FROM FRAME 47 TO FRAME 48, LH/RH 50000 FH  NOTE 1 I: 17000 FC  OR  50000 FH  R 533179-01-2 251MG 251SG 252MG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 19000 FC  252SG 146 FRAMES 48 TO 53.1 VERTICAL LEG AT STRINGER PASSAGE, I: 11800 FC  NOTE 1 LH/RH OR  35400 FH  533180-01-3 N/A TASK DELETED  533180-01-4 N/A TASK DELETED  533180-01-5 N/A TASK DELETED  533181-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 533181-01-4 N/A TASK DELETED  533181-01-5 N/A TASK DELETED  533181-01-6 N/A TASK DELETED  R 533182-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FC  JOINT IN CRACK STOPPER AREA AT STRINGER 5 LH/RH, I: 6500 FC  BETWEEN FR 53.3 AND 54, EXTERNAL SURFACE  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533182-02-1  R 533182-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  LONGITUDINAL LAP JOINT IN CRACK STOPPER AREA AT I: 20000 FC  STRINGER 5 LH/RH, BETWEEN FR 53.3 AND 54, EXTERNAL  SURFACE  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533182-01-1  R 533184-01-2 N/A 200 DETAILED INSPECTION OF SKIN AT SHEAR TIE ATTACHMENTS T: 22800 FC  BETWEEN FR 53.4 AND FR 53.9 FROM STRINGER 13 LH/RH TO OR  CROWN CENTER LINE, EXTERNAL SURFACE 90000 FH  I: 12000 FC  OR  47300 FH  N 533185-01-1 LINING 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE  NOTE 1 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM CROWN I: 12 YE  253 CENTER LINE TO MAIN DECK FLOOR LEVEL, LH/RH.  254  533186-01-1 N/A TASK DELETED  N 533188-01-1 MAIN DECK FLOOR 251 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3  PANELS 252 BETWEEN FR.36 AND FR.53. I: 6 YE  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533190-01-1 834 844 261 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR T: 12 YE 1  INSULATION 262 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR I: 6 YE  LINING 53.4 AND 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 BELOW DOOR3 T: 6 YE 1  152GW 822 152 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR I: 6 YE  FLOOR PANELS 53.4 AND 53.8 FROM MAIN DECK FLOOR DOWN TO CARGO  INSULATION FLOOR LEVEL, LH/RH  LDL TOILETS AND  FURNISHING-IF  INSTALLED  LD-MCR-IF INSTALLED  533192-01-1 N/A TASK DELETED  533193-01-1 N/A TASK DELETED  R 533193-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN (INCLUDING T: 6 YE  200 DOOR 3 CUT-OUT) BETWEEN FR 53.3 AND FR 54 FROM UPPER I: 6 YE  EDGE OF BELLY FAIRING TO CROWN CENTER LINE LH/RH,  EXTERNAL SURFACE  533194-01-1 N/A TASK DELETED  533194-01-5 N/A TASK DELETED  533194-01-6 N/A TASK DELETED  533194-01-7 N/A TASK DELETED  533194-01-8 N/A TASK DELETED  533194-01-9 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 533195-01-1 834 844 100 DETAILED INSPECTION OF DOOR 3 T: 12 YE  SCUFF PLATE (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YE  UNDERNEATH SCUFF PLATE, LH/RH.  533195-02-1 N/A TASK DELETED  533195-02-5 N/A TASK DELETED  533195-02-6 N/A TASK DELETED  533195-02-7 N/A TASK DELETED  533195-02-8 N/A TASK DELETED  533195-02-9 N/A TASK DELETED  534102-01-3 N/A TASK DELETED  534102-01-4 N/A TASK DELETED  534104-01-4 N/A TASK DELETED  534104-01-5 N/A TASK DELETED  534105-01-3 N/A TASK DELETED  534105-01-4 N/A TASK DELETED  534105-01-5 N/A TASK DELETED  534107-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534107-01-3 N/A TASK DELETED  R 534108-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN IN T: 22800 FC  CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT I: 15200 FC  FR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE,  EXTERNAL SURFACE.  R 534110-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN IN T: 22800 FC  300 CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM I: 15200 FC  STR 6 TO STR 13 LH/RH, EXTERNAL SURFACE.  R 534113-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FC  JOINTS IN FOLLOWING CRACK STOPPER AREAS : I: 6500 FC  - AT STR 13 AND STR 22 LH/RH, FROM FR 54 TO FR 72  - AT STR 17 AND STR 24 LH/RH, FROM FR 76 TO FR 80,  EXTERNAL SURFACE.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534113-02-1  R 534113-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  LONGITUDINAL LAP JOINTS IN FOLLOWING CRACK STOPPER I: 20000 FC  AREAS :  - AT STR 13 AND STR 22 LH/RH, FROM FR 54 TO FR 72  - AT STR 17 AND STR 24 LH/RH, FROM FR 76 TO FR 80,  EXTERNAL SURFACE.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534113-01-1  R 534115-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FC  JOINTS IN FOLLOWING CRACK STOPPER AREAS : I: 6500 FC  - AT STR 5 LH/RH, FROM FR 54 TO FR 72,  - AT STR 6 LH/RH, FROM FR 72 TO FR 80,  EXTERNAL SURFACE.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534115-02-1  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 534115-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  LONGITUDINAL LAP JOINTS IN FOLLOWING CRACK STOPPER I: 20000 FC  AREAS :  - AT STR 5 LH/RH, FROM FR 54 TO FR 72,  - AT STR 6 LH/RH, FROM FR 72 TO FR 80,  EXTERNAL SURFACE.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534115-01-1  R 534116-01-1 197GB 198GB 197 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  198 LONGITUDINAL LAP JOINT IN CRACK STOPPER AREAS AT I: 20000 FC  STR 44 LH/RH BETWEEN FR 54 AND FR55, EXTERNAL  SURFACE.  R 534117-01-1 N/A 100 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FC  LONGITUDINAL LAP JOINT AT STR 54 LH, BETWEEN FR I: 16000 FC  54 AND FR 58.  534120-01-2 N/A TASK DELETED  534120-01-3 N/A TASK DELETED  R 534122-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AT SHEAR T: 22800 FC  TIE ATTACHMENTS: OR  - BETWEEN FR 55 AND FR 57.4, 78000 FH  - BETWEEN FR 59 AND FR 71 AND I: 12000 FC  - BETWEEN FR 73 AND FR 79, OR  FROM STR 13 LH/RH TO CROWN CENTER LINE, 41000 FH  EXTERNAL SURFACE EXCLUDING AREA COVERED BY FIN TO  FUSELAGE FAIRING.  R 534124-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 12 YE  54 AND FR 80 FROM STR 6 TO STR 26, EXCLUDING AREA I: 12 YE  UNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE  534124-01-2 N/A TASK DELETED  534125-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534126-01-1 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 TO I: 6 YE  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  534126-01-2 N/A TASK DELETED  534127-01-1 822 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2  CARGO COMPARTMENT 154 STRUCTURE BETWEEN FR 53.2 AND 73 BELOW CARGO I: 6 YE  FLOOR PANELS 163 COMPARTMENT FLOOR PANELS.  INSULATION 164 NOTE : IF LDL INSTALLED, INSPECTION AREA BETWEEN FR  LD-MCR-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  R 534130-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AT DOOR T: 6 YE  200 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT BETWEEN FR 73 I: 6 YE  AND FR 76, FROM STR 9 TO STR 26 LH/RH, EXTERNAL  SURFACE  534130-01-2 N/A TASK DELETED  534131-01-2 N/A TASK DELETED  534131-01-3 N/A TASK DELETED  R 534132-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW T: 12 YE  SCUFF PLATE 200 DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE LH/RH I: 6 YE  534132-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534132-02-2 N/A TASK DELETED  R 534133-01-1 833 843 271 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR T: 12 YE 1  DOOR FRAME LINING 272 4 (AFT PASSENGER/ CREW DOOR) BETWEEN FR 72 AND FR 77 I: 6 YE  INSULATION FROM MAIN DECK FLOOR LEVEL TO STR 9 LH/RH  LINING  R 534134-01-1 162ZW 823 171 DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW DOOR T: 6 YE 1  NOTE 1 172 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR 73 I: 6 YE  AND FR 76 FROM MAIN DECK FLOOR LEVEL TO STR 30 LH/RH  534135-01-1 N/A TASK DELETED  534136-01-2 N/A TASK DELETED  534137-01-2 N/A TASK DELETED  R 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: 6 YE  LINING FR 66, FROM STR 26 RH TO CARGO FLOOR LEVEL  534139-01-3 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1  154 DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A I: 6 YE  AND FR 65) AS FAR AS VISIBLE.  534139-01-4 N/A TASK DELETED  534140-01-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO T: 6 YE T: 20 YE  ECCENTRIC BOLTS COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR59A AND I: 6 YE I: 6 YE  FR65  534140-02-1 822 152 GENERAL VISUAL INSPECTION OF LOCK FITTINGS OF AFT T: 6 YE 1+2  CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 59A I: 6 YE  AND FR 65  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534140-02-2 N/A TASK DELETED  534141-01-1 N/A TASK DELETED  534143-01-2 N/A TASK DELETED  534143-01-3 N/A TASK DELETED  534144-01-1 823 100 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR T: 12 YE  SCUFF PLATE CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE I: 6 YE  534144-01-2 N/A TASK DELETED  534144-01-3 N/A TASK DELETED  534145-01-1 823 162 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND BULK T: 6 YE 1  FLOOR PANELS CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 66 AND 70 I: 6 YE  LINING 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 69 I: 6 YE  534146-01-2 N/A TASK DELETED  534148-01-2 N/A TASK DELETED  534148-01-3 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 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534149-01-2 N/A TASK DELETED  534150-01-2 N/A TASK DELETED  534151-01-1 N/A TASK DELETED  534152-01-1 N/A TASK DELETED  534153-01-1 N/A TASK DELETED  534154-01-2 N/A TASK DELETED  534155-01-2 N/A TASK DELETED  534156-01-1 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW AFT T: 6 YE 1+2  CARGO FLOOR PANELS 154 CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND FR I: 6 YE  INSULATION 67, FROM CARGO FLOOR LEVEL TO STR 47 RH  LINING  534156-01-2 N/A TASK DELETED  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  R 534158-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1  CARGO COMPARTMENT 152 STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND CARGO I: 12 YE  CEILING PANELS 161 COMPARTMENT FLOOR FROM FR 53.2 TO FR 73, INCLUDING  LDL TOILETS AND 162 MAIN DECK FLOOR STRUCTURE  FURNISHING-IF 171  INSTALLED 172  LD-MCR-IF INSTALLED  LINING  NOTE 1  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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, I: 5 YE  GALLEYS 271 INCLUDING DOOR ENTRANCE AREAS, FROM FR 53,5 TO FR 80.  TOILETS 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, I: 6 YE  GALLEYS 271 INCLUDING DOOR ENTRANCE AREAS, FROM FR 53,5 TO FR 80.  TOILETS 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.  R 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) TO MAIN DECK  272 FLOOR, LH/RH  R 534162-01-1 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE T: 6 YE 1+2  ACT IF INSTALLED 152 FROM MAIN DECK FLOOR TO CARGO COMPARTMENT FLOOR, I: 6 YE  CEILINGS 161 BELOW AND 0.5 M FWD AND AFT OF UPPER DECK GALLEYS AND  LDL TOILETS AND 162 TOILETS, FROM FR 53.5 TO FR 80 LH/RH  FURNISHING-IF 171 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  INSTALLED 172 FITTED ABOVE THIS AREA  LD-MCR-IF INSTALLED  LINING  NOTE 1  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 534163-01-2 833 843 151 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE IN T: 6 YE 1+2  FLOOR PANELS 152 LDL AREA FROM FR 53.2 TO R 54A AND FROM STR 37 TO I: 6 YE  INSULATION 153 BOTTOM CENTER LINE, LH/RH, INCLUDING LDL UPPER AND  LDL CEILING 154 LOWER ATTACHMENT POINTS.  LINING NOTE : TASK ONLY APPLICABLE IF LDL INSTALLED.  TOILETS FURNISHING  534164-01-1 N/A TASK DELETED  534165-01-1 N/A TASK DELETED  534166-01-2 N/A TASK DELETED  534166-01-3 N/A TASK DELETED  N 534167-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE  SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 TO STR 6, I: 12 YE  LH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZER  FAIRING  N 534168-01-1 831 841 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3  BARRIER WALL DOORS 262 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM CROWN I: 12 YE  LINING 263 CENTERLINE TO MAIN DECK FLOOR, LH/RH.  NOTE 1 264  271  272  273  274  N 534169-01-1 831 841 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3  BARRIER WALL DOORS 262 FROM FR 53.5 TO FR 80. I: 6 YE  FLOOR PANELS 271  272  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 534177-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE  54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER LINE, I: 3 YE  EXCUDING AREA UNDER VERTICAL STABILIZER FAIRING,  EXTERNAL SURFACE.  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 BULKHEAD FWD T: 6 YE 1+2  172 FACE BELOW MAIN DECK FLOOR LEVEL INCLUDING FR 80/82, I: 6 YE  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 CENTER LINE  535103-01-2 N/A TASK DELETED  R 535104-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2  312 FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 I: 6 YE  LH/RH AND BOTTOM CENTER LINE  535104-02-1 N/A TASK DELETED  535105-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 535106-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1  CEILING PANEL 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YE  NOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN CENTER  TOILETS AND GALLEYS LINE AND AT FR 79 AND FR 80  535107-01-1 312AR 311 DETAILED INSPECTION OF FIN TO FUSELAGE MID AND AFT T: 12 YE 1  312 ATTACH FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE I: 6 YE  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  R 535109-01-1 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  HINGE ARMS 312 HINGE SUPPORT MEMBERS AND UPPER AND LOWER ATTACHMENT I: 20000 FC  LUGS OF FR 91 LH/RH  535110-01-1 312AR 311 DETAILED INSPECTION OF ATTACH FITTINGS FOR HORIZONTAL T: 12 YE T: 20 YE  312 STABILIZER TRIM ACTUATOR BETWEEN FR 86 AND FR 87 I: 12 YE I: 12 YE  R 535111-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE  CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR FROM FR 84 TO I: 6 YE  FR 85 AND BETWEEN STR 27 RH AND STR 39 RH, EXTERNAL  SURFACE  R 535111-02-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE  CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR FROM FR 84 TO I: 6 YE  FR 85 AND BETWEEN STR 27 RH AND STR 39 RH, EXTERNAL  SURFACE  535112-01-1 N/A TASK DELETED  535113-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 535114-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM FR T: 12 YE  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 SURFACE T: 6 YE 1  323BL 323BR 323 UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 6 YE  FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD FITTINGS  R 535116-01-2 321AL 323CL 323CR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE T: 6 YE 1  323DL 323DR 325LL 323 UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 6 YE  325LR 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: TPS APPLICATION IS FROM FR 80/82 TO FR 91 BELOW  STRINGER 25 LH/RH, FROM FR 92 TO FR 95 BELOW STRINGER  13 LH/RH, AND AREA BETWEEN FR 86 AND FR 88 BELOW  STR 15  535118-01-1 312AR 313AL 311 DETAILED INSPECTION OF REAR FUSELAGE T: 12 YE T: 20 YE  312 INTERNAL STRUCTURE AROUND HORIZONTAL STABILIZER I: 6 YE I: 6 YE  CUTOUT BETWEEN 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  R 535121-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YE  NOTE 1 272 FWD FACE ABOVE MAIN DECK FLOOR LEVEL I: 12 YE  TOILETS AND GALLEYS 273  274  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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: 6 YE  312 AFT FACE FROM CROWN TO BOTTOM CENTERLINE I: 6 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 CENTERLINE  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  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 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  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE SECTION: D-53 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545101-02-1 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO  463 THE ENGINE FORWARD MOUNT FITTING I: 6 YE  R 545101-02-2 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO  463 THE ENGINE FORWARD MOUNT FITTING I: 12 YE  545102-04-1 N/A TASK DELETED  545102-05-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO  463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT I: 12 YE  RIB 8C  545102-06-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO  463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT I: 12 YE  RIB 8D  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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INTERVAL 

 TPS

 545103-02-1 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OF T: 20000 FC  463 ARMS AT ENGINE FORWARD MOUNT FITTING. OR  50000 FH  I: 15100 FC  OR  50000 FH  545103-02-2 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 17000 FC  463 END OF ARMS AT ENGINE FORWARD MOUNT FITTING OR  50000 FH  I: 16000 FC  OR  48000 FH  545103-02-3 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OF T: 17000 FC  463 ARMS AT ENGINE FORWARD MOUNT FITTING. OR  50000 FH  I: 14800 FC  OR  50000 FH  R 545104-02-10 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH  I: 11000 FC  OR  50000 FH  R 545104-02-11 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  426AR 426BR 453AZ BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  463AZ I: 11400 FC  OR  50000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 545104-02-15 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  I: 11100 FC  OR  50000 FH  N 545104-02-16 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  426AR 426BR 453AZ BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  463AZ I: 11400 FC  OR  50000 FH  N 545104-02-17 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  I: 14000 FC  OR  42000 FH  N 545104-02-18 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  I: 13300 FC  OR  50000 FH  N 545104-02-19 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  I: 14000 FC  OR  42000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 545104-02-20 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH  I: 13300 FC  OR  50000 FH  545104-02-3 N/A TASK DELETED  545104-02-4 N/A TASK DELETED  545104-02-5 N/A TASK DELETED  R 545104-02-6 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN OR  RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH  I: 11600 FC  OR  34800 FH  R 545104-02-7 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FC  416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  426AR 426BR 453AZ BETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH  463AZ I: 11900 FC  OR  35700 FH  R 545104-02-8 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN OR  RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH  I: 11600 FC  OR  34800 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545104-02-9 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FC  416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS OR  426AR 426BR 453AZ BETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH  463AZ I: 11900 FC  OR  35700 FH  R 545106-01-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE T: 12 YE T: 20 YE NO  426AR 463 I: 6 YE I: 6 YE  545106-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE T: 12 YE T: 20 YE NO  416BR 425AL 425BL 463 I: 6 YE I: 6 YE  426AR 426BR  545108-03-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 6000 FC  OR  21000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545108-03-10 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 OR  426AR 426BR 50000 FH  I: 9300 FC  OR  27800 FH  545108-03-11 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 7200 FC  OR  21700 FH  545108-03-12 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 8600 FC  OR  43000 FH  545108-03-13 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 OR  426AR 426BR 50000 FH  I: 8600 FC  OR  43000 FH  545108-03-14 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 6700 FC  OR  33500 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545108-03-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NO  416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 OR  426AR 426BR 50000 FH  I: 6000 FC  OR  21000 FH  545108-03-3 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 5100 FC  OR  17800 FH  545108-03-4 N/A TASK DELETED  545108-03-5 N/A TASK DELETED  545108-03-6 N/A TASK DELETED  545108-03-7 N/A TASK DELETED  545108-03-8 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545108-03-9 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 OR  50000 FH  I: 9300 FC  OR  27800 FH  R 545108-04-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 12 YE NO  426AR 463 FORWARD MOUNT FITTING TO RIB 1 I: 6 YE  R 545108-04-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 12 YE NO  416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 I: 6 YE  426AR 426BR  545108-04-3 N/A TASK DELETED  545108-04-4 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545110-03-1 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 20000 FC NO  416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C OR  418BR 418CR 425AL 50000 FH  425BL 426AR 426BR I: 20000 FC  427AL 428AR 428BR OR  428CR 50000 FH  545110-03-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO  416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C I: 12 YE  418BR 418CR 425AL  425BL 426AR 426BR  427AL 428AR 428BR  428CR  545110-03-3 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 17000 FC NO  416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C OR  418BR 418CR 425AL 50000 FH  425BL 426AR 426BR I: 17000 FC  427AL 428AR 428BR OR  428CR 50000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545110-04-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 20000 FC NO  418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D OR  427AL 428AR 50000 FH  I: 20000 FC  OR  50000 FH  545110-04-2 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO  418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D I: 12 YE  427AL 428AR  545110-04-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 17000 FC NO  418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D OR  427AL 428AR 50000 FH  I: 17000 FC  OR  50000 FH  R 545111-01-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO  DISASSEMBLED 423 UPPER BEAM AT RIB 9C. I: 12 YE  ENGINE  545111-02-1 N/A TASK DELETED  545111-02-2 N/A TASK DELETED  545115-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545115-02-1 AFT ATTACHMENT BEAM 453 DETAILED INSPECTION OF PYLON LOWER SPAR JUNCTION WITH T: 20000 FC  DISASSEMBLED 463 RIB 9C (GE), 8C (PW), 8D (RR) OR  ENGINE 50000 FH  I: 20000 FC  OR  50000 FH  545115-02-3 AFT ATTACHMENT BEAM 453 DETAILED INSPECTION OF PYLON LOWER SPAR JUNCTION WITH T: 17000 FC  DISASSEMBLED 463 RIB 9C (GE), 8C (PW), 8D (RR). OR  ENGINE 50000 FH  I: 17000 FC  OR  50000 FH  545115-03-1 N/A TASK DELETED  545115-03-2 N/A TASK DELETED  R 545118-02-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO  418AR 425AL 426AR 463 SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 I: 12 YE I: 12 YE  427AL 428AR AND RIB 10)  545118-02-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO  416BR 417AL 418AR 463 SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 I: 12 YE I: 12 YE  425AL 425BL 426AR AND RIB 10)  426BR 427AL 428AR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545119-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO  418AR 425AL 426AR 463 SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) I: 12 YE I: 12 YE  427AL 428AR 454AL AND RIB 18A  464AL  545119-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO  416BR 417AL 418AR 463 SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) I: 12 YE I: 12 YE  425AL 425BL 426AR AND RIB 18A  426BR 427AL 428AR  454AL 464AL  R 545121-02-1 451CL 451CR 451DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  451DR 452AL 452BL 463 SURFACE, BETWEEN RIB 1 AND RIB 10A EXCLUDING I: 12 YE  452BR 452CL 452CR PRECOOLER AREA, AS FAR AS VISIBLE.  461CL 461CR 461DL  461DR 462AL 462BL  462BR 462CL 462CR  R 545121-02-2 451DL 451DR 451EL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  451ER 452AL 452BL 463 SURFACE, BETWEEN RIB 1 AND RIB 10A EXCLUDING I: 12 YE  452BR 452CL 452CR PRECOOLER AREA, AS FAR AS VISIBLE.  461DL 461DR 461EL  461ER 462AL 462BL  462BR 462CL 462CR  R 545122-01-1 451EL 451ER 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  461EL 461ER 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YE  AIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

100% THRESHOLD

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 TPS

 R 545122-01-2 451CL 451CR 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  461CL 461CR 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YE  AIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  R 545122-01-3 452BL 462BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  AIR DUCT 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YE  PRE-COOLER INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  R 545122-01-4 451EL 451ER 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  461EL 461ER 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE  AIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545122-01-5 451CL 451CR 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  461CL 461CR 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE  AIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  R 545122-01-6 452BL 462BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO  AIR DUCT 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE  PRE-COOLER INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUT  COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8  R 545124-02-1 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO  454BR 454CL 454CR 463 SURFACE, BETWEEN RIB 10A AND RIB 15A I: 12 YE  462CL 462CR 464BL  464BR 464CL 464CR  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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INTERVAL 

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 R 545124-02-2 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO  454BR 454CL 454NR 463 SURFACE, BETWEEN RIB 10A AND RIB 15A I: 12 YE  462CL 462CR 464BL  464BR 464CL 464NR  R 545126-02-1 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  464DR 463 SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A I: 12 YE I: 12 YE  R 545126-02-2 454KL 454KR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO  464KR 463 SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A I: 12 YE I: 12 YE  R 545128-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT T: 10 YE NO  464BR 463 FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 I: 10 YE  BEARING  R 545128-01-2 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT T: 10 YE T: 20 YE NO  464BR 463 FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 I: 10 YE I: 10 YE  BEARING  545129-01-1 N/A TASK DELETED  545129-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545129-01-3 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 20000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 9300 FC  OR  32500 FH  545129-01-4 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 20000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 7400 FC  OR  25900 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545129-01-5 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 9500 FC  OR  28500 FH  545129-01-6 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 7600 FC  OR  22800 FH  545129-01-7 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 8500 FC  OR  42600 FH  545129-01-8 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FC  464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 OR  50000 FH  I: 6800 FC  OR  34000 FH  R 545135-01-1 454BL 454BR 454CL 453 GENERAL VISUAL INSPECTION OF PYLON LATERAL PANELS, T: 12 YE NO  454CR 464BL 464BR 463 EXTERNAL SURFACE, EXCLUDING AREA COVERED BY ENGINE I: 6 YE  464CL 464CR COWLS.  545135-01-2 N/A TASK DELETED  545136-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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INTERVAL 

 TPS

 R 545137-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO  416AR 417AL 418AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YE  424AL 424AR 425AL CORE COWLS  426AR 427AL 428AR  R 545137-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO  416BR 417AL 418AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YE  425AL 425BL 426AR CORE COWLS  426BR 427AL 428AR  R 545137-01-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO  418AR 425AL 426AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YE  427AL 428AR CORE COWLS  545137-01-4 N/A TASK DELETED  545137-01-5 N/A TASK DELETED  545137-01-6 N/A TASK DELETED  545138-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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INTERVAL 

 TPS

 545138-01-10 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS T: 17000 FC  OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS OR  DOORS BETWEEN RIB 10 AND RIB 11 50000 FH  I: 7000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545138-02-6 35100 FH  545138-01-2 N/A TASK DELETED  545138-01-3 N/A TASK DELETED  545138-01-4 N/A TASK DELETED  545138-01-5 N/A TASK DELETED  R 545138-01-6 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS OF T: 20000 FC  FASTENERS SECURING SUPPORTS OF FRONT ACCESS DOORS OR  BETWEEN RIB 10 AND RIB 11 50000 FH  I: 12800 FC  OR  50000 FH  545138-01-7 N/A TASK DELETED  545138-01-8 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS OR  DOORS BETWEEN RIB 10 AND RIB 11 50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545138-01-9 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS OF T: 17000 FC  FASTENERS SECURING SUPPORTS OF FRONT ACCESS DOORS OR  BETWEEN RIB 10 AND RIB 11 50000 FH  I: 8000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545138-02-5 24100 FH  545138-02-1 N/A TASK DELETED  545138-02-2 N/A TASK DELETED  545138-02-3 N/A TASK DELETED  545138-02-5 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS OR  DOORS BETWEEN RIB 10 AND RIB 11 50000 FH  I: 16400 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545138-01-9 49300 FH  545138-02-6 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF FRONT OR  ACCESS DOORS BETWEEN RIB 10 AND RIB 11 50000 FH  I: 14300 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545138-01-10 50000 FH  545139-02-1 N/A TASK DELETED  545139-02-2 N/A TASK DELETED  545139-02-3 N/A TASK DELETED  545139-02-4 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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INTERVAL 

 TPS

 545139-02-5 N/A TASK DELETED  545139-02-6 N/A TASK DELETED  545139-02-7 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 20000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS OR  DOORS BETWEEN RIB 13 AND RIB 14 50000 FH  I: 7450 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-03-7 26100 FH  545139-02-8 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS OR  DOORS BETWEEN RIB 13 AND RIB 14 50000 FH  I: 10600 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-03-8 31900 FH  545139-02-9 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREAS T: 17000 FC  OF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS OR  BETWEEN RIB 13 AND RIB 14 50000 FH  I: 9800 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-03-9 49300 FH  545139-03-1 N/A TASK DELETED  545139-03-2 N/A TASK DELETED  545139-03-3 N/A TASK DELETED  545139-03-4 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545139-03-5 N/A TASK DELETED  545139-03-6 N/A TASK DELETED  545139-03-7 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 20000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS OR  DOORS BETWEEN RIB 13 AND RIB 14 50000 FH  I: 20000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-02-7 50000 FH  545139-03-8 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS OR  DOORS BETWEEN RIB 13 AND RIB 14 50000 FH  I: 17000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-02-8 50000 FH  545139-03-9 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  OF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS OR  BETWEEN RIB 13 AND RIB 14 50000 FH  I: 17000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545139-02-9 50000 FH  545140-01-1 N/A TASK DELETED  545140-01-2 N/A TASK DELETED  545140-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545140-01-4 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OR  EXTERNAL SURFACE,LH/RH. 50000 FH  I: 8100 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545140-02-4 24300 FH  545140-01-5 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OR  EXTERNAL SURFACE,LH/RH. 50000 FH  I: 7900 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545140-02-5 39500 FH  545140-02-1 N/A TASK DELETED  545140-02-2 N/A TASK DELETED  545140-02-3 N/A TASK DELETED  545140-02-4 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OR  EXTERNAL SURFACE,LH/RH 50000 FH  I: 17000 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545140-01-4 50000 FH  545140-02-5 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OR  EXTERNAL SURFACE,LH/RH 50000 FH  I: 16500 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR  545140-01-5 50000 FH  R 545142-01-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 6 YE NO  463CR 463 EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND I: 6 YE  INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13  AND RIB 14.  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545142-02-1 N/A TASK DELETED  545142-02-2 N/A TASK DELETED  545142-02-3 N/A TASK DELETED  545142-02-4 N/A TASK DELETED  545142-02-5 N/A TASK DELETED  545142-02-6 N/A TASK DELETED  545142-02-7 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545143-02-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF T: 20000 FC  463BR 463 ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 OR  AND RIB 11 50000 FH  I: 7400 FC  OR  25800 FH  545143-02-2 N/A TASK DELETED  545143-02-3 N/A TASK DELETED  545143-02-4 N/A TASK DELETED  545143-02-5 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545143-02-9 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF T: 17000 FC  463BR 463 ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 OR  AND RIB 11 50000 FH  I: 5100 FC  NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-4 OR  15300 FH  545143-03-1 N/A TASK DELETED  545143-03-2 N/A TASK DELETED  545143-03-4 453BL 453BR 463BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE OR  BETWEEN RIB 10 AND RIB 11 50000 FH  NOTE THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-9 I: 13200 FC  OR  39700 FH  545143-03-5 453BL 453BR 463BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE OR  BETWEEN RIB 10 AND RIB 11 50000 FH  NOTE:THIS TASK IS AN ALTERNATIVE TO TASK 545143-04-1 I: 11500 FC  OR  50000 FH  545143-04-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE OR  BETWEEN RIB 10 AND RIB 11 50000 FH  NOTE THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-4 I: 4450 FC  OR  22300 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545143-04-2 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE OR  BETWEEN RIB 10 AND RIB 11 50000 FH  I: 12100 FC  OR  36300 FH  545143-04-3 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FC  463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE OR  BETWEEN RIB 10 AND RIB 11 50000 FH  I: 10500 FC  OR  50000 FH  545146-02-1 N/A TASK DELETED  545146-02-2 N/A TASK DELETED  545146-02-5 N/A TASK DELETED  545146-02-6 N/A TASK DELETED  545146-03-3 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 12400 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-3 OR  37300 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545146-03-4 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 8800 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-4 OR  26500 FH  545146-03-5 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 11500 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-5 OR  50000 FH  545146-03-6 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 8200 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-6 OR  41000 FH  545146-04-3 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 6750 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-3 OR  20200 FH  545146-04-4 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 4450 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-4 OR  13300 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545146-04-5 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 6250 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-5 OR  31300 FH  545146-04-6 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FC  462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 OR  AIR DUCT NOTE: 50000 FH  PRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 4130 FC  RODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-6 OR  20600 FH  R 545150-02-1 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 20000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 9000 FC  OR  27100 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 545150-02-10 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 20000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 8650 FC  OR  43200 FH  545150-02-2 N/A TASK DELETED  545150-02-6 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 11700 FC  OR  35100 FH  545150-02-7 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 11400 FC  OR  50000 FH  545150-02-8 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 15600 FC  OR  46800 FH  545150-02-9 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FC  AIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 OR  PRE-COOLER 50000 FH  RODS I: 15200 FC  OR  50000 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545154-01-1 454EL 454ER 464EL 453 DETAILED INSPECTION OF PYLON, RIB 18A ASSEMBLY, AFT T: 12 YE T: 20 YE NO  464ER 463 FACE I: 12 YE I: 12 YE  R 545158-01-1 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL T: 12 YE T: 20 YE NO  426AR 453AZ 463AZ 463 STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD I: 6 YE I: 6 YE  FACE  545158-01-2 415BL 416BR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL T: 12 YE T: 20 YE NO  418AR 425BL 426BR 463 STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD I: 6 YE I: 6 YE  427AL 428AR 453AZ FACE  463AZ  545160-01-1 452AL 452BL 452BR 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE T: 20 YE NO  462AL 462BL 462BR 463 BETWEEN RIB 3 AFT FACE AND RIB 8 FORWARD FACE I: 6 YE I: 6 YE  AIR DUCT  PRE-COOLER  RODS  545160-01-2 N/A TASK DELETED  545162-01-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE NO  463BR 463 BETWEEN RIB 8 AFT FACE AND RIB 12 FORWARD FACE I: 6 YE  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545164-01-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE T: 20 YE NO  463CR 463 BETWEEN RIB 12 AFT FACE AND RIB 18A FORWARD FACE I: 6 YE I: 6 YE  545166-02-1 N/A TASK DELETED  545166-02-10 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 3960 FC  OR  19800 FH  545166-02-11 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 7800 FC  OR  23300 FH  545166-02-12 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 8900 FC  OR  44300 FH  N 545166-02-13 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 7050 FC  OR  35400 FH  545166-02-2 N/A TASK DELETED  545166-02-3 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545166-02-4 N/A TASK DELETED  R 545166-02-5 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 8100 FC  OR  24300 FH  545166-02-6 N/A TASK DELETED  545166-02-8 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 4440 FC  OR  13300 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545166-02-9 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  464BR 463 FITTINGS AT RIB 12 OR  50000 FH  I: 7000 FC  OR  34800 FH  545168-02-1 N/A TASK DELETED  545168-02-10 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 3960 FC  OR  19800 FH  545168-02-11 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 7800 FC  OR  23300 FH  545168-02-12 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 8900 FC  OR  44300 FH  N 545168-02-13 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454BR 462CL 462CR 464 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 7050 FC  OR  35400 FH  545168-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545168-02-3 N/A TASK DELETED  545168-02-4 N/A TASK DELETED  R 545168-02-5 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454BR 462CL 462CR 464 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 8100 FC  OR  24300 FH  545168-02-6 N/A TASK DELETED  545168-02-8 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 4440 FC  OR  13300 FH  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545168-02-9 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) OR  464BL 464BR 50000 FH  I: 7000 FC  OR  34800 FH  545170-02-1 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  454BR 462CL 462CR 464 FITTING SLEEVES, LINKS AND BOLTS AT RIB 12 (4 PLACES I: 12 YE  464BL 464BR PER PYLON)  BOLTS  ENGINE  LINKS  SLEEVES  545174-01-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A OR  454ML 454MR 464DL 50000 FH  464DR 464FL 464FR I: 11100 FC  464KL 464KR 464ML OR  464MR 38800 FH  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  R 545174-01-2 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A OR  454ML 454MR 464DL 50000 FH  464DR 464FL 464FR I: 10700 FC  464KL 464KR 464ML OR  464MR 32000 FH  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545174-01-3 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A OR  454ML 454MR 464DL 50000 FH  464DR 464FL 464FR I: 7700 FC  464KL 464KR 464ML OR  464MR 23200 FH  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  545174-01-4 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A OR  464ML 464MR 50000 FH  I: 11000 FC  OR  33000 FH  545174-01-5 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FC  454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A OR  464ML 464MR 50000 FH  I: 10400 FC  OR  50000 FH  N 545174-01-6 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A OR  454ML 454MR 464DL 50000 FH  464DR 464FL 464FR I: 7600 FC  464KL 464KR 464ML OR  464MR 38100 FH  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 545174-01-7 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FC  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A OR  454ML 454MR 464DL 50000 FH  464DR 464FL 464FR I: 10500 FC  464KL 464KR 464ML OR  464MR 50000 FH  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  545174-02-1 N/A TASK DELETED  545174-02-2 N/A TASK DELETED  545174-02-3 N/A TASK DELETED  R 545174-03-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 10 YE NO  454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A I: 10 YE  454ML 454MR 464DL  464DR 464FL 464FR  464KL 464KR 464ML  464MR  BEARINGS  ENGINE  LINKS  POST 43271 (ACCESS  WITH SUFFIX KL, KR,  ML, MR)  PRE 43271 (ACCESS  WITH SUFFIX DL, DR,  FL, FR)  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 545174-03-2 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE T: 20 YE NO  454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A I: 12 YE I: 12 YE  464ML 464MR  BEARINGS  ENGINE  LINKS  R 545180-03-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  454FR 464DL 464DR 464 FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER I: 12 YE  464FL 464FR PYLON)  BOLTS  ENGINE  LINKS  SLEEVES  R 545180-03-2 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO  454MR 464KL 464KR 464 FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER I: 12 YE  464ML 464MR PYLON)  BOLTS  ENGINE  LINKS  SLEEVES  545180-04-1 N/A TASK DELETED  545180-04-2 N/A TASK DELETED  545180-04-3 N/A TASK DELETED  545180-04-4 N/A TASK DELETED  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 545180-04-5 N/A TASK DELETED  545705-02-1 N/A TASK DELETED  545709-01-1 N/A TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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  551002-01-2 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, TRIM T: 20000 FC  312 ACTUATING ARM LUGS AND SUPPORT FITTING LUGS I: 20000 FC  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  551007-01-2 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  R 551008-01-3 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  312 BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE I: 9200 FC  FAIRING LINES OR  37100 FH  551009-01-3 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  REARMOST UPPER 343 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 10600 FC  FAIRING SUPPORT SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, OR  FITTING LH/RH 33900 FH  551009-01-4 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  REARMOST UPPER 343 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 5500 FC  FAIRING SUPPORT SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, OR  FITTING LH/RH 22500 FH  551010-01-2 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  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A330 MRB REPORT – Structures Section

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 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  20000 FC  I: 12 YE  OR  20000 FC  551012-01-2 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE  312 CENTER BOX REAR SPAR AFT FACE BETWEEN RIB 3 LH AND I: 20000 FC I: 12 YE  RIB 3 RH, EXCLUDING INBOARD JOINT PLATES  551013-01-1 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 12 YE 1  312 SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, LH/RH I: 12 YE  334  344  551013-01-4 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 20000 FC  312 SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, LH/RH I: 18300 FC  334 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  344 TASK 551013-02-3 60400 FH  551013-02-3 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 18300 FC  334 LH/RH OR  344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60400 FH  TASK 551013-01-4  R 551015-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE  312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 20000 FC I: 12 YE  RIB 3 RH  N 551015-01-3 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 12 YE  RIB 3 RH  551016-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A330 MRB REPORT – Structures Section

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 551016-01-4 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  312 CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD I: 20000 FC  OF RIB 3, LH/RH.  N 551018-01-3 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 PIPE  N 551018-01-4 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO  319BL 319DR 319ER CENTER BOX INTERNAL STRUCTURE I: 12 YE  N 551019-01-3 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  312 CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 6700 FC  REAR SPAR WEB FROM RIB 3LH TO RIB 3RH OR  26700 FH  551020-01-2 N/A 300 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES OUTBOARD I: 20000 FC  OF FUSELAGE FAIRINGS  551020-02-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES I: 6 YE  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 LH/RH  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 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  N 551024-01-1 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE  333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 12 YE  343AB 343AT RIB 4  R 551024-01-2 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE  333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 20000 FC I: 12 YE  343AB 343AT RIB 4  551025-01-2 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 TO END I: 12 YE  332AT 333AB 333AT 341 RIB AND EXTERNAL SURFACE OF END RIB  341AT 341BT 341CT 342  341DT 341ET 342AB  342AT 343AB 343AT  551026-01-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE  LATERAL BOX TOP SKIN UPPER SURFACE FROM CHORDWISE I: 6 YE  SPLICE LINE TO END RIB  551027-01-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 3 YE  LATERAL BOX BOTTOM SKIN LOWER SURFACE FROM CHORDWISE I: 3 YE  SPLICE LINE TO END RIB  R 551028-01-4 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  343 BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE I: 4700 FC  (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE OR  FAIRINGS 15500 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-4  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 551028-01-5 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  343 BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE I: 6200 FC  (5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE OR  FAIRINGS 20300 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-5  R 551028-02-4 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, I: 8100 FC  FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF OR  FUSELAGE FAIRINGS 33200 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-4  551028-02-5 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, I: 18000 FC  FIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF OR  FUSELAGE FAIRINGS 58900 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-5  R 551029-01-3 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  319BL 319BR 319CR BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO FRONT I: 20000 FC  DISCONNECT SCAVENGE SPAR WEB FROM RIB 3LH TO RIB 3RH  WATER PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 551029-02-3  R 551029-01-4 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FC  319BL 319DR 319ER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO FRONT I: 20000 FC  SPAR WEB FROM RIB 3LH TO RIB 3RH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 551029-02-4  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 R 551029-02-3 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  319BL 319BR 319CR CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 20000 FC  DISCONNECT SCAVENGE FRONT SPAR WEB FROM RIB 3LH TO RIB 3RH  WATER PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 551029-01-3  R 551029-02-4 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC  319BL 319DR 319ER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 20000 FC  FRONT SPAR WEB FROM RIB 3LH TO RIB 3RH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS  TASK 551029-01-4  551030-01-2 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 OUTBOARD I: 6 YE  334GB 344AB 344BB JOINT PLATE TO END RIB  344CB 344DB 344EB  344FB 344GB  551031-01-1 334BB 334CB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 20000 FC T: 6 YE 1  335BB 344BB 344CB 344 FITTINGS NO 2 AND 3 AND SUPPORT RIBS I: 20000 FC I: 6 YE  344DB 345BB  551032-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER ACTUATOR T: 20000 FC T: 6 YE 1  344CT 344 ATTACHMENT FITTING AND REACTION BAR AT RIBS 8 AND 9 I: 20000 FC I: 6 YE  551033-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 20000 FC T: 12 YE 1  334EB 334FB 334GB 344 FITTINGS NO 1,4,5,6 AND 7 AND SUPPORT RIBS I: 20000 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 
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 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 RIB I: 12 YE  343DB 343EB 343FB 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 RIB I: 12 YE  343DB 343EB 343FB 13 LH / END RIB RH  343GB 344GB 346AB  PEELABLE HOLE COVERS  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 I: 12 YE  PEELABLE HOLE COVERS END RIB LH  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 R 552001-01-2 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR TOP AND BOTTOM T: 3 YE  SKIN PANELS INCLUDING TRAILING EDGE, EXTERNAL SURFACE I: 3 YE  552002-01-1 334BB 334CB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO 2 T: 20000 FC T: 6 YE 1  335BB 344BB 344CB 345 AND 3 AND ACTUATOR FITTINGS, LH / RH I: 20000 FC I: 6 YE  344DB 345BB  552003-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR SPAR FORWARD FACE T: 12 YE  334DB 334EB 334FB 345 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 AND I: 6 YE  3 AND AREA OF ACTUATOR FITTINGS, EXTERNAL SURFACE  552005-01-1 334AB 334BB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO T: 20000 FC T: 12 YE 1  334EB 334FB 334GB 345 1,4,5,6 AND 7 I: 20000 FC I: 12 YE  335AB 335CB 335DB  335EB 335FB 344AB  344BB 344DB 344EB  344FB 344GB 345AB  345CB 345DB 345EB  345FB  553004-01-1 N/A TASK DELETED  553005-01-1 N/A TASK DELETED  553008-01-2 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SKIN T: 6 YE  PANELS FROM FRONT TO REAR SPAR AND FROM FIN/FUSELAGE I: 6 YE  FAIRING TO TOP, EXTERNAL SURFACE LH/RH  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
A330 MRB REPORT – Structures Section

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 553009-01-2 325AL 325BL 325CL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YE  325DL 325EL 325FL SPAR AFT FACE INCLUDING SUPPORT FITTINGS FOR RUDDER I: 6 YE  325GL 325HL 325JL HINGE ARMS  325KL  R 553010-01-2 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  553011-01-2 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YE  RIB 8, INCLUDING LOWER SURFACE OF RIB 1  553012-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YE  CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS I: 6 YE  553013-01-2 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 RIB T: 12 YE 1  1 AND RIB 5, METALLIC REINFORCEMENTS AT THE MANHOLES I: 6 YE  553015-01-1 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND SUPPORT T: 6 YE 1  325HL 325KL 326BL 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 SUPPORT T: 6 YE 1  325HL 325KL 326DL FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YE  326DR  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 R 553020-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SKIN T: 6 YE  PANELS FROM FRONT TO REAR SPAR AND FROM FIN/FUSELAGE I: 6 YE  FAIRING TO TOP, EXTERNAL SURFACE LH/RH.  553021-01-1 325LL 325ML 325NL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YE  325PL 325QL 325RL SPAR AFT FACE I: 6 YE  R 553021-01-2 325LL 325NL 325SL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YE  325TL 325UL 325VL SPAR AFT FACE I: 6 YE  553022-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  322DL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YE  FACE.  R 553022-01-2 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  322EL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YE  FACE.  553023-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YE  RIB 5 INCLUDING LOWER SURFACE OF RIB 1.  R 553023-01-2 311AZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YE  STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YE  RIB 5 INCLUDING LOWER SURFACE OF RIB 1.  553024-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YE  323CL 323DL 325LL CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS. I: 6 YE  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 R 553024-01-2 311AZ 312AR 323DL 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YE  323EL 325LL CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS. I: 6 YE  553025-01-1 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  324CT 325ML 325NL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 5 AND I: 12 YE  325PL 325QL 325RL RIB 13.  PEELABLE HOLE COVERS  R 553025-01-2 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YE  324CT 325NL 325SL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 5 AND I: 12 YE  325TL 325UL 325VL RIB 13.  PEELABLE HOLE COVERS  553026-01-1 325LL 325ML 325NL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR T: 6 YE 1  325PL 325QL 325RL SUPPORT FITTINGS. I: 6 YE  326ML 326NL 326PL  326QL  R 553026-01-2 325LL 325NL 325SL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR T: 6 YE 1  325TL 325UL 325VL SUPPORT FITTINGS. I: 6 YE  326ML 326NL 326PL  326RL 326SL  R 554001-01-2 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 
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 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 554005-01-2 N/A TASK DELETED  554006-01-1 N/A TASK DELETED  554007-01-1 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  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  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 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 RUDER 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  N 554014-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0 T: 6 YE  I: 6 YE  R 554020-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YE  EXTERNAL SURFACE LH/RH. I: 6 YE  R 554021-01-1 325LL 325LR 325ML 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YE  325MR 325NL 325NR I: 6 YE  325PL 325PR 325QL  325QR 325RL 325RR  326AT 326ML 326NL  326PL 326QL  PEELABLE HOLE COVERS  R 554021-01-2 325LL 325LR 325NL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YE  325NR 325SL 325TL I: 6 YE  325TR 325UL 325UR  325VL 325VR 326AT  326ML 326NL 326PL  326RL 326SL  PEELABLE HOLE COVERS  D 554022-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 STABILIZERS SECTION: D-55 
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 TPS

 R 554023-01-1 325LL 325ML 325NL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1  325PL 325QL 325RL I: 6 YE  326ML 326NL 326PL  326QL  R 554023-01-2 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 554024-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  BOOSTER AREA, LH/RH. I: 6 YE  N 554025-01-1 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 554026-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YE  AREA OF HOISTING POINTS AND SCREW LINE, LH/RH. I: 6 YE  N 554027-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YE  ATTACH FITTING AREA, LH/RH I: 6 YE  N 554028-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YE  INTERNAL STRUCTURE, LH/RH I: 6 YE  N 554029-01-1 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 
A330 MRB REPORT – Structures Section

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 R 562101-01-2 830 840 221 DETAILED INSPECTION OF MAIN DECK WINDOW PANES T: 6 YE  222 INCLUDING PASSENGER/COURIER/CREW DOOR AND EMERGENCY I: 6 YE  231 EXIT WINDOW PANES  232  241  242  251  252  261  262  271  272  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINDOWS SECTION: D-56 
A330 MRB REPORT – Structures Section

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 571102-01-3 N/A TASK DELETED  571102-01-4 N/A TASK DELETED  571102-01-5 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  AIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 OR  DUCTS LEVEL, LH/RH 50000 FH  LINING I: 5550 FC  NOTE 1 OR  16600 FH  571102-01-6 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FC  AIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 OR  DUCTS LEVEL, LH/RH 50000 FH  LINING I: 5140 FC  NOTE 1 OR  25700 FH  571103-01-3 N/A TASK DELETED  571103-01-4 N/A TASK DELETED  571103-02-3 N/A TASK DELETED  571103-02-4 N/A TASK DELETED  571105-01-1 734 744 143 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN T: 12 YE 1  AIR CONDITIONING 191 LOWER SURFACE FROM FR 40 TO FR 47 BETWEEN RIB 1 LH I: 12 YE  PACKS 192 AND RIB 1 RH  FAIRING PANELS 193  BETWEEN FR 40 AND FR 195  47 196  HEATSHIELDS  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 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  N 571107-01-1 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OR  21, LH/RH 50000 FH  I: 5300 FC  OR  26700 FH  N 571107-01-3 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OR  21, LH/RH 50000 FH  I: 5900 FC  OR  17700 FH  R 571107-01-4 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OR  21, LH/RH 50000 FH  I: 6200 FC  OR  18600 FH  571107-01-5 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  196 LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS OR  20 & 21, LH/RH 50000 FH  I: 5100 FC  OR  25500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571107-01-6 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  196 LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS OR  20 & 21, LH/RH 50000 FH  I: 5770 FC  OR  17300 FH  N 571108-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 8300 FC  OR  25100 FH  R 571108-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 8400 FC  OR  25200 FH  R 571108-01-6 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 7400 FC  OR  37300 FH  R 571108-01-7 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 8150 FC  OR  24500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571108-01-8 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 17000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 7900 FC  OR  23600 FH  571108-01-9 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 17000 FC  744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR  50000 FH  I: 7000 FC  OR  35000 FH  R 571114-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR  28. 50000 FH  I: 13000 FC  OR  39000 FH  R 571114-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 18000 FC  744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR  28. 72000 FH  I: 10900 FC  OR  54500 FH  R 571114-01-7 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 OR  AND 28. 50000 FH  I: 11900 FC  OR  35800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571114-01-8 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR  28. 50000 FH  I: 12000 FC  OR  36000 FH  571114-01-9 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR  28 50000 FH  I: 10600 FC  OR  50000 FH  N 571116-01-2 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN OR  STRINGERS 21 & 22, AT Y =-567.5 50000 FH  I: 5350 FC  OR  26700 FH  N 571116-01-3 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN OR  STRINGERS 21 & 22, AT Y =-567.5 50000 FH  I: 5900 FC  OR  17700 FH  R 571116-01-4 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN OR  STRINGERS 21 & 22, AT Y =-567.5 50000 FH  I: 6200 FC  OR  18600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571116-01-5 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN OR  STRINGERS 21 & 22, AT Y =-567.5 50000 FH  I: 5100 FC  OR  25500 FH  571116-01-6 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN OR  STRINGERS 21 & 22, AT Y =-567.5 50000 FH  I: 5770 FC  OR  17300 FH  571118-01-10 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  BETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR  47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FH  STR 28. I: 5770 FC  OR  17300 FH  N 571118-01-6 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  BETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR  47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FH  STR 28. I: 5350 FC  OR  26700 FH  R 571118-01-7 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  BETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR  47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FH  STR 28. I: 6200 FC  OR  18600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 571118-01-8 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  BETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR  47 STRINGERS 25 & 26, AND AT Y=180 BETWEEN STRINGERS 27 50000 FH  & 28. I: 5900 FC  OR  17700 FH  571118-01-9 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  BETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR  47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FH  STR 28. I: 5100 FC  OR  25500 FH  571119-01-1 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  GALLEYS 146 STRUCTURE, LONGITUDINAL BEAMS ABOVE CWB, WEB HOLE I: 3100 FC  AREA BETWEEN FRAMES 41 AND 42 FROM Y=-1456 TO Y=1456.  (7 BEAMS TO BE INSPECTED)  571121-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FC  148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL I: 8000 FC  BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO  Y=1959. (9 ASSY TO BE INSPECTED)  571121-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL OR  BEAM AT JUNCTION WITH CWB AFT PANEL 50000 FH  FROM Y=-1959 TO Y=1959. (9 ASSY TO BE INSPECTED) I: 8000 FC  OR  24000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571121-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FC  148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL OR  BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO 50000 FH  Y=1959. (9 ASSY TO BE INSPECTED) I: 8000 FC  OR  40000 FH  R 571122-01-4 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER OR  CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 50000 FH  TO Y=1959, LH/RH. I: 4900 FC  OR  14700 FH  571122-01-5 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER OR  CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 50000 FH  TO Y=1959, LH/RH. I: 4380 FC  OR  15300 FH  571122-01-6 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX EXTERN T: 20000 FC  196 STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER CHORD OR  (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO 50000 FH  Y=1959, LH/RH. I: 4270 FC  OR  14900 FH  571122-01-7 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER OR  (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO 50000 FH  Y=1959, LH/RH. I: 4450 FC  OR  13300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571122-01-8 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER OR  CHORD (L FITTING) AND LOWER SKIN JUNCTION, 50000 FH  FROM Y=953 TO Y=1959, LH/RH. I: 3920 FC  OR  19600 FH  R 571125-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 20000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND OR  FRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FH  I: 6150 FC  OR  18500 FH  R 571125-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 18000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND OR  FRAME 47 LOWER CORNER FITTING, LH/RH. 72000 FH  I: 4000 FC  OR  20000 FH  R 571125-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 20000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND OR  FRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FH  I: 4400 FC  OR  13300 FH  571125-01-6 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 17000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND OR  FRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FH  I: 4320 FC  OR  12900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571125-01-7 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 17000 FC  148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND OR  FRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FH  I: 3820 FC  OR  19100 FH  R 571126-01-3 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER. 50000 FH  I: 13600 FC  OR  41000 FH  R 571126-01-4 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER. 50000 FH  I: 10800 FC  OR  54200 FH  R 571126-01-5 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER. 50000 FH  I: 11900 FC  OR  35700 FH  571126-01-6 734 147 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR T: 17000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER. 50000 FH  I: 11400 FC  OR  34300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571126-01-7 734 147 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR T: 17000 FC  SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE OR  LOWER CORNER. 50000 FH  I: 10200 FC  OR  50000 FH  R 571129-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 20000 FC  744 142 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OR  50000 FH  I: 11500 FC  OR  34600 FH  571129-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 20000 FC  744 142 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OR  50000 FH  I: 12000 FC  OR  34700 FH  571129-01-6 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER T: 17000 FC  744 142 SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OR  50000 FH  I: 17000 FC  OR  50000 FH  R 571130-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR  147 50000 FH  148 I: 6900 FC  OR  20700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571130-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR  147 50000 FH  148 I: 7500 FC  OR  26200 FH  571130-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FC  744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR  147 50000 FH  148 I: 7300 FC  OR  25800 FH  571130-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 17000 FC  744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR  147 50000 FH  148 I: 10100 FC  OR  30400 FH  571130-01-7 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 17000 FC  744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR  147 50000 FH  148 I: 9400 FC  OR  46700 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571133-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON T: 20000 FC  744 142 LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS OR  (63 PLACES). 50000 FH  I: 10000 FC  OR  29000 FH  571133-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS T: 17000 FC  744 142 ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTION OR  (63 PLACES). 50000 FH  I: 17000 FC  OR  50000 FH  571137-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR.40, LH/RH. 50000 FH  I: 8000 FC  OR  23200 FH  571137-01-4 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR.40, LH/RH. 50000 FH  I: 8000 FC  OR  40800 FH  571137-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL OR  AT FR.40, LH/RH. 50000 FH  I: 8000 FC  OR  24000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571137-01-6 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM OR  AT FR.40, LH/RH. 50000 FH  I: 8000 FC  OR  40000 FH  571138-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, LOWER L FITTING AT CONNECTION OR  WITH LOWER SKIN PANEL AT KEEL BEAM LEVEL, LH/RH. 50000 FH  I: 8000 FC  OR  23200 FH  R 571140-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 6 YE 1  GALLEYS 146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 6 YE  TOILETS BETWEEN FR 40 AND FR 47  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE  FITTED ABOVE THIS AREA  R 571140-02-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 12 YE 1  146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 12 YE  BETWEEN FR 40 AND FR 47  NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOT  FITTED ABOVE THIS AREA  N 571140-02-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 6 YE 1  146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 6 YE  BETWEEN FR 40 AND FR 47.  571141-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 571144-01-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 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 50000 FH  196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 9600 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 28800 FH  571144-01-2 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 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 50000 FH  196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 11100 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 33200 FH  571144-01-3 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 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 50000 FH  196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5700 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 28100 FH  571144-01-4 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 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 50000 FH  196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, STR. I: 5600 FC  18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 27500 FH  571144-01-5 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 17000 FC  192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR  195 OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 50000 FH  196 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 6200 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH 18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571144-01-6 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 17000 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 50000 FH  196 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5500 FC  STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, OR  LH/RH. 27400 FH  R 571145-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FH  STR.21 AND STR.25 TO 29, LH/RH. I: 7600 FC  OR  22900 FH  571145-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FH  STR.21 AND STR.25 TO 29, LH/RH. I: 9600 FC  OR  28700 FH  R 571145-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FH  STR.21 AND STR.25 TO 29, LH/RH. I: 8150 FC  OR  40700 FH  571145-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FH  STR.21 AND STR.25 TO 29, LH/RH. I: 8900 FC  OR  26800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571145-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, 50000 FH  STR.20, STR.21 AND STR.25 TO 29, LH/RH. I: 7800 FC  OR  39200 FH  R 571145-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD OR  SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, 50000 FH  STR.20, STR.21 AND STR.25 TO 29, LH/RH. I: 9000 FC  OR  27200 FH  571146-01-4 N/A TASK DELETED  571146-01-5 N/A TASK DELETED  571146-01-6 N/A TASK DELETED  R 571146-02-4 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR  195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, 50000 FH  196 STR21 AND STR25 TO STR29, LH/RH. I: 9600 FC  OR  28800 FH  R 571146-02-5 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR  195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, STR21 50000 FH  196 AND STR25 TO STR29, LH/RH. I: 7900 FC  OR  39400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571146-02-6 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR  195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, STR21 50000 FH  196 AND STR25 TO STR29, LH/RH. I: 8300 FC  OR  25000 FH  571146-02-7 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR  195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, 50000 FH  196 STR21 AND STR25 TO STR29, LH/RH. I: 7400 FC  OR  37000 FH  R 571146-02-8 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 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 50000 FH  196 STR25 TO STR29, LH/RH. I: 8650 FC  OR  25900 FH  571148-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL, KEEL BEAM FITTING 4 FIRST BORE HOLES AFT FRAME OR  40 DATUM, LH/RH. 50000 FH  I: 8000 FC  OR  23200 FH  571149-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 OR  DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FH  I: 6100 FC  OR  17600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571149-01-6 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 OR  DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FH  I: 6500 FC  OR  19000 FH  571149-01-7 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 OR  DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FH  I: 6400 FC  OR  18700 FH  571149-01-8 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 OR  DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FH  I: 6400 FC  OR  19100 FH  571149-01-9 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FC  192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 OR  DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FH  I: 5900 FC  OR  29500 FH  571152-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571152-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, OR  RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 50000 FH  FASTENERS 3 TO 12, LH/RH. I: 8000 FC  OR  28000 FH  571152-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, OR  RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE 50000 FH  AT FASTENERS 3 TO 12, LH/RH. I: 8000 FC  OR  24000 FH  571152-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, OR  RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 50000 FH  FASTENERS 3 TO 12, LH/RH. I: 8000 FC  OR  40000 FH  571153-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF OR  SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 50000 FH  WITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 15200 FC  RADIUS ON EACH SIDE OF GUSSET, LH/RH OR  45600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571153-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF OR  SEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 50000 FH  WITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 12900 FC  RADIUS ON EACH SIDE OF GUSSET, LH/RH. OR  64600 FH  R 571154-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX INTERNAL T: 12 YE NO  744 142 STRUCTURE EXCLUDING STRUTS I: 12 YE  571157-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FC  744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, OR  SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN CONNECTION 50000 FH  OF KEEL BEAM FITTING TO PANEL, LH/RH I: 20000 FC  OR  50000 FH  571157-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, OR  SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 50000 FH  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 17000 FC  OR  50000 FH  571158-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 20000 FC  192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN OR  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FH  I: 5310 FC  OR  15900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 571158-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 17000 FC  192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN OR  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FH  I: 5310 FC  OR  15900 FH  571158-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 17000 FC  192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN OR  CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FH  I: 4900 FC  OR  24500 FH  R 571159-01-3 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FC  146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FH  I: 8350 FC  OR  25000 FH  R 571159-01-4 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FC  146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FH  I: 8850 FC  OR  44400 FH  R 571159-01-5 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FC  146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FH  I: 9450 FC  OR  28300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 R 571159-01-6 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FC  146 PORTAL BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FH  I: 9700 FC  OR  29000 FH  R 571159-01-7 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 17000 FC  146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL OR  STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FH  I: 8900 FC  OR  44600 FH  571160-01-1 147AZ 148AZ 141 DETAILED INSPECTION OF CENTER WING BOX, STRUTS (54 T: 12 YE  142 PLACES) I: 12 YE  571165-01-3 N/A TASK DELETED  R 572001-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 5100 FC  OR  23400 FH  572001-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 7000 FC  OR  21900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572001-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 5600 FC  OR  16700 FH  R 572001-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 5400 FC  OR  15900 FH  572001-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 8900 FC  OR  25400 FH  572001-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 7500 FC  OR  34000 FH  572001-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 9400 FC  OR  26300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572001-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FH  REINFORCING I: 7500 FC  OR  34000 FH  572002-01-10 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 9800 FC  OR  44400 FH  572002-01-11 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 7800 FC  OR  24400 FH  572002-01-12 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 12300 FC  OR  34300 FH  572002-01-13 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 8400 FC  OR  33700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572002-01-4 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 8400 FC  OR  33700 FH  572002-01-5 454DL 454DR 454FL 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454FR 464DL 464DR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464FL 464FR 462 50000 FH  464 I: 8300 FC  OR  26000 FH  572002-01-6 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 8400 FC  OR  26300 FH  R 572002-01-8 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 NOTE 8  I: 8300 FC  OR  26000 FH  572002-01-9 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR  464ML 464MR 462 50000 FH  464 I: 11600 FC  OR  33100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572003-01-10 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464CR 50000 FH  I: 20000 FC  OR  50000 FH  R 572003-01-4 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454NR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464NR 50000 FH  I: 6200 FC  OR  28100 FH  R 572003-01-5 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464CR 50000 FH  I: 7000 FC  OR  21900 FH  R 572003-01-6 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464CR 50000 FH  I: 6700 FC  OR  20000 FH  R 572003-01-7 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464CR 50000 FH  I: 6400 FC  OR  19100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572003-01-9 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OR  464CL 464CR 50000 FH  I: 17000 FC  OR  50000 FH  R 572003-02-2 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  454CR 464BL 464BR 464 LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING I: 12 YE  464CL 464CR PLATE  R 572003-02-3 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  454NR 464BL 464BR 464 LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING I: 12 YE  464CL 464NR PLATE  572004-02-1 N/A TASK DELETED  R 572004-02-3 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FH  REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 8100 FC  FAIRING OR  24000 FH  572004-02-4 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 572004-02-6 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FH  REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 6800 FC  FAIRING OR  19500 FH  572004-02-7 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FH  REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 5800 FC  FAIRING OR  26200 FH  572004-02-8 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FH  REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 7300 FC  FAIRING OR  20200 FH  572004-02-9 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FH  REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 5800 FC  FAIRING OR  26200 FH  572005-01-10 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 8000 FC  OR  22700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572005-01-11 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 6700 FC  OR  30400 FH  572005-01-12 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 4900 FC  OR  15300 FH  572005-01-13 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 8400 FC  OR  23500 FH  572005-01-14 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 6700 FC  OR  30400 FH  572005-01-6 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 6700 FC  OR  21000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572005-01-7 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 6800 FC  OR  27300 FH  R 572005-01-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 9700 FC  OR  28700 FH  R 572005-01-9 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING OR  GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FH  SPAR. I: 9700 FC  OR  28700 FH  572006-01-1 N/A TASK DELETED  572006-01-2 N/A TASK DELETED  572006-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 6 YE NO  600 MAIN LANDING GEAR REINFORCING PLATE I: 6 YE  572006-02-2 N/A TASK DELETED  572006-02-3 N/A TASK DELETED  572006-02-4 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572006-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 17000 FC  600 MAIN LANDING GEAR REINFORCING PLATE OR  50000 FH  I: 14100 FC  OR  40000 FH  572006-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 17000 FC  600 MAIN LANDING GEAR REINFORCING PLATE OR  50000 FH  I: 11900 FC  OR  50000 FH  572006-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 20000 FC  600 MAIN LANDING GEAR REINFORCING PLATE OR  50000 FH  I: 14900 FC  OR  41500 FH  572006-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 20000 FC  600 MAIN LANDING GEAR REINFORCING PLATE OR  50000 FH  I: 11900 FC  OR  53600 FH  572007-01-1 N/A TASK DELETED  572007-01-10 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH  631 I: 9400 FC  OR  42700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572007-01-11 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH  631 I: 11800 FC  OR  33000 FH  572007-01-12 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH  631 I: 9400 FC  OR  42700 FH  572007-01-4 N/A TASK DELETED  R 572007-01-5 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH  631 I: 13800 FC  OR  40800 FH  572007-01-6 N/A TASK DELETED  572007-01-7 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 12 YE T: 20 YE  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY I: 12 YE I: 12 YE  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING.  631  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572007-01-9 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR  531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH  631 I: 11200 FC  OR  31900 FH  572008-01-10 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6900 FC  OR  31300 FH  572008-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 7100 FC  OR  28500 FH  R 572008-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6900 FC  OR  20500 FH  572008-01-5 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 7000 FC  OR  21900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572008-01-6 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8200 FC  OR  23400 FH  572008-01-7 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6900 FC  OR  31300 FH  572008-01-8 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6500 FC  OR  20300 FH  572008-01-9 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8700 FC  OR  24200 FH  572008-02-1 531AB 631AB 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  631 LOWER SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY I: 12 YE  FLAP TRACK 2 FAIRING.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572009-01-10 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 8800 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  24600 FH  572009-01-11 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 7000 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 31800 FH  572009-02-11  572009-01-4 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 5400 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 21700 FH  572009-01-5 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 4100 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5 12800 FH  572009-01-6 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 5300 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6 16600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572009-01-7 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 8300 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-7 23700 FH  572009-01-8 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 7000 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-8 31800 FH  572009-01-9 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), OR  INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FH  FAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 4900 FC  8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-9 15300 FH  572009-02-1 N/A TASK DELETED  572009-02-2 N/A TASK DELETED  572009-02-4 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 12400 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  2-3) 49800 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572009-02-5 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 7600 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  2-3) 23800 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5  572009-02-6 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 12200 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  (2-3) 38200 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6  572009-02-7 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 17000 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  (2-3) 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-7  572009-02-8 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 17000 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  (2-3) 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-8  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572009-02-9 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY OR  INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FH  FAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 11400 FC  BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR  (2-3) 35700 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-9  572010-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO  541DB 541EB 541FB 641 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUTS I: 12 YE I: 12 YE  641AB 641BB 641CB IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12.  641DB 641EB 641FB  572010-02-10 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 10000 FC  OR  27900 FH  572010-02-11 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 8000 FC  OR  36000 FH  R 572010-02-4 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 6400 FC  OR  29100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572010-02-5 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 8500 FC  OR  26600 FH  R 572010-02-6 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 6900 FC  OR  20500 FH  R 572010-02-7 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 6700 FC  OR  20000 FH  572010-02-8 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 9400 FC  OR  26900 FH  572010-02-9 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH  641DB 641EB 641FB 11-12. I: 8000 FC  OR  36000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572011-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 6100 FC  OR  24500 FH  572011-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 5700 FC  OR  17800 FH  572011-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 6000 FC  OR  18800 FH  572011-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 10100 FC  OR  28800 FH  572011-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 8500 FC  OR  38600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572011-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 5600 FC  OR  17500 FH  572011-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 10700 FC  OR  29800 FH  572011-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 OR  AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FH  I: 8500 FC  OR  38600 FH  R 572012-02-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 4700 FC  PLATE. OR  21400 FH  R 572012-02-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 6300 FC  PLATE. OR  18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 572012-02-3 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 5100 FC  PLATE. OR  15000 FH  R 572012-02-4 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 4800 FC  PLATE. OR  14300 FH  572012-02-5 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 9000 FC  PLATE. OR  25500 FH  572012-02-6 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 7600 FC  PLATE. OR  34200 FH  572012-02-7 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 9500 FC  PLATE. OR  26500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572012-02-8 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 OR  AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FH  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 7600 FC  PLATE. OR  34200 FH  572012-03-1 N/A TASK DELETED  572012-03-2 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 RIB I: 6 YE  10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING  AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING  PLATE.  R 572013-03-1 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6400 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 29300 FH  464HR 464KL 464KR  464ML 464MR 464NR  R 572013-03-2 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454CR 454DL 454DR 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454FL 454FR 454GL AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454GR 454HL 454HR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6300 FC  464BL 464BR 464CL OR  464CR 464DL 464DR 18700 FH  464FL 464FR 464GL  464GR 464HL 464HR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 572013-03-3 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7100 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 21100 FH  464HR 464KL 464KR  464ML 464MR 464NR  R 572013-03-4 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6600 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 19600 FH  464HR 464KL 464KR  464ML 464MR 464NR  572013-03-5 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 9000 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 25500 FH  464HR 464KL 464KR  464ML 464MR 464NR  572013-03-6 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7600 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 34200 FH  464HR 464KL 464KR  464ML 464MR 464NR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572013-03-7 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 9500 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 26500 FH  464HR 464KL 464KR  464ML 464MR 464NR  572013-03-8 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR  454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH  454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7600 FC  464BL 464BR 464CL OR  464GL 464GR 464HL 34200 FH  464HR 464KL 464KR  464ML 464MR 464NR  R 572013-04-1 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454CR 454DL 454DR 464 LOWER SURFACE IN AREA COVERED BY PYLON FAIRING, I: 12 YE  454FL 454FR 454GL EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND  454GR 454HL 454HR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.  464BL 464BR 464CL  464CR 464DL 464DR  464FL 464FR 464GL  464GR 464HL 464HR  R 572013-04-2 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE  454GL 454GR 454HL 464 LOWER SURFACE IN AREA COVERED BY PYLON FAIRING, I: 12 YE  454HR 454KL 454KR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND  454ML 454MR 454NR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.  464BL 464BR 464CL  464FR 464GL 464HL  464HR 464KL 464KR  464ML 464MR 464NR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572014-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 6600 FC  OR  26500 FH  R 572014-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 7900 FC  OR  23300 FH  572014-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 6600 FC  OR  20700 FH  572014-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 8400 FC  OR  23900 FH  572014-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 7100 FC  OR  32000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572014-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 6100 FC  OR  19100 FH  572014-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FH  COVERED BY FAIRINGS. I: 8900 FC  OR  24800 FH  572014-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING 50000 FH  AREAS COVERED BY FAIRINGS. I: 7100 FC  OR  32000 FH  572015-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO  600 SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR I: 6 YE  AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.  R 572015-02-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 6800 FC  OR  31200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572015-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 6600 FC  OR  19600 FH  R 572015-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 8100 FC  OR  23900 FH  R 572015-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 6900 FC  OR  20500 FH  572015-02-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 8500 FC  OR  24300 FH  572015-02-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 7200 FC  OR  32600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572015-02-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 9000 FC  OR  25200 FH  572015-02-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT OR  SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FH  I: 7200 FC  OR  32600 FH  572016-01-1 N/A TASK DELETED  572016-01-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN VISIBLE T: 6 YE NO  600 SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB I: 6 YE  4.  572016-02-10 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 9500 FC  OR  26400 FH  572016-02-11 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 7600 FC  OR  34200 FH  572016-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 572016-02-4 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 3100 FC  OR  14200 FH  R 572016-02-5 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 4600 FC  OR  13600 FH  R 572016-02-6 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 3500 FC  OR  10400 FH  D 572016-02-7 N/A TASK DELETED  572016-02-8 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 9000 FC  OR  25500 FH  572016-02-9 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 OR  AND RIB 4. 50000 FH  I: 7600 FC  OR  34200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 572017-01-10 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR  50000 FH  I: 19700 FC  OR  50000 FH  R 572017-01-11 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR  50000 FH  I: 15700 FC  OR  50000 FH  572017-01-4 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. OR  50000 FH  I: 7000 FC  OR  28100 FH  572017-01-5 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. OR  50000 FH  I: 7900 FC  OR  24700 FH  572017-01-6 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. OR  50000 FH  I: 6800 FC  OR  21300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 572017-01-7 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 17000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR  50000 FH  I: 15700 FC  OR  50000 FH  572017-01-8 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 17000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR  50000 FH  I: 17000 FC  OR  50000 FH  572017-01-9 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FC  641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR  50000 FH  I: 6300 FC  OR  19700 FH  572017-02-2 541AB 641AB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641 ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. I: 12 YE  572018-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ & 20. I: 9200 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 41600 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 572018-01-11 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH  541FZ 641AB 641AZ & 20 I: 7300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 21600 FH  641EZ 641FZ  N 572018-01-12 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ 20 I: 7700 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 22700 FH  641EZ 641FZ  R 572018-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ 20. I: 7100 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 32300 FH  641EZ 641FZ  R 572018-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ 20. I: 7300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 21700 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572018-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ 20. I: 10900 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 31000 FH  641EZ 641FZ  572018-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ 20. I: 10900 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 31000 FH  641EZ 641FZ  572018-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  541FZ 641AB 641AZ & 20. I: 9300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 41600 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 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING I: 12 YE  541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &  541FZ 641AB 641AZ 20.  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572019-01-10 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH  & 20. I: 6900 FC  OR  31100 FH  R 572019-01-11 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH  & 20. I: 5600 FC  OR  16600 FH  N 572019-01-12 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 20 50000 FH  I: 5900 FC  OR  17500 FH  R 572019-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  20. I: 5400 FC  OR  24900 FH  R 572019-01-6 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  20. I: 7300 FC  OR  21700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572019-01-7 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  20. I: 8100 FC  OR  23200 FH  572019-01-8 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH  20. I: 8200 FC  OR  23200 FH  572019-01-9 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING OR  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH  & 20. I: 6900 FC  OR  31100 FH  572019-02-2 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING I: 12 YE  STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &  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.  572021-03-1 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 7600 FC  OR  30500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572021-03-2 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 10200 FC  OR  30300 FH  572021-03-3 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 7600 FC  OR  23800 FH  572021-03-4 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 10800 FC  OR  30800 FH  572021-03-5 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING 50000 FH  631AB 631 AND FLAP TRACK 2 FAIRING. I: 9100 FC  OR  41200 FH  572021-03-6 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  454GR 464FL 464FR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 7100 FC  OR  22200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572021-03-7 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 11400 FC  OR  31900 FH  572021-03-8 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH  631AB 631 FLAP TRACK 2 FAIRING. I: 9100 FC  OR  41200 FH  R 572021-04-1 454FL 454FR 454GL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  454GR 464FL 464FR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND I: 12 YE  464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND  631AB 631 FLAP TRACK 2 FAIRING.  R 572021-04-2 454GL 454GR 454ML 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  454MR 464GL 464GR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND I: 12 YE  464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND  631AB 631 FLAP TRACK 2 FAIRING.  D 572022-01-4 N/A TASK DELETED  D 572022-01-5 N/A TASK DELETED  D 572022-01-6 N/A TASK DELETED  D 572022-01-7 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 D 572022-01-8 N/A TASK DELETED  D 572022-01-9 N/A TASK DELETED  572023-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  600 AT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM I: 6 YE  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.  572023-01-2 N/A TASK DELETED  572023-02-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 6900 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR  31300 FH  R 572023-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3600 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR  16500 FH  R 572023-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 4000 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR  12000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572023-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3900 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR  11600 FH  R 572023-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3700 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR  11000 FH  572023-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 17000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 8200 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR  23400 FH  572023-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 17000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 6900 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR  31300 FH  572023-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FC  600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM OR  FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FH  PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 8700 FC  GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR  24200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572025-01-3 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641AB 641BB 641CB 641 STRINGER JOINTS AT STRINGER 11 BETWEEN RIBS 3 AND 4 OR  AND STRINGERS 12 AND 14 BETWEEN RIBS 5 AND 6. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7000 FC  TASK 572025-02-3 OR  21900 FH  572025-02-3 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641AB 641BB 641CB 641 STRINGER JOINTS AT STRINGER 11 BETWEEN RIBS 3 AND 4 OR  NUT REMOVAL AS PER AND STRINGERS 12 AND 14 BETWEEN RIBS 5 AND 6. 50000 FH  NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7000 FC  TASK 572025-01-3 OR  21900 FH  572026-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 10100 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 28200 FH  641EZ 641FZ  572026-01-11 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND R OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 8100 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 36500 FH  641EZ 641FZ  572026-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 9000 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 36200 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572026-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 7000 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 21900 FH  641EZ 641FZ  572026-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 9000 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 28200 FH  641EZ 641FZ  572026-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 9600 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 27200 FH  641EZ 641FZ  572026-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 8100 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 36500 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572026-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR  541DB 541DZ 541EZ 50000 FH  541FZ 641AB 641AZ I: 8400 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 26300 FH  641EZ 641FZ  572026-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  541BZ 541CB 541CZ 641 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  R 572027-01-10 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 6500 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 19200 FH  641EZ 641FZ  572027-01-11 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 14300 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 39700 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572027-01-12 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 11400 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50000 FH  641EZ 641FZ  R 572027-01-5 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 6200 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 28300 FH  641EZ 641FZ  R 572027-01-6 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 8600 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 25600 FH  641EZ 641FZ  572027-01-7 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 7400 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 23200 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572027-01-8 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 13500 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 38300 FH  641EZ 641FZ  572027-01-9 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR  541DB 541DZ 541EZ AND RIB 9. 50000 FH  541FZ 641AB 641AZ I: 11400 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50000 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 & STRINGER 20 BETWEEN RIB 1 I: 12 YE  541DB 541DZ 541EZ AND RIB 9.  541FZ 641AB 641AZ  641BB 641BZ 641CB  641CZ 641DB 641DZ  641EZ 641FZ  572028-01-3 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8. OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572028-02-3 I: 7000 FC  OR  21900 FH  572028-02-3 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  NTM TASK 572028-01-3 I: 7000 FC  OR  21900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572029-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  RIB 12 50000 FH  I: 9100 FC  OR  40000 FH  572029-01-3 N/A TASK DELETED  572029-01-4 N/A TASK DELETED  572029-01-5 N/A TASK DELETED  572029-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 OR  AND RIB 12. 50000 FH  I: 11000 FC  OR  31200 FH  572029-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OR  1 AND RIB 12 50000 FH  I: 9100 FC  OR  40000 FH  572029-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR  RIB 12 50000 FH  I: 11800 FC  OR  32500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 572030-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND OR  RIB 11 50000 FH  I: 20000 FC  OR  50000 FH  D 572030-01-4 N/A TASK DELETED  572030-01-5 N/A TASK DELETED  572030-01-6 N/A TASK DELETED  572030-01-7 N/A TASK DELETED  572030-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND OR  RIB 11 50000 FH  I: 17000 FC  OR  50000 FH  D 572032-01-11 N/A TASK DELETED  R 572032-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 7. 50000 FH  I: 11800 FC  OR  53700 FH  572032-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572032-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 7. 50000 FH  I: 9500 FC  OR  28200 FH  R 572032-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 7. 50000 FH  I: 10000 FC  OR  28500 FH  572032-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 7. 50000 FH  I: 10000 FC  OR  28500 FH  572032-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND OR  RIB 7 50000 FH  I: 8300 FC  OR  36600 FH  572033-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 12200 FC  OR  33400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

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 572033-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 9300 FC  OR  41100 FH  R 572033-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 6600 FC  OR  30100 FH  R 572033-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 8600 FC  OR  25500 FH  R 572033-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 6600 FC  OR  19700 FH  R 572033-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 6000 FC  OR  17800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 572033-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 11300 FC  OR  32000 FH  572033-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 9300 FC  OR  41100 FH  572033-02-2 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.  572034-01-4 N/A TASK DELETED  572034-01-5 N/A TASK DELETED  572034-01-6 N/A TASK DELETED  572034-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEEN OR  RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 50000 FH  BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 I: 17000 FC  AND 13 OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 572034-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEEN OR  RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 50000 FH  BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 I: 20000 FC  AND 13. OR  50000 FH  572035-01-4 N/A TASK DELETED  572035-01-5 N/A TASK DELETED  572035-01-6 N/A TASK DELETED  572035-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO OR  RIB 8. 50000 FH  I: 17000 FC  OR  50000 FH  572035-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 OR  TO RIB 8. 50000 FH  I: 20000 FC  OR  50000 FH  572036-01-10 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT OR  TO REAR SPARS. 50000 FH  I: 20000 FC  OR  50000 FH  D 572036-01-4 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572036-01-5 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FC  641AB 641AZ 641BZ 641 CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR OR  SPARS. 50000 FH  I: 12700 FC  OR  37700 FH  572036-01-6 N/A TASK DELETED  572036-01-8 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO OR  REAR SPARS. 50000 FH  I: 15900 FC  OR  50000 FH  572036-01-9 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT OR  TO REAR SPARS. 50000 FH  I: 17000 FC  OR  50000 FH  572036-02-2 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.  572037-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FC  541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO OR  541DB 541DZ 541EZ REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 12800 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 46200 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572037-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FC  541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO OR  541DB 541DZ 541EZ REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 11900 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 37900 FH  641EZ 641FZ  572037-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FC  541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO OR  541DB 541DZ 541EZ REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 12400 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 39500 FH  641EZ 641FZ  572037-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 17000 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50000 FH  641EZ 641FZ  572037-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 12200 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 38800 FH  641EZ 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572037-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OR  541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FH  541FZ 641AB 641AZ I: 20000 FC  641BB 641BZ 641CB OR  641CZ 641DB 641DZ 50000 FH  641EZ 641FZ  572037-02-2 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  572038-02-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO  641FB 641 LOWER SURFACE, PYLON REINFORCING PLATE . I: 12 YE  572039-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 10800 FC  OR  29700 FH  572039-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 8300 FC  OR  36600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572039-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 14600 FC  OR  66500 FH  R 572039-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 16400 FC  OR  48900 FH  R 572039-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 16300 FC  OR  48500 FH  R 572039-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 14800 FC  OR  44000 FH  572039-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 10000 FC  OR  28500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572039-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 OR  AND FROM RIB 11 TO 12. 50000 FH  I: 8300 FC  OR  36600 FH  R 572040-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND OR  RIB 13. 91100 FH  I: 13500 FC  OR  61500 FH  R 572040-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND OR  RIB 13. 50000 FH  I: 11000 FC  OR  32900 FH  R 572040-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND OR  RIB 13. 50000 FH  I: 16100 FC  OR  47800 FH  R 572040-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND OR  RIB 13. 50000 FH  I: 15100 FC  OR  44900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572040-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND OR  RIB 13. 50000 FH  I: 17000 FC  OR  50000 FH  572040-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 OR  AND RIB 13. 50000 FH  I: 20000 FC  OR  50000 FH  572041-01-1 573DB 573FB 673DB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE  673FB 573 FACE BETWEEN RIB 1 AND RIB 12. I: 12 YE  FLAPS EXTENDED 671  673  572043-01-10 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 20000 FC  673 FACE SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 10900 FC  OR  30400 FH  R 572043-01-11 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 20000 FC  673 FACE SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 8600 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572043-01-4 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  673 SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 10300 FC  OR  47600 FH  R 572043-01-5 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  673 SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 5800 FC  OR  18500 FH  R 572043-01-6 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  673 SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 11100 FC  OR  35600 FH  R 572043-01-7 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  673 SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 9400 FC  OR  30000 FH  572043-01-8 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FC  673 SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 10000 FC  OR  31500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572043-01-9 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 17000 FC  673 FACE SPAR JOINT PLATE AT RIB 9. OR  50000 FH  I: 8600 FC  OR  50000 FH  572043-02-2 573FB 673FB 573 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE  673 FACE SPAR JOINT PLATE AT RIB 9. I: 12 YE  572045-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  641AB 641AZ 641BZ 641 FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YE  R 572046-01-4 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND OR  641AB 641BB 641CB BOTTOM FLANGE. 50000 FH  641DB 641EB 641FB I: 5400 FC  OR  24900 FH  572046-01-5 N/A TASK DELETED  572046-01-6 N/A TASK DELETED  572046-01-7 N/A TASK DELETED  R 572046-01-8 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FC  541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND OR  641AB 641BB 641CB BOTTOM FLANGE. 50000 FH  641DB 641EB 641FB I: 8000 FC  OR  25100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572046-01-9 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FC  541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND OR  641AB 641BB 641CB BOTTOM FLANGE. 50000 FH  641DB 641EB 641FB I: 6900 FC  OR  40600 FH  572046-02-2 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 FLANGE.  641DB 641EB 641FB  572047-01-11 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR  641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 50000 FH  641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7 I: 13100 FC  SEALANT REMOVAL AS OR  PER NTM 36400 FH  572047-01-3 N/A TASK DELETED  D 572047-01-4 N/A TASK DELETED  572047-01-5 N/A TASK DELETED  572047-01-6 N/A TASK DELETED  R 572047-01-7 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR  641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 50000 FH  641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7. I: 12000 FC  SEALANT REMOVAL AS OR  PER NTM 37300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572047-01-8 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR  641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 100500 FH  641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7. I: 10300 FC  SEALANT REMOVAL AS OR  PER NTM 60900 FH  R 572047-01-9 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR  641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 118200 FH  641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7 I: 10300 FC  SEALANT REMOVAL AS OR  PER NTM 60900 FH  572047-02-2 541AB 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR 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 SIDESTAY  641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.  N 572048-01-1 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9. OR  50000 FH  I: 10300 FC  OR  47600 FH  N 572048-01-2 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 OR  50000 FH  I: 5800 FC  OR  18500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572048-01-3 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 OR  50000 FH  I: 11100 FC  OR  35600 FH  N 572048-01-4 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 OR  50000 FH  I: 9400 FC  OR  30000 FH  572049-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 13600 FC  OR  38000 FH  572049-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 10800 FC  OR  50000 FH  R 572049-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  92100 FH  I: 15500 FC  OR  71400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 R 572049-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 8700 FC  OR  27800 FH  R 572049-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  63900 FH  I: 16700 FC  OR  53400 FH  R 572049-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 14100 FC  OR  45000 FH  572049-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 12500 FC  OR  39300 FH  572049-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR  50000 FH  I: 10800 FC  OR  50000 FH  572050-01-4 N/A TASK DELETED  572050-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572050-01-6 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  FLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER OR  671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FH  673 I: 7200 FC  OR  23200 FH  572050-01-7 N/A TASK DELETED  572050-01-8 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FC  FLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER OR  671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FH  673 I: 17000 FC  OR  50000 FH  572050-01-9 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  FLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER OR  671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FH  673 I: 20000 FC  OR  50000 FH  572051-01-10 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. OR  PER NTM 50000 FH  I: 17000 FC  OR  50000 FH  572051-01-11 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. OR  PER NTM 50000 FH  I: 20000 FC  OR  50000 FH  572051-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572051-01-6 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  SEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. OR  PER NTM 50000 FH  I: 5200 FC  OR  16600 FH  572051-01-7 N/A TASK DELETED  572051-01-8 N/A TASK DELETED  572052-01-4 N/A TASK DELETED  572052-01-5 N/A TASK DELETED  572052-01-6 N/A TASK DELETED  572052-01-7 N/A TASK DELETED  572052-01-8 N/A TASK DELETED  572052-02-2 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 FLANGE.  572052-03-1 N/A TASK DELETED  572052-03-2 N/A TASK DELETED  572052-03-3 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572052-03-4 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP OR  SEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FH  PER NTM I: 7700 FC  OR  24600 FH  572052-03-5 N/A TASK DELETED  R 572052-03-6 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP OR  SEALANT REMOVAL AS AND BOTTOM FLANGE. 50000 FH  PER NTM I: 9200 FC  OR  28700 FH  572052-03-7 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP OR  SEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FH  PER NTM I: 9200 FC  OR  28700 FH  572052-03-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP OR  SEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FH  PER NTM I: 7900 FC  OR  46400 FH  572054-01-10 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. OR  50000 FH  I: 7400 FC  OR  43600 FH  572054-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 D 572054-01-6 N/A TASK DELETED  572054-01-7 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. OR  50000 FH  I: 8300 FC  OR  26600 FH  572054-01-8 N/A TASK DELETED  572054-01-9 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. OR  50000 FH  I: 8600 FC  OR  27000 FH  572061-01-2 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 ALL I: 6 YE  521GB 521HB 521JB 621 CUTOUTS AND IN VICINITY OF FORWARD PYLON ATTACHMENT  522AB 522BB 522CB 622 FITTING IN REGION OF RIB BAY 10-10A AND BUILD DOOR.  522DB 522EB 621AB  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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572063-01-10 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 7300 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  43000 FH  N 572063-01-11 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 8500 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12 OR  26600 FH  R 572063-01-5 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 5500 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  25600 FH  R 572063-01-6 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 6600 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  21300 FH  R 572063-01-7 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 6100 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  19700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572063-01-8 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 5700 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  18400 FH  572063-01-9 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FC  541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OR  641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH  641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 17000 FC  AND SPAR JOINT BOLTING INBOARD OF RIB 12. OR  50000 FH  572063-02-2 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 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF  641DB 641EB 641FB FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB  BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB  R 572064-01-10 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  640 BETWEEN RIB 8 AND RIB 10,INCLUDING TOP AND BOTTOM OR  FLANGES 50000 FH  I: 7300 FC  OR  43000 FH  R 572064-01-5 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM OR  FLANGES 50000 FH  I: 6900 FC  OR  31700 FH  572064-01-6 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572064-01-7 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM OR  FLANGES. 50000 FH  I: 8500 FC  OR  26000 FH  R 572064-01-8 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FC  640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM OR  FLANGES. 50000 FH  I: 10000 FC  OR  31300 FH  R 572064-01-9 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FC  640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM OR  FLANGES. 50000 FH  I: 8600 FC  OR  43400 FH  R 572064-02-2 541EB 641EB 540 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO  640 AFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND I: 12 YE  BOTTOM FLANGES  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572065-01-1 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OR I: 6 YE  20000 FC  OR  50000 FH  I: 6 YE  OR  20000 FC  OR  50000 FH  R 572065-01-4 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 20000 FC  622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OR  50000 FH  I: 14600 FC  OR  46800 FH  572065-01-5 N/A TASK DELETED  572065-01-6 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OR I: 6 YE  17000 FC  OR  50000 FH  I: 6 YE  OR  17000 FC  OR  50000 FH  R 572065-01-7 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  622EB 622 FACE SPAR JOINT PLATE AT RIB 12. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572066-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OR  50000 FH  I: 20000 FC  OR  50000 FH  R 572066-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OR  50000 FH  I: 14600 FC  OR  46800 FH  572066-01-6 N/A TASK DELETED  572066-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 17000 FC  600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OR  50000 FH  I: 17000 FC  OR  50000 FH  572067-01-10 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 17000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 17000 FC  OR  50000 FH  572067-01-11 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 17000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572067-01-13 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 18600 FC  OR  50000 FH  572067-01-14 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  50000 FH  572067-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  R 572067-01-5 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 8100 FC  OR  23000 FH  D 572067-01-6 N/A TASK DELETED  572067-01-8 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572067-01-9 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  572067-02-2 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6 FORWARD T: 12 YE NO  541FZ 641CB 641DB 641 AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING I: 12 YE  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS  AND ACCESS CUTOUT SURROUNDS.  572068-01-11 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 18600 FC  OR  50000 FH  572068-01-12 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  50000 FH  572068-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FC  541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  572068-01-5 N/A TASK DELETED  D 572068-01-6 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572068-01-7 N/A TASK DELETED  572068-01-8 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 17000 FC  541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 17000 FC  OR  50000 FH  572068-01-9 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 17000 FC  541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FH  AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  50000 FH  572068-02-2 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7 FORWARD T: 12 YE NO  541FZ 641CB 641DB 641 AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING I: 12 YE  641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS  AND ACCESS CUTOUT SURROUNDS.  572069-01-10 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 17000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  50000 FH  R 572069-01-11 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 62800 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 17100 FC  OR  53700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572069-01-12 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 117900 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 14700 FC  OR  86700 FH  N 572069-01-13 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS,SPAR ATTACHMENTS, REGION OF STRINGER 50000 FH  CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  R 572069-01-4 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  R 572069-01-5 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 6700 FC  OR  19000 FH  R 572069-01-6 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 6100 FC  OR  17400 FH  572069-01-7 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572069-01-8 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FC  OR  50000 FH  572069-01-9 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 17000 FC  641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS OR  INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FH  STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 17000 FC  OR  50000 FH  572069-02-2 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.  572071-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FC  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT OR  541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR  50000 FH  572071-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FC  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT OR  541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 6800 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR  21700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572071-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FC  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT OR  541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR  50000 FH  572071-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FC  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A OR  541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH  641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR  50000 FH  572071-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 17000 FC  541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A OR  541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), 50000 FH  641BB 641BZ 641CZ SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 17000 FC  641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR  50000 FH  572071-02-2 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIBS T: 12 YE NO  541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB I: 12 YE  541EZ 641AB 641AZ 2A 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  572073-01-10 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 18600 FC  SURROUNDS. OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572073-01-11 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 14700 FC  SURROUNDS. OR  50000 FH  572073-01-4 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 20000 FC  SURROUNDS. OR  50000 FH  R 572073-01-5 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 6400 FC  SURROUNDS. OR  18200 FH  572073-01-6 N/A TASK DELETED  572073-01-7 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 17000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 17000 FC  SURROUNDS. OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572073-01-8 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 17000 FC  641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN OR  ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FH  REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 14700 FC  SURROUNDS. OR  50000 FH  572073-02-2 541FB 541GB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 10 T: 12 YE NO  641GB 641 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 10 T: 12 YE NO  641FB 641 FORWARD, RIB 10A AND PYLON DIAPHRAGM. I: 12 YE  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  D 572081-01-10 N/A TASK DELETED  572081-01-11 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 17000 FC  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  50000 FH  I: 7100 FC  OR  41800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572081-01-12 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 17000 FC  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  50000 FH  I: 8200 FC  OR  25900 FH  572081-01-13 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 20000 FC  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  50000 FH  I: 9000 FC  OR  25000 FH  572081-01-14 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 20000 FC  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR  50000 FH  I: 7100 FC  OR  41800 FH  D 572081-01-5 N/A TASK DELETED  572081-01-6 N/A TASK DELETED  572081-01-7 N/A TASK DELETED  572081-01-8 N/A TASK DELETED  572081-01-9 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO  641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572082-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 17000 FC  541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR  541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND 99800 FH  541FZ 641AB 641AZ ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 23400 FC  641BB 641CB 641DB OR  641DZ 641EB 641EZ 137500 FH  641FB 641FZ  D 572082-01-5 N/A TASK DELETED  R 572082-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 20000 FC  541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR  541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 50000 FH  541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 8400 FC  641BB 641CB 641DB OR  641DZ 641EB 641EZ 26900 FH  641FB 641FZ  R 572082-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 20000 FC  541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR  541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 50000 FH  541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 8400 FC  641BB 641CB 641DB OR  641DZ 641EB 641EZ 26900 FH  641FB 641FZ  572082-01-8 N/A TASK DELETED  R 572082-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 17000 FC  541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR  541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 53200 FH  541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 27200 FC  641BB 641CB 641DB OR  641DZ 641EB 641EZ 85200 FH  641FB 641FZ  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572082-02-2 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 CONDUIT  641BB 641CB 641DB HOLES.  641DZ 641EB 641EZ  641FB 641FZ  572083-01-1 541AB 541BZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO  641BZ 641 ASSEMBLY AFT FACE BETWEEN RIBS 1 AND 2. I: 12 YE I: 12 YE  572084-01-1 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 9900 FC  OR  29700 FH  572084-01-2 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 12700 FC  OR  38200 FH  572084-01-3 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 11400 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572084-01-4 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 17000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 12500 FC  OR  37500 FH  572084-01-5 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 17000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 11000 FC  OR  50000 FH  572084-01-6 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FC  SEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD OR  PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH  20 AND AT STR. 23 TO 28 LH/RH. I: 11200 FC  OR  50000 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  R 572090-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND OR  RIB 9. 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-1 I: 5200 FC  OR  23600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572090-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND OR  RIB 9. 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-2 I: 4400 FC  OR  13800 FH  R 572090-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND OR  RIB 9. 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-3 I: 5700 FC  OR  16800 FH  R 572090-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 OR  AND RIB 9. 50000 FH  I: 5400 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-4 OR  16100 FH  R 572090-02-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OR  8 AND RIB 9. 90900 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-1 I: 12800 FC  OR  58200 FH  572090-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OR  8 AND RIB 9. 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-2 I: 12000 FC  OR  37600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572090-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OR  8 AND RIB 9. 50000 FH  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-3 I: 14000 FC  OR  41500 FH  R 572090-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN OR  RIB 8 AND RIB 9. 50000 FH  I: 13400 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-4 OR  39600 FH  572091-01-3 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10. OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572091-02-3 I: 7000 FC  OR  21900 FH  572091-02-3 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  NTM TASK 572091-01-3 I: 7000 FC  SEALANT REMOVAL AS OR  PER NTM 21900 FH  572092-01-10 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 10100 FC  OR  28200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572092-01-11 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 8100 FC  OR  36500 FH  572092-01-4 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 9000 FC  OR  36200 FH  572092-01-5 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 7000 FC  OR  21900 FH  572092-01-6 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 9000 FC  OR  28200 FH  572092-01-7 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 9600 FC  OR  27200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572092-01-8 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 8100 FC  OR  36500 FH  572092-01-9 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OR  EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FH  I: 8400 FC  OR  26300 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.  R 572093-01-10 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FC  TASK 572093-02-10 OR  18100 FH  R 572093-01-11 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 17000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FC  TASK 572093-02-11 OR  22700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572093-01-12 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 17000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FC  TASK 572093-02-12 OR  30400 FH  R 572093-01-13 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FC  TASK 572093-02-13 OR  22700 FH  R 572093-01-14 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FC  TASK 572093-02-14 OR  30300 FH  R 572093-01-6 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572093-02-6 I: 5900 FC  OR  26800 FH  R 572093-01-7 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572093-02-7 I: 6300 FC  OR  18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572093-01-8 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572093-02-8 I: 6800 FC  OR  21300 FH  R 572093-01-9 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FC  641 OF STRINGER 15 TO CENTER SPAR OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572093-02-9 I: 6500 FC  OR  19400 FH  R 572093-02-10 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FC  TASK 572093-01-10 OR  18100 FH  572093-02-11 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FC  TASK 572093-01-11 OR  22700 FH  572093-02-12 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FC  TASK 572093-01-12 OR  30400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572093-02-13 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FC  TASK 572093-01-13 OR  22700 FH  R 572093-02-14 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  SEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FC  TASK 572093-01-14 OR  30300 FH  R 572093-02-6 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  TASK 572093-01-6 I: 5900 FC  OR  26800 FH  R 572093-02-7 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  TASK 572093-01-7 I: 6300 FC  OR  18800 FH  572093-02-8 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  TASK 572093-01-8 I: 6800 FC  OR  21300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572093-02-9 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  TASK 572093-01-9 I: 6500 FC  OR  19400 FH  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  R 572094-01-10 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 6500 FC  OR  19200 FH  572094-01-11 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 14300 FC  OR  39700 FH  572094-01-12 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 11400 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572094-01-5 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 6200 FC  OR  28300 FH  R 572094-01-6 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 8600 FC  OR  25600 FH  572094-01-7 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 7400 FC  OR  23200 FH  572094-01-8 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 13500 FC  OR  38300 FH  572094-01-9 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 OR  AND RIB 12. 50000 FH  I: 11400 FC  OR  50000 FH  572094-02-2 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO  641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 I: 12 YE  AND RIB 12.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572095-01-10 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 11400 FC  OR  50000 FH  R 572095-01-11 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 14300 FC  OR  39700 FH  R 572095-01-12 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 11400 FC  OR  50000 FH  R 572095-01-5 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 6900 FC  OR  31500 FH  R 572095-01-6 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 7300 FC  OR  21700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572095-01-7 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 7500 FC  OR  22100 FH  R 572095-01-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 7100 FC  OR  21100 FH  R 572095-01-9 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR  50000 FH  I: 13500 FC  OR  38300 FH  572101-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 9400 FC  OR  26300 FH  572101-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED 50000 FH  BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 7500 FC  OR  34000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 N 572101-01-12 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5. I: 6900 FC  OR  21600 FH  R 572101-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5. I: 5600 FC  OR  25500 FH  572101-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5. I: 5700 FC  OR  17800 FH  R 572101-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK FAIRINGS 3, 4 AND 5. I: 6300 FC  OR  18800 FH  R 572101-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 50000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 5500 FC  OR  16300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572101-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 50000 FH  AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 8900 FC  OR  25400 FH  572101-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 7500 FC  OR  34000 FH  572101-02-1 N/A TASK DELETED  572102-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 17100 FC  OR  47600 FH  572102-01-11 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 13600 FC  OR  50000 FH  572102-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 4400 FC  OR  17600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572102-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 6400 FC  OR  20000 FH  572102-01-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 4400 FC  OR  13800 FH  572102-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 16100 FC  OR  45900 FH  572102-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOMSKIN T: 17000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 13600 FC  OR  50000 FH  572102-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR  50000 FH  I: 4000 FC  OR  12500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572104-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED 50000 FH  BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 9400 FC  RIB 39. OR  26300 FH  572104-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 7500 FC  RIB 39. OR  34000 FH  N 572104-01-12 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6900 FC  RIB 39. OR  21600 FH  R 572104-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 5600 FC  RIB 39. OR  25500 FH  R 572104-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6800 FC  RIB 39. OR  20200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572104-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6300 FC  RIB 39. OR  18800 FH  R 572104-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDINGAREAS 50000 FH  COVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS I: 5500 FC  AT RIB 27 AND RIB 39. OR  16300 FH  572104-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED 50000 FH  BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 8900 FC  RIB 39. OR  25400 FH  572104-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FH  FLAP TRACK 5 FAIRING AND SKIN JOINTS AT I: 7500 FC  RIB 27 AND RIB 39. OR  34000 FH  572106-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 9000 FC  OR  25100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572106-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 7200 FC  OR  32500 FH  572106-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 7700 FC  OR  30900 FH  572106-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 9100 FC  OR  28500 FH  572106-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 7600 FC  OR  23800 FH  572106-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 8500 FC  OR  24300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572106-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB OR  12 AND RIB 23. 50000 FH  I: 7200 FC  OR  32500 FH  572106-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 OR  AND RIB 23. 50000 FH  I: 7100 FC  OR  22200 FH  572107-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 9000 FC  OR  25100 FH  572107-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 7200 FC  OR  32500 FH  572107-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 7700 FC  OR  30900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572107-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 9100 FC  OR  28500 FH  572107-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 7600 FC  OR  23800 FH  572107-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 8500 FC  OR  24300 FH  572107-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 7200 FC  OR  32500 FH  572107-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 OR  AND RIB 39. 50000 FH  I: 7100 FC  OR  22200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572108-01-2 532AB 533AB 534AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  541GB 541HB 541JB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YE  541KB 541LB 541MB 641 IN ALL BAYS BETWEEN RIBS 12 AND 27.  541NB 541PB 541QB 642  541RB 541SB 542AB  542BB 542CB 542DB  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572108-02-10 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 8400 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 23500 FH  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572108-02-11 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 6700 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 30400 FH  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 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572108-02-4 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 6600 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 30000 FH  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572108-02-5 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 9100 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 28500 FH  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  R 572108-02-6 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 7100 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 21100 FH  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 
A330 MRB REPORT – Structures Section

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 R 572108-02-7 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 6900 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 26000 FH  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572108-02-8 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 8000 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 22700 FH  632AB 633AB 634AB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572108-02-9 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR  541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH  541NB 541PB 541QB 642 I: 6700 FC  541RB 541SB 542AB OR  542BB 542CB 542DB 30400 FH  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 
A330 MRB REPORT – Structures Section

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 TPS

 572109-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO  542HB 542JB 542KB 550 AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, I: 6 YE  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND  550DB 550EB 550FB 650 39.  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-1 N/A TASK DELETED  572109-02-10 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 8400 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 23500 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-11 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 6700 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 30400 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-4 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 13100 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 50000 FH  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 572109-02-5 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 10200 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 30300 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-6 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 13200 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 41400 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-7 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 8000 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 22700 FH  650AB 650BB 650CB  650DB 650EB 650FB  572109-02-8 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 6700 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 30400 FH  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572109-02-9 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR  550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH  550DB 550EB 550FB 650 39. I: 12100 FC  642EB 642FB 642GB OR  642HB 642JB 642KB 37900 FH  650AB 650BB 650CB  650DB 650EB 650FB  572110-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 9200 FC  OR  25700 FH  572110-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 7400 FC  OR  33300 FH  R 572110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 9400 FC  OR  43000 FH  D 572110-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572110-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 10600 FC  OR  31500 FH  R 572110-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 9800 FC  OR  29100 FH  572110-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 8700 FC  OR  24800 FH  572110-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRINGS 3, 4 AND 5. I: 7400 FC  OR  33300 FH  572110-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  600 LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT I: 6 YE  SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP  TRACK FAIRINGS 3, 4 AND 5.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572111-01-10 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR  632AB 632CB 633AB 534 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 9200 FC  633 OR  634 25700 FH  572111-01-11 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR  632AB 632CB 633AB 534 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 7400 FC  633 OR  634 33300 FH  D 572111-01-4 N/A TASK DELETED  D 572111-01-5 N/A TASK DELETED  R 572111-01-6 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR  632AB 632CB 633AB 534 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 9200 FC  633 OR  634 27400 FH  D 572111-01-7 N/A TASK DELETED  572111-01-8 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR  632AB 632CB 633AB 534 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 8700 FC  633 OR  634 24800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572111-01-9 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR  632AB 632CB 633AB 534 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 7400 FC  633 OR  634 33300 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  572112-03-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 10500 FC  OR  42200 FH  572112-03-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 9900 FC  OR  31000 FH  572112-03-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 10600 FC  OR  33200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572112-03-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 8700 FC  OR  24800 FH  572112-03-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 7400 FC  OR  33300 FH  572112-03-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 9800 FC  OR  30700 FH  572112-03-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 9200 FC  OR  25700 FH  572112-03-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO OR  REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FH  FAIRING 5. I: 7400 FC  OR  33300 FH  572112-04-1 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.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572116-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5900 FC  OR  23700 FH  R 572116-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 7200 FC  OR  21400 FH  572116-02-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5900 FC  OR  18500 FH  572116-02-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 9600 FC  OR  27500 FH  572116-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 8100 FC  OR  36800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572116-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5500 FC  OR  17200 FH  572116-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 10200 FC  OR  28500 FH  572116-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND OR  STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FH  COVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 8100 FC  OR  36800 FH  572117-01-10 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH  633CB 634AB 634CB 632 I: 12600 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 35100 FH  572117-01-11 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH  633CB 634AB 634CB 632 I: 10000 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 45400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572117-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FH  633CB 634AB 634CB 632 5. I: 7700 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 30900 FH  R 572117-01-5 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FH  633CB 634AB 634CB 632 5. I: 8400 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 25000 FH  572117-01-6 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FH  633CB 634AB 634CB 632 5. I: 7600 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 23800 FH  572117-01-7 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. 50000 FH  633CB 634AB 634CB 632 I: 11900 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 33900 FH  572117-01-8 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH  633CB 634AB 634CB 632 I: 10000 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 45400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 572117-01-9 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR  632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH  633CB 634AB 634CB 632 I: 7100 FC  FAIRINGS ATTACHMENT 633 OR  BRACKET 634 22200 FH  572119-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 6900 FC  OR  27700 FH  572119-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 6600 FC  OR  20700 FH  572119-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 7000 FC  OR  21900 FH  572119-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 16200 FC  OR  46200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 572119-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 13700 FC  OR  50000 FH  572119-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 6300 FC  OR  19700 FH  572119-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 17200 FC  OR  47800 FH  572119-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FH  SPAR, BETWEEN RIBS 12 AND 23. I: 13700 FC  OR  50000 FH  N 572119-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND I: 6 YE  DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR  SPAR, BETWEEN RIBS 12 AND 23.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572120-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 9300 FC  OR  25900 FH  572120-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 7400 FC  OR  33500 FH  572120-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 6500 FC  OR  26100 FH  572120-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 9300 FC  OR  29100 FH  572120-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 6500 FC  OR  20300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572120-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 8800 FC  OR  25000 FH  572120-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 7400 FC  OR  33500 FH  572120-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC  600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 OR  IN RIB BAY 22-23. 50000 FH  I: 6100 FC  OR  19100 FH  572121-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  541RB 541SB 641GB AND 20. I: 7000 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 31600 FH  641PB 641QB 641RB  641SB  N 572121-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  541RB 541SB 641GB AND 20. I: 5400 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 16100 FH  641PB 641QB 641RB  641SB  D 572121-01-4 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 D 572121-01-5 N/A TASK DELETED  R 572121-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  541RB 541SB 641GB AND 20. I: 8300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 23600 FH  641PB 641QB 641RB  641SB  D 572121-01-7 N/A TASK DELETED  572121-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 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 50000 FH  541RB 541SB 641GB AND 20. I: 8300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 23600 FH  641PB 641QB 641RB  641SB  572121-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 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 50000 FH  541RB 541SB 641GB AND 20. I: 7000 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 31600 FH  641PB 641QB 641RB  641SB  572121-02-2 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572122-01-10 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR  542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH  550CB 550DB 550EB 650 I: 8800 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 24400 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572122-01-11 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR  542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH  550CB 550DB 550EB 650 I: 7000 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 31600 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  D 572122-01-4 N/A TASK DELETED  D 572122-01-5 N/A TASK DELETED  R 572122-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR  542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH  550CB 550DB 550EB 650 I: 5300 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 15800 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  D 572122-01-7 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572122-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR  542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH  550CB 550DB 550EB 650 I: 8300 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 23600 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  572122-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR  542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH  550CB 550DB 550EB 650 I: 7000 FC  550FB 642AB 642BB OR  642CB 642FB 642GB 31600 FH  642HB 642JB 650AB  650BB 650CB 650DB  650EB 650FB  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 BAY I: 12 YE  542JB 550AB 550BB 642 26-28 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 SKIN ACCESS T: 12 YE NO  542HB 542JB 542KB 550 DOORS BETWEEN RIB 27 AND RIB 39 INCLUDING NACA DUCT I: 6 YE  550AB 550BB 550CB 642 DOOR.  550DB 550EB 550FB 650  642EB 642FB 642GB  642HB 642JB 642KB  650AB 650BB 650CB  650DB 650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572124-01-3 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  572125-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  I: 17000 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME OR  AS TASK 572125-02-8 49100 FH  572125-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  I: 14600 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME OR  AS TASK 572125-02-9 50000 FH  572125-01-12 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  I: 18300 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-02-10 50000 FH  572125-01-13 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  I: 14600 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-02-11 50000 FH  572125-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING I: 12 YE I: 12 YE  JOINTS ON STRINGERS 15 AND 18.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572125-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 9900 FC  TASK 572125-02-4 OR  45200 FH  R 572125-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FC  TASK 572125-02-5 OR  38500 FH  R 572125-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 11200 FC  TASK 572125-02-6 OR  33200 FH  R 572125-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  JOINTS ON STRINGERS 15 AND 18. 50000 FH  I: 10200 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-02-7 30100 FH  572125-02-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM I: 18300 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-12 50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572125-02-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM I: 14600 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-13 50000 FH  R 572125-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 9900 FC  TASK 572125-01-6 OR  45200 FH  R 572125-02-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FC  TASK 572125-01-7 OR  38500 FH  R 572125-02-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 11200 FC  TASK 572125-01-8 OR  33200 FH  R 572125-02-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM I: 10200 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-9 30100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572125-02-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FH  PER NTM I: 17000 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-10 49100 FH  572125-02-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING OR  SEALANT REMOVAL AS ON STRINGERS 15 AND 18. 50000 FH  PER NTM I: 14600 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572125-01-11 50000 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  572126-02-10 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 13800 FC  OR  38500 FH  572126-02-11 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 11000 FC  OR  49700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572126-02-4 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 5100 FC  OR  20500 FH  572126-02-5 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 6200 FC  OR  19400 FH  572126-02-6 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 5100 FC  OR  15900 FH  572126-02-7 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 13000 FC  OR  37100 FH  572126-02-8 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 11000 FC  OR  49700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572126-02-9 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 4400 FC  OR  13800 FH  572127-01-2 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  D 572129-01-3 N/A TASK DELETED  D 572129-02-3 N/A TASK DELETED  D 572130-01-3 N/A TASK DELETED  D 572130-02-3 N/A TASK DELETED  572131-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 11800 FC  OR  32500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572131-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 9100 FC  OR  40000 FH  R 572131-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 91700 FH  I: 13600 FC  OR  62400 FH  R 572131-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 16400 FC  OR  48900 FH  R 572131-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 15800 FC  OR  47100 FH  R 572131-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 15000 FC  OR  44600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572131-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 11000 FC  OR  31200 FH  572131-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR OR  SPAR BETWEEN RIB 12 AND RIB 27. 50000 FH  I: 9100 FC  OR  40000 FH  572132-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 9100 FC  OR  40000 FH  572132-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 16400 FC  OR  50000 FH  572132-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 16000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572132-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 16700 FC  OR  50000 FH  572132-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 11000 FC  OR  31200 FH  572132-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 9100 FC  OR  40000 FH  572132-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 15600 FC  OR  49600 FH  572132-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR OR  BETWEEN RIB 27 AND RIB 39. 50000 FH  I: 11800 FC  OR  32500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572133-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT OR  SPAR TO REAR SPAR. 50000 FH  I: 13200 FC  OR  36100 FH  572133-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 10100 FC  OR  44500 FH  R 572133-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 5800 FC  OR  26300 FH  R 572133-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 8900 FC  OR  26600 FH  572133-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO OR  REAR SPAR. 50000 FH  I: 6800 FC  OR  21800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572133-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR OR  TO REAR SPAR. 50000 FH  I: 6200 FC  OR  18500 FH  572133-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR OR  TO REAR SPAR. 50000 FH  I: 12200 FC  OR  34700 FH  572133-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FC  600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR OR  TO REAR SPAR. 50000 FH  I: 10100 FC  OR  44500 FH  572133-02-2 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.  N 572134-02-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  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 
A330 MRB REPORT – Structures Section

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 572134-02-2 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 OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  6600 FC  OR  27900 FH  572134-02-3 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 OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  9900 FC  OR  31500 FH  572134-02-4 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 OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  7000 FC  OR  22300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572134-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR. 17000 FC  OR  50000 FH  I: 6 YE  OR  12200 FC  OR  34700 FH  572134-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR. 17000 FC  OR  50000 FH  I: 6 YE  OR  10100 FC  OR  44500 FH  572134-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  6300 FC  OR  20200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572134-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  13200 FC  OR  36100 FH  572134-02-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE  600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT OR  SPAR TO REAR SPAR. 20000 FC  OR  50000 FH  I: 6 YE  OR  10100 FC  OR  44500 FH  572135-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 10400 FC  OR  37400 FH  572135-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 7600 FC  OR  24100 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572135-01-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 10600 FC  OR  33700 FH  572135-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 17000 FC  OR  50000 FH  572135-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 9900 FC  OR  31600 FH  572135-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 OR  BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FH  STRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 20000 FC  OR  50000 FH  N 572138-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA 50000 FH  I: 20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572138-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA. 50000 FH  I: 20000 FC  OR  50000 FH  572138-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA. 50000 FH  I: 20000 FC  OR  50000 FH  572138-01-6 N/A TASK DELETED  N 572138-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA 50000 FH  I: 20000 FC  OR  50000 FH  572138-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA. 50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572138-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN OR  JOINT AREA 50000 FH  I: 20000 FC  OR  50000 FH  N 572139-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA OR  50000 FH  I: 20000 FC  OR  50000 FH  R 572139-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  50000 FH  I: 20000 FC  OR  50000 FH  572139-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  50000 FH  I: 20000 FC  OR  50000 FH  572139-01-6 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572139-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  50000 FH  I: 20000 FC  OR  50000 FH  572139-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  50000 FH  I: 17000 FC  OR  50000 FH  N 572139-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FC  600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OR  50000 FH  I: 20000 FC  OR  50000 FH  R 572140-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 8700 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 39600 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  R 572140-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 8900 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 26400 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572140-01-6 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 10600 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 33800 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-01-7 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 17000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT OR  541LB 541MB 541NB STR 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 17000 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 50000 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-01-8 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 9900 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 31600 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  572140-01-9 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR  541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH  541PB 541QB 541RB I: 20000 FC  541SB 641EB 641FB OR  641GB 641HB 641JB 50000 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572140-02-2 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 19 AND ALL STRINGER JOINTS.  541PB 541QB 541RB  541SB 641EB 641FB  641GB 641HB 641JB  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB  R 572141-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 10000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 45300 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  R 572141-01-5 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 12600 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 37600 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572141-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 13000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 41400 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  572141-01-7 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 17000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 17000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 50000 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  R 572141-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 11000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 32600 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572141-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FC  542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR  542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH  542KB 550AB 550BB 650 I: 20000 FC  550CB 550DB 550EB OR  550FB 642AB 642BB 50000 FH  642CB 642DB 642EB  642FB 642GB 642HB  642JB 642KB 650AB  650BB 650CB 650DB  650EB 650FB  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 BUTTSTRAPS 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  N 572144-01-10 542EB 642EB 500 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FC  600 SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572144-01-4 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 20000 FC  OR  50000 FH  572144-01-5 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 20000 FC  OR  50000 FH  572144-01-6 N/A TASK DELETED  572144-01-7 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 20000 FC  OR  50000 FH  572144-01-8 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 17000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27. OR  50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572144-01-9 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FC  642 SURFACE AT CHORDWISE JOINT AT RIB 27 OR  50000 FH  I: 20000 FC  OR  50000 FH  572144-02-2 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  572147-01-2 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL T: 12 YE NO  641 REFUELLING APERTURE REINFORCING PLATE IN RIB BAY I: 12 YE  22-23.  572148-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 16400 FC  OR  45700 FH  572148-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 20000 FC  OR  50000 FH  R 572148-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 9900 FC  OR  45200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572148-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 13000 FC  OR  38500 FH  R 572148-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 11200 FC  OR  33300 FH  R 572148-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 10200 FC  OR  30100 FH  572148-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 15500 FC  OR  44200 FH  572148-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR  50000 FH  I: 13100 FC  OR  50000 FH  572148-02-2 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572149-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 17200 FC  OR  47800 FH  572149-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 20000 FC  OR  50000 FH  N 572149-01-12 N/A 500 DTEAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO  600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES I: 6 YE  AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR  SPAR, BETWEEN RIBS 23 AND 39.  572149-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 6900 FC  OR  27700 FH  572149-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 9900 FC  OR  31000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572149-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 7000 FC  OR  21900 FH  572149-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 13700 FC  OR  50000 FH  572149-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 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 50000 FH  SPAR, BETWEEN RIBS 23 AND 39. I: 16200 FC  OR  46200 FH  572149-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 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 50000 FH  OF REAR SPAR, BETWEEN RIBS 23 AND 39. I: 6300 FC  OR  19700 FH  572151-01-1 574AT 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  574DB 574EB 574FB 674 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572152-01-1 574AT 575AT 575BT 575 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  591AB 591BB 591CB 675 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  572153-01-1 N/A TASK DELETED  572153-01-10 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 8600 FC  OR  50000 FH  572153-01-11 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 10900 FC  OR  30400 FH  R 572153-01-12 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  575 JOINT PLATE AT RIB 27. OR  674 118100 FH  675 I: 8600 FC  OR  50800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572153-01-4 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 10300 FC  OR  47600 FH  R 572153-01-5 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 5800 FC  OR  18500 FH  R 572153-01-6 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 11100 FC  OR  35600 FH  572153-01-7 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE  575 JOINT PLATE AT RIB 27. I: 12 YE I: 12 YE  674  675  R 572153-01-8 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR T: 20000 FC  575 SPAR AFT FACE JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 9400 FC  OR  30000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572153-01-9 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FC  575 JOINT PLATE AT RIB 27. OR  674 50000 FH  675 I: 10000 FC  OR  31500 FH  572154-01-1 N/A TASK DELETED  R 572154-01-10 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 9700 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 31200 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  572154-01-11 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572154-01-12 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 10300 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 32900 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  R 572154-01-4 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 9400 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 43300 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  R 572154-01-5 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 7800 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 24900 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572154-01-6 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 62700 FH  541QB 541RB 541SB 642 I: 17200 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 54000 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  572154-01-7 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 17000 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 50000 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  572154-01-8 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FC  541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR  541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH  541QB 541RB 541SB 642 I: 17000 FC  542AB 542BB 542CB OR  542DB 542EB 542GB 50000 FH  641FB 641GB 641HB  641JB 641KB 641LB  641MB 641NB 641PB  641QB 641RB 641SB  642AB 642BB 642CB  642DB 642EB 642GB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572155-01-1 542HB 542JB 542KB 542 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO  550AB 550BB 550CB 550 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  572156-01-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 13600 FC  OR  38000 FH  572156-01-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 20000 FC  OR  50000 FH  572156-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 11600 FC  OR  41700 FH  572156-01-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 6200 FC  OR  20000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572156-01-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 10800 FC  OR  34700 FH  572156-01-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 12500 FC  OR  39300 FH  572156-01-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 10800 FC  OR  50000 FH  572156-01-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 9100 FC  OR  29300 FH  R 572158-01-10 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 OR  541NB 541PB 541QB AND RIB 23. 50000 FH  541RB 541SB 641GB I: 5500 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 16500 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572158-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 OR  541NB 541PB 541QB AND RIB 23. 50000 FH  541RB 541SB 641GB I: 15700 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 43800 FH  641PB 641QB 641RB  641SB  572158-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23. 50000 FH  541RB 541SB 641GB I: 12500 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 50000 FH  641PB 641QB 641RB  641SB  R 572158-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23. 50000 FH  541RB 541SB 641GB I: 5300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 24300 FH  641PB 641QB 641RB  641SB  R 572158-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23. 50000 FH  541RB 541SB 641GB I: 6900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 20500 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572158-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR  541NB 541PB 541QB RIB 23. 50000 FH  541RB 541SB 641GB I: 6300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 19700 FH  641PB 641QB 641RB  641SB  572158-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 OR  541NB 541PB 541QB AND RIB 23. 50000 FH  541RB 541SB 641GB I: 14900 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 42300 FH  641PB 641QB 641RB  641SB  572158-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN OR  541NB 541PB 541QB RIB 12 AND RIB 23. 50000 FH  541RB 541SB 641GB I: 12600 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 50000 FH  641PB 641QB 641RB  641SB  572158-02-2 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572159-01-10 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 15700 FC  OR  43800 FH  572159-01-11 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 12500 FC  OR  50000 FH  R 572159-01-4 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 5700 FC  OR  26100 FH  R 572159-01-5 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 8100 FC  OR  23900 FH  572159-01-6 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 6800 FC  OR  21300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572159-01-7 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 14900 FC  OR  42300 FH  572159-01-8 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 12600 FC  OR  50000 FH  R 572159-01-9 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 6000 FC  OR  17700 FH  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 522RB 522SB 623  522TB 523AB 523BB  523CB 523DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 622TB  623AB 623BB 623CB  623DB  572162-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572162-01-4 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. OR I: 6 YE  20000 FC  OR  50000 FH  I: 6 YE  OR  20000 FC  OR  50000 FH  R 572162-01-5 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 20000 FC  623 FACE SPAR JOINT PLATE AT RIB 27. OR  50000 FH  I: 14600 FC  OR  46800 FH  572162-01-6 N/A TASK DELETED  572162-01-7 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. OR I: 6 YE  17000 FC  OR  50000 FH  I: 6 YE  OR  17000 FC  OR  50000 FH  R 572162-01-8 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572163-01-1 523EB 523FB 523GB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE  523HB 523JB 523KB 623 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  572164-01-10 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 17000 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 50000 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  R 572164-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 7500 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 44300 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  N 572164-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES 50000 FH  541RB 541SB 542AB 642 I: 8700 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 27400 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572164-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 7500 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 34900 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  R 572164-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 6900 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 22300 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  R 572164-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 8300 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 26500 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572164-01-8 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  R 572164-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FC  541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OR  541NB 541PB 541QB 641 FLANGES. 50000 FH  541RB 541SB 542AB 642 I: 8100 FC  542BB 542CB 542DB OR  641GB 641HB 641JB 25900 FH  641KB 641LB 641MB  641NB 641PB 641QB  641RB 641SB 642AB  642BB 642CB 642DB  572165-01-1 N/A TASK DELETED  572165-01-10 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. 20000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 572165-01-11 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  642AB 642BB 642CB  642DB 642EB 642FB  642GB 642HB 642JB  642KB 650AB 650BB  650CB 650DB 650EB  650FB  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 OR I: 12 YE  550AB 550BB 550CB 642 FLANGES. 20000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 8800 FC  OR  31800 FH  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. 20000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 7600 FC  OR  24500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572165-01-7 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. 20000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 8400 FC  OR  26900 FH  572165-01-8 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. 17000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 17000 FC  OR  50000 FH  572165-01-9 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. 20000 FC  550DB 550EB 550FB 650 OR  642EB 642FB 642GB 50000 FH  642HB 642JB 642KB I: 12 YE  650AB 650BB 650CB OR  650DB 650EB 650FB 8200 FC  OR  26300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572166-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 20000 FC  OR  50000 FH  R 572166-01-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 14600 FC  OR  46800 FH  572166-01-6 N/A TASK DELETED  572166-01-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 17000 FC  642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. OR  SEALANT REMOVAL AS 50000 FH  PER NTM I: 17000 FC  OR  50000 FH  572171-02-1 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 STR CUTOUTS EXCLUDING RIBS 18 & 23.  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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572174-01-4 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. 20000 FC  641NB 641SB 642AB 642 OR  50000 FH  I: 12 YE  OR  20000 FC  OR  50000 FH  572174-01-5 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. 20000 FC  641NB 641SB 642AB 642 OR  50000 FH  I: 12 YE  OR  6900 FC  OR  21900 FH  572174-01-6 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. 17000 FC  641NB 641SB 642AB 642 OR  50000 FH  I: 12 YE  OR  17000 FC  OR  50000 FH  N 572174-01-7 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 I: 12 YE I: 12 YE  641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS  641NB 641SB 642AB 642  D 572180-01-11 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 D 572180-01-4 N/A TASK DELETED  D 572180-01-5 N/A TASK DELETED  R 572180-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR  541NB 541PB 541QB 50000 FH  541RB 541SB 641GB I: 10300 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 30600 FH  641PB 641QB 641RB  641SB  R 572180-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR  541NB 541PB 541QB 50000 FH  541RB 541SB 641GB I: 8400 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 24000 FH  641PB 641QB 641RB  641SB  572180-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR  541NB 541PB 541QB 50000 FH  541RB 541SB 641GB I: 8400 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 24000 FH  641PB 641QB 641RB  641SB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572180-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR  541NB 541PB 541QB 50000 FH  541RB 541SB 641GB I: 7100 FC  641HB 641JB 641KB OR  641LB 641MB 641NB 32100 FH  641PB 641QB 641RB  641SB  572180-02-2 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  572181-01-10 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 8900 FC  OR  24900 FH  572181-01-11 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 7100 FC  OR  32200 FH  D 572181-01-4 N/A TASK DELETED  D 572181-01-5 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 572181-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 10300 FC  OR  30600 FH  D 572181-01-7 N/A TASK DELETED  572181-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 8400 FC  OR  24000 FH  572181-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR  50000 FH  I: 7100 FC  OR  32200 FH  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  572182-01-10 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 8900 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 24900 FH  650CB 650DB 650EB  650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572182-01-11 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 7100 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 32200 FH  650CB 650DB 650EB  650FB  572182-01-4 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 6500 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 26100 FH  650CB 650DB 650EB  650FB  572182-01-5 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 6200 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 19400 FH  650CB 650DB 650EB  650FB  572182-01-6 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 6500 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 20300 FH  650CB 650DB 650EB  650FB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572182-01-7 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 8400 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 24000 FH  650CB 650DB 650EB  650FB  572182-01-8 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 7100 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 32200 FH  650CB 650DB 650EB  650FB  572182-01-9 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR  550BB 550CB 550DB 642 50000 FH  550EB 550FB 642FB 650 I: 6000 FC  642GB 642HB 642JB OR  642KB 650AB 650BB 18800 FH  650CB 650DB 650EB  650FB  572182-02-2 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 
A330 MRB REPORT – Structures Section

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 572183-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  I: 8900 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-02-10 24900 FH  572183-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  I: 7100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-02-11 32200 FH  572183-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FC  TASK 572183-02-4 OR  26100 FH  572183-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6200 FC  TASK 572183-02-5 OR  19400 FH  572183-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FC  TASK 572183-02-6 OR  20300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 572183-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  I: 8400 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-02-7 24000 FH  572183-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  I: 7100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME OR  AS TASK 572183-02-8 32200 FH  572183-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  STRINGER JOINTS. 50000 FH  I: 5900 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-02-9 18500 FH  572183-02-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM I: 8900 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-01-10 24900 FH  572183-02-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM I: 7100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-01-11 32200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 572183-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FC  TASK 572183-01-4 OR  26100 FH  572183-02-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6200 FC  TASK 572183-01-5 OR  19400 FH  572183-02-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FC  TASK 572183-01-6 OR  20300 FH  572183-02-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM I: 8400 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-01-7 24000 FH  572183-02-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM I: 7100 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-01-8 32200 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572183-02-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING OR  SEALANT REMOVAL AS STRINGER JOINTS. 50000 FH  PER NTM I: 5900 FC  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR  TASK 572183-01-9 18500 FH  572183-03-2 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.  D 572184-01-4 N/A TASK DELETED  D 572184-01-5 N/A TASK DELETED  R 572184-01-6 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OR  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FH  TASK 572184-02-6 I: 5600 FC  OR  16600 FH  D 572184-01-7 N/A TASK DELETED  572184-01-8 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 17000 FC  TASK 572184-02-8 OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572184-01-9 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OR  50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 20000 FC  TASK 572184-02-9 OR  50000 FH  D 572184-02-4 N/A TASK DELETED  D 572184-02-5 N/A TASK DELETED  R 572184-02-6 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 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 50000 FH  TASK 572184-01-6 I: 5600 FC  OR  16600 FH  D 572184-02-7 N/A TASK DELETED  572184-02-8 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  SEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 17000 FC  TASK 572184-01-8 OR  50000 FH  572184-02-9 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  SEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OR  PER NTM 50000 FH  NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 20000 FC  TASK 572184-01-9 OR  50000 FH  572601-01-2 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE  671 GEAR SIDE STAY FITTING (RIB 2). I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572602-01-2 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE  671 GEAR FORWARD PINTLE FITTING (RIB 5). I: 12 YE  572603-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE  671 GEAR RETRACTION JACK FITTING. I: 12 YE  572604-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE  671 GEAR SUPPORT RIB 6. I: 12 YE  572605-01-1 N/A TASK DELETED  572605-01-3 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 20000 FC  AND THRUST PADS). I: 12 YE  OR  10700 FC  572605-01-4 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 20000 FC  AND THRUST PADS). I: 12 YE  OR  9200 FC  572605-01-5 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 17000 FC  AND THRUST PADS). I: 12 YE  OR  17000 FC  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572605-01-6 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP 20000 FC  (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YE  PADS). OR  10700 FC  572605-01-7 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP 20000 FC  (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YE  PADS). OR  18400 FC  572605-01-8 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YE  AFT PICK UP 20000 FC  (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YE  PADS). OR  20000 FC  N 572605-01-9 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 I: 12 YE I: 12 YE  AFT PICK UP (INCLUDING BOX BRACKET,INTERFACE PLATE  AND THRUST PADS).  572606-01-2 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 T: 20000 FC  632CB 633CB 634CB 533 AND 5 AFT PICK-UP, ASSEMBLY. I: 20000 FC  534  632  633  634  572606-01-3 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572606-01-6 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, T: 20000 FC  632CB 633CB 634CB 533 4 AND 5 AFT PICK-UP, ASSEMBLY. I: 17400 FC  534  632  633  634  572606-02-2 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  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 FITTINGS. OR I: 12 YE  534AB 534CB 631AB 533 20000 FC  631CB 632AB 632CB 534 I: 12 YE  633AB 633CB 634AB 631 OR  634CB 632 8300 FC  633  634  572607-01-4 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 FITTINGS. OR I: 12 YE  534AB 534CB 631AB 533 17000 FC  631CB 632AB 632CB 534 I: 12 YE  633AB 633CB 634AB 631 OR  634CB 632 8300 FC  633  634  N 572607-01-5 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2,3, T: 12 YE T: 20 YE  532CB 533AB 533CB 532 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. I: 12 YE I: 12 YE  534AB 534CB 631AB 533  631CB 632AB 632CB 534  633AB 633CB 634AB 631  634CB 632  633  634  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572608-02-1 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. I: 20000 FC  622BB 622CT  ENGINE  LINKS  SLEEVES  572608-02-2 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR  622BB 622CT 50000 FH  ENGINE I: 8200 FC  LINKS OR  SLEEVES 48500 FH  572608-02-3 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR  622BB 622CT 50000 FH  ENGINE I: 9600 FC  LINKS OR  SLEEVES 30200 FH  572608-02-5 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR  622BB 622CT 50000 FH  ENGINE I: 10400 FC  LINKS OR  SLEEVES 28900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572608-02-6 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR  622BB 622CT 50000 FH  ENGINE I: 8200 FC  LINKS OR  SLEEVES 48500 FH  R 572610-01-1 453CL 453CR 454BL 541 DETAILED INSPECTION OF OUTER WING PYLON SPIGOT T: 12 YE T: 20 YE NO  454BR 454CL 454CR 641 FITTING. I: 12 YE I: 12 YE  463CL 463CR 464BL  464BR 464CL 464CR  SPIGOT SLEEVE  R 572610-01-2 453CL 453CR 454BL 541 DETAILED INSPECTION OF OUTER WING PYLON SPIGOT T: 12 YE T: 20 YE NO  454BR 454CL 454NR 641 FITTING. I: 12 YE I: 12 YE  463CL 463CR 464BL  464BR 464CL 464NR  SPIGOT SLEEVE  572610-02-10 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454NR 464BL 464BR 641 SPIGOT FITTING. OR  464CL 464NR 50000 FH  I: 10800 FC  OR  30200 FH  572610-02-11 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454CR 464BL 464BR 641 SPIGOT FITTING. OR  464CL 464CR 50000 FH  I: 8600 FC  OR  50000 FH  572610-02-2 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454CR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FC  464CL 464CR  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572610-02-3 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454CR 464BL 464BR 641 SPIGOT FITTING. I: 9000 FC  464CL 464CR  572610-02-4 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454NR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FC  464CL 464NR  572610-02-5 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454NR 464BL 464BR 641 SPIGOT FITTING. I: 9000 FC  464CL 464NR  572610-02-8 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  454NR 464BL 464BR 641 SPIGOT FITTING. OR  464CL 464NR 50000 FH  I: 17000 FC  OR  50000 FH  572610-02-9 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FC  454NR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FC  464CL 464NR  R 572612-01-2 454DL 454DR 454FL 541 DETAILED INSPECTION OF OUTER WING PYLON AFT T: 12 YE T: 20 YE NO  454FR 464DL 464DR 641 ATTACHMENT FITTING. I: 12 YE I: 12 YE  464FL 464FR  PIPE SUPPORT BRACKET  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572612-01-3 454KL 454KR 454ML 541 DETAILED INSPECTION OF OUTER WING PYLON AFT T: 12 YE T: 20 YE NO  454MR 464KL 464KR 641 ATTACHMENT FITTING. I: 12 YE I: 12 YE  464ML 464MR  PIPE SUPPORT BRACKET  572612-02-1 N/A TASK DELETED  572612-02-10 N/A TASK DELETED  R 572612-02-11 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  454MR 464BL 464BR 641 AFT ATTACHMENT FITTING. OR  464ML 464MR 50000 FH  PIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-5 I: 11300 FC  OR  35500 FH  572612-02-12 N/A TASK DELETED  572612-02-13 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454MR 464BL 464BR 641 ATTACHMENT FITTING. OR  464ML 464MR 50000 FH  PIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-6 I: 6200 FC  OR  19800 FH  572612-02-14 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 572612-02-15 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454MR 464BL 464BR 641 ATTACHMENT FITTING. OR  464ML 464MR 50000 FH  PIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-7 I: 12300 FC  OR  34300 FH  572612-02-16 N/A TASK DELETED  R 572612-02-17 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454FR 464BL 464BR 641 ATTACHMENT FITTING. OR  464FL 464FR 50000 FH  PIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-8 I: 9700 FC  OR  50000 FH  572612-02-18 N/A TASK DELETED  572612-02-3 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454FR 464BL 464BR 641 ATTACHMENT FITTING. OR  464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-1 50000 FH  PIPE SUPPORT BRACKET I: 7800 FC  OR  24600 FH  572612-02-4 N/A TASK DELETED  572612-02-5 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454FR 464BL 464BR 641 ATTACHMENT FITTING. OR  464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-2 50000 FH  PIPE SUPPORT BRACKET I: 6400 FC  OR  20500 FH  572612-02-6 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572612-02-7 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454MR 464BL 464BR 641 ATTACHMENT FITTING. OR  464ML 464MR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-3 50000 FH  PIPE SUPPORT BRACKET I: 6400 FC  OR  20300 FH  572612-02-8 N/A TASK DELETED  R 572612-02-9 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  454MR 464BL 464BR 641 AFT ATTACHMENT FITTING. OR  464ML 464MR 50000 FH  PIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-4 I: 9700 FC  OR  50000 FH  572612-03-1 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454DR 454FL 454FR 641 ATTACHMENT FITTING. OR  464CL 464CR 464DL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-3 50000 FH  464DR 464FL 464FR I: 17500 FC  BEARING REMOVAL OR  ENGINE, LINKS AND 50000 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572612-03-2 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454DR 454FL 454FR 641 ATTACHMENT FITTING. OR  464CL 464CR 464DL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-5 50000 FH  464DR 464FL 464FR I: 14500 FC  BEARING REMOVAL OR  ENGINE, LINKS AND 45900 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572612-03-3 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454ML 454MR 454NR 641 ATTACHMENT FITTING. OR  464CL 464KL 464KR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-7 50000 FH  464ML 464MR 464NR I: 14400 FC  BEARING REMOVAL OR  ENGINE, LINKS AND 45600 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572612-03-4 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FC  454ML 454MR 454NR 641 AFT ATTACHMENT FITTING. OR  464CL 464KL 464KR 50000 FH  464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-9 I: 17000 FC  BEARING REMOVAL OR  ENGINE, LINKS AND 50000 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572612-03-5 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 17000 FC  454ML 454MR 454NR 641 ATTACHMENT FITTING. OR  464CL 464KL 464KR 50000 FH  464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 17000 FC  BEARING REMOVAL TASK 572612-02-11 OR  ENGINE, LINKS AND 50000 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572612-03-6 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454ML 454MR 454NR 641 ATTACHMENT FITTING. OR  464CL 464KL 464KR 50000 FH  464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 14000 FC  BEARING REMOVAL TASK 572612-02-13 OR  ENGINE, LINKS AND 44400 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 572612-03-7 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454ML 454MR 454NR 641 ATTACHMENT FITTING. OR  464CL 464KL 464KR 50000 FH  464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 20000 FC  BEARING REMOVAL TASK 572612-02-15 OR  ENGINE, LINKS AND 50000 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572612-03-8 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FC  454DR 454FL 454FR 641 ATTACHMENT FITTING. OR  464CL 464CR 464DL 50000 FH  464DR 464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 20000 FC  BEARING REMOVAL TASK 572612-02-17 OR  ENGINE, LINKS AND 50000 FH  SLEEVES, PIPE  SUPPORT BRACKET  REMOVED / DISPLACED  572614-01-2 N/A TASK DELETED  572614-02-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR HINGED T: 6 YE  743 DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YE  572615-01-2 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  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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

 TASK ACCESS ZONE

 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 573001-01-1 N/A TASK DELETED  R 573001-01-10 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 5700 FC  OR  18300 FH  573001-01-11 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 17000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 9100 FC  OR  50000 FH  573001-01-12 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 17000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 10600 FC  OR  33200 FH  573001-01-13 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 11500 FC  OR  32000 FH  573001-01-14 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 9100 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

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 TPS

 R 573001-01-5 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 5300 FC  OR  24400 FH  573001-01-6 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 10700 FC  OR  33800 FH  R 573001-01-7 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 5600 FC  OR  18000 FH  R 573001-01-8 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FC  635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND OR  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FH  I: 5800 FC  OR  18700 FH  573001-01-9 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 I: 12 YE I: 12 YE  REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 573002-01-10 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 17000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 9100 FC  OR  50000 FH  573002-01-11 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 17000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 10600 FC  OR  33200 FH  573002-01-12 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 11500 FC  OR  32000 FH  573002-01-13 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 9100 FC  OR  50000 FH  R 573002-01-5 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 5300 FC  OR  24400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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INTERVAL 

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 573002-01-6 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 10700 FC  OR  33800 FH  R 573002-01-7 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 5600 FC  OR  18000 FH  R 573002-01-8 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 5800 FC  OR  18700 FH  R 573002-01-9 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FC  600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR  50000 FH  I: 5700 FC  OR  18300 FH  573002-02-2 N/A 500 GENERAL VISUAL INSPECTION OF WINGTIP BOX TOP SKIN T: 6 YE NO  600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. I: 6 YE  573003-01-1 WINGLET 535 DETAILED INSPECTION OF WINGTIP TO WINGLET FORWARD AND T: 12 YE T: 20 YE  635 AFT LUGS (BOTH ON WINGTIP AND WINGLET). I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 573003-02-10 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 5100 FC  OR  16500 FH  N 573003-02-11 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 5200 FC  OR  16800 FH  R 573003-02-4 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 4700 FC  OR  21900 FH  R 573003-02-5 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 6800 FC  OR  21800 FH  R 573003-02-6 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 8200 FC  OR  25800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 573003-02-7 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 17000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 17000 FC  OR  50000 FH  R 573003-02-8 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 17000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  99800 FH  I: 14900 FC  OR  87500 FH  573003-02-9 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FC  635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR  50000 FH  I: 7100 FC  OR  41600 FH  573004-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE  635BZ 635 FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 573004-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE  635BZ 635 FLANGE TO SKIN ATTACHMENT. OR I: 12 YE  17000 FC  OR  50000 FH  I: 12 YE  OR  17000 FC  OR  50000 FH  573004-01-3 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE  635BZ 635 FLANGE TO SKIN ATTACHMENT. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  20000 FC  OR  50000 FH  N 573004-01-4 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE  635BZ 635 FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YE  573005-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF WINGTIP TO WINGLET JOINT T: 12 YE  635BB 635 BOLTS. I: 12 YE  JOINT BOLTS  573006-01-2 N/A 500 GENERAL VISUAL INSPECTION OF WINGLET EXTERNAL T: 5 YE NO  600 SURFACE. I: 5 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574101-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 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 N/A TASK DELETED  574102-01-10 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 7200 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 22700 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-11 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 14700 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 41000 FH  622JB 622LB 622NB  622RB 622TB 623CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574102-01-12 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 11700 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 50000 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-4 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 7600 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 27300 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-5 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 8100 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 25500 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-6 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 5700 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 18000 FH  622JB 622LB 622NB  622RB 622TB 623CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574102-01-7 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 7300 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 23000 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-8 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 11700 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 50000 FH  622JB 622LB 622NB  622RB 622TB 623CB  574102-01-9 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FC  521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR  522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH  522RB 522TB 523CB 621 I: 13600 FC  621BB 621CB 621DB 622 OR  621GB 621JB 622CB 623 42500 FH  622JB 622LB 622NB  622RB 622TB 623CB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574103-02-1 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 13600 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 48900 FH  574103-02-2 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 10300 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 32500 FH  574103-02-3 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 13100 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 41300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574103-02-4 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 17000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 9000 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 50000 FH  574103-02-5 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 17000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 10400 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 32800 FH  574103-02-6 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 12900 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 40700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 574103-02-7 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 11300 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 31600 FH  574103-02-8 521DB 521FB 521GB 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 OR I: 12 YE  522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC  522JB 522NB 522RB 621 OR  522UB 523AB 523BB 622 50000 FH  621DB 621FB 621GB 623 I: 12 YE  622AB 622BB 622CB OR  622EB 622GB 622HB 9000 FC  622JB 622NB 622RB OR  622UB 623AB 623BB 50000 FH  N 574103-02-9 521DB 521FB 521GB 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.  522JB 522NB 522RB 621  522UB 523AB 523BB 622  621DB 621FB 621GB 623  622AB 622BB 622CB  622EB 622GB 622HB  622JB 622NB 622RB  622UB 623AB 623BB  574104-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574104-01-10 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 12400 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 34500 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574104-01-11 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 9800 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 50000 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574104-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 7800 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 28000 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 574104-01-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 5900 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 18600 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 574104-01-6 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 7500 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 23600 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 574104-01-7 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 9800 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 50000 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574104-01-8 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 11400 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 35800 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574104-01-9 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR  521GB 521HB 521JB 523 50000 FH  522AB 522BB 522CB 621 I: 7400 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 23300 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  574105-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574105-01-10 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 14300 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 39700 FH  623JB 623LB 623NB  574105-01-11 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 11300 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 50000 FH  623JB 623LB 623NB  N 574105-01-12 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 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 623GB  623JB 623LB 623NB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574105-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 7600 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 27300 FH  623GB 623JB 623LB  623NB  574105-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 523CB 523DB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 5800 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 18300 FH  623GB 623JB 623LB  623NB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574105-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 6800 FC  622LB 622NB 622RB OR  622TB 623CB 623EB 21400 FH  623GB 623JB 623LB  623NB  574105-01-6 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 7300 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 23000 FH  623JB 623LB 623NB  574105-01-7 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 17000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 11300 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 50000 FH  623JB 623LB 623NB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574105-01-8 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 17000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 13100 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 41100 FH  623JB 623LB 623NB  574105-01-9 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE  522JB 522LB 522NB 523 20000 FC  522RB 522TB 523CB 621 OR  523EB 523GB 523JB 622 50000 FH  523LB 523NB 621BB 623 I: 12 YE  621CB 621DB 621GB OR  621JB 622CB 622JB 7200 FC  622LB 622NB 622RB OR  622TB 623CB 623GB 22700 FH  623JB 623LB 623NB  574106-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-10 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK I: 12 YE I: 12 YE  521HB 521JB 522AB 523 RIB 16.  522BB 522CB 522DB 621  522EB 522FB 522GB 622  522HB 522JB 522KB 623  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-11 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 20000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 20000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 20000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-6 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 20000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-7 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 17000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-8 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 20000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574106-01-9 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR  521HB 521JB 522AB 523 RIB 16. 50000 FH  522BB 522CB 522DB 621 I: 17000 FC  522EB 522FB 522GB 622 OR  522HB 522JB 522KB 623 50000 FH  522LB 522MB 522NB  522PB 522RB 522SB  523CB 523DB 523EB  523FB 523GB 523HB  523JB 523KB 523LB  523MB 523NB 523PB  621BB 621CB 621DB  621EB 621FB 621GB  621HB 621JB 622AB  622BB 622CB 622DB  622EB 622FB 622GB  622HB 622JB 622KB  622LB 622MB 622NB  622PB 622RB 622SB  623CB 623DB 623EB  623FB 623GB 623HB  623JB 623KB 623LB  623MB 623NB 623PB  574107-01-2 521FB 521GB 521HB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521JB 522AB 522BB 522 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YE  522CB 522DB 522EB 523 RIB 3 TO TRACK RIB 12.  522FB 522GB 522HB 621  522JB 522KB 522LB 622  522MB 522NB 522PB 623  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574107-02-10 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 10400 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 28900 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  574107-02-11 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 8200 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 48500 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 R 574107-02-4 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 92400 FH  522FB 522GB 522HB 621 I: 14100 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 65200 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  R 574107-02-5 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 12500 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 40000 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574107-02-6 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 16000 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 50000 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  574107-02-7 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 8200 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 48500 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 574107-02-8 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 9600 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 30000 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  574107-02-9 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FC  521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR  522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH  522FB 522GB 522HB 621 I: 15500 FC  522JB 522KB 522LB 622 OR  522MB 522NB 522PB 623 48900 FH  522RB 522SB 523CB  523DB 523EB 621FB  621GB 621HB 621JB  622AB 622BB 622CB  622DB 622EB 622FB  622GB 622HB 622JB  622KB 622LB 622MB  622NB 622PB 622RB  622SB 623CB 623DB  623EB  574108-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 12 YE  621 EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAIN I: 12 YE  ATTACHMENTS TO FRONT SPAR AND FUSELAGE.  574109-02-1 N/A TASK DELETED  574109-02-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 TPS

 574109-02-3 N/A TASK DELETED  574109-02-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT OR  521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING 50000 FH  522AB 522BB 522CB 621 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. I: 8600 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 27100 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 TPS

 574109-02-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT OR  521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING 50000 FH  522AB 522BB 522CB 621 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. I: 7400 FC  522DB 522EB 522FB 622 OR  522GB 522HB 522JB 623 43700 FH  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 574109-02-8 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT I: 12 YE I: 12 YE  521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS  522AB 522BB 522CB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT  522DB 522EB 522FB 622 HOLD DOWN RIBS.  522GB 522HB 522JB 623  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  574110-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 17700 FC  OR  50000 FH  574110-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 6000 FC  OR  18800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574110-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 16800 FC  OR  50000 FH  574110-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 16200 FC  OR  50000 FH  574110-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 17000 FC  OR  50000 FH  574110-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 16100 FC  OR  50000 FH  574110-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574110-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YE  SPAR FROM RIB 1 TO RIB 9. 50000 FH  I: 16200 FC  OR  50000 FH  N 574110-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 6 YE NO  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT I: 6 YE  SPAR FROM RIB 1 TO RIB 9.  574111-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR OR  FROM RIB 1 TO RIB 39. 50000 FH  I: 14800 FC  OR  50000 FH  574111-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR OR  FROM RIB 1 TO RIB 39. 50000 FH  I: 6000 FC  OR  19000 FH  574111-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR OR  FROM RIB 1 TO RIB 39. 50000 FH  I: 15300 FC  OR  48400 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574111-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR OR  FROM RIB 1 TO RIB 39. 50000 FH  I: 17000 FC  OR  50000 FH  574111-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR OR  FROM RIB 1 TO RIB 39. 50000 FH  I: 13900 FC  OR  44000 FH  574111-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 20000 FC  600 EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD OR  OF FRONT SPAR FROM RIB 1 TO RIB 39. 50000 FH  I: 20000 FC  OR  50000 FH  574111-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 6 YE NO  600 EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT I: 6 YE  SPAR FROM RIB 1 TO RIB 39.  574112-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  623NB 623 HOLD DOWN RIB BETWEEN SLAT TRACK RIB 15 AND SLAT I: 12 YE I: 12 YE  TRACK 16, AREA OF SLAT TRACK BRAKE FITTING  R 574114-03-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 114600 FH  I: 12400 FC  OR  56600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 574114-03-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 5500 FC  OR  16400 FH  R 574114-03-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 13900 FC  OR  41000 FH  R 574114-03-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 12700 FC  OR  37500 FH  574114-03-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 16200 FC  OR  50000 FH  574114-03-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574114-03-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR  SPAR FROM RIB 11 TO RIB 39. 50000 FH  I: 20000 FC  OR  50000 FH  574114-04-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 12 YE NO  600 EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF I: 12 YE  FRONT SPAR FROM RIB 11 TO RIB 39.  574115-02-1 N/A TASK DELETED  574115-02-2 N/A TASK DELETED  574115-02-3 N/A TASK DELETED  574115-02-4 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE  622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT I: 12 YE I: 12 YE  SPAR BETWEEN RIBS 9 AND 11.  574115-02-6 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT OR  SPAR BETWEEN RIBS 9 AND 11. 50000 FH  I: 16200 FC  OR  50000 FH  574115-02-7 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC  622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT OR  SPAR BETWEEN RIBS 9 AND 11. 50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574115-02-8 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT OR  SPAR BETWEEN RIBS 9 AND 11. 50000 FH  I: 20000 FC  OR  50000 FH  574115-02-9 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC  622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT OR  SPAR BETWEEN RIBS 9 AND 11. 50000 FH  I: 16200 FC  OR  50000 FH  574116-01-10 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 10400 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 28900 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574116-01-11 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 8200 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 48500 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 N 574116-01-12 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 I: 12 YE I: 12 YE  521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC DUCT RIBS) AND  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS.  522DB 522EB 522FB 622  522GB 522HB 522JB 623  522KB 522LB 522MB  522NB 522PB 522RB  522SB 523CB 523DB  523EB 523FB 523GB  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 14600 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 50000 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 INTERVAL 

 

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 574116-01-5 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 13500 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 42600 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574116-01-6 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 15200 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 48000 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574116-01-7 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 17000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 8200 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 48500 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574116-01-8 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 17000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 9600 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 30000 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 623CB  623DB 623EB 623FB  623GB 623HB 623JB  623KB 623LB 623MB  623NB 623PB  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 574116-01-9 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 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC  522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR  522DB 522EB 522FB 622 50000 FH  522GB 522HB 522JB 623 I: 12 YE  522KB 522LB 522MB OR  522NB 522PB 522RB 14000 FC  522SB 523CB 523DB OR  523EB 523FB 523GB 44200 FH  523HB 523JB 523KB  523LB 523MB 523NB  523PB 621AB 621BB  621CB 621DB 621EB  621FB 621GB 621HB  621JB 622AB 622BB  622CB 622DB 622EB  622FB 622GB 622HB  622JB 622KB 622LB  622MB 622NB 622PB  622RB 622SB 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 LEADING EDGE T: 12 YE T: 20 YE  523JB 523LB 523NB 523 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YE  621BB 621GB 623GB 621 RIBS 1 AND 2 AND TRACK RIBS 13 TO 16.  623JB 623LB 623NB 623  R 574301-01-3 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 & 3, T: 20000 FC  611 VISIBLE PART OF ROLLER CONTACT AREA. OR  50000 FH  I: 9400 FC  OR  30900 FH  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.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 574303-02-3 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 20000 FC  611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574304-03-2.  R 574304-02-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 20000 FC  611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  R 574304-03-2 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.  574305-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  611 LH/RH. I: 12 YE I: 12 YE  R 574306-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1 TRAILING EDGE T: 3 YE  611 LOWER FACE, 100 MM FROM 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 574308-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL SURFACE T: 6 YE NO  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  R 574401-01-3 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 20000 FC  612 6; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 7000 FC  OR  22800 FH  574401-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6; T: 12 YE T: 20 YE  612 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  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 574403-02-3 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 20000 FC  612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574404-03-2.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 574404-02-3 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT T: 20000 FC  612 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  R 574404-03-2 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  612 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 574404-01-1.  574405-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  612 LH/RH. I: 12 YE I: 12 YE  R 574406-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2 TRAILING EDGE T: 3 YE  612 LOWER FACE, 100 MM FROM AFT EDGE LH/RH. I: 3 YE  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 SURFACE T: 6 YE  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  574501-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ; T: 12 YE T: 20 YE  613 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 574501-02-4 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 20000 FC  613 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 7000 FC  OR  22800 FH  R 574503-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 & 8 T: 12 YE  613 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574503-02-3 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3, TRACKS 7 TO 8 T: 20000 FC  613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574504-02-3.  R 574504-02-3 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  613 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 574504-01-1.  R 574504-02-4 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT T: 20000 FC  613 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  R 574505-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 3 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  612 LH/RH. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 574506-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3 TRAILING EDGE T: 3 YE  613 LOWER FACE, 100 MM FROM AFT EDGE LH/RH. I: 3 YE  N 574507-01-1 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.  574507-01-2 N/A TASK DELETED  R 574508-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, EXTERNAL SURFACE T: 6 YE  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  574601-01-1 N/A TASK DELETED  R 574601-01-3 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 20000 FC  614 10 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 9400 FC  OR  30900 FH  R 574601-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 , T: 12 YE T: 20 YE  614 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574603-01-2 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 & 10 T: 12 YE NO  614 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  574603-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 574603-02-3 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND 10 T: 20000 FC  614 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 FH  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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574604-02-1.  R 574604-02-1 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 574604-02-3 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 20000 FC  614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  574605-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  614 LH/RH. I: 12 YE I: 12 YE  574606-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4 TRAILING EDGE, T: 3 YE  614 LOWER FACE, 100 MM FROM 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 SURFACE T: 6 YE  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 574701-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 , T: 12 YE T: 20 YE  615 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574701-02-4 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 20000 FC  615 12 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 13300 FC  OR  43500 FH  R 574703-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 T: 12 YE  615 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574703-02-3 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5, TRACKS 11 AND 12 T: 20000 FC  615 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574704-03-1.  R 574704-02-3 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT T: 20000 FC  615 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  R 574704-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  615 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 574704-01-1.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 574705-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  615 LH/RH. I: 12 YE I: 12 YE  574706-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5 TRAILING EDGE, T: 3 YE  615 LOWER FACE, 100 MM FRONT 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.  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  574801-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND 14; T: 12 YE T: 20 YE  616 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  R 574801-02-3 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 20000 FC  616 14; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 7000 FC  OR  22800 FH  R 574803-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND 14 T: 12 YE  616 ATTACHMENTS INCLUDING TRACK RIB LUGS,TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574803-02-3 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6, TRACKS 13 AND 14 T: 20000 FC  616 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 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 STATIONS, I: 12 YE I: 12 YE  INTERNAL, LH/RH.  NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME AS  TASK 574804-03-2.  574804-02-1 N/A TASK DELETED  R 574804-02-4 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT T: 20000 FC  616 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  R 574804-03-2 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT T: 12 YE T: 20 YE  616 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 574804-01-1.  574805-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  616 LH/RH. I: 12 YE I: 12 YE  R 574806-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6 TRAILING EDGE T: 3 YE  616 LOWER FACE, 100 MM FRONT 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 SURFACE T: 6 YE  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  574901-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND 16; T: 12 YE T: 20 YE  617 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 574901-02-3 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 20000 FC  617 16; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OR  50000 FH  I: 7000 FC  OR  22800 FH  R 574903-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND 16 T: 12 YE  617 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YE  BOLTS, LINKS AND LINK PLATE, LH/RH.  R 574903-02-3 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7, TRACKS 15 AND 16 T: 20000 FC  617 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, OR  BOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FH  I: 6600 FC  OR  24000 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 STATIONS, I: 12 YE I: 12 YE  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 CONNECTIONS AT T: 12 YE T: 20 YE  617 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 574904-01-1.  R 574904-02-4 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN CONNECTIONS AT T: 20000 FC  617 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OR  50000 FH  I: 9300 FC  OR  27900 FH  574905-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7 HOLD DOWN BRACKET, T: 12 YE T: 20 YE  617 LH/RH. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 R 574906-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7 TRAILING EDGE T: 3 YE  617 LOWER FACE, 100 MM FRONT 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 RECORD CPCP ONLY.  THE TASK IS COVERED BY MSI 27.80.00.  574908-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 7, EXTERNAL SURFACE T: 6 YE  600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YE  575001-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YE  20000 FC  I: 12 YE  OR  10700 FC  575001-01-4 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YE  17000 FC  I: 12 YE  OR  12900 FC  575001-01-6 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  SPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YE  20000 FC  I: 12 YE  OR  12900 FC  N 575001-01-7 FLAPS EXTENDED SLATS 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITING. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
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 575002-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE  673BB 673DB 673FB 673 1-6, COMPRISING ATTACHMENTS TO REAR SPAR OR FALSE I: 12 YE I: 12 YE  REAR SPAR AND SPOILER 1 HINGE FITTINGS.  575003-01-1 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 (5 I: 12 YE I: 12 YE  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 (5 OR I: 12 YE  PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 20000 FC  OVERHANG. I: 12 YE  OR  20000 FC  575004-01-4 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 17000 FC  OVERHANG. I: 12 YE  OR  17000 FC  575004-01-6 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 20000 FC  SKIN OVERHANG. I: 12 YE  OR  20000 FC  N 575004-01-7 FLAPS EXTENDED SLATS 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  EXTENDED 674 SPOILERS 2,3,4,5 AND 6 ACTUATOR SUPPORT FITTING I: 12 YE I: 12 YE  (5 PLACES)ATTACHMENT TO REAR SPAR AND TOP SKIN  OVERHANG.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 575005-01-1 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 (16 PLACES).  575006-01-1 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 (4 PLACES) I: 12 YE I: 12 YE  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 EDGE RIB T: 12 YE T: 20 YE  SPOILERS EXTENDED 574 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 EDGE T: 12 YE  573EB 573FB 573GB 673 RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, TOP AND I: 12 YE  673BB 673CB 673DB BOTTOM SKIN OVERHANGS AND OUTER FLAP CRUISE ROLLER  673EB 673FB 673GB SUPPORT ATTACHMENT TO TRAILING EDGE RIB 10.  575010-01-1 N/A TASK DELETED  575010-01-10 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. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  20000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575010-01-11 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. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  15900 FC  OR  50000 FH  N 575010-01-12 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES I: 12 YE I: 12 YE  575010-01-4 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  7500 FC  OR  27000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575010-01-5 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  8300 FC  OR  26700 FH  575010-01-6 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  7000 FC  OR  22600 FH  575010-01-7 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE  673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE  17000 FC  OR  50000 FH  I: 12 YE  OR  15900 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575010-01-8 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. OR I: 12 YE  17000 FC  OR  50000 FH  I: 12 YE  OR  17000 FC  OR  50000 FH  575010-01-9 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. OR I: 12 YE  20000 FC  OR  50000 FH  I: 12 YE  OR  6800 FC  OR  21900 FH  575011-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FC  600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 OR  AND RIB 14. 50000 FH  I: 8700 FC  OR  38400 FH  R 575011-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 14. 59500 FH  I: 19000 FC  OR  56600 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 575011-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FC  600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND OR  RIB 14. 90700 FH  I: 17300 FC  OR  78500 FH  575011-01-5 N/A TASK DELETED  R 575011-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FC  600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND OR  RIB 14. 59300 FH  I: 19400 FC  OR  57600 FH  575011-01-7 N/A TASK DELETED  575011-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 17000 FC  600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND OR  RIB 14. 50000 FH  I: 10000 FC  OR  28500 FH  575011-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 17000 FC  600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 OR  AND RIB 14. 50000 FH  I: 8300 FC  OR  36500 FH  575011-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE NO  600 TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 I: 12 YE  AND RIB 14.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 575012-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 8000 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  22900 FH  575012-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6800 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  30600 FH  575012-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 5200 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  21000 FH  575012-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 4200 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  13700 FH  R 575012-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 5200 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  16500 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575012-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6800 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  30600 FH  575012-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 8000 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  22900 FH  575012-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN OR  RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH  2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 4800 FC  INBOARD OF GEAR SUPPORT RIB 6. OR  15300 FH  575012-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN I: 6 YE  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 SUPPORT RIB 6.  575013-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 14900 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575013-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 10600 FC  OR  34000 FH  575013-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 14700 FC  OR  46200 FH  575013-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 17000 FC  600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR OR  JUST INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 12300 FC  OR  50000 FH  575013-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 14500 FC  OR  41400 FH  575013-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 13900 FC  OR  43800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575013-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  .NBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 15400 FC  OR  42800 FH  575013-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FC  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST OR  INBOARD OF GEAR SUPPORT RIB 6. 50000 FH  I: 12300 FC  OR  50000 FH  575013-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO  600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6 YE  INBOARD OF GEAR SUPPORT RIB 6.  575014-01-4 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 17700 FC  OR  50000 FH  575014-01-5 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 14800 FC  OR  47300 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575014-01-6 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 16700 FC  OR  50000 FH  575014-01-7 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 17000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 17000 FC  OR  50000 FH  575014-01-8 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 16200 FC  OR  50000 FH  575014-01-9 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG OR  REINFORCING. 50000 FH  I: 20000 FC  OR  50000 FH  575015-01-1 454HL 464HL 532AB 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE NO  533AB 534AB 632AB 464 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB I: 12 YE  633AB 634AB 500 12 TO RIB 39.  532  533  534  600  632  633  634  575016-01-1 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575016-01-10 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8000 FC  OR  22900 FH  575016-01-11 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8500 FC  OR  23700 FH  575016-01-12 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6800 FC  OR  30600 FH  R 575016-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8300 FC  OR  37700 FH  575016-01-5 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 7700 FC  OR  24700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 575016-01-6 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 8000 FC  OR  23700 FH  575016-01-7 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 UNDER FLAP I: 12 YE I: 12 YE  TRACK 2 FAIRING.  R 575016-01-8 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 7600 FC  OR  22500 FH  575016-01-9 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP OR  TRACK 2 FAIRING. 50000 FH  I: 6800 FC  OR  30600 FH  R 575017-01-4 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, OR  INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FH  OF GEAR SUPPORT RIB 6. I: 5000 FC  OR  22800 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575017-01-5 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, OR  INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FH  OF GEAR SUPPORT RIB 6. I: 8200 FC  OR  26400 FH  R 575017-01-6 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, OR  INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FH  OF GEAR SUPPORT RIB 6. I: 5500 FC  OR  16300 FH  R 575017-01-7 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, OR  INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST 50000 FH  OUTBOARD OF GEAR SUPPORT RIB 6. I: 5200 FC  OR  15500 FH  575017-01-8 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 17000 FC  673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, OR  INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FH  OF GEAR SUPPORT RIB 6. I: 17000 FC  OR  50000 FH  575017-01-9 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FC  673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL OR  AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FH  OF GEAR SUPPORT RIB 6. I: 20000 FC  OR  50000 FH  575017-02-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO  673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND I: 6 YE  EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR  SUPPORT RIB 6.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575018-01-10 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  192CT 672 ATTACHMENT OF SHROUD BOX. OR  FLAPS EXTENDED 50000 FH  I: 20000 FC  OR  50000 FH  575018-01-3 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  192CT 672 ATTACHMENT OF SHROUD BOX. OR  FLAPS EXTENDED 50000 FH  I: 20000 FC  OR  50000 FH  D 575018-01-4 N/A TASK DELETED  575018-01-5 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  192CT 672 ATTACHMENT OF SHROUD BOX. OR  FLAPS EXTENDED 50000 FH  I: 20000 FC  OR  50000 FH  575018-01-6 N/A TASK DELETED  575018-01-7 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  192CT 672 ATTACHMENT OF SHROUD BOX. OR  FLAPS EXTENDED 50000 FH  I: 17000 FC  OR  50000 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575018-01-8 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  192CT 672 ATTACHMENT OF SHROUD BOX. OR  FLAPS EXTENDED 50000 FH  I: 17000 FC  OR  50000 FH  575018-02-1 147AT 148AT 191CT 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 10 YE  192CT 672 ATTACHMENT OF SHROUD BOX. I: 10 YE  FLAPS EXTENDED  R 575019-01-1 147AT 148AT 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 10 YE  671 ATTACHMENT OF OVERWING PANEL. I: 10 YE  575022-01-1 N/A TASK DELETED  575022-01-2 N/A TASK DELETED  D 575022-01-3 N/A TASK DELETED  D 575022-01-5 N/A TASK DELETED  575022-01-6 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675BB 675 INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO I: 12 YE I: 12 YE  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.  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 575023-01-1 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FC  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YE  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OR  EXTERNAL. 9000 FC  575023-01-3 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT OR I: 12 YE  TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, 17000 FC  HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO OR  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL 50000 FH  AND EXTERNAL. I: 12 YE  OR  7300 FC  OR  42800 FH  575023-01-4 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 17000 FC  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR OR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND 50000 FH  EXTERNAL. I: 12 YE  OR  8400 FC  OR  26500 FH  575023-01-5 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FC  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YE  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OR  EXTERNAL. 9200 FC  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 575023-01-6 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FC  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YE  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OR  EXTERNAL. 9200 FC  R 575023-01-7 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FC  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR OR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND 50000 FH  EXTERNAL. I: 12 YE  OR  7300 FC  OR  42800 FH  N 575023-01-8 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE  675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO I: 12 YE I: 12 YE  REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4  AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR  AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND  EXTERNAL.  575025-01-10 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  FROM RIB 8 TO RIB 12. 50000 FH  I: 8500 FC  OR  23700 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 575025-01-11 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM OR  RIB 8 TO RIB 12. 50000 FH  I: 6800 FC  OR  30600 FH  R 575025-01-4 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  531 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 OR  600 TO RIB 12. 50000 FH  631 I: 7300 FC  OR  33300 FH  R 575025-01-5 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  531 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 OR  600 TO RIB 12. 50000 FH  631 I: 6600 FC  OR  19700 FH  R 575025-01-6 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 OR  TO RIB 12. 50000 FH  I: 8100 FC  OR  24000 FH  R 575025-01-7 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 OR  TO RIB 12. 50000 FH  I: 8400 FC  OR  23900 FH  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 575025-01-8 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM OR  RIB 8 TO RIB 12. 50000 FH  I: 7100 FC  OR  32000 FH  R 575025-01-9 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FC  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR OR  FROM RIB 8 TO RIB 12. 50000 FH  I: 7600 FC  OR  22700 FH  575025-02-1 532AB 632AB 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE  600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 I: 12 YE  TO RIB 12.  575051-01-1 N/A TASK DELETED  R 575053-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, DRIVE LINK, T: 12 YE T: 20 YE  FLAPS EXTENDED 148 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 BOX, T: 12 YE T: 20 YE  FLAPS EXTENDED 148 FORK ASSY, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 575055-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, ATTACHMENTS 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.  575055-01-2 N/A TASK DELETED  575057-01-2 N/A TASK DELETED  R 575059-01-1 AFT FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, T: 12 YE T: 20 YE  FAIRINGS 532 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE I: 12 YE I: 12 YE  FLAPS EXTENDED 533 ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND  534 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.2,3,4 AND 5, T: 12 YE T: 20 YE  532 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  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 575063-01-3 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  R 575065-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO. T: 12 YE T: 20 YE NO  532 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 AND T: 12 YE T: 20 YE  FAIRINGS 532 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 BOLT 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO. T: 12 YE T: 20 YE NO  FWD FLAP TRACK 532 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 
A330 MRB REPORT – Structures Section

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 TPS

 R 575069-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2,3,4 AND T: 12 YE T: 20 YE NO  532 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE  533  534  631  632  633  634  575069-01-2 N/A TASK DELETED  R 575401-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL T: 6 YE  600 SURFACE OF UPPER AND LOWER SKIN. I: 6 YE  575401-01-2 N/A TASK DELETED  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 SUPPORT T: 12 YE T: 20 YE  744 681 FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND I: 12 YE I: 12 YE  EXTERNAL.  575403-01-2 N/A TASK DELETED  R 575403-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  744 681 SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL. I: 12 YE I: 12 YE  SPEED TAPES  N 575404-01-1 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 
A330 MRB REPORT – Structures Section

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 N 575404-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 6 YE  681 EDGE. I: 6 YE  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 SUPPORT T: 12 YE T: 20 YE  631CB 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  ATTACHMENT BRACKET.  575405-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 575405-01-3 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE  631CB 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  ATTACHMENT BRACKET.  R 575405-02-1 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  631CB 681 SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YE  FLAPS EXTENDED  SPEED TAPES  R 575405-02-2 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO  631CB 681 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 END-RIB T: 12 YE T: 20 YE NO  RUBBER SEALS 681 INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT I: 12 YE I: 12 YE  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  N 575501-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 6 YE  600 SURFACES OF UPPER AND LOWER SKIN. I: 6 YE  575501-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 6 YE  600 SURFACE OF UPPER AND LOWER SKIN I: 6 YE  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 575503-01-1 532AT 532CB 632AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE  632CB 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 ATTACHMENT  FITTING.  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, INTERNAL T: 12 YE T: 20 YE  633CB 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.  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, INTERNAL T: 12 YE T: 20 YE  633CB 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.  575507-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 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  576101-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, UPPER AND T: 6 YE  690 LOWER SKINS, EXTERNAL SURFACE I: 6 YE  576103-01-1 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  576104-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS (7 T: 12 YE T: 20 YE  592AB 592BB 592CB 692 PLACES) I: 12 YE I: 12 YE  592DB 675BT 675CB  675DB 692AB 692BB  692CB 692DB  R 576106-01-2 JACK FITTING FAIRING 592 DETAILED INSPECTION OF OUTBOARD AILERONS, FIRST LINE T: 20000 FC  692 OF FASTENERS ON OUTER JACK FITTING FLANGE LH/RH. I: 5100 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  576106-02-2  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 R 576106-02-2 JACK FITTING FAIRING 592 SPECIAL DETAILED INSPECTION OF OUTBOARD AILERONS, T: 20000 FC  692 FIRST LINE OF FASTENERS ON OUTER JACK FITTING FLANGE I: 14600 FC  LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  576106-01-2  576111-01-1 N/A 500 DETAILED INSPECTION OF INBOARD AILERON, UPPER AND T: 6 YE  600 LOWER SKINS, EXTERNAL SURFACE I: 6 YE  576113-01-1 INBOARD AILERON ONLY 591 DETAILED INSPECTION OF INBOARD AILERON END RIBS, T: 12 YE T: 20 YE  DEFLECTED 691 EXTERNAL SURFACE I: 12 YE I: 12 YE  576114-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON FITTINGS (7 T: 12 YE T: 20 YE  591AB 591BB 591CB 691 PLACES) I: 12 YE I: 12 YE  591DB 675AB 675AT  675BB 691AB 691BB  691CB 691DB  R 576116-01-3 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD AILERONS, T: 20000 FC  691 FIRST LINE OF FASTENERS ON OUTER JACK FITTING FLANGE, I: 14600 FC  LH/RH.  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  576116-02-2  R 576116-02-2 JACK FITTING FAIRING 591 DETAILED INSPECTION OF INBOARD AILERONS, FIRST LINE T: 20000 FC  691 OF FASTENERS ON OUTER JACK FITTING FLANGE, LH/RH. I: 5100 FC  NOTE: THIS TASK IS AN ALTERNATIVE TO TASK  576116-01-3  R 577001-01-2 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO.1, UPPER AND T: 6 YE  SPOILERS DEPLOYED 682 LOWER SKIN, EXTERNAL SURFACE,LH/RH. I: 6 YE  R 577003-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO. 1, HINGE AND T: 12 YE T: 20 YE  SPOILERS DEPLOYED 682 ACTUATOR ATTACHMENT FITTINGS. I: 12 YE I: 12 YE  577003-01-2 N/A TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: D-57 
A330 MRB REPORT – Structures Section

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 TPS

 R 711141-01-1 415AL 416AR 425AL 411 GENERAL VISUAL INSPECTION OF INLET COWL ATTACHMENT T: 6 YE NO  426AR 421 (A1 FLANGE). I: 6 YE  711141-01-2 N/A TASK DELETED  R 711142-01-1 415AL 416AR 425AL 411 GENERAL VISUAL INSPECTION OF SURROUNDING STRUCTURE OF T: 3 YE  426AR 421 INLET COWL ATTACHMENT (15 CM AROUND A1 FLANGE). I: 3 YE  711200-01-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND T: 3 YE  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YE  425  426  711200-01-2 N/A TASK DELETED  711200-02-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR HINGES AND T: 12 YE NO  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 12 YE  DISASSEMBLY OF PIN 425  ASSY 426  711246-01-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES T: 3 YE  426AR 416 AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 3 YE  425 FITTINGS).  426  711246-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A330 MRB REPORT – Structures Section

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 711246-02-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR LATCHES AND T: 6 YE NO  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 6 YE  425  426  711301-01-1 415AL 415BL 416AR 415 DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR T: 6 YE NO  416BR 425AL 425BL 416 HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE I: 6 YE  426AR 426BR 425 FITTINGS).  426  711301-02-1 415AL 415BL 416AR 415 GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL T: 3 YE  416BR 425AL 425BL 416 DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  426AR 426BR 425 HINGE FITTINGS).  426  711301-02-2 N/A TASK DELETED  711302-01-1 415AL 415BL 416AR 415 DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR T: 6 YE NO  416BR 425AL 425BL 416 LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 6 YE  426AR 426BR 425 FITTINGS).  426  711302-02-1 415AL 415BL 416AR 415 GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL T: 3 YE  416BR 425AL 425BL 416 DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  426AR 426BR 425 LATCH FITTINGS).  426  711302-02-2 N/A TASK DELETED  R 711341-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR HINGES AND T: 6 YE NO  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 6 YE  425  426  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A330 MRB REPORT – Structures Section

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 R 711341-02-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND T: 3 YE  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YE  425  426  711341-02-2 N/A TASK DELETED  R 711343-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR LATCHES AND T: 6 YE NO  426AR 416 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 6 YE  425  426  711343-02-1 N/A TASK DELETED  R 711345-01-1 414AL 414AR 424AL 414 DETAILED INSPECTION OF CORE COWL DOOR HINGES AND T: 12 YE NO  424AR 424 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 12 YE  711345-02-1 N/A TASK DELETED  711347-01-1 N/A TASK DELETED  R 711347-02-1 414AL 414AR 424AL 414 DETAILED INSPECTION OF CORE COWL DOOR LATCHES AND T: 12 YE NO  424AR 424 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 12 YE  712101-01-2 N/A TASK DELETED  712101-02-1 N/A TASK DELETED  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A330 MRB REPORT – Structures Section

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 TPS

 712101-03-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO  FWD ENGINE MOUNT 423 I: 12 YE  DISASSEMBLED  712101-04-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO  FWD ENGINE MOUNT 423 I: 12 YE  DISASSEMBLED  R 712101-06-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO  FWD ENGINE MOUNT 423 I: 12 YE  DISASSEMBLED  712102-01-1 N/A TASK DELETED  712102-01-2 N/A TASK DELETED  712103-01-1 N/A TASK DELETED  712103-01-2 N/A TASK DELETED  712103-01-3 N/A TASK DELETED  712103-01-4 N/A TASK DELETED  712104-01-1 N/A TASK DELETED  712105-01-1 N/A TASK DELETED  712106-01-1 N/A TASK DELETED  712106-01-2 N/A TASK DELETED  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A330 MRB REPORT – Structures Section

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 TPS

 R 712201-03-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO  DISASSEMBLED 423 I: 12 YE  ENGINE  R 712201-04-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO  DISASSEMBLED 423 I: 12 YE  ENGINE  R 712201-05-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO  DISASSEMBLED 423 I: 12 YE  ENGINE  712202-01-1 N/A TASK DELETED  712203-01-1 N/A TASK DELETED  712204-01-1 N/A TASK DELETED  712204-02-1 N/A TASK DELETED  712204-02-2 N/A TASK DELETED  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT SECTION: D-71 
A330 MRB REPORT – Structures Section

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INTERVAL 

 TPS

 783200-01-1 N/A TASK DELETED  783200-01-2 N/A TASK DELETED  783200-02-1 417DL 417EL 418DR 417 DETAILED INSPECTION OF THRUST RESERVER HINGES, T: 6 YE NO  418ER 427DL 427EL 418 SLEEVES AND PINS. I: 6 YE  428DR 428ER 427  PINS, SLEEVES AND 428  BUSHES  783200-03-1 417DL 417EL 418DR 417 SPECIAL DETAILED INSPECTION OF THRUST RESERVER HINGE T: 3 YE  418ER 427DL 427EL 418 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YE  428DR 428ER 427  428  R 783201-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER HINGES, T: 6 YE NO  418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 6 YE  427AL 428AR 427 HINGE ATTACHMENTS).  FWD HINGE COVER, 428  HINGE BEAM PINS  783201-02-1 415BL 416BR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER HINGES AND T: 6 YE NO  418AR 425BL 426BR 418 PINS. I: 6 YE  427AL 428AR 427  FWD HINGE COVER 428  783201-03-1 N/A TASK DELETED  R 783201-03-2 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, T: 3 YE  418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  427AL 428AR 427 HINGE ATTACHMENTS).  428  783201-04-1 N/A TASK DELETED  ISSUE: JUL 01/10 EXHAUST SECTION: D-78 
A330 MRB REPORT – Structures Section

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 REFERENCE 

 TASK DESCRIPTION SAMPLE THRESHOLD

 INTERVAL 

 

100% THRESHOLD

INTERVAL 

 TPS

 783201-04-2 415BL 416BR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, T: 3 YE  418AR 425BL 426BR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  427AL 428AR 427 HINGE ATTACHMENTS).  428  R 783202-01-1 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, T: 3 YE  418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  427AL 428AR 427 LATCH ATTACHMENTS).  LATCH ACCESS DOOR 428  783202-01-2 N/A TASK DELETED  783202-02-1 415BL 416BR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, T: 3 YE  418AR 425BL 426BR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE  427AL 428AR 427 LATCH ATTACHMENTS).  LATCH ACCESS DOOR 428  783202-02-2 N/A TASK DELETED  783203-01-1 DEPLOY TRANSLATING 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 3 YE  COWL 418 TRANSLATING COWL T-SLIDER, ATTACHMENTS AND I: 3 YE  427 SURROUNDING STRUCTURE (15 CM AROUND T-SLIDER  428 ATTACHMENTS).  783245-01-1 418HR 418JR 428HR 417 SPECIAL DETAILED INSPECTION OF THRUST REVERSER T: 3 YE  428JR 418 LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 3 YE  427 FITTINGS).  428  783245-02-1 N/A TASK DELETED  783245-02-2 418HR 418JR 428HR 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES T: 6 YE NO  428JR 418 AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 6 YE  427 FITTINGS).  428  * * * * * E N D * * * * *  ISSUE: JUL 01/10 EXHAUST SECTION: D-78 
 A330 MRB REPORT 

Issue : July 2010 Page : E-INTRO-1

SECTION E

 ZONAL

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 and security (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. 

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 
 A330 MRB REPORT 

Issue : July 2010 Page : E-INTRO-2

be deleted from an operator’s maintenance program. 

With respect to General Rule 18 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 SSI's 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 SSI's and MSI's 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 sections. 

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 
 A330 MRB REPORT 

Issue : July 2010 Page : E-INTRO-3

700 Landing gear & landing gear doors 36 hours 

800 Doors 36 hours 

123 Nose gear well 7 days 

149 Center line bay 7 days 

711 Nose landing gear 7 days 

731/741 LH & RH main landing gear 7 days 

4. INSPECTIONS INTERVALS

 It is recommended that these inspection intervals are considered by all operators: 

 Check Interval 

 

 A - Check & multiples - 800 FH & multiples 

 C - Check - 18 months 

 2C - Check - 36 months 

 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. 
 A330 MRB REPORT 

Issue : July 2010 

Sequence number: Indicates separate tasks within the same 

Zone number: Indicates the zone number Abbreviation for Zonal 

Applicablity index: Identifies successive variants of the Task 

ZL – XXX – XX - X

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:

The Zone number is represented by the three first digits, 151-01-01. The first digit, 151-01-01, is in accordance with the A330 

breakdown, showing the major section where the zone is located e.g 100 Lower Half of Fuselage. The second digit, 151-01-0

with the A330 ATA 100 breakdown, showing the sub section where the zone is located e.g 150 Aft Cargo Compartment. The tthe sub section where the zone is located e.g (RH- or LH - side of applicable the zone). 

The Sequential Number is composed of two digits. It follows the Zone number and is separated by a dash e.g. 151-01-01. 

inspections at different intervals . These two digits are also changed when the inspections have a major difference in access (e

The Applicability Index is composed of one digit. It follows the Sequential Number and is separated by a dash, 151-0

applicability e.g aircraft series, mod status etc ...This digit is also used to differentiate between minor access differences enumbers and differences in reference information. 

2- This column indicates the access and preparation requirements to adequately perform the inspection. 
 A330 MRB REPORT 

Issue : July 2010 

(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 FR XY " 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. 7- This column indicates the A/C model/Mod status/engine type to which this requirement is applicable. 
This page intentionally left blank 
A330 MRB REPORT – Zonal Section

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 R ZL-100-01-2 N/A 100 LOWER HALF OF FUSELAGE I: C MSI N SSI 5 SSI 5 SSI 5 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-121-02-1 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  122KF 122LF 122NF  122PF 131AW 131BW  132AZ 132CW 821  NOTE 1  ZL-121-02-2 N/A TASK DELETED MSI N SSI N R ZL-123-01-1 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI N SSI N N ZL-125-01-1 125AL 125BL 125CL 125 NOSE FAIRING, FR10 TO BETWEEN FR21 AND FR22, LH/RH. I: 48 MO MSI N 125DL 125EL 125FL 126  125GL 125HL 126BR SSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-125-01-1 * * * * * C O N T I N U E * * * * *  126CR 126FR  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 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 131BC 131FC 131FX 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI N 131KW 131PC 131RC 132  131TC 131VC 131XC SSI N 132FX 132UW 132WW  821  N ZL-131-02-3 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 132  SSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-131-02-3 * * * * * C O N T I N U E * * * * *  SIDEWALL AND CEILING  PANELS FROM FR 20 TO  FR 39.2  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 FR 20 TO  FR 39.2  ZL-131-04-1 N/A TASK DELETED MSI N SSI N R ZL-133-01-1 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 FLOOR PANELS FROM 134 MSI 2 FR20 TO FR 39.2 MSI 3 NOTE 1  SSI N R ZL-137-01-1 131BX 131CG 131CX 137 BAY BEHIND FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI 2 131DG 131DX 132CG 138  132CX 132DG 132DX SSI N 821  R ZL-141-01-1 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI N 744 142  SSI 5 D ZL-141-01-2 N/A CENTER WING TANK MSI N TASK DELETED SSI N ZL-141-03-1 N/A TASK DELETED MSI N SSI N ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A330 MRB REPORT – Zonal Section

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 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 HYDRAULICS COMPARTMENT (EWIS) I: A MSI 2 148  SSI N ZL-149-01-1 N/A TASK DELETED MSI N SSI N R ZL-149-05-1 149AB 149CB 734 149 CENTER LINE BAY (EWIS) I: 8 C MSI N 744  SSI N R ZL-151-01-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: A MSI 2 152 MSI 2 (AS FAR AS VISIBLE IF LD-MCR AND/OR LDL INSTALLED) 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 ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
A330 MRB REPORT – Zonal Section

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 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  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  LD-MCR-IF INSTALLED  R ZL-151-02-3 151BC 151BW 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151JW 151TW 152BW 152  152DW 152EW 152GW SSI N 152JW 822  R ZL-151-02-4 151EC 151FX 151HX 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI N 151LX 151NC 152FX 152  152HX 152LX 822 SSI N LAVATORIES AND LDL-  FURNISHING  LD-MCR-IF INSTALLED  N ZL-151-02-5 822 000 AFT CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 SIDEWALL AND CEILING  PANELS FROM FR 53.2 SSI N TO FR 66  R ZL-151-03-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 LD-MCR-IF INSTALLED 152  NOTE 1 SSI N SIDEWALL AND CEILING  PANELS FROM FR 53.2  TO FR 66  ZL-151-04-1 N/A TASK DELETED MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-151-04-1 * * * * * C O N T I N U E * * * * *  SSI N 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 2 53.2 TO FR 66, MSI 3 LD-MCR-IF INSTALLED  NOTE 1 SSI N 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 53.2 TO FR66  LDL - LAVATORIES AND SSI N FURNISHING  LD-MCR-IF INSTALLED  NOTE 1  R ZL-161-01-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: A MSI 2 162 MSI 3 (IF FLIGHT KIT CONTAINER INSTALLED, AS FAR AS  VISIBLE) SSI N 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  N ZL-161-02-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 72 MO MSI N FLIGHT KIT CONTAINER 162  REMOVED, IF SSI N INSTALLED  SIDEWALL AND CEILING  PANELS FROM FR 65 TO  FR 73  R ZL-161-03-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 3 NOTE 1 162  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-161-03-1 * * * * * C O N T I N U E * * * * *  SIDEWALL AND CEILING SSI N PANELS FROM FR 65 TO  FR 73  N ZL-161-03-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 144 MO MSI N FLIGHT KIT CONTAINER 162  REMOVED, 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 FLOOR PANELS FROM FR 164  65 TO FR 73 SSI N NOTE 1  N ZL-163-01-2 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 FLIGHT KIT CONTAINER 164  REMOVED, 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 N ZL-171-01-2 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 24 MO MSI N 172  SSI N R ZL-171-02-1 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 3 FLOOR PANELS FROM FR 172 MSI 3 73 TO FR 80  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-171-02-1 * * * * * C O N T I N U E * * * * *  NOTE 1 SSI 5 N ZL-171-02-2 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 72 MO MSI N FLOOR PANELS FROM FR 172  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 2 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-193-01-1 193BB 193DB 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-195-01-1 734 744 195 HYDRAULIC COMPARTMENT AND FAIRINGS (AS FAR AS I: A MSI N 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 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 ZL-195-02-1 * * * * * C O N T I N U E * * * * *  SSI N R ZL-197-01-1 734 744 197 REAR FAIRINGS (EWIS) I: A MSI N 198  SSI N R ZL-197-02-1 197EB 198EB 197 REAR FAIRINGS (EWIS) I: 4 C MSI N 198  SSI N * * * * * E N D * * * * *  ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100 
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 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 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  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  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
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 ZL-221-01-1 N/A TASK DELETED MSI N SSI N R ZL-221-02-1 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 2 CREW REST ROOM IF 222  INSTALLED SSI 5 DOOR FRAME LINING  FLOOR PANELS FROM FR  11 TO FR 17  GALLEYS AND TOILETS  IF INSTALLED  NOTE 1  SEATS AND  FURNISHINGS  N ZL-221-03-1 831 841 221 COURIER COMPARTMENT (EWIS) I: 144 MO MSI N FCRC, GALLEYS AND 222  TOILETS IF INSTALLED SSI N NOTE 1  SEATS AND  FURNISHINGS  SIDEWALL AND DOOR  FRAME LINING AND  FLOOR PANELS FROM  FRAME FR 11/11A TO  FR 19/20  R ZL-223-01-1 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 - IF  INSTALLED FROM FR 11  TO FR 17  NOTE 1  N ZL-223-02-1 831 841 223 COURIER OVERHEAD COMPARTMENT (EWIS) I: 144 MO MSI N 224  SSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
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 ACCESS DESCRIPTION INTERVAL 

R

 ZL-223-02-1 * * * * * C O N T I N U E * * * * *  CEILING PANELS AND  UPPER SIDEWALL  LININGS FROM FR  11/11A TO FR 19/20  FCRC, GALLEYS AND  TOILETS 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  N ZL-231-03-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 2 BARRIER WALL (AFT 232 OR MSI 2 FACE) INCLUDING 6 MO MSI 2 UPPER SURFACE (ZONE MSI 2 233/234), BARRIER MSI 2 WALL ACCESS DOORS, MSI 2 LH/RH MSI 2 MSI 2 MSI 2 MSI 2 SSI N N ZL-231-04-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 232  SSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-231-04-1 * * * * * C O N T I N U E * * * * *  FLOOR PANELS BETWEEN  FR 19/20 AND FR 31,  LOWER SIDEWALL  LININGS (DADO  PANELS)  NOTE 1  N ZL-231-05-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 232  SIDEWALL LININGS SSI N FROM FR 19/20 TO FR  31.  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  N ZL-233-02-1 835 233 FWD MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI N UPPER SIDEWALL 234  LININGS BETWEEN FR SSI N 19/20 AND FR 31  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 LINING 242  AND FLOOR PANELS SSI 5 FROM FR 31 TO FR 36 SSI 5 GALLEYS AND TOILETS  IF INSTALLED  NOTE 1  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-241-02-1 * * * * * C O N T I N U E * * * * *  SEATS AND  FURNISHINGS  N ZL-241-03-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 800 FH MSI 2 242 OR MSI 2 6 MO MSI 2 MSI 2 MSI 2 SSI N N ZL-241-04-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 72 MO MSI 2 FLOOR PANELS BETWEEN 242  FR 31 AND FR 36 SSI N LOWER SIDEWALL (DADO  PANELS)  NOTE 1  N ZL-241-05-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 144 MO MSI N NOTE 1 242  SIDEWALL LININGS SSI N BETWEEN FR 31 AND FR  36  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  N ZL-243-02-1 835 243 FWD MID MAIN DECK OVERHEAD CARGO COMPARTMENT AREA I: 144 MO MSI N NOTE 1 244 (EWIS)  UPPER SIDEWALL SSI N LININGS FROM FR 31  TO FR 36  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-251-01-1 N/A TASK DELETED MSI N SSI N R ZL-251-02-1 834 842 251 MID CABIN (EWIS) I: 8 C MSI 2 GALLEYS, TOILETS AND 252  STAIRHOUSE (IF SSI 5 INSTALLED)  NOTE 1  SEATS AND  FURNISHINGS  SIDEWALL AND FLOOR  PANELS FROM FR 36 TO  FR 53.5  N ZL-251-03-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 2 252 OR MSI 2 6 MO MSI 2 MSI 2 SSI N N ZL-251-04-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 FLOOR PANELS BETWEEN 252  FR 36 AND FR 53.5 SSI N LOWER SIDEWALL  LININGS (DADO  PANELS)  NOTE 1  N ZL-251-05-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 252  SIDEWALL LININGS SSI 5 BETWEEN FR 36 TO FR  53.5  R ZL-253-01-1 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 2 CEILING PANELS 254  SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-253-01-1 * * * * * C O N T I N U E * * * * *  GALLEYS, TOILETS AND  STAIRHOUSE (IF  INSTALLED) FROM FR36  TO FR53.5  NOTE 1  OVERHEAD STOWAGE  BINS  N ZL-253-02-1 835 253 MID MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 254  UPPER SIDEWALL SSI 5 LININGS BETWEEN FR  36 TO FR 53.5  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 LINING 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  N ZL-261-03-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 2 262 OR MSI 2 6 MO MSI 2 MSI 2 SSI N N ZL-261-04-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 262  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-261-04-1 * * * * * C O N T I N U E * * * * *  FLOOR PANELS BETWEEN SSI N FR 53.5 TO FR 72  LOWER SIDEWALL  LININGS (DADO  PANELS)  NOTE 1  N ZL-261-05-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 262  SIDEWALL LININGS SSI N BETWEEN FR 53.5 TO  FR 72  R ZL-263-01-1 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI N CEILING PANELS 264  GALLEYS AND TOILETS SSI 5 (IF INSTALLED) FROM  FR 53.5 TO FR 72  NOTE 1  OVERHEAD STOWAGE  BINS  N ZL-263-02-1 835 263 AFT MID MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 264  UPPER SIDEWALL SSI N LININGS FROM FR 53.5  TO FR 72  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 DOOR FRAME LININGS, 272  SIDEWALL AND FLOOR SSI 5 PANELS FROM FR 72 TO SSI 5 FR 80 SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 ZL-271-02-1 * * * * * C O N T I N U E * * * * *  GALLEYS AND TOILETS  IF INSTALLED  NOTE 1  SEATS AND  FURNISHINGS  N ZL-271-03-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 2 272 OR MSI 2 6 MO MSI 2 MSI 2 MSI 2 MSI 2 SSI N N ZL-271-04-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 2 FLOOR PANELS BETWEEN 272  FR 72 TO FR 80/82 SSI N LOWER SIDEWALL (DADO  PANELS)  NOTE 1  N ZL-271-05-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI N NOTE 1 272  SIDEWALL LININGS SSI 5 BETWEEN FR 72 TO FR  80/82  R ZL-273-01-1 271AZ 271BZ 271CZ 273 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  N ZL-273-02-1 835 273 AFT MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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R

 ZL-273-02-1 * * * * * C O N T I N U E * * * * *  NOTE 1 274 SSI 5 UPPER SIDEWALL  LININGS FROM FR 72  TO FR 80/82  * * * * * E N D * * * * *  ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200 
A330 MRB REPORT – Zonal Section

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 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 SSI 5 SSI 5 R ZL-311-01-1 312AR 313AL 311 REAR FUSELAGE SECTIO (EWIS) I: C MSI 2 312 MSI 4 SSI 5 SSI 5 SSI 5 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 SSI N R ZL-315-01-1 315AL 316AR 315 TAIL CONE, APU AND ACCESSORY COMPARTMENT (EWIS) I: C MSI 4 316  SSI N R ZL-317-01-1 317AL 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 ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 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 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 322DL  SSI 5 R ZL-322-01-3 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 SSI 5 SSI 5 R ZL-323-02-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 ZL-323-02-1 * * * * * C O N T I N U E * * * * *  322AL 322BL 322CL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 5 323AL 323BL 325AL FITTINGS)  325BL 325CL 325DL  325EL 325FL 325GL  325HL 325JL 325KL  PEELABLE HOLE COVERS  R ZL-323-02-2 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI N 322AL 322BL 322CL  322DL 323CL 323DL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 5 325LL 325ML 325NL FITTINGS)  325PL 325QL 325RL  PEELABLE HOLE COVERS  R ZL-323-02-3 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI N 322AL 322BL 322CL  322EL 323DL 323EL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 5 325LL 325NL 325SL FITTINGS)  325TL 325UL 325VL  PEELABLE HOLE COVERS  ZL-323-03-1 N/A TASK DELETED MSI N SSI N 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 SSI 5 SSI 5 ZL-324-02-1 N/A TASK DELETED MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 ZL-324-02-1 * * * * * C O N T I N U E * * * * *  SSI N 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 325ML 325NL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 325PL 325QL 325RL  SSI 5 R ZL-325-02-3 325LL 325NL 325SL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI N 325TL 325UL 325VL  SSI 5 ZL-325-03-1 N/A TASK DELETED MSI N SSI N ZL-325-04-1 N/A TASK DELETED MSI N SSI N R ZL-326-01-1 326DL 326 RUDDER (EWIS) I: C MSI N (AREA OF BEARINGS 2, 3 AND 4) SSI N ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 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 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-326-02-3 325ML 325NL 325PL 326 RUDDE (EWIS) I: 4 C MSI N 325QL 325RL 326ML  326NL 326PL 326QL (AREA OF BEARINGS 1 TO 8) SSI N R ZL-326-02-4 325NL 325SL 325TL 326 RUDDER (EWIS) I: 4 C MSI N 325UL 325VL 326ML  326NL 326PL 326RL (AREA OF BEARINGS 1 TO 8) SSI N 326SL  R ZL-326-03-1 325AL 325BL 325DL 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI N 325FL 325HL 325KL FAR ASVISIBLE) (EWIS)  326AL 326BL 326BR SSI N 326CL 326DL 326DR  326EL 326FL 326FR  326GL 326HL 326HR  326JL 326KL 326KR  326LL  R ZL-326-03-2 325AL 325BL 325CL 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI N 325CR 325DL 325EL FAR AS VISIBLE) (EWIS)  325ER 325FL 325GL SSI N 325GR 325HL 325JL  325JR 325KL 326AT  326DL 326DR  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 R ZL-326-03-3 324CT 325LL 325LR 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI N 325ML 325MR 325NL FAR AS VISIBLE) (EWIS)  325NR 325PL 325PR SSI N 325QL 325QR 325RL  325RR 326AT 326ML  326NL 326PL 326QL  R ZL-326-03-4 324CT 325LL 325LR 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI N 325NL 325NR 325SL FAR AS VISIBLE)(EWIS)  325SR 325TL 325TR SSI N 325UL 325UR 325VL  325VR 326AT 326ML  326NL 326PL 326RL  326SL  ZL-326-04-1 N/A TASK DELETED MSI N SSI N ZL-326-05-1 N/A TASK DELETED MSI N SSI N ZL-326-06-1 N/A TASK DELETED MSI N SSI N ZL-326-07-1 N/A TASK DELETED MSI N SSI N ZL-326-08-1 N/A TASK DELETED MSI N SSI N 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 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 ZL-331-01-1 * * * * * C O N T I N U E * * * * *  341CT 341DT 341ET SSI 5 343AB 343AT SSI 5 R ZL-332-01-1 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-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-334-02-1 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-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 
A330 MRB REPORT – Zonal Section

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 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 STRUCTURE AS FAR AS VISIBLE) SSI N 335CB 335DB 335EB  335FB 344AB 344BB  344CB 344DB 344EB  344FB 344GB 345AB  345BB 345CB 345DB  345EB 345FB  * * * * * E N D * * * * *  ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300 
A330 MRB REPORT – Zonal Section

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 ZL-400-01-1 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI 7 SSI N ZL-400-01-2 N/A TASK DELETED MSI N SSI N ZL-411-01-1 N/A TASK DELETED MSI N SSI N ZL-411-02-1 N/A TASK DELETED MSI N SSI N R ZL-411-03-1 411AL 411AR 411BL 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI 3 421AL 421AR 421BL 421  SSI N R ZL-411-03-2 411AL 411AR 421AL 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI N 421AR 421  SSI N R ZL-411-04-1 411AL 411AR 411AZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI N 411BL 411BZ 411CZ 421  411DZ 411EZ 415AL SSI N 416AR 421AL 421AR  421AZ 421BL 421BZ  421CZ 421DZ 421EZ  425AL 426AR  ZL-412-01-1 N/A TASK DELETED MSI N SSI N ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 R ZL-412-02-1 415AL 416AR 417AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI N 418AR 425AL 426AR 422  427AL 428AR SSI N R ZL-412-02-2 415AL 415BL 416AR 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 7 416BR 425AL 425BL 422  426AR 426BR SSI N R ZL-412-02-3 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 7 426AR 422 MSI 7 SSI N ZL-413-01-1 N/A TASK DELETED MSI N SSI N R ZL-413-02-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI N 418AR 425AL 426AR 423  427AL 428AR SSI N R ZL-413-02-2 415AL 415BL 416AR 413 HOT SECTION (EWIS) I: C MSI N 416BR 417AL 418AR 423  425AL 425BL 426AR SSI N 426BR 427AL 428AR  R ZL-413-02-3 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI 7 418AR 425AL 426AR 423  427AL 428AR SSI N ZL-414-01-1 N/A TASK DELETED MSI N SSI N ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 R ZL-414-02-1 414AL 414AR 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI N 424  SSI N R ZL-414-02-2 415BL 416BR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI N 418AR 425BL 426BR 424  427AL 428AR SSI N R ZL-414-02-3 415AL 416AR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI N 418AR 425AL 426AR 424  427AL 428AR SSI N ZL-415-01-1 N/A TASK DELETED MSI N SSI N R ZL-415-02-1 415AL 415BL 416AR 415 FAN COWL (EWIS) I: 2 C MSI N 416BR 425AL 425BL 416  426AR 426BR 425 SSI 7 426 SSI 7 SSI 7 R ZL-415-02-2 415AL 415BL 415CL 415 FAN COWL (EWIS) I: 2 C MSI N 416AR 416BR 425AL 416  425BL 425CL 426AR 425 SSI 7 426BR 426 SSI 7 R ZL-415-02-3 415AL 415BL 415CL 415 FAN COWL (EWIS) I: 2 C MSI N 416AR 416BR 416CR 416  425AL 425BL 425CL 425 SSI 7 426AR 426BR 426CR 426 SSI 7 ZL-415-03-1 N/A TASK DELETED MSI N SSI N ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 ZL-417-01-1 N/A TASK DELETED MSI N SSI N R ZL-417-02-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 7 418AR 418BR 425AL 418  426AR 427AL 428AR 427 SSI 7 428BR 428 SSI 7 THRUST REVERSER  DEPLOYED  R ZL-417-02-2 415BL 416BR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 7 417DL 417EL 417FL 418 MSI 7 417GL 417HL 418AR 427  418BR 418CR 418FR 428 SSI 7 418GR 418HR 418JR SSI 7 425BL 426BR 427AL SSI 7 427DL 427EL 427FL  427GL 427HL 428AR  428BR 428CR 428FR  428GR 428HR 428JR  THRUST REVERSER  DEPLOYED  R ZL-417-02-3 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 7 417BL 417CL 417DL 418  417EL 417FL 417GL 427 SSI N 418AR 418BR 418CR 428  418DR 418ER 418FR  418GR 418HR 418JR  425AL 426AR 427AL  427BL 427CL 427DL  427EL 427FL 427GL  428AR 428BR 428CR  428DR 428ER 428FR  428GR 428HR 428JR  THRUST REVERSER  DEPLOYED  ZL-417-03-1 N/A TASK DELETED MSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 ZL-417-03-1 * * * * * C O N T I N U E * * * * *  SSI N ZL-451-01-1 N/A TASK DELETED MSI N SSI N R ZL-451-02-1 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI N 451CR 451DL 451DR 461  461BL 461BR 461CL SSI N 461CR 461DL 461DR  R ZL-451-02-2 451BL 451CL 451DL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI N 451DR 451EL 451ER 461  461BL 461CL 461DL SSI N 461DR 461EL 461ER  R ZL-451-02-3 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI N 451DL 451DR 451EL 461  451ER 461BL 461BR SSI N 461CL 461DL 461DR  461EL 461ER  ZL-451-03-1 N/A TASK DELETED MSI N SSI N R ZL-452-01-1 452AL 452BL 452BR 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI N 452CL 452CR 462AL 462  462BL 462BR 462CL SSI N 462CR  R ZL-453-01-1 453BL 453BR 453CL 453 LOWER PYLON (EWIS) I: 2 C MSI N 453CR 463BL 463BR 463  463CL 463CR SSI N ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 N ZL-453-01-2 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI N 453BR 453CL 453CR 463  463AL 463AR 463BL SSI N 463BR 463CL 463CR  ZL-454-01-1 N/A TASK DELETED MSI N SSI N ZL-454-02-1 N/A TASK DELETED MSI N SSI N R ZL-454-05-1 454BL 454BR 454CL 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 2 C MSI N 454CR 454DL 454FL 464  454GL 454HL 454JL SSI N 464BL 464BR 464CL  464CR 464DL 464FL  464GL 464HL 464JL  R ZL-454-05-2 454BL 454BR 454CL 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 2 C MSI N 454GL 454HL 454JL 464  454KL 454ML 454NR SSI N 464BL 464BR 464CL  464GL 464HL 464JL  464KL 464ML 464NR  R ZL-454-06-1 454AL 454BL 454BR 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 4 C MSI N 454CL 454CR 454DL 464  454DR 454EL 454ER SSI 5 454FL 454FR 454GL SSI 5 454GR 454HL 454HR SSI 5 454JL 464AL 464BL SSI 5 464BR 464CL 464CR SSI 5 464DL 464DR 464EL  464ER 464FL 464FR  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 ZL-454-06-1 * * * * * C O N T I N U E * * * * *  464GL 464GR 464HL  464HR 464JL  R ZL-454-06-2 454AL 454BL 454BR 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 4 C MSI N 454CL 454EL 454ER 464  454GL 454GR 454HL SSI 5 454HR 454JL 454KL SSI 5 454KR 454ML 454MR SSI 5 454NR 464AL 464BL SSI 5 464BR 464CL 464EL SSI 5 464ER 464GL 464GR  464HL 464HR 464JL  464KL 464KR 464ML  464MR 464NR  * * * * * E N D * * * * *  ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400 
A330 MRB REPORT – Zonal Section

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 R ZL-500-01-1 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 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 
A330 MRB REPORT – Zonal Section

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 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 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 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 
A330 MRB REPORT – Zonal Section

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 ZL-500-02-1 * * * * * 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 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-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 SSI 5 522RB 522TB 522UB  622AB 622AT 622BB  622BT 622CB 622CT  622EB 622HB 622JB  622LB 622NB 622QB  622RB 622TB 622UB  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  * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A330 MRB REPORT – Zonal Section

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 ZL-523-01-1 * * * * * C O N T I N U E * * * * *  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 (INCLUDING RAT ATTACHMENT POINTS, AS FAR AS VISIBLE) SSI N FLAPS EXTENDED 534  631  632  633  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 SSI 5 R ZL-535-01-1 535AB 535BB 635AB 535 WING TIP (EWIS) I: 4 C MSI N 635BB 635  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 SSI 5 R ZL-541-02-1 541AB 541AZ 541BB 541 INNER FUEL TANK (EWIS) I: 8 C MSI N 541BZ 541CB 541CZ 641  541DB 541DZ 541EB (AREA BETWEEN RIB 1 TO RIB 23). SSI 5 541EZ 541FB 541FZ SSI 5 541GB 541GZ 541HB SSI 5 541JB 541KB 541LB SSI 5 541MB 541NB 541PB SSI 5 541QB 541RB 541SB SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A330 MRB REPORT – Zonal Section

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 ZL-541-02-1 * * * * * C O N T I N U E * * * * *  641AB 641AZ 641BB SSI 5 641BZ 641CB 641CZ SSI 5 641DB 641DZ 641EB SSI 5 641EZ 641FB 641FZ SSI 5 641GB 641GZ 641HB SSI 5 641JB 641KB 641LB SSI 5 641MB 641NB 641PB SSI 5 641QB 641RB 641SB 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-542-01-1 542AB 542BB 542CB 542 OUTER FUEL TANK (EWIS) I: 8 C MSI N 542DB 542EB 542FB 642  542GB 542HB 542JB (RIB 23 TO RIB 33) SSI 5 542KB 560DB 642AB SSI 5 642BB 642CB 642DB SSI 5 642EB 642FB 642GB SSI 5 642HB 642JB 642KB SSI 5 660DB SSI 5 SSI 5 SSI 5 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 R ZL-571-01-1 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI N 671  SSI 5 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 WINGS SECTION: E-500 
A330 MRB REPORT – Zonal Section

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 ZL-571-01-1 * * * * * C O N T I N U E * * * * *  SSI 5 SSI 5 SSI 5 SSI 5 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-573-01-1 573CB 573DB 573GB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 673CB 673DB 673GB 673  FLAPS EXTENDED (RIB 6 TO RIB 12) SSI 5 SSI 5 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-575-01-1 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI N 575BT 575CB 575DB 675  675AB 675AT 675BB (RIB 27 TO RIB 39) SSI N 675BT 675CB 675DB  R ZL-591-01-1 575AB 575BB 591AB 591 INBOARD AILERON (EWIS) I: 2 C MSI N 591BB 591CB 591DB 691  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 
A330 MRB REPORT – Zonal Section

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 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 
A330 MRB REPORT – Zonal Section

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 ZL-700-01-1 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-715-01-1 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI N 716  SSI 5 R ZL-731-01-1 734 744 731 LH AND RH MAIN LANDING GEAR (EWIS) I: A MSI 3 741 MSI 3 SSI N R ZL-732-01-1 N/A 732 MAIN LANDING GEAR LEG DOOR (EWIS) I: A MSI N 742  SSI 5 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-734-01-1 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI N 744  SSI 5 SSI 5 * * * * * E N D * * * * *  ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700 
A330 MRB REPORT – Zonal Section

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 R 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 SSI 5 R ZL-811-01-1 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 5 SSI 5 R ZL-821-01-1 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 5 (INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 5 DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SSI 5 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 (INCLUDING DOOR HINGE ARMS AREA ATTACHMENT AREA) 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 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 * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
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 ZL-822-02-1 * * * * * C O N T I N U E * * * * *  152DR 152ER 152FR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) SSI N 152GR 152HR 152JR  152KR 152LR 822  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-823-02-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI N INSULATION  SSI N R ZL-831-01-1 831 841 831 FWD PASSENGER/CREW DOOR (EWIS) I: C MSI 5 841  (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 DOOR (EWIS) I: C MSI 5 842  (INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SSI N SCUFF PLATES)  ISSUE: JUL 01/10 DOORS SECTION: E-800 
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 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 DOOR (EWIS) I: C MSI 5 843  (INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SSI N SCUFF PLATES)  R ZL-833-02-1 833 833AZ 833BZ 833 AFT PASSENGER/CREW DOOR (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 EXITS (EWIS) I: C MSI 5 844  (INCLUDING DOOR STOPS ON FUSELAGE SIDE ,DOOR SEALS SSI N AND SCUFF PLATES)  R ZL-834-02-1 834 834AZ 834BZ 834 EMERGENCY EXIT (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-834-03-1 834 834KZ 834LZ 834 EMERGENCY EXIT (EWIS) I: 8 C MSI N 834MZ 834NZ 834PZ 844  834QZ 844 844KZ SSI N * * * * * C O N T I N U E D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
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 ZL-834-03-1 * * * * * C O N T I N U E * * * * *  844LZ 844MZ 844NZ  844PZ 844QZ  INSULATION  N ZL-835-01-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 800 FH MSI 5 OR MSI 5 (INCLUDING DOOR SEALS, DOOR FRAMES AND FITTING AREA 6 MO MSI 5 AT FUSELAGE AND VISIBLE PART OF DOOR SILL)  SSI N N ZL-835-02-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 72 MO MSI N LINING AND DADO  LINER SSI N N ZL-835-03-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 144 MO MSI N LINING AND DADO  LINER, INSULATION SSI N * * * * * E N D * * * * *  ISSUE: JUL 01/10 DOORS SECTION: E-800 
A330 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 A330 

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

Inspection Intervals 

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. 
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. 9 12 MO A330 

 

 34-70-00 Aircraft Environment Surveillance System 

 

2. FNC Functional Check of the Air Traffic 

 Control Transponder System per 

 14 CFR Part 91.413. 9 24 MO A330 

 78-31-00 Thrust Reverser Control Activation System 

7831006 FNC Holding Torque Check of the Thrust 

 Reverser Electro - Mechanical Brake, 9 3000 FC GE CF6-80E1 

SECTION D

 None applicable at this time 

SECTION E

 None applicable at this time 
A330 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

A330 Certification Maintenance Requirements (CMRs) 

Appendix 1b

A330 Airworthiness Limitation Items - (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. 
A330 MRB REPORT 

Issue : July 2010 Page : APX 1.2 

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A330 MRB REPORT 

Issue : July 2010 Page : APX 2. 1

APPENDIX 2

ZONE DIAGRAMS

1. The A330 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 A330 Maintenance Planning Document (MPD) - 

Section 10 and the Aircraft Maintenance Manual (AMM) - Chapter 06. 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

A330 MRB REPORT 

Issue : July 2010  100 LOWER HALF OF FUSELAGE 

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

 FR0 - STA6382 TO FR80/82 - STA55287,3 

 200 UPPER HALF OF FUSELAGE 

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

 FR1 - STA7662  TO FR80/82 - STA55287,3 

 300 STABILIZER AND FUSELAGE REAR 

SECTION FROM REAR OF AFT PRESSURE BULKHEAD 

 FR80/82 - STA55287,3  TO FR106 - STA63894,3  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 

A330-200 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

A330 MRB REPORT 

Issue : July 2010  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

A330-300 
A330 MRB REPORT 

Issue : July 2010 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010  110 RADOME (NOSE CONE TO FR 1) 

 - STA 6382,5 TO - STA7662,5 

 120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

 FR1 - STA7662,5  TO FR20 - STA144585 

 130 LOWER DECK FORWARD CARGO 

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

 FR20 - STA14458,5  TO FR40 - STA27708,5 

 140 WING CENTER BOX, AIR COND, 

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

 FR40 - STA27708,5  TO FR53,2 - STA36737,3 

 150 LOWER DECK AFT CARGO 

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

 FR53,2 - STA36737,3  TO BETWEEN FR65 - STA46807,3  AND FR66 - STA47337,3 

 160 LOWER DECK BULK CARGO 

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

 BETWEEN FR 65 - STA47337,3  AND FR66 - STA47337,3  TO FR73 - STA51047,3 

 170 AFT CABIN UNDERFLOOR 

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

 FR73 - STA51047,3  TO FR80/82 - STA55287,3 

 190 BELLY FAIRING; AIR 

CONDITIONING COMPARTMENT, HYDRAULIC COMPARTMENT 

BETWEEN FR37,2 - STA23468,5  AND FR37,3 - STA23998,5  TO FR56 - STA42037,3 

 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 

 230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5  TO FR31 - STA19228,5 

 240 MID CABIN UTILITY AREA AFT OF 

FORWARD CABIN TO FRONT OF MID CABIN 

 FR31 - STA19228,5  TO FR36 - STA21878,5 

 250 MID CABIN AFT OF MID CABIN 

UTILITY AREA TO FRONT OF AFT CABIN 

 FR36 - STA21878,5  TO FR53,5 - STA38327,3 

 260 AFT CABIN AFT OF MID CABIN TO 

FRONT OF AFT CABIN UTILITY AREA 

 FR53,5 - STA38327,3  TO FR72 - STA50517,3 

 270 AFT CABIN UTILITY AREA AFT OF 

AFT CABIN TO FRONT OF AFT PRESSURE BULKHEAD 

 FR72 - STA50517,3  TO FR80/82 - STA55287,5 

 310 FUSELAGE REAR SECTION AFT OF 

AFT PRESSURE BULKHEAD 

 FR80/82 - STA55287,5  TO FR106 - STA63894,5 

 320 VERT

RUDD

 330 TRIMM

STABELEVA

 340 TRIMM

STABELEVA

 710 NOSE  730 L MAI

DOOR

 740 R MAI

DOOR

 810 FORW

COMP

 820 CARG 830 L PAS

EMER

 840 R PAS

EMER

A330-200 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010  110 RADOME (NOSE CONE TO FR 1) 

 - STA 6382,5 TO - STA7662,5 

 120 AVIONICS COMPARTMENT : 

FORWARD PRESSURE BULKHEAD TO AFT PARTITION OF AVIONICS COMPARTMENT 

 FR1 - STA7662,5  TO FR20 - STA144585 

 130 LOWER DECK FORWARD CARGO 

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

 FR20 - STA14458,5  TO FR40 - STA30381,1 

 140 WING CENTER BOX, AIR COND, 

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

 FR40 - STA30381,1  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 FR 65 - STA52134,5  AND FR66 - STA52664,5  TO FR73 - STA56374,5 

 170 AFT CABIN UNDERFLOOR 

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

 FR73 - STA56374,5  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 

 230 FORWARD CABIN AFT OF 

FORWARD CABIN UTILITY AREA TO FRONT OF MID CABIN 

FR17 - STA13153,5  TO FR31 - STA22408, 

 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 VERT

RUDD

 330 TRIMM

STABELEVA

 340 TRIMM

STABELEVA

 710 NOSE  730 L MAI

DOOR

 740 R MAI

DOOR

 810 FORW

COMP

 820 CARG 830 L PAS

EMER

 840 R PAS EMER

A330-300 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

DESCRIPTION/BOUNDARIES

A330 MRB REPORT 

Issue : July 2010  410 ENGINE 1 (LEFT ENGINE), ENGINE 

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

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

TIP 

 540 FUEL TANK 

RIB 1 - 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 

 420 ENGINE 2 (RIGHT ENGINE) ENGINE 

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

 460 ENGINE 2 PYLON  610 SLATS  620 FIXED LEADING EDGE  630 FLAP TRACK FAIRINGS AND WING  640 FUEL TANK 

RIG1 - 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 AND SPOILERS  690 AFT OUTBOARD SECTION OF 

TRAILING EDGE 
A330 MRB REPORT 

Issue : July 2010 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010 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 - STA14448,5  TO FR39,1 - STA26118,5  AND FR39,2 - STA26648,5 

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 - STA26118,5  AND FR39,2 - STA26648,5 

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 --STA26118,5  AND FR39,2 STA26648,5  TO FR39 - STA25588,5  AND FR40 - STA27708,5 

141/142 WING CENTER BOX 

 FR40 - STA27708,5  AND FR47 - STA32478,5 

 143 AREA BETWEEN KEEL BEAMS 

UNDER WING CENTER BOX TO BOTTOM FUSELAGE BETWEEN 

 FR44 AND FR45 - STA30888,5  TO FR49 - STA33543,2 

145/146 PRESSURIZED ZONE BETWEEN 

WING CENTER BOX; MAIN GEAR WELL AND CABIN FLOOR 

 FR40 - STA27708,5  TO FR53,2 - STA36737,3 

147/148 MAIN GEAR WELL AND HYDRAULIC 

COMPARTMENT 

 FR47 - -STA32478,  TO FR53,2 - STA36737,3 

 149 CENTERLINE BAY BETWEEN KEEL 

BEAMS UNDER ZONE 143 BETWEEN 

 FR44 AND FR45 - STA30888,5  TO FR49 - STA33543,2  AND BETWEEN KEEL BEAMS  FR49 - STA33543,2  TO FR53,2 - STA36737,3 

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 L/R IN CYLINDRICAL SECTION) 

 FR53,2 - STA36737,3  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 - STA46807,3  AND FR66 - STA47337,3 

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 - STA46807,3  AND FR66 - STA47337,3  TO FR73 - STA51047,3 

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 - STA46807,3  AND FR66 - STA47337,3  TO FR73 - STA51047,3 

171/172 AFT CA

COMPASIDE OFLOOR (STR26 

 FR7 TO FR8

 191 DRY BA

BETWESTA23AND FR

 192 AIR CO

COMPABETWESTA22

AND FR

 193 AIR CO

COMPA

 FR40  BETWE

STA314

195/196 HYDRA

FAIRINFR45 SSTA324

197/198 REAR 

 FR5 TO FR5

A330-200 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010 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 - STA19228,5 

233/234 FORWARD CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

 FR17 - STA13153,5  TO FR31 - STA19228,5 

241/242 MID CABIN UTILITY AREA : FROM 

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

 FR31 - STA19228,5  TO FR36 - STA21878,5 

243/244 MID CABIN UTILITY AREA : 

OVERHEAD COMPARTMENT FROM CROWN CENTER LINE TO STR15 L/R 

 FR31 - STA19228,5  TO FR36 - STA21878,5 

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

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

 FR36 - STA21878,5  TO FR53,5 - STA38327,3 

253/254 MID CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

 FR36 - STA21878,5  TO FR53,5 - STA38327,3 

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

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

 FR53,5 - STA38327,3  TO FR72 - STA50517,3 

263/264 AFT CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

 FR53,5 - STA38327,3  TO FR72 - STA50517,3 

271/272 AFT CABIN UTILITY AREA : FROM 

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

 FR72 - STA50517,3  TO FR80 - STA55287,3 

273/274 AFT CABIN UTILITY AREA 

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

 FR72 - STA50517,3  TO FR80 - STA55287,3 

311/312 REAR 

 FR8 TO BET

313/314 TAIL C

 BETWE TO FR9

315/316 TAIL C

COMPT 

 FR9 TO FR1

 317 TAIL C

 FR1 TO FR1

 321 DORSA 322 VERTIC

EDGE 

 323 VERTIC 324 VERTIC 325 VERTIC

EDGE 

 326 RUDDE

A330-200 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010 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 - STA14448,5  TO FR39,1 - STA29312,1  AND FR39,5 - 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 FR39,2 - 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 FR39 - STA28782,1  AND FR40 - STA30372,1 

141/142 WING CENTER BOX 

 FR40 - STA30372,1  AND FR47 - STA35672,1 

 143 AREA BETWEEN KEEL BEAMS 

UNDER WING CENTER BOX TO BOTTOM FUSELAGE BETWEEN 

 FR44 AND FR45 - STA 34176,2  TO FR49 - STA36736,8 

145/146 PRESSURIZED ZONE BETWEEN 

WING CENTER BOX; MAIN GEAR WELL AND CABIN FLOOR 

 FR40 - STA30372,1  TO FR53,2 - STA39930,9 

147/148 MAIN GEAR WELL AND HYDRAULIC 

COMPARTMENT 

 FR47 - STA35672,1  TO FR53,2 - STA39930,9 

 149 CENTERLINE BAY BETWEEN KEEL 

BEAMS UNDER ZONE 143 BETWEEN 

 FR44 AND FR45 - STA34176,2  TO FR49 - STA36736,8  AND BETWEEN KEEL BEAMS  FR49 - STA36136,8  TO FR53,2 - STA39930,9 

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 L/R 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 CA

COMPASIDE OFLOOR (STR26 

 FR7 TO FR8

 190 DRY BA

BETWESTA23AND FR

 192 AIR CO

COMPA

BETWESTA23AND FR

 193 AIR CO

COMPA

  BETWE

STA32

195/196 HYDRA

FAIRINFR45 SSTA33

197/198 REAR 

 FR5 TO FR5

A330-300 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

A330 MRB REPORT 

Issue : July 2010 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) 

 FR36 - STA25056,5  TO FR53,5 - STA41520,9 

253/254 MID CABIN OVERHEAD 

COMPARTMENT : FROM CROWN CENTER LINE TO STR15 L/R 

 FR36 - STA25058,5  TO FR53,5 - STA41520,9 

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

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

 FR53,5 - STA41520,9  TO FR72 - STA55844,5 

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 

 FR8 TO BET

313/314 TAIL C

 BETWE TO FR9

315/316 TAIL C

COMPT 

 FR9 TO FR1

 317 TAIL C

 FR1 TO FR1

 321 DORSA 322 VERTIC

EDGE 

 323 VERTIC 324 VERTIC 325 VERTIC

EDGE 

 326 RUDDE

A330-300 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

DESCRIPTION/BOUNDARIES

A330 MRB REPORT 

Issue : July 2010  319 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 

 RIB 19 TO RIB 21  HORIZONTAL TAIL (RH)

 341 TRIMMABLE HORIZONTAL 

STABILIZER LEADING EDGE 

 342 TRIMMABLE HORIZONTAL 

STABILIZER TIP 

 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 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

DESCRIPTION/BOUNDARIES

A330 MRB REPORT 

Issue : July 2010  ENGINE 1

 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 

 ENGINE 2

 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 
A330 MRB REPORT 

Issue : July 2010 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DESCRIPTION/BOUNDARIES

A330 MRB REPORT 

Issue : July 2010  511 SLAT 1  512 SLAT 2  513 SLAT 3  514 SLAT 4  515 SLAT 5  516 SLAT 5  517 SLAT 7  521 INBOARD FIXED LEADING EDGE 

STRUCTURE 

 RIB1 - STA0  TO RIB9 - STA5676 

 522 CENTER FIXED LEADING EDGE 

STRUCTURE 

 RIB9 - STA5686  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 

 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
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DESCRIPTION/BOUNDARIES

A330 MRB REPORT 

Issue : July 2010  611 SLAT 1  612 SLAT 2  613 SLAT 3  614 SLAT 4  615 SLAT 5  616 SLAT 5  617 SLAT 7  621 INBOARD FIXED LEADING EDGE 

STRUCTURE 

 RIB1 - 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 

 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 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 
MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

A330 MRB REPORT 

Issue : July 2010  NOSE LANDING GEAR

 711 NOSE GEAR  712 LEG DOOR 713/714 MAIN DOORS 715/716 AFT DOORS  MAIN LANDING GEAR (LH)

 731 L MAIN GEAR  732 CYLINDER DOOR  733 SECONDARY DOOR  734 MAIN DOOR  MAIN LANDING GEAR (RH)

 741 R MAIN GEAR  742 CYLINDER DOOR  743 SECONDARY DOOR  744 MAIN DOOR 
A330 MRB REPORT 

Issue : July 2010 

MAJOR 

ZONES

DESCRIPTION/BOUNDARIES 

MAJOR 

ZONES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES

MAJOR

ZONES

DESCRIPTION/BOUNDARIES DE

 811 FORWARD AVIONICS 

COMPARTMENT DOOR FR7 AND FR8 TO FR9 AND FR10 

 821 LOWER DECK FORWARD CARGO 

COMPARTMENT DOOR BETWEEN FR20A AND FR25A 

 822 LOWER DECK AFT CARGO 

COMPARTMENT DOOR BETWEEN FR59A AND FR65 

 823 LOWER DECK BULK CARGO 

COMPARTMENT DOOR BETWEEN FR67 AND FR69 

 831 L FWD PASSENGER/CREW DOOR 

BETWEEN FR14B AND FR16B 

 832 L MID PASSENGER/CREW DOOR 

BETWEEN FR33 TO FR35A 

 833 L AFT PASSENGER/CREW DOOR 

BETWEEN FR73A AND FR75A 

 834 L EMERGENCY EXIT BETWEEN 

FR53,5 TO FR53,7 AND FR53,8 

 836 MAIN DECK CARGO 

COMPARTMENT DOOR FR59 TO FR66 (OPTION MOD 40051) 

 841 R FWD PASSENGER/CREW DOOR 

BETWEEN FR14B AND FR16A 

 842 R MID PASSENGER/CREW DOOR 

BETW

 843 R AF

BETW

 844 R EM

FR53
Issue : July 2010 

A330-200F 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 
Issue : July 2010 

This page intentionally left blank
A330 MRB REPORT 

Issue : July 2010 Page : APX 3. 1

APPENDIX 3

ETOPS MAINTENANCE STANDARDS

 DELETED 

ETOPS Maintenance Standards identified during the Type Certification process were originally listed in the 

MRB Report Appendix 3. These Standards included ETOPS related tasks (which are also included in MRB 

Report Section C) and ETOPS specific tasks/intervals (which are included in the ETOPS CMP document 

but not in MRB Report Section C). In 2002 revision, the Appendix 3 was deleted in the MRBR revision 7 

since it no longer provided complete information necessary for maintenance program development. 

Operators should note that the ETOPS CMP, reference AI/EA5000, is the authoritative document for 

mandatory ETOPS Maintenance Standards. This includes ETOPS Maintenance Standards identified by inservice experience in addition to those originally quoted in Appendix 3. 
A330 MRB REPORT 

Issue : July 2010 Page : APX 3. 2

This page intentionally left blank 
A330 MRB REPORT 

Issue : July 2010 Page : APX 4.1

APPENDIX 4

SSI's WITHOUT REQUIREMENTS

DELETED 

Appendix 4 deleted in MRB Report Rev 7 following ISC/MWG decision that information was of no practical 

value. 
A330 MRB REPORT 

Issue : July 2010 Page : APX 4.2

This page intentionally left blank 

This page intentionally left blank
A330 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 Oct 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 Dec 97 

J. PHIPPS Jan 98 to end 99
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.2

A330/A340 MAINTENANCE REVIEW BOARD (2000 onwards) 

EASA MEMBERS 

F. JOUVARD DGAC/EASA (Chairperson) Mar 02 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 

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) 

D. HUSSENOT AFR Apr 93 to Dec 94 (1) 

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 Jun 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) 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.3

J. MERCKX SAB Jan 92 to Apr 93 (2) 

M. PEREIRA TAP Feb 90 to Sep 92 (7) 

C. LEITAO TAP Dec 92 to Dec 94 (5) 

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 (7) 

A. LUJIN TWA Feb 90 to Dec 94 (12) 

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 Dec 94 (6) 

P. MANLEY BAe Jun 91 to Dec 94 (11) 

P. WEYH DA Feb 90 to Dec 94 (17) 

A330/A340 INDUSTRY STEERING COMMITTEE (1995 to 1999) 

A. MARCOUT ITF (Chairman) Sep 95 to Oct 96 

R. RODRIGUEZ AFR (Chairman) Fev 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 

D. 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 Dec 97 

J. RIDDERBEEK 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. WIDEMER 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.4

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 

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 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 Jun 06 

B. HOVINE AFR Jan 00 to Mar 01 

P. GROSEILLE AFR Mar 01 to Dec 02 

J.F DERU AFR Dec 02 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. Mc ALLISTER BMI Nov 04 onwards 

B. DYSON CPA Jan 00 to Jun 00 

M. HOLDEN CPA Jun 00 to Dec 02 

M. KANAGASABI CPA Dec 02 onwards 

W. SCHOLZ DLH Jan 00 to Dec 02 

W. REICHER DLH Dec 02 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.5

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 

. 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 03 

M. BLUESTONE QFA May 03 to Sep 05 

D. SPIRITOSANTO QFA Sep 05 onwards 

G. VAN HUMBEECK SAB Jan 00 to Dec 02 

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 onwards 

V.M. SANTOS TAP Jan 00 to Mar 01 

F. MOREIRA TAP Mar 01 onwards 

E. BAYIR THY Jan 00 to Nov 04 

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 

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.6

J.C. BOISSEAU ITF 

J.B. GARCIA ITF 

G. MACARY 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 

SURACHAI P. THA 

P. BERGER UTA 

F. JOUAN UTA 

Y. MELISSE UTA 

N. KONZALI 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 

D. ANCEL ITF 

R. LILLY NWA 

T. CARLSON NWA 

J. DAVIS NWA 

J. ANDRE SAB 

P. HENDRIX SAB 

J. KIRSCHFINK SAB 

R. STAUBAUT SAB 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.7

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 

F. DEMARTY 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. KUHN DA 

U. LASZIG DA 

C. MACPHERSON DA 

M. MOLL DA 

P. OBERSCHELP-MÜLLER DA 

E. PODIEN DA 

T. ROEYER DA 

O. SCHOLZ 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.8

CHATTAWANICH K. THA 

TUMPRAYOTH C. THA 

B. HOLMES TWA 

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 

K. MILLER FAA 

Sub-group ATA 49 

G. MACARY ITF 

M. LINNEMANN DLH 

A. SCHEFFER NWA 

J. VIEGAS TAP 

YUTHASIT SUWANLOY THA 

J. LIGHTLY TWA 

D. TAMZALI UTA 

H. HOFFMANN DA 

K.P. SELLMANN DA 

B. SHALK GARRETT 

K. ANDERSON GARRETT 

MRB ADVISORS 

P. VAQUEZ BV (JAA) 

H. PRUIS RLD (JAA) 

K. MILLER FAA 

Sub-group powerplant ATA 71 to 80 (GE) 

R. TILNEY COA 

D. JAMAUX ITF 

D. ROYER ITF 

G. MACARY ITF 

D. ANCEL ITF 

C. HARDY ITF 

C. TACHDJIAN ITF 

C. DELMAS AS 

P. ESPINOSA AS 

P. REED GE 

T. ENDER PALMER ROHR 

R.B. SMITH ROHR 

MRB ADVISORS 

P. VAQUEZ BV (JAA) 

H. PRUIS RLD (JAA) 

J. HARRINGTON FAA 

Sub-group powerplant ATA 71-80 (PW) 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.9

ALFI AHMAD MAS 

GHAZALI MD ISA MAS 

YUTHASIT SUWANLOY THA 

D. TUTTLE PW 

C. DELMAS AS 

J.F HUIX AS 

MRB ADVISORS 

P. VAQUEZ BV (JAA) 

H. PRUIS RLD (JAA) 

R. MORRILL FAA 

Sub-group powerplant ATA 71-80 (RR) 

P. BARWELL CPA 

K. LOH CPA 

KINAN ARINAN GIA 

AZWIR BUAT GIA 

A. MOWREY TWA 

B. BROWN RR 

S. FURNESS RR 

C. DELMAS AS 

J.F HUIX AS 

MRB ADVISORS 

P. VAQUEZ BV (JAA) 

H. PRUIS RLD (JAA) 

K. MILLER FAA (1st & 3rd mtg) 

R. MORRILL FAA (2nd mtg) 

MAINTENANCE WORKING GROUP No.4 (until 1999)

(Systems 22, 23, 24, 26, 31, 33, 34, 45) 

M. ERAN-TASKER AIB (Chairman to DEC 92) 

S. THOMAS AIB (Chairman from JAN 93) 

C. GLASHAGEN DLH 

A. NESSEL DLH 

G. ALCOL IBE 

A. GORDO IBE 

G. BOUSSAC ITF 

D. LE BON ITF 

J. MARCHEBOUT ITF 

D. ROYER ITF 

P. DARRACQ 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.10

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 

MAINTENANCE WORKING GROUP No.5 (until 1997)

(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 

Y.S. LEE KAL 

M. HILLBORN NWA 

A. BRANCO TAP 

A. FERREIRA TAP 

MARAYAT J. THA 

PAITOON M. THA 

MAHAPHRAM P. 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)
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.11

(Zonal) 

G. ADLER DA Chairman 

H. OYAMA 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 

MRB ADVISORS 

S. LAGNEL BV (JAA) 

S. LEEPER FAA 

A330-200 (Systems) MWG - Sept 97 

T. HARBOTTLE AIB (Chairman) 

D.W. JEON KAL 

H. SCHNEIDER LHT 

J. RIDDERBECK LTU 

J. LEWIS MON 

R. WIDMER SRT 

G. HILLS BAe 

M. WOODS BAe 

M. POSTAL AS 

A. ERDINC 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.12

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) 

A340-500/600 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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.13

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)) 

T. ROEGER AIB Chairman 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.14

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 

B. GABLER AUA 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.15

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.16

MRB ADVISORS

N. CLOUT GSAC (JAA) 

F. LEBLOND GSAC (JAA) 

D. LAMOTHE GSAC (JAA) 

D. STRICKLAND FAA 

ISC ADVISOR

C. MAC P ̈HERSON 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 

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) 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.17

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 

F. DELGADO Airbus Spain 

F. CERVANTES Airbus Spain 

R. ARROYO 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
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.18

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.19

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

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.20

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.21

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.22

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 

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 

Zonal Maintenance Working Group 2009.1 February 2009 (A330-200F)

Mustafa EREN Airbus Chairman 

Ali ZENGIN MNG Airlines 

Carsten MARKS Lufthansa Technik 

Joanne BRAGANZE Lufthansa Technik 

Walter PRESS Lufthansa Technik 

Bilal DEMIC Turkish Airlines 

John W. HAMILTON Thomas Cook 

Jose Antonio HUERTAS-DIEZ Airbus 

Frans-Hidayat PRIYATNA Airbus 

Jacqueline SAULNIER Airbus 

Anthony MONTILLA Airbus 

Melih DEMIR Airbus 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.23

Lorenz WENK Airbus 

Frank JAEHN Airbus 

Anja HERTERICH Airbus 

MRB Advisor

Malcolm, EUSTICE CAA 

Roy, PATZKE FAA 

ISC Advisor

None 

Zonal Maintenance Working Group 2009.2 May 2009 (A330-200F)

Mustafa EREN Airbus Chairman 

Frank JAEHN On behalf of MWG Zonal Chair

Joanne BRAGANZE Lufthansa Technik 

Murat GÖKDEMIR Turkish Airlines 

John W. HAMILTON Thomas Cook 

Jose Antonio HUERTAS-DIEZ Airbus 

Frans-Hidayat PRIYATNA Airbus 

Jacqueline SAULNIER Airbus 

Anthony MONTILLA Airbus 

Melih DEMIR Airbus 

Lorenz WENK Airbus 

Frank JAEHN Airbus 

Oliver WEISS Airbus 

MRB Advisor

Malcolm, EUSTICE CAA 

Roy, PATZKE FAA 

ISC Advisor

None 

Zonal Maintenance Working Group 2009.3 August 2009 (A330-200F)

Mustafa EREN Airbus Chairman 

Guenter POST On behalf of MWG Zonal Chair

John W. HAMILTON Thomas Cook 

Ali ZENGIN MNG Airlines 

Musa GÖNÜLTAS MNG Airlines 

Yavuz ATES MNG Airlines 

Annika SPALLEK Lufthansa Technik 

Joanne BRAGANZE Lufthansa Technik 

Li ZHIYONG Air China 

Yin MIAO Air China 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.24

Bilal DEMIC Turkish Airlines 

Murat GÖKDEMIR Turkish Airlines 

Tülay BÖTKLÜ Turkish Airlines 

John W. HAMILTON Thomas Cook 

Erdem GÜNDÜZ Izmir Airlines 

Jose Antonio HUERTAS-DIEZ Airbus 

Anthony MONTILLA Airbus 

Melih DEMIR Airbus 

Lorenz WENK Airbus 

MRB Advisor

Thomas, BADIA EASA

Roy, PATZKE FAA 

ISC Advisor

None 

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)
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.25

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 

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
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.26

None

MRB ADVISOR 

Boualem BACHA DGAC 

Richard E. JONES FAA 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.27

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.28

ISC ADVISOR

None

MRB ADVISOR 

Ralf Schneider LBA 

Ronald J. Gleiter FAA 

Laurent PINSARD EASA (STG Advisor) 

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)
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.29

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.30

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 

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 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.31

POWERPLANT AND APU MAINTENANCE WORKING GROUP (APRIL 2007)

J. NICOLAS Airbus Central Entity Chairperson 

Eric WOON SEK LAW AIR MAURITIUS 

Martyn HORSTINK KLM 

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 

Mike Fabritz Honeywell 

Richard BARKLEY Rolls-Royce 

Brian Ives PW 

Douglas Stevenson General Electric 

Gary SANDERS Hamilton Sundstrand 

Amine TAOURCHI Airbus Central Entity 

Jean-Francois HUIX Airbus Central Entity 

Raquel SANCHEZ-GARCIA Airbus Central Entity 

Vincent FONDEVIOLE Airbus Central Entity 

Fabien VILLARD Airbus Central Entity 

Alexandre LENINGER Airbus Central Entity 

Frederic LAIR Airbus Central Entity 

Jean-Guy Galier Airbus Central Entity 

Julien Baptiste Airbus Central Entity 

David SANZ-MERINO Airbus Spain 

MRB advisors

Boualem BACHA EASA 

Donald LEVESQUE FAA 
A330 MRB REPORT 

Issue : July 2010 Page : APX 5.32

This page intentionally left blank
A330 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 procedure. 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. 
A330 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. 
A330 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. 
A330 MRB REPORT 

Issue : July 2010 Page : APX 6. 4

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. 

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. 
A330 MRB REPORT 

Issue : July 2010 Page : APX 7. 1

APPENDIX 7

ABBREVIATIONS USED IN THE MRB REPORT

A/C aircraft 

AC alternating current 

ACARS Aircraft Communications Addressing & Reporting System 

ACMS Aircraft Condition Monitoring System 

ACP Audio Control Panel 

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 

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 

ATIMS Air Traffic and Information Management System 

A/THR autothrust 

ATT attitude 

BAT Battery 

BAC Bulk Avionics Compartment 

BCRC Bulk Crew Rest Compartment 

BITE Built In Test Equipment 

CBB Connexion By Boeing 

CDU Center Drive Unit 

CPCP Corrosion Prevention and Control Program 

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 

DEU Decoder/Encoder Unit 

DI Detailed Inspection 

DFDR Digital Flight Data Recorder 

DMC Display Management Computer 

DME Distance Measuring Equipment 

DS discard 

DY Days 

EASA European Aviation Safety Agency 
A330 MRB REPORT 

Issue : July 2010 Page : APX 7. 2

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 Locator 

EPSU Emergency Power Supply Unit 

ESM Engine Shop Manual 

ESS essential 

EVAC evacuation 

EWIS Electrical Wiring Interconnection System 

FAA Federal Aviation Administration 

FADEC Full Authority Digital Engine Control 

FANS Future Air Navigation System 

FC flight cycles 

FC functional check 

FCC FWD Cargo Compartment 

FCD Fan Cowl Door 

FCRC Flight Crew Rest Compartment 

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 

GCU Generator Control Unit 

GPWC Ground Proximity Warning Computer 

GPWS Ground Proximity Warning System 

GVI General Visual Inspection 

HDG heading 

HF high frequency 

HIRF High Intensity Radiated Fields 

HP high pressure 

HPT High Pressure Turbine 

HRS hours (elapsed time) 

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 Aviation Authorities 

JAR Joint Aviation Requirement 
A330 MRB REPORT 

Issue : July 2010 Page : APX 7. 3

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 

MCDU Multi Control Display Unit 

MDCC Main Deck Cargo Compartment 

MLG Main Landing Gear 

MO Months 

MORV Mixer Overpressure Relief Valve 

MPD Maintenance Planning Document 

MRB Maintenance Review Board 

MSI Maintenance Significant Item 

MSN Manufacturers Serial Number 

N/A not applicable 

ND Navigation Display 

NLG Nose Landing Gear 

NR national requirement 

NT Note 

NTM Non-Destructive Testing Manual 

OP operational 

QAR Quick Access RecorderPA Public Address 

P/B SW pushbutton switch 

PCU Power Control Unit 

PDU Power Drive Unit 

PFD Primary Flight Display 

POB Pressure-OFF Brake 

PTLU Pedal Travel Limitation Unit 

PTT press to test 

PUA Air Pressurisation Unit 

RAT Ram Air Turbine 

RCC Remote Control Centre 

RCT Rear Center Tank 

RH right hand 

RMP Radio Management Panel 

RS restoration 

RSVR reservoir 

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 

STR stringer 

SV servicing 
A330 MRB REPORT 

Issue : July 2010 Page : APX 7. 4

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 

ZIP Zonal Inspection Program
This page intentionally left blank 
A330 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 Manager 

 1 Rond Point Maurice Bellonte 

 31707 BLAGNAC CEDEX 

 FRANCE 
A330 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 :
A330 MRB REPORT 

Issue : July 2010 Page : APX9. 1

APPENDIX 9

HIRF/LIGHTNING PROTECTION 

1 Background

During development of the initial A330 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 A330 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 

- individual shielding for engine cables (nacelle, pylon,wing) 

c) equipment protection 
A330 MRB REPORT 

Issue : July 2010 Page : APX9. 2

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 

(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. 

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. 
A330 MRB REPORT 

Issue : July 2010 Page : APX9. 3

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 must 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 resistance 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. 

Details of the A330/A340 HIRF/Lightning Assurance Plan are given in document 524.5012-01 

prepared by Airbus dept EYDVB. 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

R 20- 00- 01- 1 522 

622 

522AB 522BB 454BL 622AB 622BB 464BL 

4C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

Security check of the following harnesses end fittings, from ri10A : - 7021VP, 7001VC- A, 7021VC- A, 7025VC- A, 10HA1, LH si

- 7024VP, 7002VC- A, 7022VC- A, 7026VC- A, 10HA2, RH s

 20- 00- 01- 2 TASK RESERVED 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 

623NB 675DB 635AB 

C WING ELECTRICAL WIRING PROTECTION ELEMENTS

GVI of elements fitted on the following harnesses end fittings wing tip to rib 39: - 7621VB, 7623VB, 7625VB, 7627VB, LH side - 7622VB, 7624VB, 7626VB, 7628VB, RH side 

 20- 00- 01- 5 533 

633 

533AB 533CB 574CB 574DB 574EB 574FB 633AB 633CB 674CB 674DB 674EB 674FB Flaps extended 

2C WING ELECTRICAL WIRING PROTECTION ELEMENTS 

GVI of elements fitted on the following harnesses end fittingsrib19 to rib 14 : - 7633VB LH side - 7634VB RH side 

 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 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 7 TASK RESERVED  20- 00- 01- 8 571/671 N/A 2C WING ELECTRICAL WIRING PROTECTION ELEMENTS

GVI of the following braided conduit end fittings, from rib 6 to - 112QA1-A, 121QA1-A, 122QA1-A, LH side - 112QA2-A, 121QA2-A, 122QA2-A, RH side 

 20- 00- 01- 9 531 

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 : - 7652VB, 7646VB, 7634VB, RH side - 7651VB, 7645VB, 7633VB, LH side 

 20- 00- 01- 10 TASK RESERVED 20- 00- 01- 11 TASK RESERVED 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 01- 12 TASK RESERVED  20- 00- 01- 13 TASK RESERVED  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, 35033505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 37443721VP, 3735VP, 3737VP, 3743VP

 20- 00- 01- 15 TASK RESERVED 20- 00- 02- 1 311 

312 

312AR 2C SECTION 19 BRAIDED CONDUIT

Security check of the following harnesses end fittings at Fr. 8- 1CS- G, 1CS- H 

 20- 00- 03- 1 193 193AB 2C BELLY FAIRING BRAIDED CONDUIT 

GVI of elements fitted on the following harnesses end fittings39 to Fr. 40.2 : - 1541VB, 1543VB 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

 20- 00- 03- 2 TASK RESERVED  20- 00- 03- 3 191 

192 198 

 198GB, 191CB and 192CB 4C BELLY FAIRING BRAIDED CONDUIT

Functional check of the following belly fairing pressure seal b3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VP

 20- 00- 03- 4 TASK RESERVED  20- 00- 04- 1 454/464 454BR 454NR 

464BR 464NR 

2C ENGINE PYLON BRAIDED CONDUIT

GVI of elements fitted on the harnesses end fittings, from rib1

 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 union interface bracket on strut at MLG braided conduit 

 20- 00- 05- 3 TASK DELETED 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

 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 TASK RESERVEDR 20- 00- 07- 1 323 A330-200: 

325ML 325NL 312AR A330-300: 325BL 325DL 312AR 

2C VERTICAL FIN 

GVI of fly by wire protection installation at vertical fin : 5994VB 5995VB 5996VB 5997VB 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

R 20- 00- 07- 2 323 A330-200 PRE 48979: 

325ML 325NL 312AR A330-200 POST 48979: 325SL 325NL 312AR 311AZ 

313BL A330-300: 325BL 325DL 312AR

2C VERTICAL FIN 

GVI of fly by wire protection installation at vertical fin : 5989VB 5994VB 5995VB 5996VB 5997VB 6989VB 6994VB 
 A330 MRB REPORT – HIRF/Lightning Protection Scheduled Maintenance Req

 Reference Zone Access Interval Description Issue : July 2010 

This page intentionally left blank 
 A330 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 

40017 OXYGEN-DEFINE BASIC SYSTEM 

40041 EQUIPMENT/FURNISHINGS-DEFINE BASIC LOWER CARGO COMPARTMENT 

40063 AIR CONDITIONING-AVIONICS COMPARTMENT- DEFINE GROUND COOLING UNIT 

INSTALLATION 

40065 COMMUNICATIONS-DEFINE ACARS MU INSTALLATION (SUNDSTRAND) 

40068 COMMUNICATIONS-DEFINE INSTALLATION OF A SINGLE HF SYSTEM 

40069 COMMUNICATIONS-DEFINE INSTALLATION OF A SECOND HF SYSTEM 

40097 AIR CONDITIONING-DEFINE TEMPERATURE CONTROL OF FORWARD CARGO 

COMPARTMENT 

40117 LANDING GEAR-CENTER LINE GEAR –INSTALL PROVISIONS FOR T.P.I.S (TYRE 

PRESSURE INDICATING SYSTEM)

40118 LANDING GEAR-NOSE AND MAIN GEARS-INSTALL PROVISIONS FOR T.P.I.S (TYRE 

PRESSURE INDICATING SYSTEM) 

40208 EQUIPMENT/FURNISHINGS-BULK CARGO COMPARTMENT-PROVIDE CAPABILITY 

FOR LD3 CONTAINERS 

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 

40347 FUSELAGE-NOSE FORWARD FUSELAGE MODIFY DOOR NR 1 SURROUND 

40366 WINGS-STRUCTURE-INTRODUCE POST A330 COMMON WING BOX DEFINITION 

40379 EQUIPMENT/FURNISHINGS-INSTALL PROVISIONS FOR AN UNDERFLOOR CREW 

REST CONTAINER (BFE) 

40391 GENERAL-INTRODUCE MINOR IMPROVEMENTS FROM A/C 29 

40440 WINGS-LEADING EDGE-ADD STRUCTURAL PROVISIONS FOR REFUEL PANEL 

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

40611 EQUIPMENT/FURNISHINGS-UNDERFLOOR CREW REST ROOM-ADAPT PROVISIONS 

FOR ST2 VERSIONS

40676 E/F-LAVATORIES-DEFINE PIN PROGRAMMING AND WATER HEATING SYSTEM 

CONNEXION IN L42 ZONE

40701 FLIGHT CONTROLS-FLAPS-INSTALL KAMATICS FLAP TRACK ROLLER BEARINGS 

40823 COMMUNICATIONS-PASSENGER ADDRESS SYSTEM CONNECT PUBLIC ADDRESS 

TO BATTERY BUSBAR

40838 HYDRAULIC POWER-GREEN HYDRAULIC POWER-PROTECT GREEN HYDRAULIC 

CIRCUIT AGAINST OUTER WING STRUCTURAL DAMAGE
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 2

MOD 

NUMBER MOD TITLE 

40843 STABILIZER-VERTICAL STABILIZER-FINBOX-REINFORCE CFRP STRUCTURE PARTSSERIAL 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 

41323 AIR CONDITIONING-CABIN AIR DISTRIBUTION AND RECIRCULATION-INSTALL LE 

BOZEC RECIRCULATION FILTERS

41367 WATER/WASTE-WASTE WATER DRAIN-RELOCATE FWD DRAIN MAST IN SECT 13/14

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 

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 

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)

42044 NACELLES/PYLONS-PYLONS-REPLACE MATERIAL OF UPPER AND LOWER 

SPIGOT FITTINGS (A330)

42069 FUSELAGE-FORWARD FUSELAGE-INTRODUCE ADDITIONAL ACCOUSTIC 

INSULATION 

42102 NACELLES/PYLONS-REINFORCE BRACKET OF PRECOOLER COLD AIR DUCT 

BRACKET 

42275 WINGS-STRUCTURE-FIT T PLATES TO CENTRE SPAR 

42276 WINGS-STRUCTURE-REINFORCE SKIN PANEL NR 3 BETWEEN RIBS 10 AND 11 

(A330)

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)

42418 FUSELAGE-CENTRE FUSELAGE-REINFORCE MEMBRANE LIAISON ATFR 47/48 

42478 COMMUNICATIONS-CIDS-INTRODUCE CIDS VERSION 113 

42481 FUSELAGE-GENERAL-IMPROVE UPPER PARTS OF FR 12 AND 13 

42487 ELECTRIC AND ELECTRONIC COMMON INSTALLATION-MODIFY FEEDER ROUTING 

AT PYLON/WING INTERFACE (A330)

42547 WINGS-STRUCTURE-INTRODUCE NEW INNER REAR SPAR MACHINING 

42550 WINGS-GENERAL-DEFINE A330-300 +(217 T MTOW) AIRCRAFT 

42605 FUSELAGE-CENTER FUSELAGE-REINFORCE CENTER L/G DOOR JOINT 

42699 WINGS-STRUCTURES-FIT NEW REINFORCING STRAP TO BOTTOM OF SKIN 

PANEL NR 3 

42704 WATER/WASTE - POTABLE - INSTALL FILTER FOR WATER SUPPLY IN EACH 

LAVATORY. 

42829 FUSELAGE - SECTION 11/12 – REINFORCE FRAME 10 LATERAL PART 

42890 FUEL - APU FUEL PUMP SYSTEM – INTRODUCE SHORTENED SUCTION LINE IN AIR 

SEPARATOR 

42921 FUSELAGE - REAR FUSELAGE – INSTALL ADDITIONAL ACCESS DOOR FOR 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 3

MOD 

NUMBER MOD TITLE 

DRAINAGE OF AIR SEPARATOR (RETROFIT SOLUTION) 

42953 INDICATING/RECORDING SYSTEMS -ELECTRICAL CLOCK - INSTALL SMITH P/N 2610-

13 

43021 A/S PART OF RETRO-SOLUTION IS COVERED UNDER MOD 43272 

43069 LIGHTS - EMERGENCY LIGHTING SYSTEM - INSTALL MODIFIED EPSU 

43142 INDICATING/RECORDING SYSTEMS –DEFINE PIN-PROGRAMMING FOR DLH2 

VERSION 

43260 NAVIGATION - RADIO ALTIMETER - INSTALL ALLIED SIGNAL QUANTUM LINE P/N 

066.50007-0202 - (SFE)

43271 NACELLES/PYLONS - GENERAL – MODIFY WING/PYLON FILLET 

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 

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 

43462 POWER PLANT - GENERAL – PROPULSION SYSTEM GE CF6-80E1 COLLECTIVE MOD 

FOR CHANGES CLASSIFIED A2-1

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

43503 WINGS-INNER REAR SPAR TRAILING EDGE-FIT MODIFIED INNER REAR AND ROOT 

JOINT WITH IMPROVED FATIGUE CHARACT. (A330 217T)

43517 GENERAL - INTRODUCE MINOR IMPROVEMENTS FROM A/C 149 ONWARDS (DAPART ONLY)

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 

43719 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - INSTALL 

COMPARTMENT DRAINAGE

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 

44043 FUSELAGE - REAR FUSELAGE – REINFORCE COVER PLATE OF TORSION BOX 

FRAME 73A AND 75A (SERIAL SOLUTION)

44047 FLIGHT CONTROLS - EFCS / CONTROL INPUT AND POWER SUPPLY - PROVIDE A 

SECOND ELECTRICAL POWER SUPPLY TO FCSC2 

44058 COMMUNICATION - CIDS – INTRODUCE IMPROVED NS/FSB SIGNS 

44072 FUSELAGE – FORWARD/REAR FUSELAGE - REINFORCE CARGO DOOR ACTUATOR 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 4

MOD 

NUMBER MOD TITLE 

SUPPORT BEAM 

44100 NAVIGATION - WEATHER RADAR SYSTEM - ACTIVATE DUAL PREDICTIVE 

WINDSHEAR RADAR SYSTEM, COLLINS

44147 FUSELAGE - FORWARD FUSELAGE - REINFORCE FRAME C33 

44203 FUSELAGE - REAR FUSELAGE – DEFINE COMMON STRUCTURE FOR SECTION 17 

44204 FUSELAGE - REAR FUSELAGE – DEFINE COMMON STRUCTURE FOR SECTION 18 

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

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

44442 FLIGHT CONTROLS - RUDDER TRAVEL LIMITATION UNIT - INSTALL NEW STANDARD 

EQUIPMENT 

44482 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION - 

DEACTIVATE RAIN REPELLENT SYSTEM 

44504 FUEL - APU FUEL PUMP SYSTEM - INTRODUCE NEW APU AFT PUMP 

44522 ENGINE FUEL AND CONTROL - GENERAL - INSTALL FADEC SOFTWARE STD E1I 

44601 EQUIPMENT/FURNISHINGS - FWD AND AFT CARGO COMPARTMENT - ADAPT BASIC 

ST6 DEFINITION TO ST7 

44603 FUEL - APU FUEL PUMP SYSTEM – PREVENT AN ELECTRICAL ESS NETWORK 

"OVERLOAD" (A330)

44620 COMMUNICATIONS-SATCOM-INSTALL BALL AEROSPACE HIGH GAIN ANTENNA 

SYSTEM 

44647 FLIGHT CONTROL - RUDDER HYDRAULIC ACTUATION - INSTALL A NEW RUDDER 

SERVOCONTROL ON A330-200 FIN

44676 WINGS - LEADING EDGE - FIT TWO PART LOWER ACCESS PANEL AT TRACK RIB 10 

44723 FUSELAGE - CENTER FUSELAGE – REINFORCE ORBITAL JUNCTION AT FR53.3 

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 ANINSPECTION ACCESS 

44826 FUSELAGE - FORWARD FUSELAGE- MODIFY ACOUSTIC INSULATION 

44950 FUSELAGE - NOSE FORWARD FUSELAGE - INSTALL NEW GENERATION OF RADOME 

USING QUARTZ MATERIAL 

45008 FUEL - JETTISON SYSTEM - INSTALL JETTISON SYSTEM ON A330-200 

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

45199 AIR CONDITIONING - ADAPT FWD CARGO COMPARTMENT TEMPERATURE 

CONTROL SYSTEM FOR ST7 VERSIONS 

45223 FUSELAGE - FORWARD FUSELAGE - REINFORCE TORSION BOX BEAM COVER 

PLATE 

45226 FUSELAGE - FORWARD FUSELAGE - REDUCE BENDING EFFECTS 

45293 FUSELAGE - FORWARD FUSELAGE - REINFORCE PAX DOOR II CUT-OUT CORNER 

AREAS 

45307 FUSELAGE - CENTER FUSELAGE - REINFORCE BEAM Y +/- 1456 AND HYDRAULIC 

BRACKET 

45326 WINGS - INBOARD FLAP – INTRODUCE SIMPLIFIED SUPPORT 1 ASSEMBLY 

45395 EQUIPMENT/FURNISHINGS-CARGO COMPART.- ADAPT HEATED DRAINAGE SYSTEM 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 5

MOD 

NUMBER MOD TITLE 

IN FWD ANDAFT C.C. FOR ST7 A/C 

45415 WINGS - STRUCTURE - REPLACE CLEARANCE FIT BOLTS WITH INTERFERENCE FIT 

BOLTS AT CENTRE SPAR/STRINGER 15 JOINT 

45489 FUSELAGE - FORWARD/REAR FUSELAGE - REINFORCE CARGO DOOR ACTUATOR 

SUPPORT BEAM 

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 

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 

46201 E/F-CREW REST ROOM-INSTALL SYST. PROV. FOR LDMCRC BEHIND LOWER DECK 

LAVATORIES 

46202 E/F-LOWER DECK LAVATORIES-INSTALL STRUCTURAL PROV. FOR UNDERFLOOR 

LAV. COMPARTMENT

46203 E/F-LOWER DECK LAVATORIES-INSTALL SYSTEM PROVISIONS FOR UNDERFLOOR 

LAV. COMPARTMENT (RETRO IN LINE SOLUTION)

46231 LANDING GEAR - EMERGENCY BRAKING - INTRODUCE SHUT-OFF VALVE 

46241 WINGS - STRUCTURE - REPROFILE INNER REAR SPAR UPPER BUILD SLOT 

46307 LIGHTS-CABIN EMERGENCY LIGHTING- INSTALL PHOTOLUMINISCENT ESCAPE 

PATH MARKING FLOOR 

46386 AIR CONDITIONING-AVIONICS EQUIPMENT GROUND COOLING-IMPROVE GRU 

LOGICS 

46441 EQUIPMENT/FURNISHINGS-CARGO CONPARTMENTS-INSTALL SYSTEM PROV. FOR 

VCC IN BULK CARGO COMPARTMENT 

46636 FUSELAGE - FORWARD FUSELAGE – REINFORCE CIRCUMFERENTIAL JOINT 

FR31/37.1 AND LONGITUDINAL JOINT (SERIAL SOLUTION)

46732 NAVIGATION - RADIO ALTIMETER - INSTALL ALLIED SIGNAL QUANTUM LINE P/N 

066.50007-0212 

46772 E/F-PASSENGER COMPARTMENT SEATS- INTRODUCE IN-SEAT POWER SUPPLY 

SYSTEM (ISPSS) 15V DC FROM VENDOR PRIMEX

46849 FUSELAGE - REAR FUSELAGE SECT. 16 - RELOCATE VHF 2 ANTENNA (ADAPTATION 

SOLUTION)

46866 FUSELAGE - REAR FUSELAGE – REINFORCE FLOOR BEAM ATTACHMENT 

FITTING C75A AT P26 LH/RH

46879 THRUST REVERSER - STRUCTURE A330 RR - INTRODUCE THRUST REVERSER 

UNITS CAPABLE OF 25000 CYCLES
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 6

MOD 

NUMBER MOD TITLE 

46900 FUSELAGE - REAR FUSELAGE SECT. 16 - RELOCATE VHF 2 ANTENNA (SERIAL 

SOLUTION)

46972 E/F-PASSENGER COMPARTMENT SEATS - INTRODUCE IN-SEAT POWER SUPPLY 

SYSTEM (ISPSS) 110V FROM VENDOR K.I.D.

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 

47057 COMMUNICATIONS - GENERAL - ADAPT ATA 23 CABIN SYSTEMS FOR A340-500/600

47063 AIR CONDITIONING - GENERAL - ADAPT BASIC DEFINITION FOR A340-500/600 

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 

47358 EXHAUST - THRUST REVERSER STRUCTURE -INTRODUCE THRUST REVERSER 

UNIT CAPABLE OF 40.000 CYCLES - A330 RR 

47372 WINGS - T/E AND TRAILING EDGE DEVICES - INSTALL NEW KAMATICS SELFLUBRIFICATING TRACK ROLLERS AT TRACK 1-5

47423 EQUIPMENT/FURNISHINGS - DOOR AREA FLOOR PANEL HEATING - REMOVE 

HEATING ELEMENTS FOR PAX DOORS 1, 2, 3, 4

47433 FLIGHT CONTROLS – AILERON AND HYDRAULIC ACTUATION - INTRODUCE ROLLER 

BEARING ON AILERON SERVOCONTROL

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

47606 INDICATING/RECORDING SYSTEMS - RECORDERS - INSTALL A SYSTEM PROVISIONS 

FOR THE COMBINED FDIU/DMU (FDIMU)

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 

47879 COMMUNICATIONS-CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)-IMPROVE 

FAP SOFTWARE 

47928 INDICATING/RECORDING SYSTEMS – EIS - INSTALL DISPLAY UNITS WITH VIDEO 

CAPACITY 

48298 NACELLES/PYLONS-PYLONS-CHANGE MATERIAL OF PRIMARY STRUCTURE RIBS

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

48818 COMMUNICATIONS - GENERAL – BASIC PROVISIONS FOR IN FLIGHT 

ENTERTAINMENT SYSTEM A330/A340-200/300

48823 COMMUNICATIONS - GENERAL - ADAPT ATA 23 CABIN SYSTEMS FOR ENHANCED 

CABIN A330/A340-300

48979 STABILIZERS - GENERAL – INTRODUCE A340-500/-600 VERTICAL STABILIZER/ 

RUDDER ON A330-200

48904 INDICATING/RECORDING SYSTEM - ACMS - INSTALL SYSTEM PROVISIONS FOR 

THE COMBINED FDIU/DMU (FDIMU)

48980 FUSELAGE - GENERAL - REAR FUSELAGE INTRODUCE CFRP PRESSURE 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 7

MOD 

NUMBER MOD TITLE 

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 

49304 COMMUNICATIONS - GENERAL – INSTALL ENTERTAINMENT SYSTEM FOR QFA01 

VERSION 

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

49411 FUSELAGE-FORWARD FUSELAGE-REINFORCE CIRCUMFERENTIAL JOINT FRAME 

13 STR 9 FOR MAINTENANCE TASK IMPROVEMENT

49520 AIR CONDITIONING-CENTER FUSELAGE- INSTALL HEATSHIELDS IN BELLY 

FAIRING TO SEGREGATE AIR SYSTEM

49586 FLIGHT CONTROLS-ELEVATOR AND HYDRAULIC ACTUATION - INTRODUCE ROD 

END ROLLER BEARING ON S/C ELEVATOR - SB ONLY

49610 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL T SHAPED 

CENTERLINE GUIDE FOR A330-200

49705 WATER/WASTE-WASTE WATER DRAIN-INSTALL A NEW DRAIN ASSY FOR A340-

500/600 AND ENHANCED CABIN

49748 FLIGHT CONTROLS - ELECTRICAL FLIGHT CONTROL SYST.(EFCS)-ADAPT 

ELECTRICAL WIRING ON A330-200 AND A330-300

49769 NAVIGATION - ATC - INSTALL REMOTE ATC CONTROL BOX

49951 WATER/WASTE - POTABLE - INSTALL A NEW POTABLE WATER FILTER IN EACH 

LAVATORY

50003 NACELLES/PYLONS - GENERAL - PRODUCE CORROSION RESISTANT STEEL RIB 

18 

50014 EQUIPMENT/FURNISHINGS - COCKPIT - INSTALL AN ARMOURED COCKPIT DOOR

50088 WATER/WASTE - POTABLE - INSTALL INFRA RED WATER FAUCETS TOGETHER 

WITH CHOOSEABLE DRAIN ASSY.

50091 AIR CONDITIONING-DISTRIBUTION-INSTALL A SMOKE DETECTION SYSTEM FOR 

A VCC IN DOOR 1 AREA ON ENHANCED CABIN

50138 FLIGHT CONTROLS - SLATS – INTRODUCE ROTARY ACTUATOR WITH IMPROVED 

TORQUE LIMITER PERFORMANCE

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. 

50453 NAVIGATION - DDRMI - INSTALL UPDATED DDRMI WITH NEW TRANSFORMER 

50471 FLIGHT CONTROLS - SLATS – INTRODUCE ROTARY ACTUATOR WITH IMPROVED 

TORQUE LIMITER ASSEMBLY 

50567 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL "T-SHAPED" 

CENTER LINE GUIDE FOR A330-300 

50675 FUSELAGE - FAIRINGS - USE OF TITANIUM ON 31 BELLY FAIRING PARTS 

50723 DOORS - COCKPIT DOOR RELEASE SYSTEM - OVERRIDE ELECTRICAL SYSTEM 

50755 FUSELAGE - FWD AND CENTER SECTION - REDUCE APPLICATION OF MOD 49194 

AND 49202 

50860 NAVIGATION - ADF - INSTALL ADF1 900 COLLINS RECEIVER 

50995 AIR CONDITIONING - DISTRIBUTION - INSTALL AIR EXTRACTION LINE COMBINED 

WITH SMOKE DETECTION SYSTEM FOR VC 

51302 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT INSTALL A 3 CLASS SEAT 

LAYOUT FOR DLH06 VERSION 

51312 AIR CONDITIONING-DISTRIBUTION-INSTALL A SMOKE DETECTION SYS. FOR VCC 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 8

MOD 

NUMBER MOD TITLE 

CONNECTED TO AIR EXTRACTION SYS. FWD OF DOOR 2 LH 

51336 AIR CONDITIONING - AVIONICS EQUIPMENT GROUND COOLING- DE-ACTIVATE 

THE GROUND REFRIGERATION UNIT (GRU)

51337 AIR CONDITIONING - AVIONICS EQUIPMENT GROUND COOLING - REMOVE THE 

GROUND REFRIGERATION UNIT (GRU)

51363 FLIGHT CONTROLS -FLAPS -REPLACE FLAP TRACK ROLLER BEARING 

ALTERNATE EQUIPMENT MANUFACTURED BY TORRINGTON 

51617 EQUIPMENT/FURNISHINGS – ANCILLARY EQUIPMENT - INTRODUCE FLOOR 

TEMPERATURE SETTING PANEL IN DOOR AREA 

51642 ICE AND RAIN PROTECTION - ESCAPE SLIDE LOCKING MECHANISM ICE 

PROTECTION - REMOVE CONTROL UNIT 

52146 AIR CONDITIONING - DISTRIBUTION-INSTALL A SMOKE DETECTION SYSTEM -VCC 

CONNECTED TO AIR EXTRACTION SYS. AFT DOOR 2 LH 

52339 EQUIPMENT/FURNISHINGS – MISCELLANEOUS COMPARTMENTS - INSTALL 

LDMCR (LOWER DECK MOBILE CREW REST) 

52485 OXYGEN - PASSENGER OXYGEN - INSTALL A GASEOUS OXYGEN SYSTEM FOR 

A330-200 ENHANCED 

52720 AIR CONDITIONING-DISTRIBUTION-INSTALL A SMOKE DETECTION SYS FOR A 

VCC CONNECTED TO AIR EXTRACTION SYSTEM AT DOOR 1 AREA 

52911 FUSELAGE - CENTER FUSELAGE - REINFORCE STRUCTURE TO IMPROVE 

FATIGUE MAINTENANCE TASK 

53102 FUSELAGE - NOSE FORWARD FUSELAGE - MODIFY ORBITAL JUNCTION IN 

SECTION 12 AT FRAME 13

53123 DOORS - COCKPIT DOOR RELEASE SYSTEM- ELECTRICAL BACK- UP SYSTEM 

53622 NAVIGATION - SWITCHING AND INDICATING - REMOVE DDRMI INDICATORS 

53391 EQUIPMENT/FURNISHINGS -CREW REST ROOM- DEFINE SINGLE PILOT FLIGHT 

CREW REST (FCRC) SFE MODULE 

53522 NAVIGATION - ATC/MODE S - DEACTIVATE RATC FUNCTION 

54399 NACELLES / PYLONS - PYLON BOX - REPLACE RIB18 IN 40CDV12 BY RIB18 IN 15, -

5PH 

54455 COMMUNICATIONS - SATELLITE TV/DATA TRANSCEIVER SYSTEM - ADAPT ANTI 

COLLISION LIGHTINGS TO A330-200

54477 COMMUNICATIONS -SATELLITE TV/DATA TRANSCEIVER SYSTEM-INSTALL SYS 

PROV FOR TAILWIND 560 SYSTEM ON A330-200

54760 COMMUNICATIONS - SATELLITE TV/DATA TRANSCEIVER SYSTEM - ADAPT ANTI 

COLLISION LIGHTINGS TO A330-300

54762 COMMUNICATIONS - SATELLITE TV/DATA TRANSCEIVER SYS. (INCL. 

TERRESTRIAL TV) - INSTALL TAILWIND 560 SYSTEM PARTIALLY 

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

54946 COMMUNICATIONS - SATELLITE TV/DATA TRANSCEIVER SYSTEM (INCL. 

TERRESTRIAL TV) - INSTALL TAILWIND 560 SYSTEM

55244 EQUIPMENT/FURNISHINGS - CREW REST ROOM (UNDERFLOOR) - INSTALL AN 

EUROCOPTER LDMCR (BY SB) 

55380 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- INSTALL ADVANCED 

CARGO LOADING SYSTEM ON BASIC LR 

55381 EQUIPMENT/FURNISHINGS-CARGO COMPARTMENT- ADAPT ADVANCED CARGO 

LOADING SYSTEM FOR A330-200 

55534 FUSELAGE - GENERAL - MODIFY PARTIALLY ORBITAL JUNCTION IN SECTION 12, 

FRAME 13 

55559 OXYGEN-CABIN ATTENDANTS PORTABLE DEVICE- INTRODUCE NEW STD 

LAYOUT LIGHT WEIGHT PORTABLE OXYGEN CYLINDER ASSEMBLY 

55652 WINGS - TRAILING EDGE AND TRAILING EDGEDEVICES-CHANGE SEMI 
 A330 MRB REPORT 

Issue : July 2010 Page : APX 10. 9

MOD 

NUMBER MOD TITLE 

MATERIALS FOR PARTSOF FLAP TRACK 2, 3, 4 AND 5.

55780 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE 

MODIFIED THSA (P/N 47172-510)

56001 FUSELAGE - CENTER FUSELAGE - REINFORCE ORBITAL LINK FRAME 45TO 

IMPROVE FATIGUE BEHAVIOUR

56284 AIRBORNE AUXILIARY POWER - STORAGE AND DISTRIBUTION - INTRODUCE AN 

ENHANCED RECOGNITION OF OIL SYSTEM CONTAMINATION 

56296 AIR COND. – COMPARTMENT VENTILATION – MODIFY ISOLATION VALVE MPD 

TASK AND PIN PROG.FOR LDMCR CONTAINER W/O STAIRHOUSE 

56322 OXYGEN – PASSENGER OXYGEN – ADAPT GASEOUS OXYGEN SYSTEM TO A330-

300 

56713 ENGINE - GENERAL - ACTIVATE ELECTRONIC MAGNETIC CHIP DETECTOR 

(EMCD) FUNCTION ON IN-SERVICE RRT700 ENGINES 

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 

56835 E/F - CARGO COMPARTMENTS - INSTALL HEATED DRAINAGE IN FWD AND AFT 

C.C. FOR A330-200 - ADVANCED CLS

56837 E/F - LOWER DECK BULK CARGO COMPARTMENT- PROVIDE CAPABILITY FOR 

LD3 CONTAINERS- FOR A330-300/A340-300 - ADVANCED CLS 

56839 E/F-LWR DECK AFT C.C.-ADAPT STRUCTURAL AND SYST. PROVISIONS FOR AN 

UCRC (LD-MCR) FOR A330-200 - ADVANCED CLS

57371 EQUIPMENT/FURNISHING - CURTAINS AND PARTITIONS - INTRODUCE IMPROVED 

DECOMPRESSION PANEL IN COCKPIT DOOR

58204 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL A 

MAIN DECK CLS (BFE) - ANCRA

58215 WATER / WASTE - AIR SUPPLY - INSTALL AN AUXILIARY COMPRESSOR 

58552 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL OF 

MAIN DECK CLS (BFE) MULTIPLE CHOICE CONFIGURATION - AAR 

58623 FUEL-TANKS- REMOVE OF THE CENTRE TANK CAPABILITY 

200281 FUEL - TANKS - ADDITION OF CENTRE TANK CAPABILITY 
This page intentionally left blank
 A330 MRB REPORT 

Issue : July 2010 

Page: APX 11. 1

 

APPENDIX 11

 

LANDING GEAR OVERHAUL / RESTORATION INTERVAL REQUIREMENTS 

1. INTRODUCTION 

2. A330 MAIN LANDING GEAR 

3. A330 NOSE LANDING GEAR 

4. LANDING GEAR SAMPLING POLICY 

1. INTRODUCTION

This Appendix summarises the requirements to justify the Time Between Overhaul (TBO) interval for 

restoration of the A330 Main Landing Gear (MLG) and Nose Landing Gear (NLG). 

The interval selected for restoration of A330 Landing Gears is 10 years or 17,000FC, whichever occurs 

first. 

The above intervals are dependent on the Inspection and Lubrication requirements stated in Paragraph 

a) of Sections 2 & 3. 

 

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 A330 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 A330 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 and 3, Paras b) and c). 

Items requiring additional Sampling are listed in Sections 2 & 3, Paras d) and e). 

The Landing Gear Sampling Policy is stated in Section 4. 

The requirements stated in Sections 2 & 3 are temporary. Following a working group review, they are 

expected to be superseded by new or revised tasks in MRBR rev 12. 

2. A330 MAIN LANDING GEAR
A330 MRB REPORT 

Issue : July 2010 Page: APX 11a) 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 (A330-32-3135) 

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 (A330-32-3162) 

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 
A330 MRB REPORT 

Issue : July 2010 Page: APX 11b) MLG modifications recommended to be accomplished prior to a 10 year TBO 

Airbus and Messier-Dowty advise A330 operators to consider accomplishing the following recommended product improvement modifications 

overhaul. The benefit to the operator will be an improved operational reliability of the post mod parts and a lower level of degradation at over

Vendor Service Bulletin Reference 

Airbus Service Bulletin Reference 

Mod Number 

Threshold/ Interval 

Description Introduced as 

Standard in 

Production From MSN: 

A33/34-32-171 

A330-32-3135 

49358 3 years from EIS Introduce new adjustable link assembly 

(201254 Series – Basic Gear) 

MSN 435 

A33/34-32-172 

A330-32-3135 

49358 3 years from EIS Introduce new adjustable link assembly 

(201489 Series – Growth Gear) 

MSN 435 

A33/34-32-197 

A330-32-3141 

49664 4 years from EIS New Shortening Mechanism connecting link 

(201254 Series – Basic Gear) 

MSN 454 

A33/34-32-198 

A330-32-3141 

49664 4 years from EIS New Shortening Mechanism connecting link 

(201489 Series – Growth Gear) 

MSN 454 
A330 MRB REPORT 

Issue : July 2010 Page: APX 11c) MLG modifications recommended to be accomplished at the 10 year overhaul Based on in-service data, Airbus and Messier-Dowty advise A330 operators to consider accomplishing the following recommended product imoverhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a loweoverhaul. 

Vendor Service Bulletin Reference

Airbus Service Bulletin Reference 

Mod Number 

Description Introduced as 

Standard in 

Production 

From MSN: 

A33/34-32-153 

A330-32- 3114 

47523 New Aluminum Piston with Nickel under Chrome 

Oxide coating (201254 Series – Basic Gear) 

MSN 315 All in-s

mod. 

A33/34-32-154 

A330-32-3114 

47523 New Aluminum Piston with Nickel under Chrome 

Oxide coating (201489 Series – Growth Gear) 

MSN 315 All in-s

mod. 

A33/34-32-175 

A330-32-3126 

48246 New Bushes in Bogie Beam & Slider 

(201254 Series – Basic Gear) 

MSN 366 Bushe

standa

A33/34-32-176 

A330-32-3126 

48246 New Bushes in Bogie Beam & Slider 

(201489 Series – Growth Gear) 

MSN 366 Bushe

standa

A33/34-32-190 

A330-32- 3143 

49777 Improved corrosion protection for Retraction Link & 

‘W’ Pin (201254 Series – Basic Gear)

MSN 454 Improv

applied 

A33/34-32-191 

A330-32- 3143 

49777 Improved corrosion protection for Retraction Link & 

‘W’ Pin (201489 Series – Growth Gear)

MSN 454 Improv

applied 

A33/34-32-193 

A330-32-3142 

49806 New Axle with Additional Corrosion Protection 

(201254 Series – Basic Gear)

MSN 459 Applic

A33/34-32-194 

A330-32-3142 

49806 New Axle with Additional Corrosion Protection 

(201489 Series – Growth Gear)

MSN 459 Applic

A33/34-32-195 

A330-32-3162 

50959 Modified Uplock Roller assembly & new bolts 

(201254 Series – Basic Gear) 

MSN 527 Basic 

at ov

n

A33/34-32-196 

A330-32-3162 

50959 Modified Uplock Roller assembly & new bolts 

(201489 Series – Growth Gear) 

MSN 527 Repla

Roller 
A330 MRB REPORT 

Issue : July 2010 Page: APX 11d) MLG items requiring further sampling and/or data from recent overhauls to justify 10 year TBO interval on individual 

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overhaul interva

satisfactory addit

sampling not achie

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 YEARS *

(based on previous 

sample) 

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 YEARS * 

(10-year TBO low 

based on samples to 

* 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 such

overhaul. 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. 
A330 MRB REPORT 

Issue : July 2010 Page: APX 11e) MLG items requiring further sampling or using 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 

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. 
A330 MRB REPORT 

Issue : July 2010 Page: APX 113. A330 NOSE LANDING GEAR

a) 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 A330 operators to consider accomplishing the following recommended product im

overhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a loweoverhaul. 

Vendor Service Bulletin Reference

Airbus Service Bulletin Reference 

Mod Number 

Description Introduced as 

Standard in 

Production 

From MSN: 

Comm

D23581-32-053 

None 54793 Introduction of a New Shock Absorber Tube and 

Modification of the Material of the diaphragm 

MSN 793 Replac

new Sand m
A330 MRB REPORT 

Issue : July 2010 Page: APX 11d) NLG items requiring sampling and/or data from recent overhauls to justify 10 year TBO interval on individual parts 

Item/ Component 

Item Part 

Number 

Comments / 

Reason 

Requirement Applicability 

Mod Status 

Sampling/OVH data 

Reporting Date 

Overh

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 

To be just

from Overh

Flee

Note: At the time of the sampling program, the NLG Retraction Actuator was considered by the industry as an “on-condition” item. A

tested at overhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and compleRetrospective compliance is currently not required for Retraction Actuators not having been overhauled. However, this is under revie

 Once completed, sampling results will be communicated to the MRB/ISC for review. 
A330 MRB REPORT 

Issue : July 2010 Page: APX 11e) 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 

Overha

satisfacto

sampling 

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,

* 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. 
 A330 MRB REPORT 

Issue : July 2010 Page: APX 11. 10

4. 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 17000FC, whichever 

occurs first. 

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 A330 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 A330 ALS Pt 1. 

A nose gear comprises: 

- main fitting 

- shock absorber assembly 

- torque links 

- axles 

- dragstay assembly (including downlock mechanism & springs) 

- retraction actuator 

For a complete list of NLG Life Limited Parts refer to A330 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. 

A330 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).