# @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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 32 

### TITLE: LANDING GEAR - MAIN GEAR - REPEAT INSPECTION OF THE INTERNAL SURFACE OF THE BOGIE BEAM 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 inspection is valid for aircraft Pre Modification No. 54500H15561 (Service Bulletin A330-32-3212) and Pre Modification No. 58896H16335 (Service Bulletin A330-32-3237). (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 0069-0073 0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 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 0247-0251 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 DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 1 7

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SERVICE BULLETIN

0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 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 0716-0718 0720-0722 0724-0726 0728-0730 0732-0734 0737 0739 0741 0743 0745-0746 0749 0752 0755 0760 (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 AAR 0640 0676 0708 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AEA 0461 0505 0526 0551 0597 0733 0745 0749 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 ALK 0303 0306 0311 0313 0404 0456 0627 AZA 0272 0339 BEL 0030 0037 0045 0082 0095 0229 0249 BER 0120 0127 0288 0322 0403 0432 0444 0454 0469 0476 0493 0739 BMA 0398 0401 BTV 0205 0330 CAL 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 CES 0713 0720 0728 0732 CPA 0012 0017 0071 0102 0113 0118 0121 0155 0244 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 CRL 0285 0320 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 0718 0722 DGA 0240 DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 EDW 0291 EIN 0269 0397 ETD 0658 0688 0717 0724 0729 0730 0737 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 0755 FWI 0253 GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 2 7

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# @A330
SERVICE BULLETIN

OPERATOR MSN GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0083 0099 0106 0109 0234 0405 0479 0512 0581 0654 0662 0692 0716 0741 HFY 0096 0211 HVN 0262 0275 0294 0299 0366 I2L 0364 IAC 0353 0362 ISS 0665 IWD 0670 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 0425 0428 0484 0490 0550 KKK 0343 0358 KLM 0682 0686 0703 MAS 0067 0069 0073 0077 0100 0107 0110 0116 0119 0290 0296 0300 MON 0261 0265 MSR 0600 0610 0666 0683 0696 0709 0726 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 0721 0734 0743 0746 0760 RSY 0171 SAS 0496 0497 0515 0568 SWR 0324 TAM 0232 0238 0247 0259 0361 0466 0472 0477 0486 0700 TAP 0181 0195 0223 0305 0308 0312 0317 TCX 0254 0266 0301 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0463 0504 0697 0704 TSC 0111 0132 0177 0250 0271 0369 0407 0427 0480 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 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 VLK 0055 0070 0086 VOZ 0365 0372 XAX 0054 XLF 0501 0635

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 3 7

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SERVICE BULLETIN
(4) Configuration by MSN MSN CONFIGURATION 0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064 0065 0066 0067 0069 0070 0071 0072 0073 0077 0082 0083 0086 0087 0095 0096 0098 0099 0100 0102 0106 0107 0109 0110 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 0205 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 0524 0525 0526 0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549 0550 0551 0552 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 0632 0633 0634 0635 0636 0637 0638 0640 0641 0642 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 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729 0730 0732 0733 0734 0737 0739 0741 0743 0745 0746 0749 0752 0755 0760 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 None

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 4 7

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# @A330
SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS None C. REASON (1) History An operator of an A330 in-service aircraft reported that the bogie beam on the right hand MLG ruptured while taxiing during a slow turning manoeuvre. Investigations have revealed that the rupture was due to compromized paint protection leading to excessive corrosion on the internal surface of the bogie beam. Further investigations indicate that a corrosion pit reached a depth sufficient to promote stress corrosion cracking and a subsequent fast static rupture. No evidence of fatigue was apparent. Initial inspections of 15 aircraft on the bogie beams belonging to 5 operators have found 8 further bogie beams with compromized paint surfaces and corrosion in this area. A further 2 bogie beams were suffering from paint damage. So far no bogie beams have been scrapped but some repairs outside the published limits have been necessary. (2) Objective/Action This Service Bulletin is published to advise operators of A330 aircraft of the issue of MESSIER DOWTY Service Bulletin No. A33/34-32-272. This Service Bulletin details instructions to perform a repeat inspection on the internal surface of the bogie beam assemblies to ensure that there is no corrosion. The inspection requires the removal of the bogie beam assembly and a detailed inspection of the internal surfaces using a boroscope. (3) Advantages This Service Bulletin will give an early detection of corrosion and prevent possible rupture of the bogie beam due to corrosion. The inspection requirement is cancelled by the accomplishment of Service Bulletin No. A330-32-3237. MESSIER-DOWTY Service Bulletin No. A33/34-32-284. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 323225-832-895-001: INSPECTION (1) Remove the Bogie Beam Assembly from both the LH and RH Wings (2) Do the inspection on the Bogie Beam Assembly LH and RH Wings

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 5 7

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# @A330
SERVICE BULLETIN
(3) Install the Bogie Beam Assembly to the LH and RH Wings E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must be used as the reference document for the mandated accomplishment timescale. MLG Bogie Beam Condition Inspection Threshold Inspection Interval MLG bogie beams which have not embodied AIRBUS modification 54500H15561 in production nor AIRBUS Service Bulletin No. A330-32-3212 in service, and which had accumulated on 03 June 2008 (the effective date of EASA AD 2008-0093) less than or equal to 4.5 years since their first flight on an aeroplane or since their first flight after their last overhaul, as applicable. At the first convenient maintenance opportunity which occurs after the 4.5 years threshold, but no later than 6 years since the LH or RH MLG bogie beam first flight on an aeroplane or since first flight after its last overhaul, as applicable

MLG bogie beams which have not embodied AIRBUS modification 54500H15561 in production nor AIRBUS Service Bulletin A330-32-3212 in service, and which had accumulated on 03 June 2008 more than 4.5 years since their first flight on an aeroplane or since their first flight after their last overhaul, as applicable. At the next convenient maintenance opportunity, or within 18 months after 04 January 2008 (the effective date of EASA AD 2007-0314R1), whichever occurs first and without exceeding the next bogie beam overhaul. No later than 6 years, but no earlier than 4 years since its first flight after the MLG bogie beam overhaul which occurs after the last inspection

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 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 6 7

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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 323225-832-895-001: INSPECTION Get Access 1.00 On Aircraft Remove the Bogie Beam Assembly from both the LH and RH Wings 10.00 Install the Bogie Beam Assembly to the LH and RH Wings 10.00 Tests 2.50 Close-Up 1.00 TOTAL MANHOURS 24.50 ELAPSED TIME (HOURS) 12.00 Additional manhours related to Vendor SB; refer to: Do the inspection on the Bogie Beam Assembly LH and RH Wings MESSIER DOWTY Service Bulletin No. A33/34-32-272 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 20-11-11 20-21-12 20-28-00 32-11-14 Elec. Std. Practices Manual (ESPM) 20-55-00 Vendor Service Bulletin (VSB) MESSIER DOWTY Service Bulletin No. A33/34-32-272 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 7 7

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# @A330
SERVICE BULLETIN

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# @A330
SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Inspection and repair of removed equipment should be negotiated directly with MESSIER DOWTY as per instructions given in Service Bulletin No. A33/34-32-272. (2) Price and Availability No AIRBUS kit will be provided. Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272 for the equipment sales terms. B. INDUSTRY SUPPORT INFORMATION Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272 for the industry support terms. C. LIST OF COMPONENTS Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272. D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials To accomplish this Service Bulletin it will be necessary to use the consumable materials included in AMM Task 32-11-14-410-801 and MESSIER DOWTY Service Bulletin No. A33/34-32-272. (2) Components To accomplish this Service Bulletin it will be necessary to use the expendable parts included in AMM Task 32-11-14-410-801 and MESSIER DOWTY Service Bulletin No. A33/34-32-272. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272. DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 9 7

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# @A330
SERVICE BULLETIN
(2) Tools To accomplish this Service Bulletin it will be necessary to use the tools listed in AMM Task 32-11-14-010-801 and AMM Task 32-11-14-410-801. Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272. (3) Special Tools Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 10 7

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# @A330
SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 323225-832-895-001 - INSPECTION WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. Task Associated Data Zone 731 741 Manpower TOTAL MANHOURS 24.50 ELAPSED TIME (HOURS) 12.00 Additional manhours related to Vendor SB; refer to: MESSIER DOWTY Service Bulletin No. A33/34-32-272 A. GENERAL (1) Subtask 323225-910-401-001 - Standard Practices Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803 Task 20-21-12-911-801 Task 20-28-00-912-802 (a) Put blanking caps on all the related disconnected electrical-connectors. (b) Put blanking caps on all the related disconnected hydraulic-connectors.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 11 7

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# @A330
SERVICE BULLETIN
(c) Tightening Torques for Pipe Unions (Refer to AMM Task 20-21-12-911-801). (d) Electrical Bonding of Components with Conductive Screws and Bolts (Refer to AMM Task 20-28-00-912-802). (e) For the removal and installation of wire locking (Refer to AMM Task 20-11-11-911-803). (2) Subtask 323225-839-401-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in the Service Bulletin. B. PREPARATION (1) Subtask 323225-941-401-001 - Job Set-Up Work Zones and Access Panels Zone Access/Work location 731 741 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 32-11-14-010-801 (a) Do the "Job Set-up" procedures as specified in AMM Task "Removal of the MLG Bogie Beam Assembly for Access, Complete with Wheels and Brakes" (Refer to AMM Task 32-11-14-010-801). C. PROCEDURE (1) Subtask 323225-020-401-001 - Remove the Bogie Beam Assembly from both the LH and RH Wings Work Zones and Access Panels Zone Access/Work location 731 741 Manpower Resources Manhours 10.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 12 7

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# @A330
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 32-11-14-010-801 (a) Remove the LH and RH Bogie Beam Assembly for Access, Complete with Wheels and Brakes (Refer to AMM Task 32-11-14-010-801). (2) Subtask 323225-832-405-001 - Do the inspection on the Bogie Beam Assembly LH and RH Wings Work Zones and Access Panels Zone Access/Work location 731 741 References Vendor Service Bulletin (VSB) MESSIER DOWTY A33/34-32-272 Fig. A-UFAAA Inspection Flowchart Sheet 01
NOTE: The latest revision of MESSIER DOWTY Service Bulletin No. A33/34-32-272 must be used. Refer to Fig. A-UFAAA Sheet 01

. (a) Do the inspection on the bogie beam assembly LH and RH (Refer to MESSIER DOWTY Service Bulletin No. A33/34-32-272). (b) Report all findings, including nil findings, to AIRBUS SEEL3 department within 90 days. Refer to Appendix. 1 - Inspection Report of Bogie Beam Assembly , Inspection Report. (3) Subtask 323225-420-401-001 - Install the Bogie Beam Assembly to the LH and RH Wings Work Zones and Access Panels Zone Access/Work location 731 741 Manpower Resources Manhours 10.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 13 7

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SERVICE BULLETIN
(a) Install the LH and RH Bogie Beam assembly After Access, Complete with Wheels and Brakes (Refer to AMM Task 32-11-14-410-801). D. TEST (1) Subtask 323225-700-401-001 - Test Work Zones and Access Panels Zone Access/Work location 731 741 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801 (a) Do the test procedures as specified in AMM Task "Installation of the MLG Bogie Beam Assembly after Access, Complete with Wheels and Brakes" (Refer to AMM Task 32-11-14-410-801). E. CLOSE-UP (1) Subtask 323225-832-408-001 - Close-Up Work Zones and Access Panels Zone Access/Work location 731 741 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 32-11-14-410-801 (a) Make sure that the work area is clean and clear of tools and other items of equipment. (b) Do the "Close up" procedures as specified in AMM Task "Installation of the MLG Bogie Beam Assembly after Access, Complete with Wheels and Brakes" (Refer to AMM Task 32-11-14-410-801).

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 14 7

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SERVICE BULLETIN

**CONF ALL

YES
QUESTION
ACTION
FINDING DO A DETAILED INSPECTION
OR RH BOGIE BEAM INTERNAL DIAMETER FOR CORROSION OR IN PARAGRAPH 1E(2) OF THE LH

BEAM INTERNAL SURFACE

PROTECTION INTACT? IS THE BOGIE

CONFIRM THE EXTENT OF THE CADMIUM/BASE METAL DAMAGE) BEFORE NEXT FLIGHT DAMAGE (LEVEL OF PAINT/

IS THE REPAIRABLE? BOGIE BEAM

PROCEED WITH REPAIR BEFORE NEXT FLIGHT, AND

RECORD THE DAMAGE.
RECORD THE REPAIRS MADE FINDINGS AND RETURN INTO SERVICE RECORD THE NIL

SCRAP THE BOGIE BEAM RECORD THE FINDINGS. WITHIN 90 DAYS, INFORM AIRBUS AND MESSIER−DOWTY LTD. OF INSPECTION RESULTS

BEEN EMBODIED ON THE AIRCRAFT OR A33/34−32−284 HAS SB32−3237
BEEN APPLIED ON THE

NO FURTHER ACTION BOGIE BEAM) ? YES

YES NO

NO

NO BETWEEN 4 AND 6 YEARS REPEAT THE INSPECTION AFTER OVERHAUL, WITHIN THE TIMESCALE DEFINED

PAINT DAMAGE

**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. G_SB_323225_7_FAAA_01_03 Figure A-UFAAA - Sheet 01 Inspection Flowchart

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 15 7

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SERVICE BULLETIN

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# @A330
SERVICE BULLETIN Appendix. 1 - Inspection Report of Bogie Beam Assembly **CONF ALL (1) Appendix. 1 - Inspection Report of Bogie Beam Assembly INSPECTION REPORT OF BOGIE BEAM ASSEMBLY LH WING SERVICE BULLETIN NO. A330-32-3225 DATE OF INSPECTION: OPERATOR: AIRCRAFT MSN: SERIAL NUMBER FLIGHT HOURS FLIGHT CYCLES BOGIE BEAM PAINT DAMAGE FOUND YES NO OVER WHAT AREA LOCATION (AXIALLY AND CIRCUMFERENTIALLY) USE THE ILLUSTRATIONS SUPPLIED IN MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272 TO INDICATE THE AREA AND THE LOCATION AND RETURN TO AIRBUS WITH THIS REPORT. BOGIE BEAM CORROSION DAMAGE FOUND YES NO OVER WHAT AREA LOCATION (AXIALLY AND CIRCUMFERENTIALLY) USE THE ILLUSTRATIONS SUPPLIED IN MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272 TO INDICATE THE AREA AND THE LOCATION AND RETURN TO AIRBUS WITH THIS REPORT. DEPTH OF THE CORROSION: SURFACE ONLY, REFER TO MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272. WITHIN REPAIRABLE LIMITS, REFER TO MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272. OUTSIDE THE ABOVE REPAIR LIMITS, CONTACT AIRBUS CUSTOMER SERVICES FOR FURTHER ADVICE / NTO APPLICATION. AREA AND MAXIMUM BLEND NECESSARY TO CLEAR THE CORROSION NOTE: Include photographs of the area before repair and return to AIRBUS. Report all findings including nil findings to AIRBUS Customer Services. INSPECTION REPORT OF BOGIE BEAM ASSEMBLY RH WING SERVICE BULLETIN NO. A330-32-3225 DATE OF INSPECTION: OPERATOR: AIRCRAFT MSN: SERIAL NUMBER FLIGHT HOURS FLIGHT CYCLES BOGIE BEAM PAINT DAMAGE FOUND YES NO OVER WHAT AREA LOCATION (AXIALLY AND CIRCUMFERENTIALLY) USE THE ILLUSTRATIONS SUPPLIED IN MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272 TO INDICATE THE AREA AND THE LOCATION AND RETURN TO AIRBUS WITH THIS REPORT. BOGIE BEAM CORROSION DAMAGE FOUND YES NO

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 1 7

Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

# @A330
SERVICE BULLETIN Appendix. 1 - Inspection Report of Bogie Beam Assembly
OVER WHAT AREA LOCATION (AXIALLY AND CIRCUMFERENTIALLY) USE THE ILLUSTRATIONS SUPPLIED IN MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272 TO INDICATE THE AREA AND THE LOCATION AND RETURN TO AIRBUS WITH THIS REPORT. DEPTH OF THE CORROSION: SURFACE ONLY, REFER TO MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272. WITHIN REPAIRABLE LIMITS, REFER TO MESSIER DOWTY SERVICE BULLETIN NO. A33/34-32-272. OUTSIDE THE ABOVE REPAIR LIMITS, CONTACT AIRBUS CUSTOMER SERVICES FOR FURTHER ADVICE / NTO APPLICATION. AREA AND MAXIMUM BLEND NECESSARY TO CLEAR THE CORROSION NOTE: Include photographs of the area before repair and return to AIRBUS. Report all findings including nil findings to AIRBUS Customer Services.

DATE: Nov 21/07 SERVICE BULLETIN No.: A330-32-3225 REVISION No.: 02 - Oct 26/12 Page: 2 7

Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.