# 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.

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# 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

A 330-200F"

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

A 330-300 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

A 330-200F"

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

A RM 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

A ND 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 - A DAPT BASIC

ST6 DEFINITION TO ST7

45395 EQUIPMENT/FURNISHINGS-CARGO COMPART.- A DAPT 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 FL Y -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

A T 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

C A RGO COMPARTMENT - A DVANCED CLS

56835 E/F - CARGO COMPARTMENTS - INSTALL HEATED DRAINAGE IN FWD AND AFT

C.C. FOR A330-200 - A DVANCED CLS

56837 E/F - LOWER DECK BULK CARGO COMPARTMENT- PROVIDE CAPABILITY FOR

LD3 CONTAINERS- FOR A330-300/A340-300 - A DVANCED CLS

56839 E/F-LWR DECK AFT C.C.-ADAPT STRUCTURAL AND SYST. PROVISIONS FOR AN

UCRC ( LD-MCR ) FOR A330-200 - A DVANCED 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 LAVATOR Y

58204 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL A

MAIN DECK CLS ( BFE )

- A NCRA

58215 WATER / WASTE - A IR SUPPLY - INSTALL AN AUXILIARY COMPRESSOR

58552 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL OF

MAIN DECK CLS ( BFE ) MULTIPLE CHOICE CONFIGURATION - A AR

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 Spec ific 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 b een 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 th e manufacturer's appropriate maintenance

publications for additional lubrication information.

(j) In the Systems and Powerplant Section, some MSI references and titles include two

or more ATA subchapters.

In this issue of MRB Report produced from a Data Base Management System, only

the first reference is printed and the title must have less than 120 characters. This

concerns the following items:

QUOTED REFERENCE- ABBREVIATED TITLE COMPLETE REFERENCE AND TITLE

21.28.00 LOWER DECK CARGO

COMPARTMENT HEATING, VENTILATION

AND COOLING (FWD, AFT AND BULK) 21.28.00 LOWER DECK CARGO

COMPARTMENT VENTILATION AND COOLING

(FWD, AFT AND BULK)

21.43.00 LOWER DECK CARGO

COMPARTMENT HEATING (FWD, AFT AND

BULK)

21.50.00 A IR COOLING, TEMPERATURE

CONTROL 21.50.00 A IR COOLING

21.60.00 TEMPERATURE CONTROL

23.33.00 IN FLIGHT ENTERTAINMENT

SYSTEM 23.33.00 IN FLIGHT ENTERTAINMENT

SYSTEM

23.36.00 PASSENGER VIDEO

ENTERTAINMENT

25.52.00 LOWER DECK FORWARD AND AFT

CARGO COMPARTMENT 25.52.00 LOWER DECK FORWARD CARGO

COMPARTMENT

25.53.00 LOWER DECK AFT CARGO

COMPARTMENT

32.30.00 EXTENSION AND RETRACTION,

POSITION AND WARNING 32.30.00 EXTENSION AND RETRACTION

32.60.00 POSITION AND WARNING

34.48.00 TERRAIN AWARENESS AND

WARNING SYSTEM (INCLUDING (E)GPWS

AND T2CAS-TAWS) 34.43.20 T2CAS - TERRAIN AWARENESS AND

WARNING SYSTEM

34.48.00 TERRAIN AWARENESS AND

WARNING SYSTEM (INCLUDING (E)GPWS

AND T2CAS-TAWS)

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.A330MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-63. EXPLANATION OF SYSTEMS AND POWERPLANT SECTION FORMATMSIREFERENCETASK MSI AND TASK DESCRIPTION FEC INTERVALZIPREFERENCEAPPLICABILITY1 2 3 4 5 6 71- This column indicates the MSI reference number and is directly obtained from the Airbus ATA Breakdown and Nomenclature Reference document.Paragraph C1(j) identifies MSIs that address two or more systems / sub-systems.2- This column identifies the task type and thus enables the user to understand from which MSG-3 Level 2 logic question the task has been developed, ie :- LU Lubrication 5A, 6A, 7A, 8A, 9A- SV Servicing 5A, 6A, 7A, 8A, 9A- OP Operational Check 8B, 9B- VC Visual Check 8B, 9B- GVI, DI, SDI Inspection 5B, 6B, 7B, 8C, 9C- FC Functional Check 5B, 6B, 7B, 8C, 9C- RS Restoration 5C, 6C, 7C, 8D, 9D- DS Discard 5D, 6D, 7D, 8E, 9EThis information can be used to clarify whether the task is to detect a failure (8B, 9B) or to detect degradation (5B, 6B, 7B,8C, 9C).3- This column identifies the MSI title (which is in accordance with the Airbus ATA Breakdown) and the description of each taskidentified through the MRBReport development process.The term "No task selected" indicates that the MSI has been subjected to a full MSG-3 analysis but no applicable and effectivetasks were identified.The term "-task deleted-" indicates that during the development process a task had been proposed which was eventually deleted due to re analysis, taskamalgamation or ISC decision. Renumbering of tasks was avoided inorder to minimise impact on cross reference data in operatorsinitial maintenanceschedules.A330MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-7The term "-reserved-" indicates that the task number has been allocated to an A340 MRB Report task. This ensures that corresponding Systems sectiontasks have the same reference number in the A330 and A340 MRB Reports.4- This column identifies the Failure Effect Category (FEC). MSG-3 analysis allocates tasks against the following FECs depending on the consequence offailure :- FEC 5 : Evident Safety Effects- FEC 6 : Evident Operational Effects- FEC 7 : Evident Economic Effects- FEC 8 : Hidden Safety Effects- FEC 9 : Hidden Non-Safety Effects.The notation "-" (hyphen) in the FEC column indicates that the task has not been developed through the MSG-3 systems and powerplant logic process.Such tasks arise from either a specific MRB requirement (e.g. escape slide sampling) or have been determined as necessary to maintain compliance withType Certification requirements or are the results of the ATA 20 HIRF/EZAP analysis process.Multiple FECs are quoted only when the task is associated with both a hidden and an evident FEC. Where multiple hidden FECs (8,9) or multiple evidentFECs (5, 6, 7) are applicable only the most important one is quoted.5- This column identifies the interval between successive accomplishments of the task. Refer to Section A para 5 "Inspection Intervals".The "Note x." referred to in this column is detailed in Section C para 2.Some of the tasks necessary to maintain compliance with Type Certification requirements have been determined to warrant Certification MaintenanceRequirement (CMR) status. Such tasks are highlighted in this section by the notation "NOTE 24" in the interval column. The corresponding handlinginstructions are given in the approved document "A330 Certification Maintenance Requirements" reference 955.2074/93. Instructions to locate the CMRDocument 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)A330MRB REPORT - Systems and PowerplantIssue : July 2010Page : C-INTRO-86- The scheduled maintenance task derived from MSG-3 analysis is considered adequately covered by the referenced Zonal tasks inthis column. It should benoted that the Zonal task interval may be more frequent than that required by the Systems and Powerplant task.These requirements are quoted for record purposes and are not subject to tasks additional to those given in Section E.7- This column indicates the A/C configuration, model or enginetype to which this requirement is applicable. Examples are given below:ALLTask applicable to all A330 aircraft, including A330-200FA330-200 Task applicable to all A330-200 only, excluding A330-200FA330-200ORA330-300Task applicable to all A330 aircraft excluding A330-200FA330-200FTask applicable to all A330-200F onlyPRE 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 ROOMINSTALLEDSelf-explanatoryA330-300PRE 44051Task applicable to A330-300 without modification 44051embodied.A330-200POST 44051Task applicable to A330-200 (excluding A330-200F) withmodification 44051 embodied.POST 44051POST 44061POST 44085Task applicable to all A330 with modification 44051 and 44061 and44085 embodied.i.e. only to Aircraft with all modifications embodied.POST 45040ORPOST 45056Task applicable to all A330 with modification 45040 or 45056embodied i.e. to Aircraft with one of the modification or bothmodifications embodied.PRE 45040PRE 45056Task applicable to all A330 without both modification 45051 and45085 embodied at the same timei.e. without any if these modifications embodiedPOST 44040PRE 44057Task applicable to all A330 with modification 44040 and withoutmodification 44057 embodied at the same time.This page intentionally left blankAPPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.00.00 ENHANCED ZONAL20.0.121 AVIONICS COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AVIONICS - I: 72 MOALLCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF 710VU AND 740VU IN THE - I: 144 MOALLAVIONICS COMPARTMENT, (EWIS).20.0.131 FORWARD CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO - I: 72 MOALLCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOALLINSTALLED IN THE FORWARD CARGO COMPARTMENT, (EWIS).20.0.137 BAY BEHIND FWD CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD - I: 72 MOALLCARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).20.0.141 CENTER WING BOXR GVI 01 GENERAL VISUAL INSPECTION OF EWIS INSTALLED INSIDE - I: 144 MOALLTHE FUEL TANK (AS FAR AS VISIBLE), (EWIS).20.0.145 ZONE UNDER CABIN FLOORR RS 01 CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN - I: 144 MOALLFLOOR (ONLY IF CONTAMINATED), (EWIS).20.0.151 AFT CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA330-300COMPARTMENT (ONLY IF CONTAMINATED),(EWIS).* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.151 * * * * * C O N T I N U E * * * * *R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA330-200COMPARTMENT (ONLY IF CONTAMINATED),(EWIS).ORA330-200FR RS 03 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA330-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).WITHOUT LD-MCRWITHOUT LDLR RS 04 CLEANING OF EWIS INSTALLED IN THE AFT CARGO - I: 72 MOA330-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).WITH LDLR GVI 05 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOALLINSTALLED IN THE AFT CARGO COMPARTMENT, (EWIS).20.0.161 BULK CARGO COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MOA330-200COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).ORA330-300R GVI 02 GENERAL VISUAL INSPECTION OF G AND P ROUTES - I: 144 MOA330-200INSTALLED IN THE BULK CARGO COMPARTMENT, (EWIS).ORA330-300N RS 03 CLEANING OF EWIS INSTALLED IN THE BULK CARGO - I: 72 MOA330-200FCOMPARTMENT (ONLY IF CONTAMINATED).(EWIS).N GVI 04 GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED - I: 144 MOA330-200FIN THE BULK CARGO COMPARTMENT. (EWIS)20.0.211 COCKPITR RS 01 CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY - I: 144 MOALLIF CONTAMINATED), (EWIS).R GVI 02 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE - I: 144 MOALLCOCKPIT AT LEVEL OF LATERAL FLOOR STRUCTUREBETWEEN 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-20PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.221 * * * * * C O N T I N U E * * * * *R GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEATS AND A/C AND SEAT TO SEAT CONNECTION INSTALLEDORIN THE FWD CABIN UTILITY AREA, (EWIS).A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTESEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN UTILITY - I: 144 MOA330-200AREA (ONLY IF CONTAMINATED), (EWIS).ORA330-300R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MOA330-200IN THIS AREA, (EWIS).ORA330-300N RS 04 CLEANING OF EWIS INSTALLED IN THE COURIER COMPARTMENT - I: 144 MOA330-200FAREA (ONLY IF CONTAMINATED), (EWIS)N GVI 05 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES INSTALLED - I: 144 MOA330-200FIN THE COURIER COMPARTMENT AREA,(EWIS).N GVI 06 GENERAL VISUAL INSPECTION OF EWIS CONNECTION, - I: 72 MOA330-200FATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLEDIN THE COURIER COMPARTMENT AREA,(EWIS).NOTE: TASK ONLY APPLICAPBLE IF SEATS WITH EWISCONNECTION BETWEEN SEAT AND A/C AND/OR SEAT TO SEATCONNECTIONS INSTALLED.20.0.223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT / COURIER OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS AND CIRCUIT BREAKERS "5001 VE" - I: 144 MOA330-200INSTALLED IN THE FWD CABIN ULITY AREA OVERHEADORCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).A330-300R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001 - I: 144 MOA330-200VE" AND  ́G, AND P ́ ROUTES INSTALLED IN THE FWDORCABIN UTILITY AREA OVERHEAD COMPARTMENT, (EWIS).A330-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.223 * * * * * C O N T I N U E * * * * *N RS 03 CLEANING OF ALL EWIS AND CIRCUIT BREAKERS "5001 VE" - I: 144 MOA330-200FINSTALLED IN THE COURIER OVERHEAD COMPARTMENT (ONLYIF CONTAMINATED), (EWIS).N GVI 04 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5001 - I: 144 MOA330-200FVE" AND "G, AND P" ROUTES INSTALLED IN THE COURIEROVERHEAD COMPARTMENT AREA, (EWIS).20.0.230 FWD MAIN DECK CARGO COMPARTMENTN RS 01 CLEANING OF EWIS INSTALLED IN THE FWD MAIN DECK CARGO - I: 144 MOA330-200FCOMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MOA330-200FIN THE FWD MAIN DECK CARGO COMPARTMENT AREA. (EWIS)20.0.231 FWD CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLEDORIN THE FWD CABIN AREA, (EWIS).A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTESEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION,ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE FWD CABIN AREA. - I: 144 MOA330-200(ONLY IF CONTAMINATED), (EWIS).ORA330-30020.0.233 FWD CABIN OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE FWD CABIN OVERHEAD - I: 144 MOA330-200COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).ORA330-300N GVI 03 GENERAL VISUAL INSPECTION OF "G" AND "P" ROUTES - I: 144 MOA330-200INSTALLED IN THE FORWARD CABIN OVERHEADORCOMPARTMENT, (EWIS).A330-300ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.240 FWD MID MAIN DECK CARGO COMPARTMENTN RS 01 CLEANING OF ALL EWIS INSTALLED IN THE FWD MID MAIN - I: 144 MOA330-200FDECK CARGO COMPARTMENT AREA (ONLY IF CONTAMINATED),(EWIS).N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MOA330-200FIN THE FWD MID MAIN DECK OVERHEAD CARGO COMPARTMENTAREA, (EWIS).20.0.241 MID CABIN UTILITY AREAR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION INSTALLEDORIN THE MID CABIN UTILITY AREA, (EWIS).A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTESEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND A/C AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN UTILITY - I: 144 MOA330-200AREA (ONLY IF CONTAMINATED), (EWIS).ORA330-30020.0.243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENTR RS 01 CLEANING OF ALL EWIS INSTALLED IN THE MID CABIN - I: 144 MOA330-200UTILITY AREA OVERHEAD COMPARTMENT AREAOR(ONLY IF CONTAMINATED), (EWIS).A330-300N GVI 03 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA330-200INSTALLED IN THE MID CABIN UTILITY AREA OVERHEADORCOMPARTMENT AREA, (EWIS)A330-30020.0.250 MID MAIN DECK CARGO COMPARTMENTN RS 01 CLEANING OF EWIS INSTALLED IN THE MID MAIN DECK CARGO - I: 144 MOA330-200FCOMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).N GVI 02 GENERAL VISUAL INSPECTION OF "G" ROUTES INSTALLED - I: 144 MOA330-200FIN THE MID MAIN DECK CARGO COMPARTMENT AREA, (EWIS).ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.251 MID CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS, BETWEENNOTESEAT AND A/C AND/OR SEAT TO SEAT CONNECTION,ORINSTALLED IN THE MID CABIN AREA. (EWIS).A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTESEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND AND/OR SEAT TO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE MID CABIN AREA - I: 144 MOA330-200(ONLY IF CONTAMINATED), (EWIS).ORA330-300R GVI 03 GENERAL VISUAL INSPECTION OF ALL "G AND P" ROUTES - I: 144 MOA330-200INSTALLED IN THIS AREA.(EWIS)ORA330-30020.0.253 MID CABIN OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE MID CABIN OVERHEAD - I: 144 MOA330-200COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).OR.A330-300N GVI 04 GENERAL VISUAL INSPECTION OF "G AND P" ROUTES - I: 144 MOA330-200INSTALLED IN THE MID CABIN OVERHEAD COMPARTMENTORAREA. (EWIS)A330-30020.0.260 AFT MID MAIN DECK CARGO COMPARTMENTN RS 01 CLEANING OF EWIS INSTALLED IN THE AFT MID MAIN DECK - I: 144 MOA330-200FCARGO COMPARTMENT AREA (ONLY IF CONTAMINATED).(EWIS).20.0.261 AFT CABINR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS,NOTEBETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTIONORINSTALLED IN THE AFT CABIN AREA, (EWIS).A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTESEATS AND WITH EWIS CONNECTIONS BETWEEN SEATAND 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-20PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.261 * * * * * C O N T I N U E * * * * *R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN AREA - I: 144 MOA330-200(ONLY IF CONTAMINATED), (EWIS).ORA330-30020.0.263 AFT CABIN OVERHEAD COMPARTMENTR RS 01 CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD - I: 144 MOA330-200COMPARTMENT AREA (ONLY IF CONTAMINATED), (EWIS).ORA330-300N RS 04 GENERAL VISUAL INSPECTION OF "P" ROUTE INSTALLED - I: 144 MOA330-200IN THE AFT CABIN OVERHEAD COMPARTMENT AREA (EWIS).ORA330-30020.0.270 AFT MAIN DECK CARGO COMPARTMENTN RS 01 CLEANING OF ALL EWIS INSTALLED IN THE AFT MAIN DECK - I: 144 MOA330-200FCARGO COMPARTMENT (ONLY IF CONTAMINATED), (EWIS).20.0.271 AFT CABIN UTILITY AREAR GVI 01 GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS, - I: 72 MOA330-200ATTACHMENT POINTS AND ELECTRICAL CONNECTORS,NOTEBETWEEN SEAT AND A/C AND/OR SEAT TO SEAT CONNECTIONORINSTALLED IN THE AFT CABIN UTILITY AREA, (EWIS)A330-300NOTE: THIS TASK IS APPLICABLE FOR A/C VERSIONS WITHNOTEEWIS CONNECTIONS BETWEEN SEAT AND A/C AND/OR SEATTO SEAT CONNECTION, ONLY.R RS 02 CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY - I: 144 MOA330-200AREA (ONLY IF CONTAMINATED), (EWIS).ORA330-300R GVI 03 GENERAL VISUAL INSPECTION OF ALL "P" ROUTES IN THIS - I: 144 MOA330-200AREA, (EWIS).ORA330-30020.0.273 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.273 * * * * * C O N T I N U E * * * * *R RS 01 CLEANING OF EWIS AND CIRCUIT BREAKERS "5005 VE" - I: 144 MOA330-200INSTALLED IN THE AFT CABIN UTILITY AREA OVERHEADORCOMPARTMENT (ONLY IF CONTAMINATED), (EWIS).A330-300R GVI 02 GENERAL VISUAL INSPECTION OF CIRCUIT BREAKERS "5005 - I: 144 MOA330-200VE" AND "P" ROUTE INSTALLED IN THE AFT CABIN UTILITYORAREA OVERHEAD COMPARTMENT, (EWIS).A330-30020.0.315 TAIL CONE, APU AND ACCESSORY COMPARTMENTR GVI 01 GENERAL VISUAL INSPECTION OF "G AND "P" ROUTES - I: 54 MOALLINSTALLED IN THE TAIL CONE FIREWALL AND APU AREA,(EWIS).20.0.319 HORIZONTAL STABILIZER CENTER BOXR GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).PRE 41600ORA330-300PRE 41600R GVI 02 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200CENTER BOX EWIS (AS FAR AS VISIBLE), (EWIS).POST 41600ORA330-300POST 41600ORA330-200F20.0.333 HORIZONTAL STABILIZER LATERAL BOXR GVI 01 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOALLLATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 3 TORIB 4 LH/RH, (EWIS).* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.333 * * * * * C O N T I N U E * * * * *R SDI 02 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPRE 43491RIB 19LH/20RH, (EWIS).ORA330-300PRE 43491R SDI 03 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPOST 43491RIB 13LH/20RH, (EWIS).PRE 44818ORA330-300POST 43491PRE 44818R GVI 04 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 13 TOPOST 43491RIB 20LH, (EWIS).PRE 44818ORA330-300POST 43491PRE 44818R SDI 05 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER - I: 144 MOA330-200LATERAL BOX EWIS (AS FAR AS VISIBLE) FROM RIB 4 TOPOST 44818RIB 20LH/RH, (EWIS).ORA330-300POST 44818ORA330-200F20.0.541 INNER FUEL TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE INNER - I: 144 MOALLFUEL TANK (AS FAR AS VISIBLE)(EWIS).20.0.542 OUTER FUEL TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS IN THE OUTER FUEL - I: 144 MOALLTANK (RIB 23 TO RIB 33)(AS FAR AS VISIBLE)(EWIS).ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section20.0.550 VENT SURGE TANKR GVI 01 GENERAL VISUAL INSPECTION OF EWIS WITHIN THE VENT - I: 144 MOALLSURGE TANK (AS FAR AS VISIBLE)(EWIS).20.0.571 MAIN LANDING GEAR WELLR GVI 01 GENERAL VISUAL INSPECTION OF FUEL PUMP EWIS (AS FAR - I: 144 MOALLAS VISIBLE)(EWIS).* * * * * E N D * * * * *ISSUE: JUL 01/10 ENHANCED ZONAL SECTION: C-20PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.00.00 AIR CONDITIONING21.21.00 CABIN AIR DISTRIBUTION AND RECIRCULATIONVC 01 VISUAL CHECK OF MIXER UNIT 9 I: 4 CALL02 TASK RESERVEDDS 03 DISCARD RECIRCULATION FILTER ELEMENTS (PALL). 7 I: 5600 FHPRE 41323NOTE 15PRE 45081R OP 04 OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC 9 I: 2 CA330-200CLOSING OF ISOLATION VALVES OF THE STOWAGEPOST 46203COMPARTMENTR OP 05 OPERATIONAL CHECK TO VERIFY MANUAL AND AUTOMATIC 8 I: 3200 FHA330-200CLOSING OF ISOLATION VALVES OF THE CREW REST ROOM NOTEPOST 46201(UNDERFLOOR) IN LOWER DECK LAVATORY CONFIGURATION.NOTE: IF MOBILE CREW REST ROOM IS NOT FITTED WHENTASK BECOMES DUE IT MUST BE PERFORMED WHEN MCR ISNEXT INSTALLED.DS 06 DISCARD VIDEO CONTROL CENTER AIR FILTER ELEMENTS 9 I: 1 AIF VCCNOTE 1INSTALLEDOP 07 OPERATIONAL CHECK OF "STAND ALONE" SMOKE DETECTION 9 I: 2 CIF VCCSYSTEM VIA "SMOKE TEST" BUTTONINSTALLEDOP 08 OPERATIONAL CHECK OF VCC FAN DEACTIVATION BY 9 I: 2 CIF VCC WITH FANUSING THE FAN OFF SWITCHOFF SWITCHINSTALLED09 TASK RESERVED10 TASK RESERVEDDS 11 DISCARD ODOR RECIRCULATION FILTER ELEMENTS. 7 I: 2400 FHPOST 45081NOTE 15DS 12 DISCARD RECIRCULATION FILTER ELEMENTS (LE BOZEC - 7 I: 4000 FHPOST 41323DONALDSON). NOTE 15N OP 13 OPERATIONAL CHECK TO VERIFY CLOSING OF ISOLATION 8 I: 3200 FHA330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.21.00 * * * * * C O N T I N U E * * * * *VALVES OF THE MDCC.N OP 14 OPERATIONAL CHECK OF MORV. 9 I: 34000 FHA330-200FOR12 YE21.23.00 LAVATORY/GALLEY VENTILATIONDS 01 DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 7 I: 1200 FHPOST 46135NOTE 1R DS 02 DISCARD FILTER ELEMENT 6 I: 1200 FHA330-200NOTE 1POST 4620321.25.00 AIR CONDITIONING COMPARTMENT VENTILATIONOP 01 OPERATIONAL CHECK OF ABNORMAL VENTILATION WARNING 9 I: CALLDI 02 DETAILED INSPECTION OF TURBOFAN SUPPLY DUCT 9 I: 4 CALLGVI 03 GENERAL VISUAL INSPECTION OF PICCOLO TUBES 9 I: 2 C ZL-191-01-1 ALLZL-193-01-1ZL-195-02-104 TASK RESERVED21.26.00 AVIONICS EQUIPMENT VENTILATIONOP 01 OPERATIONAL CHECK OF OVERRIDE (OVRD) FUNCTION 9 I: CALLOP 02 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CALL(THIS TASK COVERS TASKS 73.25.00/01-G6,73.25.00/01-PW, 73.25.00/01-RR)OP 03 OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL 9 I: 2 CALLOP 04 OPERATIONAL CHECK OF COOLING EFFECT DETECTOR (AEVC 8 I: 10000 FHALLSYSTEM TEST)GVI 05 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-121-02-1 ALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.26.00 * * * * * C O N T I N U E * * * * *INSULATIONRS 06 CLEANING OF RELAY BOX VU PANELS GRIDS 9 I: 2 CALL21.27.00 AVIONICS EQUIPMENT GROUND COOLINGOP 01 OPERATIONAL CHECK OF FAULT WARNING 9 I: 2 CPOST 40063PRE 51336PRE 51337GVI 02 GENERAL VISUAL INSPECTION OF BLANKING PLATE 9 I: 4 C ZL-121-02-1 POST 40063INSULATIONPRE 51336PRE 51337OP 03 OPERATIONAL CHECK OF GRU START 9 I: 2 CPOST 46386PRE 51336PRE 5133721.28.00 LOWER DECK CARGO COMPARTMENT HEATING, VENTILATION AND COOLING(FWD, AFT AND BULK)OP 01 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 3200 FHALLISOLATION VALVES AND SHUT-OFF OF EXTRACTION FANS IN NOTE 24CASE OF SMOKE WARNING.(THIS TASK COVERS TASK 26.16.00/02)R OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 3200 FHA330-300COLD AIR VALVE IN CASE OF SMOKE WARNING NOTE 24POST 40097ORA330-200POST 45199ORA330-200FR OP 03 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FHA330-200LOWER DECK MOBILE CREW REST ISOLATION VALVES IN NOTE 24POST 40379CASE OF SMOKE WARNING.PRE 56296(THIS TASK COVERS TASK 26.18.00/05)ORA330-300POST 40379PRE 56296* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.28.00 * * * * * C O N T I N U E * * * * *R OP 04 OPERATIONAL CHECK OF HARDWIRED BACKUP TO VERIFY 9 I: 4 CA330-200CLOSING OF LOWER DECK MOBILE CREW REST ISOLATIONPOST 40379VALVESPRE 56296ORA330-300POST 40379PRE 56296OP 05 OPERATIONAL CHECK OF HARD WIRED BACKUP OF VENTILATION 9 I: 4 CALLCONTROLLER (TO VERIFY CLOSING OF ISOLATION VALVES ANDCOLD AIR VALVE)R DS 06 DISCARD FILTER ELEMENT OF BULK VIDEO COMPARTMENT 9 I: 2400 FHA330-200NOTE 1POST 46441ORA330-300POST 46441R OP 07 OPERATIONAL CHECK OF AUTOMATIC AND MANUAL SHUT OFF OF 9 I: 2 CA330-200BULK VIDEO COMPARTMENT VENTILATION AND ELECTRICALPOST 46441POWER AND CHECK NON RETURN VALVE IS IN CLOSEDORPOSITIONA330-300POST 4644121.31.00 PRESSURE CONTROL AND MONITORINGOP 01 OPERATIONAL CHECK OF MANUAL MODE 8 I: 20000 FHALLOP 02 OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN 9 I: 2 CALLDITCHING CONFIGURATIONOP 03 OPERATIONAL CHECK OF OUTFLOW VALVE OPENING (50%) BY 9 I: 2 CALLEMERGENCY RAM AIR SWITCHOP 04 OPERATIONAL CHECK OF LANDING FIELD ELEVATION SELECTOR 9 I: 2 CALLBY MEANS OF INITIATED TEST (VIA MCDU)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.31.00 * * * * * C O N T I N U E * * * * *FC 05 FUNCTIONAL CHECK OF POSITIVE AND NEGATIVE DELTA P 6,9 I: 24000 FHALLPROTECTION OF SAFETY VALVES OR6 YENOTE 2406 TASK DELETEDOP 07 OPERATIONAL CHECK OF NEGATIVE PRESSURE RELIEF VALVE 9 I: 4 CALLOP 08 OPERATIONAL CHECK OF POSITION INDICATION OF SAFETY 9 I: 4 CALLVALVESRS 09 REMOVE SAFETY VALVE FOR RESTORATION. 9 I: 50000 FHALLOR12 YE21.50.00 AIR COOLING TEMPERATURE CONTROLRS 01 CLEAN FLIGHT DECK TEMPERATURE SENSORS 7 I: CALLOP 02 OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM 9 I: 2 CALLOPENINGDI 03 DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS 9 I: 4 CALLFOR CONDITION AND OPERATIONDI 04 DETAILED INSPECTION OF LP GROUND AIR CHECK VALVE 9 I: 24000 FHALLFLAPPERS FOR CONDITION AND OPERATION.VC 05 VISUAL CHECK OF PACK AIR SUPPLY DUCTS, CLAMPS AND 9 I: 24000 FHALLBELLOWS (BETWEEN PACK OUTLET AND MIXER UNIT)DI 06 DETAILED INSPECTION OF PACK DOWNSTREAM CHECK VALVES 6,9 I: 24000 FHALLFLAPPERS FOR CONDITION AND OPERATIONGVI 07 GENERAL VISUAL INSPECTION OF TRIM AIR DUCTS BETWEEN 9 I: 4 C ZL-137-01-1 ALLFLOW CONTROL VALVES AND HOT AIR MANIFOLDS ZL-191-02-1ZL-193-02-1FC 08 REMOVE OZONE CONVERTER FOR FUNCTIONAL CHECK 9 I: 2 CPOST 40219NOTE 1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section21.50.00 * * * * * C O N T I N U E * * * * *R RS 09 CLEANING OF CABIN TEMPERATURE SENSORS, SENSE LINES 7 I: 2 AA330-200AND INLETS NOTE 1PRE 43750PRE 44729ORA330-300PRE 43750PRE 44729R DS 10 DISCARD CABIN TEMPERATURE SENSOR FILTERS 7 I: 1 AA330-200NOTE 1POST 43750ORA330-200POST 44729ORA330-300POST 43750ORA330-300POST 4472911 TASK RESERVEDDS 12 DISCARD FLOW CONTROL VALVE FILTERS 7 I: 2000 FCPOST 50213NOTE 1GVI 13 GENERAL VISUAL INSPECTION OF HEATSHIELDS FOR 8 I: 20000 FHPOST 49520CONDITION AND VISIBLE DAMAGERS 14 CLEANING AND DETAILED INSPECTION FOR EROSION OF PACK 7 I: 2 CALLWATER INJECTOR NOZZELS.DI 15 DETAILED INSPECTION OF EMERGENCY RAM AIR CHECK VALVE; 9 I: 4 CALLSKIN VALVE FLAPPERS FOR CONDITION AND OPERATION.N RS 16 CLEANING OF COURIER AREA AND MDCC TEMPERATURE 7 I: 1600 FHA330-200FSENSORS, SENSE LINES & INLETS. NOTE 1* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR CONDITIONING SECTION: C-21PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section22.00.00 AUTO FLIGHT22.10.00 AUTOPILOT/FLIGHT DIRECTOROP 01 OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION 9 I: 2 CALLOP 02 OPERATIONAL CHECK OF AUTOPILOT ENGAGEMENT AND LOCKING 9 I: 4 CALLDEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS22.30.00 AUTOTHRUSTOP 01 OPERATIONAL CHECK OF A/THR ISOLATION FROM ENGINE 9 I: 4 CALLCONTROL22.60.00 FLIGHT ENVELOPENO TASK SELECTED22.70.00 FLIGHT MANAGEMENTOP 01 OPERATIONAL CHECK OF BACK-UP NAVIGATION FUNCTION 9 I: CALLOP 02 OPERATIONAL CHECK OF MCDU 3 TRANSFER 9 I: CALLOP 03 OPERATIONAL CHECK OF MCDU ANNUNCIATORS 9 I: CALLOP 04 OPERATIONAL CHECK OF FM SOURCE SWITCHING 9 I: 2 CALL22.90.00 AUTOFLIGHT SYSTEM BITENO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AUTO FLIGHT SECTION: C-22PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section23.00.00 COMMUNICATIONS23.11.00 HF SYSTEM (MOD 40068, 40069)NO TASK SELECTED23.12.00 VHF SYSTEMNO TASK SELECTED23.24.00 AIRCRAFT COMMUNICATIONS ADDRESSING & REPORTING SYSTEM (ACARS)(MOD 40065)NO TASK SELECTED23.28.00 SATELLITE COMMUNICATIONNO TASK SELECTED23.33.00 IN-FLIGHT ENTERTAINMENT SYSTEM (IFES)OP 01 OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION 9 I: 2 CIF IFESFROM FLIGHT DECK (IF INSTALLED) AND CABIN.INSTALLEDDS 02 DISCARD IFE-RACK FILTERS. 9 I: 2400 FHIF IFE-RACKSWITHAIR-FILTERSINSTALLEDR RS 03 CLEANING OF VENTILATION GRIDS AND VENTILATOR HOUSING 9 I: 10000 FHIF VCC(IF INSTALLED) FROM IFE COMPONENTS INSTALLEDORIN THE CABIN (VCC/RCC)RCC INSTALLED23.39.01 SATELLITE TV TRANSCEIVER SYSTEM TAILWIND (TW560) ANDPANASONIC (IDTV)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section23.39.01 * * * * * C O N T I N U E * * * * *R DS 01 DISCARD ALL FILTER ELEMENTS ON TAILWIND SYSTEM 7 I: AA330-200/300IF TAILWINDSYSTEMINSTALLED23.39.02 SATELLITE DATA TRANSCEIVER SYSTEM CONNEXION BY BOEING (CBB).OP 01 OPERATIONAL CHECK OF CONNEXION BY BOEING SYSTEM POWER 9 I: 4 CIF CBB SYSTEMOFF PROCEDURE.INSTALLEDOP 02 OPERATIONAL CHECK OF COOLING LOSS DETECTION OF 9 I: 4 CIF CBB SYSTEMCONNEXION BY BOEING SYSTEM.INSTALLED23.42.00 COCKPIT TO GROUND CREW CALL SYSTEMNO TASK SELECTED23.51.00 AUDIO MANAGEMENT (INTEGRATING/FLIGHT INTERPHONE/SELCAL/CALL)OP 01 OPERATIONAL CHECK OF OXYGEN MASK MICROPHONE 9 I: CALLOP 02 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING. 9 I: CALL(COVERED BY MSI 23-71-00, TASK NO1)OP 03 OPERATIONAL CHECK OF CAPTAIN AND F/O ACP SWITCHING TO 9 I: 2 CALLTHIRD ACP23.61.00 STATIC DISCHARGERFC 01 CHECK RESISTANCE FROM THE DISCHARGER TO THE BASE 9 I: CALL(RETAINER) AND FROM THE BASE (RETAINER) TO THEAIRCRAFT STRUCTUREGVI 02 GENERAL VISUAL INSPECTION OF STATIC DISCHARGER. 9 I: CALL23.71.00 COCKPIT VOICE RECORDEROP 01 OPERATIONAL CHECK OF CVR AND CVR CHANNEL RECORDING 9 I: CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section23.71.00 * * * * * 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: CALLTIME DELAY RELAYDS 03 DISCARD ULB BATTERY 9 I: VRALLOP 04 OPERATIONAL CHECK OF THE ULB 9 I: VRALL23.72.00 COCKPIT DOOR SURVEILLANCE SYSTEM (CDSS)NO TASK SELECTED23.73.00 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)R OP 01 OPERATIONAL CHECK OF CABIN SIGNS VIA MCDU 9 I: 2 AA330-200NOTE 26PRE 45556ORA330-200PRE 48823ORA330-300PRE 44058PRE 45556ORA330-300PRE 48823R OP 02 OPERATIONAL CHECK OF LOUDSPEAKERS VIA MCDU 9 I: 1 CA330-200NOTE 26ORA330-300R OP 03 OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, 9 I: 2 CA330-200DEUS-A CUT OFF FUNCTIONORA330-300OP 04 OPERATIONAL CHECK OF EVAC FUNCTION 9 I: 2 CIF EVACINSTALLEDR OP 05 OPERATIONAL CHECK OF HOT BATTERY BUS POWERED CIDS 9 I: 20000 FHPOST 40823OPERATIONPRE 49314* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section23.73.00 * * * * * C O N T I N U E * * * * *06 TASK DELETED07 TASK DELETEDOP 08 OPERATIONAL CHECK OF LDL/LDF SIGNS VIA MCDU 9 I: 4 CIF LDL/LDFNOTE 26INSTALLEDR OP 09 OPERATIONAL CHECK OF EMERGENCY CABIN ALERT SYSTEM 9 I: 2 CPOST 50156(ECAS)ORPOST 50157N OP 10 OPERATIONAL CHECK OF BATTERY POWERED CIDS PA 9 I: 20000 FHPOST 49314OPERATION23.73.01 CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS)N OP 01 OPERATIONAL CHECK OF DEUS ESSENTIAL POWER SUPPLY, AND 9 I: 20000 FHA330-200FDEUS-A CUT OFF FUNCTIONN OP 02 OPERATIONAL CHECK OF EVAC FUNCTION 9 I: 20000 FHA330-200FN OP 03 OPERATIONAL CHECK OF BATTERY POWERED CIDS PA 9 I: 20000 FHA330-200FOPERATION23.81.00 RADIO MANAGEMENTOP 01 OPERATIONAL CHECK OF RMP LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF RADIO NAVIGATION BACK-UP MODE 9 I: CALL* * * * * E N D * * * * *ISSUE: JUL 01/10 COMMUNICATIONS SECTION: C-23PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section24.00.00 ELECTRICAL POWER24.20.00 AC GENERATIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(THIS TASK COVERS TASKS 24.50.00/01 AND 24.60.00/01) NOTE 24OP 02 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FHALLSUPPLY NOTE 24(THIS TASK COVERS TASK 24.30.00/01)03 TASK DELETEDOP 04 OPERATIONAL CHECK OF LIGHTS. 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)DS 05 DRAIN IDG OIL SYSTEM, DISCARD SCAVENGE FILTER ELEMENT 7 I: AALLAND REPLENISHFC 06 CHECK TORQUE OF IDG QUICK-ATTACH-DETACH TENSION BOLT 9 I: 2100 FHALLOP 07 OPERATIONAL CHECK OF AC GENERATION SIDE 1 AND SIDE 2 9 I: CALLISOLATIONOP 08 OPERATIONAL CHECK OF EMERGENCY GCU FROM CMS 9 I: CALLOP 09 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION MANUAL 9 I: CALLSWITCHINGOP 10 OPERATIONAL CHECK OF EMERGENCY GENERATOR AUTOMATIC 8 I: 18 MOALLCONNECTION NOTE 24OP 11 OPERATIONAL CHECK OF EMERGENCY GENERATOR MANUAL 8 I: 18 MOALLCONNECTION NOTE 24OP 12 OPERATIONAL CHECK OF CSM/G DISCONNECTION WITH 8 I: 18 MOALLSIMULATED ENGINES FLAMED OUT CONDITION AND SLATSEXTENDEDRS 13 CLEAN IDG OIL COOLER 7 I: 4 CALLOP 14 OPERATIONAL CHECK OF IDG DISCONNECT FUNCTION 9 I: 4 CALLOP 15 OPERATIONAL CHECK OF GENERATOR SHUT-DOWN WHEN ENGINE 9 I: 60 MOALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section24.20.00 * * * * * C O N T I N U E * * * * *FIRE HANDLE IS OPERATED(COVERED BY MSI 26-21-00, TASK NO3).16 TASK DELETEDOP 17 OPERATIONAL CHECK OF AC ESSENTIAL GENERATION 9 I: CALLAUTOMATIC SWITCHING18 TASK RESERVED24.30.00 DC GENERATIONOP 01 OPERATIONAL CHECK OF STATIC INVERTER AND DC ESS. BUS 8 I: 800 FHALLSUPPLY (COVERED BY MSI 24-20-00, TASK NO2). NOTE 2402 TASK DELETEDR RS 03 REMOVE BATTERIES (1, 2, APU) FOR OVERHAUL 6 I: VRALLOP 04 OPERATIONAL CHECK OF DC MAIN GENERATION SWITCHING 9 I: CALLOP 05 OPERATIONAL CHECK OF DC ESSENTIAL GENERATION 9 I: CALLSWITCHINGOP 06 OPERATIONAL CHECK OF DC BAT BUS AND DC ESS BUS 8 I: 800 FHALLISOLATION24.40.00 EXTERNAL POWER01 TASK DELETED24.50.00 AC ELECTRICAL LOAD DISTRIBUTIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(COVERED BY MSI 24-20-00, TASK NO1). NOTE 24OP 02 OPERATIONAL CHECK OF COMMERCIAL LOAD SHEDDING 9 I: CALLOP 03 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MOALL(THIS TASK COVERS TASK 24.60.00/02)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section24.50.00 * * * * * C O N T I N U E * * * * *OP 04 OPERATIONAL CHECK OF 905XP BUSBAR SHEDDING IN 9 I: 2 CALLEMERGENCY CONFIGURATIONOP 05 OPERATIONAL CHECK OF LEFT AND RIGHT FUEL PUMP 2 8 I: 18 MOALLSHEDDING IN LAND RECOVERY CONFIGURATION NOTE 24OP 06 OPERATIONAL CHECK AFT APU PUMP SHEDDING IN LAND 8 I: 18 MOPOST 44504RECOVERY CONFIGURATIONPOST 4460324.60.00 DC ELECTRICAL LOAD DISTRIBUTIONOP 01 OPERATIONAL CHECK OF EMERGENCY GENERATION SYSTEM 8 I: 800 FHALL(COVERED BY MSI 24-20-00, TASK NO1). NOTE 24OP 02 OPERATIONAL CHECK OF LAND RECOVERY CONFIGURATION 8 I: 18 MOALL(COVERED BY MSI 24-50-00, TASK NO3).* * * * * E N D * * * * *ISSUE: JUL 01/10 ELECTRICAL POWER SECTION: C-24PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.00.00 EQUIPMENT/FURNISHINGS25.11.00 COCKPIT SEATSDI 01 DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT 8 I: 6 YEALLATTACHMENTFC 02 FUNCTIONAL CHECK OF HORIZONTAL/VERTICAL MECHANICAL 6,9 I: CALLCONTROL CABLE ADJUSTMENT OF COCKPIT SEATS25.21.00 PASSENGER COMPARTMENT SEATSGVI 01 GENERAL VISUAL INSPECTION OF SEAT TO FLOOR ATTACHMENT 8 I: 36 MOALLGVI 02 GENERAL VISUAL INSPECTION OF LOWER SEAT STRUCTURE, 8 I: 36 MOALLBAGGAGE RESTRAINT BAR, BACKREST AND BACKREST SUPPORTOP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MOALLBELT ATTACHMENTSR OP 04 OPERATIONAL CHECK OF ELECTRONIC CIRCUIT OF THE 8 I: VRIF INFLATABLEINFLATABLE RESTRAINT SYSTEM.RESTRAINTSYSTEMINSTALLEDRS 05 REMOVE SEATBELT SYSTEM FOR RESTORATION OF AIRBAG AND 7,8 I: VRIF INFLATABLEDISCARD BATTERY, HOSE, SQUIB AND GAS STORAGERESTRAINTACCORDING TO CMM.SYSTEMINSTALLED25.22.00 CABIN ATTENDANT SEATSR GVI 01 GENERAL VISUAL INSPECTION OF SEAT ATTACHMENT POINTS. 8 I: 36 MOA330-200ORA330-300ORA330-200FIF CASINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.22.00 * * * * * C O N T I N U E * * * * *R GVI 02 GENERAL VISUAL INSPECTION OF SEAT STRUCTURE. 8 I: 36 MOA330-200ORA330-300ORA330-200FIF CASINSTALLEDR OP 03 OPERATIONAL CHECK AND VISUAL CHECK OF SEAT BELTS AND 8 I: 36 MOA330-200BELT ATTACHMENTSORA330-300ORA330-200FIF CASINSTALLED25.23.44 LININGS AND FURNISHINGS (DADO PANELS)R VC 01 VISUAL CHECK TO ENSURE THAT ALL DECOMPRESSION PANELS 8 I: 18 MOA330-200IN CABIN ARE CLOSEDORA330-300R OP 02 OPERATIONAL CHECK OF CABIN DECOMPRESSION PANELS 9 I: 4 CA330-200OPENINGORA330-30025.24.00 OVERHEAD STOWAGE COMPARTMENTSNO TASK SELECTED25.27.00 DOOR AREA HEATING SYSTEM* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.27.00 * * * * * C O N T I N U E * * * * *R OP 01 OPERATIONAL CHECK OF THE DOOR AREA HEATING SYSTEM BY 9 I: 2 CA330-200USING THE TEST BUTTON ON EACH CONTROL UNIT.POST 45670PRE 47423PRE 51617ORA330-200POST 45670PRE 56746ORA330-300POST 45670PRE 47423PRE 51617ORA330-300POST 45670PRE 5674625.30.00 BUFFET AND GALLEYDS 01 DISCARD GALLEY AIR EXTRACTION FILTER ELEMENT 9 I: 1400 FHALL02 TASK DELETEDDI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 CALLPOINTS (COVERED BY SSI ́S 53.11.72, 53.21.34,53.31.70AND 53.41.59).04 TASK DELETED05 TASK RESERVED25.34.00 GALLEY COOLINGRS 01 CLEAN AIR CHILLER CONDENSER AIR FILTER. 7 I: 1400 FHIF AIR CHILLERNOTE 1SYSTEMINSTALLED02 TASK RESERVED03 TASK RESERVED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.34.00 * * * * * C O N T I N U E * * * * *RS 04 CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES 7 I: 1400 FHIF AIR CHILLERIN THE GALLEY CABINET. NOTE 1SYSTEM ANDGALLEY WITHGRILLESINSTALLED25.40.00 LAVATORIESDI 01 DETAILED INSPECTION OF WASTE COMPARTMENT FOR FIRE 9 I: NRALLCONTAINMENT CAPABILITY. OR1 CNOTE 8OP 02 OPERATIONAL CHECK OF WASTE COMPARTMENT FLAP 9 I: NRALLOR1 CNOTE 8DI 03 DETAILED INSPECTION OF UPPER AND LOWER ATTACHMENT 9 I: 4 CALLPOINTS (COVERED BY SSI ́S 53.11.72, 53.21.34, 53.31.70AND 53.41.59).04 TASK DELETED25.47.00 LOWER DECK LAVATORIESRS 01 CLEANING OF DRAIN OPENINGS 9 I: CPOST 46203VC 02 VISUAL CHECK OF LDL RAPID DECOMPRESSION PANELS 8 I: 800 FHPOST 4620325.51.00 LOWER DECK CARGO LOADING SYSTEMR OP 01 OPERATIONAL CHECK OF POWER DRIVE UNITS 9 I: CA330-200NOTE 11PRE 55381ORA330-300PRE 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *R DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA330-200PRE 55381ORA330-300PRE 55380R DI 03 REMOVE CREW REST ROOM CONTAINER LATCHES AT C53.7 FOR 8 I: 34000 FHA330-200DETAILED INSPECTION.POST 40611R GVI 04 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES 9 I: A ZL-131-01-1 A330-200ZL-151-01-1 PRE 55381ORA330-300PRE 55380R GVI 05 GENERAL VISUAL INSPECTION OF OVERRIDEABLE Y-DOOR SILL 9 I: A ZL-131-01-1 A330-200LATCHES ZL-151-01-1 PRE 55381ORA330-300PRE 55380R GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS 9 I: A ZL-131-01-1 A330-200ZL-151-01-1 PRE 55381ORA330-300PRE 55380R GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS INCLUDING 9 I: A ZL-131-01-1 A330-200TRANSPORT ROLLER. ZL-151-01-1 PRE 55381NOTE 11ORA330-300PRE 55380R DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 300 FCA330-200WEAR AND DAMAGE. NOTE 11PRE 55381ORA330-300PRE 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *R GVI 09 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS 9 I: 4 A ZL-131-01-1 A330-200NOTE 11 ZL-151-01-1 PRE 55381ORA330-300PRE 55380R GVI 10 GENERAL VISUAL INSPECTION OF XZ LATCHES 8 I: 3200 FHA330-200NOTE 11PRE 55381ORA330-300PRE 55380R GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AT C20, C39, 9 I: 4 A ZL-131-01-1 A330-200C53.2, C65 AND C68 ZL-151-01-1 PRE 55381NOTE 11ORA330-300PRE 55380R GVI 12 GENERAL VISUAL INSPECTION OF FIXED, RETRACTABLE AND 9 I: 4 A ZL-131-01-1 A330-200OVERRIDEABLE YZ-LATCHES ZL-151-01-1 PRE 55381NOTE 11ORA330-300PRE 55380R GVI 13 GENERAL VISUAL INSPECTION OF Y-GUIDE ROLLERS, 9 I: C ZL-131-01-1 A330-200AUTOMATIC Z-GUIDES, GUIDE RAILS, YZ-LATCH GUIDE ZL-151-01-1 PRE 55381ROLLERS, XY-ENTRANCE GUIDE ASSEMBLIES, Y-GUIDES ANDORY-GUIDE ACTUATION MECHANISMS (AND X-GUIDES WITH MODA330-30040208)PRE 55380NOTE 1114 TASK RESERVED15 TASK DELETED16 TASK RESERVEDR GVI 17 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-131-01-1 A330-200ZL-151-01-1 PRE 55381ORA330-300PRE 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.00 * * * * * C O N T I N U E * * * * *GVI 18 GENERAL VISUAL INSPECTION OF PALLET STOP. 9 I: 4 A ZL-131-01-1 A330-300POST 42261N OP 19 OPERATIONAL CHECK OF BRAKING ROLLER. 9 I: 2 CA330-200PRE 55381ORA330-300PRE 55380N OP 20 OPERATIONAL CHECK OF CENTERLINE GUIDE SWIVEL NOSES. 9 I: 4 CA330-200POST 49610ORA330-300POST 5056725.51.01 ADVANCED LOWER DECK CARGO LOADING SYSTEMN OP 01 OPERATIONAL CHECK OF SWIVEL NOSE AT XZ-LATCHES EG 9 I: 4 CA330-200F(ENTRANCE GUIDE) AND SWIVEL NOSES AT OVERRIDEABLEORCENTER LATCHES. (NOTE 11)A330-200POST 55381ORA330-300POST 55380N DI 02 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA330-200FORA330-200POST 55381ORA330-300POST 55380N DI 03 REMOVE LOWER DECK-MOBIL CREW REST CONTAINER LATCHES 8 I: 34000 FHA330-200FOR DETAILED INSPECTION.POST 56839* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.01 * * * * * C O N T I N U E * * * * *N OP 04 OPERATIONAL CHECK OF BRAKING ROLLER AND SWIVEL 9 I: 2 CA330-200FCASTER. (NOTE 11)ORA330-200POST 55381ORA330-300POST 55380N GVI 05 GENERAL VISUAL INSPECTION OF YZ-DOOR SILL LATCHES AND 9 I: A ZL-131-01-1 A330-200FOVERRIDEABLE ARO DEVICES. ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N GVI 06 GENERAL VISUAL INSPECTION OF BALL UNITS, BALL MATS 9 I: A ZL-131-01-1 A330-200FAND BALL STRIPS. ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N GVI 07 GENERAL VISUAL INSPECTION OF ROLLER TRACKS, TRANSPORT 9 I: A ZL-131-01-1 A330-200FROLLERS. (NOTE 11) ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N DI 08 DETAILED INSPECTION OF POWER DRIVE UNIT ROLLER FOR 9 I: 1500 FCA330-200FWEAR AND DAMAGE. (NOTE 11) OROR18 MOA330-200POST 55381ORA330-300POST 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.01 * * * * * C O N T I N U E * * * * *N GVI 09 GENERAL VISUAL INSPECTION OF OVERRIDEABLE CENTER 9 I: 4 A ZL-131-01-1 A330-200FLATCHES AND SPLITTER. (NOTE 11) ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N GVI 10 GENERAL VISUAL INSPECTION OF XZ-LATCHES. (NOTE 11) 8 I: 3200 FHA330-200FORA330-200POST 55381ORA330-300POST 55380N GVI 11 GENERAL VISUAL INSPECTION OF XZ-ENDSTOPS AND 9 I: 4 A ZL-131-01-1 A330-200FXZ-LATCHES EG (ENTRANCE GUIDE). (NOTE 11) ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N GVI 12 GENERAL VISUAL INSPECTION OF FIXED YZ-LATCHES AND 9 I: 4 A ZL-131-01-1 A330-200FYZ-LATCHES WITH TRANSPORT ROLLER (MOD 56837). ZL-151-01-1 OR(NOTE 11)A330-200POST 55381ORA330-300POST 55380N GVI 13 GENERAL VISUAL INSPECTION OF YZ LATCH-GUIDE ROLLERS, 9 I: C ZL-131-01-1 A330-200FLATERAL ENTRANCE GUIDE, Y-GUIDE 42 L, SCUFF PLATE ZL-151-01-1 ORROLLER, SIDE GUIDES, ENTRANCE ROLLER, DOOR SILL LATCHA330-200SUPPORT ROLLER AND OVERROLLABLE GUIDE (MOD 56837).POST 55381(NOTE 11)ORA330-300POST 55380* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.51.01 * * * * * C O N T I N U E * * * * *N GVI 14 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS. 9 I: C ZL-131-01-1 A330-200FZL-151-01-1 ORA330-200POST 55381ORA330-300POST 55380N GVI 15 GENERAL VISUAL INSPECTION OF BRAKING ROLLERS AND 9 I: 4 A ZL-131-01-1 A330-200FSWIVEL CASTERS. (NOTE 11) ZL-151-01-1 ORA330-200POST 55381ORA330-300POST 5538025.52.00 LOWER DECK FORWARD/AFT CARGO COMPARTMENTVC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING 8 I: 8 DYALLSTRIPS, PROTECTION PLATES, CENTER LINE COVER PLATESAND ACCESS DOORS.NOTE 11VC 02 VISUAL CHECK OF DECOMPRESSION PANELS 8 I: 8 DYALLNOTE 11R VC 03 VISUAL CHECK OF DRAIN FUNNELS AT THE END OF THE 9 I: AALLROLLER TRACKS AND BELOW THE PDUS FOR EVIDENCE OFCLOGGING OR OBSTRUCTION AND CLEAN AS NECESSARY.(NOTE 11)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.52.00 * * * * * C O N T I N U E * * * * *N OP 04 OPERATIONAL CHECK OF AIR STOP VALVES FOR HEATED 9 I: 4 CA330-200FDRAINAGE SYSTEM.ORA330-200POST 45395ORA330-200POST 56835ORA330-300POST 43719ORA330-300POST 56834N GVI 05 GENERAL VISUAL INSPECTION OF THE DRAINAGE SYSTEM 9 I: 4 C ZL-133-01-1 ALLINSTALLATION. ZL-153-01-1ZL-153-01-2ZL-163-01-1ZL-163-01-2N VC 06 VISUAL CHECK OF DRAIN PANS BELOW BALL MAT AREA FOR 9 I: AA330-200FEVIDENCE OF CLOGGING OR OBSTRUCTION AND CLEAN ASORNECESSARY.A330-200POST 55381ORA330-300POST 5538025.54.00 LOWER DECK BULK CARGO COMPARTMENTVC 01 VISUAL CHECK OF LININGS, FLOOR PANELS, SEALING STRIPS 8 I: 8 DYALLAND ACCESS DOOR AT C73VC 02 VISUAL CHECK OF DECOMPRESSION PANELS 8 I: 8 DYALLGVI 03 GENERAL VISUAL INSPECTION OF TIE-DOWN POINTS 9 I: C ZL-161-01-1 ALLR DI 04 DETAILED INSPECTION OF DIVIDER NETS, NET 9 I: CALLATTACHMENT POINTS, NET CONNECTING DEVICES AND TENSIONBUCKLESR DI 05 DETAILED INSPECTION OF NET SCREENS, NET SCREEN 9 I: CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 11APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.54.00 * * * * * C O N T I N U E * * * * *ATTACHMENT POINTS AND TENSION BUCKLESR DI 06 DETAILED INSPECTION OF SCREEN DECOMPRESSION 9 I: CALLTARPAULINS25.55.00 MAIN DECK CARGO COMPARTMENT (INCLUDING DRAINAGE AND BARRIERWALL)N DI 01 DETAILED INSPECTION OF BARRIER WALL, BARRIER WALL 8 I: 1000 FHA330-200FATTACHMENTS, DECOMPRESSION PANEL, SMOKE CURTAIN AND ORACCESS DOOR SEALING. 3 MON GVI 02 GENERAL VISUAL INSPECTION OF MDCC LINING. 9 I: A ZL-231-03-1 A330-200FZL-241-03-1ZL-251-03-1ZL-261-03-1ZL-271-03-1N GVI 03 GENERAL VISUAL INSPECTION OF THE DRAINAGE SYSTEM 9 I: 4 C ZL-131-02-3 A330-200FINSTALLATION. ZL-133-01-1ZL-151-02-5ZL-153-01-1ZL-231-04-1ZL-241-04-1ZL-251-04-1ZL-261-04-1ZL-271-04-1N GVI 04 GENERAL VISUAL INSPECTION OF THE PROTECTION ANGLE AT 9 I: A ZL-231-03-1 A330-200FTHE BARRIER WALL AND THE REAR BULK HEAD. ZL-271-03-1N VC 05 VISUAL CHECK OF THE DRAIN FUNNELS WITHIN THE DRAIN 9 I: 1000 FHA330-200FPANS FOR CLOGGING OR OBSTRUCTION AND CLEAN ASNECESSARY.25.56.00 MAIN DECK CARGO LOADING SYSTEMN OP 01 OPERATIONAL CHECK OF BRAKING ROLLER. 9 I: 36 MOA330-200FN GVI 02 GENERAL VISUAL INSPECTION OF XZ-LATCHES. 8 I: 3200 FHA330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 12APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.56.00 * * * * * C O N T I N U E * * * * *N DI 03 REMOVE XZ-LATCHES FOR DETAILED INSPECTION. 8 I: 34000 FHA330-200FN OP 04 OPERATIONAL CHECK OF XZ-ENDSTOP SWIVEL NOSES. 9 I: 4 CA330-200FPOST 58552N GVI 05 GENERAL VISUAL INSPECTION OF BALL TRANSFER UNITS, 9 I: 1000 FH ZL-231-03-1 A330-200FBALL MATS.N GVI 06 GENERAL VISUAL INSPECTION OF LOADING BRIDGE. 9 I: 1000 FH ZL-231-03-1 A330-200FN GVI 07 GENERAL VISUAL INSPECTION XZ-ENDSTOPS. 9 I: 4 A ZL-231-03-1 A330-200FZL-271-03-1N GVI 08 GENERAL VISUAL INSPECTION OF GUIDING COMPONENTS. 9 I: 4 A ZL-231-03-1 A330-200FZL-241-03-1ZL-251-03-1ZL-261-03-1ZL-271-03-1N GVI 09 GENERAL VISUAL INSPECTION OF SPLITTER. 9 I: 4 A ZL-231-03-1 A330-200FZL-241-03-1 POST 58204N GVI 10 GENERAL VISUAL INSPECTION OF ROLLER TRAYS, TRANSPORT 9 I: 1000 FH ZL-231-03-1 A330-200FROLLERS AND BRAKING ROLLERS. ZL-241-03-1ZL-251-03-1ZL-261-03-1ZL-271-03-1N GVI 11 GENERAL VISUAL INSPECTION OF FIXED YZ-LATCHES, 9 I: 4 A ZL-231-03-1 A330-200FOVERRIDEABLE CENTER LATCHES, RETRACTABLE SIDE ZL-241-03-1RESTRAINT ASSEMBLIES. ZL-251-03-1ZL-261-03-1ZL-271-03-1N GVI 12 GENERAL VISUAL INSPECTION OF OVERRIDEABLE ANTI ROLL 9 I: 4 A ZL-231-03-1 A330-200FOUT DEVICE.25.61.00 COCKPIT ESCAPE FACILITIESVC 01 VISUAL CHECK OF EMERGENCY ESCAPE ROPE AND ROPE 8 I: 6 YEALLATTACHMENTISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 13APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.62.00 CABIN ESCAPE FACILITIESFC 01 REMOVE SLIDE/RAFT BOTTLE FOR HYDROSTATIC TEST 6 I: NRALLORVRR RS 02 RESTORATION OF LIFE RAFTS BY REMOVAL AND REPLACEMENT 8 I: VRALLWITH OVERHAULED.R OP 03 OPERATIONAL CHECK OF SLIDE/RAFT DEPLOYMENT - I: NRALLORVRNOTE 1004 TASK RESERVED05 TASK RESERVED06 TASK RESERVED07 TASK RESERVED25.65.32 EMERGENCY LOCATOR TRANSMITTER (PORTABLE)R RS 01 REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER 9 I: VRIF SURVIVAL ELT(ELT(S)) FOR WORKSHOP CHECK.INSTALLED25.65.34 EMERGENCY VHF TRANSCEIVERFC 01 REMOVE EMERGENCY VHF TRANSCEIVER FOR SHOP INSPECTION 9 I: VRIF EMERGENCYORVHF TRANSCEIVER24 MOINSTALLED25.65.35 EMERGENCY LOCATOR TRANSMITTER SYSTEMR OP 01 OPERATIONAL CHECK OF AUTOMATIC FIXED EMERGENCY 8 I: 18 MOIF AUTOMATICLOCATOR TRANSMITTER (ELT(AF)) SYSTEM BY MANUALFIXED ELTACTIVATION.INSTALLEDR RS 02 REMOVE AUTOMATIC FIXED EMERGENCY LOCATOR TRANSMITTER 8 I: VRIF AUTOMATIC(ELT(AF)) FOR RESTORATION IN WORKSHOP INCLUDINGFIXED ELTBATTERY REPLACEMENT AND CHECK OF AUTOMATIC ELTINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 14APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.65.35 * * * * * C O N T I N U E * * * * *ACTIVATION.25.65.51 MEGAPHONER DS 01 DISCARD MEGAPHONE BATTERIES 9 I: VRA330-200ORA330-300ORA330-200FIF MEGAPHONEINSTALLEDR OP 02 OPERATIONAL CHECK OF MEGAPHONE 9 I: CA330-200ORA330-300ORA330-200FIF MEGAPHONEINSTALLED25.66.52 LIFE VESTR RS 01 RESTORATION OF LIFE VESTS BY REMOVAL AND REPLACEMENT 9 I: VRALLWITH OVERHAULED.25.74.00 CREW REST ROOM (CABIN)DI 01 DETAILED INSPECTION OF SEAT BELTS, BELT ATTACHMENTS 8 I: 36 MOIF FCRCAND LOWER BUNK STRUCTURE.INSTALLEDGVI 02 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-221-02-1 IF FCRCATTACHMENT POINTS OF THE CREW REST ROOM (REST ROOM ZL-223-01-1 INSTALLEDREMOVED).25.75.00 CREW REST ROOM (UNDERFLOOR)OP 01 OPERATIONAL CHECK OF EMERGENCY EXIT HATCH OPENING 8 I: 18 MOIF LDMCRFROM INSIDE AND FROM OUTSIDEINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 15APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section25.75.00 * * * * * C O N T I N U E * * * * *DI 02 DETAILED INSPECTION OF BED BELTS AND BELT 8 I: 36 CRR MOIF LDMCRATTACHMENTS ON CREW REST BUNKSINSTALLED03 TASK RESERVEDVC 04 VISUAL CHECK OF CARGO COMPARTMENT CEILING WELL, 8 I: 6 YEIF LDMCRINTERFACE LININGS AND OF THE OUTSIDE OF THE CONTAINERINSTALLEDR GVI 05 GENERAL VISUAL INSPECTION OF UPPER AND LOWER 9 I: 8 C ZL-251-02-1 IF LDMCRATTACHMENT POINTS OF THE STAIRHOUSE (STAIRHOUSE ZL-253-01-1 INSTALLEDREMOVED).OP 06 OPERATIONAL CHECK OF DOOR HINGE AND LOCK 9 I: 36 CRR MOIF LDMCR ANDLDL INSTALLED07 TASK RESERVED08 TASK RESERVED09 TASK RESERVED10 TASK RESERVED11 TASK RESERVED12 TASK RESERVEDVC 13 VISUAL CHECK OF HATCH SEAL, DOOR SEALS AND BELLOW 8 I: 36 MOIF LDMCRSEALS.INSTALLED* * * * * E N D * * * * *ISSUE: JUL 01/10 EQUIPMENT/FURNISHINGS SECTION: C-25PAGE 16APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.00.00 FIRE PROTECTION26.12.00 ENGINE FIRE AND OVERHEAT DETECTIONNO TASK SELECTED26.13.00 APU FIRE AND OVERHEAT DETECTIONOP 01 OPERATIONAL CHECK OF APU FIRE AND OVERHEAT DETECTION 9 I: 8000 FHALLLOOPS(COVERED BY MSI 26.22.00, TASK NO1)26.15.00 AVIONICS COMPARTMENT SMOKE DETECTIONOP 01 OPERATIONAL CHECK OF AVIONICS COMPARTMENT SMOKE 9 I: 4 AALLDETECTION BY PTT NOTE 5RS 02 REMOVE AVIONICS SMOKE DETECTION PICCOLO TUBES FOR 8 I: 36 MOALLCLEANING03 TASK DELETED26.16.00 LOWER DECK CARGO COMPARTMENT SMOKE DETECTIONOP 01 OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE 9 I: 4 AALLDETECTION BY PTT NOTE 5OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 9 I: CALLCARGO COMPARTMENT ISOLATION VALVES(COVERED BY MSI 21-28-00, TASK NO1)03 TASK DELETED26.17.00 LAVATORY SMOKE DETECTION01 TASK DELETED26.18.00 AUXILIARY AREAS SMOKE DETECTION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.18.00 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF LDMCR SMOKE DETECTION BY PTT. 9 I: 2 APOST 55244NOTE 25ORPOST 52339RS 02 REMOVE AND CLEAN LDMCR SMOKE DETECTORS. 6 I: 72 CRR MOPOST 55244ORPOST 52339OP 03 OPERATIONAL CHECK OF LDMCR STAIRHOUSE SMOKE DETECTION 9 I: CPOST 55244SYSTEM BY MCDU.ORPOST 52339OP 04 OPERATIONAL CHECK OF FCRC SMOKE DETECTION SYSTEM BY 9 I: CPOST 51302MCDU.ORPOST 53391OP 05 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF 8 I: 1600 FHPOST 55244LDMCR ISOLATION VALVE (IN CASE OF FIRE IN LDMCRORSTAIRHOUSE OR CREW REST ROOM)POST 52339(COVERED BY MSI 21-28-00, TASK NO 3)OP 06 OPERATIONAL CHECK OF LDMCR SMOKE DETECTORS WITH 9 I: 18 CRR MOPOST 55244AEROSOL.ORPOST 5233907 TASK DELETED08 TASK RESERVED09 TASK RESERVEDOP 10 OPERATIONAL CHECK OF VCC SMOKE DETECTION BY MCDU. 8 I: 18 MOPOST 49304ORPOST 50091ORPOST 52720ORPOST 50995ORPOST 51312ORPOST 52146* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.18.00 * * * * * C O N T I N U E * * * * *RS 11 REMOVE VCC PICCOLO TUBES FOR CLEANING. 7 I: 18000 FHPOST 49304ORPOST 50091ORPOST 52720ORPOST 50995ORPOST 51312ORPOST 52146OP 12 OPERATIONAL CHECK OF IFES SMOKE DETECTION BY MCDU. 8 I: 18 MOPOST 48818RS 13 REMOVE IFES PICCOLO TUBES FOR CLEANING. 7 I: 18000 FHPOST 4881814 TASK RESERVED15 TASK RESERVED16 TASK RESERVED17 TASK RESERVEDOP 18 OPERATIONAL CHECK OF FCC SMOKE DETECTION BY MCDU. 9 I: CPOST 54477ORPOST 54762ORPOST 54946N RS 19 REMOVE AND CLEAN PICCOLO TUBES OF FCC RACK SMOKE 8 I: 18000 FHPOST 54128DETECTION.ORPOST 54477ORPOST 54762ORPOST 54946N OP 20 OPERATIONAL CHECK OF ALNAV2 CENTER RACK IV SMOKE 9 I: 18 MOPOST 56389DETECTION BY MCDUN RS 21 REMOVE AND CLEAN PICCOLO TUBES OF ALNAV2 CENTER 8 I: 17000 FHPOST 56389RACK IV SMOKE DETECTIONISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.18.01 BULK AVIONICS COMPARTMENT SMOKE DETECTION (MOD 46441)RS 01 REMOVE AND CLEAN BULK AVIONICS SMOKE DETECTOR PICCOLO 8 I: 36 MOIF VIDEO RACKTUBESIN BACINSTALLEDOP 02 OPERATIONAL CHECK OF THE BULK AVIONICS COMPARTMENT 9 I: CIF VIDEO RACKSMOKE DETECTION SYSTEM VIA MCDUIN BACINSTALLED26.18.02 SMOKE DETECTION COURIER AREAN NO TASK SELECTED26.19.00 MAIN DECK CARGO COMPARTMENT SMOKE DETECTIONN OP 01 OPERATIONAL CHECK OF MAIN DECK CARGO COMPARTMENT 9 I: 3200 FHA330-200FSMOKE DETECTION BY PTT.N OP 02 OPERATIONAL CHECK TO VERIFY AUTOMATIC CLOSING OF MDCC 9 I: 18 MOA330-200FISOLATION VALVES.26.21.00 ENGINE FIRE EXTINGUISHINGOP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING SYSTEM 9 I: 1 AALLNOTE 5OP 02 OPERATIONAL CHECK OF ENGINE FIRE EXTINGUISHER BOTTLE 9 I: CALLLOW PRESSURE INDICATING CIRCUITOP 03 OPERATIONAL CHECK TO VERIFY ENGINE FIRE P/B SW 8 I: 18 MOALLFUNCTION(THIS TASK COVERS TASKS 24.20.00/15, 28.24.00/02 AND36.00.00/04)FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,9 I: NR OR VRALLPRESSURE SWITCH SETTING NOTE 805 TASK DELETED06 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.21.00 * * * * * C O N T I N U E * * * * *FC 07 FUNCTIONAL CHECK OF FIRING CIRCUIT CONTINUITY 9 I: 2 CALLFC 08 FUNCTIONAL CHECK OF DISTRIBUTION PIPING FOR LEAKAGE 8 I: 12000 FHALLAND OBSTRUCTIONDS 09 DISCARD CARTRIDGE 9 I: VRALL26.22.00 APU FIRE EXTINGUISHINGOP 01 OPERATIONAL CHECK OF APU FIRE EXTINGUISHING SYSTEM 9 I: 2 AALL(THIS TASK COVERS TASK 26.13.00/01)OP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING VIA 9 I: 4800 FHALLMCDU AND CHECK OF "FIRE EMERGENCY STOP RELAYS" (5WF,6WF)(THIS TASK COVERS TASK 49.62.00/03)OP 03 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 9 I: CALLTRIGGER CIRCUIT04 TASK DELETEDFC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 7,9 I: VRALLPRESSURE SWITCH SETTING ORNRNOTE 806 TASK DELETEDOP 07 OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 9 I: 2 CALLDI 08 DETAILED INSPECTION OF DISTRIBUTION PIPING FOR CRACKS 8 I: 14000 FHALLOP 09 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 36 MOALLOP 10 OPERATIONAL CHECK OF APU FIRE P/B SW FUNCTION (THIS 8 I: 36 MOALLTASK COVERS TASKS 28.29.00/01 AND 49.62.00/04)DS 11 DISCARD CARTRIDGE 8 I: VRALL26.23.00 LOWER DECK CARGO COMPARTMENT FIRE EXTINGUISHING (FWD, AFT ANDBULK)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.23.00 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW 9 I: CALLPRESSURE INDICATION CIRCUIT BY PTTR DS 02 DISCARD AND REPLACE WATER ADSORBING FILTER ELEMENT 8 I: 15 MOPOST 40041ORPOST 44601FC 03 REMOVE BOTTLE FOR WEIGHT CHECK 8 I: 8000 FHALLOP 04 OPERATIONAL CHECK OF FIRING CIRCUIT CONTINUITY 8 I: 10000 FHALLFC 05 REMOVE BOTTLE FOR HYDROSTATIC TEST 6,9 I: VRALLORNRNOTE 8FC 06 FUNCTIONAL CHECK OF PRESSURE REDUCER 8 I: 14000 FHALLNOTE 2407 TASK DELETED08 TASK DELETEDFC 09 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND 8 I: 14000 FHALLOBSTRUCTION10 TASK DELETEDDS 11 DISCARD CARTRIDGE UNIT 8 I: VRALLDI 12 DETAILED INSPECTION OF RESTRICTOR, HALON FILTER AND 8 I: 14000 FHALLCHECK VALVE NOTE 2413 TASK DELETED14 TASK DELETED15 TASK DELETED26.24.00 PORTABLE FIRE EXTINGUISHER* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.24.00 * * * * * C O N T I N U E * * * * *FC 01 REMOVE BOTTLES FOR WEIGHT CHECK 9 I: VRALLNOTE 26FC 02 REMOVE BOTTLES FOR HYDROSTATIC TEST 9 I: VRALLORNRNOTE 803 TASK DELETEDGVI 04 GENERAL VISUAL INSPECTION OF PORTABLE FIRE 9 I: 1000 FHALLEXTINGUISHER ATTACHMENT.26.25.00 LAVATORY FIRE EXTINGUISHINGOP 01 CHECK PRESSURE OF EXTINGUISHING AGENT 9 I: CALLFC 02 REMOVE BOTTLE FOR WEIGHT CHECK 9 I: 4 CALL26.28.00 AUXILIARY AREAS FIRE EXTINGUISHING (IF INSTALLED) (CREW RESTROOM - UNDERFLOOR)01 TASK RESERVEDOP 02 OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING 8 I: 12000 CRRPOST 52339CIRCUIT IN THE LDMCR. FHPRE 47549ORPOST 55244PRE 47549DS 03 DISCARD CARTRIDGE OF FIRE EXTINGUISHING BOTTLE 8 I: VRPOST 55244IN THE LDMCR.ORPOST 52339FC 04 REMOVE BOTTLE FOR HYDROSTATIC TEST AND CHECK OF 6,8 I: VRPOST 55244PRESSURE SWITCH SETTING IN THE LDMCR. ORORNRPOST 52339NOTE 8* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *OP 05 OPERATIONAL CHECK OF FIRE EXTINGUISHING LINES FOR 8 I: 72 CRR MOPOST 55244OBSTRUCTION IN THE LDMCR.ORPOST 52339OP 06 OPERATIONAL CHECK OF SQUIB FUNCTIONALITY 8 I: 800 CRRPOST 55244IN THE LDMCR. FHORPOST 52339OP 07 OPERATIONAL CHECK OF THE MANUAL FIRE EXTINGUISHING 9 I: 36 CRR MOPOST 55244CIRCUIT IN THE LDMCR.ORPOST 52339OP 08 OPERATIONAL CHECK OF THE PRESSURE INDICATING CIRCUIT 8 I: 18 CRR MOPOST 55244IN THE LDMCR.ORPOST 5233909 TASK RESERVED10 TASK RESERVED11 TASK RESERVED12 TASK DELETED13 TASK RESERVED14 TASK RESERVED15 TASK DELETED16 TASK RESERVED17 TASK RESERVED18 TASK RESERVED19 TASK RESERVED20 TASK RESERVED21 TASK RESERVED22 TASK RESERVED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section26.28.00 * * * * * C O N T I N U E * * * * *23 TASK RESERVED24 TASK RESERVED25 TASK RESERVED* * * * * E N D * * * * *ISSUE: JUL 01/10 FIRE PROTECTION SECTION: C-26PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.00.00 FLIGHT CONTROLS27.14.00 AILERON AND HYDRAULIC ACTUATIONOP 01 OPERATIONAL CHECK OF AILERON DAMPING MEASUREMENT BY 8 I: 10000 FHALLBITE NOTE 24(THIS TASK COVERS TASK 29.10.00/12)VC 02 CHECK AILERON SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FHALLPOSITIONFC 03 CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FHALLEXCESSIVE PLAY AND GENERAL CONDITIONLU 04 LUBRICATION OF AILERON HINGE BEARINGS 9 I: 7500 FHALLOR18 MOLU 05 LUBRICATION OF AILERON SERVO CONTROL ROLLER BEARINGS 8 I: 7500 FHPOST 45512OROR18 MOPOST 47433ORPOST 48221OP 06 OPERATIONAL CHECK OF FCPC AND FCSC AILERON SERVO 9 I: CALLLOOPS (COVERED BY MSI 27-90-00 TASK NO 6)27.21.00 RUDDER MECHANICAL CONTROL01 TASK DELETED02 TASK DELETEDR OP 03 OPERATIONAL CHECK OF YAW DAMPER SERVO ACTUATOR 9 I: CA330-200STANDBY SERVO LOOPPRE 49144ORA330-300PRE 49144* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.21.00 * * * * * C O N T I N U E * * * * *R VC 04 CHECK POINTER OF CABLE TENSION REGULATOR WITHIN 9 I: 2 CA330-200LIMITSPRE 49144ORA330-300PRE 49144R OP 05 OPERATIONAL CHECK OF TRIM ACTUATOR STANDBY CHANNEL 9 I: 2 CA330-200PRE 49144ORA330-300PRE 49144R OP 06 OPERATIONAL CHECK OF RUDDER AND PEDALS TRAVEL 9 I: 2 CA330-200LIMITATION UNITS STANDBY CHANNELPRE 49144ORA330-300PRE 49144R VC 07 VISUAL CHECK OF RUDDER MECHANICAL CONTROL IN FIN 8 I: 20000 FHA330-200PRE 49144ORA330-300PRE 49144R DI 08 DETAILED INSPECTION OF RUDDER MECHANICAL CONTROL 6,9 I: 4 CA330-200(EXCLUDING FIN)PRE 49144ORA330-300PRE 49144R OP 09 OPERATIONAL CHECK OF AP ARTIFICIAL FEEL SPRING ROD 9 I: 4 CA330-200PRE 49144ORA330-300PRE 4914410 TASK RESERVEDR FC 11 FUNCTIONAL CHECK FOR RUDDER SERVO-CONTROLS 8 I: 42 MOA330-200SYNCHRONIZATION FOLLOWED BY SPRING-ROD REMOVAL FOR ORPRE 49144WORKSHOP CHECK 20000 FHORA330-300PRE 49144* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.21.00 * * * * * C O N T I N U E * * * * *R OP 12 OPERATIONAL CHECK OF CENTERING MECHANISM 8 I: 34000 FHA330-200PRE 49144ORA330-300PRE 49144R OP 13 OPERATIONAL CHECK OF BACK-UP YAW DAMPER BY BITE 8 I: 3200 FHA330-200NOTE 24PRE 49144ORA330-300PRE 4914414 TASK DELETEDR VC 15 VISUAL CHECK TO CONFIRM INTEGRITY OF CONTROL ROD 8 I: 20000 FHA330-200(ITEM 220 IN IPC 272147-1A) IN PTLU LINKAGE NOTE 24POST 44442PRE 49144ORA330-300POST 44442PRE 49144LU 16 LUBRICATION OF THE RUDDER PEDALS ADJUSTMENT MECHANISM 6 I: CALL17 TASK DELETEDR DI 18 DETAILED INSPECTION OF THE RUDDER MECHANICAL INPUT 6 I: 4 CA330-200POST 49144ORA330-300POST 49144ORA330-200FR OP 19 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM 9 I: 2 CA330-200STANDBY CHANNELPOST 49144(THIS TASK COVERS TASK 27.90.00/18)ORA330-300POST 49144ORA330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.21.00 * * * * * C O N T I N U E * * * * *R OP 20 OPERATIONAL CHECK OF THE AP ARTIFICIAL FEEL 9 I: 4 CA330-200POST 49144ORA330-300POST 49144ORA330-200F27.24.00 RUDDER HYDRAULIC ACTUATIONLU 01 LUBRICATION OF RUDDER HINGE BEARING NO4 9 I: 7500 FHA330-300OR18 MOR OP 02 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH 8 I: 800 FHA330-200INDIVIDUAL HYDRAULIC SYSTEMS (THIS TASK COVERS TASKPRE 4914429.10.00/08)ORA330-300PRE 49144R OP 03 OPERATIONAL CHECK OF RUDDER SERVO CONTROL JAMMING 9 I: 2 CA330-200DEVICEPRE 49144ORA330-300PRE 49144FC 04 CHECK RUDDER SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 34000 FHALLEXCESSIVE PLAY AND GENERAL CONDITION05 TASK DELETEDR LU 06 LUBRICATION OF RUDDER SERVO CONTROL TAILSTOCK ROLLER 8 I: 7500 FHA330-200BEARING (RUDDER SIDE) ORPOST 4464718 MOPRE 49144ORA330-200POST 49144ORA330-300POST 49144ORA330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.24.00 * * * * * C O N T I N U E * * * * *R LU 07 LUBRICATION OF RUDDER HINGE BEARING NO 6 9 I: 7500 FHA330-200OROR18 MOA330-200FR OP 08 OPERATIONAL CHECK OF RUDDER DAMPING MEASUREMENT BY 9 I: 1 CA330-200BITE NOTE 24POST 49144ORA330-300POST 49144ORA330-200F09 TASK DELETEDFC 10 FUNCTIONAL CHECK OF THE INDIVIDUAL RUDDER 9 I: 10000 FHA330-300SERVOCONTROLSPRE 4914427.34.00 ELEVATOR AND HYDRAULIC ACTUATIONOP 01 OPERATIONAL CHECK OF ELEVATOR DAMPING MEASUREMENT BY 8 I: 10000 FHALLBITE OR18 MONOTE 24FC 02 CHECK ELEVATOR SERVO CONTROL AND HINGE BEARINGS FOR 8 I: 30000 FHALLEXCESSIVE PLAY AND GENERAL CONDITIONVC 03 CHECK ELEVATOR SERVO CONTROL ACCUMULATOR PISTON 8 I: 34000 FHALLPOSITIONLU 04 LUBRICATION OF ELEVATOR SERVO CONTROL ROLLER BEARING 8 I: 7500 FHPOST 47674OROR18 MOPOST 49586OP 05 OPERATIONAL CHECK OF FCPCS AND FCSCS STANDBY SERVO 9 I: CALLLOOPS ON PITCH CONTROL (COVERED BY MSI 27-90-00TASK NO 9)06 TASK RESERVED27.40.00 TRIMMABLE HORIZONTAL STABILIZER (THS)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.40.00 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL 8 I: 800 FHALLHYDRAULIC SYSTEMS NOTE 24LU 02 LUBRICATION OF THS ACTUATOR BALL SCREW NUT 8 I: 700 FHALLSV 03 CHECK OIL LEVEL OF THS ACTUATOR GEARBOX 6,9 I: 8 AALLOP 04 OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION 8 I: 5600 FHALLDEVICE NOTE 24DI 05 CHECK MAGNETIC CHIP DETECTOR OF THS ACTUATOR GEARBOX 9 I: CALLDI 06 DETAILED INSPECTION OF THS ACTUATOR FAIL SAFE NUT 8 I: 12000 FHALLDI 07 DETAILED INSPECTION OF UPPER THS ACTUATOR ATTACHMENT 8 I: 12000 FHALL(PRIMARY AND SECONDARY) AND NO-BACK HOUSINGDI 08 DETAILED INSPECTION OF LOWER THS ACTUATOR ATTACHMENT 8 I: 12000 FHALL(PRIMARY AND SECONDARY).LU 09 LUBRICATION OF THS MECHANICAL CONTROL CHAINS 6 I: 2 CALLFC 10 CHECK MOVABLE INDEX ON THS CABLE TENSION COMPENSATOR 6 I: CALLSCALE IS WITHIN LIMITS.VC 11 CHECK WEAR INDICATOR OF THS ACTUATOR NO-BACK SYSTEM 8 I: 15000 FHALLFC 12 CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT 8 I: 16000 FHALL(PRIMARY AND SECONDARY LOAD PATH).OP 13 OPERATIONAL CHECK OF THS ACTUATOR NO-BACK SYSTEM 8 I: 34000 FHALLDI 14 DETAILED INSPECTION OF THS MECHANICAL CONTROL LOOP 6 I: 4 CALLFC 15 FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE-OFF BRAKE 9 I: 4 CALL(CHECK OF STATIC TORQUE)VC 16 VISUAL CHECK OF THS ACTUATOR DRAIN COLLECTING 9 I: 2 APOST 43683CONTAINER ASSEMBLY INCLUDING HOSESORPOST 4557817 TASK RESERVED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.40.00 * * * * * C O N T I N U E * * * * *OP 18 OPERATIONAL CHECK OF THSA CHECKABLE SHEAR PIN. 9 I: 10000 FHA330-200POST 54880ORA330-300POST 54880ORA330-300POST 54881ORA330-200POST 55780ORA330-300POST 5578027.50.00 FLAPSLU 01 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 4 APRE 40701BEARINGS.PRE 47372PRE 51363SV 02 TOP UP PCU TO CONFIRM FLUID LEVEL 6 I: CALLDI 03 DETAILED INSPECTION OF TRANSMISSION ASSY 6 I: 60 MOALLDI 04 DETAILED INSPECTION OF CRUISE ROLLERS, FLAP TRACKS 9 I: 60 MOALLAND CARRIAGES, ROTARY ACTUATORS AND ATTACHMENTSSV 05 DRAIN AND REFILL ROTARY ACTUATOR WITH SEMI-FLUID 6 I: 60 MOALLDI 06 DETAILED INSPECTION OF TRACK 4 SENSORS 9 I: 60 MOALLDI 07 DETAILED INSPECTION OF INTERCONNECTION STRUT AND 8 I: 60 MOALLATTACHMENTSFC 08 REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YEALL(THIS TASK COVERS TASK 27.80.00/05)SV 09 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 CALLGVI 10 GENERAL VISUAL INSPECTION OF FLAP TRACK FAIRING 9 I: 4 C ZL-531-02-1 ALLSUPPORT STRUTS AND LINKAGE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.50.00 * * * * * C O N T I N U E * * * * *LU 11 LUBRICATION OF FLAP CARRIAGE (2 TO 5) LEVER BEARINGS 9 I: 4 APRE 43303LU 12 LUBRICATION OF STEADY BEARINGS 6 I: CALLLU 13 LUBRICATION OF FLAP TRACK/CARRIAGE (1-5) ROLLER 9 I: 2 CPOST 51363BEARINGS.OP 14 OPERATIONAL CHECK OF FLAP WTB/POB PERFOMANCE TEST. 8 I: 6400 FHALL27.64.00 SPOILER HYDRAULIC ACTUATIONLU 01 LUBRICATION OF ALL SPOILER LINKAGE BEARINGS PROVIDED 9 I: CALLWITH GREASE NIPPLESDI 02 DETAILED INSPECTION OF LINKAGE AND ATTACHMENT OF 9 I: 4 CALLSPOILERS 1 TO 627.80.00 LIFT AUGMENTING (SLATS)LU 01 LUBRICATION OF ALL SLAT TRACK ROLLER BEARINGS, PINION 6,9 I: 2800 FHALLBEARINGS, PINION AND RACK TEETH AND SLAT TRACK 2 AND3 LEVER BEARINGSSV 02 TOP UP PCU GEARBOX TO CONFIRM FLUID LEVEL 6 I: CALLDI 03 DETAILED INSPECTION OF SLAT TRANSMISSION ASSY 6 I: 4 CALLDI 04 DETAILED INSPECTION OF SLAT TRACKS AND ROLLERS, 9 I: 4 CALLPINIONS AND CURVED RACK GEARSFC 05 REMOVAL OF CSU FOR WORKSHOP CHECK OF FRICTION BRAKE 8 I: 12 YEALL(COVERED BY MSI 27-50-00, TASK 08)SV 06 TOP UP SYSTEM TORQUE LIMITER TO CONFIRM FLUID LEVEL 6,9 I: 2 CALLLU 07 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE A 6 I: 4 CPOST 50471(TRACK 2-3).ORPOST 50138LU 08 LUBRICATION OF STEADY BEARINGS 6 I: CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.80.00 * * * * * C O N T I N U E * * * * *LU 09 LUBRICATION OF SLAT ROTARY ACTUATOR TYPE B 6 I: 4 CALL(TRACK 5-16).OP 10 OPERATIONAL CHECK OF SLAT WTB/POB PERFOMANCE TEST. 8 I: 6400 FHALL27.90.00 ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS)OP 01 OPERATIONAL CHECK OF TAKEOVER AND PRIORITY FUNCTION 8 I: 18 MOALLOP 02 OPERATIONAL CHECK OF FCPCS AND FCSCS YAW DAMPER SERVO 9 I: CPRE 49144LOOPS.03 TASK RESERVEDOP 04 OPERATIONAL CHECK OF FCPC1 AND FCSC1 POWER SUPPLY 9 I: CALLOP 05 OPERATIONAL CHECK OF FCPC2 AND THS ACTUATOR 9 I: 1 CPRE 44047ELECTRICAL MOTOR 2 POWER SUPPLY NOTE 24OP 06 OPERATIONAL CHECK OF FCPCS AND FCSCS AILERON SERVO 9 I: CALLLOOPS(THIS TASK COVERS TASK 27.14.00/06)OP 07 OPERATIONAL CHECK OF GREEN SERVOCONTROLS TRAVEL SPEED 8 I: 18 MOALLLIMITATION WHEN RAT IS EXTENDED NOTE 24OP 08 OPERATIONAL CHECK OF RETURN TO LOW SPEED 9 I: 4 CPRE 49144CONFIGURATION OF RUDDER AND PEDAL TRAVEL LIMITATIONUNITSOP 09 OPERATIONAL CHECK OF FCPCS AND FCSCS STANDBY SERVO 9 I: 15 MOALLLOOPS ON PITCH CONTROL NOTE 24(THIS TASK COVERS TASK 27.34.00/05)OP 10 OPERATIONAL CHECK OF FCPC 3 POWER SUPPLY 9 I: CPOST 44385OP 11 OPERATIONAL CHECK OF POWER SUPPLY OF THE FCSC2 9 I: 1 CPOST 44047NOTE 2412 TASK RESERVEDOP 13 OPERATIONAL CHECK OF LIGHTS 9 I: 2 AALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 9APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section27.90.00 * * * * * 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 FHPOST 49144BACK UP POWER SUPPLY (BCM/BPS)OP 15 OPERATIONAL CHECK OF FCSC1 RUDDER SERVO LOOP 9 I: CPOST 49144OP 16 OPERATIONAL CHECK RUDDER ELECTRICAL BACK UP 8 I: 5000 FHPOST 4914417 TASK RESERVEDOP 18 OPERATIONAL CHECK OF FLY-BY-WIRE RUDDER TRIM STANDBY 9 I: 2 CPOST 49144CHANNEL (COVERED BY MSI 27-21-00 TASK NO 19)OP 19 OPERATIONAL CHECK OF POWER SUPPLY OF THE RTA2, RTLU 9 I: CPOST 44047AND PTLU MOTOR 2PRE 49144OP 20 OPERATIONAL CHECK OF PFTU-TRIM 2 NORMAL/BACK-UP 9 I: CPOST 44047POWER SUPPLYPOST 49144* * * * * E N D * * * * *ISSUE: JUL 01/10 FLIGHT CONTROLS SECTION: C-27PAGE 10APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.00.00 FUEL28.11.00 TANKSR OP 01 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DYA330-200FFROM INNER, OUTER AND WING VENT SURGE TANKS NOTE 1POST 58623PRE 200281ORA330-300OP 02 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 2 MOALLFROM TRIM TANK AND TRIM VENT SURGE TANK NOTE 1OP 03 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE, 9 I: CALLUSING INDIVIDUAL MOTORS, TO PROVE CORRECT ACTUATOROPERATION AND COCKPIT INDICATIONOP 04 OPERATIONAL CHECK OF EACH EMERGENCY ISOLATION VALVE 8 I: 6 YEALLTO PROVE THAT NEITHER VALVE HAS JAMMED IN THE OPENPOSITION AND TO VERIFY CORRECT OPERATION OF THE P/BSWOP 05 OPERATIONAL CHECK OF ALL COLLECTOR CELL CLACK VALVES 9 I: 8 CALLTO ENSURE FULL AND FREE MOVEMENT06 TASK DELETED07 TASK RESERVEDOP 08 OPERATIONAL CHECK OF STANDBY FUEL CELL CLACK VALVES 9 I: 8 CALLTO ENSURE FULL AND FREE MOVEMENTR OP 09 OPERATE WATER DRAIN VALVES TO DRAIN ACCUMULATED WATER 9 I: 7 DYA330-200FROM CENTER, INNER, OUTER AND WING VENT SURGE TANKS NOTE 1ORA330-200FPRE 58623ORA330-200FPOST 20028110 TASK RESERVED11 TASK RESERVED12 TASK RESERVED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.11.00 * * * * * C O N T I N U E * * * * *13 TASK RESERVED28.12.00 TANK VENTING SYSTEMVC 01 VISUAL CHECK OF THE APERTURE LEADING TO WING AND TRIM 9 I: 2 CALLSURGE TANK FLAME ARRESTORS (INSIDE THE NACA INTAKES)FOR BLOCKAGEVC 02 VISUAL CHECK OF THE WING AND TRIM VENT SURGE TANK 9 I: 1 CALLOVERPRESSURE PROTECTORS (BURST DISCS) FOR INTEGRITY NOTE 528.13.00 CENTER BOX VENTING AND DRAINAGER OP 01 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: AA330-200FCENTER BOX (THIS TASK COVERS TASKS 28.22.00/06,POST 5862328.23.00/03 AND 28.25.00/03)PRE 200281ORA330-30028.14.00 TRIM PIPE SHROUD DRAINAGE01 TASK DELETED02 TASK DELETEDFC 03 FUNCTIONAL CHECK OF TRIM PIPE SHROUD DRAIN LINE AND 8 I: 36 MOALLCONNECTORS WITHIN PRESSURIZED FUSELAGE(COVERED BY MSI MSI 28.27.00 TASK N03)28.17.00 WATER SCAVANGE01 TASK DELETED28.18.00 IGNITION PREVENTIONDI 01 DETAILED INSPECTION OF THE WING AND TRIM TANK BONDING 9 I: 8 CALLLEADS (SFAR88)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.18.00 * * * * * C O N T I N U E * * * * *GVI 02 GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND 9 I: 8 CALLPROBE ATTACHMENTS (SFAR88)GVI 03 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS 9 I: 8 CALL(SFAR88)R DI 04 DETAILED INSPECTION OF THE HEATSHIELDS BELOW THE 8 I: 6 YEA330-200CENTER TANK (SFAR88)POST 49520ORA330-200FPRE 58623ORA330-200FPOST 200281VC 05 VISUAL CHECK OF CENTER TANK FOR LEAKS (SFAR88) 8 I: 700 FHA330-200PRE 49520R GVI 06 GENERAL VISUAL INSPECTION OF CENTER TANK FORWARD 9 I: 4 CA330-200CARGO BAY INSULATION MATS (SFAR88)ORA330-200FPRE 58623ORA330-200FPOST 200281R GVI 07 GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE 9 I: 8 CA330-200CENTER TANK (SFAR88)ORA330-200FPRE 58623ORA330-200FPOST 200281GVI 08 GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND 9 I: 8 CALLTRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS(SFAR88)GVI 09 GENERAL VISUAL INSPECTION OF TRIM TANK EXTERNAL 9 I: 8 CALLELECTRICAL WIRING AND CONNECTIONS (SFAR88)GVI 10 GENERAL VISUAL INSPECTION OF WING FUEL PUMP 9 I: 8 CALLELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.18.00 * * * * * C O N T I N U E * * * * *SUPPLY CABLE (SFAR88)28.21.00 MAIN FUEL PUMP SYSTEMOP 01 OPERATIONAL CHECK TO VERIFY ISOLATION OF RIGHT NO.2 8 I: 4800 FHALLMAIN FUEL PUMP WHEN LEFT NO.2 MAIN FUEL PUMP IS NOTE 24RUNNING IN ELECTRICAL EMERGENCY CONFIGURATION AND TOVERIFY LEFT NO.2 PUMP "OFF" FUNCTION IS OPERATIVEOP 02 OPERATIONAL CHECK TO VERIFY THAT RELAY 27QA HAS NOT 8 I: 15000 FHALLFAILED IN THE ENERGISED POSITIONOP 03 OPERATIONAL CHECK OF STANDBY PUMP AUTOMATIC CONTROL. 9 I: CALL04 TASK RESERVEDOP 05 OPERATIONAL CHECK TO ENSURE THAT THE RIGHT NO.2 MAIN 8 I: 18 MOALLFUEL PUMP OPERATES WHEN THE LEFT NO.2 MAIN FUEL PUMPIS SWITCHED OFF IN ELECTRICAL EMERGENCY CONFIGURATION06 TASK RESERVED07 TASK RESERVED28.22.00 APU FUEL PUMP SYSTEM01 TASK RESERVED02 TASK DELETEDOP 03 OPERATIONAL CHECK OF FWD APU FUEL FEED PUMP 9 I: CPRE 44603ACTIVATION 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: CALLCIRCUIT VIA APU FIRE EMERGENCY STOP RELAYS (5WF AND6WF)GVI 05 GENERAL VISUAL INSPECTION OF APU FUEL FEED SHROUD 9 I: 4 C ZL-311-01-1 ALLLINE AND FUEL/AIR SEPARATOR FOR INTEGRITY AND ABSENCE ZL-313-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.22.00 * * * * * 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: AA330-200FCENTER BOXPOST 58623(COVERED BY MSI 28-13-00 TASK NO1)PRE 200281ORA330-300OP 07 OPERATE THE DRAIN VALVE OF THE FUEL/AIR SEPARATOR TO 9 I: 2800 FHPOST 42890DRAIN ANY ACCUMULATED WATERORPOST 4292108 TASK RESERVED09 TASK RESERVEDOP 10 OPERATIONAL CHECK TO VERIFY THAT RELAY 15QC HAS NOT 8 I: 36 MOPOST 44603FAILED IN ENERGIZED POSITION.28.23.00 CROSSFEED SYSTEMOP 01 OPERATIONAL CHECK OF CROSSFEED VALVE TO VERIFY THAT 8 I: 34000 FHALLINDIVIDUAL ENGINE FUEL FEED SYSTEMS CAN BE ORINTERCONNECTED 12 YEOP 02 OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL 9 I: 2 CALLMOTORSR OP 03 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: AA330-200FCENTER BOXPOST 58623(COVERED BY MSI 28.13.00 TASK NO1)PRE 200281ORA330-30004 TASK RESERVED05 TASK RESERVED06 TASK RESERVED28.24.00 ENGINE LP FUEL SHUT-OFF* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.24.00 * * * * * C O N T I N U E * * * * *OP 01 OPERATIONAL CHECK OF THE LP VALVE USING INDIVIDUAL 9 I: 2 CALLMOTORS, TO CHECK CORRECT ACTUATOR MOVEMENT ANDCORRECT COCKPIT INDICATIONOP 02 OPERATIONAL CHECK OF THE FIRE CONTROL P/B SW 8 I: 18 MOALLSUB-FUNCTIONS(COVERED BY MSI 26.21.00, TASK NO3)N OP 03 OPERATIONAL CHECK TO CONFIRM LP VALVE ISOLATES FUEL 8 I: 6500 FCALLSUPPLY TO ASSOCIATED ENGINE OR12 YE28.25.00 REFUEL/DEFUEL SYSTEMDI 01 DETAILED INSPECTION OF REFUEL COUPLING(S) FOR DAMAGE 9 I: CALLOR EVIDENCE OF WEAROP 02 OPERATIONAL CHECK TO PROVE THAT THERE IS NO FUEL 8 I: 34000 FHALLTRANSFER FROM AFT TO FWD INNER TANK WHEN EMERGENCY ORISOLATION VALVE IS SELECTED CLOSED 12 YER OP 03 OPERATE LEAK MONITOR TO CHECK FOR LEAKS INTO WING 9 I: AA330-200FCENTER BOXPOST 58623(COVERED BY MSI 28-13-00 TASK NO1)PRE 200281ORA330-30028.26.00 MAIN TRANSFER SYSTEMNO TASK SELECTED28.27.00 TRIM TANK TRANSFER SYSTEMR OP 01 OPERATIONAL CHECK TO CONFIRM CLOSURE OF VALVES 9 I: 2 CALLFOLLOWING TRIM PIPE ISOLATION BY 3 POSITION SWITCH NOTE 24R 02 TASK DELETEDR FC 03 FUNCTIONAL CHECK OF TRIM TANK TRANSFER LINE SHROUD 8 I: 36 MOALLCONNECTORS (THIS TASK COVERS TASK 28.14.00/03)ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.29.00 APU LP FUEL SHUT-OFFOP 01 OPERATIONAL CHECK OF APU LP FUEL SHUT OFF VALVE USING 9 I: 2 CALLEACH INDIVIDUAL MOTORS VIA APU FIRE EMERGENCY STOPRELAYS 5WF, 6WF(COVERED BY MSI 26-22-00, TASK NO10)28.31.00 JETTISON SYSTEMR GVI 01 GENERAL VISUAL INSPECTION OF JETTISON PIPE FLEXIBLE 9 I: 2 CA330-200HOSE FOR SECURITY AND CONDITIONPOST 45008ORA330-200FPOST 45008R GVI 02 GENERAL VISUAL INSPECTION OF ANTI-CORONA DEVICE FOR 9 I: 2 CA330-200SECURITY OF ATTACHMENT AND FOR SATISFACTORY CONDITIONPOST 45008ORA330-200FPOST 45008R OP 03 OPERATIONAL CHECK TO VERIFY CORRECT RESPONSE OF 9 I: 4 CA330-200JETTISON VALVES TO SELECTION OF JETTISON "ON"POST 45008ORA330-200FPOST 4500828.42.00 QUANTITY INDICATINGNO TASK SELECTED28.46.00 TANK LEVEL SENSING01 TASK DELETEDOP 02 OPERATIONAL CHECK OF INNER TANK LOW LEVEL SENSORS AND 8 I: 10000 FHALLASSOCIATED WARNINGS28.49.00 FUEL TEMPERATURE MEASUREMENT01 TASK RESERVEDISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section28.51.00 FUEL CONTROL AND MONITORING01 TASK RESERVED* * * * * E N D * * * * *ISSUE: JUL 01/10 FUEL SECTION: C-28PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section29.00.00 HYDRAULIC POWER29.10.00 MAIN HYDRAULIC POWERFC 01 CHECK NITROGEN CHARGING PRESSURE ON HYDRAULIC POWER 9 I: 400 FHALLACCUMULATORSVC 02 CHECK CLOGGING INDICATORS OF HIGH PRESSURE (HP), 9 I: AALLRETURN, ENGINE DRIVEN PUMPS (EDP) CASE DRAIN,RESERVOIR FILL AND AIR PRESSURIZATION UNIT (PUA)FILTERSR SV 03 DRAINING OF WATER SEPARATORS 9 I: AA330-200PRE 47625ORA330-300PRE 47625SV 04 SERVICING OF LEAKAGE RECOVERY TANKS 9 I: 2 AALLOP 05 OPERATIONAL CHECK OF EDP DEPRESSURIZATION 9 I: CALLDI 06 CHECK FOR CORRECT AIR PRESSURE BY READING GAUGES ON 6 I: CALLEACH RESERVOIRFC 07 FUNCTIONAL CHECK OF PRIORITY VALVE 6,9 I: 4 CALLOP 08 OPERATIONAL CHECK OF RUDDER SERVO CONTROL WITH GREEN 8 I: 18 MOALLHYDRAULIC SYSTEM PRESSURIZED.OP 09 OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT-OFF VALVES 8 I: 18 MOALLOP 10 OPERATIONAL CHECK OF AUTOMATIC CONTROL OF FIRE 8 I: 18 MOALLSHUT-OFF VALVE IN CASE OF LOW LEVEL ON GREENHYDRAULIC SYSTEMFC 11 HYDRAULIC FLUID ANALYSIS 9 I: 2 CALLOP 12 OPERATIONAL CHECK OF AILERON SERVOCONTROL WITH GREEN 9 I: 12500 FHALLHYDRAULIC SYSTEM(COVERED BY MSI 27-14-00 TASK NO 01)FC 13 FUNCTIONAL CHECK OF GREEN LOW LEVEL WARNING SYSTEM 8 I: 12000 FHALL(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-29PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section29.10.00 * * * * * C O N T I N U E * * * * *OP 14 OPERATIONAL CHECK OF INHIBITION OF MANUAL CONTROL OF 9 I: 4 CALLLEAK MEASUREMENT SOLENOID VALVEFC 15 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 6 I: 4 CALLYELLOW AND BLUE HYDRAULIC SYSTEMFC 16 REMOVE FIN HYDRAULIC FUSE FOR WORKSHOP CHECK 8 I: 6 YEPOST 40838GVI 17 GENERAL VISUAL INSPECTION OF SEAL DRAIN SYSTEM 9 I: 4 C ZL-147-01-1 ALLZL-195-02-1FC 18 REMOVE WING HYDRAULIC FUSES FOR WORKSHOP CHECK 8 I: 6 YEPOST 4083819 TASK RESERVED20 TASK RESERVEDVC 21 VISUAL CHECK OF THE PRESSURE UNIT AIR AUTOMATIC DRAIN 9 I: APOST 47625VALVE POSITION22 TASK RESERVED23 TASK RESERVEDFC 24 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE IN 6 I: 10000 FHALLGREEN SYSTEM.(COVERED BY MSI 29-20-00 TASK NO 08)29.20.00 AUXILIARY HYDRAULIC POWEROP 01 OPERATIONAL CHECK OF GREEN, YELLOW AND BLUE ELECTRIC 9 I: 4 AALLPUMPSOP 02 OPERATIONAL CHECK OF AUTOMATIC START OF GREEN AND 9 I: 4 AALLYELLOW ELECTRIC PUMPSOP 03 OPERATIONAL CHECK OF AUTOMATIC RAT DEPLOYMENT 8 I: 18 MOALL04 TASK DELETEDDI 05 DETAILED INSPECTION OF RAT IN DEPLOYED POSITION 8 I: 18 MOALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section29.20.00 * * * * * C O N T I N U E * * * * *FC 06 OPERATIONAL CHECK OF MANUAL RAT DEPLOYMENT FOLLOWED 8 I: 18 MOALLBY FUNCTIONAL CHECK OF RAT OPERATION AND INSPECTION NOTE 24OF FILTER ELEMENT BY REFERENCE TO DIFFERENTIALPRESSURE INDICATOR:FC 07 FUNCTIONAL CHECK OF GREEN, BLUE AND YELLOW LOW LEVEL 8 I: 12000 FHALLWARNING SYSTEM(THIS TASK COVERS TASK 29.10.00/13)FC 08 FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF 8 I: 10000 FHALLGREEN HYDRAULIC SYSTEM(THIS TASK COVERS TASK 29.10.00/24)09 TASK RESERVEDOP 10 OPERATIONAL CHECK OF THE AUTOMATIC START OF THE BLUE 9 I: CPOST 49748ELECTRIC PUMP.29.30.00 HYDRAULIC SYSTEM DATA ACQUISITION / INTERFACE AND INDICATINGOP 01 CROSS CHECK FLUID LEVEL ON EACH RESERVOIR, ON ECAM 9 I: 2 AALLHYDRAULIC PAGE AND GROUND SERVICE PANEL INDICATOROP 02 OPERATIONAL CHECK OF OVERHEAT DETECTION SYSTEM 9 I: CALLOP 03 OPERATIONAL CHECK OF RESERVOIRS LOW AIR PRESSURE 9 I: CALLWARNING* * * * * E N D * * * * *ISSUE: JUL 01/10 HYDRAULIC POWER SECTION: C-29PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section30.00.00 ICE AND RAIN PROTECTION30.11.00 WING ICE PROTECTIONDI 01 DETAILED INSPECTION OF TELESCOPIC DUCTS, FLEXIBLE 9 I: 2 CALLSLAT INTERCONNECTION SLEEVES AND, IN WING LEADINGEDGE, ANTI-ICING DUCT COUPLINGS, CLAMPS ANDATTACHMENT POINTS30.21.01 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 GE CF6-80E1)DI 01 DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY 6 I: CCF6-80E1DUCTS AND ASSOCIATED HARDWARE IN CORE AND FANCOMPARTMENTSOP 02 OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE PROTECTION 9 I: 2 CCF6-80E1FAULT WARNINGGVI 03 GENERAL VISUAL INSPECTION OF INLET COWL ANTI-ICE 9 I: 4 C ZL-411-03-1 CF6-80E1SUPPLY DUCT (BETWEEN SWIRL NOZZLE AND AFT BULKHEAD)30.21.02 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 PW4000)R NO TASK SELECTED30.21.03 ENGINE AIR INTAKE ICE PROTECTION (30.21.00 RR TRENT 768/772)NO TASK SELECTED30.31.00 PROBE ICE PROTECTIONNO TASK SELECTED30.42.00 WINDSHIELD ANTI-ICING AND DEFOGGINGNO TASK SELECTED30.45.00 WINDSHIELD RAIN PROTECTION* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section30.45.00 * * * * * C O N T I N U E * * * * *01 TASK DELETED02 TASK DELETED30.46.00 ESCAPE SLIDE LOCKING MECHANISM ICE PROTECTIONR OP 01 OPERATIONAL CHECK OF ESCAPE SLIDE LOCKING MECHANISM 9 I: CA330-200ICE PROTECTIONPOST 40335PRE 51642PRE 51617ORA330-300POST 40335PRE 51642PRE 5161730.70.00 WATER LINESNO TASK SELECTED30.81.00 ICE DETECTIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ICE AND RAIN PROTECTION SECTION: C-30PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section31.00.00 INDICATING/RECORDING SYSTEMS31.21.00 ELECTRICAL CLOCKDS 01 DISCARD CLOCK BATTERY 9 I: VRIF CLOCK FITTEDWITH BATTERY31.33.00 DIGITAL FLIGHT DATA RECORDING SYSTEM (DFDRS)R DS 01 DISCARD ULB BATTERY. 9 I: VRA330-200PRE 48904ORA330-300PRE 48904R OP 02 OPERATIONAL CHECK FOR DFDR SYSTEM BY USING THE MCDU. 9 I: 1 CA330-200NOTE 8PRE 48904ORA330-300PRE 48904R OP 03 OPERATIONAL CHECK OF THE ULB. 9 I: VRA330-200PRE 48904ORA330-300PRE 4890431.36.00 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)NO TASK SELECTED31.36.01 AIRCRAFT CONDITION MONITORING SYSTEM (ACMS)R DS 01 DISCARD ULB BATTERY 9 I: VRPOST 48904R OP 02 OPERATIONEL CHECK FOR DFDR SYSTEM BY USING THE MCDU. 9 I: 1 CPOST 48904NOTE 8R OP 03 OPERATIONAL CHECK OF ULB 9 I: VRPOST 48904* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section31.36.01 * * * * * C O N T I N U E * * * * *N OP 04 OPERATIONAL CHECK OF WGL-QAR/DAR INTERLOCK AND 8 I: 24000 FHPOST 55048TRANSMISSION LOGIC.ORPOST 5629331.44.00 WEIGHT AND BALANCE SYSTEM (IF INSTALLED)NO TASK SELECTED31.50.00 CENTRAL WARNING SYSTEMOP 01 OPERATIONAL CHECK OF ATTENTION GETTER LIGHTS 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1).OP 02 OPERATIONAL CHECK OF AUTOLAND LIGHTS 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 03 OPERATIONAL CHECK OF SLAT AND FLAP SENSOR CIRCUIT VIA 8 I: 34000 FHALLMCDUOP 04 OPERATIONAL CHECK OF DMC OUTPUT CIRCUITS TO FWC ́S 8 I: 34000 FHALL31.60.00 ELECTRONIC INSTRUMENT SYSTEMOP 01 OPERATIONAL CHECK OF PFD/ND AND ECAM/ND MANUAL 9 I: CPRE 50161TRANSFEROP 02 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 9 I: CPRE 50161OP 03 OPERATIONAL CHECK OF CORRECT EFIS AND ECAM TRANSFER 9 I: 2 CPRE 50161WHEN BUSBAR 105XP IS LOST04 TASK DELETEDOP 05 OPERATIONAL CHECK OF EFIS OFFSIDE AND ECAM NON ACTIVE 8 I: 34000 FHPRE 50161MONITORING CIRCUITS31.60.01 ELECTRONIC INSTRUMENT SYSTEM 2 (LCD TECHNOLOGY)OP 01 OPERATIONAL CHECK OF PFD-ND AND ECAM-ND MANUAL 9 I: CPOST 50161* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section31.60.01 * * * * * C O N T I N U E * * * * *TRANSFEROP 02 OPERATIONAL CHECK OF BRIGHTNESS CONTROL THROUGH MCDU 9 I: CPOST 50161OP 03 OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN 9 I: 2 CPOST 50161BUSBAR 105XP IS LOSTOP 04 OPERATIONAL CHECK OF EFIS AND ECAM DMC TRANSFER 8 I: 18 MOPOST 50161* * * * * E N D * * * * *ISSUE: JUL 01/10 INDICATING/RECORDING SYSTEMS SECTION: C-31PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section32.00.00 LANDING GEAR32.11.00 MAIN GEARLU 01 LUBRICATION OF MAIN GEAR 6,9 I: 500 FCALLOR4 MOLU 02 LUBRICATION OF SHORTENING MECHANISM HINGE JOINTS 5 I: 500 FCALLOR4 MOFC 03 CHECK OF SHOCK ABSORBER NITROGEN CHARGE PRESSURE 6 I: CALLSV 04 SERVICE MLG SHOCK ABSORBER 6 I: 2 CALLFC 05 CHECK MAIN GEAR TORQUE LINKS FOR EXCESSIVE PLAY 6 I: 2 CALLRS 06 RESTORATION OF MAIN GEAR 5 I: NOTE 7ALLOP 07 REMOVE HYDRAULIC FUSE IN MLG BOGIE PITCH TRIMMER 9 I: 10 YEALLSUPPLY LINE FOR OPERATIONAL CHECK IN WORKSHOP.GVI 08 GENERAL VISUAL INSPECTION OF PITCH TRIMMER AND 6 I: A ZL-731-01-1 ALLASSOCIATED PIPING AND COMPONENTSGVI 09 GENERAL VISUAL INSPECTION OF SHOCK ABSORBER SLIDING 6 I: AALLMEMBER FOR SIGNS OF LEAKAGE AND NORMAL EXTENSION10 TASK DELETED32.21.00 NOSE GEARLU 01 LUBRICATION OF NOSE GEAR 6 I: 500 FCALLOR4 MOFC 02 CHECK NOSE GEAR SHOCK ABSORBER NITROGEN CHARGE 6 I: CALLPRESSUREFC 03 FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE 6 I: 2 CALLPLAY* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section32.21.00 * * * * * C O N T I N U E * * * * *SV 04 SERVICE NLG SHOCK ABSORBER 6 I: 2 CALLRS 05 REMOVE NOSE GEAR FOR RESTORATION 6 I: NOTE 7ALL(THIS TASK COVERS TASK 32.50.00/03).GVI 06 GENERAL VISUAL INSPECTION OF NOSE GEAR FOR SIGNS OF 6 I: AALLLEAKAGE AND NORMAL EXTENSION07 TASK DELETED32.30.00 EXTENSION AND RETRACTION POSITION AND WARNINGLU 01 LUBRICATION OF ALL GEAR UP-LOCKS, DOOR UP-LOCK UNITS 6,8 I: 500 FCALLAND PINS AND DOOR HINGES OR4 MO02 TASK DELETEDLU 03 LUBRICATE ALL GEAR DOWN LOCK PIVOT PINS 5,8 I: 500 FCALLOR4 MOVC 04 VISUAL CHECK OF DOWN LOCK SPRINGS ON ALL LANDING 9 I: 2 AALLGEARS05 TASK DELETEDOP 06 OPERATIONAL CHECK OF LANDING GEAR INDICATION CIRCUITS 9 I: CALLTO ENSURE "GEAR NOT DOWN FOR LANDING" WARNINGSOPERATE07 TASK DELETEDOP 08 OPERATIONAL CHECK OF LANDING GEAR FREE-FALL SYSTEM 8 I: 8000 FHALLFOR CORRECT OPERATION OF UP-LOCK RELEASEOP 09 OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK 9 I: 4 CALL(AIRCRAFT ON WHEELS)OP 10 OPERATIONAL CHECK OF GROUND DOORS CLOSURE INHIBIT 9 I: 4 CALLFC 11 FUNCTIONAL CHECK TO ENSURE THAT SAFETY VALVE CLOSES 9 I: 4 CALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section32.30.00 * * * * * C O N T I N U E * * * * *AT 280 KTSFC 12 FUNCTIONAL CHECK OF LANDING GEAR FREE-FALL EXTENSION 8 I: 6 YEALLGVI 13 GENERAL VISUAL INSPECTION OF LANDING GEAR HYDRAULIC 6 I: A ZL-711-01-1 ALLSYSTEM FOR SIGNS OF EXTERNAL LEAKAGE ZL-731-01-114 TASK RESERVED15 TASK RESERVED16 TASK RESERVED17 TASK RESERVED18 TASK RESERVED19 TASK RESERVED32.40.00 WHEELS AND BRAKESVC 01 CHECK HEAT PACK WEAR INDICATOR 9 I: 7 DYALL(PARKING BRAKE APPLIED)FC 02 CHECK TYRE PRESSURES 9 I: 3 DYALLVC 03 PERFORM CROSS-CHECK OF TPIS AND TYRE PRESSURE GAUGE 9 I: AIF TPISREADINGINSTALLEDFC 04 FUNCTIONAL CHECK OF NORMAL AND ALTERNATE BRAKE RETURN 6,9 I: 2 AALLACCUMULATORS NITROGEN PRESSURES BY READING GAUGESFC 05 CHECK FLUID LEVEL OF BRAKE LOW PRESSURE RESERVOIR 6 I: CALLFC 06 FUNCTIONAL CHECK OF NITROGEN CHARGE PRESSURE ON 9 I: AALLALTERNATE PARKING BRAKE ACCUMULATORS BY READINGGAUGESGVI 07 GENERAL VISUAL INSPECTION OF TYRES 6,9 I: 36 HRALLGVI 08 GENERAL VISUAL INSPECTION OF WHEELS 9 I: 36 HRALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section32.40.00 * * * * * C O N T I N U E * * * * *VC 09 VISUAL CHECK OF BRAKE FOR HYDRAULIC LEAKS 9 I: 36 HRALLOP 10 OPERATIONAL CHECK OF EMERGENCY BRAKE SHUT-OFF VALVE 9 I: 4 APOST 46231SV 11 DRAIN WATER ACCUMULATION IN THE DRAIN TUBE OF BRAKE 9 I: 4 APOST 47210DISTRIBUTION DUAL VALVE (BDDV).32.50.00 STEERINGLU 01 LUBRICATION OF NOSE LANDING GEAR ROTATING SLEEVE 6 I: 500 FCALLOR4 MOFC 02 CHECK NITROGEN PRESSURE ON NOSE WHEEL STEERING 9 I: CALLACCUMULATORRS 03 REMOVE NOSE GEAR FOR RESTORATION 9 I: NOTE 7ALL(COVERED BY MSI 32-21-00, TASK NO5)32.53.00 NOSE LANDING GEAR-STEERING ANGLE PROTECTIONOP 01 OPERATIONAL CHECK OF COCKPIT AND NLG WARNING LAMPS 9 I: APOST 43442FC 02 FUNCTIONAL CHECK OF OVERSTEER INDICATION SYSTEM 9 I: CPOST 43442* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: C-32PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section33.00.00 LIGHTS33.14.00 ANNUNCIATOR LIGHT TEST AND DIMMINGOP 01 OPERATIONAL CHECK OF LIGHTS 9 I: 2 AALL(THIS TASK COVERS TASKS 23.81.00/01, 24.20.00/04,27.90.00/13, 31.50.00/01, 31.50.00/02, 34.13.00/01,34.14.00/01, 34.48.00/01, 34.52.00/01, 35.20.02/06).33.41.00 NAVIGATION LIGHTSNO TASK SELECTED33.48.00 ANTI-COLLISION/STROBE LIGHTINGNO TASK SELECTED33.51.00 CABIN EMERGENCY LIGHTINGOP 01 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA MCDU 9 I: 2 APOST 43069OP 02 BATTERY CAPACITY CHECK VIA MCDU 9 I: 6 MOPOST 43069NOTE 26OP 03 OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM 9 I: 2 CALLAUTOMATIC CONTROL CIRCUIT AND MANUAL ACTIVATION FROMBOTH CONTROL PANELS AND CHECK ALL LIGHTS AND SIGNSILLUMINATED BY BATTERIES04 TASK DELETEDR OP 05 OPERATIONAL CHECK OF EMERGENCY LIGHTS VIA THE EPSU 9 I: 2 AA330-200TEST PUSHBUTTON.PRE 43069ORA330-300PRE 43069* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LIGHTS SECTION: C-33PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section33.51.00 * * * * * C O N T I N U E * * * * *R OP 06 REMOVE BATTERY FOR CAPACITY CHECK. 9 I: 6 MOA330-200NOTE 26PRE 43069ORA330-300PRE 43069* * * * * E N D * * * * *ISSUE: JUL 01/10 LIGHTS SECTION: C-33PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section34.00.00 NAVIGATION34.13.00 AIR DATAOP 01 OPERATIONAL CHECK OF ADR SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF PITOT PROBES HEATING (115 VAC) 9 I: 2 CALLAND ADR/AOA POWER SUPPLY (26 VAC) IN EMERGENCYCONFIGURATIONRS 03 FLUSHING OF PRINCIPAL TOTAL PRESSURE LINES 6 I: 24 MOALLNOTE 1FC 04 LOW RANGE LEAK CHECK OF PRINCIPAL PNEUMATIC CIRCUITS 6 I: 2 CALLN OP 05 OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY 8 I: 12000 FHPOST 5336834.14.00 ATTITUDE, HEADING AND POSITIONOP 01 OPERATIONAL CHECK OF THE IR SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF ATT/HDG SWITCHING 9 I: CALLOP 03 OPERATIONAL CHECK OF ADIRU 1, 2 AND 3 POWER SUPPLY IN 9 I: 2 CALLEMERGENCY CONFIGURATION34.21.00 ALTITUDE AND AIRSPEED STANDBY DATARS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MOPRE 47244NOTE 1FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 CPRE 4724434.22.00 ATTITUDE AND HEADING STANDBY DATANO TASK SELECTED34.22.20 INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section34.22.20 * * * * * C O N T I N U E * * * * *RS 01 DRAIN AND FLUSH STANDBY PNEUMATIC CIRCUITS 6 I: 24 MOPOST 47244NOTE 1FC 02 LOW RANGE LEAK CHECK OF STANDBY PNEUMATIC CIRCUITS 6 I: 2 CPOST 47244OP 03 OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY 8 I: 800 FHPOST 4724434.35.00 HEAD-UP DISPLAY (HUD) (IF INSTALLED)NO TASK SELECTED34.36.00 INSTRUMENT LANDING SYSTEM (ILS)NO TASK SELECTED34.36.01 MULTI-MODE RECEIVER (MMR)NO TASK SELECTED34.41.00 WEATHER RADAR SYSTEMFC 01 REMOVE RADOME FOR RADIO ELECTRICAL TEST 9 I: 30 MOPOST 44754PRE 44950ORPOST 44100PRE 4495034.42.00 RADIO ALTIMETEROP 01 OPERATIONAL CHECK OF FAN 9 I: NOTEALLNOTE:- 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-34PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section34.43.00 * * * * * C O N T I N U E * * * * *NO TASK SELECTED34.48.00 TERRAIN AWARNESS AND WARNING SYSTEM (INCLUDING (E)GPWS ANDT2CAS-TAWS)R OP 01 OPERATIONAL CHECK OF GPWS LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1).R OP 02 OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM 9 I: 2 CALL34.51.00 DISTANCE MEASURING EQUIPMENT (DME)NO TASK SELECTED34.52.00 ATC MODE S (SELECT)OP 01 OPERATIONAL CHECK OF ATC SYSTEM LIGHT 9 I: 2 AALL(COVERED BY MSI 33-14-00, TASK NO1)OP 02 OPERATIONAL CHECK OF THE REMOTE ATC SYSTEM 8 I: 24000 FHPOST 49769PRE 5352234.53.00 AUTOMATIC DIRECTION FINDER (ADF)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section34.53.00 * * * * * C O N T I N U E * * * * *R OP 01 OPERATIONAL CHECK OF ADF 1 IN EMERGENCY CONFIGURATION 9 I: CPRE 47245PRE 53622ORPRE 47245POST 54662ORPRE 50859PRE 53622ORPRE 50859POST 54662ORPOST 50860PRE 53622ORPOST 50860POST 5466234.55.00 VOR/MARKERR OP 01 OPERATIONAL CHECK OF VOR 1 IN EMERGENCY CONFIGURATION 9 I: CPRE 53622ORPOST 5466234.58.00 SATELLITE NAVIGATION (IF INSTALLED)NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 NAVIGATION SECTION: C-34PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.00.00 OXYGEN35.10.00 CREW OXYGENR VC 01 VISUAL CHECK OF OXYGEN MASKS 9 I: 18 MOALL(OUT OF BOX WITH INFLATED HARNESS)RS 02 CLEAN OXYGEN MASKS 8 I: 18 MOALLOP 03 OPERATIONAL CHECK OF FULL-FACE QUICK-DONNING MASK 8 I: 18 MOALLNOTE 5R FC 04 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6,9 I: 72 MOALLFUNCTIONAL CHECK OF OXYGEN CYLINDER PRESSURE GAUGE. OR NROR VRR FC 05 REMOVE OXYGEN MASK REGULATOR FOR FUNCTIONAL CHECK 8 I: 72 MOALLN FC 06 REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL 8 I: 72 MOA330-200CHECK.ORA330-300N FC 07 CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN 8 I: 6500 FHA330-200FILL PANEL AND GAUGES ON OXYGEN CYLINDERS. OROR24 MOA330-300N OP 08 OPERATIONAL CHECK OF OXYGEN CYLINDER HANDVALVE 8 I: 72 MOA330-200FSWITCHES.N FC 09 FUNCTIONAL CHECK OF LOW PRESSURE SWITCH. 9 I: 40000 FHA330-200FOR72 MON FC 10 FUNCTIONAL CHECK OF OXYGEN SYSTEM PRESSURE HOLDING 8 I: 72 MOA330-200FCHARACTERISTICS AND OPERATIONAL CHECK OF BLEED/VENTVALVE.N FC 11 FUNCTIONAL CHECK OF ALTITUDE PRESSURE SWITCH. 9 I: 72 MOA330-200FN OP 12 OPERATIONAL CHECK OF OXYGEN MANUAL ACTIVATION AND 8 I: 24 MOA330-200FCONTAINER DOOR OPENING.N OP 13 OPERATIONAL CHECK OF THE CABIN OXYGEN SUPPLY OFF 8 I: 72 MOA330-200FINDICATION AND MONITORING FUNCTION.* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.10.00 * * * * * C O N T I N U E * * * * *N OP 14 OPERATIONAL CHECK OF REGULATION/DISTRIUTION DEVICE 8 I: 60 MOA330-200FIN OXYGEN MASK CONTAINERS.N DI 15 DETAILED INSPECTION OF CONTINOUS FLOW OXYGEN MASKS. 8 I: 72 MOA330-200FN OP 16 OPERATIONAL CHECK OF CABIN OXYGEN SYSTEM CONTROL AND 8 I: 48 MOA330-200FREDUNDANCY FUNCTIONS.N FC 17 REMOVE PRESSURE REDUCER TRANSMITTER FOR FUNCTIONAL 6,8 I: 60 MOA330-200FCHECK.N OP 18 CROSS CHECK OF QUANTITY INDICATIONS ON ECAM, OXYGEN 8 I: 2000 FHA330-200FFILL PANEL AND GAUGES ON OXYGEN CYLINDERS.35.20.01 PASSENGER OXYGEN (CHEMICAL)R FC 01 FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE 9 I: 4 CA330-200PRE 40257PRE 52485ORA330-300PRE 40257PRE 56322R DI 02 DETAILED INSPECTION OF OXYGEN MASKS 9 I: 4 CA330-200NOTE 27PRE 40257PRE 52485ORA330-300PRE 40257PRE 56322R OP 03 OPERATIONAL CHECK OF MANUAL MASK RELEASE 8 I: 6 YEA330-200PRE 40257PRE 52485ORA330-300PRE 40257PRE 56322* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.20.01 * * * * * C O N T I N U E * * * * *R VC 04 VISUAL CHECK OF CHEMICAL OXYGEN GENERATORS FOR SIGNS 8 I: 6 YEA330-200OF DISCHARGEPRE 40257PRE 52485ORA330-300PRE 40257PRE 56322R DS 05 DISCARD CHEMICAL OXYGEN GENERATORS 8 I: VRA330-200PRE 40257PRE 52485ORA330-300PRE 40257PRE 56322OP 06 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 CIF PASSENGERINTERRUPTIONOXYGEN SYSTEM(CHEMICAL) ANDINSEAT POWERSUPPLYINSTALLEDVC 07 VISUAL CHECK OF CRR CHEMICAL OXYGEN GENERATORS FOR 8 I: 6 YEIF CREW RESTSIGNS OF DISCHARGE. NOTE 26ROOM WITHCHEMICALOXYGENINSTALLEDDS 08 DISCARD CRR CHEMICAL OXYGEN GENERATORS. 8 I: VRIF CREW RESTNOTE 26ROOM WITHCHEMICALOXYGENINSTALLED35.20.02 PASSENGER OXYGEN (GASEOUS)* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R FC 01 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST AND 6 I: NR OR VRA330-200FUNCTIONAL CHECK OF PRESSURE REDUCER NOTE 8POST 40257NOTE 24ORPOST 52485ORA330-300POST 40257ORPOST 56322R VC 02 CROSS-CHECK OF QUANTITY INDICATIONS ON ECAM 8 I: 1400 FHA330-200"DOOR/OXY"-PAGE, OXYGEN FILL PANEL AND OXYGENPOST 40257CYLINDERSORPOST 52485ORA330-300POST 40257ORPOST 56322R FC 03 FUNCTIONAL CHECK OF AUTOMATIC SYSTEM OPERATION 8 I: 18 MOA330-200POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322R OP 04 OPERATIONAL CHECK OF THE SYSTEM SHUT-OFF VALVES 8 I: 18 MOA330-200(MOD.40257)/ PRESSURE REGULATORS (MOD.52485/56322)POST 40257OPENING.ORPOST 52485ORA330-300POST 40257ORPOST 56322* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R OP 05 OPERATIONAL CHECK OF MANUAL SYSTEM OPERATION 8 I: 18 MOA330-200POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322R OP 06 OPERATIONAL CHECK OF "SYS ON" LIGHT BY ANNUNCIATOR 9 I: 1600 FHA330-200LIGHT TESTPOST 40257(COVERED BY MSI 33-14-00 TASK NO1).ORPOST 52485ORA330-300POST 40257ORPOST 56322R OP 07 OPERATIONAL CHECK OXYGEN CONTAINER OPENING AND VENT 8 I: 30 MOA330-200FUNCTION OF BLEED/VENT VALVE NOTE 24POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322R FC 08 FUNCTIONAL CHECK OF PRESSURE HOLDING/DECAY 8 I: 30 MOA330-200CHARACTERISTICS OF OXYGEN DISTRIBUTION SYSTEM NOTE 24POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R VC 09 VISUAL CHECK OF OVERBOARD DISCHARGE LINE FOR DAMAGE 8 I: 60 MOA330-200POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322R DI 10 DETAILED INSPECTION OF OXYGEN MASK ASSEMBLIES 8 I: 6 YEA330-200NOTE 24POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322R OP 11 OPERATIONAL CHECK OF REGULATION/DISTRIBUTION DEVICES 8 I: 60 MOA330-200IN OXYGEN MASK CONTAINERSPOST 40257PRE 52485ORA330-300POST 40257PRE 56322R FC 12 REMOVE RISER LINE SHUT-OFF VALVES FOR FUNCTIONAL 8 I: 60 MOA330-200CHECK NOTE 24POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 6APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.20.02 * * * * * C O N T I N U E * * * * *R OP 13 OPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEM 8 I: 60 MOA330-200NOTE 24POST 40257ORPOST 52485ORA330-300POST 40257ORPOST 56322OP 14 OPERATIONAL CHECK OF IN SEAT POWER SUPPLY 9 I: 4 CIF PASSENGERINTERRUPTIONOXYGEN SYSTEM(GASEOUS) ANDINSEAT POWERSUPPLYINSTALLEDR FC 15 REMOVE PRESSURE RELIEF VALVE FOR FUNCTIONAL CHECK 9 I: 60 MOA330-200NOTE 24POST 52485ORA330-300POST 56322R FC 16 REMOVE PRESSURE REGULATOR FOR PRESSURE REGULATING 8 I: 60 MOA330-200AND LEAKAGE TEST IN THE SHOP NOTE 24POST 52485ORA330-300POST 56322R OP 17 OPERATIONAL CHECK OF CYLINDER VALVE SWITCH 9 I: 4 CA330-200POST 52485ORA330-300POST 5632235.30.00 PORTABLE OXYGENVC 01 VISUAL CHECK OF TAMPER SEAL/SERVICEABILITY INDICATION 8 I: 8 DYALLOF PROTECTIVE BREATHING EQUIPMENT NOTE 26VC 02 CHECK PRESSURE OF OXYGEN CYLINDER BY READING GAUGE 9 I: 8 DYALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 7APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section35.30.00 * * * * * C O N T I N U E * * * * *R FC 03 REMOVE OXYGEN CYLINDER FOR HYDROSTATIC TEST 9 I: NRPRE 55559ORVRR DS 04 DISCARD PROTECTIVE BREATHING EQUIPMENT 8 I: VRALLNOTE 26R VC 05 VISUAL CHECK OF OXYGEN CYLINDER ATTACHMENT 9 I: 72 MOALLN DI 06 DETAILED INSPECTION OF THE OXYGEN CONTINOUS FLOW MASK 9 I: 24 MOALLN FC 07 REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR 9 I: VRPOST 55559HYDROSTATIC TEST INCLUDING FUNCTIONAL CHECK OF OROXYGEN REGULATOR. NR* * * * * E N D * * * * *ISSUE: JUL 01/10 OXYGEN SECTION: C-35PAGE 8APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section36.00.00 PNEUMATIC36.00.00 PNEUMATICDI 01 REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION 6 I: 6400 FHCF6 80E1OP 02 OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE 9 I: 4000 FCALLFC 03 FUNCTIONAL CHECK OF OVERPRESSURE VALVE 9 I: 2 CALLOP 04 OPERATIONAL CHECK OF CLOSING SIGNAL TO TEMPERATURE 9 I: CALLLIMITATION THERMOSTAT SOLENOID FROM FIRE P/B SW(COVERED BY MSI 26-21-00, TASK NO3).GVI 05 GENERAL VISUAL INSPECTION OF NACA AIR INLETS OF WING 9 I: C ZL-521-01-1 ALLVENTILATION SYSTEM FOR BLOCKAGE AND DAMAGE.R DI 06 REMOVE IP BLEED CHECK VALVE FOR DETAILED INSPECTION 6 I: 10000 FHPWORRRR DI 07 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: CPRE 5741808 TASK RESERVED09 TASK RESERVED10 TASK RESERVED11 TASK RESERVEDN DI 12 REMOVE APU BLEED CHECK VALVE FOR DETAILED INSPECTION 9 I: 10000 FCPOST 57418* * * * * E N D * * * * *ISSUE: JUL 01/10 PNEUMATIC SECTION: C-36PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section38.00.00 WATER/WASTE38.10.00 POTABLER RS 01 DISINFECTION OF POTABLE WATER SYSTEM. 9 I: 3 MOA330-200NOTE 8ORA330-300N DS 02 DISCARD WATER FILTER CARTRIDGE OF THE LAVATORIES 7,9 I: 3 MOA330-200NOTE 8POST 42704ORA330-300POST 42704ORA330-200POST 49951ORA330-300POST 49951ORA330-200POST 57459ORA330-300POST 57459N DS 03 DISCARD WATER FILTER CARTRIDGE OF THE GALLEYS 7,9 I: 3 MOA330-200NOTE 8ORA330-300IF INSTALLED38.10.01 POTABLE WATERN RS 01 DISINFECTION OF POTABLE WATER SYSTEM. 9 I: 3 MOA330-200FORNRN DS 02 DISCARD WATER FILTER CARTRIDGE. 9 I: 3 MOA330-200FORIF WATERNRFILTERCARTRIDGEINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section38.10.01 * * * * * C O N T I N U E * * * * *N DS 03 DISCARD AIR MANIFOLD FILTER. 9 I: 40000 FHA330-200FN RS 04 RESTORATION, BY CLEANING OF COMPRESSOR AIR INLET 9 I: 25000 FHA330-200FFILTER. ORPOST 5821572 MON DS 05 DISCARD COMPRESSOR OUTLET AIR FILTER. 9 I: 40000 FHA330-200FPOST 5821538.31.00 TOILET SYSTEM01 TASK DELETEDR GVI 02 GENERAL VISUAL INSPECTION OF WASTE TANKS AND WASTE 9 I: 4 C ZL-171-02-1 A330-200DRAIN LINESORA330-300R DS 03 DISCARD WATER SEPARATOR. 9 I: 4 AA330-200NOTE 1ORA330-300R RS 04 CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING 6 I: 350 FHA330-200AGENT AND CRUSHED ICE. NOTE 1ORA330-300R RS 05 CLEANING OF LIQUID LEVEL SENSORS, WASTE TANKS AND 6,9 I: CA330-200WASTE DRAIN LINES.ORA330-300R RS 06 CLEANING OF FILTER OF POLAR CAP ASSY 9 I: 4 AA330-200NOTE 1ORA330-300R RS 07 CLEANING OF RINSE NOZZLES AND REFERENCE PRESSURE LINE 7,9 I: 4 AA330-200OF LIQUID LEVEL TRANSMITTER. NOTE 1ORA330-300N 08 TASK RESERVEDN 09 TASK RESERVEDN 10 TASK RESERVED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section38.31.00 * * * * * C O N T I N U E * * * * *N 11 TASK RESERVEDN 12 TASK RESERVEDN OP 13 OPERATIONAL CHECK OF BIDET ́S SPRAY NOZZLE. 9 I: 600 FHA330-200NOTE 1POST 55776ORA330-300POST 5577638.31.01 TOILET SYSTEMN DI 01 DETAILED INSPECTION OF FLUSH NIPPLE CAP AND THE 9 I: 24 MOA330-200FOVERFLOW PORT CAP.N DI 02 DETAILED INSPECTION OF WASTE CAP DRAIN VALVE. 6 I: 24 MOA330-200FN RS 03 CLEANING OF FILTER ELEMENT OF WASHBASIN SINK DRAIN 9 I: 2000 FHA330-200FASSEMBLY. NOTE 138.32.00 WASTE WATER DRAINR GVI 01 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN 9 I: 4 C ZL-133-01-1 A330-200LINES IN BILGE AREA FOR LEAKAGE. ZL-153-01-1 ORZL-153-01-2 A330-300ZL-171-02-1R GVI 02 GENERAL VISUAL INSPECTION OF WASTE WATER DRAIN 9 I: 8 C ZL-131-03-1 A330-200LINES IN CARGO COMPARTMENTS FOR LEAKAGE. ZL-151-03-1 ORZL-161-01-1 A330-300ZL-161-03-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section38.32.00 * * * * * C O N T I N U E * * * * *R RS 03 CLEANING OF FILTER ELEMENTS OF WASHBASIN DRAIN VALVE 7 I: 600 FHA330-200POST 45556ORA330-200POST 49705ORA330-200POST 50088ORA330-300POST 45556ORA330-300POST 49705ORA330-300POST 5008838.40.00 AIR SUPPLYR DI 01 DETAILED INSPECTION OF COMPRESSOR INLET FILTER 9 I: 2 CA330-200POST 40243ORA330-300POST 40243R DS 02 DISCARD SYSTEM FILTER ELEMENT 6,9 I: 4 CA330-200ORA330-300R DS 03 DISCARD COMPRESSOR OUTLET FILTER ELEMENT 9 I: 4 CA330-200POST 40243ORA330-300POST 40243* * * * * E N D * * * * *ISSUE: JUL 01/10 WATER/WASTE SECTION: C-38PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section45.00.00 ONBOARD MAINTENANCE SYSTEM45.10.00 CENTRAL MAINTENANCE SYSTEM (CMS)01 TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 ONBOARD MAINTENANCE SYSTEM SECTION: C-45PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section46.00.00 INFORMATION SYSTEMS46.11.00 FLYSMART WITH AIRBUSN RS 01 CALIBRATION OF BASE TRANSCEIVER STATION 7 I: VRA330-200POST 58640ORA330-300POST 5864046.11.34 SIU (SERVER INTERFACE UNIT)NO TASK SELECTED46.21.00 ATIMSNO TASK SELECTED46.21.01 ATIMS FANS CONFIGURATIONSR NO TASK SELECTED46.55.00 ON-BOARD INFORMATION TERMINAL (OIT)N NO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 INFORMATION SYSTEMS SECTION: C-46PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionAPU 331-35049.00.00 AIRBORNE AUXILIARY POWER49.12.00 APU MOUNTSVC 01 VISUAL CHECK OF APU SUSPENSION SYSTEM INCLUDING 9 I: CALLSHOCKMOUNT STRUCTURE AND BRACKETS49.13.00 FIRE SEALSGVI 01 GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE 8 I: 20000 FHALLWALLS INCLUDING FORWARD, AFT, UPPER, SIDE ANDCOMPARTMENT DOORS49.16.00 AIR INTAKE SYSTEMGVI 01 GENERAL VISUAL INSPECTION OF DIVERTER AND FLUID 9 I: 2 C ZL-311-01-1 ALLGUTTERS ZL-313-01-149.17.00 POWERPLANT DRAIN SYSTEM01 TASK RESERVEDGVI 02 GENERAL VISUAL INSPECTION OF DRAIN PIPES 9 I: C ZL-315-01-1 ALLZL-317-01-149.20.00 ENGINENO TASK SELECTED49.23.00 LOAD COMPRESSORNO TASK SELECTED49.26.00 ACCESSORY DRIVE GEARBOXNO TASK SELECTEDISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-49PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section49.30.00 FUEL DISTRIBUTION AND CONTROLVC 01 VISUAL CHECK OF DIFFERENTIAL PRESSURE INDICATOR 9 I: 1500 AHALLBUTTON ON FUEL FILTER49.34.00 APU FUEL LOW PRESSURE WARNINGNO TASK SELECTED49.40.00 IGNITION AND STARTINGNO TASK SELECTED49.51.00 BLEED AND SURGE AIRNO TASK SELECTED49.52.00 ACCESSORY COOLINGNO TASK SELECTED49.60.00 ENGINE CONTROLSNO TASK SELECTED49.62.00 EMERGENCY SHUTDOWNOP 01 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CALLAPU STOP SWITCH 1KLOP 02 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT USING 9 I: 2 CALLAPU STOP SWITCH 2KLNOTE: IT IS RECOMMENDED THAT BOTH TASKS 1 AND 2 AREPERFORMED ALTERNATELYOP 03 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT (APU 9 I: 2 CALLFIRE 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-49PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section49.62.00 * * * * * C O N T I N U E * * * * *R OP 04 OPERATIONAL CHECK OF EMERGENCY SHUTDOWN CIRCUIT. (APU 9 I: 2 CALLFIRE P/B SW)(COVERED BY MSI 26-22-00, TASK NO10)49.70.00 INDICATINGNO TASK SELECTED49.80.00 EXHAUSTVC 01 VISUAL CHECK OF V-CLAMP AND EXHAUST DUCT 9 I: CALLVC 02 VISUAL CHECK OF EXHAUST DUCT HEAT INSULATION 9 I: 2 CALLDI 03 DETAILED INSPECTION OF SEALING RING COUPLING AND 9 I: 2 CALLBELLOWS49.90.00 OILVC 01 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON LUBE 9 I: 500 AHPRE 56284FILTER.VC 02 CHECK DIFFERENTIAL PRESSURE INDICATOR BUTTON ON 9 I: 500 AHPRE 56284GENERATOR SCAVENGE FILTER* * * * * E N D * * * * *ISSUE: JUL 01/10 AIRBORNE AUXILIARY POWER SECTION: C-49PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section52.00.00 DOORS52.10.00 PASSENGER/CREW DOORSR LU 01 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 6,9 I: CA330-200HANDLENOTENOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDORREGULARLY DURING DAY TO DAY OPERATION. ANY DOORA330-300INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGERNOTECOMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/02R OP 02 OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN 9 I: CA330-200POSITIONNOTENOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDORREGULARLY DURING DAY TO DAY OPERATION. ANY DOORA330-300INFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGERNOTECOMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/0303 TASK DELETEDR FC 04 FUNCTIONAL CHECK OF LOCKING MECHANISM 6,9 I: 2 CA330-200NOTE: TASKS APPLY ONLY WHEN THE DOOR IS USEDNOTEREGULARLY DURING DAY TO DAY OPERATION. ANY DOORORINFREQUENTLY USED SHALL BE MAINTAINED AS A PASSENGERA330-300COMPARTMENT EMERGENCY EXIT. REFER TO MSI 52-22-00/05NOTEOP 05 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 CALLIS OPENED FROM OUTSIDEOP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 CALLLEVER IS LOCKED IN DISARMED POSITION WHEN DOOR ISOPENGVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-831-01-1 ALLZL-832-01-1ZL-833-01-1VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 CALLFITTINGSFC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MOALLSLIDER.N LU 10 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 6,9 I: CA330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section52.10.00 * * * * * C O N T I N U E * * * * *HANDLE.NOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. INTERVAL FORANY DOOR INFREQUENTLTY USED IS 18 MO.N OP 11 OPERATIONAL CHECK OF DOOR LATCHING IN FULLY OPEN 6,9 I: CA330-200FPOSITION.NOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. INTERVAL FORANY DOOR INFREQUENTLTY USED IS 18 MO.N FC 12 FUNCTIONAL CHECK OF LOCKING MECHANISM. 6,9 I: 2 CA330-200FNOTE: INTERVAL APPLIES ONLY WHEN THE DOOR IS USEDREGULARLY DURING DAY TO DAY OPERATION. INTERVAL FORANY DOOR INFREQUENTLTY USED IS 36 MO.52.22.00 PASSENGER COMPARTMENT EMERGENCY EXITR OP 01 OPERATIONAL CHECK OF DOOR DAMPING, ESCAPE SLIDE 9 I: CA330-200RELEASE MECHANISM DISARMING, AND TO ENSURE THAT DOORORCANNOT BE LOWERED AND LOCKED WHEN OPENA330-300R LU 02 LUBRICATION OF TELESCOPIC ARM AND EXTERIOR CONTROL 8 I: 18 MOA330-200HANDLEORA330-300R OP 03 OPERATIONAL CHECK OF DOOR UNLOCKING/LOCKING AND DOOR 8 I: 18 MOA330-200OPENING/CLOSING FROM INSIDE AND OUTSIDE AND DOORORLATCHING IN FULLY OPEN POSITIONA330-300R OP 04 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 9 I: 2 CA330-200IS OPENED FROM OUTSIDEORA330-300R FC 05 FUNCTIONAL CHECK OF LOCKING MECHANISM 8 I: 36 MOA330-200ORA330-300R OP 06 OPERATIONAL CHECK TO ENSURE THAT ESCAPE SLIDE ARMING 9 I: 4 CA330-200LEVER IS LOCKED IN DISARMED POSITION WHEN DOOR ISOROPENA330-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section52.22.00 * * * * * C O N T I N U E * * * * *R GVI 07 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-834-01-1 A330-200ORA330-300R VC 08 VISUAL CHECK TO CONFIRM PRESENCE OF DOOR STOP 9 I: 4 CA330-200FITTINGSORA330-300R FC 09 FUNCTIONAL CHECK AND LUBRICATION OF DOOR GIRT BAR 8 I: 18 MOA330-200SLIDER.ORA330-30052.31.00 FWD AND AFT CARGO COMPARTMENT DOORLU 01 LUBRICATION OF HINGE ARM BEARINGS AND OF LOCKING, 6,9 I: CALLLATCHING AND INTERLOCK MECHANISMSFC 02 FUNCTIONAL CHECK OF LATCHING AND LOCKING HANDLE 6,9 I: 4 CALLFORCES, AND OF WEAR AND OVERCENTER POSITIONS OFLATCHING, LOCKING AND INTERLOCK MECHANISMSGVI 03 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-821-01-1 ALLZL-822-01-152.33.00 BULK CARGO COMPARTMENT DOOROP 01 OPERATIONAL CHECK OF DOOR BALANCE MECHANISM AND OF 9 I: CALLDOOR LATCHING IN FULLY OPEN POSITIONGVI 02 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-823-01-1 ALLLU 03 LUBRICATION OF BULK CARGO COMPARTMENT DOOR COMPONENTS 6 I: CALL52.36.00 CARGO COMPARTMENT DOOR HYDRAULIC SYSTEMNO TASK SELECTED52.38.00 MAIN DECK CARGO COMPARTMENT DOOR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section52.38.00 * * * * * C O N T I N U E * * * * *N LU 01 LUBRICATION OF DOOR HINGE. 9 I: 24 MOA330-200FN FC 02 FUNCTIONAL CHECK OF LATCHING AND LOCKING MECHANISM. 6,9 I: 72 MOA330-200FN VC 03 VISUAL CHECK OF DRAIN VALVES. 9 I: 72 MOA330-200FN GVI 04 GENERAL VISUAL INSPECTION OF GUIDE FITTING. 9 I: 24 MO ZL-835-01-1 A330-200FN GVI 05 GENERAL VISUAL INSPECTION OF DOOR STOP BOLTS. 9 I: 24 MO ZL-835-01-1 A330-200FN GVI 06 GENERAL VISUAL INSPECTION OF DOOR SEAL AND RETAINER 9 I: 24 MO ZL-835-01-1 A330-200FPROFILE.N LU 07 LUBRICATION OF LATCHING MECHANISM, LOCKING MECHANISM, 6,9 I: 18 MOA330-200FSEQUENCE SHAFT AND INTERLOCK MECHANISM.52.41.11 AVIONICS COMPARTMENT FWD DOORGVI 01 GENERAL VISUAL INSPECTION OF DOOR SEAL 9 I: C ZL-811-01-1 ALL52.51.11 COCKPIT DOORR FC 01 FUNCTIONAL CHECK OF SPRING LOADED DOOR STOP MECHANISM 9 I: 2 CA330-200PRE 50014ORA330-300PRE 50014R DI 02 DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR 6,9 I: 2 CPOST 50014LOCKING SYSTEMORA330-200FIF COCKPIT DOORINSTALLEDR OP 03 OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS 9 I: 2 CPOST 50014FOR RAPID DECOMPRESSION, CHECK OF DOOR OPENING INORCASE OF POWER OFF AND BY USING THE EMERGENCY CODEA330-200FIF COCKPIT DOORINSTALLED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 4APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section52.51.11 * * * * * C O N T I N U E * * * * *R OP 04 OPERATIONAL CHECK OF DECOMPRESSION FLAP RELEASE 8 I: 11000 FHPOST 50014MECHANISM NOTE 24PRE 57371R DI 05 DETAILED INSPECTION OF FLAP BELLOW 8 I: 36 MOPOST 50014PRE 57371OP 06 OPERATIONAL CHECK OF MANUAL SWITCH OVER 9 I: 2 CPOST 50723ORPOST 53123N OP 07 OPERATIONAL CHECK OF FLAP RELEASE MECHANISM (MANUAL 8 I: 72 MOPOST 57371OPENING).ORA330-200FIF COCKPIT DOORINSTALLEDN GVI 08 GENERAL VISUAL INSPECTION OF AIR CYLINDER OF 8 I: 72 MOPOST 57371DECOMPRESSION PANEL.ORA330-200FIF COCKPIT DOORINSTALLED52.70.00 DOOR WARNINGOP 01 OPERATIONAL CHECK OF DOOR WARNING SYSTEM 9 I: 4 CALLFC 02 CHECK BATTERY CAPACITY OF AUTONOMOUS STANDBY POWER 9 I: 8 MOALLSUPPLY UNIT (ASPSU)OP 03 BITE TEST OF AUTONOMOUS STANDBY POWER SUPPLY UNIT 9 I: 4 AALL(ASPSU)OP 04 OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE 9 I: 2 CALLWARNING SYSTEMFC 05 OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING 9 I: 4 CALLSYSTEM AND FUNCTIONAL CHECK OF ASSOCIATED PRESSURESWITCH* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: C-52PAGE 5APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section53.00.00 FUSELAGE53.19.00 FUSELAGE DRAINSVC 01 VISUAL CHECK OF DRAIN HOLES IN LOWER PART OF FR1 AND 9 I: CALLFR80 (FROM INSIDE)VC 02 VISUAL CHECK OF PISTON TYPE DRAIN VALVES IN LOWER 9 I: CALLFUSELAGE SHELL (FROM OUTSIDE) AND IN FWD AND AFTCARGO COMPARTMENT DOORSOP 03 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT UPPER 9 I: CALLAFT END OF CENTER WING BOX (FROM MAIN LANDING GEARBAY).OP 04 OPERATIONAL CHECK OF DRAIN MAST/PIPES AFT OF FR80. 9 I: 5 MOALLOP 05 OPERATIONAL CHECK OF DRAIN HOLES IN UNPRESSURIZED 9 I: CALLPART OF FUSELAGE (IN RADOME, FORWARD OF FR1, BEHINDREAR PRESSURE BULKHEAD, IN BELLY FAIRING, TAIL CONEAND IN CARGO COMPARTMENT DOORS).VC 06 VISUAL CHECK OF HOLES OF PISTON TYPE DRAIN OR 9 I: 4 CALLPRESSURE DRAIN VALVES AND PRESSURE SEAL DRAINS FROMINSIDE (IN FUSELAGE BILGE AREA, AT UPPER AFT END OFCENTER WING BOX AND IN CARGO COMPARTMENT DOORS).07 TASK RESERVED08 TASK RESERVEDOP 09 OPERATIONAL CHECK OF PRESSURE SEAL DRAINS AT BULK 9 I: CALLCARGO COMPARTMENT DOOR (FROM OUTSIDE).N VC 10 VISUAL CHECK OF DRAIN FUNNEL(S) IN BARRIER WALL. 9 I: 4 CA330-200F* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE SECTION: C-53PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400054.00.00 NACELLES/PYLONS54.59.00 PYLON DRAINS (PW 4000)R OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 CPWF AND OF HYDRAULIC AND FUEL PAN DRAIN SYSTEM* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 PW 4000PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E54.00.00 NACELLES/PYLONS54.59.00 PYLON DRAINS (GE CF6-80E1)OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 CCF6 80E1F AND OF HYDRAULIC AND FUEL PAN DRAIN SYSTEM* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 CF6-80EPAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70054.00.00 NACELLES/PYLONS54.59.00 PYLON DRAINS (RR TRENT 768/772)OP 01 OPERATIONAL AND VISUAL CHECK OF COMPARTMENT A, C AND 9 I: 2 CRRF DRAIN SYSTEM* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: C-54 T700PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section55.00.00 STABILIZERS55.16.00 TRIMMABLE HORIZONTAL STABILIZER ATTACH FITTINGSLU 01 LUBRICATION OF THS HINGE LINE BEARINGS 9 I: 7500 FHALLOR18 MOLU 02 LUBRICATION OF UPPER AND LOWER FRAME ATTACHMENT 9 I: 7500 FHALLBEARINGS OR18 MO* * * * * E N D * * * * *ISSUE: JUL 01/10 STABILIZERS SECTION: C-55PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section56.00.00 WINDOWS56.12.00 SLIDING WINDOWSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 WINDOWS SECTION: C-56PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section57.00.00 WINGS57.29.00 WING DRAINS (OUTER WING)OP 01 OPERATIONAL CHECK OF DRAIN HOSES AND DESIGNATED DRAIN 9 I: 4 CALLHOLES FOR CLOGGING57.39.00 WING DRAINS (WING TIP)OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 CALL57.59.00 WING DRAINS (LEADING/TRAILING EDGE AND LEADING/TRAILING EDGEDEVICES)OP 01 OPERATIONAL CHECK OF DRAIN HOLES FOR CLOGGING 9 I: 4 CALL* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: C-57PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E71.00.00 POWERPLANT71.10.00 ENGINE COWLINGDI 01 DETAILED INSPECTION OF AIR INTAKE COWL INNER BARREL 9 I: CCF6 80E1ASSEMBLY02 TASK DELETED03 TASK DELETEDGVI 04 GENERAL VISUAL INSPECTION OF FIRESHIELD, FIRE SEALS 8 I: 18 MOCF6 80E1AND HEAT BLANKETSFC 05 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 9 I: CCF6 80E171.70.00 POWERPLANT DRAINSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-CF6-80E-71PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E72.00.00 ENGINE72.20.00 FAN SECTIONDI 01 DETAILED INSPECTION OF FAN BLADES AND SPINNER 6 I: 4500 FHCF6 80E1DS 02 DISCARD LIFE LIMITED PARTS OF LP COMPRESSOR 5 I: NOTE 4CF6 80E1DI 03 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FHCF6 80E1(COVERED BY MSI 79-20-00, TASK NO2)72.30.00 HP COMPRESSOR SECTIONDS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4CF6 80E1DI 02 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FHCF6 80E1(COVERED BY MSI 79-20-00, TASK NO2)72.40.00 COMBUSTION SECTIONNO TASK SELECTED72.50.00 TURBINE SECTIONSDI 01 BORESCOPE INSPECTION OF STAGE 1 AND STAGE 2 HP 6 I: 500 FCCF6 80E1TURBINE BLADESNOTE: OPERATOR SHOULD CONTACT THE OEM TO ADJUST THEINTERVAL FOR LOW FLIGHT LENGTHDS 02 DISCARD LIFE LIMITED PARTS OF HPT AND LPT ROTORS 5 I: NOTE 4CF6 80E1DI 03 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FHCF6 80E1(COVERED BY MSI 79-20-00, TASK NO2)72.60.00 ACCESSORY DRIVE SECTIONDI 01 CHECK MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: 1000 FHCF6 80E1(COVERED BY MSI 79-20-00, TASK NO2)* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-CF6-80E-72PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E73.00.00 ENGINE FUEL AND CONTROL73.00.00 ENGINE FUEL AND CONTROL GENERALDS 01 DISCARD FUEL FILTER 9 I: 6000 FHCF6 80E102 TASK DELETED03 TASK DELETED73.25.00 FUNCTIONAL INTERFACEOP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CCF6 80E1(COVERED BY MSI 21-26-00, TASK NO2).* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-CF6-80E-73PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E74.00.00 IGNITION74.00.00 IGNITION GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 IGNITION SECTION: C-CF6-80E-74PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E75.00.00 AIR75.00.00 AIR GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR SECTION: C-CF6-80E-75PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E76.00.00 ENGINE CONTROLS76.00.00 ENGINE CONTROLS GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-CF6-80E-76PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E77.00.00 ENGINE INDICATING77.00.00 ENGINE INDICATING GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-CF6-80E-77PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E78.00.00 EXHAUST78.11.00 COLLECTOR/NOZZLENO TASK SELECTED78.31.00 THRUST REVERSER CONTROL/ACTUATION SYSTEMRS 01 REMOVE AND REPACK ANGLE GEARBOX 6 I: 6000 FCCF6 80E1LU 02 LUBRICATE FLEXIBLE DRIVE SHAFTS 6 I: CCF6 80E1LU 03 LUBRICATE BALLSCREW ACTUATORS 6 I: 1000 FCCF6 80E1FC 04 HOLDING TORQUE CHECK OF THE CDU CONE BRAKE 9 I: 4 CCF6 80E1NOTE 24DI 05 DETAILED INSPECTION OF TRANSCOWL INNER BONDMENT SEAL 9 I: 4 CCF6 80E1AND MATING SURFACES (FORWARD FAIRING AND AFT FRAME NOTE 24ASSEMBLY)FC 06 HOLDING TORQUE CHECK OF THE THRUST REVERSER 9 I: 7000 FHCF6 80E1ELECTROMECHANICAL BRAKE NOTE 24FC 07 THRUST REVERSER DIRECTIONAL PILOT VALVE LEAK CHECK 9 I: 7000 FHCF6 80E178.32.00 THRUST REVERSER ASSEMBLYVC 01 VISUAL CHECK OF THE BLOCKER DOORS, HINGES AND 9 I: CCF6 80E1ADJACENT STRUCTURE WITH T/R DEPLOYEDVC 02 VISUAL CHECK OF FAN REVERSER DEFLECTORS WITH T/R 9 I: CCF6 80E1DEPLOYED03 TASK DELETED04 TASK DELETED05 TASK DELETED* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-CF6-80E-78PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section78.32.00 * * * * * C O N T I N U E * * * * *GVI 06 GENERAL VISUAL INSPECTION OF REVERSER 8 I: 18 MOCF6 80E1FIRESHIELD/SEALSGVI 07 GENERAL VISUAL INSPECTION OF FIRE PROTECTION COATING 8 I: 18 MOCF6 80E1GVI 08 GENERAL VISUAL INSPECTION OF FAN EXIT FLOWPATH 9 I: C ZL-417-02-1 CF6 80E1SURFACES* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-CF6-80E-78PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E79.00.00 OIL79.11.00 OIL SYSTEM STORAGENO TASK SELECTED79.20.00 DISTRIBUTIONDS 01 DISCARD OIL SCAVENGE FILTER ELEMENT 6 I: CCF6 80E1DI 02 CHECK THE MASTER CHIP DETECTOR FOR PARTICLES 6 I: 1000 FHCF6 80E1(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 SYSTEMNO TASK SELECTED79.32.00 OIL TEMPERATURE INDICATING SYSTEMNO TASK SELECTED79.33.00 OIL PRESSURE INDICATING SYSTEMNO TASK SELECTED79.34.00 LOW OIL PRESSURE WARNING SYSTEMNO TASK SELECTED79.35.00 OIL FILTER CLOGGING WARNING SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-CF6-80E-79PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionCF6-80E80.00.00 STARTING80.00.00 ENGINE STARTING SYSTEMSV 01 STARTER OIL CHANGE 6 I: 1600 FHCF6 80E1OR800 FCDI 02 STARTER OIL LEVEL CHECK 6 I: ACF6 80E1DI 03 INSPECTION OF STARTER CHIP DETECTOR 6 I: 1600 FHCF6 80E1OR800 FC* * * * * E N D * * * * *ISSUE: JUL 01/10 STARTING SECTION: C-CF6-80E-80PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400071.00.00 POWERPLANT71.13.00 FAN COWLDI 01 DETAILED INSPECTION OF AIR INTAKE COWL LIP AND INNER 9 I: CPWSKIN02 TASK DELETED03 TASK DELETEDFC 04 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 8 I: 18 MOPW71.70.00 POWERPLANT DRAINSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-PW 4000-71PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400072.00.00 ENGINE72.31.00 LOW PRESSURE COMPRESSOR GROUPDI 01 DETAILED INSPECTION OF FAN BLADES 6 I: 2100 FHPW02 TASK DELETEDDS 03 DISCARD FAN HUB AND LPC DRUM ROTOR 5 I: NOTE 4PW04 TASK TRANSFERED TO MSI 72.32.00/01DI 05 DETAILED INSPECTION OF INLET CONE 6 I: 4 APW72.32.00 LPC/LPT COUPLING GROUPDS 01 DISCARD LPC/LPT COUPLING 5 I: NOTE 4PW72.33.00 FAN CASES GROUPGVI 01 GENERAL VISUAL INSPECTION OF FAN CASE RUB STRIP FOR 9 I: 4 A ZL-400-01-1 PWDAMAGEGVI 02 GENERAL VISUAL INSPECTION OF FAN CASE, ACOUSTIC 9 I: C ZL-412-02-2 PWLINERS AND FAN EXIT GUIDE VANES72.34.00 INTERMEDIATE CASE GROUPDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: APW(COVERED BY MSI 79.20.00, TASK NO1)72.35.00 HIGH PRESSURE COMPRESSOR GROUPDS 01 DISCARD LIFE LIMITED PARTS OF HP COMPRESSOR 5 I: NOTE 4PW72.41.00 DIFFUSER, COMBUSTION & TURBINE NOZZLE GROUP* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-PW 4000-72PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section72.41.00 * * * * * C O N T I N U E * * * * *SDI 01 BORESCOPE INSPECTION OF INNER AND OUTER COMBUSTION 9 I: 700 FCPWCHAMBER ASSEMBLIES AND FIRST STAGE VANES OR2400 FHDI 02 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: APW(COVERED BY MSI 79.20.00, TASK NO1)72.52.00 HIGH PRESSURE TURBINE GROUPSDI 01 BORESCOPE INSPECTION OF THE FIRST AND SECOND STAGE 6 I: 700 FCPWHIGH PRESSURE TURBINE BLADES OR2400 FHDS 02 DISCARD LIFE LIMITED PARTS OF HP TURBINE 5 I: NOTE 4PW72.53.00 LOW PRESSURE TURBINE GROUPDS 01 DISCARD LIFE LIMITED PARTS OF LP TURBINE 5 I: NOTE 4PW72.54.00 TURBINE EXHAUST SECTIONDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: APW(COVERED BY MSI 79.20.00, TASK NO1)72.61.00 MAIN GEARBOX SECTIONDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: APW(COVERED BY MSI 79.20.00, TASK NO1)* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-PW 4000-72PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400073.00.00 ENGINE FUEL AND CONTROL73.10.00 FUEL DISTRIBUTIONDS 01 DISCARD FUEL FILTER ELEMENT 6 I: 5000 FHPW73.20.00 FUEL CONTROLNO TASK SELECTED73.25.00 FADEC FUNCTIONAL INTERFACEOP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CPWSYSTEM(COVERED BY MSI 21.26.00 TASK NO2)73.30.00 FUEL INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-PW 4000-73PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400074.00.00 IGNITION74.00.00 ENGINE IGNITIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 IGNITION SECTION: C-PW 4000-74PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400075.00.00 AIR75.20.00 ACCESSORY COOLING SYSTEMNO TASK SELECTED75.30.00 COMPRESSOR CONTROL SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR SECTION: C-PW 4000-75PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400076.00.00 ENGINE CONTROLS76.00.00 ENGINE CONTROLS GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-PW 4000-76PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400077.00.00 ENGINE INDICATING77.00.00 ENGINE INDICATING GENERALNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-PW 4000-77PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400078.00.00 EXHAUST78.31.00 THRUST REVERSER CONTROL AND INDICATING SYSTEMNO TASK SELECTED78.32.00 THRUST REVERSER STRUCTUREGVI 01 GENERAL VISUAL INSPECTION OF CASCADES AND BLOCKER 9 I: C ZL-417-02-2 PWDOOR ATTACHMENTSGVI 02 GENERAL VISUAL INSPECTION OF TRANSLATING COWL FORWARD 9 I: C ZL-417-02-2 PWSEAL.GVI 03 GENERAL VISUAL INSPECTION OF FIXED STRUCTURE SEALS 8 I: 18 MOPWGVI 04 GENERAL VISUAL INSPECTION OF FIRE BLANKET 8 I: 18 MOPW78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-PW 4000-78PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400079.00.00 OIL79.10.00 OIL SYSTEM STORAGENO TASK SELECTED79.20.00 ENGINE OIL SYSTEM DISTRIBUTIONDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR PARTICLES 6 I: APW(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 INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-PW 4000-79PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionPW 400080.00.00 STARTING80.00.00 ENGINE STARTING SYSTEM01 TASK DELETEDSV 02 CHANGE STARTER OIL 6 I: 600 FHPWDI 03 INSPECT STARTER CHIP DETECTOR FOR PARTICLES 6 I: 600 FHPW* * * * * E N D * * * * *ISSUE: JUL 01/10 STARTING SECTION: C-PW 4000-80PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70071.00.00 POWERPLANT71.12.00 FAN COWL01 TASK DELETED02 TASK DELETEDGVI 03 GENERAL VISUAL INSPECTION FOR THE PRESENCE AND 9 I: C ZL-412-02-3 RRSECURITY OF FAN COWL DOORS ZONE 1/AMBIENT SEALSFC 04 FUNCTIONAL CHECK OF FAN COWL LATCH TENSION 8 I: 18 MORR71.61.00 AIR INTAKE COWLGVI 01 GENERAL VISUAL INSPECTION OF THE AIRWASHED SURFACES 9 I: 4 ARRFOR DISTORTION AND SECURITY OF INSTALLATIONGVI 02 GENERAL VISUAL INSPECTION FOR THE PRESENCE AND 9 I: C ZL-412-02-3 RRSECURITY OF NOSE COWL SEAL71.71.00 POWERPLANT DRAINSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: C-RR T700-71PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70072.00.00 ENGINE72.03.00 GAS GENERATOR FAIRINGSGVI 01 GENERAL VISUAL INSPECTION FOR SIGNIFICANT FAIRING 9 I: C ZL-413-02-3 RRDAMAGE AND/OR MISSING PANELS72.31.00 LP COMPRESSOR MODULEDI 01 DETAILED INSPECTION OF LP COMPRESSOR BLADES 6 I: 2 ARRDS 02 DISCARD LIFE LIMITED PARTS OF THE LP COMPRESSOR 5 I: NOTE 4RRLU 03 RE-LUBRICATION OF LP COMPRESSOR BLADE ROOT COATINGS 6 I: 1200 FCRR72.32.00 IP COMPRESSOR MODULEDS 01 DISCARD LIFE LIMITED PARTS OF THE IP COMPRESSOR 5 I: NOTE 4RR(THIS TASK COVERS TASK 72-33-00/01-RR)72.33.00 COMPRESSOR INTERMEDIATE MODULEDS 01 DISCARD LIFE LIMITED PARTS OF THE IP COMPRESSOR 5 I: NOTE 4RR(COVERED BY MSI 72-32-00, TASK NO1)DI 02 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FHRRABNORMAL DEPOSITSWITH EMCD(COVERED BY MSI 79-20-00, TASK NO1)NOT INSTALLED03 TASK DELETEDDI 04 DETAILED INSPECTION OF EMCD 6 I: 130 FHRR(COVERED BY MSI 79-30-00, TASK NO2)WITH EMCDINSTALLEDPRE 5671372.33.40 EXTERNAL GEARBOX DRIVE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-72PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section72.33.40 * * * * * C O N T I N U E * * * * *DI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FHRRABNORMAL DEPOSITSWITH EMCD(COVERED BY MSI 79-20-00, TASK NO1)NOT INSTALLEDDI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FHRR(COVERED BY MSI 79-30-00, TASK NO2)WITH EMCDINSTALLEDPRE 5671372.34.00 LP COMPRESSOR CASINGGVI 01 GENERAL VISUAL INSPECTION OF THE FAN TRACK AND COLD 9 I: 1000 FHRRSTREAM DUCT, AS FAR AS VISIBLE FROM THE FRONT, FORSIGNIFICANT DAMAGEGVI 02 GENERAL VISUAL INSPECTION OF THE SPLITTER FAIRING 9 I: 4 ARRFOR SIGNIFICANT DAMAGE72.41.00 COMBUSTION SECTIONSDI 01 BORESCOPE INSPECTION OF COMBUSTION LINER 9 I: 1500 FCRROR6000 FH72.41.20 HP COMPRESSOR SECTIONDS 01 DISCARD LIFE LIMITED PARTS OF THE HP COMPRESSOR 5 I: NOTE 4RR72.41.50 HP TURBINE SECTIONSDI 01 BORESCOPE INSPECTION OF HP TURBINE NOZZLE GUIDE VANES 6 T: 2000 FCRROR8500 FHI: 1500 FCOR6000 FH* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-72PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section72.41.50 * * * * * C O N T I N U E * * * * *SDI 02 BORESCOPE INSPECTION OF HP TURBINE BLADES 6 T: 2000 FCRROR8500 FHI: 1500 FCOR6000 FHDS 03 DISCARD LIFE LIMITED PARTS OF THE HP TURBINE 5 I: NOTE 4RR72.51.00 IP/LP TURBINE MODULEDS 01 DISCARD LIFE LIMITED PARTS OF THE IP TURBINE 5 I: NOTE 4RR72.52.00 LP TURBINE MODULEDS 01 DISCARD LIFE LIMITED PARTS OF THE LP TURBINE 5 I: NOTE 4RR72.61.00 EXTERNAL GEARBOX MODULEDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FHRRABNORMAL DEPOSITSWITH EMCD(COVERED BY MSI 79-20-00, TASK NO1)NOT INSTALLEDDI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FHRR(COVERED BY MSI 79-30-00, TASK NO2)WITH EMCDINSTALLEDPRE 5671372.62.11 QUILLSHAFT AND SHROUDNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE SECTION: C-RR T700-72PAGE 3APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70073.00.00 ENGINE FUEL AND CONTROL73.10.00 FUEL DISTRIBUSTIONDS 01 DISCARD LP FUEL FILTER ELEMENT 9 I: 6000 FHRR73.20.00 FUEL CONTROLNO TASK SELECTED73.25.00 FADEC FUNCTIONAL INTERFACEOP 01 OPERATIONAL CHECK OF LOW EXTRACTION FLOW WARNING 9 I: 2 CRR(COVERED BY MSI 21-26-00, TASK NO2)73.30.00 FUEL INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE FUEL AND CONTROL SECTION: C-RR T700-73PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70074.00.00 IGNITION74.00.00 IGNITION SYSTEMNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 IGNITION SECTION: C-RR T700-74PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70075.00.00 AIR75.21.00 ACCESSORY/ZONE COOLINGNO TASK SELECTED75.22.00 ENGINE COOLING AND SEALINGNO TASK SELECTED75.23.00 BEARING COMPARTMENT COOLINGNO TASK SELECTED75.24.00 TURBINE CASE COOLINGNO TASK SELECTED75.33.00 IP/HP COMPRESSOR AIRFLOW CONTROLNO TASK SELECTED75.41.00 NACELLE TEMPERATURE INDICATIONNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 AIR SECTION: C-RR T700-75PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70076.00.00 ENGINE CONTROLS76.00.00 ENGINE CONTROLSNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE CONTROLS SECTION: C-RR T700-76PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70077.00.00 ENGINE INDICATING77.00.00 ENGINE INDICATINGNO TASK SELECTED* * * * * E N D * * * * *ISSUE: JUL 01/10 ENGINE INDICATING SECTION: C-RR T700-77PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70078.00.00 EXHAUST78.11.00 EXHAUST COLLECTOR/NOZZLEVC 01 VISUAL CHECK OF THE FIRE SEALS 8 I: 1600 FHRR78.31.00 THRUST REVERSER CONTROL AND INDICATIONNO TASK SELECTED78.32.00 THRUST REVERSER STRUCTUREGVI 01 GENERAL VISUAL INSPECTION OF THE FAN EXIT FLOW PATH 9 I: C ZL-417-02-3 RRSURFACES02 TASK DELETED03 TASK DELETEDGVI 04 GENERAL VISUAL INSPECTION OF THE ZONE 1/AMBIENT FIRE 8 I: 18 MORRSEALVC 05 VISUAL CHECK OF THE INNER FIXED STRUCTURE FIRE SEALS 8 I: 18 MORRGVI 06 GENERAL VISUAL INSPECTION OF THE PIVOT DOOR 9 I: 6000 FHRRDEFLECTOR PLATES, MOVEABLE PANELS AND MECHANISM(THRUST REVERSER DEPLOYED)GVI 07 GENERAL VISUAL INSPECTION OF FRONT FRAME AND INNER 9 I: 2 ARRFIXED STRUCTURE THERMAL BLANKETSOP 08 OPERATIONAL CHECK OF THE SECONDARY AND TERTIARY LOCKS 9 I: 2 CRR(THIS TASK COVERS TASK 78.37.00/01-RR)09 TASK DELETED78.37.00 THRUST REVERSER INDEPENDENT LOCKING SYSTEMOP 01 OPERATIONAL CHECK OF THE TERTIARY LOCKS 9 I: 2 CRR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: C-RR T700-78PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant Section78.37.00 * * * * * 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 T700-78PAGE 2APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70079.00.00 OIL79.10.00 OIL SYSTEM STORAGENO TASK SELECTED79.20.00 OIL DISTRIBUTIONDI 01 INSPECT MASTER MAGNETIC CHIP DETECTOR FOR EVIDENCE OF 6 I: 130 FHRRABNORMAL DEPOSITSWITH EMCD(THIS TASK COVERS TASK 72.33.00/02-RR,NOT INSTALLED72.33.40/01-RR, 72.61.00/01-RR)RS 02 REMOVE, CLEAN AND REINSTALL PRESSURE OIL FILTER 6 I: 1600 FHRRELEMENTDS 03 REMOVE, DISCARD AND REPLACE OIL SCAVENGE FILTER 9 I: 1600 FHRR79.30.00 OIL INDICATING SYSTEMRS 01 CLEANING AND FUNCTIONAL CHECK OF EMCD 6,9 I: 2500 FHRRPOST 56713DI 02 DETAILED INSPECTION OF EMCD 6 I: 130 FHRR(THIS TASK COVERS TASKS 72.33.00/04-RR,WITH EMCD72.33.40/02-RR, 72.61.00/02-RR)INSTALLEDPRE 56713* * * * * E N D * * * * *ISSUE: JUL 01/10 OIL SECTION: C-RR T700-79PAGE 1APPLICABILITYMSIREFERENCETASKMSI AND TASK DESCRIPTIONFECINTERVALZIPREFERENCEA330MRB REPORT – Systems and Powerplant SectionRR T70080.00.00 STARTING80.11.00 PNEUMATIC STARTINGSV 01 STARTER OIL CHANGE AND INSPECTION OF STARTER CHIP 6,9 I: ARRDETECTORSV 02 STARTER OIL REPLENISHMENT 6,9 I: 400 FHRR* * * * * E N D * * * * *ISSUE: JUL 01/10 STARTING SECTION: C-RR T700-80PAGE 1

# 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 REPORTIssue : July 2010 Page : D-INTRO-5Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/YrS.T = 50000 FH= Aircraft InspectionI= 6100 FC10Yrs15Yrs20Yrs25YrsTASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY572011-02-1DI 20000 FCOR50000 FH6100 FCOR24500 FHGRP 32A572011-02-2DI 20000 FCOR50000 FH5700 FCOR17800 FHGRP 33AORGRP 33B572011-02-3DI 20000 FCOR50000 FH6000 FCOR18800 FHGRP 33CExample 1 : SSI 57201132A1232A1132A1032A932A832A732A632A532A432A332A232A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-6Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/YrS.T = 50000 FH= Aircraft InspectionI= 5700 FCI= 6100 FC10Yrs15Yrs20Yrs25YrsExample 2 : SSI 572011TASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY572011-02-1DI 20000 FCOR50000 FH6100 FCOR24500 FHGRP 32A572011-02-2DI 20000 FCOR50000 FH5700 FCOR17800 FHGRP 33AORGRP 33B572011-02-3DI 20000 FCOR50000 FH6000 FCOR18800 FHGRP 33C32B1232B1132B1032B932B832B732B632A532A432A332A232A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-7Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/Yr= Aircraft Inspection100% T= 25800 FC10Yrs15Yrs20Yrs25YrsExample 3 : SSI 531134TASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY531134-01-1SDI20000 FC35400 FC 7000 FC531134-01-2SDI20000 FC25800 FC3500 FCGRP 32AORGRP 33CGRP 33AORGRP 33BS.T = 20000 FCI = 3500 FC32A1232A1132A1032A932A832A732A632A532A432A332A232A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-8Yrs, FC, FH= Sampling ProgramAircraft= Aircraft DeliveryAircraft Utilisation: 950 FC/Yr3000 FH/Yr= Aircraft InspectionI= 7500 FCI= 7500 FC10Yrs15Yrs20Yrs25YrsExample 4 : SSI 533135TASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL APPLICABILITY535103-01-1DI 10 YEOR16500 FC20 YE 10 YEOR7500 FCALLS.T = 10 Yrs100% T= 16500 FC33B1233B1133B1033B933B833B733B633A533A433A333A233A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-9Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/YrT= 12100 FC= Aircraft InspectionExample 5 : SSI 533154NOTE: A/C 1 to 4 are Pre mod 41652I= 8100 FC10Yrs15Yrs20Yrs25YrsTASK REF Level SAMPLE100% THRESHOLDINTERVALAPPLICABILIT533154-01-4DI 12100 FC8100 FCGRP 33APRE 41652ORGRP 33BPRE 41652533154-01-5DI20000 FC13300 FCGRP 33APOST 41652ORGRP 33BPOST 41652ORGRP 32AORGRP 33CI= 8100 FC33A1233A1133A1033A933A833A733A633A533A433A333A233A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-10Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/YrT= 20000 FC= Aircraft InspectionExample 6 : SSI 53315410Yrs15Yrs20Yrs25YrsNOTE: A/C 1 to 4 are Pre mod 41652TASK REF Level SAMPLE100% THRESHOLDINTERVALAPPLICABILIT533154-01-4DI 12100 FC8100 FC GRP 33APRE 41652ORGRP 33BPRE 41652533154-01-5DI20000 FC13300 FCGRP 33APOST 41652ORGRP 33BPOST 41652ORGRP 32AORGRP 33CT= 12100 FCI= 8100 FCI= 8100 FC33B1233B1133B1033B933B833B733A633A533A433A333A233A1GrpA/CA330 MRB REPORTIssue : July 2010 Page : D-INTRO-11Yrs, FC, FH= Sampling Program Aircraft= Aircraft DeliveryAircraft Utilisation: 1100 FC/Yr3000 FH/YrT= 10 Yrs= Aircraft InspectionI= 6200 FCExample 7: SSI 574109T= 15800 FC100% T= 20000 FCI= 8200 FC10Yrs15Yrs20Yrs25YrsTASK REF LevelSAMPLETHRESHOL100%THRESHOLINTERVAL EFFECTIVITY574109-02-1DI 10 YE20 YEOR20000 FCOR50000 FH10 YEOR8200 FCOR29500 FHGRP 33C574109-02-2DI 10 YE20 YEOR15600 FCOR49200 FH10 YEOR6200 FCOR19500 FHGRP 33AORGRP 33B574109-02-3DI 10 YE20 YEOR20000 FCOR50000 FH10 YEOR7900 FCOR24900 FHGRP 32AI= 8200 FCI= 6200 FC33A1233A1133A1033A933A833A733A632A532A432A332A232A1GrpA/C

# 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 Lev el 3 in a given area, then the existing program is

not effective for the concerned area.

In addition to the considerations given for Leve l 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% Th reshold/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 in spection 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 A3 3 0

Y : Model ( 2 for – 2 00 / 3 for – 3 00)

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

EXAMPLES

GROUP 32A : A3 3 0- 2 00 WV 020, 021, 022, 023, 024, 025, 026, 027

(1 st 

# WV Group of A330-200 Series)

GROUP 33B : A3 3 0- 3 00 WV 010, 011, 012, 013, 014

(2 nd 

# WV group of A330-300 Series)A330MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-1810. EXPLANATION OF STRUCTURES SECTION FORMATDetailed information is given below concerning the format of the inspection requirements provided on subsequent pages.TASKREFERENCEACCESSZONETASKDESCRIPTIONSAMPLETHRESHOLDINTERVAL100%THRESHOLDINTERVALTPSCPCPZIPREFERENCEAPPLICABILITY1 2 3 4 5 6 7 8 9 101. This column indicates the SSI task number, e.g. 531109-01-1. It is composed of 9 or 10 digits as follows:XXXXXX – XX – XXThe SSI number is represented by the six first digits, 531109.The first set of two digits are in accordance with the A330 ATA100 breakdown, showing the majorsection where the SSI is located e.g 53 Fuselage. The second set of two digits are also in accordance with the A330 ATA 100 breakdown, showing the subsection where the SSI is located e.g 53-11 Fwd fuselage. The third set of two digits are sequential numbers within the sectione.g 01, 02, 03 up to 99.The Sequential Number is composed of two digits. It follows the SSI number and is separated by a dash e.g. 531109-01. It identifies different inspectionse.g.Detailed or Special Detailed. These two digits are also changed when the inspection areas are physically different (e.g. rib 8 or rib 9) or when the inspectionshave a major difference in access (e.g. actuator removal).The Applicability Index is composed of either one or two digits. Numbers 1 to 9 have one digit; numbers 10 and subsequent have2 digits. It follows the SequentialNumber and is separated by a dash, 531109-01-1. It identifies different applicability e.g aircraft series, mod status, WV groupetc ...The digits are also used todifferentiate between minor access differences e.g. different access panel numbers.Applicability indexSequence numberSSInumberA330MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-192. This column indicates the access requirement to adequately perform the required maintenance task, i.e. all items listed must be removed or opened (E.g hingedpanels or doors) unless otherwise stated (e.g. to be lifted).3. This column indicates the zone(s) where the SSI is located. For the zone boundaries refer to Zone Diagrams, APPENDIX 2.4. This column describes the task to be performed, additional information may be added to clarify the inspection area. Detailsof partial application of TPS areprovided, where applicable. The SSI description states the boundaries of the inspection area. All items within this boundary are to be inspected e.g. fasteners,cutouts, attachments, unless otherwise stated.5 This column indicates the Sample Threshold and the repeat Interval. This requirement is only applicable to selected sample A/C.6. This column indicates the 100% Threshold and the repeat interval. This requirement is applicable to all A/C.7.This column indicates if a Temporary Protection System (TPS) is to be applied, as indicated below:‘ ‘ : A blank indicates that application of TPS is at the discretion of the operator.‘1’ : Type 1 Grade 2 or Grade 3 TPS is to be applied.‘1+2’ : Type 1 TPS plus a subsequent application of Type 2 TPS is to be applied.‘2’ : Type 2 TPS is to be applied.‘3’ : Type 3 TPS is to be applied.'No' : TPS must not be applied in the area (example: inside fuel tank, pylon).Note: If “1+2” is stated in the TPS column, it is at the discretion of the operator to apply either “Type 1 TPS plus Type 2 TPS”or“Type 3 TPS”If “3” is stated in the TPS column, it is at the discretion of the operator to apply either “Type 3 TPS”or“Type 1 TPS plus Type 2 TPS”The technical specification for corrosion preventive temporary protective compounds can be found in the Process and Material Specifications Manual (PMS),Volume 5 , Section 02-16-00.8. This column indicates whether the considered task is a CPCP requirement.9. This column indicates the equivalent zonal tasks which cover the SSI task requirements.10. This column indicates the A/C model/mod status/engine type to which this requirement is applicable. Some examples are givenbelow:A330MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-20Applicability Task applicable toALL All A330 aircraft.A330-200-200 PAXseries aircraftonlyA330-200F-200 Freighter series onlyPRE nnnnn All A330 PRE MOD nnnnn.i.e. A330 that do nothave MOD nnnnn embodied.POST nnnnnAll A330 POST MOD nnnnn.i.e. A330 that dohave MOD nnnnn embodied.POST nnnnn Sxxxxx All A330 POST MOD nnnnn (at least with mod proposal no. Sxxxxx embodied).POST nnnnnPOST mmmmmAll A330 POST MOD nnnnn and POST MOD mmmmm.i.e. A330 that dohave MOD nnnnn andMOD mmmmm embodied.A330-200ORA330-300PRE nnnnnAll A330-200 PAXOr,All A330-300 that do nothave MOD nnnnn embodied.A330-200POST nnnnnORPOST mmmmAll A330-200 PAX that dohave MOD nnnnn embodied,Or,All A330-200 PAX that dohave MOD mmmm embodied.A330-200POST nnnnnORA330-300POST nnnnnPRE mmmmmAll A330-200 PAX that dohave MOD nnnnn embodied,Or,All A330-300 that dohave MOD nnnnn embodied anddo nothave MOD mmmmm embodied.POST nnnnn(xx-yyyy)All A330 that dohave MOD nnnnn embodied.(xx-yyyy) is the Service Bulletin reference associated to the modification.GE All A330 equipped with GE CF6-80 E1 engines.A330MRB REPORT - StructuresIssue : July 2010Page : D-INTRO-21Applicability Task applicable toPW 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 XYZGROUP XYZPRE nnnnAll aircraft with weight variant group XYZ that do nothave MOD nnnn embodiedGROUP XYZPOST nnnnAll aircraft with weight variant group XYZ that dohave MOD nnnn embodiedAPPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS321101-01-1 N/A 731 DETAILED INSPECTION OF MLG MAIN FITTING T: 6 YE CPCP ALL741 I: 6 YE321102-01-1 MLG FULLY EXTENDED 731 DETAILED INSPECTION OF MLG SLIDING MEMBER T: 6 YE CPCP ALL741 I: 6 YE321103-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG STATIC PISTON T: 10 YE CPCP ALL741 I: 10 YE321104-01-1 N/A 731 DETAILED INSPECTION OF MLG BOGIE BEAM T: 6 YE CPCP ALL741 I: 6 YE321105-01-1 MLG PITCH TRIMMER 731 DETAILED INSPECTION OF MLG PITCH TRIMMER T: 6 YE CPCP ALLEXTENDED 741 I: 6 YE321106-01-1 N/A 731 DETAILED INSPECTION OF MLG SIDESTAY ASSEMBLY T: 6 YE CPCP ALL741 I: 6 YE321107-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCK STAY ASSEMBLY T: 6 YE CPCP ALL741 I: 6 YE321108-01-1 AT MLG RESTORATION 731 DETAILED INSPECTION OF MLG AXLES T: 10 YE CPCP ALL741 I: 10 YE321109-01-1 N/A 731 DETAILED INSPECTION OF MLG TORQUE LINK, LOWER AND T: 6 YE CPCP ALL741 UPPER I: 6 YE321110-01-1 N/A 731 DETAILED INSPECTION OF MLG ARTICULATING LINK, LOWER T: 6 YE CPCP ALL741 AND UPPER I: 6 YE321114-01-1 PINS 731 DETAILED INSPECTION OF BOGIE PIVOT PIN, SIDESTAY ASSY T: 10 YE CPCP ALL741 PINS, TORQUE LINKS, LOCKSTAY PINS, SIDESTAY ATTACH I: 10 YEPINS, ARTICULATING LINKAGE PINS, PITCH TRIMMER ATTACHPINS, FORWARD PINTLE PINS AND SHORTENING LINKAGE PINSISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS321124-01-1 N/A 731 DETAILED INSPECTION OF MLG LOCKSTAY ACTUATOR T: 6 YE CPCP ALL741 I: 6 YE321125-01-1 MLG FULLY LOWERED 570 DETAILED INSPECTION OF MLG PINTLE PINS AT OUTER WING T: 10 YE CPCP ALL670 TRAILING EDGE I: 10 YE321126-01-1 PINS 570 DETAILED INSPECTION OF MLG SHORTENING MECHANISM AT T: 10 YE CPCP ALL670 OUTER WING TRAILING EDGE I: 10 YE321127-01-1 PINS 570 DETAILED INSPECTION OF MLG ECCENTRIC EARTHING PIN AT T: 10 YE CPCP ALL670 OUTER WING TRAILING EDGE I: 10 YE322101-01-1 N/A 711 DETAILED INSPECTION OF NLG MAIN FITTING (BARREL) T: 6 YE CPCP ALLI: 6 YE322102-01-1 WHEELS AND SLEEVES, 711 DETAILED INSPECTION OF NLG SLIDING MEMBER T: 6 YE CPCP ALLSLIDING MEMBER FULLY I: 6 YEEXTENDED322103-01-1 N/A 711 DETAILED INSPECTION OF NLG TORQUE LINKS T: 6 YE CPCP ALLI: 6 YE322104-01-1 713 714 715 711 DETAILED INSPECTION OF NLG DRAGSTAY UPPER ARM T: 6 YE CPCP ALL716 I: 6 YE322105-01-1 N/A 711 DETAILED INSPECTION OF NLG DRAGSTAY LOWER ARM T: 6 YE CPCP ALLI: 6 YE322106-01-1 N/A 711 DETAILED INSPECTION OF NLG DOWNLOCK LINK T: 6 YE CPCP ALLI: 6 YEISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS322107-01-1 PINS 711 DETAILED INSPECTION OF NLG PINS : T: 10 YE CPCP ALL- 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 CPCP ALL716 I: 5 YEDRAG STRUTDISCONNECTEDPINTLE PIN* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: D-32PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS521101-01-1 N/A TASK DELETED521103-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD T: 6 YE CPCP ZL-800-01-1 ALLPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE I: 6 YE521103-01-2 N/A TASK DELETED521104-01-1 ESCAPE SLIDE 831 DETAILED INSPECTION OF DOOR 1 (FORWARD PASSENGER/CREW T: 6 YE 1 CPCP ALLINSULATION 841 DOOR), INTERNAL STRUCTURE I: 6 YELININGR 521201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 2 (MID T: 6 YE CPCP ZL-800-01-1 A330-200PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE I: 6 YEORA330-300521201-01-2 N/A TASK DELETEDR 521202-01-1 832 842 832 DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW T: 6 YE 1 CPCP A330-200ESCAPE SLIDE 842 DOOR), INTERNAL STRUCTURE I: 6 YEORINSULATIONA330-300LINING521203-01-1 N/A TASK DELETED521203-01-2 N/A TASK DELETEDR 521301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 4 (AFT T: 6 YE CPCP ZL-800-01-1 A330-200PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE I: 6 YEORA330-300521301-01-2 N/A TASK DELETEDISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 521302-01-1 833 843 833 DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW T: 6 YE 1 CPCP A330-200ESCAPE SLIDE 843 DOOR), INTERNAL STRUCTURE I: 6 YEORINSULATIONA330-300LINING521303-01-1 N/A TASK DELETED521303-01-2 N/A TASK DELETEDR 522201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF DOOR 3 T: 6 YE CPCP ZL-800-01-1 A330-200(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL I: 6 YEORSURFACEA330-300522201-01-2 N/A TASK DELETEDR 522202-01-1 834 844 834 DETAILED INSPECTION OF DOOR 3 T: 6 YE 1 CPCP A330-200ESCAPE SLIDE 844 (EMERGENCY/PASSENGER/CREW DOOR), INTERNAL STRUCTURE I: 6 YEORINSULATIONA330-300LINING522203-01-1 N/A TASK DELETED522203-01-2 N/A TASK DELETED523101-01-1 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE CPCP ZL-800-01-1 ALLCOMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 6 YER 523101-01-2 N/A 800 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 3000 FCZL-821-01-1 A330-200COMPARTMENT DOOR SKIN, EXTERNAL SURFACE I: 3000 FCORA330-300R 523102-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT T: 12 YE 1 CPCP ALL821CR 821DR DOOR, INTERNAL STRUCTURE I: 6 YELININGISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 523103-01-1 821 821AR 821BR 821 DETAILED INSPECTION OF LATCHING HOOKS OF FORWARD T: 12000 FCA330-200CARGO COMPARTMENT DOOR (10 PLACES) I: 9000 FCORA330-300523104-01-1 132AR 132BR 132CR 132 DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR T: 12 YE 1 CPCP ALL132DR 132ER 132FR 821 HINGE ASSEMBLIES AT FR 20B TO FR25 (10 PLACES). I: 12 YE132GR 132HR 132JR132KR 132LRR 523105-01-1 821 821 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FCA330-200FITTING OF FORWARD CARGO COMPARTMENT DOOR AT FR 22A I: 8300 FCORA330-300523106-01-1 N/A TASK DELETED523201-01-1 N/A 800 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE CPCP ZL-800-01-1 ALLDOOR SKIN, EXTERNAL SURFACE I: 6 YER 523201-01-2 N/A 822 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 3000 FCZL-822-01-1 A330-200DOOR SKIN, EXTERNAL SURFACE I: 3000 FCORA330-300R 523202-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, T: 12 YE 1 CPCP ALL822CR 822DR INTERNAL STRUCTURE I: 6 YELININGR 523203-01-1 822 822AR 822BR 822 DETAILED INSPECTION OF LATCHING HOOKS OF AFT CARGO T: 12000 FCA330-200COMPARTMENT DOOR (10 PLACES) I: 9000 FCORA330-300523204-01-1 152AR 152BR 152CR 152 DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR T: 12 YE 1 CPCP ALL152DR 152ER 152FR 822 HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES) I: 12 YE152GR 152HR 152JR152KR 152LRISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 523205-01-1 822 822 SPECIAL DETAILED INSPECTION OF ACTUATOR ATTACH T: 8300 FCA330-200FITTING OF AFT CARGO COMPARTMENT DOOR AT FR 62A I: 8300 FCORA330-300523301-01-1 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE CPCP ZL-800-01-1 ALLDOOR SKIN, EXTERNAL SURFACE I: 6 YER 523301-01-2 N/A 800 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 550 FCZL-823-01-1 A330-200DOOR SKIN, EXTERNAL SURFACE I: 550 FCORA330-300523302-01-1 823 823 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR, T: 12 YE 1 CPCP ALLLINING INTERNAL STRUCTURE I: 6 YE523303-01-1 823 823 DETAILED INSPECTION OF STOP FITTINGS ON BULK CARGO T: 12 YE 1 CPCP ALLCOMPARTMENT DOOR I: 12 YEN 523801-01-1 N/A 835 GENERAL VISUAL INSPECTION OF MAIN DECK CARGO DOOR T: 12 YE CPCP ZL-800-01-1 A330-200FSKIN, EXTERNAL SURFACE. I: 12 YEN 523802-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR, INTERNAL T: 12 YE 3 CPCP A330-200FLINING INSULATION STRUCTURE, EXCLUDING SIDE FRAMES AND ACTUATOR FRAME. I: 12 YEN 523803-01-1 835 835 DETAILED INSPECTION OF ACTUATOR ATTACH FITTINGS T: 12 YE 1 CPCP A330-200FLINING INSULATION INCLUDING RIVETING AND BUSH. I: 12 YEN 523804-01-1 835 835 DETAILED INSPECTION OF LOCKING MECHANISM, ATTACH T: 12 YE CPCP A330-200FMCD ACCESS PANELS FITTINGS AND SUPPORT STRUCTURE OF MAIN DECK CARGO I: 12 YEDOOR AT ALL FRAMES.N 523805-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR T: 12 YE CPCP A330-200FLATCHING HOOKS AND BOLTS. I: 12 YEN 523806-01-1 835 835 DETAILED INSPECTION OF PIANO HINGE FITTING AND HINGE T: 12 YE CPCP A330-200FPIN. I: 12 YEISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 523807-01-1 835 835 DETAILED INSPECTION OF MAIN DECK CARGO DOOR SIDE T: 12 YE CPCP A330-200FLINING INSULATION FRAMES AND STOP FITTINGS. I: 12 YE524101-01-2 N/A TASK DELETED524101-02-3 N/A 800 GENERAL VISUAL INSPECTION OF AVIONICS COMPARTMENT T: 6 YE CPCP ZL-811-01-1 ALLLOWER ACCESS DOOR SKIN, EXTERNAL SURFACE I: 6 YE524102-01-1 811 121 DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER T: 6 YE 1+2 CPCP ALLDOOR FLOOR PANEL 122 ACCESS DOOR INTERNAL STRUCTURE, INCLUDING DOOR STOPS I: 6 YE811 AND HINGE FITTINGS ON FUSELAGE524103-01-2 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ADOOR FLOOR PANEL 122 AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS I: 14300 FCOR811GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D524103-01-3 811 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32EDOOR FLOOR PANEL 122 AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS. I: 14300 FCOR811GROUP 33E528101-01-1 N/A 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, MAIN T: 3 YEZL-734-01-1 ALL744 DOOR, EXTERNAL SKIN, LH/RH I: 3 YE528102-01-1 734 744 734 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR, MAIN T: 3 YEZL-734-01-1 ALL744 DOOR, INTERNAL SKIN, LH/RH I: 3 YE528103-01-1 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, T: 12 YE 1 CPCP ALL744 FORWARD AND AFT FITTINGS, LH/RH I: 12 YE528104-01-1 N/A TASK DELETEDISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 528104-01-2 734 744 734 DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN DOOR, T: 6 YE 1 CPCP ALL744 CENTER FITTING AND SURROUNDING AREA (300 MM AROUND), I: 6 YELH/RHNOTE: TPS APPLICATION REQUIRED ON FITTING ONLY528201-01-1 N/A 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-1 ALL714 FORWARD DOOR, EXTERNAL SKIN, LH/RH I: 3 YE528202-01-1 713 714 713 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, T: 3 YEZL-713-01-1 ALL714 FORWARD DOOR, INTERNAL SKIN, LH/RH I: 3 YER 528203-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1 CPCP A330-200714 DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON I: 6 YEORFUSELAGE, LH/RHA330-300528203-01-2 N/A TASK DELETED528204-01-1 715 716 715 GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR, AFT T: 3 YEZL-715-01-1 ALL716 DOOR, EXTERNAL AND INTERNAL SKINS, LH/RH I: 3 YEN 528206-01-1 713 714 713 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD T: 6 YE 1 CPCP A330-200F714 DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON I: 6 YEFUSELAGE, LH/RHN 528207-01-1 715 716 715 DETAILED INSPECTION OF NOSE LANDING GEAR AFT DOOR, T: 6 YE 1 CPCP A330-200F716 HINGES (NO 4 & NO 5) INCLUDING FITTINGS ON FUSELAGE, I: 6 YELH/RH* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: D-52PAGE 6APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531101-01-1 INSULATION PANELS 110 DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE T: 6 YE 3 CPCP ALLRADOME OPENED BULKHEAD ATTACHED TO FR 1 I: 6 YE531102-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL T: 6 YE CPCP ALLVISIBLE PORTIONS OF FRAMEWORK BETWEEN FR 3 AND FR 10, I: 6 YELH/RH531103-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 6 YE CPCP ZL-200-01-1 ALL10 AND FR 18 FROM CABIN FLOOR LEVEL TO STR 9 (FWD AND I: 6 YEAFT), EXTERNAL SURFACE, LH/RH531104-01-1 RETAINERS 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 12 YE CPCP ALLPORTIONS OF FRAMEWORK COVERED BY RETAINERS I: 12 YE531105-01-1 N/A 200 DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL T: 6 YE CPCP ALLVISIBLE PORTIONS OF RETAINERS I: 6 YE531106-01-3 N/A TASK DELETED531106-01-4 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 AND T: 20000 FCGROUP 32AFR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, I: 10200 FCOREXTERNAL SURFACE, LH/RH.GROUP 33APOST 41652ORGROUP 33BPOST 41652ORGROUP 33CORGROUP 33D531106-01-5 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN T: 17000 FCGROUP 32EBETWEEN FR.9 AND FR.10A AT COCKPIT LATERAL WINDOW I: 10200 FCORLOWER CORNER AREA, EXTERNAL SURFACE, LH/RHGROUP 33EISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 531107-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE CPCP ZL-200-01-1 ALL0 AND FR 10 FROM FLOOR LEVEL TO CROWN CENTERLINE, I: 3 YEEXTERNAL SURFACE531110-02-2 N/A TASK DELETEDR 531111-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE CPCP ZL-200-01-1 ALL10 AND FR 18 FROM STR 9 (FWD & AFT) TO CROWN I: 3 YECENTERLINE, EXTERNAL SURFACE, LH/RH531112-01-1 N/A TASK DELETED531112-02-1 N/A TASK DELETEDR 531115-01-1 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 6 YE CPCP A330-200INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YEPRE 40347CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RHORA330-300PRE 40347R 531115-01-2 SCUFF PLATE 100 DETAILED INSPECTION OF SKIN AND FAIL SAFE RING (IF T: 12 YE CPCP A330-200INSTALLED) OF DOOR NO1 (FORWARD PASSENGER/CREW DOOR) I: 6 YEPOST 40347CUTOUT UNDERNEATH THE SCUFF-PLATE, LH/RHORA330-200FORA330-300POST 40347R 531116-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND JOINT T: 6 YE CPCP ZL-100-01-2 A330-200SURFACES BETWEEN FR 0 AND FR 18/19 BELOW CABIN FLOOR I: 6 YEORLEVEL, EXTERNAL SURFACEA330-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531117-01-1 AVIONIC BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP ALLPANELS 122 STRUCTURE BETWEEN FR 1 AND FR 20 FROM CABIN FLOOR I: 12 YENOTE 1 LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL INCLUDINGCABIN FLOOR SUPPORT STRUCTURE AND NLG BAY PANELS ANDBEAMSNOTE: TPS APPLICATION REQUIRED ONLY BETWEEN FR 10 ANDFR 20, EXCLUDING NLG BAY PANELS531118-01-1 N/A TASK DELETED531120-01-1 713 714 123 GENERAL VISUAL INSPECTION OF NLG BAY INTERNAL T: 6 YE 1+2 CPCP ALLSTRUCTURE, NOSE LANDING GEAR WELL PANELS I: 6 YE531120-01-2 N/A TASK DELETED531121-01-1 AVIONICS BAY FLOOR 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2 CPCP ALLPANEL 122 BETWEEN FR 10 AND FR 20 BELOW AVIONICS COMPARTMENT I: 12 YEFLOOR LEVEL531122-01-1 AVIONICS BAY FLOOR 121 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1+2 CPCP ALLPANEL 122 STRUCTURE BETWEEN FR 1 AND FR 10 BELOW AVIONICS I: 12 YECOMPARTMENT FLOOR LEVEL531123-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP ALL122 BELOW GALLEYS AND TOILETS FROM CABIN FLOOR LEVEL TO I: 6 YENOTEAVIONICS COMPARTMENT FLOOR LEVEL BETWEEN FR 10 AND FR13A, LH/RHNOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREFITTED IN THIS AREA.531124-01-3 N/A TASK DELETED531124-01-4 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531124-01-6 713 714 123 DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER T: 17000 FCGROUP 32ERADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT I: 17000 FCORPANEL, LH/RHGROUP 33E531125-01-3 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 20000 FCGROUP 33AAVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH I: 5700 FCORPANELSGROUP 33B531125-01-4 N/A TASK DELETED531125-01-5 811 821 121 SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO T: 17000 FCGROUP 32EAVIONIC BAY FLOOR 122 BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH I: 17000 FCORPANELSGROUP 33E531126-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR AFT SIDE T: 12 YE 1 CPCP ALL716 PANEL TRUNNION HOLE ZONES AND ATTACHMENTS, LH/RH I: 12 YE531127-01-1 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 20000 FCGROUP 33A716 STRUT FITTING LUG BORE I: 20000 FCORGROUP 33B531127-01-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR DRAG T: 20000 FCGROUP 32A716 STRUT FITTING LUG BORE I: 20000 FCORGROUP 33CORGROUP 33D531127-01-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 17000 FCGROUP 32E716 DRAG STRUT FITTING LUG BORE I: 17000 FCORGROUP 33E531129-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR T: 12 YE 1+2 CPCP ALL716 FITTING I: 12 YEBOLTSNLG ACTUATORDISCONNECTEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531129-02-2 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 20000 FCGROUP 32A716 ACTUATOR FITTING I: 4700 FCORBOLTSGROUP 33ANLG ACTUATORORDISCONNECTEDGROUP 33BORGROUP 33CORGROUP 33D531129-02-3 713 714 715 123 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR T: 17000 FCGROUP 32E716 ACTUATOR FITTING I: 11500 FCORBOLTSGROUP 33ENLG ACTUATORDISCONNECTED531130-01-2 N/A TASK DELETED531131-01-2 N/A TASK DELETED531131-02-2 N/A TASK DELETED531132-01-2 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32A122 FRAME 14 JOINT BETWEEN STRINGERS 28 AND 30 LEVEL, I: 12900 FCORLH/RHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531132-01-3 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32E122 FRAME 14 JOINT BETWEEN STRINGERS 28 AND 30 LEVEL, LH/ I: 17000 FCORGROUP 33E531133-01-3 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531133-01-4 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 17000 FCGROUP 32ENOTE 1 122 BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON I: 17000 FCORFRAME 12A AT STRINGER 26 LEVEL, LH/RHGROUP 33E531134-01-1 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33ADOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 7000 FCORSKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.GROUP 33B531134-01-2 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32ADOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 3500 FCORSKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.GROUP 33C531134-01-3 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33DDOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 3500 FCSKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.531134-01-4 FWD AVIONICS BAY 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32EDOOR OPENED 122 STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO I: 17000 FCORSKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.GROUP 33E531135-01-2 N/A TASK DELETED531136-01-2 N/A TASK DELETED531137-01-1 713 714 715 123 DETAILED INSPECTION OF NOSE LANDING GEAR DRAG STRUT T: 12 YE 1 CPCP ALL716 FITTING ATTACHMENTS TO UPPER AND FORWARD CANTED PANEL I: 12 YE531138-01-2 NOTE 1 110 DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD T: 20000 FCGROUP 32APANELS RADOME OPENED FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 I: 9200 FCORABOVE COCKPIT FLOOR LEVEL.GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 6APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531138-01-3 NOTE 1 110 DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD T: 17000 FCGROUP 32EPANELS RADOME OPENED FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 I: 9200 FCORABOVE COCKPIT FLOOR LEVEL.GROUP 33E531139-01-2 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 212 FORWARD PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND I: 9200 FCORUPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPITGROUP 33AFLOOR LEVEL.ORGROUP 33BORGROUP 33CORGROUP 33D531139-01-3 811 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 212 PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND UPPER I: 9200 FCORSHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT FLOORGROUP 33ELEVEL531140-01-1 N/A TASK DELETED531141-01-2 N/A TASK DELETED531142-01-2 CEILING PANELS 211 DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER T: 20000 FCGROUP 32ANOTE 1 212 BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, I: 5250 FCORSPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.GROUP 33AORNOTE: THIS TASK IS AN ALTERNATIVE TO TASKGROUP 33B531142-02-2ORGROUP 33CORGROUP 33D531142-01-3 CEILING PANELS 211 DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER T: 17000 FCGROUP 32ENOTE 1 212 BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, I: 5250 FCORSPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.GROUP 33ENOTE: THIS TASK IS AN ALTERNATIVE TO TASK531142-02-3ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 7APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531142-02-2 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED T: 20000 FCGROUP 32ANOTE 1 212 MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL I: 7800 FCORSPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.GROUP 33AORNOTE: THIS TASK IS AN ALTERNATIVE TO TASKGROUP 33B531142-01-2ORGROUP 33CORGROUP 33D531142-02-3 CEILING PANELS 211 SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED T: 17000 FCGROUP 32ENOTE 1 212 MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL I: 7800 FCORSPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.GROUP 33ENOTE: THIS TASK IS AN ALTERNATIVE TO TASK531142-01-3531143-01-2 N/A TASK DELETED531143-01-3 AIR DUCTS 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 122 FLOOR BEAM AND CRUCIFORM FITTING AT FR.14, LH/RH I: 4000 FCORVACUUM PIPESGROUP 33E531144-01-2 N/A TASK DELETEDR 531144-01-3 LINING 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32ENOTE 1 122 STRUCTURE, JUNCTION AREA BETWEEN FRAME 14 AND I: 7100 FCORTOILET CRUCIFORM FITTING, LH/RH.GROUP 33E531146-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 212 LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 I: 8750 FCORUPPER MEMBER, LH/RH.GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 8APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531146-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 212 LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 I: 8750 FCORUPPER MEMBER, LH/RH.GROUP 33E531149-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 212 ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING I: 8500 FCORTOP 3 NUTS ON CENTRE POST.GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531149-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 212 ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, I: 8500 FCORINCLUDING TOP 3 NUTS ON CENTRE POSTGROUP 33ER 531150-01-1 311VU 312VU 313VU 211 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP ALL314VU 811 212 BULKHEAD ABOVE FLOOR LEVEL, INCLUDING FR1, AS FAR AS I: 12 YEACCESS BETWEEN FR1 A VISIBLEND FR2 FROM AVIONICBAY NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THENOTE 1 PRESSURE BULKHEAD (SEE SSI 531151-01-1) THE COMPLETEAFT FACE (UPPER AND LOWER AREA) HAS TO BE INSPECTEDAND ELECTRONIC DEVICE REMOVED.R 531151-01-1 AVIONICS FORWARD 121 DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE T: 12 YE 1 CPCP ALLFLOOR PANELS 122 BULKHEAD BELOW LOWER SURFACE OF COCKPIT FLOOR PANELS, I: 6 YENOTE 1 INCLUDING FR 1 AND STRINGER CONNECTIONS.WIRING BUNDLESDISPLACED NOTE: IF CORROSION IS FOUND ON THE LOWER PART OF THEPRESSURE BULKHEAD (SEE SSI 531151-01-1) THECOMPLETE AFT FACE (UPPER AND LOWER AREA) HAS TOBE INSPECTED AND ELECTRONIC DEVICE REMOVED.531152-01-1 LINING 211 DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND T: 12 YE T: 20 YE CPCP ALLNOTE 1 212 CLOSING PANELS, INTERNAL STRUCTURE (FR 10 AND I: 12 YE I: 12 YEFORWARD).ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 9APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531154-01-2 N/A TASK DELETED531154-01-3 LINING 211 DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING T: 17000 FCGROUP 32ENOTE 1 212 PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, I: 8100 FCORSLIDING WINDOWS INTERNAL STRUCTURE, LH/RH.GROUP 33EOPENED531156-01-1 CEILING PANELS 211 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-211-02-1 ALLFCRC (IF INSTALLED) 212 STRUCTURE ABOVE FLOOR LEVEL, FROM FR 1 TO FR 17, I: 12 YEZL-221-02-1GALLEYS AND TOILETS 221 EXCLUDING :ZL-223-01-1NOTE 1 222 - UPPER AFT FACE OF FORWARD PRESSURE BULKHEAD,OVERHEAD PANELS 223 - WINDSHIELD AND WINDOW FRAMES SURROUNDINGS BETWEENSIDEWALL PANELS 224 FWD COCKPIT AND FR 10,- INTERNAL STRUCTURE AROUND DOOR 1 (FORWARDPASSENGER/CREW DOOR)531157-01-2 LINING 233 DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPER T: 20000 FCGROUP 33ANOTE 1 234 KEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL, I: 10170 FCPRE 41652INTERNAL STRUCTURE, LH/RH.ORGROUP 33BPRE 41652531158-01-1 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 212 JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 I: 15600 FCORAND 9 UPPER MEMBERS, LH/RH.GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531158-01-2 LINING 211 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 212 JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 I: 15600 FCORAND 9 UPPER MEMBERS, LH/RHGROUP 33EISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 10APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531159-01-1 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1+2 CPCP ALLNOTE 1 222 AROUND DOOR 1 (FORWARD PASSENGER/CREW DOOR), BETWEEN I: 6 YEFR 13A AND FR 17 AND BETWEEN FLOOR LEVEL AND STR 9(AFT), LH/RH.531161-01-2 N/A TASK DELETED531162-01-3 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS BEAM T: 20000 FCGROUP 33ACOCKPIT FLOOR PANELS 212 ATTACHMENT AREA. I: 7800 FCORGROUP 33B531162-01-4 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS BEAM T: 20000 FCGROUP 32ACOCKPIT FLOOR PANELS 212 ATTACHMENT AREA. I: 7500 FCORGROUP 33CORGROUP 33D531162-01-5 831 841 211 SPECIAL DETAILED INSPECTION OF FRAME 7 AND CROSS T: 17000 FCGROUP 32ECOCKPIT FLOOR PANELS 212 BEAM ATTACHMENT AREA I: 17000 FCORGROUP 33E531166-01-1 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33A122 STRUCTURE, UPPER CORNERS OF PORTAL FRAME, FROM FRAMES I: 6400 FCOR11A TO 16A, LH/RH.GROUP 33B531166-01-2 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32A122 STRUCTURE, UPPER CORNERS OF PORTAL FRAME, FROM FRAMES I: 6200 FCOR11A TO 16A, LH/RH.GROUP 33CORGROUP 33D531166-01-3 811 821 121 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32E122 UPPER CORNERS OF PORTAL FRAME, FROM FRAMES 11A I: 9300 FCORTO 16A, LH/RH.GROUP 33EISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 11APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 531167-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND T: 6 YEZL-100-01-2 A330-200FJOINT SURFACE BETWEEN FR.0 AND FR.18/19 BELOW I: 6 YECABIN FLOOR LEVEL, EXTERNAL SURFACE, EXCLUDINGAREA COVERED BY NOSE FAIRING.N 531168-01-1 125CL 125DL 125EL 125 GENERAL VISUAL INSPECTION OF NOSE FORWARD T: 6 YE 1A330-200F125FL 125GL 125HL 126 FUSELAGE LOWER SKIN AND FAIRING SUBSTRUCTURE, I: 6 YE126CR 126FR AREA COVERED BY NOSE FAIRING BETWEEN FR.17 ANDFR.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 1A330-200F126BR 126CR 713 126 FUSELAGE LOWER SKIN AND FAIRING SUBSTRUCTURE, I: 6 YE714 AREA COVERED BY NOSE FAIRING BETWEEN FR.10 ANDFR.17, INCLUDING NLG BAY LATERAL PANEL EXTERNALSURFACE, FLAT PANEL, FR.16A AND FORWARD FACE OFLOWER FR.17 FITTING, LH/RH.531170-01-1 COCKPIT FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF COCKPIT FLOOR STRUCTURE T: 12 YE CPCP ZL-211-02-1 ALL212 BETWEEN FR 1 AND FR 10 I: 12 YE531171-01-1 CABIN FLOOR PANELS 211 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2 CPCP ALL212 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YE221 TOILETS AND DOORS ENTRANCE AREA, FROM FR 10 TO FR 17222531172-01-1 CABIN FLOOR PANELS 211 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2 CPCP NOTEFCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 5 YEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA FROM FR 10 TO FR 17222NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDIN 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 CPCP NOTEFCRC (IF INSTALLED) 212 AND 0.75 M AROUND GALLEYS AND TOILETS, INCLUDING I: 6 YEGALLEYS AND TOILETS 221 DOORS ENTRANCE AREA FROM FR 10 TO FR 17222 NOTE: TASK APPLICABLE IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 12APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531173-01-1 NOTE 1 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP ALL122 BELOW DOOR 1 (FORWARD PASSENGER/CREW DOOR) FROM CABIN I: 6 YEFLOOR LEVEL TO AVIONICS COMPARTMENT FLOOR LEVEL,BETWEEN FR 13A AND FR 17, LH/RH531175-01-3 N/A TASK DELETED531175-01-4 LINING 231 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT T: 17000 FCGROUP 32ENOTE 1 232 JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERS AT I: 8000 FCORSTGR.14/18/22/24, LH/RH.GROUP 33E531176-01-1 FWD AVIONICS BAY 121 GENERAL VISUAL INSPECTION OF FUSELAGE STRUCTURE BELOW T: 6 YE 1+2 CPCP ALLDOOR OPENED BATTERIES BETWEEN FR 10A AND 11A AND BETWEEN STR 41 I: 6 YENOTE 1 AND STR 43, LH531180-01-1 N/A TASK DELETED531183-01-1 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCPRE 40347LININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 10400 FCANDNOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.PRE 55534TOILETS531183-01-3 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32ALININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 9600 FCPRE 55534NOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.ORTOILETSGROUP 33APOST 40347ANDPRE 55534ORGROUP 33BPRE 55534ORGROUP 33CPRE 55534ORGROUP 33DPRE 55534ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 13APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531183-01-4 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FCGROUP 32ELININGS 224 CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD I: 9600 FCPRE 53102NOTE 1 OF FR 13 BELOW STR 9 FWD, LH/RH.ANDTOILETSPRE 55534ORGROUP 33EPRE 53102ANDPRE 55534531184-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 20000 FCGROUP 32ASTRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP I: 11100 FCORJOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A ANDGROUP 33AFROM FR.14 TO FR.16A, LH/RH.ORGROUP 33BORGROUP 33CORGROUP 33D531184-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL T: 17000 FCGROUP 32ESTRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP I: 11100 FCORJOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13AGROUP 33EAND FROM FR.14 TO FR.16A, LH/RH531185-01-2 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 222 FORWARD PASSENGER / CREW DOOR CUTOUT AFT UPPER I: 8850 FCPRE 49194CORNER, JUNCTION OF INTERNAL PLATE ON FR. 17, BETWEENORSTR.12 AND 13, LH/RH.GROUP 33AORGROUP 33BORGROUP 33CPRE 49194ORGROUP 33DPRE 49194ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 14APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531186-01-2 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCPRE 40347LININGS 224 CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF I: 10400 FCANDNOTE 1 FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.PRE 49411TOILETS531186-01-3 FASTENERS 223 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCPOST 40347LININGS 224 CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF I: 9600 FCANDNOTE 1 FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.PRE 49411TOILETS531187-01-2 N/A TASK DELETED531187-01-3 N/A TASK DELETED531187-01-4 N/A TASK DELETED531188-01-2 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCPRE 40347200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7600 FCFROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9FWD LEVEL, LH/RH.531188-01-3 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32A200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7000 FCORFROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9GROUP 33AFWD LEVEL, LH/RH.POST 40347ORGROUP 33BORGROUP 33CORGROUP 33D531188-01-4 N/A 100 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FCGROUP 32E200 CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FR.13 I: 7000 FCPRE 53102FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STR.9ORFWD LEVEL, LH/RH.GROUP 33EPRE 53102ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 15APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS531189-01-2 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERON I: 8850 FCORAT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B,GROUP 33ALH/RHORGROUP 33BORGROUP 33CORGROUP 33D531189-01-3 LINING 221 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32ENOTE 1 222 FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER I: 15200 FCORLONGERON AT STRINGER 12 LEVEL, BETWEEN FR. 13AGROUP 33EAND FR.13B, LH/RH531192-01-3 N/A TASK DELETED531192-01-4 N/A TASK DELETED531194-01-3 N/A TASK DELETED531194-01-4 N/A TASK DELETED531198-01-2 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 20000 FCGROUP 32ANOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 8850 FCORBETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531198-01-3 LINING 121 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 17000 FCGROUP 32ENOTE 1 122 BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL I: 15200 FCORBETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RHGROUP 33EISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 16APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-100-01-2 ALLSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM I: 6 YECENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS,EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH532101-01-2 N/A TASK DELETED532102-01-1 821 133 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP ALLCARGO COMPARTMENT 134 STRUCTURE BETWEEN FR 20 AND FR 39.1 BELOW CARGO I: 6 YEFLOOR PANELS COMPARTMENT FLOOR PANELSR 532103-01-1 821 131 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-131-03-1 ALLCARGO COMPARTMENT 132 STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND CARGO I: 12 YECEILINGS PANELS COMPARTMENT FLOOR FROM FR 20 TO FR 39.1LININGNOTE 1R 532104-01-1 821 131 DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE T: 6 YE 1+2 CPCP A330-200CARGO COMPARTMENT 132 FROM MAIN DECK FLOOR TO CARGO COMPARTMENT FLOOR, I: 6 YENOTELINING BELOW AND 0,75 M FWD AND AFT OF GALLEYS AND TOILETS,ORNOTE 1 FROM FR 20 TO FR 39.1, LH/RHA330-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED ABOVE THIS AREA.532105-01-1 821 134 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP ALLBALLMATS BELOW FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 6 YEFR 19 AND FR 26 FROM CARGO COMPARTMENT FLOOR TO STR46 RH532107-01-1 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1+2 CPCP ALLCOMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR I: 6 YE25 (10 PLACES)R 532107-01-2 821 134 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 7500 FCZL-821-01-1 A330-200COMPARTMENT DOOR LOCK FITTINGS BETWEEN FR 20B AND FR I: 7500 FCOR25 (10 PLACES)A330-300ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 17APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532107-02-1 821 134 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR FWD CARGO T: 6 YE T: 20 YE CPCP ALLECCENTRIC BOLTS COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 20B AND I: 6 YE I: 6 YEFR 25532108-01-1 821 122 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP ALLINSULATION 132 AROUND FORWARD CARGO COMPARTMENT DOOR CUT-OUT BETWEEN I: 12 YELINING FR 19 AND FR 26 FROM STR 26 RH TO CARGO COMPARTMENTFLOOR LEVEL532109-01-1 N/A TASK DELETED532110-01-1 N/A TASK DELETED532111-01-1 N/A TASK DELETED532114-01-2 N/A TASK DELETED532115-01-1 821 132 GENERAL VISUAL INSPECTION OF FORWARD CARGO T: 6 YE 1 CPCP ALLCOMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL I: 6 YEFRAMES (FR 20A AND FR 25A)532115-01-2 N/A TASK DELETED532116-01-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN INTERNAL T: 12 YE CPCP A330-300234 SURFACE UNDERNEATH ACOUSTIC INSULATION PANELS FROM I: 12 YEPRE 42069FR 18 TO FR 26.4 BETWEEN STR 6 AND CROWN CENTERLINE,PRE 44826LH/RH.532116-01-2 N/A TASK DELETED532116-01-3 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 18APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532116-02-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN T: 12 YE CPCP A330-300234 INTERNAL SURFACE UNDERNEATH ACOUSTIC INSULATION I: 12 YEPOST 42069PANELS FROM FR 18 TO FR 26.4 BETWEEN STR 13 ANDPRE 44826CROWN CENTER LINE, LH/RH.532116-03-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN INTERNAL T: 12 YE CPCP A330-300234 SURFACE UNDERNEATH ACOUSTIC INSULATION PANELS FROM FR I: 12 YEPOST 4482618 TO FR 26.4 BETWEEN STR 3 AND CROWN CENTERLINE ANDBETWEEN STR 7 TO STR 17, LH/RH.R 532117-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-1 A330-200SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO STR 26, I: 12 YEORLH/RHA330-300532117-01-3 N/A TASK DELETED532118-01-1 N/A TASK DELETEDR 532119-01-1 832 842 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-231-02-1 A330-200NOTE 1 232 STRUCTURE BETWEEN FR 17 AND FR 36, FROM STR 15 I: 12 YEZL-241-02-1 ORSIDEWALL LINING 241 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO MAIN DECKA330-300242 FLOOR, LH/RHR 532120-01-1 832 842 233 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-233-01-1 A330-200CEILING PANELS 234 STRUCTURE BETWEEN FR 17 AND FR 36, FROM STR 15 TO I: 12 YEZL-243-01-1 ORNOTE 1 243 CROWN CENTER LINE, LH/RHA330-300OVERHEAD STOWAGE 244BINSR 532121-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-200-01-1 A330-200SURFACE AROUND DOOR 2 (MID PASSENGER/CREW DOOR) I: 6 YEORCUT-OUTS BETWEEN FR 32 AND FR 36, FROM STR 9 TO STRA330-30026 LH/RHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 19APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 532122-01-1 821 131 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 6 YE 1+2 CPCP A330-200AIR CONDITION DUCTS 132 BELOW DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YEORNOTE 1 BETWEEN FR 32 AND FR 36, FROM MAIN DECK FLOOR DOWNA330-300SIDEWALL LINING TO STR 30, LH/RHR 532123-01-1 832 842 241 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE T: 12 YE 1 CPCP A330-200NOTE 1 242 AROUND DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT I: 6 YEORSIDEWALL/DOOR FRAME 243 BETWEEN FR 32 AND FR 36 ABOVE MAIN DECK FLOOR UPTOA330-300LINING 244 STR 9, LH/RHR 532124-01-1 832 842 100 DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW T: 12 YE CPCP A330-200SCUFF PLATE 200 DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, I: 6 YEORLH/RHA330-300532124-02-4 N/A TASK DELETED532124-02-5 N/A TASK DELETED532124-02-6 N/A TASK DELETED532124-02-7 N/A TASK DELETED532124-02-8 N/A TASK DELETED532124-02-9 N/A TASK DELETED532125-01-4 N/A TASK DELETED532125-01-5 N/A TASK DELETED532125-01-6 N/A TASK DELETED532125-01-7 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 20APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532125-01-8 N/A TASK DELETED532125-01-9 N/A TASK DELETED532126-01-1 N/A TASK DELETED532127-01-1 N/A TASK DELETED532128-01-1 N/A TASK DELETED532129-01-2 N/A TASK DELETED532129-01-3 N/A TASK DELETED532130-01-2 N/A TASK DELETED532130-01-3 N/A TASK DELETEDR 532134-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2 CPCP A330-200FLOOR PANELS 232 BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, I: 5 YENOTEGALLEYS AND 241 INCLUDING DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.ORTOILETS 242 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA330-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN NOTE 7 IN MRBR SECTION D ARE NOT INCORPORATED.R 532134-01-2 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 1+2 CPCP A330-200FLOOR PANELS 232 BELOW AND 0.75 M AROUND GALLEYS AND TOILETS, I: 6 YENOTEGALLEYS AND 241 INCLUDING DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.ORTOILETS 242A330-300NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEFITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 21APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 532135-01-1 831 841 231 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE CPCP ZL-231-02-1 A330-200FLOOR PANELS 232 STRUCTURE, EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YEZL-241-02-1 OR241 AND DOOR ENTRANCE AREAS, FROM FR 17 TO FR 36.A330-300242532136-01-1 N/A 233 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL SKIN T: 12 YE CPCP A330-200234 UNDERNEATH ACOUSTIC INSULATION PANELS FROM FR 18 TO I: 12 YEFR 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 FCA330-200JOINTS IN THE FOLLOWING CRACK STOPPER AREAS : I: 6500 FCORAT STR 5 LH/RH, FROM 18 TO FR 38, AT STR 13 AND STRA330-30022 LH/RH, FROM FR 18 TO FR 31 AND FROM FR 37.1 TO FR38, EXTERNAL SURFACENOTE: THIS TASK IS AN ALTERNATIVE TO TASK532137-02-1R 532137-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200LONGITUDINAL LAP JOINTS IN THE FOLLOWING CRACK I: 20000 FCORSTOPPER AREAS :A330-300AT STR 5 LH/RH, FROM 18 TO FR 38, AT STR 13 AND STR22 LH/RH, FROM FR 18 TO FR 31 AND FROM FR 37.1 TO FR38, EXTERNAL SURFACENOTE :- INSPECTION REQUIRES INSPECTION OF LAP JOINT LOWERRIVET ROW.- THIS TASK IS AN ALTERNATIVE TO TASK 532137-01-1532138-01-1 N/A TASK DELETED532139-01-1 N/A TASK DELETEDR 532142-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNA T: 24000 FCA330-200CUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTER I: 16000 FCORLINE, EXTERNAL SURFACEA330-300532143-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 22APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532144-01-2 N/A TASK DELETEDR 532145-02-1 N/A 200 GENERAL VISUAL INSPECTION OF SKIN AT SHEAR TIE T: 22800 FCZL-200-01-1 A330-200ATTACHMENTS BETWEEN FR 19 AND FR 25, FR 26.1 AND FR I: 12000 FCOR37, FR 37.2 AND FR 37.4, FROM STR 13 LH/RH TO CROWNA330-300CENTER LINE, EXTERNAL SURFACE532146-01-2 N/A TASK DELETED532147-01-2 N/A TASK DELETED532148-01-2 N/A TASK DELETED532149-01-2 N/A TASK DELETED532150-01-2 N/A TASK DELETED532150-01-3 N/A TASK DELETED532150-01-4 N/A TASK DELETED532151-01-1 N/A TASK DELETEDR 532152-01-1 N/A 100 DETAILED INSPECTION OF FUSELAGE SKIN AT SHEAR TIE T: 20000 FCA330-200200 ATTACHMENT BETWEEN FR 26 AND FR 37.1 FROM STR 13 TO ORORSTR 31 LH/RH, EXTERNAL SURFACE 75000 FHA330-300I: 8500 FCOR31900 FH532153-01-2 N/A TASK DELETED532153-01-3 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 23APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532154-01-2 N/A TASK DELETED532155-01-2 N/A TASK DELETED532156-01-2 N/A TASK DELETED532156-01-3 N/A TASK DELETED532156-01-4 N/A TASK DELETED532157-01-2 N/A TASK DELETED532158-01-2 N/A TASK DELETED532158-01-3 N/A TASK DELETEDR 532159-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND VHF 1 ANTENNA T: 24000 FCA330-200CUT-OUT BETWEEN FR 22 AND FR 23, ON CROWN CENTER I: 12000 FCORLINE, EXTERNAL SURFACEA330-300R 532160-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND ATC 1 + 2 ANTENNA T: 24000 FCA330-200CUT-OUT BETWEEN FR 24 AND FR 25, AND BETWEEN STR 2 I: 12000 FCPOST 40255AND STR 3, LH/RH, EXTERNAL SURFACEORA330-300POST 40255ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 24APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 532161-01-2 ANTENNA 200 DETAILED INSPECTION OF SKIN AROUND SATCOM (LG) T: 24000 FCA330-200ANTENNA CUT-OUT BETWEEN FR 26 AND FR 26.1 ON CROWN I: 12000 FCPOST 43560CENTER LINE, EXTERNAL SURFACEORA330-200POST 43956ORA330-300POST 43560ORA330-300POST 43956R 532162-01-2 831 841 233 DETAILED INSPECTION OF SKIN AROUND SATCOM (45 DEG) T: 24000 FCA330-200ANTENNA 234 ANTENNA CUT-OUT BETWEEN FR 26.1 AND FR 26.3 AND I: 12000 FCPOST 44620MAINTENANCE DOOR BETWEEN STR 12 AND STR 13, LH/RH, EXTERNAL SURFACEOROVERHEADA330-200STOWAGE-COMPARTMENTPOST 41833DOORORA330-200POST 45503ORA330-300POST 44620ORA330-300POST 41833ORA330-300POST 45503R 532163-01-1 ANTENNA REAR FAIRING 200 DETAILED INSPECTION OF SKIN AROUND SATCOM (HG) T: 24000 FCA330-200COVER AND BRACKET ANTENNA CUT-OUT BETWEEN FR 26.2 AND FR 27, ON CROWN I: 12000 FCPOST 43652CENTER LINE, EXTERNAL SURFACEORA330-300POST 43652532164-01-1 N/A TASK DELETED532165-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 25APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS532165-01-3 N/A TASK DELETED532165-02-1 N/A TASK DELETEDN 532166-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 3 YE CPCP ZL-200-01-1 ALLSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 LH/RH TO I: 3 YETO CROWN CENTER LINE.N 532167-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-1 A330-200FSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO STR 6, I: 12 YELH/RH.N 532168-01-1 831 841 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3 CPCP A330-200FBARRIER WALL DOORS 232 STRUCTURE FROM BARRIER WALL (BETWEEN FR 19 AND FR 20) I: 12 YELINING 233 TO FR 36, FROM CROWN CENTER LINE TO MAIN DECK FLOOR,NOTE 1 234 LH/RH.241242243244N 532169-01-1 831 841 231 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3 CPCP A330-200FBARRIER WALL DOORS 232 FROM BARRIER WALL (BETWEEN FR 19 AND FR 20)TO FR 36. I: 6 YEFLOOR PANELS 241242N 532170-02-1 BARRIER WALL LINING 230 DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO T: 12 YE 3 CPCP A330-200FSMOKE CURTAIN FUSELAGE, FITTING ASSEMBLIES. I: 12 YESTOWAGE BINS (IFFITTED)N 532171-02-1 BARRIER WALL LINING 230 DETAILED INSPECTION OF BARRIER WALL ATTACHMENTS TO T: 6 YE 3 CPCP A330-200FPROTECTION ANGLES CARGO FLOOR, FITTING ASSEMBLIES. I: 6 YEAND DOOR STEPSISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 26APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 532172-01-1 BARRIER WALL LINING 230 GENERAL VISUAL INSPECTION OF BARRIER WALL FRAMES AND T: 6 YE 3 CPCP A330-200FSTOWAGE BINS (IF BOX STRUCTURE. I: 6 YEFITTED)N 532175-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL T: 12 YE CPCP ZL-200-01-1 A330-200F200 STRUCTURE AROUND MAIN DECK CARGO DOOR CUT-OUT FROM I: 12 YEFRAME 18 TO FRAME 31 AND FROM CROWN CENTERLINE TOSTRINGER 35.N 532177-01-1 MDC DOOR 231 GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL T: 6 YE 3 CPCP A330-200FSTRUCTURE OF MAIN DECK CARGO DOOR LOCK FITTING I: 6 YEATTACHMENTS, SURROUNDING STRUCTURE AND LOWER LONGERONFROM FRAME 20 TO FRAME 29 AND FROM STRINGER 26 TOSTRINGER 30.N 532178-02-1 MDC DOOR 231 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE OF T: 6 YE 1 CPCP A330-200FMAIN DECK CARGO DOOR LOCK FITTINGS FROM FRAME 20 TO I: 6 YEFRAME 29 AND FROM STRINGER 26 TO STRINGER 30 AT 8PLACES.N 532179-01-1 MDC DOOR 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 3 CPCP A330-200F233 STRUCTURE OF MAIN DECK CARGO DOOR CUT-OUT FRAMES 20 I: 6 YEAND 29 FROM STRINGER 5 TO STRINGER 28.N 532180-01-1 MDC COMPARTMENT 231 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3 CPCP A330-200FLINING 233 STRUCTURE AROUND MAIN DECK CARGO DOOR CUT-OUT FROM I: 12 YEFRAME 18 TO FRAME 31 AND FROM CROWN CENTERLINE TOSTRINGER 26.N 532181-01-1 CC LINING 131 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 3 CPCP A330-200FSTRUCTURE BELOW MAIN DECK CARGO DOOR CUT-OUT FROM I: 6 YEFRAME 18 TO FRAME 31 AND FROM STRINGER 26 TO STRINGER35.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 27APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533001-01-2 196AB 196BB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FCGROUP 33ASTRUCTURE AT FRAME 46, HAT-SECTION PROFILE JUNCTION I: 5500 FCPRE 41410ON ARCH MEMBER AT Y = 1445ANDPRE 43451ORGROUP 33BPRE 41410ANDPRE 43451533001-01-4 196EB 196 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FCGROUP 33ASTRUCTURE AT FRAME 46, HAT-SECTION PROFILE I: 5500 FCPOST 41410JUNCTION ON ARCH MEMBER AT Y = 1445ANDPRE 43451ORGROUP 33BPOST 41410ANDPRE 43451533002-01-2 196AB 196BB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 20000 FCGROUP 33AFRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 13700 FCPRE 41410LONGITUDINAL WEB AT Y = 493ANDPRE 43727ORGROUP 33BPRE 41410ANDPRE 43727533002-01-4 196GB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT T: 20000 FCGROUP 33AFRAME 47, T-SECTION FLANGE BELOW ATTACHMENT OF I: 13700 FCPOST 41410LONGITUDINAL WEB AT Y = 493ANDPRE 43727ORGROUP 33BPOST 41410ANDPRE 43727ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 28APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533003-01-2 197AB 149 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE, FRAME T: 20000 FCGROUP 33A197 53.2 WEB AT Y=-1042, Y=-728.7 AND Y=728,7 BELOW I: 13700 FCPRE 43727198 LONGITUDINAL WEB ATTACHMENTORGROUP 33BPRE 43727533004-01-2 197GB 198GB 197 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 20000 FCGROUP 33A198 STRUCTURE AFT OF FRAME 53.8, T-SECTION JUNCTION ON I: 5500 FCPRE 43451LONGITUDINAL BEAM, LH/RHORGROUP 33BPRE 43451533005-01-2 N/A TASK DELETED533006-01-1 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YEPRE 50675148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 3 YE197BB 197EB 197FB 149197GB 197HB 198AT 197198BB 198EB 198GB 198198HB 734 744753 754533006-01-2 147BB 147BT 148BB 147 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YEPOST 50675148BT 197AB 197AT 148 STRUCTURE, FRAMES 53.2, 53.4, 53.6 AND 53.8 WEB. I: 6 YE197BB 197EB 197FB 149197GB 197HB 198AT 197198BB 198EB 198GB 198198HB 734 744753 754533007-01-1 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 3 YEPRE 43352191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB. I: 3 YEAND192BB 192CBPRE 50675533007-01-2 191AB 191AT 191BB 191 DETAILED INSPECTION OF BELLY FAIRING SUPPORT T: 6 YEPRE 43352191CB 191DB 192AT 192 STRUCTURE, FR 37.4 WEB. I: 6 YEAND192BB 192CBPOST 50675ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 29APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533008-01-1 N/A 190 DETAILED INSPECTION OF BELLY FAIRING PANELS AND T: 3 YEALLFASTENERS AT WING UPPER SURFACE TO FUSELAGE JUNCTION, I: 3 YEFROM WING LEADING EDGE TO TRAILING EDGE, LH/RHR 533009-01-1 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33A252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 52911FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHORNOTE 1 254 LH/RH. I: 13900 FCGROUP 33BOVERHEAD STOWAGE NOTE : ORPRE 52911BINS - ROTOTEST INSPECTION 41700 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-1R 533009-01-2 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32A252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911NOTE 1 254 LH/RH. I: 10800 FCOROVERHEAD STOWAGE NOTE : ORPOST 50755BINS - ROTOTEST INSPECTION 54200 FHPRE 56001- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-2R 533009-01-3 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33D252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911NOTE 1 254 LH/RH. I: 11400 FCOVERHEAD STOWAGE NOTE : ORBINS - ROTOTEST INSPECTION 34300 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-3N 533009-01-4 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33C252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202FASTENERS 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911NOTE 1 254 LH/RH. I: 11600 FCOVERHEAD STOWAGE NOTE : ORBINS - ROTOTEST INSPECTION 34900 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-4ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 30APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533009-02-1 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33A252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 52911NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHOROVERHEAD STOWAGE 254 LH/RH. I: 4600 FCGROUP 33BBINS NOTE : ORPRE 52911- X-RAY INSPECTION 13900 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-1R 533009-02-2 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32A252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911OVERHEAD STOWAGE 254 LH/RH. I: 3600 FCORBINS NOTE : ORPOST 50755- X-RAY INSPECTION 18100 FHPRE 56001- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-2R 533009-02-3 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33D252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911OVERHEAD STOWAGE 254 LH/RH. I: 3800 FCBINS NOTE : OR- X-RAY INSPECTION 11400 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-3N 533009-02-4 251JC 251VW 252JC 251 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33C252VW 252 CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN ORPRE 49202NOTE 1 253 STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 50000 FHPRE 52911OVERHEAD STOWAGE 254 LH/RH. I: 3800 FCBINS NOTE : OR- X-RAY INSPECTION 11600 FH- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-4ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 31APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533010-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33ACIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN ORORCENTERLINE TO STRINGER 17, LH/RH 50000 FHGROUP 33BI: 3900 FCOR11700 FHR 533010-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32ACIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN ORPRE 49202CENTERLINE TO STRINGER 17, LH/RH 50000 FHORI: 3050 FCPOST 50755OR15300 FHR 533010-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33DCIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN ORPRE 49202CENTERLINE TO STRINGER 17, LH/RH 50000 FHI: 3200 FCOR9700 FHN 533010-01-4 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33CCIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN ORPRE 49202CENTERLINE TO STRINGER 17, LH/RH 50000 FHI: 3250 FCOR9800 FH533011-01-2 N/A TASK DELETED533011-02-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 32APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533012-01-1 261CC 262CC 263 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33ANOTE 1 264 CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO ORPRE 41652OVERHEAD STOWAGE 5, LH/RH. 50000 FHPRE 52911BINS NOTE : I: 8100 FCORRIVETS - ROTOTEST INSPECTION 1MM ORGROUP 33B- THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-1 24400 FHPRE 41652PRE 52911R 533012-02-1 261CC 262CC 263 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33ANOTE 1 264 CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO ORPRE 41652OVERHEAD STOWAGE 5, LH/RH. 50000 FHPRE 52911BINS NOTE : I: 2300 FCOR- X-RAY INSPECTION 5 MM ORGROUP 33B- THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-1 6900 FHPRE 41652PRE 52911533013-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33ANOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 20000 FCORAT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH ORGROUP 33B78000 FHR 533013-01-2 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 18000 FCGROUP 32ANOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION ORAT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH 72000 FHI: 14700 FCOR73900 FHR 533013-01-3 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 19000 FCGROUP 33DNOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 15500 FCAT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH OR46500 FHN 533013-01-4 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 19000 FCGROUP 33CNOTE 1 146 STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION I: 15600 FCAT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH OR46900 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 33APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533014-01-1 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 20000 FCGROUP 33A148 LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF ORPRE 45307FRAME 47 DATUM, LH/RH 50000 FHORI: 6900 FCGROUP 33BORPRE 4530720900 FHR 533014-01-2 734 744 147 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 20000 FCGROUP 32A148 LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF ORPRE 45307FRAME 47 DATUM, LH/RH 50000 FHI: 7300 FCOR36800 FH533015-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, LOWER T: 20000 FCGROUP 32A148 FLANGE OF GANTRY Y=1959 AT FRAME 48 LEVEL, LH/RH I: 20000 FCORORGROUP 33A78000 FHPOST 42418S11929ORGROUP 33BPOST 42418S11929ORGROUP 33CORGROUP 33D533015-01-2 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 17000 FCGROUP 32E148 LOWER FLANGE OF GANTRY Y=1959 AT FRAME 48 LEVEL, LH/R OROR50000 FHGROUP 33EI: 17000 FCOR50000 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 34APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533016-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33CCIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN ORCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, 50000 FHEXTERNAL SURFACE, LH/RH I: 4400 FCOR13200 FHR 533016-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33DCIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN ORCENTERLINE TO STR 3 AND FROM STR 5 TO STR 50000 FH11, EXTERNAL SURFACE, LH/RH I: 4300 FCOR13000 FH533016-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FCGROUP 33ECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN ORCENTERLINE TO STR 3 AND FROM STR 5 50000 FHTO STR 11, EXTERNAL SURFACE, LH/RH. I: 4360 FCOR13100 FHN 533016-01-4 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FCGROUP 32ECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN ORCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, 50000 FHEXTERNAL SURFACE, LH/RH. I: 4180 FCOR20900 FH533017-01-1 N/A TASK DELETEDR 533018-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32ACIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN ORPRE 49202CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FHEXTERNAL SURFACE, LH/RH I: 4300 FCOR21800 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 35APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533018-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33DCIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN ORPRE 49202CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FHEXTERNAL SURFACE, LH/RH I: 4600 FCOR13800 FHN 533018-01-3 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 33CCIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN ORPRE 49202CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, 50000 FHEXTERNAL SURFACE, LH/RH. I: 4600 FCOR14000 FH533019-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 20000 FCGROUP 32ACIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, FROM I: 8000 FCCENTERLINE TO STRG8 (EXCLUDING AREA BETWEEN STRG3 ANDSTRG5) LH/RH533019-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE T: 17000 FCGROUP 32ECIRCUMFERENTIAL BUTT STRAP RADIUS AT FR38, ORFROM CENTERLINE TO STRG8 50000 FH(EXCLUDING AREA BETWEEN STRG3 AND STRG5) LH/RH I: 8000 FCOR40000 FHR 533035-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 2.5 YE 1+2 CPCP A330-200BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 2.5 YEPRE 50675FR.47 FROM Y=-2390 AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.A330-300PRE 50675R 533035-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A330-200BETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.37.1 I: 6 YEPOST 50675FR.47 FROM Y=-2390 AND FR.47 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.A330-200FORA330-300POST 50675ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 36APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533036-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 5 YE 1+2 CPCP A330-200BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 5 YEPRE 50675FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.A330-300PRE 50675R 533036-01-2 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 6 YE 1+2 CPCP A330-200BETWEEN FR.47 AND FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR.47 I: 6 YEPOST 50675FR.56 FROM Y=-2390 AND FR.56 FROM Y=-2390 TO Y=2390, COVERED BY BELLYORTO Y=2390 FAIRING, EXTERNAL SURFACE, LH/RH.A330-200FORA330-300POST 50675N 533037-01-1 FAIRING PANELS 190 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY T: 12 YE 1+2 CPCP ALLBETWEEN FR.37.1 AND FAIRING SUPPORT STRUCTURE UPPER PART BETWEEN FR.37.1 I: 12 YEFR.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=2390533101-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 12 YE NO CPCP ZL-100-01-2 ALL200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 12 YEZL-200-01-1CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH533101-01-5 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 20000 FCGROUP 33A200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 7860 FCORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RHGROUP 33B533101-01-6 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 20000 FCGROUP 32A200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 6340 FCORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RHGROUP 33C533101-01-7 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 20000 FCGROUP 33D200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO I: 6200 FCCROWN CENTERLINE, EXTERNAL SURFACE, LH/RHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 37APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533101-01-8 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN T: 17000 FCGROUP 33E200 FR 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO ORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 50000 FHI: 9200 FCOR27500 FH533101-01-9 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 17000 FCGROUP 32E200 38 AND FR 53.3 FROM UPPER EDGE OF BELLY FAIRING TO ORCROWN CENTERLINE, EXTERNAL SURFACE, LH/RH 50000 FHI: 8800 FCOR43900 FH533102-01-1 N/A TASK DELETED533103-02-1 N/A TASK DELETEDR 533104-01-3 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 20000 FCGROUP 33ALIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 OROROBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 50000 FHGROUP 33BINSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 5000 FCSTRINGER 1 LH AND STRINGER 1 RH OR15000 FH533104-01-4 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 20000 FCGROUP 32ALIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 FCOROBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48GROUP 33CINSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEENORSTRINGER 1 LH AND STRINGER 1 RHGROUP 33D- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 ANDFR.40.1 (IF INSTALLED)ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 38APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533104-01-5 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 FCGROUP 32ELIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43 ORPRE 54455OBTURATORS WHERE - ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 50000 FHORINSTALLED AND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN I: 17000 FCGROUP 33ESTRINGER 1 LH AND STRINGER 1 RH ORPRE 54760- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 AND 50000 FHFR.40.1533104-02-6 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 FCGROUP 32ELIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUTS BETWEEN FR.40.3 AND ORPOST 54455OBTURATORS WHERE FR.41 50000 FHINSTALLED - OBTURATOR CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 FC- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 ORAND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN 40000 FHSTRINGER 1 LH AND STRINGER 1 RH- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 ANDFR.40.1533104-02-7 ANTICOLLISION 200 DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND T: 17000 FCGROUP 33ELIGHTS, ANTENNAS AND - UPPER BEACON LIGHT CUTOUTS BETWEEN FR.40.3 AND ORPOST 54760OBTURATORS WHERE FR.41 50000 FHINSTALLED - OBTURATOR CUTOUT BETWEEN FR.42 AND FR.43 I: 8000 FC- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 ORAND FR.49 AND BETWEEN FR.52 AND FR.53, BETWEEN 24000 FHSTRINGER 1 LH AND STRINGER 1 RH- AFIS ANTENNA OR PROVISION CUTOUT BETWEEN FR.40 ANDFR.40.1533105-01-2 N/A TASK DELETEDR 533106-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 20000 FCGROUP 33AFASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE ORORSKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FHGROUP 33B53.3, LH/RH I: 6800 FCOR20600 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 39APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533106-01-3 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 20000 FCGROUP 32AFASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE ORORSKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FHGROUP 33C53.3, LH/RH I: 8000 FCORORGROUP 33D44000 FH533106-01-4 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 17000 FCGROUP 33EFASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE ORSKIN BETWEEN STRG. 18 AND STRG. 22, FROM FRAME 38 TO 50000 FH53.3, LH/RH I: 8000 FCOR24000 FH533106-01-5 N/A 200 DETAILED INSPECTION OF FUSELAGE EXTERNAL STRUCTURE, T: 17000 FCGROUP 32EFASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE ORSKIN BETWEEN STRG. 18 AND STRG. 22, 50000 FHFROM FRAME 38 TO 53.3, LH/RH I: 8000 FCOR40000 FH533107-01-3 N/A TASK DELETED533107-01-4 N/A TASK DELETED533107-01-6 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 33EDUCTS 132 STRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUST ORLINING 137 BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES 50000 FHNOTE 1 138 JUNCTION BELOW STRINGER 29 LEVEL, LH/RH I: 11000 FCOR33000 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 40APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533107-01-7 AIR CONDITIONING 131 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32EDUCTS 132 STRUCTURE FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW ORLINING 137 STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION 50000 FHNOTE 1 138 BELOW STRINGER 29 LEVEL, LH/RH. I: 9900 FCOR49800 FH533109-01-1 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FCGROUP 32ALAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT I: 10200 FCORSTRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22GROUP 33AFROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARDORAND AFT FRAME 45 LEVEL, LH/RHGROUP 33BORGROUP 33CORGROUP 33D533109-01-2 N/A 200 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 17000 FCGROUP 32ELAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT I: 10200 FCORSTRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22GROUP 33EFROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWSFORWARD AND AFT FRAME 45 LEVEL, LH/RH533113-01-4 N/A TASK DELETED533113-01-5 N/A TASK DELETED533114-01-3 N/A TASK DELETED533114-01-4 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 41APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533114-01-5 251XW 252XW 251 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32ENOTE 1 252 STRUCTURE FRAME 47 WEB AT JUNCTION WITH STABILIZERS ORORSTRINGER 20 TO 23, LH/RH 50000 FHGROUP 33EI: 17000 FCOR50000 FH533115-01-4 N/A TASK DELETED533115-01-5 N/A TASK DELETED533115-01-6 N/A TASK DELETED533117-01-1 191KB 192PB 193BB 191 DETAILED INSPECTION OF FR.40 PRESSURE BULKHEAD, AFT T: 12 YE 1 CPCP ALLRH ONLY:AIR 192 FACE BELOW CENTER WING BOX I: 12 YECONDITIONING PACK 193533117-01-2 N/A TASK DELETED533122-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CLG WELL; KEEL BEAM T: 6 YE 1 CPCP ALL148 INTERNAL STRUCTURE AND PANELS BETWEEN FR 47 AND FR I: 6 YE149 53.2NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.533123-01-1 734 744 147 DETAILED INSPECTION OF MAIN LANDING GEAR BAY, T: 6 YE 1 CPCP ALL148 PRESSURE DIAPHRAGMS AND PRESSURIZED FLOORS LOWER I: 6 YESURFACE, BETWEEN FR.47 AND FR.53.2ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 42APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533124-01-2 734 744 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT CLG T: 21300 FCGROUP 33A148 DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH I: 21300 FCPOST 42605149 NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDS11998TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INORTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALGROUP 33BCOMMONALITY WITH THE A340 IN THIS AREA.POST 42605S11998ORGROUP 32AORGROUP 33CORGROUP 33D533124-01-3 734 744 147 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT CLG T: 17000 FCGROUP 32E148 DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH I: 17000 FCOR149 NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDGROUP 33ETO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPTIN THE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA533125-01-1 734 744 147 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2 T: 6 YE 1 CPCP ALL148 PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF I: 6 YE149 THE CLG TRUNNION FITTINGSNOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.533126-01-1 N/A TASK DELETEDR 533126-01-2 734 744 147 GENERAL VISUAL INSPECTION OF SKIN PANEL, AREA AROUND T: 6 YE 1 CPCP ALL148 CLG AND MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) I: 6 YE149 EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.533126-01-5 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 43APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533127-01-1 N/A TASK DELETED533127-02-1 FAIRING PANELS 191 GENERAL VISUAL INSPECTION OF AREA AROUND T: 6 YE 1 CPCP ALLBETWEEN FR 39.1 AND 192 AIR-CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 I: 6 YEFR 47 193 CM (6.0 IN) EXTERNAL SURFACE195196533127-02-2 N/A TASK DELETED533127-03-1 N/A TASK DELETED533129-01-1 734 744 143 DETAILED INSPECTION OF KEEL BEAM INTERNAL AND T: 12 YE 1 CPCP ALLFAIRING PANELS 149 EXTERNAL STRUCTURE SKIN AND ADJACENT FUSELAGE I: 12 YEBETWEEN FR 40 AND FR 191 STRUCTURE, BETWEEN FR 40 AND FR 47 AS FAR AS VISIBLE.47 192193195196533135-01-1 734 744 147 DETAILED INSPECTION OF CLG AND MLG DOOR HINGE T: 12 YE 1 CPCP ALL148 FITTINGS NO 1 THROUGH NO 6, DOOR ACTUATOR FITTINGS I: 12 YE149 AND THEIR ATTACHMENT TO THE KEEL BEAM, LH/RHNOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.533136-01-2 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING NO 1 T: 20000 FCGROUP 32A148 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FCORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 44APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533136-01-3 734 744 147 DETAILED INSPECTION OF FLAP TRACK FITTING NO T: 17000 FCGROUP 32E148 1 ATTACHMENTS TO FUSELAGE SIDE PANELS, LH/RH I: 8200 FCORGROUP 33E533137-01-1 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND T: 20000 FCGROUP 33A252MG 146 ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 16600 FCORFUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER ATGROUP 33BY=2565, LH/RH533137-01-2 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND T: 20000 FCGROUP 32A252MG 146 ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 20000 FCORFUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER ATGROUP 33CY=2565, LH/RHORGROUP 33D533137-01-3 251FG 251MG 252FG 145 DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL T: 17000 FCGROUP 32E252MG 146 AND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM I: 17000 FCORFUSELAGE SKIN PANEL TO FIRST HORIZONTALGROUP 33ESTIFFENER AT Y=2565, LH/RH533138-01-2 N/A TASK DELETEDR 533138-01-3 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33ANOTE 1 146 STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y = 1959, ORPOST 42418AT FR 48 LEVEL, LH/RH. 50000 FHS11867I: 19800 FCORORGROUP 33B59500 FHPOST 42418S11867533140-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33A148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 7100 FCORSPLICE AT STRINGER 42, LH/RHGROUP 33B533140-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32A148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 6400 FCORSPLICE AT STRINGER 42, LH/RHGROUP 33CISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 45APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533140-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33D148 STRUCTURE, FR.53.2 BULKHEAD FORWARD FACE, ANGLE I: 5900 FCSPLICE AT STRINGER 42, LH/RH533141-01-1 822 151 DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND T: 12 YE 1 CPCP ALLCARGO FLOOR PANELS 152 PRESSURE BULKHEAD BETWEEN CABIN FLOOR STRUCTURE AND I: 12 YELD-MCR IF INSTALLED CARGO COMPARTMENT FLOOR LEVELOR POST 46678 LDLTOILETS ANDFURNISHINGSLININGNOTE 1533142-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 12 YE 1 CPCP ALLLINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 12 YENOTE 1 INTERNAL STRUCTURE BETWEEN CABIN FLOOR STRUCTURE ANDSTR 40, FROM AFT FACE OF CARGO COMPARTMENT REAR PANELTO FR 40533143-01-1 822 153 DETAILED INSPECTION OF AFT FACE OF FR 53.2 AND T: 6 YE 1+2 CPCP ALLCARGO FLOOR PANELS 154 PRESSURE BULKHEAD BELOW CARGO COMPARTMENT FLOOR LEVEL I: 6 YELD-MCR IF INSTALLEDOR POST 46678 LDLTOILETS ANDFURNISHINGS533144-01-1 AIR DUCTS 137 DETAILED INSPECTION OF FORWARD FACE OF FR 40, CENTER T: 6 YE 1+2 CPCP ALLLINING 138 WING BOX FRONT SPAR, PRESSURE BULKHEAD AND FUSELAGE I: 6 YENOTE 1 INTERNAL STRUCTURE BELOW STR 40, FROM FR 39.1 TO FR40NOTE: APPLY AFTER INSPECTION IN ADDITION TO TYPE 1TYPE 2 TEMPORARY PROTECTION SYSTEM ON FWD FACE OFFR 40 AND ON FUSELAGE STRUCTURE FROM 25 CM AFTERFR 39.2 TO FR 40R 533145-01-3 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FCGROUP 33A198HB 197 BUTT JOINT AT STRINGER 31 LEVEL FROM FRAME 53.3 TO I: 7050 FCOR198 FRAME 54, LH/RHGROUP 33BISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 46APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533145-01-4 197AT 197HB 198AT 100 SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL T: 20000 FCGROUP 32A198HB 197 BUTT JOINT AT STRINGER 31 LEVEL FROM FRAME 53.3 TO I: 6100 FCPRE 49202198 FRAME 54, LH/RHORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533146-01-1 N/A TASK DELETEDR 533147-01-2 GALLEYS 253 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-253-01-1 A330-200LINING 254 STRUCTURE BETWEEN FR 36 AND FR 53.5 FROM STR 15 TO I: 12 YEORNOTE 1 CROWN CENTER LINE, LH/RHA330-300OVERHEAD STOWAGEBINSTOILETSR 533148-01-1 GALLEYS 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-251-02-1 A330-200LINING 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM STR 15 TO I: 12 YEORNOTE 1 CABIN FLOOR LEVEL, LH/RHA330-300TOILETS533149-01-1 N/A TASK DELETEDR 533150-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 6 YE 1 CPCP A330-200GALLEYS 252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 6 YENOTETOILETS FUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2ORNOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA330-300FITTED ABOVE THIS AREA.NOTEISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 47APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533150-01-2 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF PRESSURIZED FLOORS AND T: 12 YE 1 CPCP NOTE252 PRESSURE DIAPHRAGMS, PORTAL FRAMES AND LATERAL I: 12 YEFUSELAGE STRUCTURE BETWEEN FR 47 AND FR 53.2NOTE:- IF NO GALLEYS/TOILETS ARE INSTALLED TPS APPLICATIONMAY BE LIMITED TO PRESSURIZED FLOORS AND PRESSUREDIAPHRAGM.- TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTFITTED ABOVE THIS AREA.533152-01-1 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 33A152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 7100 FCPRE 40379FAIRING LEVEL, LH/RH.ANDPRE 46202ORGROUP 33BPRE 40379ANDPRE 46202R 533152-01-2 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 33ALD-MCR IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8POST 40379FAIRING LEVEL, LH/RH. I: 7100 FCANDPRE 46202ORGROUP 33BPOST 40379ANDPRE 46202533152-01-3 151HX 152HX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 33ALDL IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 7100 FCPOST 46202FAIRING LEVEL, LH/RH.ORGROUP 33BPOST 46202ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 48APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533152-01-4 151GW 152GW 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 32A152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6200 FCPRE 40379FAIRING LEVEL, LH/RH.ANDPRE 46202ANDPRE 49202ORGROUP 33CPRE 40379ANDPRE 46202ANDPRE 49202ORGROUP 33DPRE 40379ANDPRE 46202ANDPRE 49202R 533152-01-5 151GW 152BX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 32ALD-MCR IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET NOTE 8POST 40379FAIRING LEVEL, LH/RH. I: 6200 FCANDPRE 46202ANDPRE 49202ORGROUP 33CPOST 40379ANDPRE 46202ANDPRE 49202ORGROUP 33DPOST 40379ANDPRE 46202ANDPRE 49202ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 49APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533152-01-6 151HX 152HX 151 SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL T: 20000 FCGROUP 32ALDL IF INSTALLED 152 FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET I: 6200 FCPOST 46202FAIRING LEVEL, LH/RH.ANDPRE 49202ORGROUP 33CPOST 46202ANDPRE 49202ORGROUP 33DPOST 46202ANDPRE 49202533154-01-4 N/A TASK DELETED533154-01-5 N/A TASK DELETED533154-01-6 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32EGALLEYS 146 RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS I: 17000 FCORTOILETS JUNCTION, FROM FRAME 48 TO 53.1, LH/RHGROUP 33ER 533155-01-1 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32ANOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH OR50000 FHI: 12600 FCOR63100 FHN 533155-01-2 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 33ANOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. OROR50000 FHGROUP 33BI: 9700 FCOR29100 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 50APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 533155-01-3 251FG 252FG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 33CNOTE 1 146 FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. OROR50000 FHGROUP 33DI: 13000 FCOR39100 FHR 533156-01-1 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 33ALD-MCR IF INSTALLED 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS OROROR POST 46678 LDL 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FHGROUP 33BTOILETS AND I: 6100 FCFURNISHINGS ORLINING 18300 FHNOTE 1533156-01-2 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32ALD-MCR IF INSTALLED 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS OROROR POST 46678 LDL 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FHGROUP 33CTOILETS AND I: 7300 FCORFURNISHINGS ORGROUP 33DLINING 41600 FHNOTE 1533156-01-3 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 33ELINING 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN ORNOTE 1 STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FHI: 7300 FCOR22700 FH533156-01-4 822 151 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32ELINING 152 STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN ORNOTE 1 STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. 50000 FHI: 7000 FCOR35000 FH533157-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 51APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533161-01-1 251AX 251CX 251EX 251 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRU T: 20000 FCGROUP 32A252AX 252CX 252EX 252 SPLICING AREA AT FRAMES 53 TO 53.2 BETWEEN STRINGERS I: 20000 FCORNOTE 1 24 AND 26, LH/RH ORGROUP 33A77900 FHORGROUP 33BORGROUP 33CORGROUP 33D533162-01-2 N/A TASK DELETEDR 533164-01-3 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 32A148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED ORDIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FHFROM Y=450 TO Y=1959, LH/RH I: 13700 FCOR68500 FH533164-01-4 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32E148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED ORDIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 50000 FH47 AND 48 FROM Y=450 TO Y=1959, LH/RH I: 12500 FCOR50000 FH533164-01-5 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 33E148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED ORDIAPHRAGMS ON FLOOR BEAMS BETWEEN 50000 FHFRAMES 47 AND 48 FROM Y=450 TO Y=1959, LH/RH I: 14900 FCOR44600 FHISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 52APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 533164-01-6 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 33A148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED ORORDIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FHGROUP 33BFROM Y=450 TO Y=1959, LH/RH. I: 12200 FCOR36800 FHN 533164-01-7 734 744 147 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 20000 FCGROUP 33C148 CANTED DIAPHRAGMS AND JUNCTION AREA OF CANTED ORORDIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES 47 AND 48 50000 FHGROUP 33DFROM Y=450 TO Y=1959, LH/RH. I: 14800 FCOR44400 FH533165-01-2 N/A TASK DELETED533166-01-1 N/A TASK DELETED533167-01-1 N/A TASK DELETED533168-01-1 N/A TASK DELETED533169-01-1 N/A TASK DELETEDR 533170-01-1 FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BELOW T: 5 YE 1+2 CPCP A330-200GALLEYS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 5 YENOTETOILETS AND FR 53.5ORNOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREA330-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN 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 CPCP A330-200GALLEYS 252 AND 0.75 M AROUND GALLEYS AND TOILETS, BETWEEN FR 36 I: 6 YENOTETOILETS AND FR 53.5ORNOTE: TASK APPLICABLE IF TOILETS OR GALLEYS AREA330-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 53APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533171-01-1 CABIN FLOOR PANELS 251 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE T: 12 YE 1+2 CPCP A330-200252 EXCLUDING AREAS BELOW AND 0.75 M AROUND GALLEYS AND I: 12 YEORTOILETS, BETWEEN FR 36 AND FR 53.5A330-300533178-01-1 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32AGALLEYS AND TOILETS 146 STRUCTURE FLOOR BEAM INBOARD FLANGE RADIUS AT Y=1959, I: 20000 FCORIF INSTALLED FROM FRAME 47 TO FRAME 48, LH/RH ORGROUP 33ANOTE 1 78000 FHPOST 42418ORGROUP 33BPOST 42418ORGROUP 33CORGROUP 33D533178-01-2 FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32EGALLEYS AND TOILETS 146 STRUCTURE FLOOR BEAM INBOARD FLANGE RADIUS AT ORORIF INSTALLED Y=1959, FROM FRAME 47 TO FRAME 48, LH/RH 50000 FHGROUP 33ENOTE 1 I: 17000 FCOR50000 FHR 533179-01-2 251MG 251SG 252MG 145 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 19000 FCGROUP 33A252SG 146 FRAMES 48 TO 53.1 VERTICAL LEG AT STRINGER PASSAGE, I: 11800 FCPOST 43904NOTE 1 LH/RH OROR35400 FHGROUP 33BPOST 43904533180-01-3 N/A TASK DELETED533180-01-4 N/A TASK DELETED533180-01-5 N/A TASK DELETED533181-01-3 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 54APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS533181-01-4 N/A TASK DELETED533181-01-5 N/A TASK DELETED533181-01-6 N/A TASK DELETEDR 533182-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FCA330-200JOINT IN CRACK STOPPER AREA AT STRINGER 5 LH/RH, I: 6500 FCORBETWEEN FR 53.3 AND 54, EXTERNAL SURFACEA330-300NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533182-02-1R 533182-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200LONGITUDINAL LAP JOINT IN CRACK STOPPER AREA AT I: 20000 FCORSTRINGER 5 LH/RH, BETWEEN FR 53.3 AND 54, EXTERNALA330-300SURFACENOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533182-01-1R 533184-01-2 N/A 200 DETAILED INSPECTION OF SKIN AT SHEAR TIE ATTACHMENTS T: 22800 FCA330-200BETWEEN FR 53.4 AND FR 53.9 FROM STRINGER 13 LH/RH TO ORORCROWN CENTER LINE, EXTERNAL SURFACE 90000 FHA330-300I: 12000 FCOR47300 FHN 533185-01-1 LINING 251 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YEZL-251-05-1 A330-200FNOTE 1 252 STRUCTURE BETWEEN FR 36 AND FR 53.5, FROM CROWN I: 12 YEZL-253-02-1253 CENTER LINE TO MAIN DECK FLOOR LEVEL, LH/RH.254533186-01-1 N/A TASK DELETEDN 533188-01-1 MAIN DECK FLOOR 251 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3A330-200FPANELS 252 BETWEEN FR.36 AND FR.53. I: 6 YEISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 55APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533190-01-1 834 844 261 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR T: 12 YE 1 CPCP A330-200INSULATION 262 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR I: 6 YEORLINING 53.4 AND 53.8 FROM MAIN DECK FLOOR LEVEL TO STR 9,A330-300LH/RH.R 533191-01-1 151EW 151GW 152EW 151 DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW DOOR3 T: 6 YE 1 CPCP A330-200152GW 822 152 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR I: 6 YEORFLOOR PANELS 53.4 AND 53.8 FROM MAIN DECK FLOOR DOWN TO CARGOA330-300INSULATION FLOOR LEVEL, LH/RHLDL TOILETS ANDFURNISHING-IFINSTALLEDLD-MCR-IF INSTALLED533192-01-1 N/A TASK DELETED533193-01-1 N/A TASK DELETEDR 533193-01-2 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN (INCLUDING T: 6 YE CPCP ZL-100-01-2 A330-200200 DOOR 3 CUT-OUT) BETWEEN FR 53.3 AND FR 54 FROM UPPER I: 6 YEZL-200-01-1 OREDGE OF BELLY FAIRING TO CROWN CENTER LINE LH/RH,A330-300EXTERNAL SURFACE533194-01-1 N/A TASK DELETED533194-01-5 N/A TASK DELETED533194-01-6 N/A TASK DELETED533194-01-7 N/A TASK DELETED533194-01-8 N/A TASK DELETED533194-01-9 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 56APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 533195-01-1 834 844 100 DETAILED INSPECTION OF DOOR 3 T: 12 YE CPCP A330-200SCUFF PLATE (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE I: 6 YEORUNDERNEATH SCUFF PLATE, LH/RH.A330-300533195-02-1 N/A TASK DELETED533195-02-5 N/A TASK DELETED533195-02-6 N/A TASK DELETED533195-02-7 N/A TASK DELETED533195-02-8 N/A TASK DELETED533195-02-9 N/A TASK DELETED534102-01-3 N/A TASK DELETED534102-01-4 N/A TASK DELETED534104-01-4 N/A TASK DELETED534104-01-5 N/A TASK DELETED534105-01-3 N/A TASK DELETED534105-01-4 N/A TASK DELETED534105-01-5 N/A TASK DELETED534107-01-2 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 57APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534107-01-3 N/A TASK DELETEDR 534108-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN IN T: 22800 FCA330-200CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT I: 15200 FCORFR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE,A330-300EXTERNAL SURFACE.R 534110-01-2 N/A 200 DETAILED INSPECTION OF FUSELAGE SKIN IN T: 22800 FCA330-200300 CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM I: 15200 FCORSTR 6 TO STR 13 LH/RH, EXTERNAL SURFACE.A330-300R 534113-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FCA330-200JOINTS IN FOLLOWING CRACK STOPPER AREAS : I: 6500 FCOR- AT STR 13 AND STR 22 LH/RH, FROM FR 54 TO FR 72A330-300- AT STR 17 AND STR 24 LH/RH, FROM FR 76 TO FR 80,EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534113-02-1R 534113-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200LONGITUDINAL LAP JOINTS IN FOLLOWING CRACK STOPPER I: 20000 FCORAREAS :A330-300- 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 534113-01-1R 534115-01-1 N/A 200 DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP T: 32000 FCA330-200JOINTS IN FOLLOWING CRACK STOPPER AREAS : I: 6500 FCOR- AT STR 5 LH/RH, FROM FR 54 TO FR 72,A330-300- AT STR 6 LH/RH, FROM FR 72 TO FR 80,EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534115-02-1ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 58APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 534115-02-1 N/A 200 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200LONGITUDINAL LAP JOINTS IN FOLLOWING CRACK STOPPER I: 20000 FCORAREAS :A330-300- 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 534115-01-1R 534116-01-1 197GB 198GB 197 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200198 LONGITUDINAL LAP JOINT IN CRACK STOPPER AREAS AT I: 20000 FCORSTR 44 LH/RH BETWEEN FR 54 AND FR55, EXTERNALA330-300SURFACE.R 534117-01-1 N/A 100 SPECIAL DETAILED INSPECTION OF LOWER SKIN OF T: 32000 FCA330-200LONGITUDINAL LAP JOINT AT STR 54 LH, BETWEEN FR I: 16000 FCOR54 AND FR 58.A330-300534120-01-2 N/A TASK DELETED534120-01-3 N/A TASK DELETEDR 534122-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AT SHEAR T: 22800 FCZL-200-01-1 A330-200TIE ATTACHMENTS: OROR- BETWEEN FR 55 AND FR 57.4, 78000 FHA330-300- BETWEEN FR 59 AND FR 71 AND I: 12000 FC- BETWEEN FR 73 AND FR 79, ORFROM STR 13 LH/RH TO CROWN CENTER LINE, 41000 FHEXTERNAL SURFACE EXCLUDING AREA COVERED BY FIN TOFUSELAGE FAIRING.R 534124-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 12 YE CPCP ZL-200-01-1 A330-20054 AND FR 80 FROM STR 6 TO STR 26, EXCLUDING AREA I: 12 YEORUNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACEA330-300534124-01-2 N/A TASK DELETED534125-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 59APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534126-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 6 YE CPCP ZL-100-01-2 ALLSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH TO I: 6 YEBOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND LAPJOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OFSKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR 54534126-01-2 N/A TASK DELETED534127-01-1 822 153 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP ALLCARGO COMPARTMENT 154 STRUCTURE BETWEEN FR 53.2 AND 73 BELOW CARGO I: 6 YEFLOOR PANELS 163 COMPARTMENT FLOOR PANELS.INSULATION 164 NOTE : IF LDL INSTALLED, INSPECTION AREA BETWEEN FRLD-MCR-IF INSTALLED 54A AND FR 73R 534128-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 6 YE 1+2 CPCP ALLNOTE 1 172 STRUCTURE BETWEEN FR 73 AND FR 80 BELOW MAIN DECK I: 6 YEFLOOR INCLUDING MAIN DECK FLOOR STRUCTURER 534130-01-1 N/A 100 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AT DOOR T: 6 YE CPCP ZL-100-01-2 A330-200200 4 (AFT PASSENGER/ CREW DOOR) CUT-OUT BETWEEN FR 73 I: 6 YEZL-200-01-1 ORAND FR 76, FROM STR 9 TO STR 26 LH/RH, EXTERNALA330-300SURFACE534130-01-2 N/A TASK DELETED534131-01-2 N/A TASK DELETED534131-01-3 N/A TASK DELETEDR 534132-01-1 833 843 100 DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW T: 12 YE CPCP A330-200SCUFF PLATE 200 DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE LH/RH I: 6 YEORA330-300534132-02-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 60APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534132-02-2 N/A TASK DELETEDR 534133-01-1 833 843 271 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND DOOR T: 12 YE 1 CPCP A330-200DOOR FRAME LINING 272 4 (AFT PASSENGER/ CREW DOOR) BETWEEN FR 72 AND FR 77 I: 6 YEORINSULATION FROM MAIN DECK FLOOR LEVEL TO STR 9 LH/RHA330-300LININGR 534134-01-1 162ZW 823 171 DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW DOOR T: 6 YE 1 CPCP A330-200NOTE 1 172 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, BETWEEN FR 73 I: 6 YEORAND FR 76 FROM MAIN DECK FLOOR LEVEL TO STR 30 LH/RHA330-300534135-01-1 N/A TASK DELETED534136-01-2 N/A TASK DELETED534137-01-2 N/A TASK DELETEDR 534138-01-1 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT T: 12 YE 1 CPCP A330-200INSULATION 154 CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND I: 6 YEORLINING FR 66, FROM STR 26 RH TO CARGO FLOOR LEVELA330-300534139-01-3 822 152 GENERAL VISUAL INSPECTION OF AFT CARGO COMPARTMENT T: 6 YE 1 CPCP ALL154 DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A I: 6 YEAND FR 65) AS FAR AS VISIBLE.534139-01-4 N/A TASK DELETED534140-01-1 822 152 DETAILED INSPECTION OF ECCENTRIC BOLTS FOR AFT CARGO T: 6 YE T: 20 YE CPCP ALLECCENTRIC BOLTS COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR59A AND I: 6 YE I: 6 YEFR65534140-02-1 822 152 GENERAL VISUAL INSPECTION OF LOCK FITTINGS OF AFT T: 6 YE 1+2 CPCP ALLCARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 59A I: 6 YEAND FR 65ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 61APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534140-02-2 N/A TASK DELETED534141-01-1 N/A TASK DELETED534143-01-2 N/A TASK DELETED534143-01-3 N/A TASK DELETED534144-01-1 823 100 DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR T: 12 YE CPCP ALLSCUFF PLATE CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE I: 6 YE534144-01-2 N/A TASK DELETED534144-01-3 N/A TASK DELETED534145-01-1 823 162 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND BULK T: 6 YE 1 CPCP ALLFLOOR PANELS CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 66 AND 70 I: 6 YELINING FROM STR 31 TO STR 48, RHNOTE 1534146-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1+2 CPCP ALLDOOR STOP FITTINGS AT 10 POSITIONS AT FR 67 AND 69 I: 6 YE534146-01-2 N/A TASK DELETED534148-01-2 N/A TASK DELETED534148-01-3 N/A TASK DELETED534149-01-1 823 162 GENERAL VISUAL INSPECTION OF BULK CARGO COMPARTMENT T: 6 YE 1 CPCP ALLDOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 67 I: 6 YEAND FR 69) AS FAR AS VISIBLEISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 62APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534149-01-2 N/A TASK DELETED534150-01-2 N/A TASK DELETED534151-01-1 N/A TASK DELETED534152-01-1 N/A TASK DELETED534153-01-1 N/A TASK DELETED534154-01-2 N/A TASK DELETED534155-01-2 N/A TASK DELETED534156-01-1 822 152 DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW AFT T: 6 YE 1+2 CPCP ALLCARGO FLOOR PANELS 154 CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND FR I: 6 YEINSULATION 67, FROM CARGO FLOOR LEVEL TO STR 47 RHLINING534156-01-2 N/A TASK DELETEDR 534157-01-1 833 843 261 GENERAL VISUAL INSPECTION OF MAIN DECK FLOOR T: 12 YE CPCP ZL-261-02-1 A330-200FLOOR PANELS 262 STRUCTURE EXCLUDING AREAS BELOW GALLEYS AND TOILETS I: 12 YEZL-271-02-1 OR271 AND DOOR ENTRANCE AREAS, FROM FR 53,5 TO FR 80.A330-300272R 534158-01-1 822 823 151 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 1 CPCP A330-200CARGO COMPARTMENT 152 STRUCTURE BETWEEN MAIN DECK FLOOR PANELS AND CARGO I: 12 YEORCEILING PANELS 161 COMPARTMENT FLOOR FROM FR 53.2 TO FR 73, INCLUDINGA330-300LDL TOILETS AND 162 MAIN DECK FLOOR STRUCTUREFURNISHING-IF 171INSTALLED 172LD-MCR-IF INSTALLEDLININGNOTE 1ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 63APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 534159-01-1 833 843 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 5 YE 1+2 CPCP A330-200FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS, I: 5 YENOTEGALLEYS 271 INCLUDING DOOR ENTRANCE AREAS, FROM FR 53,5 TO FR 80.ORTOILETS 272 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA330-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN 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 CPCP A330-200FLOOR PANELS 262 BELOW AND 0.75 M AROUND TOILETS AND GALLEYS, I: 6 YENOTEGALLEYS 271 INCLUDING DOOR ENTRANCE AREAS, FROM FR 53,5 TO FR 80.ORTOILETS 272 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA330-300FITTED IN THIS AREA AND IF THE IMPROVEMENTS AS STATEDNOTEIN NOTE 7 IN MRBR SECTION D ARE INCORPORATED.R 534160-01-1 833 843 263 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-263-01-1 A330-200CEILING PANELS 264 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM STR 15 TO I: 12 YEZL-273-01-1 ORNOTE 1 273 CROWN CENTER LINE, LH/RHA330-300OVERHEAD STOWAGE 274BINSR 534161-01-1 833 843 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE CPCP ZL-261-02-1 A330-200NOTE 1 262 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM STR 15 I: 12 YEZL-271-02-1 ORSIDEWALL LINING 271 (OVERHEAD STOWAGE BINS LOWER SURFACE) TO MAIN DECKA330-300272 FLOOR, LH/RHR 534162-01-1 822 823 151 DETAILED INSPECTION OF FUSELAGE SIDE SHELL STRUCTURE T: 6 YE 1+2 CPCP A330-200ACT IF INSTALLED 152 FROM MAIN DECK FLOOR TO CARGO COMPARTMENT FLOOR, I: 6 YENOTECEILINGS 161 BELOW AND 0.5 M FWD AND AFT OF UPPER DECK GALLEYS ANDORLDL TOILETS AND 162 TOILETS, FROM FR 53.5 TO FR 80 LH/RHA330-300FURNISHING-IF 171 NOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARENOTEINSTALLED 172 FITTED ABOVE THIS AREALD-MCR-IF INSTALLEDLININGNOTE 1ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 64APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS534163-01-2 833 843 151 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE IN T: 6 YE 1+2 CPCP A330-200FLOOR PANELS 152 LDL AREA FROM FR 53.2 TO R 54A AND FROM STR 37 TO I: 6 YENOTEINSULATION 153 BOTTOM CENTER LINE, LH/RH, INCLUDING LDL UPPER ANDLDL CEILING 154 LOWER ATTACHMENT POINTS.LINING NOTE : TASK ONLY APPLICABLE IF LDL INSTALLED.TOILETS FURNISHING534164-01-1 N/A TASK DELETED534165-01-1 N/A TASK DELETED534166-01-2 N/A TASK DELETED534166-01-3 N/A TASK DELETEDN 534167-01-1 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL T: 12 YE CPCP ZL-200-01-1 A330-200FSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 TO STR 6, I: 12 YELH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZERFAIRINGN 534168-01-1 831 841 261 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL T: 12 YE 3 CPCP A330-200FBARRIER WALL DOORS 262 STRUCTURE BETWEEN FR 53.5 AND FR 80, FROM CROWN I: 12 YELINING 263 CENTERLINE TO MAIN DECK FLOOR, LH/RH.NOTE 1 264271272273274N 534169-01-1 831 841 261 DETAILED INSPECTION OF MAIN DECK FLOOR STRUCTURE T: 6 YE 3 CPCP A330-200FBARRIER WALL DOORS 262 FROM FR 53.5 TO FR 80. I: 6 YEFLOOR PANELS 271272ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 65APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 534177-01-2 N/A 200 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN FR T: 3 YE CPCP ZL-200-01-1 ALL54 AND FR 80 FROM STR 6 LH/RH TO CROWN CENTER LINE, I: 3 YEEXCUDING 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 CPCP A330-200INSULATION 272 FACE ABOVE MAIN DECK FLOOR LEVEL INCLUDING FR 80/82, I: 12 YE I: 12 YEPRE 48980TOILETS AND GALLEYS RIM ANGLE AND ATTACHMENT TO SKINORA330-300PRE 48980R 535102-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2 CPCP A330-200172 FACE BELOW MAIN DECK FLOOR LEVEL INCLUDING FR 80/82, I: 6 YEPRE 48980RIM ANGLE ATTACHMENT AND ATTACHMENT TO SKINORA330-300PRE 48980R 535103-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE T: 20 YE CPCP A330-200312 FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 I: 12 YE I: 12 YEPRE 48980LH/RH AND CROWN CENTER LINEORA330-300PRE 48980535103-01-2 N/A TASK DELETEDR 535104-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2 CPCP A330-200312 FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 I: 6 YEPRE 48980LH/RH AND BOTTOM CENTER LINEORA330-300PRE 48980535104-02-1 N/A TASK DELETED535105-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 66APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS535106-01-1 833 843 273 DETAILED INSPECTION OF FIN TO FUSELAGE FWD ATTACH T: 12 YE 1 CPCP ALLCEILING PANEL 274 FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE SKIN, I: 12 YENOTE 1 INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWN CENTERTOILETS AND GALLEYS LINE AND AT FR 79 AND FR 80535107-01-1 312AR 311 DETAILED INSPECTION OF FIN TO FUSELAGE MID AND AFT T: 12 YE 1 CPCP ALL312 ATTACH FITTINGS IN AREA OF ATTACHMENTS TO FUSELAGE I: 6 YESKIN, INTERNAL STRUCTURE FROM STR 6 LH/RH TO CROWNCENTER LINE AND AT FR 84, 85, 86 AND 87535108-01-1 N/A TASK DELETEDR 535109-01-1 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCA330-200HINGE ARMS 312 HINGE SUPPORT MEMBERS AND UPPER AND LOWER ATTACHMENT I: 20000 FCORLUGS OF FR 91 LH/RHA330-300535110-01-1 312AR 311 DETAILED INSPECTION OF ATTACH FITTINGS FOR HORIZONTAL T: 12 YE T: 20 YE CPCP ALL312 STABILIZER TRIM ACTUATOR BETWEEN FR 86 AND FR 87 I: 12 YE I: 12 YER 535111-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE CPCP ZL-300-01-1 A330-200CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR FROM FR 84 TO I: 6 YEPRE 44205FR 85 AND BETWEEN STR 27 RH AND STR 39 RH, EXTERNALORSURFACEA330-300PRE 44205R 535111-02-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND T: 6 YE CPCP ZL-300-01-1 A330-200CUTOUT FOR TAIL COMPARTMENT ACCESS DOOR FROM FR 84 TO I: 6 YEPOST 44205FR 85 AND BETWEEN STR 27 RH AND STR 39 RH, EXTERNALORSURFACEA330-300POST 44205535112-01-1 N/A TASK DELETED535113-01-1 N/A TASK DELETEDISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 67APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS535114-01-1 N/A 300 GENERAL VISUAL INSPECTION OF FUSELAGE SKIN FROM FR T: 12 YE CPCP ZL-300-01-1 ALL80/82 TO FR 101 FROM CROWN TO BOTTOM CENTER LINE, I: 12 YEEXTERNAL SURFACE, AS FAR AS VISIBLE, LH/RH535115-01-1 N/A TASK DELETED535116-01-1 321AL 323AL 323AR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE T: 6 YE 1 CPCP A330-300323BL 323BR 323 UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 6 YEFUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD FITTINGSR 535116-01-2 321AL 323CL 323CR 321 DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE T: 6 YE 1 CPCP A330-200323DL 323DR 325LL 323 UNDERNEATH FIN TO FUSELAGE FAIRING AND FIN TO I: 6 YEOR325LR FUSELAGE ATTACH FITTINGS INCLUDING SIDE LOAD FITTINGSA330-200F535117-01-1 312AR 313AL 311 GENERAL VISUAL INSPECTION OF REAR FUSELAGE INTERNAL T: 6 YE 1 CPCP ALL312 STRUCTURE BETWEEN FR 80/82 AND FR 95 FROM CROWN TO I: 6 YE313 BOTTOM CENTER LINE, LH/RH314 NOTE: TPS APPLICATION IS FROM FR 80/82 TO FR 91 BELOWSTRINGER 25 LH/RH, FROM FR 92 TO FR 95 BELOW STRINGER13 LH/RH, AND AREA BETWEEN FR 86 AND FR 88 BELOWSTR 15535118-01-1 312AR 313AL 311 DETAILED INSPECTION OF REAR FUSELAGE T: 12 YE T: 20 YE CPCP ALL312 INTERNAL STRUCTURE AROUND HORIZONTAL STABILIZER I: 6 YE I: 6 YECUTOUT BETWEEN FR 86 AND FR 91 FROM STR 15 TO STR 30,AND FR 91 ASSEMBLY FROM CROWN TO BOTTOM CENTER LINEINCLUDING TAIL CONE ATTACHMENT FITTINGS, LH/RHR 535121-01-1 833 843 271 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 12 YEZL-271-02-1 A330-200NOTE 1 272 FWD FACE ABOVE MAIN DECK FLOOR LEVEL I: 12 YEZL-271-05-1 POST 48980TOILETS AND GALLEYS 273ZL-273-01-1 OR274ZL-273-02-1 A330-200FORA330-300POST 48980ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 68APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 535122-01-1 162ZW 822 171 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YEZL-171-02-1 A330-200IF LDF (PARTIAL OR 172 FWD FACE BELOW MAIN DECK FLOOR LEVEL I: 6 YEZL-171-02-2 POST 48980FULL BULK)ORINSTALLED: 833 843A330-200F161AZORA330-300POST 48980R 535123-01-1 312AR 311 GENERAL VISUAL INSPECTION OF REAR PRESSURE BULKHEAD T: 6 YE CPCP ZL-311-01-1 A330-200312 AFT FACE FROM CROWN TO BOTTOM CENTERLINE I: 6 YEPOST 48980ORA330-200FORA330-300POST 48980R 535124-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 6 YE 1+2 CPCP A330-200312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 6 YEPOST 48980BOTTOM CENTERLINEORA330-200FORA330-300POST 48980R 535129-01-1 833 843 271 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 12 YE CPCP A330-200GALLEYS AND TOILETS 272 FACE ATTACHMENT TO RIM ANGLE, ABOVE MAIN DECK FLOOR I: 12 YEPOST 48980IF INSTALLED 273 LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKINORNOTE 1 274A330-200FORA330-300POST 48980R 535130-01-1 162ZW 822 171 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD FWD T: 6 YE 1+2 CPCP A330-200IF LDF (PARTIAL OR 172 FACE ATTACHMENT TO RIM ANGLE, BELOW MAIN DECK FLOOR I: 6 YEPOST 48980FULL BULK) LEVEL, INCLUDING FR 80 AND ATTACHMENT TO SKINORINSTALLED: 833 843A330-200F161AZORA330-300POST 48980ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 69APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 535131-01-1 312AR 311 DETAILED INSPECTION OF REAR PRESSURE BULKHEAD AFT T: 12 YE CPCP A330-200312 FACE ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND I: 12 YEPOST 48980CROWN CENTER LINEORA330-200FORA330-300POST 48980* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE SECTION: D-53PAGE 70APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545101-02-1 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO CPCP A330-200463 THE ENGINE FORWARD MOUNT FITTING I: 6 YEPRE 48298ORA330-300PRE 48298R 545101-02-2 ENGINE 453 DETAILED INSPECTION OF PYLON PYRAMID MATING FACE WITH T: 12 YE NO CPCP A330-200463 THE ENGINE FORWARD MOUNT FITTING I: 12 YEPWPOST 48298ORA330-200FPWORA330-300PWPOST 48298ORA330-200RRPOST 48298ORA330-200FRRORA330-300RRPOST 48298545102-04-1 N/A TASK DELETED545102-05-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO CPCP PW463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT I: 12 YERIB 8C545102-06-1 ENGINE 453 DETAILED INSPECTION OF PYLON, AFT ENGINE ATTACHMENT T: 12 YE NO CPCP RR463 BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING AT I: 12 YERIB 8DISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545103-02-1 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OF T: 20000 FCGROUP 32A463 ARMS AT ENGINE FORWARD MOUNT FITTING. OROR50000 FHGROUP 33AI: 15100 FCORORGROUP 33B50000 FHORGROUP 33CORGROUP 33D545103-02-2 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, T: 17000 FCGROUP 33E463 END OF ARMS AT ENGINE FORWARD MOUNT FITTING OR50000 FHI: 16000 FCOR48000 FH545103-02-3 ENGINE 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OF T: 17000 FCGROUP 32E463 ARMS AT ENGINE FORWARD MOUNT FITTING. OR50000 FHI: 14800 FCOR50000 FHR 545104-02-10 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 32E426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORRRBETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FHI: 11000 FCOR50000 FHR 545104-02-11 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 32E416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORPW426AR 426BR 453AZ BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FH463AZ I: 11400 FCOR50000 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 545104-02-15 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 32A426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORRRBETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHPOST 48298I: 11100 FCOR50000 FHN 545104-02-16 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 32A416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORPW426AR 426BR 453AZ BETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHPOST 48298463AZ I: 11400 FCOR50000 FHN 545104-02-17 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 33C426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORGEBETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHPOST 48298I: 14000 FCORORGROUP 33D42000 FHGEPOST 48298N 545104-02-18 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 32A426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORGEBETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHPOST 48298I: 13300 FCOR50000 FHN 545104-02-19 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 33E426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORGEBETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHI: 14000 FCOR42000 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 545104-02-20 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 32E426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORGEBETWEEN RIB 1 AND RIB 2 (2 FASTENER LOCATIONS/PYLON). 50000 FHI: 13300 FCOR50000 FH545104-02-3 N/A TASK DELETED545104-02-4 N/A TASK DELETED545104-02-5 N/A TASK DELETEDR 545104-02-6 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 33C426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN ORRRRIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FHPOST 48298I: 11600 FCORORGROUP 33D34800 FHRRPOST 48298R 545104-02-7 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 20000 FCGROUP 33C416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORPW426AR 426BR 453AZ BETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FHPOST 48298463AZ I: 11900 FCORORGROUP 33D35700 FHPWPOST 48298R 545104-02-8 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 33E426AR 453AZ 463AZ 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN ORRRRIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FHI: 11600 FCOR34800 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545104-02-9 415AL 415BL 416AR 453 SPECIAL DETAILED INSPECTION OF PYLON PYRAMID T: 17000 FCGROUP 33E416BR 425AL 425BL 463 ATTACHMENT AREAS AT AFT END OF LOWER ARMS ORPW426AR 426BR 453AZ BETWEEN RIB 1 AND RIB2.(2 FASTENER LOCATIONS/PYLON) 50000 FH463AZ I: 11900 FCOR35700 FHR 545106-01-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE T: 12 YE T: 20 YE NO CPCP A330-200426AR 463 I: 6 YE I: 6 YEGEORA330-300GEORRR545106-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, RIB 1 FORWARD FACE T: 12 YE T: 20 YE NO CPCP PW416BR 425AL 425BL 463 I: 6 YE I: 6 YE426AR 426BR545108-03-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NOGROUP 32A426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORGE50000 FHORI: 6000 FCGROUP 33AORGE21000 FHORGROUP 33BGEORGROUP 33CGEORGROUP 33DGEISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545108-03-10 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 33E416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 ORPW426AR 426BR 50000 FHI: 9300 FCOR27800 FH545108-03-11 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 33E426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORRR50000 FHI: 7200 FCOR21700 FH545108-03-12 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 32E426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORGE50000 FHI: 8600 FCOR43000 FH545108-03-13 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 32E416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 ORPW426AR 426BR 50000 FHI: 8600 FCOR43000 FH545108-03-14 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 32E426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORRR50000 FHI: 6700 FCOR33500 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 6APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545108-03-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NOGROUP 32A416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 ORPW426AR 426BR 50000 FHORI: 6000 FCGROUP 33AORPW21000 FHORGROUP 33BPWORGROUP 33CPWORGROUP 33DPW545108-03-3 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 20000 FC NOGROUP 32A426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORRR50000 FHORI: 5100 FCGROUP 33AORRR17800 FHORGROUP 33BRRORGROUP 33CRRORGROUP 33DRR545108-03-4 N/A TASK DELETED545108-03-5 N/A TASK DELETED545108-03-6 N/A TASK DELETED545108-03-7 N/A TASK DELETED545108-03-8 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 7APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545108-03-9 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 17000 FC NOGROUP 33E426AR 463 FORWARD MOUNT FITTING TO RIB 1 ORGE50000 FHI: 9300 FCOR27800 FHR 545108-04-1 415AL 416AR 425AL 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 12 YE NO CPCP A330-200426AR 463 FORWARD MOUNT FITTING TO RIB 1 I: 6 YEGEPRE 48298ORA330-300GEPRE 48298ORA330-200RRPRE 48298ORA330-300RRPRE 48298R 545108-04-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE T: 12 YE NO CPCP A330-200416BR 425AL 425BL 463 FORWARD MOUNT FITTING TO RIB 1 I: 6 YEPW426AR 426BRPRE 48298ORA330-300PWPRE 48298545108-04-3 N/A TASK DELETED545108-04-4 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 8APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545110-03-1 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 20000 FC NOGROUP 32A416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C ORPW418BR 418CR 425AL 50000 FHOR425BL 426AR 426BR I: 20000 FCGROUP 33A427AL 428AR 428BR ORPW428CR 50000 FHORGROUP 33BPWORGROUP 33CPWORGROUP 33DPW545110-03-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO CPCP PW416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C I: 12 YE418BR 418CR 425AL425BL 426AR 426BR427AL 428AR 428BR428CR545110-03-3 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 17000 FC NOGROUP 32E416BR 417AL 418AR 463 UPPER BEAM AT RIB 8C ORPW418BR 418CR 425AL 50000 FHOR425BL 426AR 426BR I: 17000 FCGROUP 33E427AL 428AR 428BR ORPW428CR 50000 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 9APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545110-04-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 20000 FC NOGROUP 32A418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D ORRR427AL 428AR 50000 FHORI: 20000 FCGROUP 33AORRR50000 FHORGROUP 33BRRORGROUP 33CRRORGROUP 33DRR545110-04-2 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO CPCP RR418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D I: 12 YE427AL 428AR545110-04-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 17000 FC NOGROUP 32E418AR 425AL 426AR 463 UPPER BEAM AT RIB 8D ORRR427AL 428AR 50000 FHORI: 17000 FCGROUP 33EORRR50000 FHR 545111-01-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT T: 12 YE NO CPCP A330-200DISASSEMBLED 423 UPPER BEAM AT RIB 9C. I: 12 YEGEENGINEORA330-300GE545111-02-1 N/A TASK DELETED545111-02-2 N/A TASK DELETED545115-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 10APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545115-02-1 AFT ATTACHMENT BEAM 453 DETAILED INSPECTION OF PYLON LOWER SPAR JUNCTION WITH T: 20000 FCGROUP 32ADISASSEMBLED 463 RIB 9C (GE), 8C (PW), 8D (RR) ORORENGINE 50000 FHGROUP 33AI: 20000 FCORORGROUP 33B50000 FHORGROUP 33CORGROUP 33D545115-02-3 AFT ATTACHMENT BEAM 453 DETAILED INSPECTION OF PYLON LOWER SPAR JUNCTION WITH T: 17000 FCGROUP 32EDISASSEMBLED 463 RIB 9C (GE), 8C (PW), 8D (RR). ORORENGINE 50000 FHGROUP 33EI: 17000 FCOR50000 FH545115-03-1 N/A TASK DELETED545115-03-2 N/A TASK DELETEDR 545118-02-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A330-200418AR 425AL 426AR 463 SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 I: 12 YE I: 12 YEGE427AL 428AR AND RIB 10)ORA330-300GEORRR545118-02-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO CPCP PW416BR 417AL 418AR 463 SURFACE, BETWEEN RIB 1 AND FIREWALL (BETWEEN RIB 9 I: 12 YE I: 12 YE425AL 425BL 426AR AND RIB 10)426BR 427AL 428ARISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 11APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545119-01-1 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO CPCP A330-200418AR 425AL 426AR 463 SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) I: 12 YE I: 12 YEGE427AL 428AR 454AL AND RIB 18AOR464ALA330-300GEORRR545119-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LOWER SPAR LOWER T: 12 YE T: 20 YE NO CPCP PW416BR 417AL 418AR 463 SURFACE, BETWEEN FIREWALL (BETWEEN RIB 9 AND RIB 10) I: 12 YE I: 12 YE425AL 425BL 426AR AND RIB 18A426BR 427AL 428AR454AL 464ALR 545121-02-1 451CL 451CR 451DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP PW451DR 452AL 452BL 463 SURFACE, BETWEEN RIB 1 AND RIB 10A EXCLUDING I: 12 YEOR452BR 452CL 452CR PRECOOLER AREA, AS FAR AS VISIBLE.RR461CL 461CR 461DL461DR 462AL 462BL462BR 462CL 462CRR 545121-02-2 451DL 451DR 451EL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A330-200451ER 452AL 452BL 463 SURFACE, BETWEEN RIB 1 AND RIB 10A EXCLUDING I: 12 YEGE452BR 452CL 452CR PRECOOLER AREA, AS FAR AS VISIBLE.OR461DL 461DR 461ELA330-300461ER 462AL 462BLGE462BR 462CL 462CRR 545122-01-1 451EL 451ER 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A330-200461EL 461ER 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YEGEAIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11772ORA330-300GEPOST 42102S11772ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 12APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545122-01-2 451CL 451CR 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A330-200461CL 461CR 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YEPWAIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11772ORA330-200FPWORA330-300PWPOST 42102S11772R 545122-01-3 452BL 462BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A330-200AIR DUCT 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YE I: 6 YERRPRE-COOLER INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11772ORA330-200FRRORA330-300RRPOST 42102S11772R 545122-01-4 451EL 451ER 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A330-200461EL 461ER 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YEGEAIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11723ANDPRE 42102S11772ORA330-300GEPOST 42102S11723ANDPRE 42102S11772ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 13APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545122-01-5 451CL 451CR 452AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A330-200461CL 461CR 462AL 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YEPWAIR DUCT INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102PRE-COOLER COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11723ANDPRE 42102S11772ORA330-300PWPOST 42102S11723ANDPRE 42102S11772R 545122-01-6 452BL 462BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE NO CPCP A330-200AIR DUCT 463 SURFACE COVERED BY AIR DUCT BETWEEN RIB 1 AND RIB 4 I: 6 YERRPRE-COOLER INCLUDING STRUCTURAL RODS AND UPPER SPAR CUTOUTPOST 42102COVERED BY THE PRE-COOLER BETWEEN RIB 4 AND RIB 8S11723ANDPRE 42102S11772ORA330-300RRPOST 42102S11723ANDPRE 42102S11772R 545124-02-1 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO CPCP A330-200454BR 454CL 454CR 463 SURFACE, BETWEEN RIB 10A AND RIB 15A I: 12 YEPRE 43271462CL 462CR 464BLOR464BR 464CL 464CRA330-300PRE 43271ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 14APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545124-02-2 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON UPPER SPAR UPPER T: 12 YE NO CPCP A330-200454BR 454CL 454NR 463 SURFACE, BETWEEN RIB 10A AND RIB 15A I: 12 YEPOST 43271462CL 462CR 464BLOR464BR 464CL 464NRA330-200FORA330-300POST 43271R 545126-02-1 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A330-200464DR 463 SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A I: 12 YE I: 12 YEPRE 43271ORA330-300PRE 43271R 545126-02-2 454KL 454KR 464KL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR UPPER T: 12 YE T: 20 YE NO CPCP A330-200464KR 463 SURFACE, BETWEEN EXTERNAL RIB 15A AND RIB 18A I: 12 YE I: 12 YEPOST 43271ORA330-200FORA330-300POST 43271R 545128-01-1 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT T: 10 YE NO CPCP A330-200464BR 463 FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 I: 10 YEPRE 42044BEARINGORA330-300PRE 42044R 545128-01-2 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR SPIGOT T: 10 YE T: 20 YE NO CPCP A330-200464BR 463 FITTING RECEPTACLE, BETWEEN RIB 12 AND RIB 13 I: 10 YE I: 10 YEPOST 42044BEARINGORA330-200FORA330-300POST 42044545129-01-1 N/A TASK DELETED545129-01-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 15APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545129-01-3 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 20000 FCGROUP 32A464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORGE50000 FHORI: 9300 FCGROUP 32AORPW32500 FHORGROUP 33AGEORGROUP 33APWORGROUP 33BGEORGROUP 33BPWORGROUP 33CGEORGROUP 33CPWORGROUP 33DGEORGROUP 33DPW545129-01-4 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 20000 FCGROUP 32A464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORRR50000 FHORI: 7400 FCGROUP 33AORRR25900 FHORGROUP 33BRRORGROUP 33CRRORGROUP 33DRRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 16APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545129-01-5 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FCGROUP 33E464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORGE50000 FHORI: 9500 FCGROUP 33EORPW28500 FH545129-01-6 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FCGROUP 33E464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORRR50000 FHI: 7600 FCOR22800 FH545129-01-7 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FCGROUP 32E464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORGE50000 FHORI: 8500 FCGROUP 32EORPW42600 FH545129-01-8 454DL 454DR 464DL 453 DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB T: 17000 FCGROUP 32E464DR 463 CUTOUT BETWEEN RIB 16 AND RIB 17 ORRR50000 FHI: 6800 FCOR34000 FHR 545135-01-1 454BL 454BR 454CL 453 GENERAL VISUAL INSPECTION OF PYLON LATERAL PANELS, T: 12 YE NO CPCP ZL-454-06-1 A330-200454CR 464BL 464BR 463 EXTERNAL SURFACE, EXCLUDING AREA COVERED BY ENGINE I: 6 YEZL-454-06-2 PRE 48298464CL 464CR COWLS.ORA330-300PRE 48298545135-01-2 N/A TASK DELETED545136-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 17APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545137-01-1 414AL 414AR 415AL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO CPCP A330-200416AR 417AL 418AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YEGE424AL 424AR 425AL CORE COWLSPRE 48298426AR 427AL 428ARORA330-300GEPRE 48298R 545137-01-2 415AL 415BL 416AR 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO CPCP A330-200416BR 417AL 418AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YEPW425AL 425BL 426AR CORE COWLSPRE 48298426BR 427AL 428ARORA330-300PWPRE 48298R 545137-01-3 415AL 416AR 417AL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 12 YE T: 20 YE NO CPCP A330-200418AR 425AL 426AR 463 EXTERNAL LOWER AREAS COVERED BY REVERSER COWLS AND I: 6 YE I: 6 YERR427AL 428AR CORE COWLSPRE 48298ORA330-300RRPRE 48298545137-01-4 N/A TASK DELETED545137-01-5 N/A TASK DELETED545137-01-6 N/A TASK DELETED545138-01-1 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 18APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545138-01-10 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS T: 17000 FCGROUP 32EOF FASTENERS SECURING SUPPORTS OF FRONT ACCESS ORRRDOORS BETWEEN RIB 10 AND RIB 11 50000 FHI: 7000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545138-02-6 35100 FH545138-01-2 N/A TASK DELETED545138-01-3 N/A TASK DELETED545138-01-4 N/A TASK DELETED545138-01-5 N/A TASK DELETEDR 545138-01-6 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS OF T: 20000 FCGROUP 32A GEFASTENERS SECURING SUPPORTS OF FRONT ACCESS DOORS ORORBETWEEN RIB 10 AND RIB 11 50000 FHGROUP 32A PWI: 12800 FCOR50000 FH545138-01-7 N/A TASK DELETED545138-01-8 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FCGROUP 32EAREAS OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS ORGEDOORS BETWEEN RIB 10 AND RIB 11 50000 FHORI: 17000 FCGROUP 32EORPW50000 FHORGROUP 33EGEORGROUP 33EPWISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 19APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545138-01-9 N/A 400 DETAILED INSPECTION OF PYLON LATERAL PANELS, AREAS OF T: 17000 FCGROUP 33EFASTENERS SECURING SUPPORTS OF FRONT ACCESS DOORS ORRRBETWEEN RIB 10 AND RIB 11 50000 FHI: 8000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545138-02-5 24100 FH545138-02-1 N/A TASK DELETED545138-02-2 N/A TASK DELETED545138-02-3 N/A TASK DELETED545138-02-5 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FCGROUP 33EAREAS OF FASTENERS SECURING SUPPORTS OF FRONT ACCESS ORRRDOORS BETWEEN RIB 10 AND RIB 11 50000 FHI: 16400 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545138-01-9 49300 FH545138-02-6 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, T: 17000 FCGROUP 32EAREAS OF FASTENERS SECURING SUPPORTS OF FRONT ORRRACCESS DOORS BETWEEN RIB 10 AND RIB 11 50000 FHI: 14300 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545138-01-10 50000 FH545139-02-1 N/A TASK DELETED545139-02-2 N/A TASK DELETED545139-02-3 N/A TASK DELETED545139-02-4 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 20APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545139-02-5 N/A TASK DELETED545139-02-6 N/A TASK DELETED545139-02-7 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 20000 FCGROUP 32AAREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS ORORDOORS BETWEEN RIB 13 AND RIB 14 50000 FHGROUP 33AI: 7450 FCORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK ORGROUP 33B545139-03-7 26100 FHORGROUP 33CORGROUP 33D545139-02-8 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33EAREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS ORDOORS BETWEEN RIB 13 AND RIB 14 50000 FHI: 10600 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545139-03-8 31900 FH545139-02-9 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREAS T: 17000 FCGROUP 32EOF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS ORBETWEEN RIB 13 AND RIB 14 50000 FHI: 9800 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545139-03-9 49300 FH545139-03-1 N/A TASK DELETED545139-03-2 N/A TASK DELETED545139-03-3 N/A TASK DELETED545139-03-4 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 21APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545139-03-5 N/A TASK DELETED545139-03-6 N/A TASK DELETED545139-03-7 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 20000 FCGROUP 32AAREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS ORORDOORS BETWEEN RIB 13 AND RIB 14 50000 FHGROUP 33AI: 20000 FCORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK ORGROUP 33B545139-02-7 50000 FHORGROUP 33CORGROUP 33D545139-03-8 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33EAREAS OF FASTENERS SECURING SUPPORTS OF REAR ACCESS ORDOORS BETWEEN RIB 13 AND RIB 14 50000 FHI: 17000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545139-02-8 50000 FH545139-03-9 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32EOF FASTENERS SECURING SUPPORTS OF REAR ACCESS DOORS ORBETWEEN RIB 13 AND RIB 14 50000 FHI: 17000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545139-02-9 50000 FH545140-01-1 N/A TASK DELETED545140-01-2 N/A TASK DELETED545140-01-3 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 22APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545140-01-4 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33EAREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OREXTERNAL SURFACE,LH/RH. 50000 FHI: 8100 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545140-02-4 24300 FH545140-01-5 N/A 400 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32EAREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OREXTERNAL SURFACE,LH/RH. 50000 FHI: 7900 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545140-02-5 39500 FH545140-02-1 N/A TASK DELETED545140-02-2 N/A TASK DELETED545140-02-3 N/A TASK DELETED545140-02-4 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33EAREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OREXTERNAL SURFACE,LH/RH 50000 FHI: 17000 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545140-01-4 50000 FH545140-02-5 N/A 400 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32EAREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, OREXTERNAL SURFACE,LH/RH 50000 FHI: 16500 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK OR545140-01-5 50000 FHR 545142-01-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 6 YE NO CPCP ALL463CR 463 EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND I: 6 YEINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 23APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545142-02-1 N/A TASK DELETED545142-02-2 N/A TASK DELETED545142-02-3 N/A TASK DELETED545142-02-4 N/A TASK DELETED545142-02-5 N/A TASK DELETED545142-02-6 N/A TASK DELETED545142-02-7 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 24APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545143-02-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF T: 20000 FCGROUP 32A463BR 463 ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 ORGEAND RIB 11 50000 FHORI: 7400 FCGROUP 32AORPW25800 FHORGROUP 33AGEORGROUP 33APWORGROUP 33BGEORGROUP 33BPWORGROUP 33CGEORGROUP 33CPWORGROUP 33DGEORGROUP 33DPW545143-02-2 N/A TASK DELETED545143-02-3 N/A TASK DELETED545143-02-4 N/A TASK DELETED545143-02-5 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 25APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545143-02-9 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF T: 17000 FCGROUP 33E463BR 463 ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 ORRRAND RIB 11 50000 FHI: 5100 FCNOTE:THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-4 OR15300 FH545143-03-1 N/A TASK DELETED545143-03-2 N/A TASK DELETED545143-03-4 453BL 453BR 463BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33E463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE ORRRBETWEEN RIB 10 AND RIB 11 50000 FHNOTE THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-9 I: 13200 FCOR39700 FH545143-03-5 453BL 453BR 463BL 453 SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32E463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE ORRRBETWEEN RIB 10 AND RIB 11 50000 FHNOTE:THIS TASK IS AN ALTERNATIVE TO TASK 545143-04-1 I: 11500 FCOR50000 FH545143-04-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32E463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE ORRRBETWEEN RIB 10 AND RIB 11 50000 FHNOTE THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-4 I: 4450 FCOR22300 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 26APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545143-04-2 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 33E463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE ORGEBETWEEN RIB 10 AND RIB 11 50000 FHORI: 12100 FCGROUP 33EORPW36300 FH545143-04-3 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, LATERAL PANELS, T: 17000 FCGROUP 32E463BR 463 EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE ORGEBETWEEN RIB 10 AND RIB 11 50000 FHORI: 10500 FCGROUP 32EORPW50000 FH545146-02-1 N/A TASK DELETED545146-02-2 N/A TASK DELETED545146-02-5 N/A TASK DELETED545146-02-6 N/A TASK DELETED545146-03-3 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 33E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORGEAIR DUCT NOTE: 50000 FHORPRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 12400 FCGROUP 33ERODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-3 ORPW37300 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 27APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545146-03-4 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 33E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORRRAIR DUCT NOTE: 50000 FHPRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 8800 FCRODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-4 OR26500 FH545146-03-5 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 32E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORGEAIR DUCT NOTE: 50000 FHORPRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 11500 FCGROUP 32ERODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-5 ORPW50000 FH545146-03-6 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 32E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORRRAIR DUCT NOTE: 50000 FHPRE-COOLER - HIGH FREQUENCY EDDY CURRENT INSPECTION I: 8200 FCRODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-6 OR41000 FH545146-04-3 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 33E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORGEAIR DUCT NOTE: 50000 FHORPRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 6750 FCGROUP 33ERODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-3 ORPW20200 FH545146-04-4 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 33E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORRRAIR DUCT NOTE: 50000 FHPRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 4450 FCRODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-4 OR13300 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 28APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545146-04-5 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 32E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORGEAIR DUCT NOTE: 50000 FHORPRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 6250 FCGROUP 32ERODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-5 ORPW31300 FH545146-04-6 452AL 453BL 453BR 453 SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR T: 17000 FCGROUP 32E462AL 463BL 463BR 463 AND LATERAL PANEL JUNCTIONS BETWEEN RIB 6 AND RIB 7 ORRRAIR DUCT NOTE: 50000 FHPRE-COOLER - INSPECTION THROUGH FLEXIBLE BOROSCOPE I: 4130 FCRODS - THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-6 OR20600 FHR 545150-02-1 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 20000 FCGROUP 33AAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORGEPRE-COOLER 50000 FHORRODS I: 9000 FCGROUP 33BORGE27100 FHORGROUP 33CGEORGROUP 33DGEORGROUP 33ARRORGROUP 33BRRORGROUP 33CRRORGROUP 33DRRISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 29APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 545150-02-10 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 20000 FCGROUP 32AAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORGEPRE-COOLER 50000 FHORRODS I: 8650 FCGROUP 32AORRR43200 FH545150-02-2 N/A TASK DELETED545150-02-6 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FCGROUP 33EAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORPWPRE-COOLER 50000 FHRODS I: 11700 FCOR35100 FH545150-02-7 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FCGROUP 32EAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORPWPRE-COOLER 50000 FHRODS I: 11400 FCOR50000 FH545150-02-8 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FCGROUP 33EAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORGEPRE-COOLER 50000 FHORRODS I: 15600 FCGROUP 33EORRR46800 FH545150-02-9 452AL 462AL 453 DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL T: 17000 FCGROUP 32EAIR DUCT 463 PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 ORGEPRE-COOLER 50000 FHORRODS I: 15200 FCGROUP 32EORRR50000 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 30APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545154-01-1 454EL 454ER 464EL 453 DETAILED INSPECTION OF PYLON, RIB 18A ASSEMBLY, AFT T: 12 YE T: 20 YE NO CPCP A330-200464ER 463 FACE I: 12 YE I: 12 YEPRE 48298ANDPRE 50003ANDPRE 54399ORA330-300PRE 48298ANDPRE 50003ANDPRE 54399R 545158-01-1 415AL 416AR 425AL 453 SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL T: 12 YE T: 20 YE NO CPCP A330-200426AR 453AZ 463AZ 463 STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD I: 6 YE I: 6 YEGEFACEORA330-300GEORRR545158-01-2 415BL 416BR 417AL 453 SPECIAL DETAILED INSPECTION OF PYLON, INTERNAL T: 12 YE T: 20 YE NO CPCP PW418AR 425BL 426BR 463 STRUCTURE BETWEEN RIB 1 AFT FACE AND RIB 3 FORWARD I: 6 YE I: 6 YE427AL 428AR 453AZ FACE463AZ545160-01-1 452AL 452BL 452BR 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE T: 20 YE NO CPCP ALL462AL 462BL 462BR 463 BETWEEN RIB 3 AFT FACE AND RIB 8 FORWARD FACE I: 6 YE I: 6 YEAIR DUCTPRE-COOLERRODS545160-01-2 N/A TASK DELETED545162-01-1 453BL 453BR 463BL 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE NO CPCP ALL463BR 463 BETWEEN RIB 8 AFT FACE AND RIB 12 FORWARD FACE I: 6 YEISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 31APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545164-01-1 453CL 453CR 463CL 453 DETAILED INSPECTION OF PYLON, INTERNAL STRUCTURE T: 12 YE T: 20 YE NO CPCP ALL463CR 463 BETWEEN RIB 12 AFT FACE AND RIB 18A FORWARD FACE I: 6 YE I: 6 YE545166-02-1 N/A TASK DELETED545166-02-10 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E464BR 463 FITTINGS AT RIB 12 ORRR50000 FHI: 3960 FCOR19800 FH545166-02-11 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 33E464BR 463 FITTINGS AT RIB 12 ORGE50000 FHORI: 7800 FCGROUP 33EORPW23300 FH545166-02-12 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E464BR 463 FITTINGS AT RIB 12 ORPW50000 FHI: 8900 FCOR44300 FHN 545166-02-13 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 32A464BR 463 FITTINGS AT RIB 12 ORGE50000 FHORI: 7050 FCGROUP 32AORPW35400 FH545166-02-2 N/A TASK DELETED545166-02-3 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 32APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545166-02-4 N/A TASK DELETEDR 545166-02-5 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 33A464BR 463 FITTINGS AT RIB 12 ORGE50000 FHORI: 8100 FCGROUP 33BORGE24300 FHORGROUP 33CGEORGROUP 33DGEORGROUP 33APWORGROUP 33BPWORGROUP 33CPWORGROUP 33DPW545166-02-6 N/A TASK DELETED545166-02-8 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 33E464BR 463 FITTINGS AT RIB 12 ORRR50000 FHI: 4440 FCOR13300 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 33APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545166-02-9 454BL 454BR 464BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E464BR 463 FITTINGS AT RIB 12 ORGE50000 FHI: 7000 FCOR34800 FH545168-02-1 N/A TASK DELETED545168-02-10 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORRR464BL 464BR 50000 FHI: 3960 FCOR19800 FH545168-02-11 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 33E454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORGE464BL 464BR 50000 FHORI: 7800 FCGROUP 33EORPW23300 FH545168-02-12 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORPW464BL 464BR 50000 FHI: 8900 FCOR44300 FHN 545168-02-13 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 32A454BR 462CL 462CR 464 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORGE464BL 464BR 50000 FHORI: 7050 FCGROUP 32AORPW35400 FH545168-02-2 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 34APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545168-02-3 N/A TASK DELETED545168-02-4 N/A TASK DELETEDR 545168-02-5 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 33A454BR 462CL 462CR 464 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORGE464BL 464BR 50000 FHORI: 8100 FCGROUP 33BORGE24300 FHORGROUP 33CGEORGROUP 33DGEORGROUP 33APWORGROUP 33BPWORGROUP 33CPWORGROUP 33DPW545168-02-6 N/A TASK DELETED545168-02-8 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 33E454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORRR464BL 464BR 50000 FHI: 4440 FCOR13300 FHISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 35APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545168-02-9 452CL 452CR 454BL 453 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E454BR 462CL 462CR 463 FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) ORGE464BL 464BR 50000 FHI: 7000 FCOR34800 FH545170-02-1 452CL 452CR 454BL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP ALL454BR 462CL 462CR 464 FITTING SLEEVES, LINKS AND BOLTS AT RIB 12 (4 PLACES I: 12 YE464BL 464BR PER PYLON)BOLTSENGINELINKSSLEEVES545174-01-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 32A454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A ORGE454ML 454MR 464DL 50000 FHOR464DR 464FL 464FR I: 11100 FCGROUP 33A464KL 464KR 464ML ORGE464MR 38800 FHORPOST 43271 (ACCESSGROUP 33BWITH SUFFIX KL, KR,GEML, MR)ORPRE 43271 (ACCESSGROUP 33CWITH SUFFIX DL, DR,GEFL, FR)ORGROUP 33DGER 545174-01-2 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 33A454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A ORPW454ML 454MR 464DL 50000 FHOR464DR 464FL 464FR I: 10700 FCGROUP 33B464KL 464KR 464ML ORPW464MR 32000 FHORPOST 43271 (ACCESSGROUP 33CWITH SUFFIX KL, KR,PWML, MR)ORPRE 43271 (ACCESSGROUP 33DWITH SUFFIX DL, DR,PWFL, FR)ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 36APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545174-01-3 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 33A454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A ORRR454ML 454MR 464DL 50000 FHOR464DR 464FL 464FR I: 7700 FCGROUP 33B464KL 464KR 464ML ORRR464MR 23200 FHORPOST 43271 (ACCESSGROUP 33CWITH SUFFIX KL, KR,RRML, MR)ORPRE 43271 (ACCESSGROUP 33DWITH SUFFIX DL, DR,RRFL, FR)545174-01-4 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 33E454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A OR464ML 464MR 50000 FHI: 11000 FCOR33000 FH545174-01-5 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 17000 FCGROUP 32E454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A OR464ML 464MR 50000 FHI: 10400 FCOR50000 FHN 545174-01-6 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 32A454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A ORRR454ML 454MR 464DL 50000 FH464DR 464FL 464FR I: 7600 FC464KL 464KR 464ML OR464MR 38100 FHPOST 43271 (ACCESSWITH SUFFIX KL, KR,ML, MR)PRE 43271 (ACCESSWITH SUFFIX DL, DR,FL, FR)ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 37APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 545174-01-7 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 20000 FCGROUP 32A454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A ORPW454ML 454MR 464DL 50000 FH464DR 464FL 464FR I: 10500 FC464KL 464KR 464ML OR464MR 50000 FHPOST 43271 (ACCESSWITH SUFFIX KL, KR,ML, MR)PRE 43271 (ACCESSWITH SUFFIX DL, DR,FL, FR)545174-02-1 N/A TASK DELETED545174-02-2 N/A TASK DELETED545174-02-3 N/A TASK DELETEDR 545174-03-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 10 YE NO CPCP A330-200454FR 454KL 454KR 464 FITTING AND LINKS AT RIB 18A I: 10 YEPRE 48298454ML 454MR 464DLAND464DR 464FL 464FRPRE 50003464KL 464KR 464MLAND464MRPRE 54399BEARINGSORENGINEA330-300LINKSPRE 48298POST 43271 (ACCESSANDWITH SUFFIX KL, KR,PRE 50003ML, MR)ANDPRE 43271 (ACCESSPRE 54399WITH SUFFIX DL, DR,FL, FR)ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 38APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 545174-03-2 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE T: 20 YE NO CPCP A330-200454MR 464KL 464KR 464 FITTING AND LINKS AT RIB 18A I: 12 YE I: 12 YEPOST 48298464ML 464MRORBEARINGSPOST 50003ENGINEORLINKSPOST 54399ORA330-300POST 48298ORPOST 50003ORPOST 54399ORA330-200FR 545180-03-1 454DL 454DR 454FL 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A330-200454FR 464DL 464DR 464 FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER I: 12 YEPRE 43271464FL 464FR PYLON)ORBOLTSA330-300ENGINEPRE 43271LINKSSLEEVESR 545180-03-2 454KL 454KR 454ML 454 DETAILED INSPECTION OF PYLON TO WING ATTACHMENT T: 12 YE NO CPCP A330-200454MR 464KL 464KR 464 FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER I: 12 YEPOST 43271464ML 464MR PYLON)ORBOLTSA330-200FENGINEORLINKSA330-300SLEEVESPOST 43271545180-04-1 N/A TASK DELETED545180-04-2 N/A TASK DELETED545180-04-3 N/A TASK DELETED545180-04-4 N/A TASK DELETEDISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 39APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS545180-04-5 N/A TASK DELETED545705-02-1 N/A TASK DELETED545709-01-1 N/A TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 NACELLES/PYLONS SECTION: D-54PAGE 40APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS551001-01-1 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP ALL312 ASSEMBLY OF TRIM ACTUATING ARMS, SUPPORT FITTINGS AND I: 12 YE I: 12 YEUPPER AND LOWER ATTACHMENT PLATES551002-01-2 312AR 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, TRIM T: 20000 FCALL312 ACTUATING ARM LUGS AND SUPPORT FITTING LUGS I: 20000 FC551004-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER, T: 12 YE T: 20 YE CPCP ALL312 ASSEMBLY OF HINGE FITTING AT RIB 3, UPPER AND LOWER I: 12 YE I: 12 YEATTACH FITTINGS, LH/RH551007-01-2 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-1 ALL312 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 12 YESPAR AND BETWEEN FUSELAGE FAIRING LINESR 551008-01-3 312AR 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCA330-200312 BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE I: 9200 FCORFAIRING LINES ORA330-30037100 FH551009-01-3 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCGROUP 33AREARMOST UPPER 343 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 10600 FCORFAIRING SUPPORT SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, ORGROUP 33BFITTING LH/RH 33900 FHORGROUP 33CORGROUP 33D551009-01-4 333AT 343AT 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCA330-200REARMOST UPPER 343 CENTER BOX TOP SKIN UPPER SURFACE FROM FRONT TO REAR I: 5500 FCORFAIRING SUPPORT SPAR AND BETWEEN RIB 3 AND FUSELAGE FAIRING LINE, ORGROUP 33EFITTING LH/RH 22500 FH551010-01-2 312AR 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-1 ALL312 CENTER BOX BOTTOM SKIN LOWER SURFACE FROM FRONT TO I: 12 YEREAR SPAR AND BETWEEN FUSELAGE FAIRING LINESISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS551011-01-1 313AL 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 12 YE T: 20 YE CPCP ALL312 SPAR AFT FACE JOINT PLATE INBOARD OF RIB 3, LH/RH OR I: 12 YE20000 FCI: 12 YEOR20000 FC551012-01-2 313AL 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE CPCP ZL-311-01-1 ALL312 CENTER BOX REAR SPAR AFT FACE BETWEEN RIB 3 LH AND I: 20000 FC I: 12 YERIB 3 RH, EXCLUDING INBOARD JOINT PLATES551013-01-1 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 12 YE 1 CPCP ALL312 SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, LH/RH I: 12 YE334344551013-01-4 313AL 334AB 344AB 311 DETAILED INSPECTION OF HORIZONTAL STABILIZER REAR T: 20000 FCALL312 SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, LH/RH I: 18300 FC334 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS OR344 TASK 551013-02-3 60400 FH551013-02-3 313AL 334AB 344AB 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCALL312 REAR SPAR AFT FACE JOINT PLATE OUTBOARD OF RIB 3, I: 18300 FC334 LH/RH OR344 NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 60400 FHTASK 551013-01-4R 551015-01-1 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE CPCP ZL-311-01-1 A330-200312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 20000 FC I: 12 YEORRIB 3 RHA330-300N 551015-01-3 312AR 311 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-311-01-1 A330-200F312 CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO I: 12 YERIB 3 RH551016-01-2 N/A TASK DELETEDISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS551016-01-4 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCGROUP 32E312 CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD I: 20000 FCOROF RIB 3, LH/RH.GROUP 33EN 551018-01-3 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-319-02-1 A330-200319BL 319BR 319CR CENTER BOX INTERNAL STRUCTURE I: 12 YEPRE 41600DISCONNECT SCAVENGEORWATER PIPEA330-300PRE 41600N 551018-01-4 312AR 319AL 319AR 319 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE NO CPCP ZL-319-02-2 A330-200319BL 319DR 319ER CENTER BOX INTERNAL STRUCTURE I: 12 YEPOST 41600ORA330-300POST 41600ORA330-200FN 551019-01-3 313AL 311 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCA330-200312 CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 6700 FCORREAR SPAR WEB FROM RIB 3LH TO RIB 3RH ORA330-30026700 FH551020-01-2 N/A 300 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCALLBOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES OUTBOARD I: 20000 FCOF FUSELAGE FAIRINGS551020-02-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE CPCP ZL-300-01-1 ALLCENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES I: 6 YEOUTBOARD OF FUSELAGE FAIRINGS551021-01-1 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YE CPCP ZL-300-01-1 ALLCENTER BOX BOTTOM SKIN LOWER SURFACE CHORDWISE I: 6 YESPLICES OUTBOARD OF FUSELAGE FAIRINGS LH/RHISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS551022-01-1 331AT 331BT 333AB 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER LATERAL T: 12 YE NO CPCP ALL333AL 333AT 341AT 343 BOX INTERNAL STRUCTURE BETWEEN RIB 3 AND RIB 4 I: 12 YE341BT 343AB 343AR343ATN 551024-01-1 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-331-01-1 A330-200F333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 12 YE343AB 343AT RIB 4R 551024-01-2 331AT 331BT 333AB 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 20000 FC T: 12 YE CPCP ZL-331-01-1 A330-200333AT 341AT 341BT 341 LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND I: 20000 FC I: 12 YEOR343AB 343AT RIB 4A330-300551025-01-2 331AT 331BT 331CT 331 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YEZL-331-01-1 ALL331DT 331ET 332AB 332 LATERAL BOX FRONT SPAR FORWARD FACE FROM RIB 4 TO END I: 12 YEZL-332-01-1332AT 333AB 333AT 341 RIB AND EXTERNAL SURFACE OF END RIB341AT 341BT 341CT 342341DT 341ET 342AB342AT 343AB 343AT551026-01-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-300-01-1 ALLLATERAL BOX TOP SKIN UPPER SURFACE FROM CHORDWISE I: 6 YESPLICE LINE TO END RIB551027-01-2 N/A 300 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 3 YEALLLATERAL BOX BOTTOM SKIN LOWER SURFACE FROM CHORDWISE I: 3 YESPLICE LINE TO END RIBR 551028-01-4 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCGROUP 32A343 BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE I: 4700 FCOR(5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE ORGROUP 32EFAIRINGS 15500 FHORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-4GROUP 32FORGROUP 33EISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS551028-01-5 N/A 333 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCGROUP 33A343 BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, FIVE I: 6200 FCOR(5) REARMOST ROWS OF FASTENERS OUTBOARD OF FUSELAGE ORGROUP 33BFAIRINGS 20300 FHORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-02-5GROUP 33CORGROUP 33DR 551028-02-4 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCGROUP 32A343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, I: 8100 FCORFIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF ORGROUP 32EFUSELAGE FAIRINGS 33200 FHORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-4GROUP 32FORGROUP 33E551028-02-5 N/A 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCGROUP 33A343 CENTER BOX TOP SKIN UPPER SURFACE CHORDWISE SPLICES, I: 18000 FCORFIVE (5) REARMOST ROWS OF FASTENERS OUTBOARD OF ORGROUP 33BFUSELAGE FAIRINGS 58900 FHORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 551028-01-5GROUP 33CORGROUP 33DR 551029-01-3 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCA330-200319BL 319BR 319CR BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO FRONT I: 20000 FCPRE 41600DISCONNECT SCAVENGE SPAR WEB FROM RIB 3LH TO RIB 3RHORWATER PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA330-300TASK 551029-02-3PRE 41600R 551029-01-4 312AR 319AL 319AR 319 DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER T: 20000 FCA330-200319BL 319DR 319ER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO FRONT I: 20000 FCPOST 41600SPAR WEB FROM RIB 3LH TO RIB 3RHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA330-300TASK 551029-02-4POST 41600ORA330-200FISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 551029-02-3 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCA330-200319BL 319BR 319CR CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 20000 FCPRE 41600DISCONNECT SCAVENGE FRONT SPAR WEB FROM RIB 3LH TO RIB 3RHORWATER PIPE NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA330-300TASK 551029-01-3PRE 41600R 551029-02-4 312AR 319AL 319AR 319 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 20000 FCA330-200319BL 319DR 319ER CENTER BOX TOP SKIN INTEGRAL FLANGE AT ATTACHMENT TO I: 20000 FCPOST 41600FRONT SPAR WEB FROM RIB 3LH TO RIB 3RHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ASA330-300TASK 551029-01-4POST 41600ORA330-200F551030-01-2 334AB 334BB 334CB 334 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 6 YEZL-334-02-1 ALL334DB 334EB 334FB 344 LATERAL BOX REAR SPAR AFT FACE FROM RIB 3 OUTBOARD I: 6 YE334GB 344AB 344BB JOINT PLATE TO END RIB344CB 344DB 344EB344FB 344GB551031-01-1 334BB 334CB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 20000 FC T: 6 YE 1 CPCP ALL335BB 344BB 344CB 344 FITTINGS NO 2 AND 3 AND SUPPORT RIBS I: 20000 FC I: 6 YE344DB 345BB551032-01-1 334CB 334CT 344CB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER ACTUATOR T: 20000 FC T: 6 YE 1 CPCP ALL344CT 344 ATTACHMENT FITTING AND REACTION BAR AT RIBS 8 AND 9 I: 20000 FC I: 6 YE551033-01-1 334AB 334BB 334DB 334 DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE T: 20000 FC T: 12 YE 1 CPCP ALL334EB 334FB 334GB 344 FITTINGS NO 1,4,5,6 AND 7 AND SUPPORT RIBS I: 20000 FC I: 12 YE335AB 335CB 335DB335EB 335FB 344AB344BB 344DB 344EB344FB 344GB 345AB345CB 345DB 345EB345FBISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 6APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 551035-01-1 332AB 332AT 333BB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A330-200333CB 333DB 333EB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YEPOST 41471333FB 333GB 343BB RIB, LH / RHPRE 43491343CB 343DB 343EBOR343FB 343GB 344GBA330-300346ABPOST 41471PEELABLE HOLE COVERSPRE 43491R 551035-01-2 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A330-200333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND RIB I: 12 YEPOST 43491343DB 343EB 343FB 13 LH / END RIB RHPRE 44818343GB 344GB 346ABORPEELABLE HOLE COVERSA330-300POST 43491PRE 44818R 551035-01-3 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A330-200333EB 333FB 333GB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND END I: 12 YEPOST 44818334AZ 334GB 343BB RIB, LH / RHOR343CB 343DB 343EBA330-300343FB 343GB 344GBPOST 44818346ABORPEELABLE HOLE COVERSA330-200FN 551035-01-4 333BB 333CB 333DB 333 SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP A330-200333EB 343BB 343CB 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 4 AND RIB I: 12 YEPRE 41471343DB 343EB 343FB 13 LH / END RIB RHOR343GB 344GB 346ABA330-300PEELABLE HOLE COVERSPRE 41471R 551035-02-1 331ET 332AB 332AT 333 GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER T: 12 YE CPCP ZL-333-01-2 A330-200333EL 343 LATERAL BOX INTERNAL STRUCTURE BETWEEN RIB 13 AND I: 12 YEPRE 41471PEELABLE HOLE COVERS END RIB LHORPOST 43491PRE 44818ORA330-300PRE 41471ORPOST 43491PRE 44818ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 7APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 552001-01-2 N/A 300 GENERAL VISUAL INSPECTION OF ELEVATOR TOP AND BOTTOM T: 3 YEZL-300-01-1 ALLSKIN PANELS INCLUDING TRAILING EDGE, EXTERNAL SURFACE I: 3 YE552002-01-1 334BB 334CB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO 2 T: 20000 FC T: 6 YE 1 CPCP ALL335BB 344BB 344CB 345 AND 3 AND ACTUATOR FITTINGS, LH / RH I: 20000 FC I: 6 YE344DB 345BB552003-01-1 334AB 334BB 334CB 335 DETAILED INSPECTION OF ELEVATOR SPAR FORWARD FACE T: 12 YEALL334DB 334EB 334FB 345 I: 12 YE334GB 335AB 335BB335CB 335DB 335EB335FB 344AB 344BB344CB 344DB 344EB344FB 344GB 345AB345BB 345CB 345DB345EB 345FB552004-01-1 N/A 300 SPECIAL DETAILED INSPECTION OF ELEVATOR TOP AND T: 6 YEALLBOTTOM SKIN PANELS IN AREA OF HINGE FITTINGS NO 2 AND I: 6 YE3 AND AREA OF ACTUATOR FITTINGS, EXTERNAL SURFACE552005-01-1 334AB 334BB 334DB 335 DETAILED INSPECTION OF ELEVATOR HINGE FITTINGS NO T: 20000 FC T: 12 YE 1 CPCP ALL334EB 334FB 334GB 345 1,4,5,6 AND 7 I: 20000 FC I: 12 YE335AB 335CB 335DB335EB 335FB 344AB344BB 344DB 344EB344FB 344GB 345AB345CB 345DB 345EB345FB553004-01-1 N/A TASK DELETED553005-01-1 N/A TASK DELETED553008-01-2 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SKIN T: 6 YEA330-300PANELS FROM FRONT TO REAR SPAR AND FROM FIN/FUSELAGE I: 6 YEFAIRING TO TOP, EXTERNAL SURFACE LH/RHISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 8APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS553009-01-2 325AL 325BL 325CL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YEZL-325-02-1 A330-300325DL 325EL 325FL SPAR AFT FACE INCLUDING SUPPORT FITTINGS FOR RUDDER I: 6 YE325GL 325HL 325JL HINGE ARMS325KLR 553010-01-2 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-322-01-1 A330-300324AT 324BT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YEZL-324-01-1FACE553011-01-2 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-323-01-1 A330-300STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YERIB 8, INCLUDING LOWER SURFACE OF RIB 1553012-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YEA330-300CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS I: 6 YE553013-01-2 322BL 322CL 324AT 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-323-02-1 A330-300325DL 325EL 325FL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 8 AND I: 12 YE325GL 325HL 325JL RIB 18325KLPEELABLE HOLE COVERS553014-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER RIB T: 12 YE 1 CPCP A330-3001 AND RIB 5, METALLIC REINFORCEMENTS AT THE MANHOLES I: 6 YEPRE 40843553015-01-1 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND SUPPORT T: 6 YE 1 CPCP A330-300325HL 325KL 326BL FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YEPRE 40904326DL 326DR 326FL326HL 326KL553015-01-2 325BL 325DL 325FL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND SUPPORT T: 6 YE 1 CPCP A330-300325HL 325KL 326DL FITTINGS AND ACTUATOR SUPPORT FITTINGS I: 6 YEPOST 40904326DRISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 9APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 553020-01-1 N/A 300 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER SKIN T: 6 YEA330-200PANELS FROM FRONT TO REAR SPAR AND FROM FIN/FUSELAGE I: 6 YEPOST 48979FAIRING TO TOP, EXTERNAL SURFACE LH/RH.ORA330-200F553021-01-1 325LL 325ML 325NL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YEZL-325-02-2 A330-200325PL 325QL 325RL SPAR AFT FACE I: 6 YEPRE 48979R 553021-01-2 325LL 325NL 325SL 325 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER REAR T: 6 YEZL-325-02-3 A330-200325TL 325UL 325VL SPAR AFT FACE I: 6 YEPOST 48979ORA330-200F553022-01-1 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-322-01-2 A330-200322DL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YEZL-324-01-2 PRE 48979FACE.R 553022-01-2 322AL 322BL 322CL 322 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-322-01-3 A330-200322EL 324CT 324 FRONT SPAR FORWARD FACE AND UPPER CLOSING RIB UPPER I: 12 YEZL-324-01-2 POST 48979FACE.ORA330-200F553023-01-1 311AZ 311BZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-323-01-1 A330-200STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YEPRE 48979RIB 5 INCLUDING LOWER SURFACE OF RIB 1.R 553023-01-2 311AZ 312AR 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 6 YEZL-323-01-1 A330-200STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 1 AND I: 6 YEPOST 48979RIB 5 INCLUDING LOWER SURFACE OF RIB 1.ORA330-200F553024-01-1 311AZ 311BZ 312AR 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YEA330-200323CL 323DL 325LL CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS. I: 6 YEPRE 48979ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 10APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 553024-01-2 311AZ 312AR 323DL 323 DETAILED INSPECTION OF VERTICAL STABILIZER, FWD, T: 6 YEA330-200323EL 325LL CENTER AND AFT MAIN FITTINGS AND SIDELOAD FITTINGS. I: 6 YEPOST 48979ORA330-200F553025-01-1 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-323-02-2 A330-200324CT 325ML 325NL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 5 AND I: 12 YEZL-324-01-2 PRE 48979325PL 325QL 325RL RIB 13.PEELABLE HOLE COVERSR 553025-01-2 322BL 322CL 322DL 323 GENERAL VISUAL INSPECTION OF VERTICAL STABILIZER T: 12 YEZL-323-02-3 A330-200324CT 325NL 325SL STRUCTURAL BOX INTERNAL STRUCTURE BETWEEN RIB 5 AND I: 12 YEZL-324-01-2 POST 48979325TL 325UL 325VL RIB 13.ORPEELABLE HOLE COVERSA330-200F553026-01-1 325LL 325ML 325NL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR T: 6 YE 1 CPCP A330-200325PL 325QL 325RL SUPPORT FITTINGS. I: 6 YEPRE 48979326ML 326NL 326PL326QLR 553026-01-2 325LL 325NL 325SL 325 DETAILED INSPECTION OF RUDDER HINGE ARMS AND ACTUATOR T: 6 YE 1 CPCP A330-200325TL 325UL 325VL SUPPORT FITTINGS. I: 6 YEPOST 48979326ML 326NL 326PLOR326RL 326SLA330-200FR 554001-01-2 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YEZL-300-01-1 A330-300EXTERNAL SURFACE LH/RH I: 6 YER 554003-01-1 324BT 325AL 325BL 326 SPECIAL DETAILED INSPECTION OF RUDDER FRONT SPAR T: 6 YEA330-300325CL 325DL 325EL I: 6 YEPRE 40904325FL 325GL 325HL325JL 325KL 326AL326BL 326CL 326DL326EL 326FL 326GL326HL 326JL 326KL326LLPEELABLE HOLE COVERSISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 11APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 554003-01-2 324BT 325AL 325BL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YEA330-300325CL 325DL 325EL I: 6 YEPOST 40904325FL 325GL 325HL325JL 325KL 326DLPEELABLE HOLE COVERSD 554005-01-1 N/A TASK DELETEDD 554005-01-2 N/A TASK DELETED554006-01-1 N/A TASK DELETED554007-01-1 N/A TASK DELETED554008-01-1 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A330-300325HL 325KL 326BL I: 6 YEPRE 40904326BR 326DL 326DR326FL 326FR 326HL326HR 326KL 326KR554008-01-2 325BL 325DL 325FL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A330-300325HL 325KL 326DL I: 6 YEPOST 40904326DRN 554009-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA330-300BOOSTER AREA, LH/RH I: 6 YEN 554010-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 3 YEA330-300AREA OF FRONT SPAR AND RIB 0 I: 3 YEPRE 40904N 554010-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA330-300AREA OF FRONT SPAR AND RIB 0 I: 6 YEPOST 40904ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 12APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 554011-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA330-300AREA OF HOISTING POINTS AND TRAILING EDGE SCREW LINE I: 6 YELH/RHN 554012-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDER SIDE PANEL IN T: 6 YEA330-300ATTACH FITTING AREA, LH/RH. I: 6 YEPRE 40904N 554012-01-2 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA330-300ATTACH FITTING AREA, LH/RH. I: 6 YEPOST 40904N 554013-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YEA330-300INTERNAL STRUCTURE, LH/RH I: 6 YEN 554014-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0 T: 6 YEZL-300-01-1 A330-300I: 6 YER 554020-01-1 N/A 300 GENERAL VISUAL INSPECTION OF RUDDER SIDE PANELS T: 6 YEZL-300-01-1 A330-200EXTERNAL SURFACE LH/RH. I: 6 YEORA330-200FR 554021-01-1 325LL 325LR 325ML 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YEA330-200325MR 325NL 325NR I: 6 YEPRE 48979325PL 325PR 325QL325QR 325RL 325RR326AT 326ML 326NL326PL 326QLPEELABLE HOLE COVERSR 554021-01-2 325LL 325LR 325NL 326 DETAILED INSPECTION OF RUDDER FRONT SPAR T: 12 YEA330-200325NR 325SL 325TL I: 6 YEPOST 48979325TR 325UL 325UROR325VL 325VR 326ATA330-200F326ML 326NL 326PL326RL 326SLPEELABLE HOLE COVERSD 554022-01-1 N/A TASK DELETEDISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 13APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 554023-01-1 325LL 325ML 325NL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A330-200325PL 325QL 325RL I: 6 YEPRE 48979326ML 326NL 326PL326QLR 554023-01-2 325LL 325NL 325SL 326 DETAILED INSPECTION OF RUDDER HINGE FITTINGS T: 6 YE 1 CPCP A330-200325TL 325UL 325VL I: 6 YEPOST 48979326ML 326NL 326PLOR326RL 326SLA330-200FN 554024-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA330-200BOOSTER AREA, LH/RH. I: 6 YEORA330-200FN 554025-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA330-200AREA OF FRONT SPAR AND RIB 0 I: 6 YEORA330-200FN 554026-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 6 YEA330-200AREA OF HOISTING POINTS AND SCREW LINE, LH/RH. I: 6 YEORA330-200FN 554027-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL IN T: 12 YEA330-200ATTACH FITTING AREA, LH/RH I: 6 YEORA330-200FN 554028-01-1 N/A 326 SPECIAL DETAILED INSPECTION OF RUDDER SIDE PANEL T: 6 YEA330-200INTERNAL STRUCTURE, LH/RH I: 6 YEORA330-200FN 554029-01-1 N/A 326 GENERAL VISUAL INSPECTION OF RUDDER RIB 0 T: 6 YEZL-300-01-1 A330-200I: 6 YEORA330-200F* * * * * E N D * * * * *ISSUE: JUL 01/10 STABILIZERS SECTION: D-55PAGE 14APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 562101-01-2 830 840 221 DETAILED INSPECTION OF MAIN DECK WINDOW PANES T: 6 YEALL222 INCLUDING PASSENGER/COURIER/CREW DOOR AND EMERGENCY I: 6 YE231 EXIT WINDOW PANES232241242251252261262271272* * * * * E N D * * * * *ISSUE: JUL 01/10 WINDOWS SECTION: D-56PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571102-01-3 N/A TASK DELETED571102-01-4 N/A TASK DELETED571102-01-5 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 33EAIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 ORDUCTS LEVEL, LH/RH 50000 FHLINING I: 5550 FCNOTE 1 OR16600 FH571102-01-6 821 137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, T: 17000 FCGROUP 32EAIR CONDITIONING 138 FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 ORDUCTS LEVEL, LH/RH 50000 FHLINING I: 5140 FCNOTE 1 OR25700 FH571103-01-3 N/A TASK DELETED571103-01-4 N/A TASK DELETED571103-02-3 N/A TASK DELETED571103-02-4 N/A TASK DELETED571105-01-1 734 744 143 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN T: 12 YE 1 CPCP ALLAIR CONDITIONING 191 LOWER SURFACE FROM FR 40 TO FR 47 BETWEEN RIB 1 LH I: 12 YEPACKS 192 AND RIB 1 RHFAIRING PANELS 193BETWEEN FR 40 AND FR 19547 196HEATSHIELDSISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571106-01-1 191HB 191QB 192HB 191 GENERAL VISUAL INSPECTION OF CENTER WING BOX, LOWER T: 12 YE 1 CPCP ALL192QB 192 SPLICE AT RIB 1 BETWEEN FR 40 AND FR 47 I: 12 YE195196N 571107-01-1 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32A196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OR21, LH/RH 50000 FHI: 5300 FCOR26700 FHN 571107-01-3 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33C196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OROR21, LH/RH 50000 FHGROUP 33DI: 5900 FCOR17700 FHR 571107-01-4 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33A196 PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & OROR21, LH/RH 50000 FHGROUP 33BI: 6200 FCOR18600 FH571107-01-5 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E196 LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS OR20 & 21, LH/RH 50000 FHI: 5100 FCOR25500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571107-01-6 191QB 192QB 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E196 LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS OR20 & 21, LH/RH 50000 FHI: 5770 FCOR17300 FHN 571108-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FCGROUP 33C744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR50000 FHI: 8300 FCOR25100 FHR 571108-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FCGROUP 33A744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OROR50000 FHGROUP 33BI: 8400 FCOR25200 FHR 571108-01-6 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FCGROUP 32A744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR50000 FHI: 7400 FCOR37300 FHR 571108-01-7 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 20000 FCGROUP 33D744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR50000 FHI: 8150 FCOR24500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571108-01-8 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 17000 FCGROUP 33E744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR50000 FHI: 7900 FCOR23600 FH571108-01-9 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX INTERNAL T: 17000 FCGROUP 32E744 142 STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. OR50000 FHI: 7000 FCOR35000 FHR 571114-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OROR28. 50000 FHGROUP 33BI: 13000 FCOR39000 FHR 571114-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 18000 FCGROUP 32A744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR28. 72000 FHI: 10900 FCOR54500 FHR 571114-01-7 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33D744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 ORORAND 28. 50000 FHGROUP 33CI: 11900 FCOR35800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571114-01-8 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR28. 50000 FHI: 12000 FCOR36000 FH571114-01-9 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E744 142 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND OR28 50000 FHI: 10600 FCOR50000 FHN 571116-01-2 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32APANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN ORSTRINGERS 21 & 22, AT Y =-567.5 50000 FHI: 5350 FCOR26700 FHN 571116-01-3 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33CPANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN ORORSTRINGERS 21 & 22, AT Y =-567.5 50000 FHGROUP 33DI: 5900 FCOR17700 FHR 571116-01-4 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33APANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN ORORSTRINGERS 21 & 22, AT Y =-567.5 50000 FHGROUP 33BI: 6200 FCOR18600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571116-01-5 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 32EPANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN ORSTRINGERS 21 & 22, AT Y =-567.5 50000 FHI: 5100 FCOR25500 FH571116-01-6 193DB 193 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 33EPANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN ORSTRINGERS 21 & 22, AT Y =-567.5 50000 FHI: 5770 FCOR17300 FH571118-01-10 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 33EBETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FHSTR 28. I: 5770 FCOR17300 FHN 571118-01-6 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32ABETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FHSTR 28. I: 5350 FCOR26700 FHR 571118-01-7 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33ABETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OROR47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FHGROUP 33BSTR 28. I: 6200 FCOR18600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 6APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 571118-01-8 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33CBETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OROR47 STRINGERS 25 & 26, AND AT Y=180 BETWEEN STRINGERS 27 50000 FHGROUP 33D& 28. I: 5900 FCOR17700 FH571118-01-9 FAIRING PANELS 143 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 32EBETWEEN FR 44 AND FR 195 PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230 BETWEEN OR47 STR 25 AND STR 26, AND AT Y=180 BETWEEN STR 27 AND 50000 FHSTR 28. I: 5100 FCOR25500 FH571119-01-1 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCPRE 49202GALLEYS 146 STRUCTURE, LONGITUDINAL BEAMS ABOVE CWB, WEB HOLE I: 3100 FCORAREA BETWEEN FRAMES 41 AND 42 FROM Y=-1456 TO Y=1456.POST 50755(7 BEAMS TO BE INSPECTED)571121-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 20000 FCGROUP 32A148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL I: 8000 FCORBEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TOGROUP 33AY=1959. (9 ASSY TO BE INSPECTED)ORGROUP 33BORGROUP 33CORGROUP 33D571121-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 33E148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL ORBEAM AT JUNCTION WITH CWB AFT PANEL 50000 FHFROM Y=-1959 TO Y=1959. (9 ASSY TO BE INSPECTED) I: 8000 FCOR24000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 7APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571121-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL T: 17000 FCGROUP 32E148 STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL ORBEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO 50000 FHY=1959. (9 ASSY TO BE INSPECTED) I: 8000 FCOR40000 FHR 571122-01-4 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER ORORCHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 50000 FHGROUP 33BTO Y=1959, LH/RH. I: 4900 FCOR14700 FH571122-01-5 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 32A196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER ORORCHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 50000 FHGROUP 33CTO Y=1959, LH/RH. I: 4380 FCOR15300 FH571122-01-6 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX EXTERN T: 20000 FCGROUP 33D196 STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER CHORD OR(L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO 50000 FHY=1959, LH/RH. I: 4270 FCOR14900 FH571122-01-7 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER OR(L FITTING) AND LOWER SKIN JUNCTION, FROM Y=953 TO 50000 FHY=1959, LH/RH. I: 4450 FCOR13300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 8APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571122-01-8 734 744 195 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E196 EXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPAR LOWER ORCHORD (L FITTING) AND LOWER SKIN JUNCTION, 50000 FHFROM Y=953 TO Y=1959, LH/RH. I: 3920 FCOR19600 FHR 571125-01-3 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 20000 FCGROUP 33A148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND ORORFRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FHGROUP 33BI: 6150 FCOR18500 FHR 571125-01-4 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 18000 FCGROUP 32A148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND ORFRAME 47 LOWER CORNER FITTING, LH/RH. 72000 FHI: 4000 FCOR20000 FHR 571125-01-5 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 20000 FCGROUP 33C148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND ORORFRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FHGROUP 33DI: 4400 FCOR13300 FH571125-01-6 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 17000 FCGROUP 33E148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND ORFRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FHI: 4320 FCOR12900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 9APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571125-01-7 734 744 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR T: 17000 FCGROUP 32E148 SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND ORFRAME 47 LOWER CORNER FITTING, LH/RH. 50000 FHI: 3820 FCOR19100 FHR 571126-01-3 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 33ASPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORORLOWER CORNER. 50000 FHGROUP 33BI: 13600 FCOR41000 FHR 571126-01-4 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 32ASPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORLOWER CORNER. 50000 FHI: 10800 FCOR54200 FHR 571126-01-5 734 147 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 33CSPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORORLOWER CORNER. 50000 FHGROUP 33DI: 11900 FCOR35700 FH571126-01-6 734 147 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR T: 17000 FCGROUP 33ESPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORLOWER CORNER. 50000 FHI: 11400 FCOR34300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 10APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571126-01-7 734 147 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR T: 17000 FCGROUP 32ESPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE ORLOWER CORNER. 50000 FHI: 10200 FCOR50000 FHR 571129-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 20000 FCGROUP 33A744 142 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OROR50000 FHGROUP 33BI: 11500 FCOR34600 FH571129-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, T: 20000 FCGROUP 32A744 142 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OROR50000 FHGROUP 33CI: 12000 FCORORGROUP 33D34700 FH571129-01-6 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, CENTER T: 17000 FCGROUP 32E744 142 SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES). OROR50000 FHGROUP 33EI: 17000 FCOR50000 FHR 571130-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 33A744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OROR147 50000 FHGROUP 33B148 I: 6900 FCOR20700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 11APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571130-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 32A744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OROR147 50000 FHGROUP 33C148 I: 7500 FCOR26200 FH571130-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 20000 FCGROUP 33D744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR147 50000 FH148 I: 7300 FCOR25800 FH571130-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 17000 FCGROUP 33E744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR147 50000 FH148 I: 10100 FCOR30400 FH571130-01-7 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR T: 17000 FCGROUP 32E744 142 SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES). OR147 50000 FH148 I: 9400 FCOR46700 FH571131-01-1 734 744 147 GENERAL VISUAL INSPECTION OF CENTER WING BOX, REAR T: 6 YE 1 CPCP ALL148 SPAR, AFT FACE I: 6 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 12APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571133-01-4 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON T: 20000 FCGROUP 32A744 142 LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS OROR(63 PLACES). 50000 FHGROUP 33AI: 10000 FCORORGROUP 33B29000 FHORGROUP 33CORGROUP 33D571133-01-5 147AZ 148AZ 734 141 DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS T: 17000 FCGROUP 32E744 142 ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTION OROR(63 PLACES). 50000 FHGROUP 33EI: 17000 FCOR50000 FH571137-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33A192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORPOST 41652AT FR.40, LH/RH. 50000 FHORI: 8000 FCGROUP 33BORPOST 4165223200 FH571137-01-4 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32A192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORORAT FR.40, LH/RH. 50000 FHGROUP 33CI: 8000 FCORORGROUP 33D40800 FH571137-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 33E192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL ORAT FR.40, LH/RH. 50000 FHI: 8000 FCOR24000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 13APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571137-01-6 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 32E192 PANEL LOWER SURFACE, JUNCTION AREA WITH THE KEEL BEAM ORAT FR.40, LH/RH. 50000 FHI: 8000 FCOR40000 FH571138-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A744 142 INTERNAL STRUCTURE, LOWER L FITTING AT CONNECTION ORPOST 43577WITH LOWER SKIN PANEL AT KEEL BEAM LEVEL, LH/RH. 50000 FHORI: 8000 FCGROUP 33BORPOST 4357723200 FHR 571140-01-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 6 YE 1 CPCP A330-200GALLEYS 146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 6 YENOTETOILETS BETWEEN FR 40 AND FR 47ORNOTE: TASK APPLICABLE IF GALLEYS OR TOILETS AREA330-300FITTED ABOVE THIS AREANOTER 571140-02-1 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 12 YE 1 CPCP A330-200146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 12 YENOTEBETWEEN FR 40 AND FR 47ORNOTE: TASK APPLICABLE IF GALLEYS OR TOILETS ARE NOTA330-300FITTED ABOVE THIS AREANOTEN 571140-02-2 CABIN FLOOR PANELS 145 DETAILED INSPECTION OF CENTER WING BOX TOP SKIN UPPER T: 6 YE 1 CPCP A330-200F146 SURFACE, PORTAL FRAMES AND LATERAL FUSELAGE STRUCTURE I: 6 YEBETWEEN FR 40 AND FR 47.571141-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 14APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 571144-01-1 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 FCGROUP 33A192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF ORPRE 41652195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 50000 FHOR196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 9600 FCGROUP 33BSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORPRE 41652LH/RH. 28800 FH571144-01-2 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 FCGROUP 33A192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF ORPOST 41652195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 50000 FHOR196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 11100 FCGROUP 33BSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORPOST 41652LH/RH. 33200 FH571144-01-3 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 FCGROUP 32A192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OROR195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 50000 FHGROUP 33C196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5700 FCSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORLH/RH. 28100 FH571144-01-4 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 20000 FCGROUP 33D192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 50000 FH196 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, STR. I: 5600 FC18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORLH/RH. 27500 FH571144-01-5 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 17000 FCGROUP 33E192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR195 OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 50000 FH196 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 6200 FCSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORLH/RH 18800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 15APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571144-01-6 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER T: 17000 FCGROUP 32E192QB 192 SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF OR195 RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 50000 FH196 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, I: 5500 FCSTR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, ORLH/RH. 27400 FHR 571145-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORPRE 41652SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FHORSTR.21 AND STR.25 TO 29, LH/RH. I: 7600 FCGROUP 33BORPRE 4165222900 FH571145-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORPOST 41652SEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FHORSTR.21 AND STR.25 TO 29, LH/RH. I: 9600 FCGROUP 33BORPOST 4165228700 FHR 571145-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 32A744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORSEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FHSTR.21 AND STR.25 TO 29, LH/RH. I: 8150 FCOR40700 FH571145-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORSEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 50000 FHSTR.21 AND STR.25 TO 29, LH/RH. I: 8900 FCOR26800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 16APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571145-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORSEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, 50000 FHSTR.20, STR.21 AND STR.25 TO 29, LH/RH. I: 7800 FCOR39200 FHR 571145-01-6 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33C744 142 INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD ORORSEALANT REMOVAL FLANGE, FASTENERS IN RADIUS AREA AT STR.16, 50000 FHGROUP 33DSTR.20, STR.21 AND STR.25 TO 29, LH/RH. I: 9000 FCOR27200 FH571146-01-4 N/A TASK DELETED571146-01-5 N/A TASK DELETED571146-01-6 N/A TASK DELETEDR 571146-02-4 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33A192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OROR195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, 50000 FHGROUP 33B196 STR21 AND STR25 TO STR29, LH/RH. I: 9600 FCOR28800 FHR 571146-02-5 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32A192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, STR21 50000 FH196 AND STR25 TO STR29, LH/RH. I: 7900 FCOR39400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 17APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571146-02-6 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 33E192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, STR21 50000 FH196 AND STR25 TO STR29, LH/RH. I: 8300 FCOR25000 FH571146-02-7 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 32E192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OR195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, 50000 FH196 STR21 AND STR25 TO STR29, LH/RH. I: 7400 FCOR37000 FHR 571146-02-8 191HB 191QB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33C192QB 192 PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OROR195 OF RIB 1 BUTT STRAP EDGE AT STR16, STR20, STR21 AND 50000 FHGROUP 33D196 STR25 TO STR29, LH/RH. I: 8650 FCOR25900 FH571148-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33A192 PANEL, KEEL BEAM FITTING 4 FIRST BORE HOLES AFT FRAME ORPOST 4357740 DATUM, LH/RH. 50000 FHORI: 8000 FCGROUP 33BORPOST 4357723200 FH571149-01-5 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33A192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 ORPOST 41652DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FHPRE 44360I: 6100 FCORORGROUP 33A17600 FHPOST 45968ORGROUP 33BPOST 41652PRE 44360ORGROUP 33BPOST 45968ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 18APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571149-01-6 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 32A192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 ORPOST 45968DATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FHORI: 6500 FCGROUP 33COR19000 FH571149-01-7 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 20000 FCGROUP 33D192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 ORDATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FHI: 6400 FCOR18700 FH571149-01-8 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 33E192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 ORDATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FHI: 6400 FCOR19100 FH571149-01-9 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER T: 17000 FCGROUP 32E192 PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FRAME 40 ORDATUM TO STRINGER 1 LEVEL, LH/RH. 50000 FHI: 5900 FCOR29500 FH571152-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 19APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571152-01-3 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 33A744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, ORPOST 41652RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 50000 FHORFASTENERS 3 TO 12, LH/RH. I: 8000 FCGROUP 33BORPOST 4165228000 FHORGROUP 32AORGROUP 33CORGROUP 33D571152-01-4 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, ORRADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE 50000 FHAT FASTENERS 3 TO 12, LH/RH. I: 8000 FCOR24000 FH571152-01-5 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E744 142 INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, ORRADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT 50000 FHFASTENERS 3 TO 12, LH/RH. I: 8000 FCOR40000 FH571153-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF ORSEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 50000 FHWITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 15200 FCRADIUS ON EACH SIDE OF GUSSET, LH/RH OR45600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 20APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571153-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E744 142 INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF ORSEALANT REMOVAL GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA 50000 FHWITH KEEL BEAM FITTING AT FR 40, AND LOWER L FITTING I: 12900 FCRADIUS ON EACH SIDE OF GUSSET, LH/RH. OR64600 FHR 571154-01-1 147AZ 148AZ 734 141 GENERAL VISUAL INSPECTION OF CENTER WING BOX INTERNAL T: 12 YE NO CPCP ZL-141-01-1 ALL744 142 STRUCTURE EXCLUDING STRUTS I: 12 YE571157-01-1 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 20000 FCGROUP 32A744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, ORPOST 49202SEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN CONNECTION 50000 FHOROF KEEL BEAM FITTING TO PANEL, LH/RH I: 20000 FCGROUP 33CORPOST 4920250000 FHORGROUP 33DPOST 49202571157-01-2 147AZ 148AZ 734 141 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 32E744 142 INTERNAL STRUCTURE, LOWER PANEL AT KEEL BEAM LEVEL, ORORSEALANT REMOVAL FIRST FASTENER HOLE AFT OF FR 40 DATUM IN 50000 FHGROUP 33ECONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH I: 17000 FCOR50000 FH571158-01-1 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 20000 FCGROUP 32A192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN ORPOST 49202CONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FHORI: 5310 FCGROUP 33CORPOST 4920215900 FHORGROUP 33DPOST 49202ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 21APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS571158-01-2 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 17000 FCGROUP 33E192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN ORCONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FHI: 5310 FCOR15900 FH571158-01-3 191HB 192HB 191 SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING AT T: 17000 FCGROUP 32E192 FR 40, FIRST FASTENER HOLE AFT OF FR 40 DATUM IN ORCONNECTION OF KEEL BEAM FITTING TO PANEL, LH/RH 50000 FHI: 4900 FCOR24500 FHR 571159-01-3 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FCGROUP 33A146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FHGROUP 33BI: 8350 FCOR25000 FHR 571159-01-4 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FCGROUP 32A146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FHI: 8850 FCOR44400 FHR 571159-01-5 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 20000 FCGROUP 33C146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FHGROUP 33DI: 9450 FCOR28300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 22APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 571159-01-6 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX T: 17000 FCGROUP 33E146 PORTAL BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FHI: 9700 FCOR29000 FHR 571159-01-7 CABIN FLOOR PANELS 145 SPECIAL DETAILED INSPECTION OF CENTER WING BOX PORTAL T: 17000 FCGROUP 32E146 BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL ORSTIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS) 50000 FHI: 8900 FCOR44600 FH571160-01-1 147AZ 148AZ 141 DETAILED INSPECTION OF CENTER WING BOX, STRUTS (54 T: 12 YEALL142 PLACES) I: 12 YE571165-01-3 N/A TASK DELETEDR 572001-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPRE 4843712 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 5100 FCOR23400 FH572001-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OROR12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHGROUP 33BREINFORCING I: 7000 FCOR21900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 23APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572001-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPRE 4843712 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 5600 FCOR16700 FHR 572001-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPRE 4843712 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 5400 FCOR15900 FH572001-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 8900 FCOR25400 FH572001-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND OR12 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 7500 FCOR34000 FH572001-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPOST 4843712 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 9400 FCOR26300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 24APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572001-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPOST 4843712 EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON 50000 FHREINFORCING I: 7500 FCOR34000 FH572002-01-10 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR464ML 464MR 462 50000 FH464 I: 9800 FCOR44400 FH572002-01-11 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPRE 48437464ML 464MR 462 50000 FH464 I: 7800 FCOR24400 FH572002-01-12 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPOST 48437464ML 464MR 462 50000 FH464 I: 12300 FCOR34300 FH572002-01-13 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPOST 48437464ML 464MR 462 50000 FH464 I: 8400 FCOR33700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 25APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572002-01-4 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPRE 48437464ML 464MR 462 50000 FH464 I: 8400 FCOR33700 FH572002-01-5 454DL 454DR 454FL 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A454FR 464DL 464DR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPOST 43142464FL 464FR 462 50000 FHPRE 43271464 I: 8300 FCORORGROUP 33B26000 FHPRE 43271572002-01-6 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR464ML 464MR 462 50000 FH464 I: 8400 FCOR26300 FHR 572002-01-8 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A ORPOST 43142464ML 464MR 462 50000 FHPOST 43271464 NOTE 8ORI: 8300 FCGROUP 33BORPOST 4327126000 FH572002-01-9 454KL 454KR 454ML 452 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E454MR 464KL 464KR 454 MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A OR464ML 464MR 462 50000 FH464 I: 11600 FCOR33100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 26APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572003-01-10 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE ORPOST 48437464CL 464CR 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FHR 572003-01-4 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454NR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE ORPRE 48437464CL 464NR 50000 FHI: 6200 FCOR28100 FHR 572003-01-5 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OROR464CL 464CR 50000 FHGROUP 33BI: 7000 FCOR21900 FHR 572003-01-6 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE ORPRE 48437464CL 464CR 50000 FHI: 6700 FCOR20000 FHR 572003-01-7 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE ORPRE 48437464CL 464CR 50000 FHI: 6400 FCOR19100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 27APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572003-01-9 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E454CR 464BL 464BR 464 SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE OROR464CL 464CR 50000 FHGROUP 33EI: 17000 FCOR50000 FHR 572003-02-2 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-454-06-1 A330-200454CR 464BL 464BR 464 LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING I: 12 YEPRE 43271464CL 464CR PLATEORA330-300PRE 43271R 572003-02-3 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-454-06-2 A330-200454NR 464BL 464BR 464 LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING I: 12 YEPOST 43271464CL 464NR PLATEORA330-200FPOST 43271ORA330-300POST 43271572004-02-1 N/A TASK DELETEDR 572004-02-3 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORORRIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FHGROUP 33BREINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 8100 FCFAIRING OR24000 FH572004-02-4 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 28APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572004-02-6 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORRIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FHREINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 6800 FCFAIRING OR19500 FH572004-02-7 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORRIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FHREINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 5800 FCFAIRING OR26200 FH572004-02-8 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORPOST 48437RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FHREINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 7300 FCFAIRING OR20200 FH572004-02-9 FUEL PUMP FAIRINGS 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A641 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORPOST 48437RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR 50000 FHREINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON I: 5800 FCFAIRING OR26200 FH572005-01-10 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORGEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 8000 FCOR22700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 29APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572005-01-11 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORGEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 6700 FCOR30400 FH572005-01-12 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPRE 48437GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 4900 FCOR15300 FH572005-01-13 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPOST 48437GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 8400 FCOR23500 FH572005-01-14 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPOST 48437GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 6700 FCOR30400 FH572005-01-6 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORGEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 6700 FCOR21000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 30APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572005-01-7 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPRE 48437GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHSPAR. I: 6800 FCOR27300 FHR 572005-01-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641CB 641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPRE 41114GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHORSPAR. I: 9700 FCGROUP 33BORPRE 4111428700 FHR 572005-01-9 541CB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641 FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING ORPOST 41114GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR 50000 FHORSPAR. I: 9700 FCGROUP 33BORPOST 4111428700 FH572006-01-1 N/A TASK DELETED572006-01-2 N/A TASK DELETED572006-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 6 YE NO CPCP ZL-500-01-1 ALL600 MAIN LANDING GEAR REINFORCING PLATE I: 6 YE572006-02-2 N/A TASK DELETED572006-02-3 N/A TASK DELETED572006-02-4 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 31APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572006-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 17000 FCZL-500-01-1 GROUP 33E600 MAIN LANDING GEAR REINFORCING PLATE OR50000 FHI: 14100 FCOR40000 FH572006-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 17000 FCZL-500-01-1 GROUP 32E600 MAIN LANDING GEAR REINFORCING PLATE OR50000 FHI: 11900 FCOR50000 FH572006-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 20000 FCZL-500-01-1 GROUP 33D600 MAIN LANDING GEAR REINFORCING PLATE ORPOST 4843750000 FHI: 14900 FCOR41500 FH572006-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING LOWER SURFACE T: 20000 FCZL-500-01-1 GROUP 32A600 MAIN LANDING GEAR REINFORCING PLATE ORPOST 4843750000 FHI: 11900 FCOR53600 FH572007-01-1 N/A TASK DELETED572007-01-10 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH631 I: 9400 FCOR42700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 32APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572007-01-11 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY ORPOST 48437531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH631 I: 11800 FCOR33000 FH572007-01-12 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY ORPOST 48437531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH631 I: 9400 FCOR42700 FH572007-01-4 N/A TASK DELETEDR 572007-01-5 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OROR531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FHGROUP 33B631 I: 13800 FCOR40800 FH572007-01-6 N/A TASK DELETED572007-01-7 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 12 YE T: 20 YE CPCP ALL464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY I: 12 YE I: 12 YE531 FLAP TRACK 2 FAIRING AND PYLON FAIRING.631ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 33APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572007-01-9 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E464GR 531AB 631AB 464 SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY OR531 FLAP TRACK 2 FAIRING AND PYLON FAIRING. 50000 FH631 I: 11200 FCOR31900 FH572008-01-10 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORPOST 48437TRACK 2 FAIRING. 50000 FHI: 6900 FCOR31300 FH572008-01-3 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORPRE 48437TRACK 2 FAIRING. 50000 FHI: 7100 FCOR28500 FHR 572008-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORORTRACK 2 FAIRING. 50000 FHGROUP 33BI: 6900 FCOR20500 FH572008-01-5 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORTRACK 2 FAIRING. 50000 FHI: 7000 FCOR21900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 34APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572008-01-6 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORTRACK 2 FAIRING. 50000 FHI: 8200 FCOR23400 FH572008-01-7 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORTRACK 2 FAIRING. 50000 FHI: 6900 FCOR31300 FH572008-01-8 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORPRE 48437TRACK 2 FAIRING. 50000 FHI: 6500 FCOR20300 FH572008-01-9 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D631 SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP ORPOST 48437TRACK 2 FAIRING. 50000 FHI: 8700 FCOR24200 FH572008-02-1 531AB 631AB 531 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-531-02-1 ALL631 LOWER SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY I: 12 YEFLAP TRACK 2 FAIRING.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 35APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572009-01-10 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORPOST 48437INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 8800 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) OR24600 FH572009-01-11 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORPOST 48437INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 7000 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 31800 FH572009-02-11572009-01-4 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORPRE 48437INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 5400 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 21700 FH572009-01-5 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORORINBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHGROUP 33BFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 4100 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5 12800 FH572009-01-6 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORINBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 5300 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6 16600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 36APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572009-01-7 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORINBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 8300 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-7 23700 FH572009-01-8 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORINBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 7000 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-8 31800 FH572009-01-9 454GL 454GR 464GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D464GR 531AB 631AB 464 SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), ORPRE 48437INBOARD FUEL PUMP 531 STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB 50000 FHFAIRING 631 BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY I: 4900 FC8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) ORNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-9 15300 FH572009-02-1 N/A TASK DELETED572009-02-2 N/A TASK DELETED572009-02-4 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORPRE 48437INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 12400 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR2-3) 49800 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 37APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572009-02-5 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORORINBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHGROUP 33BFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 7600 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR2-3) 23800 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5572009-02-6 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORINBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 12200 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR(2-3) 38200 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6572009-02-7 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORINBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 17000 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR(2-3) 50000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-7572009-02-8 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORINBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 17000 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR(2-3) 50000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-8ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 38APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572009-02-9 454GL 454GR 464GL 454 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D464GR 531AB 631AB 464 LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY ORPRE 48437INBOARD FUEL PUMP 531 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 50000 FHFAIRING 631 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB I: 11400 FCBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY OR(2-3) 35700 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-9572010-01-1 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO CPCP ALL541DB 541EB 541FB 641 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUT-OUTS I: 12 YE I: 12 YE641AB 641BB 641CB IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12.641DB 641EB 641FB572010-02-10 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPOST 48437641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 10000 FCOR27900 FH572010-02-11 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPOST 48437641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 8000 FCOR36000 FHR 572010-02-4 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 6400 FCOR29100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 39APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572010-02-5 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OROR641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FHGROUP 33B641DB 641EB 641FB 11-12. I: 8500 FCOR26600 FHR 572010-02-6 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 6900 FCOR20500 FHR 572010-02-7 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 6700 FCOR20000 FH572010-02-8 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 9400 FCOR26900 FH572010-02-9 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541DB 541EB 541FB 641 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR641AB 641BB 641CB CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 50000 FH641DB 641EB 641FB 11-12. I: 8000 FCOR36000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 40APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572011-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORPRE 48437AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 6100 FCOR24500 FH572011-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORORAND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHGROUP 33BI: 5700 FCOR17800 FH572011-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORAND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 6000 FCOR18800 FH572011-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORAND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 10100 FCOR28800 FH572011-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORAND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 8500 FCOR38600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 41APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572011-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORPRE 48437AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 5600 FCOR17500 FH572011-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORPOST 48437AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 10700 FCOR29800 FH572011-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 1 ORPOST 48437AND RIB 12, EXCLUDING AREA COVERED BY PYLON FAIRING. 50000 FHI: 8500 FCOR38600 FHR 572012-02-1 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORPRE 48437AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 4700 FCPLATE. OR21400 FHR 572012-02-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORORAND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHGROUP 33BAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 6300 FCPLATE. OR18800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 42APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572012-02-3 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORPRE 48437AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 5100 FCPLATE. OR15000 FHR 572012-02-4 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORPRE 48437AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 4800 FCPLATE. OR14300 FH572012-02-5 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORAND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 9000 FCPLATE. OR25500 FH572012-02-6 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORAND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 7600 FCPLATE. OR34200 FH572012-02-7 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORPOST 48437AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 9500 FCPLATE. OR26500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 43APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572012-02-8 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 ORPOST 48437AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING 50000 FHAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING I: 7600 FCPLATE. OR34200 FH572012-03-1 N/A TASK DELETED572012-03-2 FUEL PUMP FAIRINGS 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ALL600 LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB I: 6 YE10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING AND PYLON REINFORCINGPLATE.R 572013-03-1 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING ORPRE 48437454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6400 FC464BL 464BR 464CL OR464GL 464GR 464HL 29300 FH464HR 464KL 464KR464ML 464MR 464NRR 572013-03-2 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A454CR 454DL 454DR 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OROR454FL 454FR 454GL AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FHGROUP 33B454GR 454HL 454HR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6300 FC464BL 464BR 464CL OR464CR 464DL 464DR 18700 FH464FL 464FR 464GL464GR 464HL 464HRISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 44APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572013-03-3 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING ORPRE 48437454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7100 FC464BL 464BR 464CL OR464GL 464GR 464HL 21100 FH464HR 464KL 464KR464ML 464MR 464NRR 572013-03-4 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING ORPRE 48437454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 6600 FC464BL 464BR 464CL OR464GL 464GR 464HL 19600 FH464HR 464KL 464KR464ML 464MR 464NR572013-03-5 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 9000 FC464BL 464BR 464CL OR464GL 464GR 464HL 25500 FH464HR 464KL 464KR464ML 464MR 464NR572013-03-6 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING OR454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7600 FC464BL 464BR 464CL OR464GL 464GR 464HL 34200 FH464HR 464KL 464KR464ML 464MR 464NRISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 45APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572013-03-7 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING ORPOST 48437454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 9500 FC464BL 464BR 464CL OR464GL 464GR 464HL 26500 FH464HR 464KL 464KR464ML 464MR 464NR572013-03-8 454BL 454BR 454CL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454GL 454GR 454HL 464 SURFACE IN AREA COVERED BY PYLON FAIRING, EXCLUDING ORPOST 48437454HR 454KL 454KR AREA COVERED BY PYLON REINFORCING PLATE AND AFT 50000 FH454ML 454MR 454NR ATTACHMENT FITTING SKIN REINFORCING PLATE. I: 7600 FC464BL 464BR 464CL OR464GL 464GR 464HL 34200 FH464HR 464KL 464KR464ML 464MR 464NRR 572013-04-1 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-454-06-1 A330-200454CR 454DL 454DR 464 LOWER SURFACE IN AREA COVERED BY PYLON FAIRING, I: 12 YEPRE 43271454FL 454FR 454GL EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE ANDOR454GR 454HL 454HR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.A330-300464BL 464BR 464CLPRE 43271464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HRR 572013-04-2 454BL 454BR 454CL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE CPCP ZL-454-06-2 A330-200454GL 454GR 454HL 464 LOWER SURFACE IN AREA COVERED BY PYLON FAIRING, I: 12 YEPOST 43271454HR 454KL 454KR EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE ANDOR454ML 454MR 454NR AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.A330-200F464BL 464BR 464CLPOST 43271464FR 464GL 464HLOR464HR 464KL 464KRA330-300464ML 464MR 464NRPOST 43271ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 46APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572014-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORPRE 48437STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 6600 FCOR26500 FHR 572014-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORORSTRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHGROUP 33BCOVERED BY FAIRINGS. I: 7900 FCOR23300 FH572014-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 6600 FCOR20700 FH572014-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 8400 FCOR23900 FH572014-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 7100 FCOR32000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 47APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572014-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORPRE 48437STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 6100 FCOR19100 FH572014-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORPOST 48437STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS 50000 FHCOVERED BY FAIRINGS. I: 8900 FCOR24800 FH572014-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE SPANWISE SKIN JOINTS AT SRINGER 13 AND ORPOST 48437STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING 50000 FHAREAS COVERED BY FAIRINGS. I: 7100 FCOR32000 FH572015-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO CPCP ALL600 SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR I: 6 YEAND 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 FCGROUP 32A600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORPRE 48437SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 6800 FCOR31200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 48APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572015-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHGROUP 33BI: 6600 FCOR19600 FHR 572015-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORPRE 48437SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 8100 FCOR23900 FHR 572015-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORPRE 48437SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 6900 FCOR20500 FH572015-02-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 8500 FCOR24300 FH572015-02-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORSPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 7200 FCOR32600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 49APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572015-02-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORPOST 48437SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 9000 FCOR25200 FH572015-02-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT ORPOST 48437SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12. 50000 FHI: 7200 FCOR32600 FH572016-01-1 N/A TASK DELETED572016-01-2 FUEL PUMP FAIRINGS 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN VISIBLE T: 6 YE NO CPCP ALL600 SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB I: 6 YE4.572016-02-10 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORPOST 48437AND RIB 4. 50000 FHI: 9500 FCOR26400 FH572016-02-11 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORPOST 48437AND RIB 4. 50000 FHI: 7600 FCOR34200 FH572016-02-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 50APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572016-02-4 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORPRE 48437AND RIB 4. 50000 FHI: 3100 FCOR14200 FHR 572016-02-5 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORORAND RIB 4. 50000 FHGROUP 33BI: 4600 FCOR13600 FHR 572016-02-6 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORPRE 48437AND RIB 4. 50000 FHI: 3500 FCOR10400 FHD 572016-02-7 N/A TASK DELETED572016-02-8 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORAND RIB 4. 50000 FHI: 9000 FCOR25500 FH572016-02-9 FUEL PUMP FAIRINGS 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E600 VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 ORAND RIB 4. 50000 FHI: 7600 FCOR34200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 51APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572017-01-10 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FCGROUP 33D641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 ORPOST 4843750000 FHI: 19700 FCOR50000 FHR 572017-01-11 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641 ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 ORPOST 4843750000 FHI: 15700 FCOR50000 FH572017-01-4 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FCGROUP 32A641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. ORPRE 4843750000 FHI: 7000 FCOR28100 FH572017-01-5 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FCGROUP 33A641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. ORPOST 4328350000 FHORI: 7900 FCGROUP 33BORPOST 4328324700 FH572017-01-6 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FCGROUP 33C641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. OR50000 FHI: 6800 FCOR21300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 52APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572017-01-7 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 17000 FCGROUP 32E641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR50000 FHI: 15700 FCOR50000 FH572017-01-8 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 17000 FCGROUP 33E641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 OR50000 FHI: 17000 FCOR50000 FH572017-01-9 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ROOT T: 20000 FCGROUP 33D641 JOINT FITTINGS ON STRINGER 13 AND STRINGER 20 ORPRE 4843750000 FHI: 6300 FCOR19700 FH572017-02-2 541AB 641AB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-01-1 ALL641 ROOT JOINT FITTINGS ON STRINGER 13 AND STRINGER 20. I: 12 YE572018-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING ORPOST 48437541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH541FZ 641AB 641AZ & 20. I: 9200 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 41600 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 53APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572018-01-11 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING ORPRE 48437541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH541FZ 641AB 641AZ & 20 I: 7300 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 21600 FH641EZ 641FZN 572018-01-12 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING ORPRE 48437541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH541FZ 641AB 641AZ 20 I: 7700 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 22700 FH641EZ 641FZR 572018-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING ORPRE 48437541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH541FZ 641AB 641AZ 20. I: 7100 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 32300 FH641EZ 641FZR 572018-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OROR541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FHGROUP 33B541FZ 641AB 641AZ 20. I: 7300 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 21700 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 54APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572018-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING ORPOST 48437541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FHOR541FZ 641AB 641AZ 20. I: 10900 FCGROUP 33D641BB 641BZ 641CB ORPOST 48437641CZ 641DB 641DZ 31000 FH641EZ 641FZ572018-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH541FZ 641AB 641AZ 20. I: 10900 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 31000 FH641EZ 641FZ572018-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING OR541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH541FZ 641AB 641AZ & 20. I: 9300 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 41600 FH641EZ 641FZ572018-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541BZ 541CB 541CZ 641 STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING I: 12 YE541DB 541DZ 541EZ STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &541FZ 641AB 641AZ 20.641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 55APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572019-01-10 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORPOST 48437STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH& 20. I: 6900 FCOR31100 FHR 572019-01-11 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORPRE 48437STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH& 20. I: 5600 FCOR16600 FHN 572019-01-12 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORPRE 48437STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 20 50000 FHI: 5900 FCOR17500 FHR 572019-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORPRE 48437STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH20. I: 5400 FCOR24900 FHR 572019-01-6 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORORSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FHGROUP 33B20. I: 7300 FCOR21700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 56APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572019-01-7 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORPOST 48437STRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FHOR20. I: 8100 FCGROUP 33DORPOST 4843723200 FH572019-01-8 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 & 50000 FH20. I: 8200 FCOR23200 FH572019-01-9 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING ORSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH& 20. I: 6900 FCOR31100 FH572019-02-2 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641EB 641FB 641GB 641 STRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDING I: 12 YESTRINGERS 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 CPCP ALL641AB 641AZ 641BZ 641 UPPER SURFACE INCLUDING STRINGERS AND BUTTSTRAPS I: 6 YEBETWEEN RIB 1 AND RIB 3.572021-03-1 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPRE 48437464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 7600 FCOR30500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 57APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572021-03-2 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OROR464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FHGROUP 33B631AB 631 FLAP TRACK 2 FAIRING. I: 10200 FCOR30300 FH572021-03-3 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 7600 FCOR23800 FH572021-03-4 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 10800 FCOR30800 FH572021-03-5 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING 50000 FH631AB 631 AND FLAP TRACK 2 FAIRING. I: 9100 FCOR41200 FH572021-03-6 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D454GR 464FL 464FR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPRE 48437464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 7100 FCOR22200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 58APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572021-03-7 454FL 454FR 454GL 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D454GR 464FL 464FR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPOST 48437464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 11400 FCOR31900 FH572021-03-8 454GL 454GR 454ML 454 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A454MR 464GL 464GR 464 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPOST 48437464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING AND 50000 FH631AB 631 FLAP TRACK 2 FAIRING. I: 9100 FCOR41200 FHR 572021-04-1 454FL 454FR 454GL 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-454-06-1 A330-200454GR 464FL 464FR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND I: 12 YEZL-531-02-1 PRE 43271464GL 464GR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING ANDOR631AB 631 FLAP TRACK 2 FAIRING.A330-300PRE 43271R 572021-04-2 454GL 454GR 454ML 454 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-454-06-2 A330-200454MR 464GL 464GR 464 LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND I: 12 YEZL-531-02-1 POST 43271464ML 464MR 531AB 531 STRINGER 20 IN AREAS COVERED BY PYLON FAIRING ANDOR631AB 631 FLAP TRACK 2 FAIRING.A330-200FPOST 43271ORA330-300POST 43271D 572022-01-4 N/A TASK DELETEDD 572022-01-5 N/A TASK DELETEDD 572022-01-6 N/A TASK DELETEDD 572022-01-7 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 59APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSD 572022-01-8 N/A TASK DELETEDD 572022-01-9 N/A TASK DELETED572023-01-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ALL600 AT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM I: 6 YEFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BYPYLON FAIRING AND REINFORCING PLATE, MAIN LANDINGGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.572023-01-2 N/A TASK DELETED572023-02-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 32A600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORPOST 48437FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 6900 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR31300 FHR 572023-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 32A600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORPRE 48437FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3600 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR16500 FHR 572023-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 33A600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHGROUP 33BPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 4000 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR12000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 60APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572023-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 33C600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORPRE 48437FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3900 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING. OR11600 FHR 572023-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 33D600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORPRE 48437FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 3700 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR11000 FH572023-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 17000 FCGROUP 33E600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 8200 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR23400 FH572023-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 17000 FCGROUP 32E600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 6900 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR31300 FH572023-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT T: 20000 FCGROUP 33D600 STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROM ORPOST 48437FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY 50000 FHPYLON FAIRING AND REINFORCING PLATE, MAIN LANDING I: 8700 FCGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING OR24200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 61APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572025-01-3 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641AB 641BB 641CB 641 STRINGER JOINTS AT STRINGER 11 BETWEEN RIBS 3 AND 4 ORPRE 44245AND STRINGERS 12 AND 14 BETWEEN RIBS 5 AND 6. 50000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7000 FCGROUP 33BTASK 572025-02-3 ORPRE 4424521900 FH572025-02-3 541AB 541BB 541CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641AB 641BB 641CB 641 STRINGER JOINTS AT STRINGER 11 BETWEEN RIBS 3 AND 4 ORPRE 44245NUT REMOVAL AS PER AND STRINGERS 12 AND 14 BETWEEN RIBS 5 AND 6. 50000 FHORNTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 7000 FCGROUP 33BTASK 572025-01-3 ORPRE 4424521900 FH572026-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. ORPOST 48437541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 10100 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 28200 FH641EZ 641FZ572026-01-11 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND R ORPOST 48437541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 8100 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 36500 FH641EZ 641FZ572026-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. ORPRE 48437541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 9000 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 36200 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 62APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572026-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OROR541DB 541DZ 541EZ 50000 FHGROUP 33B541FZ 641AB 641AZ I: 7000 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 21900 FH641EZ 641FZ572026-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 9000 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 28200 FH641EZ 641FZ572026-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 9600 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 27200 FH641EZ 641FZ572026-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. OR541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 8100 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 36500 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 63APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572026-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. ORPRE 48437541DB 541DZ 541EZ 50000 FH541FZ 641AB 641AZ I: 8400 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 26300 FH641EZ 641FZ572026-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541BZ 541CB 541CZ 641 STRINGER 18 BETWEEN RIB 1 AND RIB 9. I: 12 YE541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZR 572027-01-10 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 ORPRE 48437541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 6500 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 19200 FH641EZ 641FZ572027-01-11 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 ORPOST 48437541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 14300 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 39700 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 64APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572027-01-12 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 ORPOST 48437541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 11400 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 50000 FH641EZ 641FZR 572027-01-5 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 ORPRE 48437541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 6200 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 28300 FH641EZ 641FZR 572027-01-6 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OROR541DB 541DZ 541EZ AND RIB 9. 50000 FHGROUP 33B541FZ 641AB 641AZ I: 8600 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 25600 FH641EZ 641FZ572027-01-7 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 7400 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 23200 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 65APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572027-01-8 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 13500 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 38300 FH641EZ 641FZ572027-01-9 541AB 541AZ 541BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 OR541DB 541DZ 541EZ AND RIB 9. 50000 FH541FZ 641AB 641AZ I: 11400 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 50000 FH641EZ 641FZ572027-02-1 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541BZ 541CB 541CZ 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 I: 12 YE541DB 541DZ 541EZ AND RIB 9.541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572028-01-3 541CB 541DB 641CB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8. ORPRE 44245NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHORTASK 572028-02-3 I: 7000 FCGROUP 33BORPRE 4424521900 FH572028-02-3 541CB 541DB 641CB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641DB 641 STRINGER 18 JOINT BETWEEN RIB 7 AND RIB 8. ORPRE 44245NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHORNTM TASK 572028-01-3 I: 7000 FCGROUP 33BORPRE 4424521900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 66APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572029-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPOST 48437RIB 12 50000 FHI: 9100 FCOR40000 FH572029-01-3 N/A TASK DELETED572029-01-4 N/A TASK DELETED572029-01-5 N/A TASK DELETED572029-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 ORAND RIB 12. 50000 FHI: 11000 FCOR31200 FH572029-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FCGROUP 32E600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OR1 AND RIB 12 50000 FHI: 9100 FCOR40000 FH572029-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND ORPOST 48437RIB 12 50000 FHI: 11800 FCOR32500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 67APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572030-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND ORPOST 48437RIB 11 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FHD 572030-01-4 N/A TASK DELETED572030-01-5 N/A TASK DELETED572030-01-6 N/A TASK DELETED572030-01-7 N/A TASK DELETED572030-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9 AND ORORRIB 11 50000 FHGROUP 33EI: 17000 FCOR50000 FHD 572032-01-11 N/A TASK DELETEDR 572032-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORPRE 48437RIB 7. 50000 FHI: 11800 FCOR53700 FH572032-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 68APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572032-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORPRE 48437RIB 7. 50000 FHI: 9500 FCOR28200 FHR 572032-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORPOST 48437RIB 7. 50000 FHORI: 10000 FCGROUP 33DORPOST 4843728500 FH572032-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORRIB 7. 50000 FHI: 10000 FCOR28500 FH572032-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND ORRIB 7 50000 FHI: 8300 FCOR36600 FH572033-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORPOST 48437REAR SPAR. 50000 FHI: 12200 FCOR33400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 69APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572033-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORPOST 48437REAR SPAR. 50000 FHI: 9300 FCOR41100 FHR 572033-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORPRE 48437REAR SPAR. 50000 FHI: 6600 FCOR30100 FHR 572033-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORORREAR SPAR. 50000 FHGROUP 33BI: 8600 FCOR25500 FHR 572033-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORPRE 48437REAR SPAR. 50000 FHI: 6600 FCOR19700 FHR 572033-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORPRE 48437REAR SPAR. 50000 FHI: 6000 FCOR17800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 70APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572033-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORREAR SPAR. 50000 FHI: 11300 FCOR32000 FH572033-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO ORREAR SPAR. 50000 FHI: 9300 FCOR41100 FH572033-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 ALL600 UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT I: 6 YESPAR TO REAR SPAR.572034-01-4 N/A TASK DELETED572034-01-5 N/A TASK DELETED572034-01-6 N/A TASK DELETED572034-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEEN ORORRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 50000 FHGROUP 33EBETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 I: 17000 FCAND 13 OR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 71APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572034-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEEN ORPOST 48437RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 50000 FHORBETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11 I: 20000 FCGROUP 33DAND 13. ORPOST 4843750000 FH572035-01-4 N/A TASK DELETED572035-01-5 N/A TASK DELETED572035-01-6 N/A TASK DELETED572035-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO ORORRIB 8. 50000 FHGROUP 33EI: 17000 FCOR50000 FH572035-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 ORPOST 48437TO RIB 8. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH572036-01-10 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 32A641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT ORPOST 48437TO REAR SPARS. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FHD 572036-01-4 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 72APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572036-01-5 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FCGROUP 33A641AB 641AZ 641BZ 641 CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR ORORSPARS. 50000 FHGROUP 33BI: 12700 FCOR37700 FH572036-01-6 N/A TASK DELETED572036-01-8 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FCGROUP 32E641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO ORREAR SPARS. 50000 FHI: 15900 FCOR50000 FH572036-01-9 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FCGROUP 33E641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT ORTO REAR SPARS. 50000 FHI: 17000 FCOR50000 FH572036-02-2 541AB 541AZ 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641AB 641AZ 641BZ 641 STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO I: 12 YEREAR SPARS.572037-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO ORPRE 48437541DB 541DZ 541EZ REAR SPAR. 50000 FH541FZ 641AB 641AZ I: 12800 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 46200 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 73APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572037-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FCGROUP 33A541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO OROR541DB 541DZ 541EZ REAR SPAR. 50000 FHGROUP 33B541FZ 641AB 641AZ I: 11900 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 37900 FH641EZ 641FZ572037-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER T: 20000 FCGROUP 33C541BZ 541CB 541CZ 641 ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM FRONT SPAR TO OR541DB 541DZ 541EZ REAR SPAR. 50000 FH541FZ 641AB 641AZ I: 12400 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 39500 FH641EZ 641FZ572037-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FCGROUP 32E541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM OROR541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FHGROUP 33E541FZ 641AB 641AZ I: 17000 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 50000 FH641EZ 641FZ572037-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 33D541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM ORPRE 48437541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FH541FZ 641AB 641AZ I: 12200 FC641BB 641BZ 641CB OR641CZ 641DB 641DZ 38800 FH641EZ 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 74APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572037-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 32A541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM ORPOST 48437541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR. 50000 FHOR541FZ 641AB 641AZ I: 20000 FCGROUP 33D641BB 641BZ 641CB ORPOST 48437641CZ 641DB 641DZ 50000 FH641EZ 641FZ572037-02-2 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541BZ 541CB 541CZ 641 STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 FROM I: 12 YE541DB 541DZ 541EZ FRONT SPAR TO REAR SPAR.541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572038-02-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641FB 641 LOWER SURFACE, PYLON REINFORCING PLATE . I: 12 YE572039-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORPOST 48437AND FROM RIB 11 TO 12. 50000 FHI: 10800 FCOR29700 FH572039-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORPOST 48437AND FROM RIB 11 TO 12. 50000 FHI: 8300 FCOR36600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 75APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572039-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORPRE 48437AND FROM RIB 11 TO 12. 50000 FHI: 14600 FCOR66500 FHR 572039-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORORAND FROM RIB 11 TO 12. 50000 FHGROUP 33BI: 16400 FCOR48900 FHR 572039-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORPRE 48437AND FROM RIB 11 TO 12. 50000 FHI: 16300 FCOR48500 FHR 572039-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORPRE 48437AND FROM RIB 11 TO 12. 50000 FHI: 14800 FCOR44000 FH572039-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORAND FROM RIB 11 TO 12. 50000 FHI: 10000 FCOR28500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 76APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572039-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9 ORAND FROM RIB 11 TO 12. 50000 FHI: 8300 FCOR36600 FHR 572040-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND ORPRE 48437RIB 13. 91100 FHI: 13500 FCOR61500 FHR 572040-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND ORORRIB 13. 50000 FHGROUP 33BI: 11000 FCOR32900 FHR 572040-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND ORPRE 48437RIB 13. 50000 FHI: 16100 FCOR47800 FHR 572040-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND ORPRE 48437RIB 13. 50000 FHI: 15100 FCOR44900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 77APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572040-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 AND ORORRIB 13. 50000 FHGROUP 33EI: 17000 FCOR50000 FH572040-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 ORPOST 48437AND RIB 13. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH572041-01-1 573DB 573FB 673DB 571 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE CPCP ZL-571-01-1 ALL673FB 573 FACE BETWEEN RIB 1 AND RIB 12. I: 12 YEZL-573-01-1FLAPS EXTENDED 671673572043-01-10 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 20000 FCGROUP 33D673 FACE SPAR JOINT PLATE AT RIB 9. ORPOST 4843750000 FHI: 10900 FCOR30400 FHR 572043-01-11 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 20000 FCGROUP 32A673 FACE SPAR JOINT PLATE AT RIB 9. ORPOST 4843750000 FHI: 8600 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 78APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572043-01-4 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 32A673 SPAR JOINT PLATE AT RIB 9. ORPRE 4843750000 FHI: 10300 FCOR47600 FHR 572043-01-5 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33A673 SPAR JOINT PLATE AT RIB 9. OROR50000 FHGROUP 33BI: 5800 FCOR18500 FHR 572043-01-6 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33C673 SPAR JOINT PLATE AT RIB 9. ORPRE 4843750000 FHI: 11100 FCOR35600 FHR 572043-01-7 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33D673 SPAR JOINT PLATE AT RIB 9. ORPRE 4843750000 FHI: 9400 FCOR30000 FH572043-01-8 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FCGROUP 33E673 SPAR JOINT PLATE AT RIB 9. OR50000 FHI: 10000 FCOR31500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 79APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572043-01-9 573FB 673FB 573 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT T: 17000 FCGROUP 32E673 FACE SPAR JOINT PLATE AT RIB 9. OR50000 FHI: 8600 FCOR50000 FH572043-02-2 573FB 673FB 573 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR AFT T: 12 YE CPCP ZL-573-01-1 ALL673 FACE SPAR JOINT PLATE AT RIB 9. I: 12 YE572045-01-1 541AB 541AZ 541BZ 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP ALL641AB 641AZ 641BZ 641 FACE UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YER 572046-01-4 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 32A541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND ORPRE 48437641AB 641BB 641CB BOTTOM FLANGE. 50000 FH641DB 641EB 641FB I: 5400 FCOR24900 FH572046-01-5 N/A TASK DELETED572046-01-6 N/A TASK DELETED572046-01-7 N/A TASK DELETEDR 572046-01-8 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FCGROUP 33E541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND OR641AB 641BB 641CB BOTTOM FLANGE. 50000 FH641DB 641EB 641FB I: 8000 FCOR25100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 80APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572046-01-9 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FCGROUP 32E541DB 541EB 541FB 641 FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND OR641AB 641BB 641CB BOTTOM FLANGE. 50000 FH641DB 641EB 641FB I: 6900 FCOR40600 FH572046-02-2 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-02-1 ALL541DB 541EB 541FB 641 FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP I: 12 YE641AB 641BB 641CB AND BOTTOM FLANGE.641DB 641EB 641FB572047-01-11 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD ORPOST 48437641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 50000 FH641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7 I: 13100 FCSEALANT REMOVAL AS ORPER NTM 36400 FH572047-01-3 N/A TASK DELETEDD 572047-01-4 N/A TASK DELETED572047-01-5 N/A TASK DELETED572047-01-6 N/A TASK DELETEDR 572047-01-7 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 33E541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 50000 FH641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7. I: 12000 FCSEALANT REMOVAL AS ORPER NTM 37300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 81APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572047-01-8 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32E541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD OR641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 100500 FH641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7. I: 10300 FCSEALANT REMOVAL AS ORPER NTM 60900 FHR 572047-01-9 541AB 541BB 541BZ 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32A541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD ORPOST 48437641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY 118200 FH641CZ FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7 I: 10300 FCSEALANT REMOVAL AS ORPER NTM 60900 FH572047-02-2 541AB 541BB 541BZ 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-02-1 ALL541CB 541CZ 641AB 641 FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD I: 12 YE641BB 641BZ 641CB PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY641CZ 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 FCGROUP 32A641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9. ORPRE 4843750000 FHI: 10300 FCOR47600 FHN 572048-01-2 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33A641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 OROR50000 FHGROUP 33BI: 5800 FCOR18500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 82APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572048-01-3 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33C641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 ORPRE 4843750000 FHI: 11100 FCOR35600 FHN 572048-01-4 541DB 541EB 641DB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D641EB 641 FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9 ORPRE 4843750000 FHI: 9400 FCOR30000 FH572049-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. ORPOST 4843750000 FHI: 13600 FCOR38000 FH572049-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32A600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. ORPOST 4843750000 FHI: 10800 FCOR50000 FHR 572049-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32A600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. ORPRE 4843792100 FHI: 15500 FCOR71400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 83APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572049-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33A600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OROR50000 FHGROUP 33BI: 8700 FCOR27800 FHR 572049-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33C600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. ORPRE 4843763900 FHI: 16700 FCOR53400 FHR 572049-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. ORPRE 4843750000 FHI: 14100 FCOR45000 FH572049-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 33E600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR50000 FHI: 12500 FCOR39300 FH572049-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32E600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. OR50000 FHI: 10800 FCOR50000 FH572050-01-4 N/A TASK DELETED572050-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 84APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572050-01-6 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33BFLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ORPRE 48437671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FH673 I: 7200 FCOR23200 FH572050-01-7 N/A TASK DELETED572050-01-8 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FCGROUP 32EFLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER OROR671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FHGROUP 33E673 I: 17000 FCOR50000 FH572050-01-9 573DB 673DB 571 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 32AFLAPS EXTENDED 573 UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ORPOST 48437671 ATTACHMENT ANGLE FROM RIB 1 TO RIB 7. 50000 FHOR673 I: 20000 FCGROUP 33DORPOST 4843750000 FH572051-01-10 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32ESEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. ORORPER NTM 50000 FHGROUP 33EI: 17000 FCOR50000 FH572051-01-11 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32ASEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. ORPOST 48437PER NTM 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH572051-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 85APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572051-01-6 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33ASEALANT REMOVAL AS 671 AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. ORPOST 46241PER NTM 50000 FHORI: 5200 FCGROUP 33BORPOST 4624116600 FH572051-01-7 N/A TASK DELETED572051-01-8 N/A TASK DELETED572052-01-4 N/A TASK DELETED572052-01-5 N/A TASK DELETED572052-01-6 N/A TASK DELETED572052-01-7 N/A TASK DELETED572052-01-8 N/A TASK DELETED572052-02-2 541BB 541CB 641BB 541 GENERAL VISUAL INSPECTION OF OUTER WING REAR SPAR T: 12 YE NO CPCP ZL-541-01-1 ALL641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP I: 12 YEAND BOTTOM FLANGE.572052-03-1 N/A TASK DELETED572052-03-2 N/A TASK DELETED572052-03-3 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 86APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572052-03-4 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33B641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP ORPOST 43503SEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FHPER NTM I: 7700 FCOR24600 FH572052-03-5 N/A TASK DELETEDR 572052-03-6 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33C641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP ORPOST 48437SEALANT REMOVAL AS AND BOTTOM FLANGE. 50000 FHORPER NTM I: 9200 FCGROUP 33DORPOST 4843728700 FH572052-03-7 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 33E641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP ORSEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FHPER NTM I: 9200 FCOR28700 FH572052-03-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32E641CB 641 FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP ORSEALANT REMOVAL AS AND BOTTOM FLANGE 50000 FHPER NTM I: 7900 FCOR46400 FH572054-01-10 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32E671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. OR50000 FHI: 7400 FCOR43600 FH572054-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 87APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSD 572054-01-6 N/A TASK DELETED572054-01-7 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33A671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. ORPOST 4350350000 FHORI: 8300 FCGROUP 33BORPOST 4350326600 FH572054-01-8 N/A TASK DELETED572054-01-9 FLAPS EXTENDED 571 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 33E671 AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. OR50000 FHI: 8600 FCOR27000 FH572061-01-2 521AB 521BB 521CB 521 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE CPCP ZL-521-01-1 ALL521DB 521EB 521FB 522 FORWARD FACE BETWEEN RIB 1 AND RIB 12 INCLUDING ALL I: 6 YEZL-522-01-1521GB 521HB 521JB 621 CUTOUTS AND IN VICINITY OF FORWARD PYLON ATTACHMENT522AB 522BB 522CB 622 FITTING IN REGION OF RIB BAY 10-10A AND BUILD DOOR.522DB 522EB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB572062-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP ALL641 UPPER AND LOWER ROOT JOINT FITTINGS. I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 88APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572063-01-10 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 ORPOST 48437641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 7300 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR43000 FHN 572063-01-11 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33C541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 ORPOST 48437641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FHOR641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 8500 FCGROUP 33DAND SPAR JOINT BOLTING INBOARD OF RIB 12 ORPOST 4843726600 FHR 572063-01-5 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 ORPRE 48437641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 5500 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR25600 FHR 572063-01-6 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33A541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OROR641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FHGROUP 33B641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 6600 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR21300 FHR 572063-01-7 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33C541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 ORPRE 48437641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 6100 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR19700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 89APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572063-01-8 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33D541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 ORPRE 48437641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FH641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 5700 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR18400 FH572063-01-9 541AB 541BB 541CB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FCGROUP 32E541DB 541EB 541FB 641 BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 OROR641AB 641BB 641CB INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD 50000 FHGROUP 33E641DB 641EB 641FB PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A I: 17000 FCAND SPAR JOINT BOLTING INBOARD OF RIB 12. OR50000 FH572063-02-2 541AB 541BB 541CB 541 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-541-02-1 ALL541DB 541EB 541FB 641 AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 I: 12 YE641AB 641BB 641CB AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF641DB 641EB 641FB FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIBR 572064-01-10 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A640 BETWEEN RIB 8 AND RIB 10,INCLUDING TOP AND BOTTOM ORPOST 48437FLANGES 50000 FHI: 7300 FCOR43000 FHR 572064-01-5 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM ORPRE 48437FLANGES 50000 FHI: 6900 FCOR31700 FH572064-01-6 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 90APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572064-01-7 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33C640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM ORPOST 48437FLANGES. 50000 FHORI: 8500 FCGROUP 33DORPOST 4843726000 FHR 572064-01-8 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FCGROUP 33E640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM ORFLANGES. 50000 FHI: 10000 FCOR31300 FHR 572064-01-9 541EB 641EB 540 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FCGROUP 32E640 BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM ORFLANGES. 50000 FHI: 8600 FCOR43400 FHR 572064-02-2 541EB 641EB 540 GENERAL VISUAL INSPECTION OF OUTER WING FRONT SPAR T: 12 YE NO CPCP ZL-541-02-1 ALL640 AFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND I: 12 YEBOTTOM FLANGESISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 91APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572065-01-1 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 32A622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OR I: 6 YEOR20000 FCGROUP 33COROR50000 FHGROUP 33DI: 6 YEOR20000 FCOR50000 FHR 572065-01-4 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 20000 FCGROUP 33A622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OROR50000 FHGROUP 33BI: 14600 FCOR46800 FH572065-01-5 N/A TASK DELETED572065-01-6 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 32E622EB 622 FACE SPAR JOINT PLATE AT RIB 12. OR I: 6 YEOR17000 FCGROUP 33EOR50000 FHI: 6 YEOR17000 FCOR50000 FHR 572065-01-7 522DB 522EB 622DB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 33A622EB 622 FACE SPAR JOINT PLATE AT RIB 12. I: 6 YE I: 6 YEORGROUP 33BORGROUP 32FISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 92APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572066-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FCGROUP 32A600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OROR50000 FHGROUP 33CI: 20000 FCORORGROUP 33D50000 FHR 572066-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FCGROUP 33A600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OROR50000 FHGROUP 33BI: 14600 FCOR46800 FH572066-01-6 N/A TASK DELETED572066-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 17000 FCGROUP 32E600 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12. OROR50000 FHGROUP 33EI: 17000 FCOR50000 FH572067-01-10 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 17000 FCGROUP 33E541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 17000 FCOR50000 FH572067-01-11 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 17000 FCGROUP 32E541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 93APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572067-01-13 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 33D541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPOST 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 18600 FCOR50000 FH572067-01-14 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 32A541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPOST 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR50000 FH572067-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 32A541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPRE 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FHR 572067-01-5 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 33A541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPRE 41114641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 8100 FCOR23000 FHD 572067-01-6 N/A TASK DELETED572067-01-8 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 33C541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPRE 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 94APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572067-01-9 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND T: 20000 FCGROUP 33D541FZ 641CB 641DB 641 AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPRE 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FH572067-02-2 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 6 FORWARD T: 12 YE NO CPCP ZL-541-02-1 ALL541FZ 641CB 641DB 641 AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING I: 12 YE641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTSAND ACCESS CUTOUT SURROUNDS.572068-01-11 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FCGROUP 33D541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPOST 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 18600 FCOR50000 FH572068-01-12 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FCGROUP 32A541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPOST 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR50000 FH572068-01-4 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 20000 FCGROUP 32A541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING ORPRE 48437641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHORAND ACCESS CUTOUT SURROUNDS. I: 20000 FCGROUP 33COROR50000 FHGROUP 33DPRE 48437572068-01-5 N/A TASK DELETEDD 572068-01-6 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 95APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572068-01-7 N/A TASK DELETED572068-01-8 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 17000 FCGROUP 33E541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 17000 FCOR50000 FH572068-01-9 541CB 541DB 541EZ 541 DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND T: 17000 FCGROUP 32E541FZ 641CB 641DB 641 AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING OR641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS 50000 FHAND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR50000 FH572068-02-2 541CB 541DB 541EZ 541 GENERAL VISUAL INSPECTION OF OUTER WING RIB 7 FORWARD T: 12 YE NO CPCP ZL-541-02-1 ALL541FZ 641CB 641DB 641 AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING I: 12 YE641EZ 641FZ CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTSAND ACCESS CUTOUT SURROUNDS.572069-01-10 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 17000 FCGROUP 32E641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR50000 FHR 572069-01-11 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 33C641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORPOST 48437INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 62800 FHORSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 17100 FCGROUP 33DORPOST 4843753700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 96APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572069-01-12 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 32A641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORPOST 48437INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 117900 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 14700 FCOR86700 FHN 572069-01-13 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 33C641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORPRE 48437INCLUDING CLEATS,SPAR ATTACHMENTS, REGION OF STRINGER 50000 FHCUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FHR 572069-01-4 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 32A641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORPRE 48437INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FHR 572069-01-5 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 33A641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 6700 FCOR19000 FHR 572069-01-6 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 33B641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 6100 FCOR17400 FH572069-01-7 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 97APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572069-01-8 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 20000 FCGROUP 33D641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORPRE 48437INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 20000 FCOR50000 FH572069-01-9 541DB 541FZ 641DB 541 DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 T: 17000 FCGROUP 33E641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS ORINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF 50000 FHSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS. I: 17000 FCOR50000 FH572069-02-2 541DB 541FZ 641DB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS 8 AND 9 T: 12 YE NO CPCP ZL-541-02-1 ALL641FZ 641 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS I: 12 YEINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OFSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.572071-01-4 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FCGROUP 32A541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT OROR541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FHGROUP 33D641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FCPOST 48437641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR50000 FH572071-01-5 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FCGROUP 33A541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT OROR541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FHGROUP 33B641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 6800 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR21700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 98APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572071-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FCGROUP 33C541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT ORPRE 48437541EZ 641AB 641AZ SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR50000 FH572071-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 20000 FCGROUP 33D541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A ORPRE 48437541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR 50000 FH641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 20000 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR50000 FH572071-01-8 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 T: 17000 FCGROUP 32E541BZ 541CZ 541DZ 641 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A OROR541EZ 641AB 641AZ AT SKIN ATTACHMENTS (INCLUDING CLEATS), 50000 FHGROUP 33E641BB 641BZ 641CZ SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS I: 17000 FC641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING. OR50000 FH572071-02-2 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIBS T: 12 YE NO CPCP ZL-541-02-1 ALL541BZ 541CZ 541DZ 641 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB I: 12 YE541EZ 641AB 641AZ 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR641BB 641BZ 641CZ ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS641DZ 641EZ CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING.572072-01-1 N/A TASK DELETED572073-01-10 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FCGROUP 33D641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORPOST 48437ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 18600 FCSURROUNDS. OR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 99APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572073-01-11 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FCGROUP 32A641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORPOST 48437ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 14700 FCSURROUNDS. OR50000 FH572073-01-4 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FCGROUP 32A641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORPRE 48437ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHORREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 20000 FCGROUP 33CSURROUNDS. OROR50000 FHGROUP 33DPRE 48437R 572073-01-5 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 20000 FCGROUP 33A641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHGROUP 33BREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 6400 FCSURROUNDS. OR18200 FH572073-01-6 N/A TASK DELETED572073-01-7 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 17000 FCGROUP 33E641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 17000 FCSURROUNDS. OR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 100APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572073-01-8 541FB 541GB 641FB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, T: 17000 FCGROUP 32E641GB 641 RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ORATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, 50000 FHREGION OF STRINGER CUTOUTS AND ACCESS CUTOUT I: 14700 FCSURROUNDS. OR50000 FH572073-02-2 541FB 541GB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 10 T: 12 YE NO CPCP ZL-541-02-1 ALL641GB 641 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN I: 12 YEATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.572074-01-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING RIBS, RIB 10 T: 12 YE NO CPCP ZL-541-02-1 ALL641FB 641 FORWARD, RIB 10A AND PYLON DIAPHRAGM. I: 12 YE572075-01-1 541AB 641AB 541 DETAILED INSPECTION OF OUTER WING BOX, RIB 1 EXTERNAL T: 12 YE T: 20 YE NO CPCP ALL641 SURFACE AND UPPER SURFACE OF TRIFORM FITTING, BETWEEN I: 12 YE I: 12 YEFRONT SPAR AND REAR SPAR.572081-01-1 N/A TASK DELETEDD 572081-01-10 N/A TASK DELETED572081-01-11 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 17000 FCGROUP 32E641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR50000 FHI: 7100 FCOR41800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 101APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572081-01-12 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 17000 FCGROUP 33E641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. OR50000 FHI: 8200 FCOR25900 FH572081-01-13 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 20000 FCGROUP 33D641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. ORPOST 4843750000 FHI: 9000 FCOR25000 FH572081-01-14 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 20000 FCGROUP 32A641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. ORPOST 4843750000 FHI: 7100 FCOR41800 FHD 572081-01-5 N/A TASK DELETED572081-01-6 N/A TASK DELETED572081-01-7 N/A TASK DELETED572081-01-8 N/A TASK DELETED572081-01-9 541AB 541AZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO CPCP ALL641AZ 641 ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 102APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572082-01-10 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 17000 FCGROUP 32E541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND 99800 FH541FZ 641AB 641AZ ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 23400 FC641BB 641CB 641DB OR641DZ 641EB 641EZ 137500 FH641FB 641FZD 572082-01-5 N/A TASK DELETEDR 572082-01-6 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 20000 FCGROUP 33A541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING ORPOST 40366541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 50000 FHPOST 42275541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 8400 FC641BB 641CB 641DB OR641DZ 641EB 641EZ 26900 FH641FB 641FZR 572082-01-7 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 20000 FCGROUP 33B541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING ORPOST 42550541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 50000 FH541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 8400 FC641BB 641CB 641DB OR641DZ 641EB 641EZ 26900 FH641FB 641FZ572082-01-8 N/A TASK DELETEDR 572082-01-9 541AB 541AZ 541BB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN T: 17000 FCGROUP 33E541CB 541DB 541DZ 641 RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING OR541EB 541EZ 541FB SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS 53200 FH541FZ 641AB 641AZ HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES. I: 27200 FC641BB 641CB 641DB OR641DZ 641EB 641EZ 85200 FH641FB 641FZISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 103APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572082-02-2 541AB 541AZ 541BB 541 GENERAL VISUAL INSPECTION OF OUTER WING CENTER SPAR T: 12 YE NO CPCP ZL-541-02-1 ALL541CB 541DB 541DZ 641 BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES I: 12 YE541EB 541EZ 541FB COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA541FZ 641AB 641AZ AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT641BB 641CB 641DB HOLES.641DZ 641EB 641EZ641FB 641FZ572083-01-1 541AB 541BZ 641AB 541 DETAILED INSPECTION OF OUTER WING CENTER SPAR T: 12 YE T: 20 YE NO CPCP ALL641BZ 641 ASSEMBLY AFT FACE BETWEEN RIBS 1 AND 2. I: 12 YE I: 12 YE572084-01-1 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FCGROUP 33ASEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORPRE 41652PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FHOR20 AND AT STR. 23 TO 28 LH/RH. I: 9900 FCGROUP 33BORPRE 4165229700 FH572084-01-2 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FCGROUP 33ASEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORPOST 41652PER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FHOR20 AND AT STR. 23 TO 28 LH/RH. I: 12700 FCGROUP 33BORPOST 4165238200 FH572084-01-3 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FCGROUP 32ASEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORORPER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FHGROUP 33C20 AND AT STR. 23 TO 28 LH/RH. I: 11400 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 104APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572084-01-4 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 17000 FCGROUP 33ESEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORPER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH20 AND AT STR. 23 TO 28 LH/RH. I: 12500 FCOR37500 FH572084-01-5 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 17000 FCGROUP 32ESEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORPER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH20 AND AT STR. 23 TO 28 LH/RH. I: 11000 FCOR50000 FH572084-01-6 541AB 641AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOX T: 20000 FCGROUP 33DSEALANT REMOVAL AS 641 INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD ORPER NTM FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 50000 FH20 AND AT STR. 23 TO 28 LH/RH. I: 11200 FCOR50000 FH572085-01-1 191BT 191CT 192BT 191 GENERAL VISUAL INSPECTION OF OUTER WING BOX, T: 12 YE 1 CPCP ALL192CT 192 CRUCIFORM FITTING, OUTBOARD FLANGE UPPER SURFACE AS I: 12 YEFAR AS VISIBLE, FROM FR 40 TO FR 47, LH/RHR 572090-01-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND ORPRE 48437RIB 9. 50000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-1 I: 5200 FCOR23600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 105APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572090-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND ORORRIB 9. 50000 FHGROUP 33BNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-2 I: 4400 FCOR13800 FHR 572090-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND ORPRE 48437RIB 9. 50000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-3 I: 5700 FCOR16800 FHR 572090-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 ORPRE 48437AND RIB 9. 50000 FHI: 5400 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-4 OR16100 FHR 572090-02-1 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB ORPRE 484378 AND RIB 9. 90900 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-1 I: 12800 FCOR58200 FH572090-02-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB OROR8 AND RIB 9. 50000 FHGROUP 33BNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-2 I: 12000 FCOR37600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 106APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572090-02-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB ORPRE 484378 AND RIB 9. 50000 FHNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-3 I: 14000 FCOR41500 FHR 572090-02-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN ORPRE 48437RIB 8 AND RIB 9. 50000 FHI: 13400 FCNOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-4 OR39600 FH572091-01-3 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10. ORPRE 44245NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHORTASK 572091-02-3 I: 7000 FCGROUP 33BORPRE 4424521900 FH572091-02-3 541EB 541FB 641EB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641FB 641 STRINGER 10 JOINT BETWEEN RIB 9 AND RIB 10. ORPRE 44245NUT REMOVAL AS PER NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHORNTM TASK 572091-01-3 I: 7000 FCGROUP 33BSEALANT REMOVAL AS ORPRE 44245PER NTM 21900 FH572092-01-10 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, ORPOST 48437EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 10100 FCOR28200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 107APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572092-01-11 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, ORPOST 48437EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 8100 FCOR36500 FH572092-01-4 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, ORPRE 48437EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 9000 FCOR36200 FH572092-01-5 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OROREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHGROUP 33BI: 7000 FCOR21900 FH572092-01-6 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 9000 FCOR28200 FH572092-01-7 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 9600 FCOR27200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 108APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572092-01-8 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, OREXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 8100 FCOR36500 FH572092-01-9 541EB 541FB 641EB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, ORPRE 48437EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. 50000 FHI: 8400 FCOR26300 FH572092-02-1 541EB 541FB 641EB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641FB 641 STRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, I: 12 YEEXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR.R 572093-01-10 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT T: 20000 FCGROUP 33D641 OF STRINGER 15 TO CENTER SPAR ORPRE 4843750000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FCTASK 572093-02-10 OR18100 FHR 572093-01-11 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 17000 FCGROUP 33E641 OF STRINGER 15 TO CENTER SPAR OR50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FCTASK 572093-02-11 OR22700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 109APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572093-01-12 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 17000 FCGROUP 32E641 OF STRINGER 15 TO CENTER SPAR OR50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FCTASK 572093-02-12 OR30400 FHR 572093-01-13 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 33C641 OF STRINGER 15 TO CENTER SPAR ORPOST 4843750000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FCGROUP 33DTASK 572093-02-13 ORPOST 4843722700 FHR 572093-01-14 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 32A641 OF STRINGER 15 TO CENTER SPAR ORPOST 4843750000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FCTASK 572093-02-14 OR30300 FHR 572093-01-6 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 32A641 OF STRINGER 15 TO CENTER SPAR ORPRE 48437NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572093-02-6 I: 5900 FCOR26800 FHR 572093-01-7 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 33A641 OF STRINGER 15 TO CENTER SPAR ORMSN 0050NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHAND SUBSTASK 572093-02-7 I: 6300 FCORORGROUP 33B18800 FHMSN 0050AND SUBSISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 110APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572093-01-8 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 33A641 OF STRINGER 15 TO CENTER SPAR ORUP TO MSN 0045NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHPOST 45415TASK 572093-02-8 I: 6800 FCOR21300 FHR 572093-01-9 541FB 641FB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT T: 20000 FCGROUP 33C641 OF STRINGER 15 TO CENTER SPAR ORPRE 48437NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572093-02-9 I: 6500 FCOR19400 FHR 572093-02-10 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33DSEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPRE 48437PER NTM 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6100 FCTASK 572093-01-10 OR18100 FH572093-02-11 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33ESEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPER NTM 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FCTASK 572093-01-11 OR22700 FH572093-02-12 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32ESEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPER NTM 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FCTASK 572093-01-12 OR30400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 111APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572093-02-13 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33CSEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPOST 48437PER NTM 50000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 8000 FCGROUP 33DTASK 572093-01-13 ORPOST 4843722700 FHR 572093-02-14 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPOST 48437PER NTM 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6700 FCTASK 572093-01-14 OR30300 FHR 572093-02-6 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPRE 48437PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572093-01-6 I: 5900 FCOR26800 FHR 572093-02-7 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORMSN 0050PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHAND SUBSTASK 572093-01-7 I: 6300 FCORORGROUP 33B18800 FHMSN 0050AND SUBS572093-02-8 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33ASEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORUP TO MSN 0045PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHPOST 45415TASK 572093-01-8 I: 6800 FCOR21300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 112APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572093-02-9 541FB 641FB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33CSEALANT REMOVAL AS 641 JOINT OF STRINGER 15 TO CENTER SPAR ORPRE 48437PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572093-01-9 I: 6500 FCOR19400 FH572093-03-1 541FB 641FB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641 JOINT OF STRINGER 15 TO CENTER SPAR I: 12 YER 572094-01-10 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORPRE 48437AND RIB 12. 50000 FHI: 6500 FCOR19200 FH572094-01-11 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORPOST 48437AND RIB 12. 50000 FHI: 14300 FCOR39700 FH572094-01-12 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORPOST 48437AND RIB 12. 50000 FHI: 11400 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 113APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572094-01-5 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORPRE 48437AND RIB 12. 50000 FHI: 6200 FCOR28300 FHR 572094-01-6 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORORAND RIB 12. 50000 FHGROUP 33BI: 8600 FCOR25600 FH572094-01-7 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORAND RIB 12. 50000 FHI: 7400 FCOR23200 FH572094-01-8 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORAND RIB 12. 50000 FHI: 13500 FCOR38300 FH572094-01-9 541EB 541FB 541GB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 ORAND RIB 12. 50000 FHI: 11400 FCOR50000 FH572094-02-2 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL641EB 641FB 641GB 641 BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 I: 12 YEAND RIB 12.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 114APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572095-01-10 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR50000 FHI: 11400 FCOR50000 FHR 572095-01-11 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. ORPOST 4843750000 FHI: 14300 FCOR39700 FHR 572095-01-12 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. ORPOST 4843750000 FHI: 11400 FCOR50000 FHR 572095-01-5 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. ORPRE 4843750000 FHI: 6900 FCOR31500 FHR 572095-01-6 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OROR50000 FHGROUP 33BI: 7300 FCOR21700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 115APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572095-01-7 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. ORPRE 4843750000 FHI: 7500 FCOR22100 FHR 572095-01-8 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. ORPRE 4843750000 FHI: 7100 FCOR21100 FHR 572095-01-9 541BB 541CB 641BB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E641CB 641 STRINGER 20 BETWEEN RIB 5 AND RIB 7. OR50000 FHI: 13500 FCOR38300 FH572101-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 9400 FCOR26300 FH572101-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED 50000 FHBY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 7500 FCOR34000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 116APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572101-01-12 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK FAIRINGS 3, 4 AND 5. I: 6900 FCOR21600 FHR 572101-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK FAIRINGS 3, 4 AND 5. I: 5600 FCOR25500 FH572101-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORORBETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FHGROUP 33BFLAP TRACK FAIRINGS 3, 4 AND 5. I: 5700 FCOR17800 FHR 572101-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK FAIRINGS 3, 4 AND 5. I: 6300 FCOR18800 FHR 572101-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORPRE 48437SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 50000 FHAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 5500 FCOR16300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 117APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572101-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORSPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING 50000 FHAREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 8900 FCOR25400 FH572101-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5. I: 7500 FCOR34000 FH572101-02-1 N/A TASK DELETED572102-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33D600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. ORPOST 4843750000 FHI: 17100 FCOR47600 FH572102-01-11 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 32A600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. ORPOST 4843750000 FHI: 13600 FCOR50000 FH572102-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 32A600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. ORPRE 4843750000 FHI: 4400 FCOR17600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 118APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572102-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33A600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OROR50000 FHGROUP 33BI: 6400 FCOR20000 FH572102-01-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33C600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR50000 FHI: 4400 FCOR13800 FH572102-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCZL-500-01-1 GROUP 33E600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR50000 FHI: 16100 FCOR45900 FH572102-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOMSKIN T: 17000 FCZL-500-01-1 GROUP 32E600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. OR50000 FHI: 13600 FCOR50000 FH572102-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33D600 LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA. ORPRE 4843750000 FHI: 4000 FCOR12500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 119APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572104-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED 50000 FHBY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 9400 FCRIB 39. OR26300 FH572104-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 7500 FCRIB 39. OR34000 FHN 572104-01-12 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6900 FCRIB 39. OR21600 FHR 572104-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 5600 FCRIB 39. OR25500 FHR 572104-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORORBETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHGROUP 33BFLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6800 FCRIB 39. OR20200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 120APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572104-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 6300 FCRIB 39. OR18800 FHR 572104-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORPRE 48437SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDINGAREAS 50000 FHCOVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS I: 5500 FCAT RIB 27 AND RIB 39. OR16300 FH572104-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED 50000 FHBY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND I: 8900 FCRIB 39. OR25400 FH572104-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY 50000 FHFLAP TRACK 5 FAIRING AND SKIN JOINTS AT I: 7500 FCRIB 27 AND RIB 39. OR34000 FH572106-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORPOST 48437AND RIB 23. 50000 FHI: 9000 FCOR25100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 121APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572106-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORPOST 48437AND RIB 23. 50000 FHI: 7200 FCOR32500 FH572106-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORPRE 48437AND RIB 23. 50000 FHI: 7700 FCOR30900 FH572106-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORORAND RIB 23. 50000 FHGROUP 33BI: 9100 FCOR28500 FH572106-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORAND RIB 23. 50000 FHI: 7600 FCOR23800 FH572106-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORAND RIB 23. 50000 FHI: 8500 FCOR24300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 122APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572106-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB OR12 AND RIB 23. 50000 FHI: 7200 FCOR32500 FH572106-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT RUNOUT OF STRINGER BETWEEN RIB 12 ORPRE 48437AND RIB 23. 50000 FHI: 7100 FCOR22200 FH572107-01-10 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORPOST 48437AND RIB 39. 50000 FHI: 9000 FCOR25100 FH572107-01-11 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORPOST 48437AND RIB 39. 50000 FHI: 7200 FCOR32500 FH572107-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORPRE 48437AND RIB 39. 50000 FHI: 7700 FCOR30900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 123APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572107-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORORAND RIB 39. 50000 FHGROUP 33BI: 9100 FCOR28500 FH572107-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORAND RIB 39. 50000 FHI: 7600 FCOR23800 FH572107-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORAND RIB 39. 50000 FHI: 8500 FCOR24300 FH572107-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORAND RIB 39. 50000 FHI: 7200 FCOR32500 FH572107-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 ORPRE 48437AND RIB 39. 50000 FHI: 7100 FCOR22200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 124APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572108-01-2 532AB 533AB 534AB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP ALL541GB 541HB 541JB 542 AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS I: 6 YE541KB 541LB 541MB 641 IN ALL BAYS BETWEEN RIBS 12 AND 27.541NB 541PB 541QB 642541RB 541SB 542AB542BB 542CB 542DB632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-10 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPOST 48437541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 8400 FC541RB 541SB 542AB OR542BB 542CB 542DB 23500 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-11 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPOST 48437541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 6700 FC541RB 541SB 542AB OR542BB 542CB 542DB 30400 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 125APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572108-02-4 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 6600 FC541RB 541SB 542AB OR542BB 542CB 542DB 30000 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-5 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OROR541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FHGROUP 33B541NB 541PB 541QB 642 I: 9100 FC541RB 541SB 542AB OR542BB 542CB 542DB 28500 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBR 572108-02-6 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 7100 FC541RB 541SB 542AB OR542BB 542CB 542DB 21100 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 126APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572108-02-7 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR ORPRE 48437541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 6900 FC541RB 541SB 542AB OR542BB 542CB 542DB 26000 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-8 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 8000 FC541RB 541SB 542AB OR542BB 542CB 542DB 22700 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-9 532AB 533AB 534AB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541GB 541HB 541JB 542 UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR OR541KB 541LB 541MB 641 CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 27. 50000 FH541NB 541PB 541QB 642 I: 6700 FC541RB 541SB 542AB OR542BB 542CB 542DB 30400 FH632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 127APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572109-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE NO CPCP ALL542HB 542JB 542KB 550 AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, I: 6 YE550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND550DB 550EB 550FB 650 39.642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB572109-02-1 N/A TASK DELETED572109-02-10 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, ORPOST 48437550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 8400 FC642EB 642FB 642GB OR642HB 642JB 642KB 23500 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-11 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, ORPOST 48437550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 6700 FC642EB 642FB 642GB OR642HB 642JB 642KB 30400 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-4 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, ORPRE 48437550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 13100 FC642EB 642FB 642GB OR642HB 642JB 642KB 50000 FH650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 128APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572109-02-5 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OROR550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FHGROUP 33B550DB 550EB 550FB 650 39. I: 10200 FC642EB 642FB 642GB OR642HB 642JB 642KB 30300 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-6 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 13200 FC642EB 642FB 642GB OR642HB 642JB 642KB 41400 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-7 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 8000 FC642EB 642FB 642GB OR642HB 642JB 642KB 22700 FH650AB 650BB 650CB650DB 650EB 650FB572109-02-8 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, OR550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 6700 FC642EB 642FB 642GB OR642HB 642JB 642KB 30400 FH650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 129APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572109-02-9 542EB 542FB 542GB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D542HB 542JB 542KB 550 UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, ORPRE 48437550AB 550BB 550CB 642 INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 50000 FH550DB 550EB 550FB 650 39. I: 12100 FC642EB 642FB 642GB OR642HB 642JB 642KB 37900 FH650AB 650BB 650CB650DB 650EB 650FB572110-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORPOST 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 9200 FCOR25700 FH572110-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORPOST 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 7400 FCOR33300 FHR 572110-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORPRE 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 9400 FCOR43000 FHD 572110-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 130APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572110-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORPRE 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 10600 FCOR31500 FHR 572110-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORPRE 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 9800 FCOR29100 FH572110-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 8700 FCOR24800 FH572110-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRINGS 3, 4 AND 5. I: 7400 FCOR33300 FH572110-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ZL-500-01-1 ALL600 LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT I: 6 YESPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRINGS 3, 4 AND 5.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 131APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572111-01-10 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 ORPOST 48437632AB 632CB 633AB 534 AND 5. 50000 FH633CB 634AB 634CB 632 I: 9200 FC633 OR634 25700 FH572111-01-11 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 ORPOST 48437632AB 632CB 633AB 534 AND 5. 50000 FH633CB 634AB 634CB 632 I: 7400 FC633 OR634 33300 FHD 572111-01-4 N/A TASK DELETEDD 572111-01-5 N/A TASK DELETEDR 572111-01-6 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 ORPRE 48437632AB 632CB 633AB 534 AND 5. 50000 FH633CB 634AB 634CB 632 I: 9200 FC633 OR634 27400 FHD 572111-01-7 N/A TASK DELETED572111-01-8 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR632AB 632CB 633AB 534 AND 5. 50000 FH633CB 634AB 634CB 632 I: 8700 FC633 OR634 24800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 132APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572111-01-9 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E533CB 534AB 534CB 533 SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 OR632AB 632CB 633AB 534 AND 5. 50000 FH633CB 634AB 634CB 632 I: 7400 FC633 OR634 33300 FH572111-02-1 532AB 532CB 533AB 532 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE CPCP ZL-531-02-1 ALL533CB 534AB 534CB 533 LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS I: 6 YE632AB 632CB 633AB 534 3,4 AND 5.633CB 634AB 634CB 632633634572112-03-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORPRE 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 10500 FCOR42200 FH572112-03-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHGROUP 33BFAIRING 5. I: 9900 FCOR31000 FH572112-03-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 10600 FCOR33200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 133APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572112-03-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 8700 FCOR24800 FH572112-03-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORREAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 7400 FCOR33300 FH572112-03-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORPRE 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 9800 FCOR30700 FH572112-03-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORPOST 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 9200 FCOR25700 FH572112-03-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT SPAR TO ORPOST 48437REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK 50000 FHFAIRING 5. I: 7400 FCOR33300 FH572112-04-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-500-01-1 ALL600 LOWER SURFACE BETWEEN RIB 23 AND RIB 39 FROM FRONT I: 12 YESPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRING 5.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 134APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572116-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 32A600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORPRE 48437STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5900 FCOR23700 FHR 572116-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORORSTRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHGROUP 33BCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 7200 FCOR21400 FH572116-02-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33C600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5900 FCOR18500 FH572116-02-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCZL-500-01-1 GROUP 33E600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 9600 FCOR27500 FH572116-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCZL-500-01-1 GROUP 32E600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORSTRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 8100 FCOR36800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 135APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572116-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33D600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORPRE 48437STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 5500 FCOR17200 FH572116-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 33D600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORPOST 48437STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 10200 FCOR28500 FH572116-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCZL-500-01-1 GROUP 32A600 LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND ORPOST 48437STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS 50000 FHCOVERED BY FLAP TRACK FAIRINGS 3, 4 & 5. I: 8100 FCOR36800 FH572117-01-10 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPOST 48437632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH633CB 634AB 634CB 632 I: 12600 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 35100 FH572117-01-11 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPOST 48437632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH633CB 634AB 634CB 632 I: 10000 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 45400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 136APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572117-01-4 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPRE 48437632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FH633CB 634AB 634CB 632 5. I: 7700 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 30900 FHR 572117-01-5 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OROR632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FHGROUP 33B633CB 634AB 634CB 632 5. I: 8400 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 25000 FH572117-01-6 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 50000 FH633CB 634AB 634CB 632 5. I: 7600 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 23800 FH572117-01-7 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. 50000 FH633CB 634AB 634CB 632 I: 11900 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 33900 FH572117-01-8 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND OR632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH633CB 634AB 634CB 632 I: 10000 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 45400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 137APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572117-01-9 532AB 532CB 533AB 532 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D533CB 534AB 534CB 533 SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND ORPRE 48437632AB 632CB 633AB 534 STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5 50000 FH633CB 634AB 634CB 632 I: 7100 FCFAIRINGS ATTACHMENT 633 ORBRACKET 634 22200 FH572119-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 32A600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEPRE 48437DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 6900 FCOR27700 FH572119-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33A600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEORDRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHGROUP 33BSPAR, BETWEEN RIBS 12 AND 23. I: 6600 FCOR20700 FH572119-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33C600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEDRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 7000 FCOR21900 FH572119-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO CPCP GROUP 33E600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEDRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 16200 FCOR46200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 138APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572119-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO CPCP GROUP 32E600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEDRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 13700 FCOR50000 FH572119-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEPRE 48437DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 6300 FCOR19700 FH572119-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEPOST 48437DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 17200 FCOR47800 FH572119-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 32A600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND OR I: 6 YEPOST 48437DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 12 AND 23. I: 13700 FCOR50000 FHN 572119-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO CPCP A330-200F600 SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND I: 6 YEDRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REARSPAR, BETWEEN RIBS 12 AND 23.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 139APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572120-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORPOST 48437IN RIB BAY 22-23. 50000 FHI: 9300 FCOR25900 FH572120-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORPOST 48437IN RIB BAY 22-23. 50000 FHI: 7400 FCOR33500 FH572120-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 32A600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORPRE 48437IN RIB BAY 22-23. 50000 FHI: 6500 FCOR26100 FH572120-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33A600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORORIN RIB BAY 22-23. 50000 FHGROUP 33BI: 9300 FCOR29100 FH572120-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORIN RIB BAY 22-23. 50000 FHI: 6500 FCOR20300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 140APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572120-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 33E600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORIN RIB BAY 22-23. 50000 FHI: 8800 FCOR25000 FH572120-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FCGROUP 32E600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORIN RIB BAY 22-23. 50000 FHI: 7400 FCOR33500 FH572120-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FCGROUP 33D600 SURFACE IN AREA OF SKIN JOINT RUNOUT AT STRINGER 20 ORPRE 48437IN RIB BAY 22-23. 50000 FHI: 6100 FCOR19100 FH572121-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING ORPOST 48437541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH541RB 541SB 641GB AND 20. I: 7000 FC641HB 641JB 641KB OR641LB 641MB 641NB 31600 FH641PB 641QB 641RB641SBN 572121-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING ORPRE 48437541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH541RB 541SB 641GB AND 20. I: 5400 FC641HB 641JB 641KB OR641LB 641MB 641NB 16100 FH641PB 641QB 641RB641SBD 572121-01-4 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 141APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSD 572121-01-5 N/A TASK DELETEDR 572121-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING ORPOST 48437541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FHOR541RB 541SB 641GB AND 20. I: 8300 FCGROUP 33D641HB 641JB 641KB ORPOST 48437641LB 641MB 641NB 23600 FH641PB 641QB 641RB641SBD 572121-01-7 N/A TASK DELETED572121-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH541RB 541SB 641GB AND 20. I: 8300 FC641HB 641JB 641KB OR641LB 641MB 641NB 23600 FH641PB 641QB 641RB641SB572121-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING OR541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 50000 FH541RB 541SB 641GB AND 20. I: 7000 FC641HB 641JB 641KB OR641LB 641MB 641NB 31600 FH641PB 641QB 641RB641SB572121-02-2 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541KB 541LB 541MB 641 STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING I: 12 YE541NB 541PB 541QB STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13541RB 541SB 641GB AND 20.641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 142APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572122-01-10 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY ORPOST 48437542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH550CB 550DB 550EB 650 I: 8800 FC550FB 642AB 642BB OR642CB 642FB 642GB 24400 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-01-11 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY ORPOST 48437542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH550CB 550DB 550EB 650 I: 7000 FC550FB 642AB 642BB OR642CB 642FB 642GB 31600 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FBD 572122-01-4 N/A TASK DELETEDD 572122-01-5 N/A TASK DELETEDR 572122-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY ORPRE 48437542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH550CB 550DB 550EB 650 I: 5300 FC550FB 642AB 642BB OR642CB 642FB 642GB 15800 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FBD 572122-01-7 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 143APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572122-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH550CB 550DB 550EB 650 I: 8300 FC550FB 642AB 642BB OR642CB 642FB 642GB 23600 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY OR542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18. 50000 FH550CB 550DB 550EB 650 I: 7000 FC550FB 642AB 642BB OR642CB 642FB 642GB 31600 FH642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572122-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL542FB 542GB 542HB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY I: 12 YEZL-550-01-1542JB 550AB 550BB 642 26-28 AND STRINGERS 15 & 18.550CB 550DB 550EB 650550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB572123-01-1 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ACCESS T: 12 YE NO CPCP ALL542HB 542JB 542KB 550 DOORS BETWEEN RIB 27 AND RIB 39 INCLUDING NACA DUCT I: 6 YE550AB 550BB 550CB 642 DOOR.550DB 550EB 550FB 650642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 144APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572124-01-3 542AB 642AB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ALL642 UPPER SURFACE BETWEEN RIB 23 AND RIB 24. I: 6 YENOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENT572125-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORJOINTS ON STRINGERS 15 AND 18. 50000 FHI: 17000 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ORAS TASK 572125-02-8 49100 FH572125-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORJOINTS ON STRINGERS 15 AND 18. 50000 FHI: 14600 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ORAS TASK 572125-02-9 50000 FH572125-01-12 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPOST 48437JOINTS ON STRINGERS 15 AND 18. 50000 FHI: 18300 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-02-10 50000 FH572125-01-13 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPOST 48437JOINTS ON STRINGERS 15 AND 18. 50000 FHI: 14600 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-02-11 50000 FH572125-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE T: 20 YE NO CPCP ALL642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING I: 12 YE I: 12 YEJOINTS ON STRINGERS 15 AND 18.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 145APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572125-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437JOINTS ON STRINGERS 15 AND 18. 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 9900 FCTASK 572125-02-4 OR45200 FHR 572125-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORORJOINTS ON STRINGERS 15 AND 18. 50000 FHGROUP 33BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FCTASK 572125-02-5 OR38500 FHR 572125-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437JOINTS ON STRINGERS 15 AND 18. 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 11200 FCTASK 572125-02-6 OR33200 FHR 572125-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437JOINTS ON STRINGERS 15 AND 18. 50000 FHI: 10200 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-02-7 30100 FH572125-02-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPOST 48437SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM I: 18300 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-12 50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 146APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572125-02-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPOST 48437SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM I: 14600 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-13 50000 FHR 572125-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 9900 FCTASK 572125-01-6 OR45200 FHR 572125-02-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORORSEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHGROUP 33BPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 13000 FCTASK 572125-01-7 OR38500 FHR 572125-02-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 11200 FCTASK 572125-01-8 OR33200 FHR 572125-02-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORPRE 48437SEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM I: 10200 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-9 30100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 147APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572125-02-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORSEALANT REMOVAL AS JOINTS ON STRINGERS 15 AND 18. 50000 FHPER NTM I: 17000 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-10 49100 FH572125-02-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642EB 642 STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING ORSEALANT REMOVAL AS ON STRINGERS 15 AND 18. 50000 FHPER NTM I: 14600 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572125-01-11 50000 FH572126-01-1 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER T: 12 YE T: 20 YE NO CPCP ALL642 SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YE I: 12 YE572126-02-10 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. ORPOST 4843750000 FHI: 13800 FCOR38500 FH572126-02-11 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. ORPOST 4843750000 FHI: 11000 FCOR49700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 148APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572126-02-4 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. ORPRE 4843750000 FHI: 5100 FCOR20500 FH572126-02-5 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OROR50000 FHGROUP 33BI: 6200 FCOR19400 FH572126-02-6 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR50000 FHI: 5100 FCOR15900 FH572126-02-7 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR50000 FHI: 13000 FCOR37100 FH572126-02-8 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. OR50000 FHI: 11000 FCOR49700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 149APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572126-02-9 542EB 642EB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642 UPPER SURFACE AT CHORDWISE JOINT AT RIB 27. ORPRE 4843750000 FHI: 4400 FCOR13800 FH572127-01-2 550AB 650AB 550 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ALL650 UPPER SURFACE BETWEEN RIB 33 AND RIB 34. I: 6 YENOTE: TASK INTERVAL MAY BE INFLUENCED BYMICROBIOLOGICAL CONTAMINATION AND IS THEREFORE TO BEADJUSTED BY INDIVIDUAL OPERATORS IN CONSIDERATION OFTHEIR OWN IN-SERVICE EXPERIENCE AND OPERATIONALENVIRONMENTD 572129-01-3 N/A TASK DELETEDD 572129-02-3 N/A TASK DELETEDD 572130-01-3 N/A TASK DELETEDD 572130-02-3 N/A TASK DELETED572131-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 12 AND RIB 27. 50000 FHI: 11800 FCOR32500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 150APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572131-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 12 AND RIB 27. 50000 FHI: 9100 FCOR40000 FHR 572131-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 12 AND RIB 27. 91700 FHI: 13600 FCOR62400 FHR 572131-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORORBETWEEN RIB 12 AND RIB 27. 50000 FHGROUP 33BI: 16400 FCOR48900 FHR 572131-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 12 AND RIB 27. 50000 FHI: 15800 FCOR47100 FHR 572131-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 12 AND RIB 27. 50000 FHI: 15000 FCOR44600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 151APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572131-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 12 AND RIB 27. 50000 FHI: 11000 FCOR31200 FH572131-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN T: 17000 FCGROUP 32E600 UPPER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR ORSPAR BETWEEN RIB 12 AND RIB 27. 50000 FHI: 9100 FCOR40000 FH572132-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 27 AND RIB 39. 50000 FHI: 9100 FCOR40000 FH572132-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 27 AND RIB 39. 50000 FHI: 16400 FCOR50000 FH572132-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORORBETWEEN RIB 27 AND RIB 39. 50000 FHGROUP 33BI: 16000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 152APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572132-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 27 AND RIB 39. 50000 FHI: 16700 FCOR50000 FH572132-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 27 AND RIB 39. 50000 FHI: 11000 FCOR31200 FH572132-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORBETWEEN RIB 27 AND RIB 39. 50000 FHI: 9100 FCOR40000 FH572132-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPRE 48437BETWEEN RIB 27 AND RIB 39. 50000 FHI: 15600 FCOR49600 FH572132-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR ORPOST 48437BETWEEN RIB 27 AND RIB 39. 50000 FHI: 11800 FCOR32500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 153APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572133-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT ORPOST 48437SPAR TO REAR SPAR. 50000 FHI: 13200 FCOR36100 FH572133-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORPOST 48437REAR SPAR. 50000 FHI: 10100 FCOR44500 FHR 572133-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORPRE 48437REAR SPAR. 50000 FHI: 5800 FCOR26300 FHR 572133-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORORREAR SPAR. 50000 FHGROUP 33BI: 8900 FCOR26600 FH572133-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO ORREAR SPAR. 50000 FHI: 6800 FCOR21800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 154APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572133-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR ORPRE 48437TO REAR SPAR. 50000 FHI: 6200 FCOR18500 FH572133-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR ORTO REAR SPAR. 50000 FHI: 12200 FCOR34700 FH572133-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR ORTO REAR SPAR. 50000 FHI: 10100 FCOR44500 FH572133-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 ALL600 UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT I: 6 YESPAR TO REAR SPAR.N 572134-02-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 A330-200F600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT I: 6 YESPAR TO REAR SPAR.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 155APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572134-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 GROUP 32A600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORPRE 48437SPAR TO REAR SPAR. 20000 FCOR50000 FHI: 6 YEOR6600 FCOR27900 FH572134-02-3 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 GROUP 33A600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORORSPAR TO REAR SPAR. 20000 FCGROUP 33BOR50000 FHI: 6 YEOR9900 FCOR31500 FH572134-02-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 GROUP 33C600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORSPAR TO REAR SPAR. 20000 FCOR50000 FHI: 6 YEOR7000 FCOR22300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 156APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572134-02-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 GROUP 33E600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORSPAR TO REAR SPAR. 17000 FCOR50000 FHI: 6 YEOR12200 FCOR34700 FH572134-02-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 GROUP 32E600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORSPAR TO REAR SPAR. 17000 FCOR50000 FHI: 6 YEOR10100 FCOR44500 FH572134-02-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 GROUP 33D600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORPRE 48437SPAR TO REAR SPAR. 20000 FCOR50000 FHI: 6 YEOR6300 FCOR20200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 157APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572134-02-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 GROUP 33D600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORPOST 48437SPAR TO REAR SPAR. 20000 FCOR50000 FHI: 6 YEOR13200 FCOR36100 FH572134-02-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 6 YE CPCP ZL-500-02-1 GROUP 32A600 UPPER SURFACE BETWEEN RIB 27 AND RIB 39 FROM FRONT ORPOST 48437SPAR TO REAR SPAR. 20000 FCOR50000 FHI: 6 YEOR10100 FCOR44500 FH572135-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 32A600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORPRE 48437BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHSTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 10400 FCOR37400 FH572135-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33A600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHGROUP 33BSTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 7600 FCOR24100 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 158APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572135-01-6 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33C600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHSTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 10600 FCOR33700 FH572135-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FCZL-500-02-1 GROUP 32E600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORORBETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHGROUP 33ESTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 17000 FCOR50000 FH572135-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33D600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORPRE 48437BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHSTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 9900 FCOR31600 FH572135-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 32A600 UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 ORPOST 48437BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT 50000 FHORSTRINGER 19 BETWEEN RIB 18 AND RIB 24. I: 20000 FCGROUP 33DORPOST 4843750000 FHN 572138-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 33C600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORPRE 48437JOINT AREA 50000 FHI: 20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 159APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572138-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 32A600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORPOST48437JOINT AREA. 50000 FHORI: 20000 FCGROUP 33CORPOST4843750000 FHORGROUP 33DPOST48437572138-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33A600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORORJOINT AREA. 50000 FHGROUP 33BI: 20000 FCOR50000 FH572138-01-6 N/A TASK DELETEDN 572138-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 33D600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORPRE 48437JOINT AREA 50000 FHI: 20000 FCOR50000 FH572138-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FCZL-500-02-1 GROUP 32E600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORORJOINT AREA. 50000 FHGROUP 33EI: 17000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 160APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572138-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 32A600 UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN ORPRE 48437JOINT AREA 50000 FHI: 20000 FCOR50000 FHN 572139-01-10 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 33C600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA ORPRE 4843750000 FHI: 20000 FCOR50000 FHR 572139-01-4 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 32A600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. ORPOST4843750000 FHORI: 20000 FCGROUP 33CORPOST4843750000 FHORGROUP 33DPOST48437572139-01-5 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33A600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OROR50000 FHGROUP 33BI: 20000 FCOR50000 FH572139-01-6 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 161APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572139-01-7 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCZL-500-02-1 GROUP 33D600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. ORPRE 4843750000 FHI: 20000 FCOR50000 FH572139-01-8 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 17000 FCZL-500-02-1 GROUP 32E600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. OROR50000 FHGROUP 33EI: 17000 FCOR50000 FHN 572139-01-9 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 20000 FCGROUP 32A600 UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA. ORPRE 4843750000 FHI: 20000 FCOR50000 FHR 572140-01-4 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 32A541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR ORPRE 48437541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH541PB 541QB 541RB I: 8700 FC541SB 641EB 641FB OR641GB 641HB 641JB 39600 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SBR 572140-01-5 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33A541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OROR541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FHGROUP 33B541PB 541QB 541RB I: 8900 FC541SB 641EB 641FB OR641GB 641HB 641JB 26400 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 162APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572140-01-6 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33C541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR OR541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH541PB 541QB 541RB I: 10600 FC541SB 641EB 641FB OR641GB 641HB 641JB 33800 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-01-7 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 17000 FCGROUP 32E541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT OROR541LB 541MB 541NB STR 12 AND 19 AND ALL STRINGER JOINTS. 50000 FHGROUP 33E541PB 541QB 541RB I: 17000 FC541SB 641EB 641FB OR641GB 641HB 641JB 50000 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-01-8 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33D541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR ORPRE 48437541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FH541PB 541QB 541RB I: 9900 FC541SB 641EB 641FB OR641GB 641HB 641JB 31600 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB572140-01-9 541EB 541FB 541GB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 32A541HB 541JB 541KB 641 BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR ORPOST 48437541LB 541MB 541NB 12 AND 19 AND ALL STRINGER JOINTS. 50000 FHOR541PB 541QB 541RB I: 20000 FCGROUP 33D541SB 641EB 641FB ORPOST 48437641GB 641HB 641JB 50000 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 163APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572140-02-2 541EB 541FB 541GB 541 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541HB 541JB 541KB 641 STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING I: 12 YE541LB 541MB 541NB BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SBR 572141-01-4 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 32A542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR ORPRE 48437542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH542KB 550AB 550BB 650 I: 10000 FC550CB 550DB 550EB OR550FB 642AB 642BB 45300 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBR 572141-01-5 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33A542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OROR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FHGROUP 33B542KB 550AB 550BB 650 I: 12600 FC550CB 550DB 550EB OR550FB 642AB 642BB 37600 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 164APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572141-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33C542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH542KB 550AB 550BB 650 I: 13000 FC550CB 550DB 550EB OR550FB 642AB 642BB 41400 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572141-01-7 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 17000 FCGROUP 32E542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR OROR542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FHGROUP 33E542KB 550AB 550BB 650 I: 17000 FC550CB 550DB 550EB OR550FB 642AB 642BB 50000 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBR 572141-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 33D542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR ORPRE 48437542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FH542KB 550AB 550BB 650 I: 11000 FC550CB 550DB 550EB OR550FB 642AB 642BB 32600 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 165APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572141-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS T: 20000 FCGROUP 32A542DB 542EB 542FB 550 BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR ORPOST 48437542GB 542HB 542JB 642 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24. 50000 FHOR542KB 550AB 550BB 650 I: 20000 FCGROUP 33D550CB 550DB 550EB ORPOST 48437550FB 642AB 642BB 50000 FH642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572141-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL542DB 542EB 542FB 550 STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING I: 12 YEZL-550-01-1542GB 542HB 542JB 642 BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN542KB 550AB 550BB 650 RIB BAY 23-24.550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572142-01-1 N/A TASK DELETED572143-01-1 N/A TASK DELETEDN 572144-01-10 542EB 642EB 500 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FCGROUP 33C600 SURFACE AT CHORDWISE JOINT AT RIB 27. ORPRE 4843750000 FHI: 20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 166APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572144-01-4 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FCGROUP 32A642 SURFACE AT CHORDWISE JOINT AT RIB 27. ORPOST4843750000 FHORI: 20000 FCGROUP 33CORPOST4843750000 FHORGROUP 33DPOST48437572144-01-5 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FCGROUP 33A642 SURFACE AT CHORDWISE JOINT AT RIB 27. OROR50000 FHGROUP 33BI: 20000 FCOR50000 FH572144-01-6 N/A TASK DELETED572144-01-7 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FCGROUP 33D642 SURFACE AT CHORDWISE JOINT AT RIB 27. ORPRE 4843750000 FHI: 20000 FCOR50000 FH572144-01-8 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 17000 FCGROUP 32E642 SURFACE AT CHORDWISE JOINT AT RIB 27. OROR50000 FHGROUP 33EI: 17000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 167APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572144-01-9 542EB 642EB 542 DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER T: 20000 FCGROUP 32A642 SURFACE AT CHORDWISE JOINT AT RIB 27 ORPRE 4843750000 FHI: 20000 FCOR50000 FH572144-02-2 542EB 642EB 542 GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL642 LOWER SURFACE AT CHORDWISE JOINT AT RIB 27. I: 12 YE572147-01-2 541SB 641SB 541 DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL T: 12 YE NO CPCP MSN 0012641 REFUELLING APERTURE REINFORCING PLATE IN RIB BAY I: 12 YE22-23.572148-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. ORPOST 4843750000 FHI: 16400 FCOR45700 FH572148-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. ORPOST 4843750000 FHI: 20000 FCOR50000 FHR 572148-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. ORPRE 4843750000 FHI: 9900 FCOR45200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 168APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572148-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OROR50000 FHGROUP 33BI: 13000 FCOR38500 FHR 572148-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. ORPRE 4843750000 FHI: 11200 FCOR33300 FHR 572148-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. ORPRE 4843750000 FHI: 10200 FCOR30100 FH572148-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR50000 FHI: 15500 FCOR44200 FH572148-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. OR50000 FHI: 13100 FCOR50000 FH572148-02-2 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL642EB 642 STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS. I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 169APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572149-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEPOST 48437AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 17200 FCOR47800 FH572149-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 32A600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEPOST 48437AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 20000 FCOR50000 FHN 572149-01-12 N/A 500 DTEAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 6 YE NO CPCP A330-200F600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REARSPAR, 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 CPCP GROUP 32A600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEPRE 48437AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 6900 FCOR27700 FH572149-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33A600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEORAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHGROUP 33BSPAR, BETWEEN RIBS 23 AND 39. I: 9900 FCOR31000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 170APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572149-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33C600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 7000 FCOR21900 FH572149-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO CPCP GROUP 32E600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 13700 FCOR50000 FH572149-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 17000 FC T: 6 YE NO CPCP GROUP 33E600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEAND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR 50000 FHSPAR, BETWEEN RIBS 23 AND 39. I: 16200 FCOR46200 FH572149-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, MLI HOLES OR I: 6 YEPRE 48437AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD 50000 FHOF REAR SPAR, BETWEEN RIBS 23 AND 39. I: 6300 FCOR19700 FH572151-01-1 574AT 574BB 574CB 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP ALL574DB 574EB 574FB 674 BETWEEN RIB 12 AND RIB 27. I: 12 YE I: 12 YE574GB 574HB 574JB574KB 574LB 574MB574NB 674AT 674BB674CB 674DB 674EB674FB 674GB 674HB674JB 674KB 674LB674MB 674NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 171APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572152-01-1 574AT 575AT 575BT 575 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP ALL591AB 591BB 591CB 675 BETWEEN RIB 27 AND RIB 39. I: 12 YE I: 12 YE591DB 592AB 592BB592CB 592DB 674AT675AT 675BT 691AB691BB 691CB 691DB692AB 692BB 692CB692DB572153-01-1 N/A TASK DELETED572153-01-10 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FCGROUP 32E575 JOINT PLATE AT RIB 27. OR674 50000 FH675 I: 8600 FCOR50000 FH572153-01-11 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33D575 JOINT PLATE AT RIB 27. ORPOST 48437674 50000 FH675 I: 10900 FCOR30400 FHR 572153-01-12 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 32A575 JOINT PLATE AT RIB 27. ORPOST 48437674 118100 FH675 I: 8600 FCOR50800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 172APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572153-01-4 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 32A575 JOINT PLATE AT RIB 27. ORPRE 48437674 50000 FH675 I: 10300 FCOR47600 FHR 572153-01-5 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33A575 JOINT PLATE AT RIB 27. OROR674 50000 FHGROUP 33B675 I: 5800 FCOR18500 FHR 572153-01-6 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 20000 FCGROUP 33C575 JOINT PLATE AT RIB 27. ORPRE 48437674 50000 FH675 I: 11100 FCOR35600 FH572153-01-7 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 12 YE T: 20 YE CPCP ALL575 JOINT PLATE AT RIB 27. I: 12 YE I: 12 YE674675R 572153-01-8 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR T: 20000 FCGROUP 33D575 SPAR AFT FACE JOINT PLATE AT RIB 27. ORPRE 48437674 50000 FH675 I: 9400 FCOR30000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 173APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572153-01-9 574AT 674AT 574 DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE T: 17000 FCGROUP 33E575 JOINT PLATE AT RIB 27. OR674 50000 FH675 I: 10000 FCOR31500 FH572154-01-1 N/A TASK DELETEDR 572154-01-10 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 33D541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND ORPRE 48437541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH541QB 541RB 541SB 642 I: 9700 FC542AB 542BB 542CB OR542DB 542EB 542GB 31200 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GB572154-01-11 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP ALL541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND I: 12 YE I: 12 YE541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.541QB 541RB 541SB 642542AB 542BB 542CB542DB 542EB 542GB641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 174APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572154-01-12 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 33C541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND ORPRE 48437541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH541QB 541RB 541SB 642 I: 10300 FC542AB 542BB 542CB OR542DB 542EB 542GB 32900 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GBR 572154-01-4 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 32A541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND ORPRE 48437541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH541QB 541RB 541SB 642 I: 9400 FC542AB 542BB 542CB OR542DB 542EB 542GB 43300 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GBR 572154-01-5 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 33A541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OROR541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FHGROUP 33B541QB 541RB 541SB 642 I: 7800 FC542AB 542BB 542CB OR542DB 542EB 542GB 24900 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 175APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572154-01-6 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 20000 FCGROUP 33C541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND ORPOST 48437541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 62700 FHOR541QB 541RB 541SB 642 I: 17200 FCGROUP 33D542AB 542BB 542CB ORPOST 48437542DB 542EB 542GB 54000 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GB572154-01-7 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FCGROUP 33E541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH541QB 541RB 541SB 642 I: 17000 FC542AB 542BB 542CB OR542DB 542EB 542GB 50000 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GB572154-01-8 541FB 541GB 541HB 541 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 17000 FCGROUP 32E541JB 541KB 541LB 542 FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND OR541MB 541NB 541PB 641 BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27. 50000 FH541QB 541RB 541SB 642 I: 17000 FC542AB 542BB 542CB OR542DB 542EB 542GB 50000 FH641FB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642GBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 176APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572155-01-1 542HB 542JB 542KB 542 DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD T: 12 YE T: 20 YE NO CPCP ALL550AB 550BB 550CB 550 FACE BETWEEN RIB 30 AND RIB 39. I: 12 YE I: 12 YE550DB 550EB 550FB 642642HB 642JB 642KB 650650AB 650BB 650CB650DB 650EB 650FB572156-01-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORPOST 48437SEALANT REMOVAL AS 50000 FHPER NTM I: 13600 FCOR38000 FH572156-01-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32A642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORPOST 48437SEALANT REMOVAL AS 50000 FHPER NTM I: 20000 FCOR50000 FH572156-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 32A642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORPRE 48437SEALANT REMOVAL AS 50000 FHPER NTM I: 11600 FCOR41700 FH572156-01-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33A642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORORSEALANT REMOVAL AS 50000 FHGROUP 33BPER NTM I: 6200 FCOR20000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 177APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572156-01-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33C642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORSEALANT REMOVAL AS 50000 FHPER NTM I: 10800 FCOR34700 FH572156-01-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 33E642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORSEALANT REMOVAL AS 50000 FHPER NTM I: 12500 FCOR39300 FH572156-01-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 17000 FCGROUP 32E642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORSEALANT REMOVAL AS 50000 FHPER NTM I: 10800 FCOR50000 FH572156-01-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR T: 20000 FCGROUP 33D642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORPRE 48437SEALANT REMOVAL AS 50000 FHPER NTM I: 9100 FCOR29300 FHR 572158-01-10 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 ORPRE 48437541NB 541PB 541QB AND RIB 23. 50000 FH541RB 541SB 641GB I: 5500 FC641HB 641JB 641KB OR641LB 641MB 641NB 16500 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 178APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572158-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 ORPOST 48437541NB 541PB 541QB AND RIB 23. 50000 FH541RB 541SB 641GB I: 15700 FC641HB 641JB 641KB OR641LB 641MB 641NB 43800 FH641PB 641QB 641RB641SB572158-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND ORPOST 48437541NB 541PB 541QB RIB 23. 50000 FH541RB 541SB 641GB I: 12500 FC641HB 641JB 641KB OR641LB 641MB 641NB 50000 FH641PB 641QB 641RB641SBR 572158-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND ORPRE 48437541NB 541PB 541QB RIB 23. 50000 FH541RB 541SB 641GB I: 5300 FC641HB 641JB 641KB OR641LB 641MB 641NB 24300 FH641PB 641QB 641RB641SBR 572158-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OROR541NB 541PB 541QB RIB 23. 50000 FHGROUP 33B541RB 541SB 641GB I: 6900 FC641HB 641JB 641KB OR641LB 641MB 641NB 20500 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 179APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572158-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND OR541NB 541PB 541QB RIB 23. 50000 FH541RB 541SB 641GB I: 6300 FC641HB 641JB 641KB OR641LB 641MB 641NB 19700 FH641PB 641QB 641RB641SB572158-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 OR541NB 541PB 541QB AND RIB 23. 50000 FH541RB 541SB 641GB I: 14900 FC641HB 641JB 641KB OR641LB 641MB 641NB 42300 FH641PB 641QB 641RB641SB572158-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN OR541NB 541PB 541QB RIB 12 AND RIB 23. 50000 FH541RB 541SB 641GB I: 12600 FC641HB 641JB 641KB OR641LB 641MB 641NB 50000 FH641PB 641QB 641RB641SB572158-02-2 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541KB 541LB 541MB 641 BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND I: 12 YE541NB 541PB 541QB RIB 23.541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 180APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572159-01-10 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. ORPOST 4843750000 FHI: 15700 FCOR43800 FH572159-01-11 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. ORPOST 4843750000 FHI: 12500 FCOR50000 FHR 572159-01-4 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. ORPRE 4843750000 FHI: 5700 FCOR26100 FHR 572159-01-5 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OROR50000 FHGROUP 33BI: 8100 FCOR23900 FH572159-01-6 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR50000 FHI: 6800 FCOR21300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 181APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572159-01-7 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR50000 FHI: 14900 FCOR42300 FH572159-01-8 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. OR50000 FHI: 12600 FCOR50000 FHR 572159-01-9 542AB 542BB 542CB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. ORPRE 4843750000 FHI: 6000 FCOR17700 FH572159-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL642AB 642BB 642CB 642 BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26. I: 12 YE572161-01-1 522EB 522FB 522GB 522 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP ALL522HB 522JB 522KB 523 FACE BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE. I: 6 YE I: 6 YE522LB 522MB 522NB 622522PB 522RB 522SB 623522TB 523AB 523BB523CB 523DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 622TB623AB 623BB 623CB623DB572162-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 182APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572162-01-4 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 32A623 FACE SPAR JOINT PLATE AT RIB 27. OR I: 6 YEOR20000 FCGROUP 33COROR50000 FHGROUP 33DI: 6 YEOR20000 FCOR50000 FHR 572162-01-5 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 20000 FCGROUP 33A623 FACE SPAR JOINT PLATE AT RIB 27. OROR50000 FHGROUP 33BI: 14600 FCOR46800 FH572162-01-6 N/A TASK DELETED572162-01-7 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 32E623 FACE SPAR JOINT PLATE AT RIB 27. OR I: 6 YEOR17000 FCGROUP 33EOR50000 FHI: 6 YEOR17000 FCOR50000 FHR 572162-01-8 523CB 623CB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP GROUP 33A623 FACE SPAR JOINT PLATE AT RIB 27. I: 6 YE I: 6 YEORGROUP 33BORGROUP 32FISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 183APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572163-01-1 523EB 523FB 523GB 523 DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD T: 12 YE T: 20 YE CPCP ALL523HB 523JB 523KB 623 FACE BETWEEN RIB 27 AND RIB 39. I: 6 YE I: 6 YE523LB 523MB 523NB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB572164-01-1 N/A TASK DELETED572164-01-10 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 17000 FCGROUP 32E541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OROR541NB 541PB 541QB 641 FLANGES. 50000 FHGROUP 33E541RB 541SB 542AB 642 I: 17000 FC542BB 542CB 542DB OR641GB 641HB 641JB 50000 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBR 572164-01-11 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM ORPOST 48437541NB 541PB 541QB 641 FLANGES. 50000 FH541RB 541SB 542AB 642 I: 7500 FC542BB 542CB 542DB OR641GB 641HB 641JB 44300 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBN 572164-01-12 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33C541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM ORPOST 48437541NB 541PB 541QB 641 FLANGES 50000 FHOR541RB 541SB 542AB 642 I: 8700 FCGROUP 33D542BB 542CB 542DB ORPOST 48437641GB 641HB 641JB 27400 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 184APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572164-01-5 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 32A541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM ORPRE 48437541NB 541PB 541QB 641 FLANGES. 50000 FH541RB 541SB 542AB 642 I: 7500 FC542BB 542CB 542DB OR641GB 641HB 641JB 34900 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBR 572164-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33A541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM OROR541NB 541PB 541QB 641 FLANGES. 50000 FHGROUP 33B541RB 541SB 542AB 642 I: 6900 FC542BB 542CB 542DB OR641GB 641HB 641JB 22300 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBR 572164-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33C541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM ORPRE 48437541NB 541PB 541QB 641 FLANGES. 50000 FH541RB 541SB 542AB 642 I: 8300 FC542BB 542CB 542DB OR641GB 641HB 641JB 26500 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 185APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572164-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP ALL541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE541NB 541PB 541QB 641 FLANGES.541RB 541SB 542AB 642542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBR 572164-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 20000 FCGROUP 33D541KB 541LB 541MB 542 BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM ORPRE 48437541NB 541PB 541QB 641 FLANGES. 50000 FH541RB 541SB 542AB 642 I: 8100 FC542BB 542CB 542DB OR641GB 641HB 641JB 25900 FH641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572165-01-1 N/A TASK DELETED572165-01-10 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 32A542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEPOST 48437550AB 550BB 550CB 642 FLANGES. 20000 FCOR550DB 550EB 550FB 650 ORGROUP 33D642EB 642FB 642GB 50000 FHPOST 48437642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 186APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 572165-01-11 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP A330-200F542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM I: 12 YE I: 12 YE550AB 550BB 550CB 642 FLANGES.550DB 550EB 550FB 650642AB 642BB 642CB642DB 642EB 642FB642GB 642HB 642JB642KB 650AB 650BB650CB 650DB 650EB650FB572165-01-5 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 32A542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEPRE 48437550AB 550BB 550CB 642 FLANGES. 20000 FC550DB 550EB 550FB 650 OR642EB 642FB 642GB 50000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 8800 FCOR31800 FH572165-01-6 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 33A542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEOR550AB 550BB 550CB 642 FLANGES. 20000 FCGROUP 33B550DB 550EB 550FB 650 OR642EB 642FB 642GB 50000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 7600 FCOR24500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 187APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572165-01-7 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 33C542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YE550AB 550BB 550CB 642 FLANGES. 20000 FC550DB 550EB 550FB 650 OR642EB 642FB 642GB 50000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 8400 FCOR26900 FH572165-01-8 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 32E542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEOR550AB 550BB 550CB 642 FLANGES. 17000 FCGROUP 33E550DB 550EB 550FB 650 OR642EB 642FB 642GB 50000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 17000 FCOR50000 FH572165-01-9 542EB 542FB 542GB 542 DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE T: 12 YE T: 20 YE NO CPCP GROUP 33D542HB 542JB 542KB 550 BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM OR I: 12 YEPRE 48437550AB 550BB 550CB 642 FLANGES. 20000 FC550DB 550EB 550FB 650 OR642EB 642FB 642GB 50000 FH642HB 642JB 642KB I: 12 YE650AB 650BB 650CB OR650DB 650EB 650FB 8200 FCOR26300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 188APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572166-01-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FCGROUP 32A642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORORSEALANT REMOVAL AS 50000 FHGROUP 33CPER NTM I: 20000 FCORORGROUP 33D50000 FHR 572166-01-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 20000 FCGROUP 33A642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORORSEALANT REMOVAL AS 50000 FHGROUP 33BPER NTM I: 14600 FCOR46800 FH572166-01-6 N/A TASK DELETED572166-01-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING FRONT SPAR T: 17000 FCGROUP 32E642EB 642 UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 27. ORORSEALANT REMOVAL AS 50000 FHGROUP 33EPER NTM I: 17000 FCOR50000 FH572171-02-1 541HB 541JB 541KB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 14 TO RIB T: 12 YE T: 20 YE NO CPCP ALL541LB 541MB 541NB 542 39 AT SKIN ATTACHMENTS, SPAR ATTACHMENTS AND REGION I: 12 YE I: 12 YE541PB 541QB 541RB 550 OF STR CUTOUTS EXCLUDING RIBS 18 & 23.541SB 542AB 542BB 641542CB 542DB 542EB 642542FB 542GB 542HB 650542JB 542KB 550AB550BB 550CB 550DB550EB 550FB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 642EB 642FB642GB 642HB 642JB642KB 650AB 650BB650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 189APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572174-01-4 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 32A541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YEOR641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS. 20000 FCGROUP 33C641NB 641SB 642AB 642 OROR50000 FHGROUP 33DI: 12 YEOR20000 FCOR50000 FH572174-01-5 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 33A541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YEOR641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS. 20000 FCGROUP 33B641NB 641SB 642AB 642 OR50000 FHI: 12 YEOR6900 FCOR21900 FH572174-01-6 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP GROUP 32E541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER OR I: 12 YEOR641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS. 17000 FCGROUP 33E641NB 641SB 642AB 642 OR50000 FHI: 12 YEOR17000 FCOR50000 FHN 572174-01-7 541GB 541HB 541MB 541 DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 T: 12 YE T: 20 YE NO CPCP A330-200F541NB 541SB 542AB 542 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER I: 12 YE I: 12 YE641GB 641HB 641MB 641 CUTOUTS AND FORWARD FLAP TRACK BRACKETS641NB 641SB 642AB 642D 572180-01-11 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 190APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSD 572180-01-4 N/A TASK DELETEDD 572180-01-5 N/A TASK DELETEDR 572180-01-6 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. ORPRE 48437541NB 541PB 541QB 50000 FH541RB 541SB 641GB I: 10300 FC641HB 641JB 641KB OR641LB 641MB 641NB 30600 FH641PB 641QB 641RB641SBR 572180-01-7 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. ORPOST 48437541NB 541PB 541QB 50000 FHOR541RB 541SB 641GB I: 8400 FCGROUP 33D641HB 641JB 641KB ORPOST 48437641LB 641MB 641NB 24000 FH641PB 641QB 641RB641SB572180-01-8 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR541NB 541PB 541QB 50000 FH541RB 541SB 641GB I: 8400 FC641HB 641JB 641KB OR641LB 641MB 641NB 24000 FH641PB 641QB 641RB641SBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 191APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572180-01-9 541GB 541HB 541JB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. OR541NB 541PB 541QB 50000 FH541RB 541SB 641GB I: 7100 FC641HB 641JB 641KB OR641LB 641MB 641NB 32100 FH641PB 641QB 641RB641SB572180-02-2 541GB 541HB 541JB 541 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-541-02-1 ALL541KB 541LB 541MB 641 STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. I: 12 YE541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB572181-01-10 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. ORPOST 4843750000 FHI: 8900 FCOR24900 FH572181-01-11 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. ORPOST 4843750000 FHI: 7100 FCOR32200 FHD 572181-01-4 N/A TASK DELETEDD 572181-01-5 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 192APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572181-01-6 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. ORPRE 4843750000 FHI: 10300 FCOR30600 FHD 572181-01-7 N/A TASK DELETED572181-01-8 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR50000 FHI: 8400 FCOR24000 FH572181-01-9 542AB 542BB 542CB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. OR50000 FHI: 7100 FCOR32200 FH572181-02-2 542AB 542BB 542CB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL642AB 642BB 642CB 642 STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26. I: 12 YE572182-01-10 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. ORPOST 48437550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 8900 FC642GB 642HB 642JB OR642KB 650AB 650BB 24900 FH650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 193APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572182-01-11 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. ORPOST 48437550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 7100 FC642GB 642HB 642JB OR642KB 650AB 650BB 32200 FH650CB 650DB 650EB650FB572182-01-4 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. ORPRE 48437550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 6500 FC642GB 642HB 642JB OR642KB 650AB 650BB 26100 FH650CB 650DB 650EB650FB572182-01-5 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OROR550BB 550CB 550DB 642 50000 FHGROUP 33B550EB 550FB 642FB 650 I: 6200 FC642GB 642HB 642JB OR642KB 650AB 650BB 19400 FH650CB 650DB 650EB650FB572182-01-6 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 6500 FC642GB 642HB 642JB OR642KB 650AB 650BB 20300 FH650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 194APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572182-01-7 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 8400 FC642GB 642HB 642JB OR642KB 650AB 650BB 24000 FH650CB 650DB 650EB650FB572182-01-8 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. OR550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 7100 FC642GB 642HB 642JB OR642KB 650AB 650BB 32200 FH650CB 650DB 650EB650FB572182-01-9 542FB 542GB 542HB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. ORPRE 48437550BB 550CB 550DB 642 50000 FH550EB 550FB 642FB 650 I: 6000 FC642GB 642HB 642JB OR642KB 650AB 650BB 18800 FH650CB 650DB 650EB650FB572182-02-2 542FB 542GB 542HB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL542JB 542KB 550AB 550 STRINGERS 15 AND 18 BETWEEN RIB 28 AND RIB 39. I: 12 YEZL-550-01-1550BB 550CB 550DB 642550EB 550FB 642FB 650642GB 642HB 642JB642KB 650AB 650BB650CB 650DB 650EB650FBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 195APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572183-01-10 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPOST 48437STRINGER JOINTS. 50000 FHI: 8900 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-02-10 24900 FH572183-01-11 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPOST 48437STRINGER JOINTS. 50000 FHI: 7100 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-02-11 32200 FH572183-01-4 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPRE 48437STRINGER JOINTS. 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FCTASK 572183-02-4 OR26100 FH572183-01-5 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORORSTRINGER JOINTS. 50000 FHGROUP 33BNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6200 FCTASK 572183-02-5 OR19400 FH572183-01-6 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSTRINGER JOINTS. 50000 FHNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FCTASK 572183-02-6 OR20300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 196APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572183-01-7 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSTRINGER JOINTS. 50000 FHI: 8400 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-02-7 24000 FH572183-01-8 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSTRINGER JOINTS. 50000 FHI: 7100 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME ORAS TASK 572183-02-8 32200 FH572183-01-9 542DB 542EB 642DB 542 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPRE 48437STRINGER JOINTS. 50000 FHI: 5900 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-02-9 18500 FH572183-02-10 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPOST 48437SEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM I: 8900 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-01-10 24900 FH572183-02-11 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPOST 48437SEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM I: 7100 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-01-11 32200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 197APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572183-02-4 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPRE 48437SEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FCTASK 572183-01-4 OR26100 FH572183-02-5 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORORSEALANT REMOVAL AS STRINGER JOINTS. 50000 FHGROUP 33BPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6200 FCTASK 572183-01-5 OR19400 FH572183-02-6 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 6500 FCTASK 572183-01-6 OR20300 FH572183-02-7 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM I: 8400 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-01-7 24000 FH572183-02-8 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORSEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM I: 7100 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-01-8 32200 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 198APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572183-02-9 542DB 542EB 642DB 542 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING ORPRE 48437SEALANT REMOVAL AS STRINGER JOINTS. 50000 FHPER NTM I: 5900 FCNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS ORTASK 572183-01-9 18500 FH572183-03-2 542DB 542EB 642DB 542 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 12 YE NO CPCP ZL-542-01-1 ALL642EB 642 STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING I: 12 YESTRINGER JOINTS.D 572184-01-4 N/A TASK DELETEDD 572184-01-5 N/A TASK DELETEDR 572184-01-6 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. ORPRE 48437NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572184-02-6 I: 5600 FCOR16600 FHD 572184-01-7 N/A TASK DELETED572184-01-8 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32E641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. OROR50000 FHGROUP 33ENOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 17000 FCTASK 572184-02-8 OR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 199APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572184-01-9 541QB 641QB 541 DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. ORPOST 4843750000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 20000 FCGROUP 33DTASK 572184-02-9 ORPOST 4843750000 FHD 572184-02-4 N/A TASK DELETEDD 572184-02-5 N/A TASK DELETEDR 572184-02-6 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33CSEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. ORPRE 48437PER NTM NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS 50000 FHTASK 572184-01-6 I: 5600 FCOR16600 FHD 572184-02-7 N/A TASK DELETED572184-02-8 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 32ESEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. ORORPER NTM 50000 FHGROUP 33ENOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 17000 FCTASK 572184-01-8 OR50000 FH572184-02-9 541QB 641QB 541 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32ASEALANT REMOVAL AS 641 STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21. ORPOST 48437PER NTM 50000 FHORNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS I: 20000 FCGROUP 33DTASK 572184-01-9 ORPOST 4843750000 FH572601-01-2 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE CPCP ZL-571-01-1 ALL671 GEAR SIDE STAY FITTING (RIB 2). I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 200APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572602-01-2 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE CPCP ZL-571-01-1 ALL671 GEAR FORWARD PINTLE FITTING (RIB 5). I: 12 YE572603-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE CPCP ZL-571-01-1 ALL671 GEAR RETRACTION JACK FITTING. I: 12 YE572604-01-1 734 744 571 GENERAL VISUAL INSPECTION OF OUTER WING MAIN LANDING T: 12 YE CPCP ZL-571-01-1 ALL671 GEAR SUPPORT RIB 6. I: 12 YE572605-01-1 N/A TASK DELETED572605-01-3 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 32A673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEPRE 48437AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 20000 FCORAND THRUST PADS). I: 12 YEGROUP 33COR10700 FC572605-01-4 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 33A673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEORAFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 20000 FCGROUP 33BAND THRUST PADS). I: 12 YEOR9200 FC572605-01-5 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 32E673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEORAFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE 17000 FCGROUP 33EAND THRUST PADS). I: 12 YEOR17000 FCISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 201APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572605-01-6 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 33D673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEPRE 48437AFT PICK UP 20000 FC(INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YEPADS). OR10700 FC572605-01-7 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 33D673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEPOST 48437AFT PICK UP 20000 FC(INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YEPADS). OR18400 FC572605-01-8 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP GROUP 32A673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 OR I: 12 YEPOST 48437AFT PICK UP 20000 FC(INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST I: 12 YEPADS). OR20000 FCN 572605-01-9 573BB 573FB 673BB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP A330-200F673FB 673 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 I: 12 YE I: 12 YEAFT PICK UP (INCLUDING BOX BRACKET,INTERFACE PLATEAND THRUST PADS).572606-01-2 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 T: 20000 FCGROUP 32A632CB 633CB 634CB 533 AND 5 AFT PICK-UP, ASSEMBLY. I: 20000 FCPRE 48437534OR632GROUP 33A633OR634GROUP 33BORGROUP 33CPRE 48437572606-01-3 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 202APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572606-01-6 532CB 533CB 534CB 532 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, T: 20000 FCGROUP 33D632CB 633CB 634CB 533 4 AND 5 AFT PICK-UP, ASSEMBLY. I: 17400 FCPRE 48437534632633634572606-02-2 532CB 533CB 534CB 532 GENERAL VISUAL INSPECTION OF OUTER WING FLAP TRACKS T: 12 YE CPCP ZL-531-02-1 ALL632CB 633CB 634CB 533 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. I: 12 YE534632633634572607-01-1 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE CPCP GROUP 32A532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTINGS. OR I: 12 YEOR534AB 534CB 631AB 533 20000 FCGROUP 33A631CB 632AB 632CB 534 I: 12 YEOR633AB 633CB 634AB 631 ORGROUP 33B634CB 632 8300 FCOR633GROUP 33C634ORGROUP 33D572607-01-4 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 T: 12 YE T: 20 YE CPCP GROUP 32E532CB 533AB 533CB 532 AND 5 FORWARD PICK-UP LUGS FITTINGS. OR I: 12 YEOR534AB 534CB 631AB 533 17000 FCGROUP 33E631CB 632AB 632CB 534 I: 12 YE633AB 633CB 634AB 631 OR634CB 632 8300 FC633634N 572607-01-5 531AB 531CB 532AB 531 DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2,3, T: 12 YE T: 20 YE CPCP A330-200F532CB 533AB 533CB 532 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. I: 12 YE I: 12 YE534AB 534CB 631AB 533631CB 632AB 632CB 534633AB 633CB 634AB 631634CB 632633634ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 203APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572608-02-1 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 32A522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. I: 20000 FCPRE 48437622BB 622CTORENGINEGROUP 33ALINKSORSLEEVESGROUP 33BORGROUP 33CORGROUP 33DPRE 48437572608-02-2 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 32E522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR622BB 622CT 50000 FHENGINE I: 8200 FCLINKS ORSLEEVES 48500 FH572608-02-3 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 33E522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. OR622BB 622CT 50000 FHENGINE I: 9600 FCLINKS ORSLEEVES 30200 FH572608-02-5 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33D522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. ORPOST 48437622BB 622CT 50000 FHENGINE I: 10400 FCLINKS ORSLEEVES 28900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 204APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572608-02-6 522AB 522AT 522BB 522 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 32A522CT 622AB 622AT 622 INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTING. ORPOST 48437622BB 622CT 50000 FHENGINE I: 8200 FCLINKS ORSLEEVES 48500 FHR 572610-01-1 453CL 453CR 454BL 541 DETAILED INSPECTION OF OUTER WING PYLON SPIGOT T: 12 YE T: 20 YE NO CPCP A330-200454BR 454CL 454CR 641 FITTING. I: 12 YE I: 12 YEPRE 43271463CL 463CR 464BLOR464BR 464CL 464CRA330-300SPIGOT SLEEVEPRE 43271R 572610-01-2 453CL 453CR 454BL 541 DETAILED INSPECTION OF OUTER WING PYLON SPIGOT T: 12 YE T: 20 YE NO CPCP A330-200454BR 454CL 454NR 641 FITTING. I: 12 YE I: 12 YEPOST 43271463CL 463CR 464BLOR464BR 464CL 464NRA330-200FSPIGOT SLEEVEPOST 43271ORA330-300POST 43271572610-02-10 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33D454NR 464BL 464BR 641 SPIGOT FITTING. ORPOST 48437464CL 464NR 50000 FHI: 10800 FCOR30200 FH572610-02-11 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 32A454CR 464BL 464BR 641 SPIGOT FITTING. ORPOST 48437464CL 464CR 50000 FHI: 8600 FCOR50000 FH572610-02-2 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 32A454CR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FCPRE 48437464CL 464CRISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 205APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572610-02-3 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33A454CR 464BL 464BR 641 SPIGOT FITTING. I: 9000 FCPRE 43271464CL 464CRORGROUP 33BPRE 43271572610-02-4 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33C454NR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FC464CL 464NR572610-02-5 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33A454NR 464BL 464BR 641 SPIGOT FITTING. I: 9000 FCPOST 43271464CL 464NRORGROUP 33BPOST 43271572610-02-8 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 32E454NR 464BL 464BR 641 SPIGOT FITTING. OROR464CL 464NR 50000 FHGROUP 33EI: 17000 FCOR50000 FH572610-02-9 454BL 454BR 454CL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 20000 FCGROUP 33D454NR 464BL 464BR 641 SPIGOT FITTING. I: 11600 FCPRE 48437464CL 464NRR 572612-01-2 454DL 454DR 454FL 541 DETAILED INSPECTION OF OUTER WING PYLON AFT T: 12 YE T: 20 YE NO CPCP A330-200454FR 464DL 464DR 641 ATTACHMENT FITTING. I: 12 YE I: 12 YEPRE 43271464FL 464FRORPIPE SUPPORT BRACKETA330-300PRE 43271ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 206APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572612-01-3 454KL 454KR 454ML 541 DETAILED INSPECTION OF OUTER WING PYLON AFT T: 12 YE T: 20 YE NO CPCP A330-200454MR 464KL 464KR 641 ATTACHMENT FITTING. I: 12 YE I: 12 YEPOST 43271464ML 464MRORPIPE SUPPORT BRACKETA330-200FPOST 43271ORA330-300POST 43271572612-02-1 N/A TASK DELETED572612-02-10 N/A TASK DELETEDR 572612-02-11 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 33E454MR 464BL 464BR 641 AFT ATTACHMENT FITTING. OR464ML 464MR 50000 FHPIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-5 I: 11300 FCOR35500 FH572612-02-12 N/A TASK DELETED572612-02-13 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33D454MR 464BL 464BR 641 ATTACHMENT FITTING. ORPRE 48437464ML 464MR 50000 FHPIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-6 I: 6200 FCOR19800 FH572612-02-14 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 207APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 572612-02-15 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33D454MR 464BL 464BR 641 ATTACHMENT FITTING. ORPOST 48437464ML 464MR 50000 FHPIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-7 I: 12300 FCOR34300 FH572612-02-16 N/A TASK DELETEDR 572612-02-17 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 32A454FR 464BL 464BR 641 ATTACHMENT FITTING. ORPOST 48437464FL 464FR 50000 FHPIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-8 I: 9700 FCOR50000 FH572612-02-18 N/A TASK DELETED572612-02-3 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 32A454FR 464BL 464BR 641 ATTACHMENT FITTING. ORPRE 48437464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-1 50000 FHPIPE SUPPORT BRACKET I: 7800 FCOR24600 FH572612-02-4 N/A TASK DELETED572612-02-5 454BL 454BR 454FL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33A454FR 464BL 464BR 641 ATTACHMENT FITTING. ORPRE 43271464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-2 50000 FHORPIPE SUPPORT BRACKET I: 6400 FCGROUP 33BORPRE 4327120500 FH572612-02-6 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 208APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572612-02-7 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33C454MR 464BL 464BR 641 ATTACHMENT FITTING. OR464ML 464MR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-3 50000 FHPIPE SUPPORT BRACKET I: 6400 FCOR20300 FH572612-02-8 N/A TASK DELETEDR 572612-02-9 454BL 454BR 454ML 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 32E454MR 464BL 464BR 641 AFT ATTACHMENT FITTING. OR464ML 464MR 50000 FHPIPE SUPPORT BRACKET NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-03-4 I: 9700 FCOR50000 FH572612-03-1 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 32A454DR 454FL 454FR 641 ATTACHMENT FITTING. ORPRE 48437464CL 464CR 464DL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-3 50000 FH464DR 464FL 464FR I: 17500 FCBEARING REMOVAL ORENGINE, LINKS AND 50000 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572612-03-2 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33A454DR 454FL 454FR 641 ATTACHMENT FITTING. ORPRE 43271464CL 464CR 464DL NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-5 50000 FHOR464DR 464FL 464FR I: 14500 FCGROUP 33BBEARING REMOVAL ORPRE 43271ENGINE, LINKS AND 45900 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 209APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572612-03-3 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33C454ML 454MR 454NR 641 ATTACHMENT FITTING. OR464CL 464KL 464KR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-7 50000 FH464ML 464MR 464NR I: 14400 FCBEARING REMOVAL ORENGINE, LINKS AND 45600 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572612-03-4 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON T: 17000 FCGROUP 32E454ML 454MR 454NR 641 AFT ATTACHMENT FITTING. OR464CL 464KL 464KR 50000 FH464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572612-02-9 I: 17000 FCBEARING REMOVAL ORENGINE, LINKS AND 50000 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572612-03-5 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 17000 FCGROUP 33E454ML 454MR 454NR 641 ATTACHMENT FITTING. OR464CL 464KL 464KR 50000 FH464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 17000 FCBEARING REMOVAL TASK 572612-02-11 ORENGINE, LINKS AND 50000 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572612-03-6 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33D454ML 454MR 454NR 641 ATTACHMENT FITTING. ORPRE 48437464CL 464KL 464KR 50000 FH464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 14000 FCBEARING REMOVAL TASK 572612-02-13 ORENGINE, LINKS AND 44400 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 210APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS572612-03-7 454CL 454KL 454KR 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 33D454ML 454MR 454NR 641 ATTACHMENT FITTING. ORPOST 48437464CL 464KL 464KR 50000 FH464ML 464MR 464NR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 20000 FCBEARING REMOVAL TASK 572612-02-15 ORENGINE, LINKS AND 50000 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572612-03-8 454CL 454CR 454DL 541 SPECIAL DETAILED INSPECTION OF OUTER WING PYLON AFT T: 20000 FCGROUP 32A454DR 454FL 454FR 641 ATTACHMENT FITTING. ORPOST 48437464CL 464CR 464DL 50000 FH464DR 464FL 464FR NOTE: THIS TASK IS AN ALTERNATIVE TO I: 20000 FCBEARING REMOVAL TASK 572612-02-17 ORENGINE, LINKS AND 50000 FHSLEEVES, PIPESUPPORT BRACKETREMOVED / DISPLACED572614-01-2 N/A TASK DELETED572614-02-1 733 743 733 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR HINGED T: 6 YE CPCP ZL-732-01-1 ALL743 DOOR FORWARD AND AFT SWAN-NECK HINGES. I: 6 YEZL-733-01-1572615-01-2 N/A TASK DELETED572615-02-1 732 742 732 GENERAL VISUAL INSPECTION OF MAIN LANDING GEAR LEG T: 6 YE CPCP ZL-732-01-1 ALL742 FAIRING ATTACHMENT ASSEMBLIES TO LEG STRUCTURE. I: 6 YEN 572617-01-1 734 744 571 DETAILED INSPECTION OF OUTER WING MAIN LANDING GEAR T: 12 YE CPCP A330-200671 SUPPORT RIB 6 BEARING LUGS. I: 12 YEPOST 49353ORA330-200FPOST 49353ORA330-300POST 49353ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 211APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS573001-01-1 N/A TASK DELETEDR 573001-01-10 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 33D635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPRE 48437REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 5700 FCOR18300 FH573001-01-11 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 17000 FCGROUP 32E635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 9100 FCOR50000 FH573001-01-12 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 17000 FCGROUP 33E635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 10600 FCOR33200 FH573001-01-13 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 33D635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPOST 48437REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 11500 FCOR32000 FH573001-01-14 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 32A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPOST 48437REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 9100 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 212APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 573001-01-5 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 32A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPRE 48437REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 5300 FCOR24400 FH573001-01-6 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 33A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPRE 41460REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 10700 FCOR33800 FHR 573001-01-7 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 33A635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPOST 41460REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHORI: 5600 FCGROUP 33BOR18000 FHR 573001-01-8 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 20000 FCGROUP 33C635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND ORPRE 48437REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS. 50000 FHI: 5800 FCOR18700 FH573001-01-9 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT T: 12 YE T: 20 YE CPCP ALL635BZ 635 AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND I: 12 YE I: 12 YEREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 213APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS573002-01-10 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 17000 FCGROUP 32E600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR50000 FHI: 9100 FCOR50000 FH573002-01-11 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 17000 FCGROUP 33E600 SURFACE AND BOTTOM SKIN LOWER SURFACE. OR50000 FHI: 10600 FCOR33200 FH573002-01-12 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPOST 4843750000 FHI: 11500 FCOR32000 FH573002-01-13 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPOST 4843750000 FHI: 9100 FCOR50000 FHR 573002-01-5 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 32A600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPRE 4843750000 FHI: 5300 FCOR24400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 214APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS573002-01-6 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPRE 4146050000 FHI: 10700 FCOR33800 FHR 573002-01-7 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 33A600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPOST 4146050000 FHORI: 5600 FCGROUP 33BOR18000 FHR 573002-01-8 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 33C600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPRE 4843750000 FHI: 5800 FCOR18700 FHR 573002-01-9 N/A 500 DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER T: 20000 FCGROUP 33D600 SURFACE AND BOTTOM SKIN LOWER SURFACE. ORPRE 4843750000 FHI: 5700 FCOR18300 FH573002-02-2 N/A 500 GENERAL VISUAL INSPECTION OF WINGTIP BOX TOP SKIN T: 6 YE NO CPCP ZL-500-02-1 ALL600 UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. I: 6 YE573003-01-1 WINGLET 535 DETAILED INSPECTION OF WINGTIP TO WINGLET FORWARD AND T: 12 YE T: 20 YE CPCP ALL635 AFT LUGS (BOTH ON WINGTIP AND WINGLET). I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 215APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 573003-02-10 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 33D635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). ORPRE 4843750000 FHI: 5100 FCOR16500 FHN 573003-02-11 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 33C635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). ORPRE 4843850000 FHI: 5200 FCOR16800 FHR 573003-02-4 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 32A635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). ORPRE 4843750000 FHI: 4700 FCOR21900 FHR 573003-02-5 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 33A635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OROR50000 FHGROUP 33BI: 6800 FCOR21800 FHR 573003-02-6 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 33C635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). ORPOST 4843750000 FHORI: 8200 FCGROUP 33DORPOST 4843725800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 216APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 573003-02-7 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 17000 FCGROUP 33E635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR50000 FHI: 17000 FCOR50000 FHR 573003-02-8 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 17000 FCGROUP 32E635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). OR99800 FHI: 14900 FCOR87500 FH573003-02-9 WINGLET 535 SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET T: 20000 FCGROUP 32A635 FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). ORPOST 4843750000 FHI: 7100 FCOR41600 FH573004-01-1 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE CPCP GROUP 32A635BZ 635 FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YEPRE 48437ORGROUP 33AORGROUP 33CORGROUP 33DPRE 48437ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 217APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS573004-01-2 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE CPCP GROUP 32E635BZ 635 FLANGE TO SKIN ATTACHMENT. OR I: 12 YEOR17000 FCGROUP 33EOR50000 FHI: 12 YEOR17000 FCOR50000 FH573004-01-3 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE CPCP GROUP 32A635BZ 635 FLANGE TO SKIN ATTACHMENT. OR I: 12 YEPOST 4843720000 FCORORGROUP 33D50000 FHPOST 48437I: 12 YEOR20000 FCOR50000 FHN 573004-01-4 535AZ 535BZ 635AZ 535 DETAILED INSPECTION OF WINGTIP AFT FITTING BOTTOM T: 12 YE T: 20 YE CPCP A330-200F635BZ 635 FLANGE TO SKIN ATTACHMENT. I: 12 YE I: 12 YE573005-01-1 535AB 535BB 635AB 535 DETAILED INSPECTION OF WINGTIP TO WINGLET JOINT T: 12 YE CPCP ALL635BB 635 BOLTS. I: 12 YEJOINT BOLTS573006-01-2 N/A 500 GENERAL VISUAL INSPECTION OF WINGLET EXTERNAL T: 5 YE NO CPCP ZL-500-02-1 ALL600 SURFACE. I: 5 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 218APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574101-01-1 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL521GB 521JB 522CB 522 TRACK RIBS 1 TO 16. I: 12 YE I: 12 YE522JB 522LB 522NB 523522RB 522TB 523CB 621523EB 523GB 523JB 622523LB 523NB 621BB 623621CB 621DB 621GB621JB 622CB 622JB622LB 622NB 622RB622TB 623CB 623EB623GB 623JB 623LB623NB574102-01-1 N/A TASK DELETED574102-01-10 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33D521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK ORPRE 48437522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 7200 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 22700 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-11 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33D521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK ORPOST 48437522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 14700 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 41000 FH622JB 622LB 622NB622RB 622TB 623CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 219APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574102-01-12 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 32A521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK ORPOST 48437522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 11700 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 50000 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-4 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 32A521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK ORPRE 48437522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 7600 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 27300 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-5 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33A521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 8100 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 25500 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-6 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33B521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 5700 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 18000 FH622JB 622LB 622NB622RB 622TB 623CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 220APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574102-01-7 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33C521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 7300 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 23000 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-8 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FCGROUP 32E521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 11700 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 50000 FH622JB 622LB 622NB622RB 622TB 623CB574102-01-9 521BB 521CB 521DB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FCGROUP 33E521GB 521JB 522CB 522 LEADING EDGE FORWARD UPPER ROLLER PIN HOLES IN TRACK OR522JB 522LB 522NB 523 RIBS 1 TO TRACK RIB 11. 50000 FH522RB 522TB 523CB 621 I: 13600 FC621BB 621CB 621DB 622 OR621GB 621JB 622CB 623 42500 FH622JB 622LB 622NB622RB 622TB 623CBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 221APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574103-02-1 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YEPRE 48437522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 13600 FC622JB 622NB 622RB OR622UB 623AB 623BB 48900 FH574103-02-2 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33A522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YEOR522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FCGROUP 33B522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 10300 FC622JB 622NB 622RB OR622UB 623AB 623BB 32500 FH574103-02-3 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33C522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YE522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 13100 FC622JB 622NB 622RB OR622UB 623AB 623BB 41300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 222APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574103-02-4 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32E522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YE522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 17000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 9000 FC622JB 622NB 622RB OR622UB 623AB 623BB 50000 FH574103-02-5 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33E522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YE522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 17000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 10400 FC622JB 622NB 622RB OR622UB 623AB 623BB 32800 FH574103-02-6 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YEPRE 48437522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 12900 FC622JB 622NB 622RB OR622UB 623AB 623BB 40700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 223APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574103-02-7 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YEPOST 48437522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 11300 FC622JB 622NB 622RB OR622UB 623AB 623BB 31600 FH574103-02-8 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING OR I: 12 YEPOST 48437522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. 20000 FC522JB 522NB 522RB 621 OR522UB 523AB 523BB 622 50000 FH621DB 621FB 621GB 623 I: 12 YE622AB 622BB 622CB OR622EB 622GB 622HB 9000 FC622JB 622NB 622RB OR622UB 623AB 623BB 50000 FHN 574103-02-9 521DB 521FB 521GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A330-200F522AB 522BB 522CB 522 CUTOUTS IN ALL INTERMEDIATE RIBS (INCLUDING CLOSING I: 12 YE I: 12 YE522EB 522GB 522HB 523 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.522JB 522NB 522RB 621522UB 523AB 523BB 622621DB 621FB 621GB 623622AB 622BB 622CB622EB 622GB 622HB622JB 622NB 622RB622UB 623AB 623BB574104-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 224APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-10 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. ORPOST 48437521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 12400 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 34500 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 225APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-11 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. ORPOST 48437521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 9800 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 50000 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 226APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. ORPRE 48437521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 7800 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 28000 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 227APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33A521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OROR521GB 521HB 521JB 523 50000 FHGROUP 33B522AB 522BB 522CB 621 I: 5900 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 18600 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 228APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-6 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33C521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 7500 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 23600 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 229APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-7 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 9800 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 50000 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 230APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-8 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 33E521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. OR521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 11400 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 35800 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 231APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574104-01-9 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D521DB 521EB 521FB 522 TRACK RIBS PINION AND ACTUATOR BOLT HOLES. ORPRE 48437521GB 521HB 521JB 523 50000 FH522AB 522BB 522CB 621 I: 7400 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 23300 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PB574105-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 232APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574105-01-10 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YEPOST 48437522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 14300 FC622LB 622NB 622RB OR622TB 623CB 623GB 39700 FH623JB 623LB 623NB574105-01-11 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YEPOST 48437522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 11300 FC622LB 622NB 622RB OR622TB 623CB 623GB 50000 FH623JB 623LB 623NBN 574105-01-12 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A330-200F521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. I: 12 YE I: 12 YE522JB 522LB 522NB 523522RB 522TB 523CB 621523EB 523GB 523JB 622523LB 523NB 621BB 623621CB 621DB 621GB621JB 622CB 622JB622LB 622NB 622RB622TB 623CB 623GB623JB 623LB 623NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 233APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574105-01-3 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YEPRE 48437522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 7600 FC622LB 622NB 622RB OR622TB 623CB 623EB 27300 FH623GB 623JB 623LB623NB574105-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33A521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE522JB 522LB 522NB 523 20000 FC522RB 523CB 523DB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 5800 FC622LB 622NB 622RB OR622TB 623CB 623EB 18300 FH623GB 623JB 623LB623NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 234APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574105-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33B521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 6800 FC622LB 622NB 622RB OR622TB 623CB 623EB 21400 FH623GB 623JB 623LB623NB574105-01-6 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33C521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 7300 FC622LB 622NB 622RB OR622TB 623CB 623GB 23000 FH623JB 623LB 623NB574105-01-7 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32E521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE522JB 522LB 522NB 523 17000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 11300 FC622LB 622NB 622RB OR622TB 623CB 623GB 50000 FH623JB 623LB 623NBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 235APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574105-01-8 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33E521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YE522JB 522LB 522NB 523 17000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 13100 FC622LB 622NB 622RB OR622TB 623CB 623GB 41100 FH623JB 623LB 623NB574105-01-9 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D521GB 521JB 522CB 522 BOTTOM SPREADER PLATE ON TRACK RIB 1 TO TRACK RIB 16. OR I: 12 YEPRE 48437522JB 522LB 522NB 523 20000 FC522RB 522TB 523CB 621 OR523EB 523GB 523JB 622 50000 FH523LB 523NB 621BB 623 I: 12 YE621CB 621DB 621GB OR621JB 622CB 622JB 7200 FC622LB 622NB 622RB OR622TB 623CB 623GB 22700 FH623JB 623LB 623NB574106-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 236APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-10 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK I: 12 YE I: 12 YE521HB 521JB 522AB 523 RIB 16.522BB 522CB 522DB 621522EB 522FB 522GB 622522HB 522JB 522KB 623522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 237APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-11 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK ORPOST 48437521HB 521JB 522AB 523 RIB 16. 50000 FHOR522BB 522CB 522DB 621 I: 20000 FCGROUP 33D522EB 522FB 522GB 622 ORPOST 48437522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 238APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-4 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK ORPRE 48437521HB 521JB 522AB 523 RIB 16. 50000 FH522BB 522CB 522DB 621 I: 20000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 239APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-5 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33A521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OROR521HB 521JB 522AB 523 RIB 16. 50000 FHGROUP 33B522BB 522CB 522DB 621 I: 20000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 240APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-6 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33C521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK ORPRE 48437521HB 521JB 522AB 523 RIB 16. 50000 FH522BB 522CB 522DB 621 I: 20000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 241APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-7 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR521HB 521JB 522AB 523 RIB 16. 50000 FH522BB 522CB 522DB 621 I: 17000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 242APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-8 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK ORPRE 48437521HB 521JB 522AB 523 RIB 16. 50000 FH522BB 522CB 522DB 621 I: 20000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 243APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574106-01-9 521BB 521CB 521DB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 33E521EB 521FB 521GB 522 BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK OR521HB 521JB 522AB 523 RIB 16. 50000 FH522BB 522CB 522DB 621 I: 17000 FC522EB 522FB 522GB 622 OR522HB 522JB 522KB 623 50000 FH522LB 522MB 522NB522PB 522RB 522SB523CB 523DB 523EB523FB 523GB 523HB523JB 523KB 523LB523MB 523NB 523PB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622RB 622SB623CB 623DB 623EB623FB 623GB 623HB623JB 623KB 623LB623MB 623NB 623PB574107-01-2 521FB 521GB 521HB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL521JB 522AB 522BB 522 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YE522CB 522DB 522EB 523 RIB 3 TO TRACK RIB 12.522FB 522GB 522HB 621522JB 522KB 522LB 622522MB 522NB 522PB 623522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 244APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574107-02-10 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33D521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT ORPOST 48437522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 10400 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 28900 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EB574107-02-11 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 32A521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT ORPOST 48437522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 8200 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 48500 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 245APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574107-02-4 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 32A521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT ORPRE 48437522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 92400 FH522FB 522GB 522HB 621 I: 14100 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 65200 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EBR 574107-02-5 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33A521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OROR522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FHGROUP 33B522FB 522GB 522HB 621 I: 12500 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 40000 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 246APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574107-02-6 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33C521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 16000 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 50000 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EB574107-02-7 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FCGROUP 32E521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 8200 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 48500 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 247APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574107-02-8 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 17000 FCGROUP 33E521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT OR522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 9600 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 30000 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EB574107-02-9 521FB 521GB 521HB 521 SPECIAL DETAILED INSPECTION OF OUTER WING FIXED T: 20000 FCGROUP 33D521JB 522AB 522BB 522 LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT ORPRE 48437522CB 522DB 522EB 523 STRAPS AT TRACK RIB 3 TO TRACK RIB 12. 50000 FH522FB 522GB 522HB 621 I: 15500 FC522JB 522KB 522LB 622 OR522MB 522NB 522PB 623 48900 FH522RB 522SB 523CB523DB 523EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622KB 622LB 622MB622NB 622PB 622RB622SB 623CB 623DB623EB574108-01-1 521AB 621AB 521 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 12 YE CPCP ZL-521-01-1 ALL621 EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAIN I: 12 YEZL-522-01-1ATTACHMENTS TO FRONT SPAR AND FUSELAGE.574109-02-1 N/A TASK DELETED574109-02-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 248APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574109-02-3 N/A TASK DELETED574109-02-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 33E521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT OR521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING 50000 FH522AB 522BB 522CB 621 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. I: 8600 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 27100 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 249APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574109-02-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT OR521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING 50000 FH522AB 522BB 522CB 621 RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS. I: 7400 FC522DB 522EB 522FB 622 OR522GB 522HB 522JB 623 43700 FH522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 250APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574109-02-8 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL521DB 521EB 521FB 522 BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT I: 12 YE I: 12 YE521GB 521HB 521JB 523 STRAPS ON ALL INTERMEDIATE RIBS522AB 522BB 522CB 621 (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT522DB 522EB 522FB 622 HOLD DOWN RIBS.522GB 522HB 522JB 623522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PB574110-02-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 32A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YEPRE 48437SPAR FROM RIB 1 TO RIB 9. 50000 FHI: 17700 FCOR50000 FH574110-02-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 33A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YEORSPAR FROM RIB 1 TO RIB 9. 50000 FHGROUP 33BI: 6000 FCOR18800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 251APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574110-02-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 33C600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YESPAR FROM RIB 1 TO RIB 9. 50000 FHI: 16800 FCOR50000 FH574110-02-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC T: 6 YE NO CPCP GROUP 32E600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YESPAR FROM RIB 1 TO RIB 9. 50000 FHI: 16200 FCOR50000 FH574110-02-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FC T: 6 YE NO CPCP GROUP 33E600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YESPAR FROM RIB 1 TO RIB 9. 50000 FHI: 17000 FCOR50000 FH574110-02-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YEPRE 48437SPAR FROM RIB 1 TO RIB 9. 50000 FHI: 16100 FCOR50000 FH574110-02-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 33D600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YEPOST 48437SPAR FROM RIB 1 TO RIB 9. 50000 FHI: 20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 252APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574110-02-8 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FC T: 6 YE NO CPCP GROUP 32A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT OR I: 6 YEPOST 48437SPAR FROM RIB 1 TO RIB 9. 50000 FHI: 16200 FCOR50000 FHN 574110-02-9 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 6 YE NO CPCP A330-200F600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT I: 6 YESPAR FROM RIB 1 TO RIB 9.574111-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR ORPRE 48437FROM RIB 1 TO RIB 39. 50000 FHI: 14800 FCOR50000 FH574111-01-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33A600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR ORORFROM RIB 1 TO RIB 39. 50000 FHGROUP 33BI: 6000 FCOR19000 FH574111-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33C600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR ORFROM RIB 1 TO RIB 39. 50000 FHI: 15300 FCOR48400 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 253APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574111-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR ORORFROM RIB 1 TO RIB 39. 50000 FHGROUP 33EI: 17000 FCOR50000 FH574111-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D600 TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR ORPRE 48437FROM RIB 1 TO RIB 39. 50000 FHI: 13900 FCOR44000 FH574111-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING T: 20000 FCGROUP 32A600 EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD ORPOST 48437OF FRONT SPAR FROM RIB 1 TO RIB 39. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH574111-02-2 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 6 YE NO CPCP ZL-500-02-1 ALL600 EDGE TOP SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT I: 6 YESPAR 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 CPCP ALL623NB 623 HOLD DOWN RIB BETWEEN SLAT TRACK RIB 15 AND SLAT I: 12 YE I: 12 YETRACK 16, AREA OF SLAT TRACK BRAKE FITTINGR 574114-03-1 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORPRE 48437SPAR FROM RIB 11 TO RIB 39. 114600 FHI: 12400 FCOR56600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 254APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574114-03-2 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORORSPAR FROM RIB 11 TO RIB 39. 50000 FHGROUP 33BI: 5500 FCOR16400 FHR 574114-03-3 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33C600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORPRE 48437SPAR FROM RIB 11 TO RIB 39. 50000 FHI: 13900 FCOR41000 FHR 574114-03-4 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORPRE 48437SPAR FROM RIB 11 TO RIB 39. 50000 FHI: 12700 FCOR37500 FH574114-03-5 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORSPAR FROM RIB 11 TO RIB 39. 50000 FHI: 16200 FCOR50000 FH574114-03-6 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 33E600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORSPAR FROM RIB 11 TO RIB 39. 50000 FHI: 17000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 255APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574114-03-7 N/A 500 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A600 BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT ORPOST 48437SPAR FROM RIB 11 TO RIB 39. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH574114-04-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING FIXED LEADING T: 12 YE NO CPCP ZL-500-01-1 ALL600 EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF I: 12 YEFRONT SPAR FROM RIB 11 TO RIB 39.574115-02-1 N/A TASK DELETED574115-02-2 N/A TASK DELETED574115-02-3 N/A TASK DELETED574115-02-4 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT I: 12 YE I: 12 YESPAR BETWEEN RIBS 9 AND 11.574115-02-6 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 32E622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT ORSPAR BETWEEN RIBS 9 AND 11. 50000 FHI: 16200 FCOR50000 FH574115-02-7 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 17000 FCGROUP 33E622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT ORSPAR BETWEEN RIBS 9 AND 11. 50000 FHI: 17000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 256APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574115-02-8 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 33D622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT ORPOST 48437SPAR BETWEEN RIBS 9 AND 11. 50000 FHI: 20000 FCOR50000 FH574115-02-9 522AB 522BB 522CB 522 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 20000 FCGROUP 32A622AB 622BB 622CB 622 BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT ORPOST 48437SPAR BETWEEN RIBS 9 AND 11. 50000 FHI: 16200 FCOR50000 FH574116-01-10 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEPOST 48437521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 10400 FC522SB 523CB 523DB OR523EB 523FB 523GB 28900 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 257APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-11 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEPOST 48437521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 8200 FC522SB 523CB 523DB OR523EB 523FB 523GB 48500 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 258APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 574116-01-12 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP A330-200F521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS I: 12 YE I: 12 YE521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPIC DUCT RIBS) AND522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS.522DB 522EB 522FB 622522GB 522HB 522JB 623522KB 522LB 522MB522NB 522PB 522RB522SB 523CB 523DB523EB 523FB 523GB523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 259APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-4 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEPRE 48437521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 14600 FC522SB 523CB 523DB OR523EB 523FB 523GB 50000 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 260APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-5 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33A521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEOR521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FCGROUP 33B522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 13500 FC522SB 523CB 523DB OR523EB 523FB 523GB 42600 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 261APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-6 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33C521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 15200 FC522SB 523CB 523DB OR523EB 523FB 523GB 48000 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 262APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-7 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 32E521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 17000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 8200 FC522SB 523CB 523DB OR523EB 523FB 523GB 48500 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 263APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-8 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33E521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YE521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 17000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 9600 FC522SB 523CB 523DB OR523EB 523FB 523GB 30000 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PBISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 264APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574116-01-9 521AB 521BB 521CB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D521DB 521EB 521FB 522 SUB SPAR TOP JOINT STRAPS AT ALL INTERMEDIATE RIBS OR I: 12 YEPRE 48437521GB 521HB 521JB 523 (INCLUDING CLOSING RIBS AND TELESCOPE DUCT RIBS) AND 20000 FC522AB 522BB 522CB 621 SLAT HOLD DOWN RIBS. OR522DB 522EB 522FB 622 50000 FH522GB 522HB 522JB 623 I: 12 YE522KB 522LB 522MB OR522NB 522PB 522RB 14000 FC522SB 523CB 523DB OR523EB 523FB 523GB 44200 FH523HB 523JB 523KB523LB 523MB 523NB523PB 621AB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622RB 622SB 623CB623DB 623EB 623FB623GB 623HB 623JB623KB 623LB 623MB623NB 623PB574119-01-1 521BB 521GB 523GB 521 DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE T: 12 YE T: 20 YE CPCP ALL523JB 523LB 523NB 523 TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK I: 12 YE I: 12 YE621BB 621GB 623GB 621 RIBS 1 AND 2 AND TRACK RIBS 13 TO 16.623JB 623LB 623NB 623R 574301-01-3 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, TRACKS 2 & 3, T: 20000 FCA330-200611 VISIBLE PART OF ROLLER CONTACT AREA. OROR50000 FHA330-300I: 9400 FCOR30900 FH574303-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 12 YE CPCP ALL611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, LINKS AND LINK PLATE, LH/RH.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 265APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574303-02-3 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 T: 20000 FCZL-500-01-1 A330-200611 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574304-01-1 SLAT FULLY EXTENDED 511 SPECIAL DETAILED INSPECTION OF SLAT 1, SKIN T: 12 YE T: 20 YE NO CPCP ALL611 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574304-03-2.R 574304-02-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 20000 FCA330-200611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FHR 574304-03-2 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP ALL611 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574304-01-1.574305-01-1 SLAT FULLY EXTENDED 511 DETAILED INSPECTION OF SLAT 1 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL611 LH/RH. I: 12 YE I: 12 YER 574306-02-1 SLAT FULLY EXTENDED 511 GENERAL VISUAL INSPECTION OF SLAT 1 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 ALL611 LOWER FACE, 100 MM FROM AFT EDGE, LH/RH. I: 3 YER 574307-01-1 521DB 521GB 621DB 511 DETAILED INSPECTION OF SLAT 1, TRACKS 2 AND 3 T: 12 YE T: 20 YE CPCP ALL621GB 611 ACTUATION LINK CONNECTION BOLTS LH/RH. I: 6 YE I: 6 YEREMOVAL OF THE BOLTSONE AT A TIME.SLAT FULLY EXTENDEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 266APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574308-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 1, EXTERNAL SURFACE T: 6 YE NO CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1R 574401-01-3 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND T: 20000 FCA330-200612 6; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 7000 FCOR22800 FH574401-02-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6; T: 12 YE T: 20 YE CPCP ALL612 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YE574403-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 T: 12 YE CPCP ALL612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, 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 FCZL-500-01-1 A330-200612 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574404-01-1 SLAT FULLY EXTENDED 512 SPECIAL DETAILED INSPECTION OF SLAT 2, SKIN T: 12 YE T: 20 YE NO CPCP ALL612 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574404-03-2.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 267APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574404-02-3 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT T: 20000 FCA330-200612 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FHR 574404-03-2 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP ALL612 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574404-01-1.574405-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 2 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL612 LH/RH. I: 12 YE I: 12 YER 574406-01-1 SLAT FULLY EXTENDED 512 GENERAL VISUAL INSPECTION OF SLAT 2 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 ALL612 LOWER FACE, 100 MM FROM AFT EDGE LH/RH. I: 3 YEN 574407-01-1 522CB 522FB 622CB 522 DETAILED INSPECTION OF SLAT 2, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL622FB 622 LH/RH. I: 6 YE I: 6 YESLAT 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 CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1574501-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 ; T: 12 YE T: 20 YE CPCP ALL613 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 268APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574501-02-4 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 T: 20000 FCA330-200613 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 7000 FCOR22800 FHR 574503-01-1 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, TRACKS 7 & 8 T: 12 YE CPCP ALL613 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, 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 FCZL-500-01-1 A330-200613 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574504-01-1 SLAT FULLY EXTENDED 513 SPECIAL DETAILED INSPECTION OF SLAT 3, SKIN T: 12 YE T: 20 YE NO CPCP ALL613 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 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 CPCP ALL613 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574504-01-1.R 574504-02-4 SLAT FULLY EXTENDED 513 DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS AT T: 20000 FCA330-200613 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FHR 574505-01-1 SLAT FULLY EXTENDED 512 DETAILED INSPECTION OF SLAT 3 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL612 LH/RH. I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 269APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574506-02-1 SLAT FULLY EXTENDED 513 GENERAL VISUAL INSPECTION OF SLAT 3 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 ALL613 LOWER FACE, 100 MM FROM AFT EDGE LH/RH. I: 3 YEZL-500-02-1N 574507-01-1 522JB 522LB 622JB 522 DETAILED INSPECTION OF SLAT 3, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL622LB 622 LH/RH. I: 6 YE I: 6 YESLAT 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 DELETEDR 574508-01-1 SLAT FULLY EXTENDED 500 GENERAL VISUAL INSPECTION OF SLAT 3, EXTERNAL SURFACE T: 6 YE CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1574601-01-1 N/A TASK DELETEDR 574601-01-3 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND T: 20000 FCA330-200614 10 , VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 9400 FCOR30900 FHR 574601-02-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 , T: 12 YE T: 20 YE CPCP ALL614 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YER 574603-01-2 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, TRACKS 9 & 10 T: 12 YE NO CPCP ALL614 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, LINKS AND LINK PLATE, LH/RH.574603-02-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 270APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574603-02-3 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4, TRACKS 9 AND 10 T: 20000 FCZL-500-01-1 A330-200614 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574604-01-1 SLAT FULLY EXTENDED 514 SPECIAL DETAILED INSPECTION OF SLAT 4, SKIN T: 12 YE T: 20 YE NO CPCP ALL614 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 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 CPCP ALL614 TRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL, LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574604-01-1.R 574604-02-3 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS AT T: 20000 FCA330-200614 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FH574605-01-1 SLAT FULLY EXTENDED 514 DETAILED INSPECTION OF SLAT 4 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL614 LH/RH. I: 12 YE I: 12 YE574606-02-1 SLAT FULLY EXTENDED 514 GENERAL VISUAL INSPECTION OF SLAT 4 TRAILING EDGE, T: 3 YE CPCP ZL-500-01-1 ALL614 LOWER FACE, 100 MM FROM AFT EDGE LH/RH. I: 3 YEZL-500-02-1N 574607-01-1 522NB 522RB 622NB 522 DETAILED INSPECTION OF SLAT 4, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL622RB 622 LH/RH. I: 6 YE I: 6 YESLAT 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 CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 271APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574701-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 , T: 12 YE T: 20 YE CPCP ALL615 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YER 574701-02-4 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND T: 20000 FCA330-200615 12 ; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 13300 FCOR43500 FHR 574703-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 T: 12 YE CPCP ALL615 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, 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 FCZL-500-01-1 A330-200615 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574704-01-1 SLAT FULLY EXTENDED 515 SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN T: 12 YE T: 20 YE NO CPCP ALL615 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574704-03-1.R 574704-02-3 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT T: 20000 FCA330-200615 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FHR 574704-03-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP ALL615 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574704-01-1.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 272APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS574705-01-1 SLAT FULLY EXTENDED 515 DETAILED INSPECTION OF SLAT 5 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL615 LH/RH. I: 12 YE I: 12 YE574706-02-1 SLAT FULLY EXTENDED 515 GENERAL VISUAL INSPECTION OF SLAT 5 TRAILING EDGE, T: 3 YE CPCP ZL-500-01-1 ALL615 LOWER FACE, 100 MM FRONT AFT EDGE, LH/RH. I: 3 YEZL-500-02-1N 574707-01-1 523CB 523FB 623CB 523 DETAILED INSPECTION OF SLAT 5, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL623FB 623 LH/RH. I: 6 YE I: 6 YESLAT 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 CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1574801-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND 14; T: 12 YE T: 20 YE CPCP ALL616 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YER 574801-02-3 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND T: 20000 FCA330-200616 14; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 7000 FCOR22800 FHR 574803-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, TRACKS 13 AND 14 T: 12 YE CPCP ALL616 ATTACHMENTS INCLUDING TRACK RIB LUGS,TRACK LUGS, I: 6 YEBOLTS, 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 FCZL-500-01-1 A330-200616 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 273APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574804-01-1 SLAT FULLY EXTENDED 516 SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN T: 12 YE T: 20 YE NO CPCP ALL616 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574804-03-2.574804-02-1 N/A TASK DELETEDR 574804-02-4 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT T: 20000 FCA330-200616 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FHR 574804-03-2 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP ALL616 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574804-01-1.574805-01-1 SLAT FULLY EXTENDED 516 DETAILED INSPECTION OF SLAT 6 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL616 LH/RH. I: 12 YE I: 12 YER 574806-02-1 SLAT FULLY EXTENDED 516 GENERAL VISUAL INSPECTION OF SLAT 6 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 ALL616 LOWER FACE, 100 MM FRONT AFT EDGE, LH/RH. I: 3 YEN 574807-01-1 523GB 523JB 623GB 523 DETAILED INSPECTION OF SLAT 6, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL623JB 623 LH/RH. I: 6 YE I: 6 YESLAT 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 CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1574901-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND 16; T: 12 YE T: 20 YE CPCP ALL617 VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. I: 6 YE I: 6 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 274APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574901-02-3 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND T: 20000 FCA330-200617 16; VISIBLE PART OF ROLLER CONTACT AREA, LH/RH. OROR50000 FHA330-300I: 7000 FCOR22800 FHR 574903-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, TRACKS 15 AND 16 T: 12 YE CPCP ALL617 ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS, I: 6 YEBOLTS, 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 FCZL-500-01-1 A330-200617 ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, ORORBOLTS, LINKS AND LINK PLATE, LH/RH. 50000 FHA330-300I: 6600 FCOR24000 FHR 574904-01-1 SLAT FULLY EXTENDED 517 SPECIAL DETAILED INSPECTION OF SLAT 7, SKIN T: 12 YE T: 20 YE NO CPCP ALL617 CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, I: 12 YE I: 12 YEINTERNAL, LH/RH.NOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574904-02-1.R 574904-02-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN CONNECTIONS AT T: 12 YE T: 20 YE CPCP ALL617 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. I: 12 YE I: 12 YENOTE: THIS TASK MAY BE PERFORMED AT THE SAME TIME ASTASK 574904-01-1.R 574904-02-4 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7, SKIN CONNECTIONS AT T: 20000 FCA330-200617 TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. OROR50000 FHA330-300I: 9300 FCOR27900 FH574905-01-1 SLAT FULLY EXTENDED 517 DETAILED INSPECTION OF SLAT 7 HOLD DOWN BRACKET, T: 12 YE T: 20 YE CPCP ALL617 LH/RH. I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 275APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 574906-02-1 SLAT FULLY EXTENDED 517 GENERAL VISUAL INSPECTION OF SLAT 7 TRAILING EDGE T: 3 YE CPCP ZL-500-01-1 ALL617 LOWER FACE, 100 MM FRONT AFT EDGE LH/RH. I: 3 YEZL-500-02-1N 574907-01-1 523LB 523NB 623LB 523 DETAILED INSPECTION OF SLAT 7, PINION AND RACK TEETH, T: 6 YE T: 20 YE NOALL623NB 623 LH/RH. I: 6 YE I: 6 YESLAT 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 CPCP ZL-500-01-1 ALL600 OF UPPER AND LOWER SKIN, LH/RH. I: 6 YEZL-500-02-1575001-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32ASPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YEPRE 4843720000 FCORI: 12 YEGROUP 33AOROR10700 FCGROUP 33BORGROUP 33CORGROUP 33DPRE 48437575001-01-4 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32ESPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YEOR17000 FCGROUP 33EI: 12 YEOR12900 FC575001-01-6 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32ASPOILERS EXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITTING. OR I: 12 YEPOST 4843720000 FCORI: 12 YEGROUP 33DORPOST 4843712900 FCN 575001-01-7 FLAPS EXTENDED SLATS 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A330-200FEXTENDED 673 SPOILER 1 ACTUATOR SUPPORT FITING. I: 12 YE I: 12 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 276APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575002-01-1 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS T: 12 YE T: 20 YE CPCP ALL673BB 673DB 673FB 673 1-6, COMPRISING ATTACHMENTS TO REAR SPAR OR FALSE I: 12 YE I: 12 YEREAR 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 CPCP ALLSPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 I: 12 YE I: 12 YEPLACES) 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 CPCP GROUP 32ASPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING (5 OR I: 12 YEPRE 48437PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 20000 FCOROVERHANG. I: 12 YEGROUP 33AOROR20000 FCGROUP 33BORGROUP 33CORGROUP 33DPRE 48437575004-01-4 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32ESPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING OR I: 12 YEOR(5 PLACES) ATTACHMENT TO REAR SPAR AND TOP SKIN 17000 FCGROUP 33EOVERHANG. I: 12 YEOR17000 FC575004-01-6 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32ASPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR SUPPORT FITTING OR I: 12 YEPOST 48437(5 PLACES) ATTACHMENT TO REAR SPAR AND TOP 20000 FCORSKIN OVERHANG. I: 12 YEGROUP 33DORPOST 4843720000 FCN 575004-01-7 FLAPS EXTENDED SLATS 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A330-200FEXTENDED 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 SKINOVERHANG.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 277APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575005-01-1 FLAPS EXTENDED 574 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP ALLSPOILERS EXTENDED 674 SPOILERS 2, 3, 4, 5 AND 6 ACTUATOR HINGE RIBS AND I: 12 YE I: 12 YEOUTER 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 CPCP ALL675CB 675 INBOARD AND OUTBOARD AILERON JACK BRACKETS (4 PLACES) I: 12 YE I: 12 YEAT LUG AND ATTACHMENT TO TOP AND BOTTOM SKINOVERHANGS (INTERNAL AND EXTERNAL).575008-01-1 FLAPS EXTENDED 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIB T: 12 YE T: 20 YE CPCP ALLSPOILERS EXTENDED 574 10 FLAP CRUISE ROLLERS SUPPORT. I: 12 YE I: 12 YE673674575009-01-1 573BB 573CB 573DB 573 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE CPCP ALL573EB 573FB 573GB 673 RIBS 6, 8 AND 10 ATTACHMENT TO REAR SPAR, TOP AND I: 12 YE673BB 673CB 673DB BOTTOM SKIN OVERHANGS AND OUTER FLAP CRUISE ROLLER673EB 673FB 673GB SUPPORT ATTACHMENT TO TRAILING EDGE RIB 10.575010-01-1 N/A TASK DELETED575010-01-10 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEPOST 4843720000 FCOR50000 FHI: 12 YEOR20000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 278APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575010-01-11 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEPOST 4843720000 FCOR50000 FHI: 12 YEOR15900 FCOR50000 FHN 575010-01-12 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE CPCP A330-200F673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES I: 12 YE I: 12 YE575010-01-4 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE CPCP GROUP 32A673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEPRE 4843720000 FCOR50000 FHI: 12 YEOR7500 FCOR27000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 279APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575010-01-5 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE CPCP GROUP 33A673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEOR20000 FCGROUP 33BOR50000 FHI: 12 YEOR8300 FCOR26700 FH575010-01-6 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE CPCP GROUP 33C673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE20000 FCOR50000 FHI: 12 YEOR7000 FCOR22600 FH575010-01-7 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE FALSE T: 12 YE T: 20 YE CPCP GROUP 32E673BB 673DB 673FB 673 REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE17000 FCOR50000 FHI: 12 YEOR15900 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 280APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575010-01-8 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33E673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YE17000 FCOR50000 FHI: 12 YEOR17000 FCOR50000 FH575010-01-9 573BB 573DB 573FB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D673BB 673DB 673FB 673 FALSE REAR SPAR FORWARD AND AFT FACES. OR I: 12 YEPRE 4843720000 FCOR50000 FHI: 12 YEOR6800 FCOR21900 FH575011-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FCGROUP 32A600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 ORPOST 48437AND RIB 14. 50000 FHI: 8700 FCOR38400 FHR 575011-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D600 TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN ORPRE 48437RIB 1 AND RIB 14. 59500 FHI: 19000 FCOR56600 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 281APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575011-01-4 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FCGROUP 32A600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND ORPRE 48437RIB 14. 90700 FHI: 17300 FCOR78500 FH575011-01-5 N/A TASK DELETEDR 575011-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 20000 FCGROUP 33C600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND ORPRE 48437RIB 14. 59300 FHI: 19400 FCOR57600 FH575011-01-7 N/A TASK DELETED575011-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 17000 FCGROUP 33E600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND ORRIB 14. 50000 FHI: 10000 FCOR28500 FH575011-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP T: 17000 FCGROUP 32E600 SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 ORAND RIB 14. 50000 FHI: 8300 FCOR36500 FH575011-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE NO CPCP ZL-500-02-1 ALL600 TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 I: 12 YEAND RIB 14.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 282APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575012-01-10 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33C600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORPOST 48437RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FHOR2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 8000 FCGROUP 33DINBOARD OF GEAR SUPPORT RIB 6. ORPOST 4843722900 FH575012-01-11 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORPOST 48437RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6800 FCINBOARD OF GEAR SUPPORT RIB 6. OR30600 FH575012-01-2 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORPRE 48437RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 5200 FCINBOARD OF GEAR SUPPORT RIB 6. OR21000 FH575012-01-3 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33A600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORORRIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FHGROUP 33B2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 4200 FCINBOARD OF GEAR SUPPORT RIB 6. OR13700 FHR 575012-01-6 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33C600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORPRE 48437RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 5200 FCINBOARD OF GEAR SUPPORT RIB 6. OR16500 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 283APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575012-01-7 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 32E600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORRIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6800 FCINBOARD OF GEAR SUPPORT RIB 6. OR30600 FH575012-01-8 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 33E600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORRIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 8000 FCINBOARD OF GEAR SUPPORT RIB 6. OR22900 FH575012-01-9 N/A 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN ORPRE 48437RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 50000 FH2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 4800 FCINBOARD OF GEAR SUPPORT RIB 6. OR15300 FH575012-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO CPCP ZL-500-01-1 ALL600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN I: 6 YERIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUSTINBOARD OF GEAR SUPPORT RIB 6.575013-01-2 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORPRE 48437INBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 14900 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 284APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575013-01-3 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33A600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORORINBOARD OF GEAR SUPPORT RIB 6. 50000 FHGROUP 33BI: 10600 FCOR34000 FH575013-01-4 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33C600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORINBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 14700 FCOR46200 FH575013-01-5 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM T: 17000 FCGROUP 32E600 SKIN LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR ORJUST INBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 12300 FCOR50000 FH575013-01-6 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 17000 FCGROUP 33E600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORINBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 14500 FCOR41400 FH575013-01-7 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORPRE 48437INBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 13900 FCOR43800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 285APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575013-01-8 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 33D600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORPOST 48437.NBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 15400 FCOR42800 FH575013-01-9 N/A 500 SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN T: 20000 FCGROUP 32A600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST ORPOST 48437INBOARD OF GEAR SUPPORT RIB 6. 50000 FHI: 12300 FCOR50000 FH575013-02-1 N/A 500 GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM SKIN T: 6 YE NO CPCP ZL-500-01-1 ALL600 LOWER SURFACE CURVED SKIN EDGE AFT OF REAR SPAR JUST I: 6 YEINBOARD OF GEAR SUPPORT RIB 6.575014-01-4 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 32A670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORPRE 48437REINFORCING. 50000 FHI: 17700 FCOR50000 FH575014-01-5 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33A670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORORREINFORCING. 50000 FHGROUP 33BI: 14800 FCOR47300 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 286APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575014-01-6 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33C670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORREINFORCING. 50000 FHI: 16700 FCOR50000 FH575014-01-7 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 17000 FCGROUP 32E670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORORREINFORCING. 50000 FHGROUP 33EI: 17000 FCOR50000 FH575014-01-8 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33D670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORPRE 48437REINFORCING. 50000 FHI: 16200 FCOR50000 FH575014-01-9 573DB 673DB 570 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 32A670 EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG ORPOST 48437REINFORCING. 50000 FHORI: 20000 FCGROUP 33DORPOST 4843750000 FH575015-01-1 454HL 464HL 532AB 454 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE NO CPCP ZL-454-06-1 ALL533AB 534AB 632AB 464 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB I: 12 YEZL-454-06-2633AB 634AB 500 12 TO RIB 39.ZL-500-01-1532ZL-531-02-1533534600632633634575016-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 287APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575016-01-10 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 33E631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORTRACK 2 FAIRING. 50000 FHI: 8000 FCOR22900 FH575016-01-11 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORPOST 48437TRACK 2 FAIRING. 50000 FHI: 8500 FCOR23700 FH575016-01-12 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORPOST 48437TRACK 2 FAIRING. 50000 FHI: 6800 FCOR30600 FHR 575016-01-4 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORPRE 48437TRACK 2 FAIRING. 50000 FHI: 8300 FCOR37700 FH575016-01-5 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33A631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORORTRACK 2 FAIRING. 50000 FHGROUP 33BI: 7700 FCOR24700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 288APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575016-01-6 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33C631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORPRE 48437TRACK 2 FAIRING. 50000 FHI: 8000 FCOR23700 FH575016-01-7 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP ALL631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP I: 12 YE I: 12 YETRACK 2 FAIRING.R 575016-01-8 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORPRE 48437TRACK 2 FAIRING. 50000 FHI: 7600 FCOR22500 FH575016-01-9 531AB 631AB 531 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 32E631 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP ORTRACK 2 FAIRING. 50000 FHI: 6800 FCOR30600 FHR 575017-01-4 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 32A673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, ORPRE 48437INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FHOF GEAR SUPPORT RIB 6. I: 5000 FCOR22800 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 289APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575017-01-5 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33A673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, ORORINTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FHGROUP 33BOF GEAR SUPPORT RIB 6. I: 8200 FCOR26400 FHR 575017-01-6 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33C673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, ORPRE 48437INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FHOF GEAR SUPPORT RIB 6. I: 5500 FCOR16300 FHR 575017-01-7 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 33D673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, ORPRE 48437INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST 50000 FHOUTBOARD OF GEAR SUPPORT RIB 6. I: 5200 FCOR15500 FH575017-01-8 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 17000 FCGROUP 32E673 EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, ORORINTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FHGROUP 33EOF GEAR SUPPORT RIB 6. I: 17000 FCOR50000 FH575017-01-9 573DB 673DB 573 SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING T: 20000 FCGROUP 32A673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL ORPOST 48437AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD 50000 FHOROF GEAR SUPPORT RIB 6. I: 20000 FCGROUP 33DORPOST 4843750000 FH575017-02-1 573DB 673DB 573 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 6 YE NO CPCP ALL673 BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND I: 6 YEEXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEARSUPPORT RIB 6.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 290APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575018-01-10 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D192CT 672 ATTACHMENT OF SHROUD BOX. ORPRE 48437FLAPS EXTENDED 50000 FHI: 20000 FCOR50000 FH575018-01-3 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A192CT 672 ATTACHMENT OF SHROUD BOX. ORPRE 48437FLAPS EXTENDED 50000 FHI: 20000 FCOR50000 FHD 575018-01-4 N/A TASK DELETED575018-01-5 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33C192CT 672 ATTACHMENT OF SHROUD BOX. ORPRE 48437FLAPS EXTENDED 50000 FHI: 20000 FCOR50000 FH575018-01-6 N/A TASK DELETED575018-01-7 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 33E192CT 672 ATTACHMENT OF SHROUD BOX. ORFLAPS EXTENDED 50000 FHI: 17000 FCOR50000 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 291APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575018-01-8 147AT 148AT 191CT 572 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 32E192CT 672 ATTACHMENT OF SHROUD BOX. ORFLAPS EXTENDED 50000 FHI: 17000 FCOR50000 FH575018-02-1 147AT 148AT 191CT 572 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 10 YE CPCP ALL192CT 672 ATTACHMENT OF SHROUD BOX. I: 10 YEFLAPS EXTENDEDR 575019-01-1 147AT 148AT 571 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 10 YE CPCP ALL671 ATTACHMENT OF OVERWING PANEL. I: 10 YE575022-01-1 N/A TASK DELETED575022-01-2 N/A TASK DELETEDD 575022-01-3 N/A TASK DELETEDD 575022-01-5 N/A TASK DELETED575022-01-6 575AB 575BB 675AB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP ALL675BB 675 INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO I: 12 YE I: 12 YEREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4AND 5 AT LUG AND ATTACHMENT TO HINGEPOST ANDATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 292APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575023-01-1 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YEPRE 48437REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FCORAND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YEGROUP 33AAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OROREXTERNAL. 9000 FCGROUP 33BORGROUP 33C575023-01-3 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32E675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT OR I: 12 YETO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, 17000 FCHINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO ORREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL 50000 FHAND EXTERNAL. I: 12 YEOR7300 FCOR42800 FH575023-01-4 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33E675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YEREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 17000 FCAND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR ORAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND 50000 FHEXTERNAL. I: 12 YEOR8400 FCOR26500 FH575023-01-5 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YEPRE 48437REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FCAND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YEAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OREXTERNAL. 9200 FCISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 293APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575023-01-6 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 33D675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YEPOST 48437REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FCAND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR I: 12 YEAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND OREXTERNAL. 9200 FCR 575023-01-7 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP GROUP 32A675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO OR I: 12 YEPOST 48437REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 20000 FCAND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR ORAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND 50000 FHEXTERNAL. I: 12 YEOR7300 FCOR42800 FHN 575023-01-8 575CB 575DB 675CB 575 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE T: 20 YE CPCP A330-200F675DB 675 OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO I: 12 YE I: 12 YEREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPARAND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.575025-01-10 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORPOST 48437FROM RIB 8 TO RIB 12. 50000 FHI: 8500 FCOR23700 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 294APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS575025-01-11 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM ORPOST 48437RIB 8 TO RIB 12. 50000 FHI: 6800 FCOR30600 FHR 575025-01-4 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 32A531 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 ORPRE 48437600 TO RIB 12. 50000 FH631 I: 7300 FCOR33300 FHR 575025-01-5 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33A531 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 OROR600 TO RIB 12. 50000 FHGROUP 33B631 I: 6600 FCOR19700 FHR 575025-01-6 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33C600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 ORPRE 48437TO RIB 12. 50000 FHI: 8100 FCOR24000 FHR 575025-01-7 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 33E600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 ORTO RIB 12. 50000 FHI: 8400 FCOR23900 FHISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 295APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575025-01-8 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 17000 FCGROUP 32E600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM ORRIB 8 TO RIB 12. 50000 FHI: 7100 FCOR32000 FHR 575025-01-9 531AB 631AB 500 DETAILED INSPECTION OF OUTER WING TRAILING EDGE T: 20000 FCGROUP 33D600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR ORPRE 48437FROM RIB 8 TO RIB 12. 50000 FHI: 7600 FCOR22700 FH575025-02-1 532AB 632AB 500 GENERAL VISUAL INSPECTION OF OUTER WING TRAILING EDGE T: 12 YE CPCP ZL-500-01-1 ALL600 BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 I: 12 YEZL-531-02-1TO RIB 12.575051-01-1 N/A TASK DELETEDR 575053-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, DRIVE LINK, T: 12 YE T: 20 YE CPCP A330-200FLAPS EXTENDED 148 DRIVE LEVER, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YEPRE 45326ORA330-300PRE 45326575053-01-2 N/A TASK DELETEDR 575054-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1. GEAR BOX, T: 12 YE T: 20 YE CPCP A330-200FLAPS EXTENDED 148 FORK ASSY, DRIVE STRUT AND CARRIAGE. I: 12 YE I: 12 YEPOST 45326ORA330-200FPOST 45326ORA330-300POST 45326ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 296APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575055-01-1 734 744 147 DETAILED INSPECTION OF FLAP TRACK NO.1, ATTACHMENTS T: 12 YE T: 20 YE CPCP ALL148 TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING I: 12 YE I: 12 YESUPPORT STRUTS WITH ATTACHMENT FITTING.575055-01-2 N/A TASK DELETED575057-01-2 N/A TASK DELETEDR 575059-01-1 AFT FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, T: 12 YE T: 20 YE CPCP ALLFAIRINGS 532 DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE I: 12 YE I: 12 YEFLAPS EXTENDED 533 ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND534 TRAVELLING BEAM AT TRACK NO.4.631632633634575059-01-2 N/A TASK DELETEDR 575061-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACKS NO.2,3,4 AND 5, T: 12 YE T: 20 YE CPCP ALL532 CARRIAGE ASSEMBLIES. I: 12 YE I: 12 YE533534631632633634575061-01-2 N/A TASK DELETED575063-01-1 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 297APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575063-01-3 FLAP TRACK FAIRING 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO. 2,3,4 T: 12 YE CPCP A330-200REMOVED 532 AND 5 LOWER FLANGES, STRAP AND ANGLES. I: 12 YEPOST 55652533OR534A330-200F631POST 55652632OR633A330-300634POST 55652R 575065-01-1 FLAP TRACK FAIRINGS 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO. T: 12 YE T: 20 YE NO CPCP ALL532 2,3,4 AND 5, INTERNAL STRUCTURE. I: 12 YE I: 12 YE533534631632633634R 575067-01-1 FWD FLAP TRACK 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2,3,4 AND T: 12 YE T: 20 YE CPCP ALLFAIRINGS 532 5, FORWARD ATTACHMENT SPIGOTS, EXTERNAL STRUCTURE. I: 12 YE I: 12 YE533534631632633634575067-01-2 N/A TASK DELETEDR 575067-02-1 FS BOLT 531 SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO. T: 12 YE T: 20 YE NO CPCP ALLFWD FLAP TRACK 532 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS, I: 12 YE I: 12 YEFAIRINGS 533 INTERNAL STRUCTURE.534631632633634575067-02-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 298APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575069-01-1 FLAPS EXTENDED 531 DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2,3,4 AND T: 12 YE T: 20 YE NO CPCP ALL532 5, AFT ATTACHMENT SPIGOTS. I: 12 YE I: 12 YE533534631632633634575069-01-2 N/A TASK DELETEDR 575401-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL T: 6 YE CPCP ZL-500-01-1 ALL600 SURFACE OF UPPER AND LOWER SKIN. I: 6 YEZL-500-02-1575401-01-2 N/A TASK DELETED575401-02-1 N/A TASK DELETED575402-01-1 N/A TASK DELETEDR 575403-01-1 581AB 681AB 734 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE CPCP ALL744 681 FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND I: 12 YE I: 12 YEEXTERNAL.575403-01-2 N/A TASK DELETEDR 575403-02-1 581AB 681AB 734 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP ALL744 681 SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL. I: 12 YE I: 12 YESPEED TAPESN 575404-01-1 FLAPS EXTENDED 581 GENERAL VISUAL INSPECTION OF INBOARD FLAP TRAILING T: 6 YEZL-500-01-1 ALL681 EDGE. I: 6 YEZL-500-02-1ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 299APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSN 575404-03-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 6 YE CPCP A330-200681 EDGE. I: 6 YEPRE 47798PRE 49008PRE SBA330-57-3068ORA330-300PRE 47798PRE 49008PRE SBA330-57-3068N 575404-03-2 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP TRAILING T: 12 YE CPCP A330-200681 EDGE. I: 12 YEPOST 47798ORPOST 49008ORPOST SBA330-57-3068ORA330-200FPOST 47798ORPOST 49008ORPOST SBA330-57-3068ORA330-300POST 47798ORPOST 49008POST SBA330-57-3068R 575405-01-1 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE CPCP A330-200631CB 681 FITTING AT TRACK NO. 2 AND EXTERNAL DRIVE STRUT I: 12 YE I: 12 YEPRE 49008FLAPS EXTENDED BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARMORATTACHMENT BRACKET.A330-300PRE 49008575405-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 300APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575405-01-3 531AT 531CB 631AT 581 DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT T: 12 YE T: 20 YE CPCP A330-200631CB 681 FITTING AT TRACK NO. 2 AND EXTERNAL DRIVE STRUT I: 12 YE I: 12 YEPOST 49008FLAPS EXTENDED BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARMORATTACHMENT BRACKET.A330-200FORA330-300POST 49008R 575405-02-1 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP A330-200631CB 681 SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YEPRE 49008FLAPS EXTENDEDORSPEED TAPESA330-300PRE 49008R 575405-02-2 531AT 531CB 631AT 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP A330-200631CB 681 SUPPORT FITTING AT TRACK NO.2. I: 12 YE I: 12 YEPOST 49008FLAPS EXTENDEDORSPEED TAPESA330-200FORA330-300POST 49008R 575407-01-1 FLAPS EXTENDED 581 DETAILED INSPECTION OF INBOARD FLAP, OUTER END-RIB T: 12 YE T: 20 YE NO CPCP ALLRUBBER SEALS 681 INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT I: 12 YE I: 12 YEBRACKET.R 575409-01-1 FLAPS EXTENDED 581 SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL T: 12 YE T: 20 YE NO CPCP ALLSPEED TAPES 681 STRUCTURE. I: 12 YE I: 12 YEN 575501-01-1 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 6 YEZL-500-01-1 ALL600 SURFACES OF UPPER AND LOWER SKIN. I: 6 YE575501-01-2 FLAPS EXTENDED 500 GENERAL VISUAL INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 6 YEZL-500-02-1 ALL600 SURFACE OF UPPER AND LOWER SKIN I: 6 YEISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 301APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575503-01-1 532AT 532CB 632AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP ALL632CB 683 SUPPORT FITTING AT TRACK NO.3, AND EXTERNAL DRIVE I: 12 YE I: 12 YEFLAPS EXTENDED STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE WITHASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHMENTFITTING.575503-01-2 N/A TASK DELETEDR 575503-02-1 532AT 532CB 632AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP ALL632CB 683 INTERNAL SUPPORT FITTING AT TRACK NO. 3. I: 12 YE I: 12 YEFLAPS EXTENDEDSPEED TAPES575503-02-2 N/A TASK DELETEDR 575505-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP ALL633CB 683 SUPPORT FITTING AT TRACK NO.4, AND EXTERNAL FWD I: 12 YE I: 12 YEFLAPS EXTENDED SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.575505-01-2 N/A TASK DELETEDR 575505-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE CPCP ALL633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO. 4. I: 12 YE I: 12 YEFLAPS EXTENDEDSPEED TAPES575505-02-2 N/A TASK DELETEDR 575507-01-1 533AT 533CB 633AT 583 DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL T: 12 YE T: 20 YE CPCP ALL633CB 683 SUPPORT FITTING AT TRACK NO. 5, AND EXTERNAL DRIVE I: 12 YE I: 12 YEFLAPS EXTENDED STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITHASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.575507-01-2 N/A TASK DELETEDISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 302APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 575507-02-1 533AT 533CB 633AT 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP ALL633CB 683 INTERNAL SUPPORT FITTING AT TRACK NO. 5. I: 12 YE I: 12 YEFLAPS EXTENDEDSPEED TAPES575507-02-2 N/A TASK DELETED575509-01-1 FLAPS EXTENDED 583 DETAILED INSPECTION OF OUTBOARD FLAP, EXTERNAL T: 12 YE T: 20 YE CPCP ALLRUBBER SEALS 683 SURFACE OF INNER END RIB INCLUDING ROLLER AND I: 12 YE I: 12 YEINTERCONNECTION STRUT ATTACHMENT BRACKET.575509-01-2 N/A TASK DELETED575509-02-1 FLAPS EXTENDED 583 SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, T: 12 YE T: 20 YE NO CPCP ALLRUBBER SEALS 683 INTERNAL STRUCTURE OF INNER END RIB. I: 12 YE I: 12 YESPEED TAPES575509-02-2 N/A TASK DELETED576101-01-1 N/A 590 DETAILED INSPECTION OF OUTBOARD AILERON, UPPER AND T: 6 YEALL690 LOWER SKINS, EXTERNAL SURFACE I: 6 YE576103-01-1 ONLY OUTBOARD 592 DETAILED INSPECTION OF OUTBOARD AILERON END RIBS, T: 12 YE T: 20 YE CPCP ALLAILERON DEFLECTED 692 EXTERNAL SURFACE I: 12 YE I: 12 YE576104-01-1 575BT 575CB 575DB 592 DETAILED INSPECTION OF OUTBOARD AILERON FITTINGS (7 T: 12 YE T: 20 YE CPCP ALL592AB 592BB 592CB 692 PLACES) I: 12 YE I: 12 YE592DB 675BT 675CB675DB 692AB 692BB692CB 692DBR 576106-01-2 JACK FITTING FAIRING 592 DETAILED INSPECTION OF OUTBOARD AILERONS, FIRST LINE T: 20000 FCA330-200692 OF FASTENERS ON OUTER JACK FITTING FLANGE LH/RH. I: 5100 FCORNOTE: THIS TASK IS AN ALTERNATIVE TO TASKA330-300576106-02-2ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 303APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 576106-02-2 JACK FITTING FAIRING 592 SPECIAL DETAILED INSPECTION OF OUTBOARD AILERONS, T: 20000 FCA330-200692 FIRST LINE OF FASTENERS ON OUTER JACK FITTING FLANGE I: 14600 FCORLH/RH.A330-300NOTE: THIS TASK IS AN ALTERNATIVE TO TASK576106-01-2576111-01-1 N/A 500 DETAILED INSPECTION OF INBOARD AILERON, UPPER AND T: 6 YEALL600 LOWER SKINS, EXTERNAL SURFACE I: 6 YE576113-01-1 INBOARD AILERON ONLY 591 DETAILED INSPECTION OF INBOARD AILERON END RIBS, T: 12 YE T: 20 YE CPCP ALLDEFLECTED 691 EXTERNAL SURFACE I: 12 YE I: 12 YE576114-01-1 575AB 575AT 575BB 591 DETAILED INSPECTION OF INBOARD AILERON FITTINGS (7 T: 12 YE T: 20 YE CPCP ALL591AB 591BB 591CB 691 PLACES) I: 12 YE I: 12 YE591DB 675AB 675AT675BB 691AB 691BB691CB 691DBR 576116-01-3 JACK FITTING FAIRING 591 SPECIAL DETAILED INSPECTION OF INBOARD AILERONS, T: 20000 FCA330-200691 FIRST LINE OF FASTENERS ON OUTER JACK FITTING FLANGE, I: 14600 FCORLH/RH.A330-300NOTE: THIS TASK IS AN ALTERNATIVE TO TASK576116-02-2R 576116-02-2 JACK FITTING FAIRING 591 DETAILED INSPECTION OF INBOARD AILERONS, FIRST LINE T: 20000 FCA330-200691 OF FASTENERS ON OUTER JACK FITTING FLANGE, LH/RH. I: 5100 FCORNOTE: THIS TASK IS AN ALTERNATIVE TO TASKA330-300576116-01-3R 577001-01-2 FLAPS EXTENDED 582 GENERAL VISUAL INSPECTION OF SPOILER NO.1, UPPER AND T: 6 YEZL-500-02-1 ALLSPOILERS DEPLOYED 682 LOWER SKIN, EXTERNAL SURFACE,LH/RH. I: 6 YER 577003-01-1 FLAPS EXTENDED 582 DETAILED INSPECTION OF SPOILER NO. 1, HINGE AND T: 12 YE T: 20 YE CPCP ALLSPOILERS DEPLOYED 682 ACTUATOR ATTACHMENT FITTINGS. I: 12 YE I: 12 YE577003-01-2 N/A TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: D-57PAGE 304APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 711141-01-1 415AL 416AR 425AL 411 GENERAL VISUAL INSPECTION OF INLET COWL ATTACHMENT T: 6 YE NO CPCP ZL-415-02-1 A330-200426AR 421 (A1 FLANGE). I: 6 YEGEORA330-300GE711141-01-2 N/A TASK DELETEDR 711142-01-1 415AL 416AR 425AL 411 GENERAL VISUAL INSPECTION OF SURROUNDING STRUCTURE OF T: 3 YEZL-415-02-1 A330-200426AR 421 INLET COWL ATTACHMENT (15 CM AROUND A1 FLANGE). I: 3 YEGEORA330-300GE711200-01-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND T: 3 YEZL-415-02-3 RR426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YE425426711200-01-2 N/A TASK DELETED711200-02-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR HINGES AND T: 12 YE NO CPCP RR426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 12 YEDISASSEMBLY OF PIN 425ASSY 426711246-01-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES T: 3 YEZL-415-02-3 RR426AR 416 AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 3 YE425 FITTINGS).426711246-01-2 N/A TASK DELETEDISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS711246-02-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR LATCHES AND T: 6 YE NO CPCP RR426AR 416 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 6 YE425426711301-01-1 415AL 415BL 416AR 415 DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR T: 6 YE NO CPCP PW416BR 425AL 425BL 416 HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE I: 6 YE426AR 426BR 425 FITTINGS).426711301-02-1 415AL 415BL 416AR 415 GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL T: 3 YEZL-415-02-2 PW416BR 425AL 425BL 416 DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE426AR 426BR 425 HINGE FITTINGS).426711301-02-2 N/A TASK DELETED711302-01-1 415AL 415BL 416AR 415 DETAILED INSPECTION OF FWD AND AFT FAN COWL DOOR T: 6 YE NO CPCP PW416BR 425AL 425BL 416 LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 6 YE426AR 426BR 425 FITTINGS).426711302-02-1 415AL 415BL 416AR 415 GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL T: 3 YEZL-415-02-2 PW416BR 425AL 425BL 416 DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE426AR 426BR 425 LATCH FITTINGS).426711302-02-2 N/A TASK DELETEDR 711341-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR HINGES AND T: 6 YE NO CPCP A330-200426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 6 YEGE425OR426A330-300GEISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 2APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 711341-02-1 415AL 416AR 425AL 415 GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND T: 3 YEZL-415-02-1 A330-200426AR 416 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YEGE425OR426A330-300GE711341-02-2 N/A TASK DELETEDR 711343-01-1 415AL 416AR 425AL 415 DETAILED INSPECTION OF FAN COWL DOOR LATCHES AND T: 6 YE NO CPCP A330-200426AR 416 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 6 YEGE425OR426A330-300GE711343-02-1 N/A TASK DELETEDR 711345-01-1 414AL 414AR 424AL 414 DETAILED INSPECTION OF CORE COWL DOOR HINGES AND T: 12 YE NO CPCP A330-200424AR 424 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 12 YEGEORA330-300GE711345-02-1 N/A TASK DELETED711347-01-1 N/A TASK DELETEDR 711347-02-1 414AL 414AR 424AL 414 DETAILED INSPECTION OF CORE COWL DOOR LATCHES AND T: 12 YE NO CPCP A330-200424AR 424 SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). I: 12 YEGEORA330-300GE712101-01-2 N/A TASK DELETED712101-02-1 N/A TASK DELETEDISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 3APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS712101-03-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO CPCP PWFWD ENGINE MOUNT 423 I: 12 YEDISASSEMBLED712101-04-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO CPCP RRFWD ENGINE MOUNT 423 I: 12 YEDISASSEMBLEDR 712101-06-1 ENGINE 413 DETAILED INSPECTION OF FORWARD ENGINE MOUNT. T: 12 YE NO CPCP A330-200FWD ENGINE MOUNT 423 I: 12 YEGEDISASSEMBLEDORA330-300GE712102-01-1 N/A TASK DELETED712102-01-2 N/A TASK DELETED712103-01-1 N/A TASK DELETED712103-01-2 N/A TASK DELETED712103-01-3 N/A TASK DELETED712103-01-4 N/A TASK DELETED712104-01-1 N/A TASK DELETED712105-01-1 N/A TASK DELETED712106-01-1 N/A TASK DELETED712106-01-2 N/A TASK DELETEDISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 4APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPSR 712201-03-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO CPCP PWDISASSEMBLED 423 I: 12 YEENGINER 712201-04-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO CPCP RRDISASSEMBLED 423 I: 12 YEENGINER 712201-05-1 AFT ENGINE MOUNT 413 DETAILED INSPECTION OF AFT ENGINE MOUNT LOWER BEAM. T: 12 YE NO CPCP A330-200DISASSEMBLED 423 I: 12 YEGEENGINEORA330-300GE712202-01-1 N/A TASK DELETED712203-01-1 N/A TASK DELETED712204-01-1 N/A TASK DELETED712204-02-1 N/A TASK DELETED712204-02-2 N/A TASK DELETED* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT SECTION: D-71PAGE 5APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS783200-01-1 N/A TASK DELETED783200-01-2 N/A TASK DELETED783200-02-1 417DL 417EL 418DR 417 DETAILED INSPECTION OF THRUST RESERVER HINGES, T: 6 YE NO CPCP RR418ER 427DL 427EL 418 SLEEVES AND PINS. I: 6 YE428DR 428ER 427PINS, SLEEVES AND 428BUSHES783200-03-1 417DL 417EL 418DR 417 SPECIAL DETAILED INSPECTION OF THRUST RESERVER HINGE T: 3 YERR418ER 427DL 427EL 418 SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). I: 3 YE428DR 428ER 427428R 783201-01-1 415AL 416AR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER HINGES, T: 6 YE NO CPCP A330-200418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 6 YEGE427AL 428AR 427 HINGE ATTACHMENTS).ORFWD HINGE COVER, 428A330-300HINGE BEAM PINSGE783201-02-1 415BL 416BR 417AL 417 DETAILED INSPECTION OF THRUST REVERSER HINGES AND T: 6 YE NO CPCP PW418AR 425BL 426BR 418 PINS. I: 6 YE427AL 428AR 427FWD HINGE COVER 428783201-03-1 N/A TASK DELETEDR 783201-03-2 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, T: 3 YEZL-417-02-1 A330-200418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YEGE427AL 428AR 427 HINGE ATTACHMENTS).OR428A330-300GE783201-04-1 N/A TASK DELETEDISSUE: JUL 01/10 EXHAUST SECTION: D-78PAGE 1APPLICABILITYA330MRB REPORT – Structures SectionZONEACCESSTASKREFERENCETASK DESCRIPTIONSAMPLETHRESHOLDINTERVALZIPREFERENCECPCP100%THRESHOLDINTERVALTPS783201-04-2 415BL 416BR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, T: 3 YEZL-417-02-2 PW418AR 425BL 426BR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE427AL 428AR 427 HINGE ATTACHMENTS).428R 783202-01-1 415AL 416AR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, T: 3 YEZL-417-02-1 A330-200418AR 425AL 426AR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YEGE427AL 428AR 427 LATCH ATTACHMENTS).ORLATCH ACCESS DOOR 428A330-300GE783202-01-2 N/A TASK DELETED783202-02-1 415BL 416BR 417AL 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, T: 3 YEZL-417-02-2 PW418AR 425BL 426BR 418 ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND I: 3 YE427AL 428AR 427 LATCH ATTACHMENTS).LATCH ACCESS DOOR 428783202-02-2 N/A TASK DELETED783203-01-1 DEPLOY TRANSLATING 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER T: 3 YEZL-417-02-2 PWCOWL 418 TRANSLATING COWL T-SLIDER, ATTACHMENTS AND I: 3 YE427 SURROUNDING STRUCTURE (15 CM AROUND T-SLIDER428 ATTACHMENTS).783245-01-1 418HR 418JR 428HR 417 SPECIAL DETAILED INSPECTION OF THRUST REVERSER T: 3 YERR428JR 418 LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 3 YE427 FITTINGS).428783245-02-1 N/A TASK DELETED783245-02-2 418HR 418JR 428HR 417 GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES T: 6 YE NO CPCP RR428JR 418 AND SURROUNDING STRUCTURE (15 CM AROUND LATCH I: 6 YE427 FITTINGS).428* * * * * E N D * * * * *ISSUE: JUL 01/10 EXHAUST SECTION: D-78PAGE 2

# 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 accid ental 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 m anufacturer in accordance with the Structures

Reporting System (Refer to Appendix 8).

3. INSPECTIONS MORE FREQUENT THAN 'A' CHECK

The routine content of inspections with frequencies below 'A'-check shall be developed by the

operator. Consequently, even when the Zonal working group has used its experience or

engineering judgement to select an interval below 'A' check, this has not been included in the

Zonal section. However, since the justification for these inspections was based on the likelihood of

random accidental damage, they have been stated below for completeness.

It is recommended that these inspections are consid ered by all operators, for inclusion in their

routine maintenance programs. Recommended intervals are provided where no similar

inspections already exist on comparable fleets.

It is recognised that these inspections are of a lesser intensity than a General Visual Inspection,

since they are to be performed 'from the ground, as far as visible'.

RECOMMENDED

ZONE DESCRIPTION CALENDAR

INTERVAL

100 Lower half of fuselage 36 hours

200 Upper half of fuselage 36 hours

300 Empennage and fuselage tail 36 hours

400 Power plants, nacelles and pylons 36 hours

500/600 Wings, L/H and R/H 36 hours

# 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 REPORTIssue : July 2010Page : E-INTRO-4Sequence number: Indicates separate tasks within the sameZone number: Indicates the zone numberAbbreviation for ZonalApplicablity index: Identifies successive variants of the TaskZL–XXX–XX -X6. EXPLANATION OF ZONAL SECTION FORMATDetailed information is given below concerning the format of the inspection requirements provided on subsequent pages.TASKREFERENCEACCESSZONEDESCRIPTIONINTERVALMSI / SSIREFERENCEAPPLICABILITY123 45 671- This column indicates the zonal task number, e.g. ZL 151-01-1. It is composed of 9 digits as follows: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 ATA 100breakdown, showing the major section where the zone is located e.g 100 Lower Half of Fuselage. The second digit, 151-01-01, is also in accordancewith the A330 ATA 100 breakdown, showing the sub section where the zone is located e.g 150 Aft Cargo Compartment. The third digit, 151 01-1, showsthe 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. It identifies different depthinspections at different intervals . These two digits are also changed when the inspections have a major difference in access (e.g. actuator removal).The Applicability Index is composed of one digit. It follows the Sequential Number and is separated by a dash, 151-01-01. It identifies differentapplicability e.g aircraft series, mod status etc ...This digit is also used to differentiate between minor access differences e.g. different access panelnumbers and differences in reference information.2- This column indicates the access and preparation requirements to adequately perform the inspection.A330 MRB REPORTIssue : July 2010Page : E-INTRO-5(i) It lists all access panels, doors and fairings or indicates boundaries between the access panels have to be opened or removed(ii)It defines the configuration of the aircraft, if necessarye.g. "Slats and flaps extended"(iii) The removal or displacement of insulation is indicated by either 'Insulation' or 'NOTE 1' respectively.(iv) To take account of customisation and the Flexible Cabin Concept :- Galleys, toilets, stairhouse, ACT and crew rest rooms are quoted in conjunction with the note "If installed"-Floor panels are not given individual panel numbers, the term "Floor panels from FR XX TO FR XY " is used for simplicity.3- This column indicates the Zone(s).4- This column provides the description of the Zone, which is shown underlined. In certain cases, additional information is provided in brackets to precisethe Inspection areae.g. ELEVATOR(AREA BETWEEN RIBS 8 AND 9)5- This column provides the inspection interval.For the ZIP the threshold is equal to the interval. The interval starts at the time of the last inspection performed.6- A task reference information lists all MSI and SSI General Visual Inspection tasks which are contained in and covered by.7- This column indicates the A/C model/Mod status/engine type to which this requirement is applicable.This page intentionally left blankAPPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-100-01-2 N/A 100 LOWER HALF OF FUSELAGE I: C MSI NONE ALLSSI 531116-01-1SSI 531167-01-1SSI 532101-01-1SSI 533101-01-1SSI 533193-01-2SSI 534126-01-1SSI 534130-01-1R ZL-110-01-1 110AL 110 RADOME (EWIS) I: 2 C MSI NONE ALLSSI NONER ZL-121-01-1 132AZ 821 121 AVIONICS COMPARTMENT (EWIS) I: C MSI NONE ALL122SSI NONER ZL-121-02-1 121AF 121BF 121CF 121 AVIONICS COMPARTMENT (EWIS) I: 4 C MSI 21.26.00/05 ALL121DF 121EF 121FF 122 MSI 21.27.00/02121GF 121HF 121KF122CF 122DF 122FF SSI NONE122GF 122HF 122JF122KF 122LF 122NF122PF 131AW 131BW132AZ 132CW 821NOTE 1ZL-121-02-2 N/A TASK DELETED MSI NONESSI NONER ZL-123-01-1 713 714 123 NOSE GEAR WELL (EWIS) I: C MSI NONE ALLSSI NONEN ZL-125-01-1 125AL 125BL 125CL 125 NOSE FAIRING, FR10 TO BETWEEN FR21 AND FR22, LH/RH. I: 48 MO MSI NONE A330-200F125DL 125EL 125FL 126125GL 125HL 126BR SSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-125-01-1 * * * * * C O N T I N U E * * * * *126CR 126FRR ZL-131-01-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: A MSI 25.51.00/04 ALL132 MSI 25.51.00/05MSI 25.51.00/06MSI 25.51.00/07MSI 25.51.00/09MSI 25.51.00/11MSI 25.51.00/12MSI 25.51.00/13MSI 25.51.00/17MSI 25.51.00/18MSI 25.51.01/05MSI 25.51.01/06MSI 25.51.01/07MSI 25.51.01/09MSI 25.51.01/11MSI 25.51.01/12MSI 25.51.01/13MSI 25.51.01/14MSI 25.51.01/15SSI NONER ZL-131-02-1 131BC 131FC 131KC 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-300131KW 131MC 131PC 132131QW 131RC 131TC SSI NONE131VC 132QW 132SW132UW 821R ZL-131-02-2 131BC 131FC 131FX 131 FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-200131KW 131PC 131RC 132131TC 131VC 131XC SSI NONE132FX 132UW 132WW821N ZL-131-02-3 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200F132SSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-131-02-3 * * * * * C O N T I N U E * * * * *SIDEWALL AND CEILINGPANELS FROM FR 20 TOFR 39.2R ZL-131-03-1 821 131 FORWARD CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 ALLNOTE 1 132SIDEWALL AND CEILING SSI 532103-01-1PANELS FROM FR 20 TOFR 39.2ZL-131-04-1 N/A TASK DELETED MSI NONESSI NONER ZL-133-01-1 133AL 133BL 821 133 BAY UNDER FWD CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 ALLFLOOR PANELS FROM 134 MSI 25.55.00/03FR20 TO FR 39.2 MSI 38.32.00/01NOTE 1SSI NONER ZL-137-01-1 131BX 131CG 131CX 137 BAY BEHIND FORWARD CARGO COMPARTMENT (EWIS) I: 4 C MSI 21.50.00/07 ALL131DG 131DX 132CG 138132CX 132DG 132DX SSI NONE821R ZL-141-01-1 147AZ 148AZ 734 141 CENTER WING BOX (EWIS) I: 8 C MSI NONE ALL744 142SSI 571154-01-1D ZL-141-01-2 N/A CENTER WING TANK MSI NONETASK DELETED SSI NONEZL-141-03-1 N/A TASK DELETED MSI NONESSI NONEISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-143-01-1 734 744 143 AREA BETWEEN KEEL BEAMS (EWIS) I: 8 C MSI NONE ALLSSI NONER ZL-145-01-1 834 844 145 ZONE UNDER CABIN FLOOR (EWIS) I: 8 C MSI NONE ALLFLOOR PANELS FROM FR 14640 TO FR 53.2 SSI NONER ZL-147-01-1 734 744 147 MLG WELL AND HYDRAULICS COMPARTMENT (EWIS) I: A MSI 29.10.00/17 ALL148SSI NONEZL-149-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-149-05-1 149AB 149CB 734 149 CENTER LINE BAY (EWIS) I: 8 C MSI NONE ALL744SSI NONER ZL-151-01-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: A MSI 25.51.00/04 ALL152 MSI 25.51.00/05(AS FAR AS VISIBLE IF LD-MCR AND/OR LDL INSTALLED) MSI 25.51.00/06MSI 25.51.00/07MSI 25.51.00/09MSI 25.51.00/11MSI 25.51.00/12MSI 25.51.00/13MSI 25.51.00/17MSI 25.51.01/05MSI 25.51.01/06MSI 25.51.01/07MSI 25.51.01/09MSI 25.51.01/11MSI 25.51.01/12MSI 25.51.01/13MSI 25.51.01/14MSI 25.51.01/15SSI NONEISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 4APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-151-02-1 151BC 151BW 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-300151HC 151JW 151KC 152151PC 151TW 152BW SSI NONE152DW 152EW 152GW152JW 152LW 822LD-MCR-IF INSTALLEDR ZL-151-02-2 151BW 151BY 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-200151HC 151JW 151KC 152151PC 151TW 152AX SSI NONE152BW 152BX 152DW152JW 152LW 822LD-MCR-IF INSTALLEDR ZL-151-02-3 151BC 151BW 151FC 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-200151JW 151TW 152BW 152WITHOUT LD-MCR152DW 152EW 152GW SSI NONE WITHOUT LDL152JW 822R ZL-151-02-4 151EC 151FX 151HX 151 AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-200151LX 151NC 152FX 152WITH LDL152HX 152LX 822 SSI NONELAVATORIES AND LDL-FURNISHINGLD-MCR-IF INSTALLEDN ZL-151-02-5 822 000 AFT CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200FSIDEWALL AND CEILINGPANELS FROM FR 53.2 SSI NONETO FR 66R ZL-151-03-1 822 151 AFT CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 ALLLD-MCR-IF INSTALLED 152NOTE 1 SSI NONESIDEWALL AND CEILINGPANELS FROM FR 53.2TO FR 66ZL-151-04-1 N/A TASK DELETED MSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 5APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-151-04-1 * * * * * C O N T I N U E * * * * *SSI NONER ZL-153-01-1 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A330-300FLOOR PANELS FROM FR 154 MSI 25.55.00/03 OR53.2 TO FR 66, MSI 38.32.00/01 A330-200FLD-MCR-IF INSTALLEDORNOTE 1 SSI NONE A330-200WITHOUT LDLR ZL-153-01-2 154AR 822 153 BAY UNDER AFT CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A330-200FLOOR PANELS FROM FR 154 MSI 38.32.00/01 WITH LDL53.2 TO FR66LDL - LAVATORIES AND SSI NONEFURNISHINGLD-MCR-IF INSTALLEDNOTE 1R ZL-161-01-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: A MSI 25.54.00/03 ALL162 MSI 38.32.00/02(IF FLIGHT KIT CONTAINER INSTALLED, AS FAR ASVISIBLE) SSI NONER ZL-161-02-1 161AC 161BC 161CW 161 BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI NONE A330-200161EC 162LW 162RW 162OR162SW 162TW 162WW SSI NONE A330-300822N ZL-161-02-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 72 MO MSI NONE A330-200FFLIGHT KIT CONTAINER 162REMOVED, IF SSI NONEINSTALLEDSIDEWALL AND CEILINGPANELS FROM FR 65 TOFR 73R ZL-161-03-1 822 161 BULK CARGO COMPARTMENT (EWIS) I: 8 C MSI 38.32.00/02 A330-200NOTE 1 162OR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 6APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-161-03-1 * * * * * C O N T I N U E * * * * *SIDEWALL AND CEILING SSI NONE A330-300PANELS FROM FR 65 TOFR 73N ZL-161-03-2 822 161 BULK CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FFLIGHT KIT CONTAINER 162REMOVED, IF SSI NONEINSTALLEDNOTE 1SIDEWALL AND CEILINGPANELS FROM FR 65 TOFR 73R ZL-163-01-1 164AR 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 4 C MSI 25.52.00/05 A330-200FLOOR PANELS FROM FR 164OR65 TO FR 73 SSI NONE A330-300NOTE 1N ZL-163-01-2 822 163 BAY UNDER BULK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.52.00/05 A330-200FFLIGHT KIT CONTAINER 164REMOVED, IF SSI NONEINSTALLEDFLOOR PANELS FROM FR65 TO FR 73NOTE 1R ZL-171-01-1 162ZW 171AL 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: C MSI NONE A330-200172ORSSI NONE A330-300N ZL-171-01-2 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 24 MO MSI NONE A330-200F172SSI NONER ZL-171-02-1 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 4 C MSI 38.31.00/02 A330-200FLOOR PANELS FROM FR 172 MSI 38.32.00/01 OR73 TO FR 80A330-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 7APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-171-02-1 * * * * * C O N T I N U E * * * * *NOTE 1 SSI 535122-01-1N ZL-171-02-2 162ZW 822 171 AFT CABIN UNDERFLOOR COMPARTMENT (EWIS) I: 72 MO MSI NONE A330-200FFLOOR PANELS FROM FR 17273 TO FR 80 SSI 535122-01-1NOTE 1R ZL-191-01-1 191FB 191KB 192JB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 21.25.00/03 ALL192PB 192SSI NONER ZL-191-02-1 191AB 191AT 191BB 191 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 ALL191BT 191CB 191CT 192191DB 191EB 191FB SSI NONE191HB 191KB 191QB192AT 192BB 192BT192CB 192CT 192GB192HB 192JB 192MB192NB 192PB 192QBR ZL-193-01-1 193BB 193DB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 2 C MSI 21.25.00/03 ALLSSI NONER ZL-193-02-1 193AB 193BB 193CB 193 AIR CONDITIONING COMPARTMENT AND FAIRING (EWIS) I: 4 C MSI 21.50.00/07 ALL193DBSSI NONER ZL-195-01-1 734 744 195 HYDRAULIC COMPARTMENT AND FAIRINGS (AS FAR AS I: A MSI NONE ALL196 VISIBLE) (EWIS)SSI NONER ZL-195-02-1 195AB 195BB 196AB 195 HYDRAULIC COMPARTMENT AND FAIRINGS (EWIS) I: 2 C MSI 21.25.00/03 ALL196BB 196 MSI 29.10.00/17* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 8APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-195-02-1 * * * * * C O N T I N U E * * * * *SSI NONER ZL-197-01-1 734 744 197 REAR FAIRINGS (EWIS) I: A MSI NONE ALL198SSI NONER ZL-197-02-1 197EB 198EB 197 REAR FAIRINGS (EWIS) I: 4 C MSI NONE ALL198SSI NONE* * * * * E N D * * * * *ISSUE: JUL 01/10 LOWER HALF OF FUSELAGE SECTION: E-100PAGE 9APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-200-01-1 N/A 200 UPPER HALF OF FUSELAGE I: 2 C MSI NONE ALLSSI 531103-01-1SSI 531107-01-1SSI 531111-01-1SSI 532117-01-2SSI 532121-01-1SSI 532145-02-1SSI 532166-01-2SSI 532167-01-1SSI 532175-01-1SSI 533101-01-1SSI 533193-01-2SSI 534122-01-2SSI 534124-01-1SSI 534130-01-1SSI 534167-01-1SSI 534177-01-2R ZL-211-01-1 211JW 211KW 212JW 211 COCKPIT (EWIS) I: 2 C MSI NONE ALL212KW 831 841 212SSI NONER ZL-211-02-1 211AC 211AW 211BC 211 COCKPIT (EWIS) I: 8 C MSI NONE ALL211BW 211CC 211CW 212211DC 211DW 211EC SSI 531156-01-1211EW 211FC 211FW SSI 531170-01-1211GC 211GW 211HC211HW 211JC 211JW211KC 211KW 211LC211LW 211MC 211MW211PW 212BC 212CC212CW 212DC 212DW212EW 212FC 212FW212GC 212GW 212HC212HW 212JC 212JW212KW 212LW 212MW212NC 212NW 212QW831 841FLOOR PANELS FROM FR1 TO FR 11NOTE 1ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-221-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-221-02-1 831 841 221 FWD CABIN UTILITY AREA (EWIS) I: 8 C MSI 25.74.00/02 A330-200CREW REST ROOM IF 222ORINSTALLED SSI 531156-01-1 A330-300DOOR FRAME LININGFLOOR PANELS FROM FR11 TO FR 17GALLEYS AND TOILETSIF INSTALLEDNOTE 1SEATS ANDFURNISHINGSN ZL-221-03-1 831 841 221 COURIER COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FFCRC, GALLEYS AND 222TOILETS IF INSTALLED SSI NONENOTE 1SEATS ANDFURNISHINGSSIDEWALL AND DOORFRAME LINING ANDFLOOR PANELS FROMFRAME FR 11/11A TOFR 19/20R ZL-223-01-1 221AZ 221BZ 222AZ 223 FWD CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 25.74.00/02 A330-200222BZ 831 841 224ORCEILING PANELS SSI 531156-01-1 A330-300FCRC, GALLEYS ANDTOILETS - IFINSTALLED FROM FR 11TO FR 17NOTE 1N ZL-223-02-1 831 841 223 COURIER OVERHEAD COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200F224SSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-223-02-1 * * * * * C O N T I N U E * * * * *CEILING PANELS ANDUPPER SIDEWALLLININGS FROM FR11/11A TO FR 19/20FCRC, GALLEYS ANDTOILETS IF INSTALLEDNOTE 1ZL-231-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-231-02-1 831 841 231 FWD CABIN (EWIS) I: 8 C MSI NONE A330-200GALLEYS AND TOILETS 232ORIF INSTALLED SSI 532119-01-1 A330-300NOTE 1 SSI 532135-01-1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 17 TOFR 31N ZL-231-03-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 25.55.00/02 A330-200FBARRIER WALL (AFT 232 OR MSI 25.55.00/04FACE) INCLUDING 6 MO MSI 25.56.00/05UPPER SURFACE (ZONE MSI 25.56.00/06233/234), BARRIER MSI 25.56.00/07WALL ACCESS DOORS, MSI 25.56.00/08LH/RH MSI 25.56.00/09MSI 25.56.00/10MSI 25.56.00/11MSI 25.56.00/12SSI NONEN ZL-231-04-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200F232SSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-231-04-1 * * * * * C O N T I N U E * * * * *FLOOR PANELS BETWEENFR 19/20 AND FR 31,LOWER SIDEWALLLININGS (DADOPANELS)NOTE 1N ZL-231-05-1 835 231 FWD MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 232SIDEWALL LININGS SSI NONEFROM FR 19/20 TO FR31.R ZL-233-01-1 831 841 233 FWD CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A330-200CEILING PANELS 234ORGALLEYS AND TOILETS SSI 532120-01-1 A330-300IF INSTALLEDNOTE 1OVERHEAD STOWAGEBINS FROM FR 17 TOFR 31N ZL-233-02-1 835 233 FWD MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FUPPER SIDEWALL 234LININGS BETWEEN FR SSI NONE19/20 AND FR 31ZL-241-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-241-02-1 832 842 241 MID CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A330-200DOOR FRAME LINING 242ORAND FLOOR PANELS SSI 532119-01-1 A330-300FROM FR 31 TO FR 36 SSI 532135-01-1GALLEYS AND TOILETSIF INSTALLEDNOTE 1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 4APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-241-02-1 * * * * * C O N T I N U E * * * * *SEATS ANDFURNISHINGSN ZL-241-03-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 800 FH MSI 25.55.00/02 A330-200F242 OR MSI 25.56.00/086 MO MSI 25.56.00/09MSI 25.56.00/10MSI 25.56.00/11SSI NONEN ZL-241-04-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 72 MO MSI 25.55.00/03 A330-200FFLOOR PANELS BETWEEN 242FR 31 AND FR 36 SSI NONELOWER SIDEWALL (DADOPANELS)NOTE 1N ZL-241-05-1 835 241 FWD MID MAIN DECK CARGO COMPARTMENT AREA (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 242SIDEWALL LININGS SSI NONEBETWEEN FR 31 AND FR36R ZL-243-01-1 832 842 243 MID CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A330-200CEILING PANELS FROM 244ORFR 31 TO FR 36 SSI 532120-01-1 A330-300GALLEYS AND TOILETSIF INSTALLEDNOTE 1N ZL-243-02-1 835 243 FWD MID MAIN DECK OVERHEAD CARGO COMPARTMENT AREA I: 144 MO MSI NONE A330-200FNOTE 1 244 (EWIS)UPPER SIDEWALL SSI NONELININGS FROM FR 31TO FR 36ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 5APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-251-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-251-02-1 834 842 251 MID CABIN (EWIS) I: 8 C MSI 25.75.00/05 A330-200GALLEYS, TOILETS AND 252ORSTAIRHOUSE (IF SSI 533148-01-1 A330-300INSTALLED)NOTE 1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 36 TOFR 53.5N ZL-251-03-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 25.55.00/02 A330-200F252 OR MSI 25.56.00/086 MO MSI 25.56.00/10MSI 25.56.00/11SSI NONEN ZL-251-04-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200FFLOOR PANELS BETWEEN 252FR 36 AND FR 53.5 SSI NONELOWER SIDEWALLLININGS (DADOPANELS)NOTE 1N ZL-251-05-1 835 251 MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 252SIDEWALL LININGS SSI 533185-01-1BETWEEN FR 36 TO FR53.5R ZL-253-01-1 832 842 253 MID CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI 25.75.00/05 A330-200CEILING PANELS 254ORSSI 533147-01-2 A330-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 6APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-253-01-1 * * * * * C O N T I N U E * * * * *GALLEYS, TOILETS ANDSTAIRHOUSE (IFINSTALLED) FROM FR36TO FR53.5NOTE 1OVERHEAD STOWAGEBINSN ZL-253-02-1 835 253 MID MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 254UPPER SIDEWALL SSI 533185-01-1LININGS BETWEEN FR36 TO FR 53.5ZL-261-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-261-02-1 834 844 261 AFT CABIN (EWIS) I: 8 C MSI NONE A330-200DOOR FRAME LINING 262ORGALLEYS AND TOILETS SSI 534157-01-1 A330-300IF INSTALLED SSI 534161-01-1NOTE 1SEATS ANDFURNISHINGSSIDEWALL AND FLOORPANELS FROM FR 53.5TO FR 72N ZL-261-03-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 25.55.00/02 A330-200F262 OR MSI 25.56.00/086 MO MSI 25.56.00/10MSI 25.56.00/11SSI NONEN ZL-261-04-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200F262* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 7APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-261-04-1 * * * * * C O N T I N U E * * * * *FLOOR PANELS BETWEEN SSI NONEFR 53.5 TO FR 72LOWER SIDEWALLLININGS (DADOPANELS)NOTE 1N ZL-261-05-1 835 261 AFT MID MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 262SIDEWALL LININGS SSI NONEBETWEEN FR 53.5 TOFR 72R ZL-263-01-1 834 844 263 AFT CABIN OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A330-200CEILING PANELS 264ORGALLEYS AND TOILETS SSI 534160-01-1 A330-300(IF INSTALLED) FROMFR 53.5 TO FR 72NOTE 1OVERHEAD STOWAGEBINSN ZL-263-02-1 835 263 AFT MID MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 264UPPER SIDEWALL SSI NONELININGS FROM FR 53.5TO FR 72ZL-271-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-271-02-1 833 843 271 AFT CABIN UTILITY AREA (EWIS) I: 8 C MSI NONE A330-200DOOR FRAME LININGS, 272ORSIDEWALL AND FLOOR SSI 534157-01-1 A330-300PANELS FROM FR 72 TO SSI 534161-01-1FR 80 SSI 535121-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 8APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-271-02-1 * * * * * C O N T I N U E * * * * *GALLEYS AND TOILETSIF INSTALLEDNOTE 1SEATS ANDFURNISHINGSN ZL-271-03-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 800 FH MSI 25.55.00/02 A330-200F272 OR MSI 25.55.00/046 MO MSI 25.56.00/07MSI 25.56.00/08MSI 25.56.00/10MSI 25.56.00/11SSI NONEN ZL-271-04-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 72 MO MSI 25.55.00/03 A330-200FFLOOR PANELS BETWEEN 272FR 72 TO FR 80/82 SSI NONELOWER SIDEWALL (DADOPANELS)NOTE 1N ZL-271-05-1 835 271 AFT MAIN DECK CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200FNOTE 1 272SIDEWALL LININGS SSI 535121-01-1BETWEEN FR 72 TO FR80/82R ZL-273-01-1 271AZ 271BZ 271CZ 273 AFT CABIN UTILITY AREA OVERHEAD COMPARTMENT (EWIS) I: 8 C MSI NONE A330-200272AZ 272BZ 272CZ 274OR833 843 SSI 534160-01-1 A330-300CEILING PANELS FROM SSI 535121-01-1FR 72 TO FR 80GALLEYS AND TOILETSIF INSTALLEDNOTE 1N ZL-273-02-1 835 273 AFT MAIN DECK OVERHEAD CARGO COMPARTMENT (EWIS) I: 144 MO MSI NONE A330-200F* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 9APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-273-02-1 * * * * * C O N T I N U E * * * * *NOTE 1 274 SSI 535121-01-1UPPER SIDEWALLLININGS FROM FR 72TO FR 80/82* * * * * E N D * * * * *ISSUE: JUL 01/10 UPPER HALF OF FUSELAGE SECTION: E-200PAGE 10APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-300-01-1 N/A 300 STABILIZERS AND FUSELAGE REAR SECTION I: 2 C MSI NONE ALLSSI 535111-01-1SSI 535111-02-1SSI 535114-01-1SSI 551020-02-2SSI 551021-01-1SSI 551026-01-2SSI 552001-01-2SSI 554001-01-2SSI 554014-01-1SSI 554020-01-1SSI 554029-01-1R ZL-311-01-1 312AR 313AL 311 REAR FUSELAGE SECTIO (EWIS) I: C MSI 28.22.00/05 ALL312 MSI 49.16.00/01-35SSI 535123-01-1SSI 551007-01-2SSI 551010-01-2SSI 551012-01-2SSI 551015-01-1SSI 551015-01-3R ZL-313-01-1 313AL 313 TAIL CONE APU AIR INTAKE AREA (EWIS) I: C MSI 28.22.00/05 ALL314 MSI 49.16.00/01-35SSI NONER ZL-315-01-1 315AL 316AR 315 TAIL CONE, APU AND ACCESSORY COMPARTMENT (EWIS) I: C MSI 49.17.00/02-35 ALL316SSI NONER ZL-317-01-1 317AL 317 TAIL CONE, APU EXHAUST AREA (EWIS) I: C MSI 49.17.00/02-35 ALLSSI NONEZL-319-01-1 N/A TASK DELETED MSI NONESSI NONEISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-319-02-1 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL)(EWIS) I: 8 C MSI NONE A330-200319AR 319BL 319BRPRE 41600319CR SSI 551018-01-3 ORDISCONNECT SCAVENGEA330-300WATER SYSTEM PIPEPRE 41600R ZL-319-02-2 312AR 313AL 319AL 319 HORIZONTAL STABILIZER CENTER BOX (INTERNAL)(EWIS) I: 8 C MSI NONE A330-200319AR 319BL 319DRPOST 41600319ER SSI 551018-01-4 ORA330-300POST 41600ORA330-200FR ZL-321-01-1 321AL 321 DORSAL FIN (EWIS) I: 8 C MSI NONE ALLSSI NONER ZL-322-01-1 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A330-300SSI 553010-01-2R ZL-322-01-2 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A330-200322DLPRE 48979SSI 553022-01-1R ZL-322-01-3 322AL 322BL 322CL 322 VERTICAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE A330-200322ELPOST 48979SSI 553022-01-2 ORA330-200FR ZL-323-01-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 4 C MSI NONE ALLSSI 553011-01-2SSI 553023-01-1SSI 553023-01-2R ZL-323-02-1 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI NONE A330-300* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-323-02-1 * * * * * C O N T I N U E * * * * *322AL 322BL 322CL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 553013-01-2323AL 323BL 325AL FITTINGS)325BL 325CL 325DL325EL 325FL 325GL325HL 325JL 325KLPEELABLE HOLE COVERSR ZL-323-02-2 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI NONE A330-200322AL 322BL 322CLPRE 48979322DL 323CL 323DL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 553025-01-1325LL 325ML 325NL FITTINGS)325PL 325QL 325RLPEELABLE HOLE COVERSR ZL-323-02-3 311AZ 311BZ 312AR 323 VERTICAL STABILIZER SPAR BOX (EWIS) I: 8 C MSI NONE A330-200322AL 322BL 322CLPOST 48979322EL 323DL 323EL (INCLUDING FIN TO FUSELAGE ATTACHMENT AREA AND SSI 553025-01-2 OR325LL 325NL 325SL FITTINGS)A330-200F325TL 325UL 325VLPEELABLE HOLE COVERSZL-323-03-1 N/A TASK DELETED MSI NONESSI NONER ZL-324-01-1 324AT 324BT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A330-300SSI 553010-01-2R ZL-324-01-2 324CT 324 VERTICAL STABILIZER TIP (EWIS) I: 8 C MSI NONE A330-200ORSSI 553022-01-1 A330-200FSSI 553022-01-2SSI 553025-01-1SSI 553025-01-2ZL-324-02-1 N/A TASK DELETED MSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-324-02-1 * * * * * C O N T I N U E * * * * *SSI NONER ZL-325-01-1 325DL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A330-300SSI NONER ZL-325-01-2 325NL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE A330-200ORSSI NONE A330-200FR ZL-325-02-1 325AL 325BL 325CL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A330-300325DL 325EL 325FL325GL 325HL 325JL SSI 553009-01-2325KLR ZL-325-02-2 325LL 325ML 325NL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A330-200325PL 325QL 325RLPRE 48979SSI 553021-01-1R ZL-325-02-3 325LL 325NL 325SL 325 VERTICAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE A330-200325TL 325UL 325VLPOST 48979SSI 553021-01-2 ORA330-200FZL-325-03-1 N/A TASK DELETED MSI NONESSI NONEZL-325-04-1 N/A TASK DELETED MSI NONESSI NONER ZL-326-01-1 326DL 326 RUDDER (EWIS) I: C MSI NONE A330-300(AREA OF BEARINGS 2, 3 AND 4) SSI NONEISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 4APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-326-01-2 325NL 326ML 326NL 326 RUDDER (EWIS) I: C MSI NONE A330-200326PLOR(AREA OF BEARINGS 2, 3, 4 AND 5) SSI NONE A330-200FR ZL-326-02-1 326BL 326DL 326FL 326 RUDDER (EWIS) I: 4 C MSI NONE A330-300326HL 326KLPRE 40904(AREA OF BEARINGS 1 TO 7) SSI NONER ZL-326-02-2 325BL 325FL 325HL 326 RUDDER (EWIS) I: 4 C MSI NONE A330-300325KL 326DLPOST 40904(AREA OF BEARINGS 1 TO 7) SSI NONER ZL-326-02-3 325ML 325NL 325PL 326 RUDDE (EWIS) I: 4 C MSI NONE A330-200325QL 325RL 326MLPRE 48979326NL 326PL 326QL (AREA OF BEARINGS 1 TO 8) SSI NONER ZL-326-02-4 325NL 325SL 325TL 326 RUDDER (EWIS) I: 4 C MSI NONE A330-200325UL 325VL 326MLPOST 48979326NL 326PL 326RL (AREA OF BEARINGS 1 TO 8) SSI NONE OR326SLA330-200FR ZL-326-03-1 325AL 325BL 325DL 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI NONE A330-300325FL 325HL 325KL FAR ASVISIBLE) (EWIS)PRE 40904326AL 326BL 326BR SSI NONE326CL 326DL 326DR326EL 326FL 326FR326GL 326HL 326HR326JL 326KL 326KR326LLR ZL-326-03-2 325AL 325BL 325CL 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI NONE A330-300325CR 325DL 325EL FAR AS VISIBLE) (EWIS)POST 40904325ER 325FL 325GL SSI NONE325GR 325HL 325JL325JR 325KL 326AT326DL 326DRISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 5APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-326-03-3 324CT 325LL 325LR 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI NONE A330-200325ML 325MR 325NL FAR AS VISIBLE) (EWIS)PRE 48979325NR 325PL 325PR SSI NONE325QL 325QR 325RL325RR 326AT 326ML326NL 326PL 326QLR ZL-326-03-4 324CT 325LL 325LR 326 RUDDER (FRONT SPAR FWD FACE AND INTERNAL STRUCTURE AS I: 8 C MSI NONE A330-200325NL 325NR 325SL FAR AS VISIBLE)(EWIS)POST 48979325SR 325TL 325TR SSI NONE OR325UL 325UR 325VLA330-200F325VR 326AT 326ML326NL 326PL 326RL326SLZL-326-04-1 N/A TASK DELETED MSI NONESSI NONEZL-326-05-1 N/A TASK DELETED MSI NONESSI NONEZL-326-06-1 N/A TASK DELETED MSI NONESSI NONEZL-326-07-1 N/A TASK DELETED MSI NONESSI NONEZL-326-08-1 N/A TASK DELETED MSI NONESSI NONER ZL-331-01-1 331AT 331BT 331CT 331 HORIZONTAL STABILIZER LEADING EDGE (EWIS) I: 8 C MSI NONE ALL331DT 331ET 333AB 341333AT 341AT 341BT SSI 551024-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 6APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-331-01-1 * * * * * C O N T I N U E * * * * *341CT 341DT 341ET SSI 551024-01-2343AB 343AT SSI 551025-01-2R ZL-332-01-1 332AB 332AT 342AB 332 HORIZONTAL STABILIZER TIP (EWIS) I: 8 C MSI NONE ALL342AT 342SSI 551025-01-2R ZL-333-01-1 331AT 331BT 333AB 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI NONE ALL333AL 333AT 341AT 343341BT 343AB 343AR (RIB 3 TO RIB 4) SSI NONE343ATR ZL-333-01-2 331ET 332AB 332AT 333 HORIZONTAL STABILIZER LATERAL BOX (EWIS) I: 8 C MSI NONE A330-200333EL 343POST 43491(RIB 13 TO END RIB LH) SSI 551035-02-1 PRE 448180RA330-300POST 43491PRE 44818R ZL-334-01-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: C MSI NONE ALL344AB 344BB 344CB 344(FUSELAGE FAIRING TO RIB 10) SSI NONER ZL-334-02-1 334AB 334BB 334CB 334 HORIZONTAL STABILIZER TRAILING EDGE (EWIS) I: 4 C MSI NONE ALL334DB 334EB 334FB 344334GB 344AB 344BB (FUSELAGE FAIRING TO RIB 21) SSI 551030-01-2344CB 344DB 344EB344FB 344GBR ZL-335-01-1 334BB 334CB 334DB 335 ELEVATOR (EWIS) I: C MSI NONE ALL335BB 344BB 344CB 345344DB 345BB (AREA BETWEEN RIBS 8 AND 9) SSI NONEISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 7APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-335-02-1 334AB 334BB 334CB 335 ELEVATOR (EWIS) I: 8 C MSI NONE ALL334DB 334EB 334FB 345334GB 335AB 335BB (LEADING EDGE STRUCTURE AS FAR AS VISIBLE) SSI NONE335CB 335DB 335EB335FB 344AB 344BB344CB 344DB 344EB344FB 344GB 345AB345BB 345CB 345DB345EB 345FB* * * * * E N D * * * * *ISSUE: JUL 01/10 FUSELAGE TAIL SECTION: E-300PAGE 8APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-400-01-1 N/A 400 POWER PLANTS, NACELLES AND PYLONS I: A MSI 72.33.00/01-PW ALLSSI NONEZL-400-01-2 N/A TASK DELETED MSI NONESSI NONEZL-411-01-1 N/A TASK DELETED MSI NONESSI NONEZL-411-02-1 N/A TASK DELETED MSI NONESSI NONER ZL-411-03-1 411AL 411AR 411BL 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI 30.21.01/03 A330-200421AL 421AR 421BL 421GESSI NONE ORA330-300GER ZL-411-03-2 411AL 411AR 421AL 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 4 C MSI NONE PW421AR 421ORSSI NONE RRR ZL-411-04-1 411AL 411AR 411AZ 411 ENGINE AIR INTAKE AND INTAKE LIP (EWIS) I: 8 C MSI NONE A330-200411BL 411BZ 411CZ 421GE411DZ 411EZ 415AL SSI NONE OR416AR 421AL 421ARA330-300421AZ 421BL 421BZGE421CZ 421DZ 421EZ425AL 426ARZL-412-01-1 N/A TASK DELETED MSI NONESSI NONEISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-412-02-1 415AL 416AR 417AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI NONE A330-200418AR 425AL 426AR 422GE427AL 428AR SSI NONE ORA330-300GER ZL-412-02-2 415AL 415BL 416AR 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 72.33.00/02-PW PW416BR 425AL 425BL 422426AR 426BR SSI NONER ZL-412-02-3 415AL 416AR 425AL 412 FAN AND ACCESSORY GEAR BOX (EWIS) I: C MSI 71.12.00/03-RR RR426AR 422 MSI 71.61.00/02-RRSSI NONEZL-413-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-413-02-1 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI NONE A330-200418AR 425AL 426AR 423GE427AL 428AR SSI NONE ORA330-300GER ZL-413-02-2 415AL 415BL 416AR 413 HOT SECTION (EWIS) I: C MSI NONE PW416BR 417AL 418AR 423425AL 425BL 426AR SSI NONE426BR 427AL 428ARR ZL-413-02-3 415AL 416AR 417AL 413 HOT SECTION (EWIS) I: C MSI 72.03.00/01-RR RR418AR 425AL 426AR 423427AL 428AR SSI NONEZL-414-01-1 N/A TASK DELETED MSI NONESSI NONEISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-414-02-1 414AL 414AR 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI NONE A330-200424GESSI NONE ORA330-300GER ZL-414-02-2 415BL 416BR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI NONE PW418AR 425BL 426BR 424427AL 428AR SSI NONER ZL-414-02-3 415AL 416AR 417AL 414 EXHAUST NOZZLE (EWIS) I: 2 C MSI NONE RR418AR 425AL 426AR 424427AL 428AR SSI NONEZL-415-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-415-02-1 415AL 415BL 416AR 415 FAN COWL (EWIS) I: 2 C MSI NONE A330-200416BR 425AL 425BL 416GE426AR 426BR 425 SSI 711141-01-1 OR426 SSI 711142-01-1 A330-300SSI 711341-02-1 GER ZL-415-02-2 415AL 415BL 415CL 415 FAN COWL (EWIS) I: 2 C MSI NONE PW416AR 416BR 425AL 416425BL 425CL 426AR 425 SSI 711301-02-1426BR 426 SSI 711302-02-1R ZL-415-02-3 415AL 415BL 415CL 415 FAN COWL (EWIS) I: 2 C MSI NONE RR416AR 416BR 416CR 416425AL 425BL 425CL 425 SSI 711200-01-1426AR 426BR 426CR 426 SSI 711246-01-1ZL-415-03-1 N/A TASK DELETED MSI NONESSI NONEISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-417-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-417-02-1 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 78.32.00/08-G6 A330-200418AR 418BR 425AL 418GE426AR 427AL 428AR 427 SSI 783201-03-2 OR428BR 428 SSI 783202-01-1 A330-300THRUST REVERSERGEDEPLOYEDR ZL-417-02-2 415BL 416BR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 78.32.00/01-PW PW417DL 417EL 417FL 418 MSI 78.32.00/02-PW417GL 417HL 418AR 427418BR 418CR 418FR 428 SSI 783201-04-2418GR 418HR 418JR SSI 783202-02-1425BL 426BR 427AL SSI 783203-01-1427DL 427EL 427FL427GL 427HL 428AR428BR 428CR 428FR428GR 428HR 428JRTHRUST REVERSERDEPLOYEDR ZL-417-02-3 415AL 416AR 417AL 417 THRUST REVERSER (EWIS) I: C MSI 78.32.00/01-RR RR417BL 417CL 417DL 418417EL 417FL 417GL 427 SSI NONE418AR 418BR 418CR 428418DR 418ER 418FR418GR 418HR 418JR425AL 426AR 427AL427BL 427CL 427DL427EL 427FL 427GL428AR 428BR 428CR428DR 428ER 428FR428GR 428HR 428JRTHRUST REVERSERDEPLOYEDZL-417-03-1 N/A TASK DELETED MSI NONE* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 4APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-417-03-1 * * * * * C O N T I N U E * * * * *SSI NONEZL-451-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-451-02-1 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI NONE PW451CR 451DL 451DR 461461BL 461BR 461CL SSI NONE461CR 461DL 461DRR ZL-451-02-2 451BL 451CL 451DL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI NONE A330-200451DR 451EL 451ER 461GE461BL 461CL 461DL SSI NONE OR461DR 461EL 461ERA330-300GER ZL-451-02-3 451BL 451BR 451CL 451 PYLON LEADING EDGE (EWIS) I: 2 C MSI NONE RR451DL 451DR 451EL 461451ER 461BL 461BR SSI NONE461CL 461DL 461DR461EL 461ERZL-451-03-1 N/A TASK DELETED MSI NONESSI NONER ZL-452-01-1 452AL 452BL 452BR 452 UPPER FORWARD PYLON (EWIS) I: 2 C MSI NONE ALL452CL 452CR 462AL 462462BL 462BR 462CL SSI NONE462CRR ZL-453-01-1 453BL 453BR 453CL 453 LOWER PYLON (EWIS) I: 2 C MSI NONE RR453CR 463BL 463BR 463463CL 463CR SSI NONEISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 5APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEN ZL-453-01-2 453AL 453AR 453BL 453 LOWER PYLON (EWIS) I: 2 C MSI NONE PW453BR 453CL 453CR 463OR463AL 463AR 463BL SSI NONE A330-200463BR 463CL 463CRGEORA330-300GEZL-454-01-1 N/A TASK DELETED MSI NONESSI NONEZL-454-02-1 N/A TASK DELETED MSI NONESSI NONER ZL-454-05-1 454BL 454BR 454CL 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 2 C MSI NONE A330-200454CR 454DL 454FL 464PRE 43271454GL 454HL 454JL SSI NONE OR464BL 464BR 464CLA330-300464CR 464DL 464FLPRE 43271464GL 464HL 464JLR ZL-454-05-2 454BL 454BR 454CL 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 2 C MSI NONE A330-200454GL 454HL 454JL 464POST 43271454KL 454ML 454NR SSI NONE OR464BL 464BR 464CLA330-300464GL 464HL 464JLPOST 43271464KL 464ML 464NRORA330-200FR ZL-454-06-1 454AL 454BL 454BR 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 4 C MSI NONE A330-200454CL 454CR 454DL 464PRE 43271454DR 454EL 454ER SSI 545135-01-1 OR454FL 454FR 454GL SSI 572003-02-2 A330-300454GR 454HL 454HR SSI 572013-04-1 PRE 43271454JL 464AL 464BL SSI 572021-04-1464BR 464CL 464CR SSI 575015-01-1464DL 464DR 464EL464ER 464FL 464FR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 6APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-454-06-1 * * * * * C O N T I N U E * * * * *464GL 464GR 464HL464HR 464JLR ZL-454-06-2 454AL 454BL 454BR 454 LOWER AND REAR PYLON FAIRINGS (EWIS) I: 4 C MSI NONE A330-200454CL 454EL 454ER 464POST 43271454GL 454GR 454HL SSI 545135-01-1 OR454HR 454JL 454KL SSI 572003-02-3 A330-300454KR 454ML 454MR SSI 572013-04-2 POST 43271454NR 464AL 464BL SSI 572021-04-2 OR464BR 464CL 464EL SSI 575015-01-1 A330-200F464ER 464GL 464GR464HL 464HR 464JL464KL 464KR 464ML464MR 464NR* * * * * E N D * * * * *ISSUE: JUL 01/10 POWERPLANT, NACELLES AND PYLONS SECTION: E-400PAGE 7APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-500-01-1 FLAPS EXTENDED 500 WING LOWER SURFACE (EWIS) I: C MSI NONE ALLSLATS EXTENDED 600(INCLUDING SLATS AND FLAPS) SSI 572006-02-1SSI 572006-02-5SSI 572006-02-6SSI 572006-02-7SSI 572006-02-8SSI 572102-01-10SSI 572102-01-11SSI 572102-01-4SSI 572102-01-5SSI 572102-01-6SSI 572102-01-7SSI 572102-01-8SSI 572102-01-9SSI 572110-02-2SSI 572112-04-1SSI 572116-02-1SSI 572116-02-3SSI 572116-02-4SSI 572116-02-5SSI 572116-02-6SSI 572116-02-7SSI 572116-02-8SSI 574114-04-1SSI 574303-02-3SSI 574306-02-1SSI 574308-01-1SSI 574403-02-3SSI 574406-01-1SSI 574408-01-1SSI 574503-02-3SSI 574506-02-1SSI 574508-01-1SSI 574603-02-3SSI 574606-02-1SSI 574608-01-1SSI 574703-02-3SSI 574706-02-1SSI 574708-01-1SSI 574803-02-3SSI 574806-02-1SSI 574808-01-1SSI 574903-02-3SSI 574906-02-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-500-01-1 * * * * * C O N T I N U E * * * * *SSI 574908-01-1SSI 575012-02-1SSI 575013-02-1SSI 575015-01-1SSI 575025-02-1SSI 575401-01-1SSI 575404-01-1SSI 575501-01-1R ZL-500-02-1 FLAPS EXTENDED 500 WING UPPER SURFACE (EWIS) I: 2 C MSI NONE ALLSLATS EXTENDED 600SPOILERS EXTENDED (INCLUDING SLATS, FLAPS AND SPOILERS) SSI 572033-02-2SSI 572133-02-2SSI 572134-02-10SSI 572134-02-2SSI 572134-02-3SSI 572134-02-4SSI 572134-02-5SSI 572134-02-6SSI 572134-02-7SSI 572134-02-8SSI 572134-02-9SSI 572135-01-4SSI 572135-01-5SSI 572135-01-6SSI 572135-01-7SSI 572135-01-8SSI 572135-01-9SSI 572138-01-4SSI 572138-01-5SSI 572138-01-8SSI 572139-01-4SSI 572139-01-5SSI 572139-01-7SSI 572139-01-8SSI 573002-02-2SSI 573006-01-2SSI 574111-02-2SSI 574308-01-1SSI 574408-01-1SSI 574506-02-1SSI 574508-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-500-02-1 * * * * * C O N T I N U E * * * * *SSI 574606-02-1SSI 574608-01-1SSI 574706-02-1SSI 574708-01-1SSI 574808-01-1SSI 574906-02-1SSI 574908-01-1SSI 575011-02-1SSI 575401-01-1SSI 575404-01-1SSI 575501-01-2SSI 577001-01-2R ZL-521-01-1 521AB 521BB 521CB 521 INBOARD FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI 36.00.00/05 ALL521DB 521FB 521GB 621521JB 621AB 621BB SSI 572061-01-2621CB 621DB 621FB SSI 574108-01-1621GB 621JBSLATS EXTENDEDR ZL-522-01-1 522AB 522AT 522BB 522 CENTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE ALL522BT 522CB 522CT 622522EB 522HB 522JB SSI 572061-01-2522LB 522NB 522QB SSI 574108-01-1522RB 522TB 522UB622AB 622AT 622BB622BT 622CB 622CT622EB 622HB 622JB622LB 622NB 622QB622RB 622TB 622UBSLATS EXTENDEDR ZL-523-01-1 523AB 523AT 523BB 523 OUTER FIXED LEADING EDGE STRUCTURE (EWIS) I: C MSI NONE ALL523BT 523CB 523CT 623523EB 523GB 523JB SSI NONE523LB 523NB 623AB623AT 623BB 623BT623CB 623CT 623EB623GB 623JB 623LB623NB* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-523-01-1 * * * * * C O N T I N U E * * * * *SLATS EXTENDEDR ZL-531-01-1 531CB 532CB 533CB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 2 C MSI NONE ALL534CB 631CB 632CB 532633CB 634CB 533 (INCLUDING RAT ATTACHMENT POINTS, AS FAR AS VISIBLE) SSI NONEFLAPS EXTENDED 534631632633634R ZL-531-02-1 531AB 531CB 532AB 531 FLAP TRACKS AND FAIRINGS (EWIS) I: 4 C MSI 27.50.00/10 ALL532CB 533AB 533CB 532534AB 534CB 631AB 533 SSI 572008-02-1631CB 632AB 632CB 534 SSI 572021-04-1633AB 633CB 634AB 631 SSI 572021-04-2634CB 632 SSI 572111-02-1FLAPS EXTENDED 633 SSI 572606-02-2634 SSI 575015-01-1SSI 575025-02-1R ZL-535-01-1 535AB 535BB 635AB 535 WING TIP (EWIS) I: 4 C MSI NONE ALL635BB 635SSI NONER ZL-541-01-1 541AB 541BB 541BZ 541 INNER FUEL TANK (EWIS) I: 4 C MSI NONE ALL541CB 541CZ 641AB 641 NOTE 3641BB 641BZ 641CB (RIB 1 TO RIB 7) SSI 572017-02-2641CZ SSI 572052-02-2R ZL-541-02-1 541AB 541AZ 541BB 541 INNER FUEL TANK (EWIS) I: 8 C MSI NONE ALL541BZ 541CB 541CZ 641541DB 541DZ 541EB (AREA BETWEEN RIB 1 TO RIB 23). SSI 572018-02-1541EZ 541FB 541FZ SSI 572019-02-2541GB 541GZ 541HB SSI 572026-02-1541JB 541KB 541LB SSI 572027-02-1541MB 541NB 541PB SSI 572036-02-2541QB 541RB 541SB SSI 572037-02-2* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 4APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-541-02-1 * * * * * C O N T I N U E * * * * *641AB 641AZ 641BB SSI 572038-02-1641BZ 641CB 641CZ SSI 572046-02-2641DB 641DZ 641EB SSI 572047-02-2641EZ 641FB 641FZ SSI 572063-02-2641GB 641GZ 641HB SSI 572064-02-2641JB 641KB 641LB SSI 572067-02-2641MB 641NB 641PB SSI 572068-02-2641QB 641RB 641SB SSI 572069-02-2SSI 572071-02-2SSI 572073-02-2SSI 572074-01-1SSI 572082-02-2SSI 572092-02-1SSI 572093-03-1SSI 572094-02-2SSI 572121-02-2SSI 572140-02-2SSI 572158-02-2SSI 572180-02-2R ZL-542-01-1 542AB 542BB 542CB 542 OUTER FUEL TANK (EWIS) I: 8 C MSI NONE ALL542DB 542EB 542FB 642542GB 542HB 542JB (RIB 23 TO RIB 33) SSI 572122-02-2542KB 560DB 642AB SSI 572141-02-2642BB 642CB 642DB SSI 572144-02-2642EB 642FB 642GB SSI 572148-02-2642HB 642JB 642KB SSI 572159-02-2660DB SSI 572181-02-2SSI 572182-02-2SSI 572183-03-2R ZL-550-01-1 550AB 550BB 550CB 550 VENT SURGE TANK (EWIS) I: 8 C MSI NONE ALL550DB 550EB 550FB 650650AB 650BB 650CB (RIB 33 TO RIB 39) SSI 572122-02-2650DB 650EB 650FB SSI 572141-02-2SSI 572182-02-2R ZL-571-01-1 734 744 571 MAIN LANDING GEAR WELL (EWIS) I: 2 C MSI NONE ALL671SSI 572041-01-1* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 5APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-571-01-1 * * * * * C O N T I N U E * * * * *SSI 572601-01-2SSI 572602-01-2SSI 572603-01-1SSI 572604-01-1R ZL-572-01-1 572BB 572CB 572EB 572 SHROUD BOX (EWIS) I: 4 C MSI NONE ALL672BB 672CB 672EB 672SSI NONER ZL-573-01-1 573CB 573DB 573GB 573 INNER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE ALL673CB 673DB 673GB 673FLAPS EXTENDED (RIB 6 TO RIB 12) SSI 572041-01-1SSI 572043-02-2R ZL-574-01-1 574AT 674AT 574 CENTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE ALLFLAPS EXTENDED 674(RIB 12 TO RIB 27) SSI NONER ZL-575-01-1 575AB 575AT 575BB 575 OUTER TRAILING EDGE FIXED STRUCTURE (EWIS) I: 2 C MSI NONE ALL575BT 575CB 575DB 675675AB 675AT 675BB (RIB 27 TO RIB 39) SSI NONE675BT 675CB 675DBR ZL-591-01-1 575AB 575BB 591AB 591 INBOARD AILERON (EWIS) I: 2 C MSI NONE ALL591BB 591CB 591DB 691675AB 675BB 691AB SSI NONE691BB 691CB 691DBR ZL-592-01-1 575CB 575DB 592AB 592 OUTBOARD AILERON (EWIS) I: 2 C MSI NONE ALL592BB 592CB 592DB 692675CB 675DB 692AB SSI NONE692BB 692CB 692DB* * * * * E N D * * * * *ISSUE: JUL 01/10 WINGS SECTION: E-500PAGE 6APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-633-01-1 N/A TASK DELETED MSI NONESSI NONEZL-633-02-1 N/A TASK DELETED MSI NONESSI NONEZL-633-03-1 N/A TASK DELETED MSI NONESSI NONE* * * * * E N D * * * * *ISSUE: JUL 01/10 RH WING SECTION: E-600PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-700-01-1 N/A TASK DELETED MSI NONESSI NONER ZL-711-01-1 713 714 711 NOSE LANDING GEAR (EWIS) I: A MSI 32.30.00/13 ALLSSI NONER ZL-713-01-1 713 714 713 NOSE LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE ALL714SSI 528201-01-1SSI 528202-01-1R ZL-715-01-1 715 716 715 NOSE LANDING GEAR AFT DOORS (EWIS) I: A MSI NONE ALL716SSI 528204-01-1R ZL-731-01-1 734 744 731 LH AND RH MAIN LANDING GEAR (EWIS) I: A MSI 32.11.00/08 ALL741 MSI 32.30.00/13SSI NONER ZL-732-01-1 N/A 732 MAIN LANDING GEAR LEG DOOR (EWIS) I: A MSI NONE ALL742SSI 572614-02-1SSI 572615-02-1R ZL-733-01-1 N/A 733 MAIN LANDING GEAR HINGE DOOR (EWIS) I: A MSI NONE ALL743SSI 572614-02-1R ZL-734-01-1 734 744 734 MAIN LANDING GEAR MAIN DOORS (EWIS) I: A MSI NONE ALL744SSI 528101-01-1SSI 528102-01-1* * * * * E N D * * * * *ISSUE: JUL 01/10 LANDING GEAR SECTION: E-700PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-800-01-1 N/A 800 DOORS I: C MSI NONE ALLSSI 521103-01-1SSI 521201-01-1SSI 521301-01-1SSI 522201-01-1SSI 523101-01-1SSI 523201-01-1SSI 523301-01-1SSI 523801-01-1R ZL-811-01-1 121EF 811 811 FORWARD AVIONICS COMPARTMENT DOOR (EWIS) I: C MSI 52.41.11/01 ALLSSI 524101-02-3R ZL-821-01-1 821 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 ALL(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 523101-01-2DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOOR SSI 532107-01-2SILL)R ZL-821-02-1 132AR 132BR 132CR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE ALL132DR 132ER 132FR132GR 132HR 132JR (INCLUDING DOOR HINGE ARMS AREA ATTACHMENT AREA) SSI NONE132KR 132LR 821821AR 821BR 821CR821DRR ZL-821-03-1 821 821AR 821BR 821 FWD CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI NONE ALL821CR 821DRINSULATION SSI NONER ZL-822-01-1 822 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.31.00/03 ALL(INCLUDING LOCK FITTINGS AT DOOR SILL, DOOR SEALS, SSI 523201-01-2DOOR FRAMES AT FUSELAGE AND VISIBLE PART OF DOORSILL)R ZL-822-02-1 152AR 152BR 152CR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE ALL* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 1APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-822-02-1 * * * * * C O N T I N U E * * * * *152DR 152ER 152FR (INCLUDING DOOR HINGE ARMS ATTACHMENT AREA) SSI NONE152GR 152HR 152JR152KR 152LR 822822AR 822BR 822CR822DRR ZL-822-03-1 822 822AR 822BR 822 AFT CARGO COMPARTMENT DOOR (EWIS) I: 8 C MSI NONE ALL822CR 822DRINSULATION SSI NONER ZL-823-01-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: A MSI 52.33.00/02 ALL(INCLUDING FUSELAGE FRAMES, STOP FITTINGS AT FUSELAGE SSI 523301-01-2FRAMES, DOOR SEALS AND VISIBLE PART OF DOOR SILL)R ZL-823-02-1 823 823 BULK CARGO COMPARTMENT DOOR (EWIS) I: 4 C MSI NONE ALLINSULATIONSSI NONER ZL-831-01-1 831 841 831 FWD PASSENGER/CREW DOOR (EWIS) I: C MSI 52.10.00/07 ALL841(INCLUDING DOOR STOPS ON FUSELAGE SIDE ,DOOR SEALS SSI NONEAND SCUFF PLATES)R ZL-831-02-1 831 831AZ 831BZ 831 FWD PASSENGER/CREW DOOR (EWIS) I: 8 C MSI NONE ALL831CZ 831DZ 831EZ 841831FZ 831GZ 831HZ SSI NONE831JZ 841 841AZ841BZ 841CZ 841DZ841EZ 841FZ 841GZ841HZ 841JZINSULATIONR ZL-832-01-1 832 842 832 MID PASSENGER/CREW DOOR (EWIS) I: C MSI 52.10.00/07 A330-200842OR(INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SSI NONE A330-300SCUFF PLATES)ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 2APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCER ZL-832-02-1 832 832AZ 832BZ 832 MID PASSENGER/CREW DOOR (EWIS) I: 8 C MSI NONE A330-200832CZ 832DZ 832EZ 842OR832FZ 832GZ 832HZ SSI NONE A330-300832JZ 842 842AZ842BZ 842CZ 842DZ842EZ 842FZ 842GZ842HZ 842JZINSULATIONR ZL-833-01-1 833 843 833 AFT PASSENGER/CREW DOOR (EWIS) I: C MSI 52.10.00/07 A330-200843OR(INCLUDING DOOR STOPS ON FUSELAGE SIDE,DOOR SEALS AND SSI NONE A330-300SCUFF PLATES)R ZL-833-02-1 833 833AZ 833BZ 833 AFT PASSENGER/CREW DOOR (EWIS) I: 8 C MSI NONE A330-200833CZ 833DZ 833EZ 843OR833FZ 833GZ 833HZ SSI NONE A330-300833JZ 843 843AZ843BZ 843CZ 843DZ843EZ 843FZ 843GZ843HZ 843JZINSULATIONR ZL-834-01-1 834 844 834 EMERGENCY EXITS (EWIS) I: C MSI 52.22.00/07 A330-200844OR(INCLUDING DOOR STOPS ON FUSELAGE SIDE ,DOOR SEALS SSI NONE A330-300AND SCUFF PLATES)R ZL-834-02-1 834 834AZ 834BZ 834 EMERGENCY EXIT (EWIS) I: 8 C MSI NONE A330-200834CZ 834DZ 834EZ 844TYPE A834FZ 834GZ 834HZ SSI NONE OR834JZ 844 844AZA330-300844BZ 844CZ 844DZTYPE A844EZ 844FZ 844GZ844HZ 844JZINSULATIONR ZL-834-03-1 834 834KZ 834LZ 834 EMERGENCY EXIT (EWIS) I: 8 C MSI NONE A330-200834MZ 834NZ 834PZ 844TYPE I834QZ 844 844KZ SSI NONE OR* * * * * C O N T I N U E D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 3APPLICABILITYA330MRB REPORT – Zonal SectionZONETASKREFERENCEACCESSDESCRIPTIONINTERVALMSI/SSIREFERENCEZL-834-03-1 * * * * * C O N T I N U E * * * * *844LZ 844MZ 844NZA330-300844PZ 844QZTYPE IINSULATIONN ZL-835-01-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 800 FH MSI 52.38.00/04 A330-200FOR MSI 52.38.00/05(INCLUDING DOOR SEALS, DOOR FRAMES AND FITTING AREA 6 MO MSI 52.38.00/06AT FUSELAGE AND VISIBLE PART OF DOOR SILL)SSI NONEN ZL-835-02-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 72 MO MSI NONE A330-200FLINING AND DADOLINER SSI NONEN ZL-835-03-1 835 835 MAIN DECK CARGO COMPARTMENT DOOR (EWIS) I: 144 MO MSI NONE A330-200FLINING AND DADOLINER, INSULATION SSI NONE* * * * * E N D * * * * *ISSUE: JUL 01/10 DOORS SECTION: E-800PAGE 4

# 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 fo llowing 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 transmis sion 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 This page intentionally left blank

# 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.MAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 2100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR) INCLUDINGRADOME TO FORWARD FACE OFAFT PRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA55287,3200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA55287,3300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA55287,3TO FR106 - STA63894,3TOP OF RUDDER - STA70040ELEVATOR - STA70070400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSA330-200MAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 3100 LOWER HALF OF FUSELAGE(BELOW CABIN FLOOR) INCLUDINGRADOME TO FORWARD FACE OFAFT PRESSURE BULKHEADFR0 - STA6382TO FR80/82 - STA60614200 UPPER HALF OF FUSELAGE(ABOVE CABIN FLOOR) TOFORWARD FACE OF AFTPRESSURE BULKHEADFR1 - STA7662TO FR80/82 - STA60614300 STABILIZER AND FUSELAGE REARSECTION FROM REAR OF AFTPRESSURE BULKHEADFR80/82 - STA60614TO FR106 - STA69265TOP OF RUDDER - STA70040ELEVATOR - STA70070400 POWER PLANT NACELLES ANDPYLONS500 LEFT WING600 RIGHT WING700 LANDING GEARS AND LANDINGGEAR DOORS800 PASSENGER/CREW DOORS,CARGO COMPARTMENT DOORSAND EMERGENCY EXITSA330-300A330 MRB REPORTIssue : July 2010Page : APX 2. 4MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 5110 RADOME (NOSE CONE TO FR 1)- STA 6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA144585130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA27708,5140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA27708,5TO FR53,2 - STA36737,3150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA36737,3TO BETWEEN FR65 - STA46807,3AND FR66 - STA47337,3160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR 65 - STA47337,3AND FR66 - STA47337,3TO FR73 - STA51047,3170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA51047,3TO FR80/82 - STA55287,3190 BELLY FAIRING; AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR37,2 - STA23468,5AND FR37,3 - STA23998,5TO FR56 - STA42037,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR31 - STA19228,5240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR31 - STA19228,5TO FR36 - STA21878,5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR36 - STA21878,5TO FR53,5 - STA38327,3260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR53,5 - STA38327,3TO FR72 - STA50517,3270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA50517,3TO FR80/82 - STA55287,5310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA55287,5TO FR106 - STA63894,5320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER; L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSAA330-200MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 6110 RADOME (NOSE CONE TO FR 1)- STA 6382,5 TO - STA7662,5120 AVIONICS COMPARTMENT :FORWARD PRESSURE BULKHEADTO AFT PARTITION OF AVIONICSCOMPARTMENTFR1 - STA7662,5TO FR20 - STA144585130 LOWER DECK FORWARD CARGOCOMPARTMENT : AFT PARTITIONOF AVIONICS COMPARTMENT TOFORWARD PRESSURE BULKHEADOF WING CENTER BOXFR20 - STA14458,5TO FR40 - STA30381,1140 WING CENTER BOX, AIR COND,HYD COMPARTMENT : FORWARDPRESSURE BULKHEAD OF WINGCENTER BOX TO FORWARDPRESSURE BULKHEAD OF AFTCARGO COMPARTMENTFR40 - STA30381,1TO FR53,2 - STA39930,9150 LOWER DECK AFT CARGOCOMPARTMENT : FORWARDPRESSURE BULKHEAD TO AFTPARTITION OF AFT CARGOCOMPARTMENTFR53,2 - STA39930,9TO BETWEEN FR65 - STA52134,5AND FR66 - STA52664,5160 LOWER DECK BULK CARGOCOMPARTMENT : AFT PARTITION,OF AFT CARGO COMPARTMENTTO AFT PARTITION OF BULKCARGO COMPARTMENTBETWEEN FR 65 - STA52134,5AND FR66 - STA52664,5TO FR73 - STA56374,5170 AFT CABIN UNDERFLOORCOMPARTMENT : AFT PARTITIONOF BULK CARGO COMPARTMENTTO AFT PRESSURE BULKHEADFR73 - STA56374,5TO FR80/82 - STA60614,5190 BELLY FAIRING; AIRCONDITIONING COMPARTMENT,HYDRAULIC COMPARTMENTBETWEEN FR37,2 - STA26651,9AND FR37,3 - STA27185,3TO FR57,2 - STA46824,3210 COCKPIT FROM FORWARDPRESSURE BULKHEAD TOCOCKPIT PARTITIONFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5220 FORWARD CABIN UTILITY AREAAFT OF COCKPIT PARTITION TOFRONT OF FORWARD CABINBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5230 FORWARD CABIN AFT OFFORWARD CABIN UTILITY AREATO FRONT OF MID CABINFR17 - STA13153,5TO FR31 - STA22408,240 MID CABIN UTILITY AREA AFT OFFORWARD CABIN TO FRONT OFMID CABINFR31 - STA22408,5TO FR36 - STA25058,5250 MID CABIN AFT OF MID CABINUTILITY AREA TO FRONT OF AFTCABINFR36 - STA25058,5TO FR53,5 - STA41520,9260 AFT CABIN AFT OF MID CABIN TOFRONT OF AFT CABIN UTILITYAREAFR53,5 - STA41520,9TO FR72 - STA55844,5270 AFT CABIN UTILITY AREA AFT OFAFT CABIN TO FRONT OF AFTPRESSURE BULKHEADFR72 - STA55844,5TO FR80/82 - STA60614,5310 FUSELAGE REAR SECTION AFT OFAFT PRESSURE BULKHEADFR80/82 - STA60614,5TO FR106 - STA69265,5320 VERTICAL STABILIZER ANDRUDDER330 TRIMMABLE HORIZONTALSTABILIZER; L SIDE AND LELEVATOR340 TRIMMABLE HORIZONTALSTABILIZER, R SIDE AND RELEVATOR710 NOSE GEAR AND DOORS730 L MAIN LANDING GEAR ANDDOORS740 R MAIN LANDING GEAR ANDDOORS810 FORWARD AVIONICSCOMPARTMENT DOOR820 CARGO COMPARTMENT DOORS830 L PASSENGER/CREW DOORS ANDEMERGENCY EXITS840 R PASSENGER/CREW DOORS ANDEMERGENCY EXITSA330-300MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 7410 ENGINE 1 (LEFT ENGINE), ENGINEAIR I)INTAKE; FAN ANDACCESSORY GEAR BOX, THRUSTREVERSER, EXHAUST NOZZLEAND COWLS450 ENGINE 1 PYLON510 SLATS520 FIXED LEADING EDGE530 FLAP TRACK FAIRINGS AND WINGTIP540 FUEL TANKRIB 1 - STA0TO RIB33 - STA21905550 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566570 AFT SECTION OF WING ANDTRAILING EDGE FIXEDSTRUCTURE580 FLAPS AND SPOILERS590 AFT OUTBOARD SECTION OFWING TRAILING EDGE420 ENGINE 2 (RIGHT ENGINE) ENGINEAIR INTAKE, FAN AND ACCESSORYGEAR BOX; THRUST REVERSER,EXHAUST NOZZLE AND COWLS460 ENGINE 2 PYLON610 SLATS620 FIXED LEADING EDGE630 FLAP TRACK FAIRINGS AND WING640 FUEL TANKRIG1 - STA0TO RIB33 - STA21905650 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566670 AFT SECTION OF WING ANDTRAILING EDGE FIXEDSTRUCTURE680 FLAPS AND SPOILERS690 AFT OUTBOARD SECTION OFTRAILING EDGEA330 MRB REPORTIssue : July 2010Page : APX 2. 8MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 9121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14448,5TO FR39,1 - STA26118,5AND FR39,2 - STA26648,5133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14458,5TO FR39,1 - STA26118,5AND FR39,2 - STA26648,5137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGO COMPARTMENTTO FORWARD PRESSUREBULKHEAD OF WING CENTER BOXFROM LOWER SIDE OF PAXCOMPARTMENT FLOOR TOBOTTOM CENTER LINE (STR26 L/R)FR39,1 --STA26118,5AND FR39,2 STA26648,5TO FR39 - STA25588,5AND FR40 - STA27708,5141/142 WING CENTER BOXFR40 - STA27708,5AND FR47 - STA32478,5143 AREA BETWEEN KEEL BEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGE BETWEENFR44 AND FR45 - STA30888,5TO FR49 - STA33543,2145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX; MAIN GEARWELL AND CABIN FLOORFR40 - STA27708,5TO FR53,2 - STA36737,3147/148 MAIN GEAR WELL AND HYDRAULICCOMPARTMENTFR47 - -STA32478,TO FR53,2 - STA36737,3149 CENTERLINE BAY BETWEEN KEELBEAMS UNDER ZONE 143BETWEENFR44 AND FR45 - STA30888,5TO FR49 - STA33543,2AND BETWEEN KEEL BEAMSFR49 - STA33543,2TO FR53,2 - STA36737,3151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR53,2 - STA36737,3TO FR65 - STA47867,3AND FR66 - STA48397,3153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/R INCYLINDRICAL SECTION)FR53,2 - STA37797,3TO FR65 - STA46807,3AND FR66 - STA47337,3161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR65 - STA46807,3AND FR66 - STA47337,3TO FR73 - STA51047,3163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA46807,3AND FR66 - STA47337,3TO FR73 - STA51047,3171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA51047,3TO FR80 - STA55287,3191 DRY BAY AND FAIRINGS :BETWEEN FR37 AND FR37,1STA23681,5 TO BETWEEN FR44AND FR45 STA32042,6192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37 AND FR37,1STA22938,1 TO BETWEEN FR44AND FR45 STA31418,5193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR40 STA27187,3BETWEEN FR44 AND FR45STA31418,5195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS : BETWEEN FR44 ANDFR45 STA30888,5 TO FR47STA32478,5197/198 REAR FAIRINGS :FR53:2 - STA37797,3TO FR56 - STA42037,3A330-200MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 10211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR31 - STA19228,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR31 - STA19228,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR31 - STA19228,5TO FR36 - STA21878,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENT FROMCROWN CENTER LINE TO STR15L/RFR31 - STA19228,5TO FR36 - STA21878,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)FR36 - STA21878,5TO FR53,5 - STA38327,3253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR36 - STA21878,5TO FR53,5 - STA38327,3261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR53,5 - STA38327,3TO FR72 - STA50517,3263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR53,5 - STA38327,3TO FR72 - STA50517,3271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR72 - STA50517,3TO FR80 - STA55287,3273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA50517,3TO FR80 - STA55287,3311/312 REAR FUSELAGE SECTIONFR80/82 - STA60614,5TO BETWEEN 91/92 - STA65118,5313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA65118,5TO FR95 - STA66046,5315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR95 - STA66046,5TO FR101 - STA67931,5317 TAIL CONE APU EXHAUST AREAFR101 - STA67931,5TO FR106 - STA69265,5321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERA330-200MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 11121/122 AVIONICS COMPARTMENTFR1 - STA7662,5TO FR20 - STA14458,5123 NOSE GEAR WELLFR11 - STA10127,5TO FR17 - STA13153,5131/132 LOWER DECK FORWARD CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14448,5TO FR39,1 - STA29312,1AND FR39,5 - STA28842,1133/134 UNDERFLOOR COMPARTMENT OFLOWER DECK FORWARD CARGOCOMPARTMENT FROM BOTTOMCENTER LINE TO LOWER SIDE OFCARGO COMPARTMENT FLOOR(STR41 L/R IN CYLINDRICALSECTION)FR20 - STA14458,5TO FR39,1 - STA29312,1AND FR39,2 - STA29842,1137/138 COMPARTMENT BETWEEN AFTPARTITION OF LOWER DECKFORWARD CARGO COMPARTMENTTO FORWARD PRESSUREBULKHEAD OF WING CENTER BOXFROM LOWER SIDE OF PAXCOMPARTMENT FLOOR TOBOTTOM CENTER LINE (STR26 L/R)FR39,1 - STA29312,1AND FR39,2 - STA29842,1TO FR39 - STA28782,1AND FR40 - STA30372,1141/142 WING CENTER BOXFR40 - STA30372,1AND FR47 - STA35672,1143 AREA BETWEEN KEELBEAMSUNDER WING CENTER BOX TOBOTTOM FUSELAGE BETWEENFR44 AND FR45 - STA 34176,2TO FR49 - STA36736,8145/146 PRESSURIZED ZONE BETWEENWING CENTER BOX; MAIN GEARWELL AND CABIN FLOORFR40 - STA30372,1TO FR53,2 - STA39930,9147/148 MAIN GEAR WELL AND HYDRAULICCOMPARTMENTFR47 - STA35672,1TO FR53,2 - STA39930,9149 CENTERLINE BAY BETWEEN KEELBEAMS UNDER ZONE 143BETWEENFR44 AND FR45 - STA34176,2TO FR49 - STA36736,8AND BETWEEN KEEL BEAMSFR49 - STA36136,8TO FR53,2 - STA39930,9151/152 LOWER DECK AFT CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR53,2 - STA37797,3TO FR65 - STA47867,3AND FR66 - STA48397,3153/154 UNDERFLOOR COMPARTMENT OFLOWER DECK AFT CARGOCOMPARTMENT : FROM CENTERLINE TO CARGO COMPARTMENTFLOOR LOWER SIDE (STR41 L/R INCYLINDRICAL SECTION)FR53,2 - STA37797,3TO FR65 - STA47867,3AND FR66 - STA48397,3161/162 LOWER DECK BULK CARGOCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO UPPER SIDE OF CARGOCOMPARTMENT FLOOR (STR26 L/RTO STR41 L/R IN CYLINDRICALSECTION)FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3163/164 UNDERFLOOR COMPARTMENT OFLOWER DECK BULK CARGOCOMPARTMENT : FROM BOTTOMCENTER LINE TO CARGOCOMPARTMENT FLOOR LOWERSIDE (STR41 L/R IN CYLINDRICALSECTION)FR65 - STA47867,3AND FR66 - STA48397,3TO FR73 - STA52107,3171/172 AFT CABIN UNDERFLOORCOMPARTMENT : FROM LOWERSIDE OF PAX COMPARTMENTFLOOR TO BOTTOM CENTER LINE(STR26 L/R)FR73 - STA52107,3TO FR80 - STA56347,3190 DRY BAY AND FAIRINGS :BETWEEN FR37 AND FR37,1STA23681,5 TO BETWEEN FR44AND FR45 STA32042,6192 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :BETWEEN FR37 AND FR37,1STA23681,5 TO BETWEEN FR44AND FR45 STA32042,6193 AIR CONDITIONINGCOMPARTMENT AND FAIRINGS :FR40 STA28247,51BETWEEN FR44 AND FR45STA32042,6195/196 HYDRAULIC COMPARTMENT ANDFAIRINGS : BETWEEN FR44 ANDFR45 STA32042,6 TO FR47STA33538,5197/198 REAR FAIRINGS :FR53:2 - STA37797,3TO FR56 - STA43097,3A330-300MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 12211/212 COCKPITFR1 - STA7662,5TO BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5221/222 FORWARD CABIN UTILITY AREA :FROM STR15 L/R TO UPPER SIDEOF PAX COMPARTMENT FLOOR(STR26 L/R IN CYLINDRICALSECTION)BETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5223/224 FORWARD CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RBETWEEN FR11 - STA10187,5AND FR11A - STA10427,5TO FR17 - STA13153,5231/232 FORWARD CABIN : FROM STR15L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR17 - STA13153,5TO FR31 - STA22408,5233/234 FORWARD CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR17 - STA13153,5TO FR31 - STA22408,5241/242 MID CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR31 - STA22408,5TO FR36 - STA25058,5243/244 MID CABIN UTILITY AREA :OVERHEAD COMPARTMENT FROMCROWN CENTER LINE TO STR15L/RFR31 - STA22408,5TO FR36 - STA25058,5251/252 MID CABIN : FROM STR15 L/R TOPAX COMPARTMENT FLOORUPPER SIDE (STR26 L/R INCYLINDRICAL SECTION)FR36 - STA25056,5TO FR53,5 - STA41520,9253/254 MID CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR36 - STA25058,5TO FR53,5 - STA41520,9261/262 AFT CABIN : FROM STR15 L/R TOUPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR53,5 - STA41520,9TO FR72 - STA55844,5263/264 AFT CABIN OVERHEADCOMPARTMENT : FROM CROWNCENTER LINE TO STR15 L/RFR53,5 - STA39387,3TO FR72 - STA51577,3271/272 AFT CABIN UTILITY AREA : FROMSTR15 L/R TO UPPER SIDE OF PAXCOMPARTMENT FLOOR (STR26 L/RIN CYLINDRICAL SECTION)FR72 - STA51577,3TO FR80 - STA56347,3273/274 AFT CABIN UTILITY AREAOVERHEAD COMPARTMENT :FROM CROWN CENTER LINE TOSTR15 L/RFR72 - STA51577,3TO FR80 - STA56347,3311/312 REAR FUSELAGE SECTIONFR80/82 - STA60614,5TO BETWEEN 91/92 - STA65118,5313/314 TAIL CONE APU AIR INTAKE AREABETWEEN FR91/92 - STA65118,5TO FR95 - STA66046,5315/316 TAIL CONE APU AND ACCESSORYCOMPT DELIMITED BY FIREWALLSFR95 - STA66046,5TO FR101 - STA67931,5317 TAIL CONE APU EXHAUST AREAFR101 - STA67931,5TO FR106 - STA69265,5321 DORSAL FIN322 VERTICAL STABILIZER LEADINGEDGE323 VERTICAL STABILIZER SPAR BOX324 VERTICAL STABILIZER TIP325 VERTICAL STABILIZER TRAILINGEDGE326 RUDDERA330-300MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 13319 TRIMMABLE HORIZONTALSTABILIZER CENTER SPAR BOXFUEL TANKHORIZONTAL TAIL LH331 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE332 TRIMMABLE HORIZONTALSTABILIZER TIP333 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX334 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE335 ELEVATOR337 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB 19 TO RIB 21HORIZONTAL TAIL (RH)341 TRIMMABLE HORIZONTALSTABILIZER LEADING EDGE342 TRIMMABLE HORIZONTALSTABILIZER TIP343 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX344 TRIMMABLE HORIZONTALSTABILIZER TRAILING EDGE345 ELEVATOR346 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX VENT TANK347 TRIMMABLE HORIZONTALSTABILIZER SPAR BOX DRY BAYRIB20 TO RIB21MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 14ENGINE 1411 ENGINE AIR INTAKE AND AIRINTAKE LIP412 FAN AND ACCESSORY GEAR BOX415 L FAN COWL416 R FAN COWL417 L THRUST REVERSER418 R THRUST REVERSER413 HOT SECTION414 EXHAUST NOZZLE451 PYLON LEADING EDGE452 UPPER FWD PYLON453 LOWER PYLON454 LOWER AND REAR PYLONFAIRINGSENGINE 2421 ENGINE AIR INTAKE AND AIRINTAKE LIP422 FAN AND ACCESSORY GEAR BOX425 L FAN COWL426 R FAN COWL427 L THRUST REVERSER428 R THRUST REVERSER423 HOT SECTION424 EXHAUST NOZZLE461 PYLON LEADING EDGE462 UPPER FWD PYLON463 LOWER PYLON464 LOWER AND REAR PYLONFAIRINGSA330 MRB REPORTIssue : July 2010Page : APX 2. 15MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 16511 SLAT 1512 SLAT 2513 SLAT 3514 SLAT 4515 SLAT 5516 SLAT 5517 SLAT 7521 INBOARD FIXED LEADING EDGESTRUCTURERIB1 - STA0TO RIB9 - STA5676522 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA5686TO RIB24 - STA16009523 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA16009TO RIB39 - STA25566531 FLAP TRACK 2 FAIRING532 FLAP TRACK 3 FAIRING533 FLAP TRACK 4 FAIRING534 FLAP TRACK 5 FAIRING535 WING TIP541 INNER TANKRIB1 - STA0TO RIB23 - STA15298542 OUTER TANKRIB23 - STA15298TO RIB33 - STA21905550 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566571 MLG WELL572 SHROUD BOX573 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12574 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27575 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB39581 INBOARD FLAP 1582 SPOILER 1583 OUTBOARD FLAP 2584 SPOILER 2585 SPOILER 3586 SPOILER 4587 SPOILER 5588 SPOILER 6591 INBOARD AILERON592 OUTBOARD AILERONMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 17611 SLAT 1612 SLAT 2613 SLAT 3614 SLAT 4615 SLAT 5616 SLAT 5617 SLAT 7621 INBOARD FIXED LEADING EDGESTRUCTURERIB1 - STA0TO RIB9 - STA5676622 CENTER FIXED LEADING EDGESTRUCTURERIB9 - STA5676TO RIB24 - STA16009623 OUTBOARD FIXED LEADING EDGESTRUCTURERIB24 - STA16009TO RIB39 - STA25566631 FLAP TRACK 2 FAIRING632 FLAP TRACK 3 FAIRING633 FLAP TRACK 4 FAIRING634 FLAP TRACK 5 FAIRING635 WING TIP641 INNER TANKRIB1 - STA0TO RIB23 - STA15298642 OUTER TANKRIB23 - STA15298TO RIB33 - STA21905650 VENT SURGE TANKRIB33 - STA21905TO RIB39 - STA25566671 MLG WELL672 SHROUD BOX673 INNER TRAILING EDGE FIXEDSTRUCTURERIB6TO RIB12674 CENTER TRAILING EDGE FIXEDSTRUCTURERIB12TO RIB27675 OUTER TRAILING EDGE FIXEDSTRUCTURERIB27TO RIB39681 INBOARD FLAP 1682 SPOILER 1683 OUTBOARD FLAP 2684 SPOILER 2685 SPOILER 3686 SPOILER 4687 SPOILER 5688 SPOILER 6691 INBOARD AILERON692 OUTBOARD AILERONMAJORZONESDESCRIPTION/BOUNDARIESA330 MRB REPORTIssue : July 2010Page : APX 2. 18NOSE LANDING GEAR711 NOSE GEAR712 LEG DOOR713/714 MAIN DOORS715/716 AFT DOORSMAIN LANDING GEAR (LH)731 L MAIN GEAR732 CYLINDER DOOR733 SECONDARY DOOR734 MAIN DOORMAIN LANDING GEAR (RH)741 R MAIN GEAR742 CYLINDER DOOR743 SECONDARY DOOR744 MAIN DOORA330 MRB REPORTIssue : July 2010Page : APX 2. 19MAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESMAJORZONESDESCRIPTION/BOUNDARIESMAJORZONESDESCRIPTION/BOUNDARIESDESCRIPTION/BOUNDARIES811 FORWARD AVIONICSCOMPARTMENT DOOR FR7 ANDFR8 TO FR9 AND FR10821 LOWER DECK FORWARD CARGOCOMPARTMENT DOOR BETWEENFR20A AND FR25A822 LOWER DECK AFT CARGOCOMPARTMENT DOOR BETWEENFR59A AND FR65823 LOWER DECK BULK CARGOCOMPARTMENT DOOR BETWEENFR67 AND FR69831 L FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16B832 L MID PASSENGER/CREW DOORBETWEEN FR33 TO FR35A833 L AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A834 L EMERGENCY EXIT BETWEENFR53,5 TO FR53,7 AND FR53,8836 MAIN DECK CARGOCOMPARTMENT DOOR FR59 TOFR66 (OPTION MOD 40051)841 R FWD PASSENGER/CREW DOORBETWEEN FR14B AND FR16A842 R MID PASSENGER/CREW DOORBETWEEN FR33 TO FR35A843 R AFT PASSENGER/CREW DOORBETWEEN FR73A AND FR75A844 R EMERGENCY EXIT BETWEENFR53,5 TO FR53,7AIssue : July 2010 Page : APX 2. 20A330-200FIssue : July 2010 Page : APX 2. 21Issue : July 2010 Page : APX 2. 22Issue : July 2010 Page : APX 2. 23Issue : July 2010 Page : APX 2. 24Issue : July 2010 Page : APX 2. 25Issue : July 2010 Page : APX 2. 26Issue : July 2010 Page : APX 2. 27Issue : July 2010 Page : APX 2. 28Issue : July 2010 Page : APX 2. 29This 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 par agraphs 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 conne ctors 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.A330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 4R20- 00- 01- 1 522622522AB 522BB 454BL 622AB622BB 464BL4C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the following harnesses end fittings, from rib 9 to rib10A :- 7021VP, 7001VC- A, 7021VC- A, 7025VC- A, 10HA1, LH side- 7024VP, 7002VC- A, 7022VC- A, 7026VC- A, 10HA2, RH sideALL20- 00- 01- 2 TASK RESERVED20- 00- 01- 3 633 RAT extended 2C WING ELECTRICAL WIRING PROTECTION ELEMENTSSecurity check of the connectors located on the RATALLR20- 00- 01- 4 523623523NB 575DB 535AB623NB 675DB 635ABC WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of elements fitted on the following harnesses end fittings fromwing tip to rib 39:- 7621VB, 7623VB, 7625VB, 7627VB, LH side- 7622VB, 7624VB, 7626VB, 7628VB, RH sideALL20- 00- 01- 5 533633533AB 533CB 574CB 574DB574EB 574FB633AB 633CB 674CB 674DB674EB 674FBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of elements fitted on the following harnesses end fittings, fromrib19 to rib 14 :- 7633VB LH side- 7634VB RH sideALL20- 00- 01- 6 531631531CB 573CB 573BB 573DB631CB 673CB 673BB 673DBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSDET inspection of elements fitted on the following harnesses endfittings, from rib 6 to fuselage :- 7651VB, 7681VB, 7683VB, LH side- 7652VB, 7682VB, 7684VB, RH sidePRE 43165A330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 520- 00- 01- 7 TASK RESERVED20- 00- 01- 8 571/671 N/A 2C WING ELECTRICAL WIRING PROTECTION ELEMENTSGVI of the following braided conduit end fittings, from rib 6 to fuselage:- 112QA1-A, 121QA1-A, 122QA1-A, LH side- 112QA2-A, 121QA2-A, 122QA2-A, RH sideALL20- 00- 01- 9 531631531CB 573CB 573BB 573DB631CB 673CB 673BB 673DBFlaps extended2C WING ELECTRICAL WIRING PROTECTION ELEMENTSDET inspection of elements fitted on the following harnesses endfittings, from rib 6 to fuselage :- 7652VB, 7646VB, 7634VB, RH side- 7651VB, 7645VB, 7633VB, LH sidePOST 4316520- 00- 01- 10 TASK RESERVED20- 00- 01- 11 TASK RESERVEDA330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 620- 00- 01- 12 TASK RESERVED20- 00- 01- 13 TASK RESERVED20- 00- 01- 14 191/192197/198Wing fillet fairings521AB 621AB4C WING ELECTRICAL WIRING PROTECTION ELEMENTSFunctional check of the following wing pressure seal bondings:3502VP, 3504VP, 3506VP, 3508VP, 3514VP, 3501VP, 3503VP,3505VP, 3507VP, 3513VP, 3722VP, 3736VP, 3738VP, 3744VP,3721VP, 3735VP, 3737VP, 3743VPPRE MOD 5366520- 00- 01- 15 TASK RESERVED20- 00- 02- 1 311312312AR 2C SECTION 19 BRAIDED CONDUITSecurity check of the following harnesses end fittings at Fr. 87 :- 1CS- G, 1CS- HALL20- 00- 03- 1 193 193AB 2C BELLY FAIRING BRAIDED CONDUITGVI of elements fitted on the following harnesses end fittings, from Fr.39 to Fr. 40.2 :- 1541VB, 1543VBALLA330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 720- 00- 03- 2 TASK RESERVED20- 00- 03- 3 191192198198GB, 191CB and 192CB 4C BELLY FAIRING BRAIDED CONDUITFunctional check of the following belly fairing pressure seal bonding:3586VP, 3594VP, 3686VP, 3688VP, 3583VP, 3591VPPRE MOD 5366520- 00- 03- 4 TASK RESERVED20- 00- 04- 1 454/464 454BR 454NR464BR 464NR2C ENGINE PYLON BRAIDED CONDUITGVI of elements fitted on the harnesses end fittings, from rib10 to TeeALL20- 00- 05- 1 734744N/ A 2C MAIN LANDING GEAR BRAIDED CONDUITSecurity check of the end fittings at MLG braided conduitALL20- 00- 05- 2 734744N/ A 2C MAIN LANDING GEAR BRAIDED CONDUITDET inspection of elements fitted on the route 2M from union plate tointerface bracket on strut at MLG braided conduitALL20- 00- 05- 3 TASK DELETEDA330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 820- 00- 06- 1 713714N/ A 2C NOSE LANDING GEARSecurity check of the following harnesses end fittings at NLG braidedconduit :- 1605VC- A, 1607VC- A, 2GH, 1GHALL20- 00- 06- 2TASK RESERVEDR20- 00- 07- 1 323 A330-200:325ML 325NL 312ARA330-300:325BL 325DL 312AR2C VERTICAL FINGVI of fly by wire protection installation at vertical fin :5994VB 5995VB 5996VB 5997VBPRE 49144A330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 9R20- 00- 07- 2 323 A330-200 PRE 48979:325ML 325NL 312ARA330-200 POST 48979:325SL 325NL 312AR 311AZ313BLA330-300:325BL 325DL 312AR2C VERTICAL FINGVI of fly by wire protection installation at vertical fin :5989VB 5994VB 5995VB 5996VB 5997VB 6989VB 6994VB 6996VBPOST 49144A330MRB REPORT –HIRF/Lightning Protection Scheduled Maintenance RequirementsReference Zone Access Interval Description ApplicabilityIssue : July 2010Page : APX9. 10This 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

A ND 72, STRINGER P13-P'13

40611 EQUIPMENT/FURNISHINGS-UNDERFLOOR CREW REST ROOM- A DAPT 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

A T 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 – INTRO DUCE 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

A T 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 - A CTIVATE 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

A S 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 - A DAPT 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 - A CTIVATE 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

A LTIMETER 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

A REAS

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.- A DAPT 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 – IN TRODUCE SERVO CONTROLS TO ECP-9 STD

45535 ICE AND RAIN PROTECTION – WINDSHIELD RAIN PROTECTION - TREAT

WINDSHIELD WITH PPG WATERPHOBIC COATING

45556 EQUIPMENT/FURNISHINGS-PAX COMPARTMENT- IMPROVE LAVATORY MODULES

45578 FLIGHT CONTROLS - THSA – ADAPT COLLECTABLE DRAIN CONTAINER TO NEW

SECT. 19

45670 EQUIPMENT/FURNISHINGS - DOOR AREA FLOOR PANEL HEATING - INTRODUCE

HEATING ELEMENTS FOR PAX DOORS 1, 2, 3, 4

45739 WINGS - TRAILING EDGE – REPLACE CLEARANCE FIT BOLTS BY INTERFERENCE FIT

BOLTS

45749 FUSELAGE - CENTER FUSELAGE – REINFORCE FR40/ST18 JUNCTION

45968 FUSELAGE - GENERAL - INTRODUCE MINOR IMPROVEMENTS IN A/S PART

46025 FUSELAGE - REAR FUSELAGE SECT. 16 - REINFORCE LOWER SKIN PANEL FOR

INSTALL. OF VHF2 ANTENNA

46110 WINGS - STRUCTURE - PANEL NO.3 TOP -EXTEND LIFE OF REAR SPAR FLANGE/TOP

SKIN BOLT HOLES BETWEEN RIBS 2-7

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 - A DAPT

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

A NTENNAS

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

A UTOMATIC 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

A ND STRINGERS

48442 FUSELAGE - REAR FUSELAGE – INCREASE OUTER DOUBLER FOR VHF2

A NTENNA 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 FL Y -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

A T 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 ONL Y

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 - A TC - INSTALL REMOTE ATC CONTROL BO X

49951 WATER/WASTE - POTABLE - INSTALL A NEW POTABLE WATER FILTER IN EACH

LAVATOR Y

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

A LTERNATE 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 ONL Y

54881 FLIGHT CONTROLS - TRIMMABLE HORIZONTAL STABILIZER - INTRODUCE

MODIFIED THSA ( P/N 47147-700 ) FOR SB ONL Y

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 - A DVANCED 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 )

- A NCRA

58215 WATER / WASTE - A IR SUPPLY - INSTALL AN AUXILIARY COMPRESSOR

58552 EQUIPMENT/FURNISHINGS - MAIN DECK CARGO COMPARTMENT - INSTALL OF

MAIN DECK CLS ( BFE ) MULTIPLE CHOICE CONFIGURATION - A AR

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 GEARA330 MRB REPORTIssue : July 2010Page: APX 11. 2a) MLG Required Inspection and Lubrication Tasks.The following inspection and lubrication tasks are required to be performed to achieve the overhaul intervals stated above. Where applicable, a source document is stated.However, where there is no source document, ‘MRBR APX 11’ is stated as a reference. ‘MRBR APX 11’ is also stated as an additional reference, where a new interval hasbeen introduced compared to the existing source document.These tasks will be assessed through the MSG3 analyses, discussed in a dedicated Landing Gear working group meeting and may beintegrated into the MRBR in asubsequent revision.Item/ComponentPartNumberComments / Reason Task Applicability Threshold/IntervalSource Documents AircraftconfigurationShorteningMechanismAdjustable Link201479001 Inspection for crackson eye endsDetailed Inspection ofAdjustable Link Upperand Lower Eye EndsPre Mod 49358(A330-32-3135)Threshold: 3 YEInterval: 700FHISBA330-32-3131(MPD 321100-22-1)Weight OnWheelsMLGUplockRoller201275759201489624201489308Evidence of stresscorrosion found onMLG Uplock RollerInspection of MLGUplock Roller forevidence of corrosionPre Mod50959(A330-32-3162)Threshold: 5 YEor 25,000FHInterval: 5 YE or25,000FHISBA330-32-3178Weight OnWheelsBogiePivot Pin201269612201489621201454925201489751Prevention of ChromeDamageReduced LubricationintervalAll 250FC or 4MO SIL 32-114(M-D SL A33/34-A6)MRBR APX 11(MPD 321000-04-1)Weight OnWheelsBrakedAxle201272644201272649Evidence of corrosionfound on AxleDetailed Inspection ofAxle Outer DiameterAll 1Cor at opportunityof Brake changeSIL 32-088MRBR APX 11(MPD 324100-05-1)Weight offWheelsMLG BogiePivot Pin201269612201489621201454925201489751In-service issueregarding chromeloss and corrosionIn-service data collectionon Bogie Pivot PininspectionAll At opportunity ofBogie Pivot PinremovalVendor Service LetterA33-34/A26MRBR APX 11Weight OffWheelsMLGBellcrank20148300/30120148353/35420158306/30720158300/301In-service issueregarding introducinggrease to theBellcrankDetailedProcedure forLubricating theBellcrankAll 250FC or 4 MOVendor Service LetterA33-34/A27MRBR APX 11Weight OnWheelsSM 8 Pin201275789201478617In-service issue:bush migrationReduced LubricationintervalAll 250FC or 4MO MRBR APX 11(MRBR task 32.11.00/01)Weight OnWheelsSM 9 Pin 201275790201478616In-service issue:bush migrationReduced LubricationintervalAll 250FC or 4MO MRBR APX 11(MRBR task 32.11.00/01)Weight OnWheelsA330 MRB REPORTIssue : July 2010Page: APX 11. 3b) MLG modifications recommended to be accomplished prior to a 10 year TBOAirbus and Messier-Dowty advise A330 operators to consider accomplishing the following recommended product improvement modifications prior to Main Landing Gearoverhaul. The benefit to the operator will be an improved operational reliability of the post mod parts and a lower level of degradation at overhaul.VendorServiceBulletinReferenceAirbusServiceBulletinReferenceModNumberThreshold/IntervalDescriptionIntroduced asStandard inProductionFrom MSN:CommentsA33/34-32-171A330-32-313549358 3 years from EIS Introduce new adjustable link assembly(201254 Series – Basic Gear)MSN 435 Inspection taskapplicable for premod statusA33/34-32-172A330-32-313549358 3 years from EIS Introduce new adjustable link assembly(201489 Series – Growth Gear)MSN 435 Inspection taskapplicable for premod statusA33/34-32-197A330-32-314149664 4 years from EIS New Shortening Mechanism connecting link(201254 Series – Basic Gear)MSN 454 There is noInspection taskapplicable for premod, as stresscorrosion is noteasily detectableRequires jackingfor replacement.A33/34-32-198A330-32-314149664 4 years from EIS New Shortening Mechanism connecting link(201489 Series – Growth Gear)MSN 454 There is noInspection taskapplicable for premod, as stresscorrosion is noteasily detectableRequires jackingfor replacement.A330 MRB REPORTIssue : July 2010Page: APX 11. 4c) MLG modifications recommended to be accomplished at the 10 year overhaulBased on in-service data, Airbus and Messier-Dowty advise A330 operators to consider accomplishing the following recommended product improvement modifications at firstoverhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a lower level of degradation at secondoverhaul.VendorServiceBulletinReferenceAirbusServiceBulletinReferenceModNumberDescription Introduced asStandard inProductionFrom MSN:CommentsA33/34-32-153A330-32-311447523 New Aluminum Piston with Nickel under ChromeOxide coating (201254 Series – Basic Gear)MSN 315 All in-service parts postmod.A33/34-32-154A330-32-311447523 New Aluminum Piston with Nickel under ChromeOxide coating (201489 Series – Growth Gear)MSN 315 All in-service parts postmod.A33/34-32-175A330-32-312648246 New Bushes in Bogie Beam & Slider(201254 Series – Basic Gear)MSN 366 Bushes replaced with lateststandard at overhaulA33/34-32-176A330-32-312648246 New Bushes in Bogie Beam & Slider(201489 Series – Growth Gear)MSN 366 Bushes replaced with lateststandard at overhaulA33/34-32-190A330-32-314349777 Improved corrosion protection for Retraction Link &‘W’ Pin(201254 Series–Basic Gear)MSN 454 Improved protective coatingapplied at overhaulA33/34-32-191A330-32-314349777 Improved corrosion protection for Retraction Link &‘W’ Pin(201489 Series–Growth Gear)MSN 454 Improved protective coatingapplied at overhaulA33/34-32-193A330-32-314249806 New Axle with Additional Corrosion Protection(201254 Series–Basic Gear)MSN 459 Application of top coat paintover SermetalA33/34-32-194A330-32-314249806 New Axle with Additional Corrosion Protection(201489 Series–Growth Gear)MSN 459 Application of top coat paintover SermetalA33/34-32-195A330-32-316250959 Modified Uplock Roller assembly & new bolts(201254 Series – Basic Gear)MSN 527 Basic Main Fitting replacedat overhaul and includesnew Uplock RollerAssembly.A33/34-32-196A330-32-316250959 Modified Uplock Roller assembly & new bolts(201489 Series – Growth Gear)MSN 527 Replaced with new UplockRoller assembly at overhaulA330 MRB REPORTIssue : July 2010Page: APX 11. 5d) MLG items requiring further sampling and/or data from recent overhauls to justify 10 year TBO interval on individual partsItem/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationRetractionLink201489311/12 Required for10 year TBOjustificationTwo additional8-year samples(samplesperformed at 7.5years would beacceptable)Post Mod48066First Retraction Linkavailable for sampling willbe from January 20098 YEARS*(based on previous 5 yearsample)Weight OnWheelsRetractionActuator114256002-030114256002-040Required for10 year TBOjustificationAdditionalsample to beperformed atopportunity ofOverhaulAll Additional RetractionActuator will be availablefor sampling from end of20088 YEARS*(10-year TBO low riskbased on samples to date)Weight OnWheels* Note:8 Year restoration limit refers to the parts as listed, not to the assembly or the aircraft on which they are installed.At the time of the sampling program, the MLG Retraction Actuator was considered by the industry as an “on-condition” item. Assuch, it was only functionally tested atoverhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and complete overhaul.Retrospective compliance is currently not required for retraction actuators not having been overhauled. However, this is underreview by Airbus and Messier-Dowty.Once completed, sampling results will be communicated to the MRB/ISC for review.A330 MRB REPORTIssue : July 2010Page: APX 11. 6e) MLG items requiring further sampling or using data from recent overhauls to justify 20,000FC TBO interval.Item/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul requirement ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationMain GearAssembly201252001/002or201490001/002Required tojustify20,000FCTBO intervalOne sample All Proposal is to sampleMLG from MSN 428.Sample available by May200917,000FC* Aircraft onjacks – offwing task* Note:17,000FC restoration limit refers to the parts as listed, and not necessarily to the aircraft on which they are installed.Once completed, sampling results will be communicated to the MRB/ISC for review.A330 MRB REPORTIssue : July 2010Page: APX 11. 73. A330 NOSE LANDING GEARa) NLG required Inspection and Lubrication TasksThere are currently no required NLG inspections tasks affecting TBO intervals.b)NLG modifications recommended to be accomplished prior to a 10 year TBOThere are currently no NLG modifications recommended to be accomplished prior to a 10 year TBO.c) NLG modifications recommended to be accomplished at the 10 year overhaulBased on in-service data, Airbus and Messier-Dowty advise A330 operators to consider accomplishing the following recommended product improvement modifications at firstoverhaul. The benefit to the operator will be an improved operational reliability of the modified parts post overhaul. It will also lead to a lower level of degradation at secondoverhaul.VendorServiceBulletinReferenceAirbusServiceBulletinReferenceModNumberDescription Introduced asStandard inProductionFrom MSN:CommentsD23581-32-053None 54793 Introduction of a New Shock Absorber Tube andModification of the Material of the diaphragmMSN 793 Replaced at overhaul with anew Shock Absorber Tubeand modified DiaphragmA330 MRB REPORTIssue : July 2010Page: APX 11. 8d) NLG items requiring sampling and/or data from recent overhauls to justify 10 year TBO interval on individual partsItem/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval AircraftmaintenanceconfigurationRetractionActuatorD23352000seriesRequired for10 year TBOjustificationData from twoRetractionActuators at a 10year Overhauland/or from twoFleet LeadersAll Retraction Actuator will beavailablefor sampling by end of200810 YEARSTo be justified using datafrom Overhaul and/or fromFleet leadersWeight OnWheelsNote:At the time of the sampling program, the NLG Retraction Actuator was considered by the industry as an “on-condition” item. As such, it was only functionallytested at overhaul. Subsequently, some parts of the Retraction Actuator became PSE’s and therefore require sampling and complete overhaul.Retrospective compliance is currently not required for Retraction Actuators not having been overhauled. However, this is underreview by Airbus and Messier-Dowty.Once completed, sampling results will be communicated to the MRB/ISC for review.A330 MRB REPORTIssue : July 2010Page: APX 11. 9e) NLG items requiring further sampling and/or data from recent overhauls to justify 20,000FC TBO interval.Item/ComponentItem PartNumberComments /ReasonRequirement ApplicabilityMod StatusSampling/OVH dataReporting DateOverhaul interval ifsatisfactory additionalsampling not achieved.AircraftmaintenanceconfigurationNose GearAssemblyD23285001D23285051D23285101D23285151D23581100Required tojustify20,000FCTBO intervalOne sample All Proposal is to sampleNLG from MSN 428.Sample available by May2009.17,000FC* Aircraft onjacks – offwing task* Note:17,000FC restoration limit refers to the parts as listed, and not necessarily to the aircraft on which they are installed.Once completed, sampling results will be communicated to the MRB/ISC for review.

# 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).