# @A330 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for A330 aircraft, and with regards to previously embodied SRM Allowable Damage Limits (ADL), AIRBUS is requiring operators to apply specific actions defined in this Service Bulletin. This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary. Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the door surrounding skin panels at cutout corner areas. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION No Material

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 1 6

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# @A330 SERVICE BULLETIN SUMMARY EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

36V 38W 69X ABD ACA ACI AEA AFR AIC ALK ARG AZA AZU BEL BER BGH CPA CRL CSA CSC DGA EDW EIN EVA FWI GFA GIA GRL HDA HFY HVN KAL MAS MON OHY PAL QAF QFA QTR RSY SAI SAS SYA TAE TAM TAP TCX THA THY TSC UAE USA VKG WRC XAX XLF CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 533232-832-849-001: Inspection TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 APPENDICES None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 2 6

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# @A330 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE : This Service Bulletin is only applicable to aircraft on which Modification No. 49144S16279 has not been embodied. (1) Models 330-202 330-203 330-223 330-243 330-301 330-321 330-322 330-323 330-341 330-342 330-343 (2) Effectivity by MSN 0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0067 0070-0072 0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 1 6

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# @A330 SERVICE BULLETIN

0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0525-0527 0529-0530 0532 0535-0536 0539 0548 0550-0551 0565 0567-0568 0581 0584 0597 0627 0635 0657 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 36V 0437 0451 38W 0401 69X 0494 ABD 0343 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0505 0526 0551 0597 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 AIC 0353 0362 ALK 0303 0306 0311 0313 0404 0456 0627 ARG 0290 0300 0358 0364 AZA 0272 0339 AZU 0365 0372 0527 0532 BEL 0030 0037 0045 0082 0095 0229 0249 0324 BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 BGH 0255 CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 CRL 0285 0320 CSA 0425 CSC 0462 DGA 0240 EDW 0291 EIN 0269 0397 EVA 0530 0535 FWI 0253 GFA 0276 0281 0286 0287 0334 0340 GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405 0479 0512 0581 HFY 0096 0127 0211 0262 HVN 0275 0294 0299 0366 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0428 0484 0490 0550 DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 2 6

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# @A330 SERVICE BULLETIN

OPERATOR MSN MAS 0067 0116 0119 MON 0261 0265 OHY 0072 0087 0098 0143 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 QFA 0506 0508 0513 0522 QTR 0441 0473 0489 0511 0521 RSY 0120 0171 SAI 0055 0070 0086 SAS 0496 0497 0515 0568 SYA 0345 TAE 0348 TAM 0232 0238 0247 0259 0361 0466 0472 TAP 0181 0195 0223 0305 0308 0312 0317 0477 0486 TCX 0254 0266 0301 0398 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0463 0504 0529 TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392 0396 0409 0452 0455 0491 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 VKG 0309 0349 0356 0357 WRC 0296 XAX 0054 0330 XLF 0501 0635

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 3 6

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# @A330 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0067 0070 0071 0072 0082 0083 0086 0087 0095 0096 0098 0099 0102 0106 0109 0111 0112 0113 0116 0118 0119 0120 0121 0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198 0200 0203 0206 0209 0211 0219 0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240 0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256 0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275 0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324 0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343 0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358 0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400 0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420 0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484 0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0515 0516 0518 0519 0521 0522 0525 0526 0527 0529 0530 0532 0535 0536 0539 0548 0550 0551 0565 0567 0568 0581 0584 0597 0627 0635 0657 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity No Material Set B. CONCURRENT REQUIREMENTS None C. REASON (1) History Following changes in the Apr-13 revision of the Structural Repair Manual (SRM) for A330 aircraft, and with regards to previously embodied SRM Allowable Damage Limits (ADL), AIRBUS is requiring operators to apply specific actions defined in this Service Bulletin.

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 4 6

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# @A330 SERVICE BULLETIN (2) Objective/Action This Service Bulletin is issued to instruct operators to examine their records and take the applicable corrective action when necessary. (3) Advantages Accomplishment of this Service Bulletin will contribute to maintain the structural integrity of the door surrounding skin panels at cutout corner areas. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 533232-832-849-001: Inspection (1) Do a check of the Aircraft Records E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Table 1, Config. 001 - A330-200 SRM Update of the Fuselage Door Surround Panel Corners ADL Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval
All Aircraft Identify records of Structural Repair Manual Allowable Damage Limits (SRM ADLs) for the LH and RH Mid Pax door surround areas. 12 months from September 2014. See Note (**) None None

Existing ADL covered by a SRM version prior to April 2013 revision Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions. See Note (*) As soon as possible before September 2015 None None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 5 6

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# @A330 SERVICE BULLETIN
Table 1, Config. 001 - A330-200 SRM Update of the Fuselage Door Surround Panel Corners ADL Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval No existing ADL covered by an SRM version prior to April 2013 revision No further action necessary within this Service Bulletin None None None

All Aircraft Identify records of SRM ADLs for the Fwd cargo door, LH and RH emergency exit door/Pax Door 3, LH and RH Aft Pax door, Aft cargo door and Bulk cargo door surround areas. 24 months from September 2014 See note (**) None None

Existing ADL covered by a SRM version prior to April 2013 revision Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions. See Note (*) As soon as possible before September 2016 None None

No existing ADL covered by an SRM version prior to April 2013 revision No further action necessary within this Service Bulletin None None None

Table 2, Config. 001 - A330-300 SRM Update of the Fuselage Door Surround Panel Corners ADL Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval
All Aircraft Identify records of Structural Repair Manual Allowable Damage Limits (SRM ADLs) for the LH and RH Mid Pax Door, Fwd cargo door, LH and RH emergency exit door/Pax Door 3, LH and RH Aft Pax door, Aft cargo door and Bulk cargo door surround areas. 24 months from September 2014. See note (**) None None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 6 6

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# @A330 SERVICE BULLETIN
Table 2, Config. 001 - A330-300 SRM Update of the Fuselage Door Surround Panel Corners ADL Compliance time (Whichever occurs first/later) Condition Action Threshold Grace period Repetitive interval Existing ADL covered by a SRM version prior to April 2013 revision Update the recorded inspection threshold and interval in line with the value given in the April 2013 or subsequent SRM revisions. See Note (*) As soon as possible before September 2016 None None

No existing ADL covered by an SRM version prior to April 2013 revision No further action necessary within this Service Bulletin None None None

NOTE: (*): Any new ADL inspection instruction following this update can be achieved at the customers convenience: - at any time within the Service Bulletin compliance time but no later than any existing repair inspection already scheduled before the update - as per the new inspection instruction updated following this Service Bulletin, only the schedule of the updated inspection instruction is required to close the Service Bulletin, not the inspection itself. NOTE: (**): It is recommended to check records within 6 months after the SB issue date. This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and date given but reference should be made to the AD for confirmation of the mandated accomplishment timescale. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 7 6

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# @A330 SERVICE BULLETIN
G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 533232-832-849-001: Inspection On Aircraft Do a check of the Aircraft Records 1.00 TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Structural Repair Manual (SRM) 53-00-11 53-31-11 53-41-11 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 8 6

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# @A330 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY None B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 9 6

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# @A330 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 10 6

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# @A330 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 533232-832-849-001 - Inspection NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words "refer to" are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words "in accordance with" are used then the given procedure must be followed. NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. NOTE: The purpose of flow charts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin. Task Associated Data Manpower TOTAL MANHOURS 1.00 ELAPSED TIME (HOURS) 1.00 A. GENERAL (1) Subtask 533232-839-202-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 11 6

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# @A330 SERVICE BULLETIN
C. PROCEDURE (1) Subtask 533232-839-201-001 - Do a check of the Aircraft Records Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Structural Repair Manual (SRM) 53-00-11, Page Block 101 53-31-11, Page Block 101 53-41-11, Page Block 101 Fig. A-GBAAA Identification of the SRM ADLs Sheet 01 Fig. A-GFAAA Flowchart Sheet 01
NOTE : It is recommended to check the records within 6 months after Service Bulletin issue date. NOTE: Any new ADL inspection instruction following this update can be achieved at the customers convenience: - at any time within the Service Bulletin compliance time, but no later than any existing repair inspection already scheduled before update
or - as per the new inspection instruction updated following this Service Bulletin, only the schedule of updated inspection is required to close this Service Bulletin, not the inspection itself. (a) Do a check of the aircraft records against the SRM ADL in accordance with SRM 53-00-11, Page Block 101 paragraph 3.A, SRM 53-31-11, Page Block 101 paragraph 7.A and SRM 53-41-11, Page Block 101 paragraph 3.A, 3.B or 3.C. For procedure and location information, refer to Fig. A-GBAAA Sheet 01 and Fig. A-GFAAA Sheet 01 1 If in the aircraft records, some damage are covered by an ADL from a SRM revision prior to Apr-13 revision, update the recorded inspection threshold and interval in line with the values given in the Apr-13 or subsequent SRM revisions. 2 If in the aircraft records, there is no damage covered by an ADL from a SRM revision prior to Apr-13 revision, then no further action is required in accordance with this Service Bulletin.

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 12 6

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# @A330 SERVICE BULLETIN
D. TEST None E. CLOSE-UP None

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 13 6

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# @A330 SERVICE BULLETIN

**CONF ALL

200 mm (7.874 in)

200 mm (7.874 in) CORNER

AREA



## A TYPICAL

NOTE: 01 ONLY LH UPPER CORNER IS SHOWN, BUT THIS IS APPLICABLE TO ALL FOUR CORNERS. LOCATION FUSELAGE, DOOR CUT OUT AT CORNER AREAS FORWARD CARGO DOOR, MID PAX DOOR, EMERGENCY EXIT DOOR/PAX DOOR 3, AFT CARGO DOOR, BULK CARGO DOOR AND AFT PAX DOOR. 53

−00

−11 PB101 PARAGRAPH 3.A 53

−31

−11 PB101 PARAGRAPH 7.A 53

−41

−11 PB101 PARAGRAPHS 3.A, 3.B OR 3.C SRM ADL REFERENCES

MID PAX

DOOR

EMERGENCY EXIT DOOR PAX DOOR 3

DOOR CUT OUT CORNER AREAS 01 

### A

FORWARD CARGO DOOR 200 mm (7.874 in) MID PAX

DOOR

BULK CARGO DOOR AFT PAX DOOR

AFT PAX

DOOR

AFT CARGO DOOR 

### A A A A A A A

G_SB_533232_6_BAAA_01_01 Figure A-GBAAA - Sheet 01 Identification of the SRM ADLs
DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 14 6

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# @A330 SERVICE BULLETIN

**CONF ALL

EXISTING ADL IS COVERED BY A SRM VERSION PRIOR

TO APR

−13 REVISION YES

UPDATE THE RECORDED INSPECTION THRESHOLD AND INTERVALS IN LINE WITH

THE VALUES GIVEN IN THE APR

−13 OR NO

NO FURTHER ACTION AS PER THIS SERVICE BULLETIN

NOTE: THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN. IDENTIFY RECORDS OF SRM ALLOWABLE DAMAGE LIMITS (ADL) FOR EACH RECORD, FOLLOW THE INSTRUCTIONS BELOW

SUBSEQUENT SRM REVISIONS

FOR THE ACCOMPLISHMENT TIMESCALE, REFER TO PARAGRAPH 1.E.(2) ANY NEW ADL INSPECTION INSTRUCTIONS FOLLOWING THIS UPDATE CAN BE ACHIEVED AT THE OPERATORS CONVENIENCE:

−AT ANY TIME WITHIN THE SB COMPLIANCE TIME BUT NO LATER THAN ANY EXISTING

REPAIR INSPECTION ALREADY SCHEDULED BEFORE UPDATE 01 02 01 02

−AS PER THE NEW INSPECTION INSTRUCTIONS UPDATED FOLLOWING THIS SB.

ONLY THE SCHEDULE OF THE UPDATED INSPECTION INSTRUCTIONS IS REQUIRED TO CLOSE THIS SB, NOT THE INSPECTION ITSELF. G_SB_533232_6_FAAA_01_05 Figure A-GFAAA - Sheet 01 Flowchart
DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 15 6

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# @A330 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - INSPECTION OF DOOR SURROUNDING SKIN PANELS AT CUTOUT CORNER AREAS MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 1 6

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# @A330 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Nov 04/14 SERVICE BULLETIN No.: A330-53-3232 REVISION No.: 00 - Nov 04/14 Page: 1 6

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