# @ A300 SERVICE BULLETIN SUMMARY

7 DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : 1 of 4 Printed in FRANCE © AIRBUS, 2007 All rights reserved 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 : 57 TITLE : WINGS - MAIN LANDING GEAR ATTACHMENT - INSPECTION OF THE MLG RIB 5 AFT BEARING FORWARD LUG MODIFICATION No. : None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During routine maintenance, a crack has been found visually in the forward lug of the MLG rib 5 aft bearing attachment on two A310 in-service aircraft. The concerned aircraft had accumulated 24,000 Flight Cycles (FC) and 27,000 FC at the time of finding (Refer to OIT 999.0115/06). In both cases the cracks extended through the entire thickness of the forward lug. The examination of the cracked ribs has confirmed that the crack originated due to the presence of pitting corrosion in the forward lug holes. Other small corner crack sites were also identified within the corroded region adjacent to the crack. Also on both aircraft medium to heavy corrosion was found in the forward lugs on the opposite wing after removal of the bushes. As an interim measure the Alert Service Bulletin (ASB) A300-57A0248 was issued to introduce a repetitive Detailed Visual Inspection (DVI) of the forward lug of the MLG Rib 5 aft bearing attachment. This Inspection Service Bulletin introduces a repetitive inspection program to detect a crack in the forward lug of the RH and LH MLG Rib 5 aft bearing attachment. Operators now have the choice to perform an ultrasonic inspection or a DVI. The ultrasonic inspection will detect any crack at an early stage and limit the risk of extensive repairs. This earlier crack detection is not possible with the DVI. If no crack is found the operator has the option to embody the modification Service Bulletin A300-57-0249 (Mod No. 13348H5689) or to perform repeat inspections. The embodiment of Service Bulletin A300-57-0249 (Mod No. 13348H5689) is strongly recommended and will cancel the inspection requirements of this Service Bulletin.

# @ A300 SERVICE BULLETIN SUMMARY

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved This Service Bulletin supersedes Alert Service Bulletin A300-57A0248. NOTE : Aircraft which have had Service Bulletin A300-57-0249 (Mod No. 13348H5689) embodied or which have had oversized interference fit bushes installed in the LH and/or RH MLG rib 5 aft bearing forward lugs as per Repair R57240221 are not affected by this Service Bulletin. If oversized interference fit bushes have been installed as per Repair R57240221 on one wing only, then the opposite wing must be inspected. The repeat inspections will make sure that any crack in the inspection area on the forward lug of the MLG rib 5 aft bearing attachment will be identified.

EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) : 001 60W A2S ABR AFG BCS BLM DHL F2I FLM IAC IRM KZU MNB MSR NTR OHY RUN TCN TDX TNO TSY CONCURRENT REQUIREMENTS It is recommended that this Service Bulletin can be done at the same time : Service Bulletin No. A300-57-0212 REFERENCES/REPERCUSSIONS TFU : 57.51.34.004 OEB : None AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : OIT SE 999.0115/06 NATURE OF THE WORK AIRCRAFT : Yes EQUIPMENT : No EVALUATION TABLE COMPLIANCE Mandatory 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 No KIT PRICE (USD) No AIRBUS kit

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# @ A300 SERVICE BULLETIN SUMMARY

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved HARD : No SOFT : No OBRM : No MANPOWER Config. 01 Ultrasonic Inspection

Config. 01 Detailed Visual Inspection

MATERIAL INFORMATION AIRCRAFT DATA No AIRBUS kit is required for the accomplishment of this Service Bulletin. APPENDICES Appendix 01 - Inspection Report TOTAL MANHOURS 3.0 ELAPSED TIME (HOURS) 2.5

TOTAL MANHOURS 1.5 ELAPSED TIME (HOURS) 1.0

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# @ A300 SERVICE BULLETIN SUMMARY

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 4

# @ A300 SERVICE BULLETIN

7 DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : 1 of 15 Printed in FRANCE © AIRBUS, 2007 All rights reserved 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 : 57 TITLE : WINGS - MAIN LANDING GEAR ATTACHMENT - INSPECTION OF THE MLG RIB 5 AFT BEARING FORWARD LUG 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 A. EFFECTIVITY (1) Models B4-103 B4-120 B4-203 B4-2C C4-203 F4-203 (2) Aircraft (a) Effectivity by MSN This Service Bulletin is applicable to aircraft MSN : 0019 0035 0041 0044 0045 0047 0053 0055 0063 0073-0075 0078 0079 0083-0085 0093-0095 0100 0101 0105 0107 0116 0117 0121 0123-0126 0128 0129 0133-0139 0141 0147-0152 0154-0157 0170 0173 0175 0180-0184 0189 0190 0192 0196 0199 0200 0203 0204 0207 0208 0210-0212 0216 0218-0220 0222 0227 0234-0236 0239 0240 0243 0247 0249 0250 0255 0256 0259 0261 0265 0271 0274 0277 0289 0292 0299 0302 0304 (b) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the

# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 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.

(c) Effectivity by MSN and Kit/Configuration The kits and configurations applicable to these MSNs are given at the end of this list: 0019 0035 0041 0044-0045 0047 0053 0055 0063 0073-0075 0078-0079 0083-0085 0093-0095 0100-0101 0105 0107 0116-0117 0121 0123-0126 0128-0129 0133-0139 0141 0147-0152 0154-0157 0170 0173 0175 0180-0184 0189-0190 0192 0196 0199-0200 0203-0204 0207-0208 0210-0212 0216 0218-0220 0222 0227 0234-0236 0239-0240 0243 0247 0249-0250 0255-0256 0259 0261 0265 0271 0274 0277 0289 0292 0299 0302 0304 OPERATOR MSN 001 0203 60W 0073 0134 0157 0196 0218 A2S 0063 ABR 0148 0184 0189 AFG 0180 0190 BCS 0095 0116 0150 0152 0199 0208 0219 0220 0234 0235 0236 0250 0259 0274 0289 BLM 0239 DHL 0084 0085 0141 0149 0249 0265 F2I 0079 0093 0094 0128 0133 0135 0136 0137 0156 0170 0243 FLM 0151 0256 IAC 0181 0182 0240 IRM 0035 0055 0175 0204 KZU 0041 0044 0101 0117 0139 0173 MNB 0019 0047 0123 0126 0212 0222 0277 0292 0304 MSR 0200 0255 NTR 0124 0155 0210 0227 0247 0261 OHY 0138 0192 0299 0302 RUN 0075 0083 0105 0107 0121 0147 0154 0183 TCN 0125 TDX 0053 0100 0207 0211 0216 0271 TNO 0045 0074 0078 TSY 0129

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Config. 01 is valid for all the aircraft which have not had Service Bulletin A300-57-0249 (Mod. No. 13348H5689) embodied or which have not had oversized interference fit bushes installed in the LH and/or RH MLG rib 5 aft bearing forward lugs as per Repair Instruction R57240221. If oversized interference fit bushes have been installed as per Repair Instruction R57240221 on one wing only, then the opposite wing must be inspected. (3) Spares None B. CONCURRENT REQUIREMENTS It is recommended that this Service Bulletin can be done at the same time : Service Bulletin No. A300-57-0212 C. REASON (1) History During routine maintenance, a crack has been found visually in the forward lug of the MLG rib 5 aft bearing attachment on two A310 in-service aircraft. The concerned aircraft had accumulated 24,000 Flight Cycles (FC) and 27,000 FC at the time of finding (Refer to OIT 999.0115/06). In both cases the cracks extended through the entire thickness of the forward lug. The examination of the cracked ribs has confirmed that the crack originated due to the presence of pitting corrosion in the forward lug holes. Other small corner crack sites were also identified within the corroded region adjacent to the crack. Also on both aircraft medium to heavy corrosion was found in the forward lugs on the opposite wing after removal of the bushes. As an interim measure the Alert Service Bulletin (ASB) A300-57A0248 was issued to introduce a repetitive Detailed Visual Inspection (DVI) of the forward lug of the MLG Rib 5 aft bearing attachment. (2) Objective/Action This Inspection Service Bulletin introduces a repetitive inspection program to detect a crack in the forward lug of the RH and LH MLG Rib 5 aft bearing attachment. KIT No. QTY PER A/C CONFIGURATION 01

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Operators now have the choice to perform an ultrasonic inspection or a DVI. The ultrasonic inspection will detect any crack at an early stage and limit the risk of extensive repairs. This earlier crack detection is not possible with the DVI. If no crack is found the operator has the option to embody the modification Service Bulletin A300-57-0249 (Mod No. 13348H5689) or to perform repeat inspections. The embodiment of Service Bulletin A300-57-0249 (Mod No. 13348H5689) is strongly recommended and will cancel the inspection requirements of this Service Bulletin. This Service Bulletin supersedes Alert Service Bulletin A300-57A0248. NOTE : Aircraft which have had Service Bulletin A300-57-0249 (Mod No. 13348H5689) embodied or which have had oversized interference fit bushes installed in the LH and/or RH MLG rib 5 aft bearing forward lugs as per Repair R57240221 are not affected by this Service Bulletin. If oversized interference fit bushes have been installed as per Repair R57240221 on one wing only, then the opposite wing must be inspected. (3) Advantages The repeat inspections will make sure that any crack in the inspection area on the forward lug of the MLG rib 5 aft bearing attachment will be identified. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : (1) Config. 01 (a) Make the work area safe. (b) Get access to the forward lugs of the LH and RH MLG rib 5 aft bearing attachment. (c) Do a DVI or an ultrasonic inspection. (d) Close up and complete the documentation. E. COMPLIANCE (1) Classification Mandatory

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (2) Accomplishment Timescale (a) A DVI or Ultrasonic Inspection of the MLG Rib 5 is mandatory before accumulation of 12,000 FC from new or from the MLG Rib 5 replacement when applicable. If a MLG Rib 5 has been changed on one side only then the RH and LH should be considered separately. If the 12,000 FC threshold has been exceeded then the first inspection is mandatory within 10 calendar days from receipt of this Service Bulletin. 1 If there are no findings, a repeat inspection is required until accomplishment of Service Bulletin A300-57-0249 (Mod No. 13348H5689) at the intervals that follow : — DVI every 100 FC — Ultrasonic Inspection every 675 FC. NOTE : If the ASB A300-57A0248 has been accomplished then the next DVI should be 100 FC from the last inspection accomplished by ASB A300-57A0248. 2 In case of findings per the visual inspection, the MLG Rib 5 fitting will have to be replaced before the next flight. 3 In case of findings per the ultrasonic inspection and if no crack is visible, aircraft can continue operation up to the accomplishment of the Repair Instruction R57240221, providing a repeat visual inspection is performed every 36 calendar hours with no findings. In case of findings from the visual inspection, the fitting will have to be replaced before the next flight. NOTE : The ultrasonic inspection will detect any crack at an early stage and limit the risk of extensive repairs. This earlier crack detection is not possible with the DVI. NOTE : Aircraft which have had Service Bulletin A300-57-0249 (Mod No. 13348H5689) embodied or which have had oversized interference fit bushes installed in the LH and/or RH MLG rib 5 aft bearing forward lugs as per Repair R57240221 are not effected by this Service Bulletin. If oversized interference fit bushes have been installed as per Repair R57240221 on one wing only, then the opposite wing must be inspected. (b) Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals and/or date) given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale.

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved F. APPROVAL Approved under EASA 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. 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. Config. 01

H. WEIGHT AND BALANCE Not changed I. ELECTRICAL LOAD DATA Not changed J. REFERENCES Get access 0.5 Ultrasonic inspection 2.0 Close-up 0.5 TOTAL MANHOURS 3.0 ELAPSED TIME (HOURS) 2.5 Get access 0.5 Visual inspection 0.5 Close-up 0.5 TOTAL MANHOURS 1.5 ELAPSED TIME (HOURS) 1.0

Aircraft Maintenance Manual (AMM) : 24-00-00 32-00-00 Elec. Std. Practices Manual (ESPM) : 20-55-00 Non destructive Testing Manual (NTM) : 51-40-00 57-42-11 Service Bulletin : A300-57-0212 Service Bulletin : A300-57-0249

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved K. PUBLICATIONS AFFECTED

L. INTERCHANGEABILITY/MIXABILITY Not applicable Service Bulletin : A300-57A0248 Repair Instruction : R57240221

Maintenance Planning Document (MPD) : Volume 1

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 2. MATERIAL INFORMATION 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 None D. LIST OF MATERIALS — OPERATOR SUPPLIED (1) Consumable Materials

(2) Components If a repair is to be accomplished, refer to Repair Instruction R57240221 for required components. E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR None F. TOOLING — PRICE AND AVAILABILITY None G. SPECIAL TOOLS Refer to NTM 57-42-11, Part 4 and Repair Instruction R57240221 for special tooling information. DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C INST DISP Cleaning Agent 11-026 As required Ardrox AV15 15-009A As required

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 3. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING : MAKE SURE THAT THE LANDING GEAR GROUND SAFETIES AND THE WHEEL CHOCKS ARE IN POSITION. 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. (1) Preparation (a) Config. 01 1 Make sure that the ground safety pins are in position on the MLG (Refer to AMM 32-00-00 Page block 301). 2 Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00 Page block 301). 3 Put a warning notice on the panel 4VU to tell persons not to operate the landing gear. 4 Put the access platforms in position. 5 Clean the inspection area use Cleaning Agent (Mat No. 11-026) . (2) Standard Practices None B. INSPECTION NOTE (01) Operators can choose between an ultrasonic inspection as per para 3.B.(1) or a DVI as per para. 3.B.(2).

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE (02) The worksteps that follow are to be done on the wings (LH and/or RH) which have not had Service Bulletin A300-57-0249 (Mod No. 13348H5689) embodied or which have not had oversized interference fit bushes installed in the aft bearing forward lugs as per Repair R57240221. (1) Config. 01 (a) Ultrasonic Inspection Refer to Figure 1 1 Do the ultrasonic inspection of the forward lug of the MLG Rib 5 attachment fitting (Refer to NTM 57-42-11 Part 4). 2 If a crack is found, do workstep 3.B.(1)(b) and refer to the Flow Chart, Figure 2 . 3 If no cracks are found it is strongly recommended that the modification Service Bulletin A300-57-0249 (Mod No. 13348H5689) is accomplished within 675 FC. If the modification is not accomplished at this stage then apply a protective coating of Ardrox AV 15 (Mat No. 15-009A) around the interface of the bush and lug and refer to Para 3.E CLOSE-UP.
(b) Detailed Visual Inspection Refer to Figure 1 1 Prepare the area (Refer to NTM 51-40-00, Part 1). NOTE : When looking forward, cracks are most likely to occur on the aft face of the gear rib 5 forward lug at approximately the 4 O'clock position on the LH gear rib and at approximately the 8 o'clock position on the RH gear rib. 2 Visually inspect the forward lug. Pay special attention to the inboard face and to the forward and aft sides of the lug. 3 If a crack is found contact AIRBUS immediately. The cracked Rib 5 will have to be replaced before the next flight. 4 If no cracks are found it is strongly recommended that Repair Instruction R57240221 is accomplished within 100FC. If the repair is not accomplished at this stage then, apply a protective coating of Ardrox AV 15 (Mat No. 15-009A) around the interface of the bush and lug and refer to Para 3.E CLOSE-UP. (c) Report any findings to AIRBUS (Refer to Appendix 01).

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved C. TEST None D. CLOSE UP (1) Config. 01 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Remove access platforms. (c) Remove safety devices from the landing gear and landing gear doors. (d) Remove warning notices. E. DOCUMENTATION Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 1 Config. 01: DVI Area of the MLG Forward Lug Faces

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# @ A300 SERVICE BULLETIN

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 2 Sheet 1 Config. 01: LH and RH Wing MLG Forward Lug Inspection Flowchart

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# @ A300 SERVICE BULLETIN APPENDIX 01

7 DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : 1 of 2 Printed in FRANCE © AIRBUS, 2007 All rights reserved 1. INSPECTION REPORT The results of the inspection, including no findings, replacement or actions to be done, must be forwarded to AIRBUS Department (SEE82), on the attached inspection report sheet.

# @ A300 SERVICE BULLETIN APPENDIX 01

DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 1 LH and RH wing MLG rib 5 attachment lugs - Inspection Report

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# @ A300 SERVICE BULLETIN REPORTING SHEET

7 DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : 1 of 1 Printed in FRANCE © AIRBUS, 2007 All rights reserved TITLE : WINGS - MAIN LANDING GEAR ATTACHMENT - INSPECTION OF THE MLG RIB 5 AFT BEARING FORWARD LUG 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: 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.

# @ A300 SERVICE BULLETIN QUALITY PERCEPTION FORM

7 DATE : Aug 08/07 SERVICE BULLETIN No. : A300—57—0251 REVISION No. : 00 — Page : 1 of 1 Printed in FRANCE © AIRBUS, 2007 All rights reserved 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 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - 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 X Mod/Inspection X Manpower Operator Supplied 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 Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.