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@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - MAIN GEAR - INTRODUCE NEW RE-DESIGNED
PISTON ROD ON THE RETRACTION ACTUATOR MODIFICATION No.: 52980H15418 54648H15734 This page transmits Revision No.05 of Service Bulletin No.A330-32-3180
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
Additional work was required at revision 04 for aircraft in Config. 003 modified by revision 03.
ADDITIONAL WORK consisted of re-identifying the part numbers of The Main Landing Gear (MLG) Retraction-Actuator.
REASON Revision No. 05 issued to:
- update the effectivity to include MSN 0067
- add accomplishment instruction notes (AIRBUS standard sentences) to the Modification task.
CHANGES NOTE : Revision bars against references not identified in the CHANGES paragraph appear due to format changes introduced by new authorities’ rules.
SUMMARY
EFFECTIVITY
OPERATOR LIST UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 001
CONFIGURATION DEFINITION UPDATED R CONF 002
CONFIGURATION DEFINITION UPDATED R DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
MATERIAL INFORMATION
PARTS TO BE RE-IDENTIFIED BY
OPERATOR
PARTS TO BE RE-IDENTIFIED BY OPERATOR
UPDATED R Reidentified part set REIDB02
PART MATERIAL SET UPDATED R
ACCOMPLISHMENT INSTRUCTIONS TASK 323180- 831-895-001-
MODIFICATION
TASK SOLUTION UPDATED
NOTE UPDATED
CAUTION UPDATED R Subtask 323180-941-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 323180-941-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 323180-941-401-004
SUBTASK SOLUTION UPDATED R Subtask 323180-831-406-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-407-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-408-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-410-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-406-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-407-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-408-001
SUBTASK SOLUTION UPDATED R Subtask 323180-831-410-001
SUBTASK SOLUTION UPDATED R Subtask 323180-200-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 323180-831-410-003
SUBTASK SOLUTION UPDATED
PART NUMBER DESCRIPTION UPDATED R Subtask 323180-700-401-001
SUBTASK SOLUTION UPDATED R Subtask 323180-700-401-001
SUBTASK SOLUTION UPDATED R Subtask 323180-700-401-003
SUBTASK SOLUTION UPDATED R Subtask 323180-942-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 323180-942-401-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED R Subtask 323180-942-401-003
SUBTASK SOLUTION UPDATED R TASK 323180- 831-896-001-
MODIFICATION - ADDITIONAL WORK - Re-identify the part numbers of the Main Landing Gear (MLG) Retraction Actuator for aircraft that accomplished Service Bulletin at Rev 03
TASK SOLUTION UPDATED
CAUTION UPDATED R Subtask 323180-941-402-001
SUBTASK SOLUTION UPDATED R Subtask 323180-930-401-001
SUBTASK SOLUTION UPDATED
PART NUMBER DESCRIPTION UPDATED R Subtask 323180-942-402-003
SUBTASK SOLUTION UPDATED R
FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS Revision No. 3 issued to add a note that PN 114256004-005 has the strike 9 cancelled and to include the old PN 114256005-000.
Revision No. 04 issued to correct new P/N on the Retraction Actuator in interchangeability table paragraph 1L Config. 003. The opportunity has been taken to update the effectivity and to merge Config. 003 and Config. 004.
NOTE : This is only applicable for Revision No. 3 and subsequent. If information is required for Revisions issued previous to this, please check your copies of Revision Transmittal Sheets or contact AIRBUS.
REVISION SEQUENCE ORIGINAL: Sep 20/04 REVISION No. : 03 - Jan 28/11 REVISION No. : 04 - Jul 30/13 REVISION No. : 05 - Jan 27/14 DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - MAIN GEAR - INTRODUCE NEW RE-DESIGNED
PISTON ROD ON THE RETRACTION ACTUATOR **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 52980H15418 MINOR 54648H15734 NOTE : As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Two fractures of the piston rod for the MLG retraction-actuator have occurred on an in-service A330 aircraft, close to the spherical bearing. Additionally another piston rod has fractured, due to a longitudinal crack. Both failures are corrosion related.
In addition, two fatigue test failures occurred on an A340-600 piston rod, one occurred at the lug net tension area originating from the chrome plating run-out. The other failure was caused by the absence of shot peening resulting in machining marks remaining in the bore.
The mandatory ISB No. A330-32-3173 was issued to do an ultrasonic NDT and detailed visual inspection of the MLG retraction-actuator piston rod.
Service Bulletin No. A330-32-3174 (Mod No. 52424H15395) was also issued to introduce a MLG retraction-actuator which had a solid piston rod. This new design was only intended for interim use to alleviate supply demands. It was only intended to be installed to prevent an AOG situation.
This Service Bulletin is published to advise all operators of A330 aircraft of the issue of Messier-Dowty Service Bulletin No. A33/34-32-227.
This Service Bulletin introduces a new MLG retraction-actuator which has a re-designed piston rod. The new re-designed piston rod has the following changes:
DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY
- an increased radial wall thickness
- revised internal bore configuration
- safety vent hole removed
- new rod screwed plug which now includes a safety vent hole.
NOTE : Retraction actuators P/N 114256004-005 (post production modification) and P/N 114256004-000 (post retrofit modification) are fully two-way interchangeable with each other (as they are effectively the same LRU identified differently).
Accomplishment of this Service Bulletin cancels the mandatory inspection requirements of Inspection Service Bulletin No. A330-32-3173.
Accomplishment of this Service Bulletin introduces a new piston rod. The new piston rod has a higher fatigue life limit than the part number presently defined in the Airworthiness Limitation Section (ALS) Part 1.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB YES
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 YES
NORMAL JACKING YES NOTE
(1) : Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION **CONF 001 No Material **CONF 002 No Material **CONF 003 No Material
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY 31V 38W AAR ABD
ACA ACI AEA AFR AIC
ALK ARG
AZA BEL
BER CAL CES CPA CRL CSA
CSC CSN DAH DAL DGA DLH EDW EIN ETD EVA FWI GFA GIA GRL HDA HFY HVN I2L IYE JAV
JST KAL KLM MAS MON MSR OHY PAL QAF QFA QTR RSY SAI
SAS SYA
TAE TAM TAP TCX THA THY TSC UAE USA VKG VOZ WRC
XAX XLF NOTE : Modification No. 52980H15418 is embodied before delivery on aircraft MSN 0644 and subsequent.
Modification No. 54648H15734 is embodied before delivery on aircraft MSN 0717 and subsequent.
CONCURRENT REQUIREMENTS None
REFERENCES / REPERCUSSIONS TFU
32.31.46.008 OEB None AOT None SIL None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT Yes * NOTE : * Retraction Actuator Piston Rod is life limited to ALS Part 1.
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT YES HARD NO SOFT NO OBRM NO
MANPOWER **CONF 001 Task 323180-831-895-001: MODIFICATION
TOTAL MANHOURS
22.50
ELAPSED TIME (HOURS)
22.50 Additional manhours relat ed to Vendor SB; refer to:
Do the Modification to the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227 Re-identify the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227 DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY Task 323180-831-896-001: MODIFICATION - ADDITIONAL WORK - Re-identify the part numbers of the Main Landing Gear (MLG) Retraction Actuator for aircraft that accomplished Service Bulletin at Rev 03
TOTAL MANHOURS
0.00 **CONF 002 Task 323180-831-895-001: MODIFICATION
TOTAL MANHOURS
22.50
ELAPSED TIME (HOURS)
22.50 Additional manhours relat ed to Vendor SB; refer to:
Do the Modification to the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227 Re-identify the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227 Task 323180-831-896-001: MODIFICATION - ADDITIONAL WORK - Re-identify the part numbers of the Main Landing Gear (MLG) Retraction Actuator for aircraft that accomplished Service Bulletin at Rev 03
TOTAL MANHOURS
0.00 **CONF 003 Task 323180-831-895-001: MODIFICATION
TOTAL MANHOURS
2.00
ELAPSED TIME (HOURS)
2.00 Additional manhours relat ed to Vendor SB; refer to:
Re-identify the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227 Task 323180-831-896-001: MODIFICATION - ADDITIONAL WORK - Re-identify the part numbers of the Main Landing Gear (MLG) Retraction Actuator for aircraft that accomplished Service Bulletin at Rev 03
TOTAL MANHOURS
2.00
ELAPSED TIME (HOURS)
2.00 Additional manhours relat ed to Vendor SB; refer to:
Re-identify the MLG Retraction Actuator MESSIER-DOWTY Service Bulletin No. A33/34-32-227
APPENDICES **CONF ALL None DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - MAIN GEAR - INTRODUCE NEW RE-DESIGNED
PISTON ROD ON THE RETRACTION ACTUATOR MODIFICATION No.: 52980H15418 54648H15734 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 Pre Mod No. 54500H15561 (Service Bulletin No. A330-32-3212) (Enhanced MLG).
(1) Models 330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321 330-322 330-323 330-341 330-342 330-343
(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 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0249 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: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 0711-0714 0716
(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 31V 0205 38W 0401 AAR 0640 0676 0708 ABD 0343 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0505 0526 0551 0597 0670 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 0358 0364 AZA 0272 0339 BEL 0030 0037 0045 0082 0095 0229 0249 0324 BER 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 CES 0713 CPA 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0679 CRL 0285 0320 CSA 0425 CSC 0462 CSN 0649 0652 0656 0664 DAH 0644 0647 0650 0653 0667 DAL 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620 0621 0631 0633 0663 0674 0690 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 EDW 0291 EIN 0269 0397 ETD 0658 0688 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
OPERATOR MSN FWI 0253 GFA 0276 0281 0286 0287 0334 0340 0527 0532 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 0654 0669 0673 HFY 0096 0127 0211 0262 HVN 0275 0294 0299 0366 I2L 0480 IYE 0625 0632 JAV 0255 JST 0506 0508 0513 0522 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0428 0484 0490 0550 KLM 0682 0686 0703 MAS 0067 0116 0119 0300 MON 0261 0265 MSR 0600 0610 0666 0683 0696 0709 OHY 0072 0087 0098 0143 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 0605 QFA 0553 0558 0564 0574 0593 0595 0603 0695 0705 0712 QTR 0441 0473 0489 0511 0521 0571 0612 0616 0623 0637 0638 0659 0680 0684 0711 RSY 0120 0171 SAI 0055 0070 0086 SAS 0496 0497 0515 0568 SYA 0345 TAE 0348 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 TAP 0181 0195 0223 0305 0308 0312 0317 TCX 0254 0266 0301 0398 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0463 0504 0529 0697 0704 TSC 0111 0132 0177 0271 0369 0407 0427 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0382 0384 0392 0396 0409 0437 0451 0452 0455 0491 0494 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 VKG 0309 0349 0356 0357 VOZ 0365 0372 WRC 0296 XAX 0054 0330 0662 0692 0716 XLF 0501 0635 DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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 0183 0184 0188 0189 0191 0198 0200 0203 0206 0209 0219 0224 0231 0234 0241 0244 0256 0267 0277 0279 0284 0315 0323 0333 0337 0338 0342 0344 0346 0349 0350 0351 0356 0357 0368 0370 0375 0380 0386 0388 0389 0393 0400 0405 0407 0408 0412 0418 0419 0420 0421 0423 0425 0428 0439 0479 0484 0490 0496 0497 0512 0515 0524 0533 0539 0542 0548 0549 0550 0552 0553 0558 0564 0565 0568 0570 0574 0576 0578 0579 0581 0588 0591 0593 0595 0602 0603 0607 0623 0629 0636 0637 0640 0641 0642 002 0181 0195 0205 0211 0222 0223 0226 0229 0230 0232 0238 0240 0247 0248 0249 0251 0253 0254 0255 0258 0259 0261 0262 0265 0266 0269 0271 0272 0275 0276 0281 0283 0285 0286 0287 0288 0290 0291 0293 0294 0295 0296 0299 0300 0301 0303 0305 0306 0308 0309 0311 0312 0313 0314 0316 0317 0320 0322 0324 0326 0328 0330 0334 0339 0340 0343 0345 0348 0353 0358 0361 0362 0364 0365 0366 0369 0372 0382 0384 0392 0396 0397 0398 0401 0403 0404 0409 0422 0427 0432 0437 0441 0443 0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463 0465 0466 0469 0472 0473 0476 0477 0480 0481 0486 0487 0489 0491 0493 0494 0498 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0513 0516 0518 0519 0521 0522 0525 0526 0527 0529 0530 0532 0535 0536 0551 0555 0567 0571 0573 0584 0587 0597 0600 0605 0609 0610 0612 0614 0616 0618 0620 0621 0625 0627 0631 0632 0633 0634 0635 0638 001 0644 0645 0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658 0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671 0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686 0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700 0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714 0716 003
(5) Configuration definition **CONF 001 Config. 001 is valid for A330-200 aircraft which are pre Modification No. 52980H15418 and pre Modification No. 54648H15734.
**CONF 002 Config. 002 is valid for A330-300 aircraft which are pre Modification No. 52980H15418 and pre Modification No. 54648H15734.
**CONF 003 Config. 003 is valid for A330-200 and A330-300 aircraft which are post Modification No.
52980H15418 and pre Modification No. 54648H15734.
DATE: Sep 20/04 SERVICE BULLETIN No.: A330-32-3180 REVISION No.: 05 - Jan 27/14 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.