# @ A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : 1 of 3 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 

# MANDATORYMANDATORY MANDATORY

ATA SYSTEM : 53 TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES. MODIFICATION No. : NONE This page transmits Revision No. 03 of Service Bulletin No. A300-53-0350. ADDITIONAL WORK No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 03 issued to update the effectivity, to update the price of the Kit A05, A08, A09 and A10, to add the reference of the existing splice A53834139202/203. CHANGES SUMMARY : — REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES . Evaluation table updated. — EFFECTIVITY . Operators updated. NOTE added. PLANNING INFORMATION : — EFFECTIVITY . Para. 1.A. Operator AIB, aircraft MSN 0195, 0238, 0305 deleted. Aircraft MSN 0177 deleted for operator AIC. Operator BAE, aircraft MSN 0158, 0161 deleted. Operator CAL, aircraft 0193, 0197, 0221, 0232 deleted. Aircraft MSN 0023 deleted for operator C2A. Operator E4G, aircraft MSN 0069 deleted. Operator F2I, aircraft MSN 0033, 0145 deleted. Aircraft MSN 0131 deleted for operator HLA. Aircraft MSN 0262 deleted for operator IAC. Aircraft MSN 0110, 0169, 0174, 0178, 0194 deleted for operator JAS. Operator LFA, aircraft MSN 0066 deleted. Operator NTL, aircraft MSN

# @ A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 0046, 0127 deleted. Aircraft MSN 0086, 0087 deleted for operator OHY. Operator P2G, aircraft MSN 0091 deleted. Operator PIA, aircraft MSN 0064, 0096, 0098, 0099, 0114, 0144, 0146, 0269 deleted. Aircraft MSN 0106, 0140, 0142 deleted for operator TAI. Aircraft MSN 0042 deleted for operator TLP. Operators updated. NOTE updated. — COMPLIANCE . Para. 1.E. Sentence updated. — APPROVAL . Para. 1.F. Sentence updated. — REFERENCES . Para. 1.J. Reference of the ESPM 20-55-00 added. Reference of the AMM 24-40-00 becomes 24-00-00. MATERIAL INFORMATION : — MATERIAL - PRICE AND AVAILABILITY . Para. 2.A. Address updated. Price updated for Kit A05, A08, A09 and A10. — INDUSTRIAL SUPPORT . Para. 2.B. Sentence added. — LIST OF COMPONENTS . Para. 2.C. NOTE concerning the Standards Manual added. — TOOLING - PRICE AND AVAILABILITY . Para. 2.F. Address updated. ACCOMPLISHMENT INSTRUCTIONS : — GENERAL . Para. 3.A. Paragraph concerning the WARNING and CAUTION added. Reference of the AMM 24-40-00 becomes 24-00-00. — ILLUSTRATIONS . Figure 1 modified. . Figure 2, Sheet 1 modified and Sheet 2 added. . Figure 10, Sheet 1 modified. APPENDIX 1 : — Para. 1. AIRBUS DEPT. updated.

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# @ A300 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS Revision No. 01 issued to inform the operators that Service Bulletin No. A300-53-0350 replaces the All Operator Telex (AOT) A300-53A0350. The All Operator Telex (AOT) requires the inspection of one hole, the Service Bulletin requires the inspection of the 14 holes. Revision No.02 is issued to inform the operators of the SB update further to the validation of the equivalent A300-600 Service Bulletin on MSN 0635.The Service Bulletin becomes mandatory and The Airworthiness Directive No.2002-184 (B) is added. REVISION SEQUENCE ORIGINAL : Oct 25/99 REVISION No. : 01 — Dec 18/01 REVISION No. : 02 — Nov 12/02 REVISION No. : 03 — Jul 26/07

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# @ A300 SERVICE BULLETIN SUMMARY

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 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 

# MANDATORYMANDATORY MANDATORY

ATA SYSTEM : 53 TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES. MODIFICATION No. : NONE REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Service Bulletin No. A300-53-0199 (A300) and Service Bulletin A300-53-6131 (A300-600), modification No. 05890S6739, specifies cold working of fastener holes in the splice fitting at FR47. The Service Bulletin No. A300-53-0199 currently terminates the inspection requirements of Service Bulletin No. A300-53-0200. Cracks have been found on post Service Bulletin No. A300-53-0199 aircraft in the fastener holes which attach the splice fitting to FR47 (ref. A300 SRM 53-15-00 Fig. 112 item 39 and A300-600 SRM 57-10-24 Fig. 8 item 125A). A laboratory investigation has been performed on a cracked splice fitting, and the analysis of the crack growth rate shows that an inspection program is required for post Service Bulletin No. A300-53-0199 B4/C4/F4 aircraft. Due to the structural similarity, the inspection is also required on A300-600 aircraft. AOT A300-53A350 and A300-600-53A6123 were issued to call for a one-time inspection of the splice fitting between stringers 24 and 26, LH and RH sides. This Service Bulletin has been created to define a new inspection program for the pre-mod. and post-mod. 05890S6739 aircraft (FUSELAGE - FRAME 47 - REINFORCE LATERAL SECTION BY STRENTHENED FISH PLATE) and supersede previous inspection Service Bulletin A300-53-0200. This Service Bulletin recommends an HFEC rotating probe inspection after bolt removals of the splice fitting between stringers 24 and 26 and subsequent action in case of findings. Accomplishment of this Service Bulletin permits early detection of cracking in the splice fitting to avoid cracking in the FR47 which would require extensive repairs.

# @ A300 SERVICE BULLETIN SUMMARY

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved The equivalent of this Service Bulletin has been validated on A300-600 aircraft MSN 0635.

EFFECTIVITY This Service Bulletin is applicable to these operators : 001 60W A2S ABR AFG BCS BLM DHL F2I FLM IAC IRB IRM KZU MNB MSR NTR OHY RUN TCN TDX TNO TSY NOTE : This Inspection Service Bulletin is applicable on all A/C model B4, C4, F4 pre or post Mod. 05890S6739, with or without Service Bulletin No. A320-53-0199 retrofitted. CONCURRENT REQUIREMENTS None REFERENCES/REPERCUSSIONS TFU : None OEB : None AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : None NATURE OF THE WORK AIRCRAFT : YES EQUIPMENT : NO HARD : NO SOFT : NO OBRM : NO EVALUATION TABLE COMPLIANCE Mandatory CANCELS INSPECTION SB No 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) See SB . .

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# @ A300 SERVICE BULLETIN SUMMARY

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved MANPOWER Config. 01 thru Config. 02 , INSPECTION : Inspect fastener holes A to N (holes without crack), LH and RH sides :

Config. 01 thru Config. 02 , REPAIR : Eliminate crack and inspect adjacent holes

Config. 01 thru Config. 02 , REPAIR : Replacement splice LH side

Config. 01 thru Config. 02 , REPAIR : Replacement splice RH side

MATERIAL INFORMATION AIRCRAFT DATA Kit 530350A01R00 thru Kit 530350A05R01 Bolts, nuts, washers Kit 530350A06R00 and Kit 530350A07R00 Splice Kit 530350A08R00 thru Kit 530350A10R00 Bolts, nuts APPENDICES Appendix 1 - INSPECTION REPORT. TOTAL MANHOURS 28.0 ELAPSED TIME (HOURS) 14.0

TOTAL MANHOURS 12.0 ELAPSED TIME (HOURS) 6.0

TOTAL MANHOURS 26.0 ELAPSED TIME (HOURS) 20.0

TOTAL MANHOURS 26.0 ELAPSED TIME (HOURS) 20.0

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# @ A300 SERVICE BULLETIN SUMMARY

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 4

# @ A300 SERVICE BULLETIN

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : 1 of 44 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 

# MANDATORYMANDATORY MANDATORY

ATA SYSTEM : 53 TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES. 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's 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 0023 0033 0035 0041 0042 0044-0047 0053 0055 0063 0064 0066 0069 0073-0075 0078 0079 0083-0087 0091 0093-0096 0098-0101 0105-0107 0110 0114 0116 0117 0121 0123-0129 0131 0133-0142 0144-0152 0154-0158 0161 0169 0170 0173-0175 0177 0178 0180-0184 0189 0190 0192-0197 0199 0200 0203 0204 0207 0208 0210-0212 0216 0218-0222 0227 0232 0234-0236 0238-0240 0243 0247 0249 0250 0255 0256 0259 0261 0262 0265 0269 0271 0274 0277 0289 0292 0299 0302 0304 0305 NOTE : This Inspection Service Bulletin is applicable on all A/C model B4, C4, F4 pre or post Mod. 05890S6739, with

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved or without Service Bulletin No. A320-53-0199 retrofitted. (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 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: 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 IRB 0299 0302 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 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 : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 0035 0041 0044 0055 0063 0079 0094 0105 0124 0128 0133 0135-0136 0148 0151 0156 0170 0184 0189 0239

The kits and configurations applicable to these MSNs are given at the end of this list: 0019 0045 0047 0053 0073-0075 0078 0083-0085 0093 0095 0100-0101 0107 0116-0117 0121 0123 0125-0126 0129 0134 0137-0139 0141 0147 0149-0150 0152 0154-0155 0157 0173 0175 0180-0183 0190 0192 0196 0199-0200 0203-0204 0207-0208 0210-0212 0216 0218-0220 0222 0227 0234-0236 0240 0243 0247 0249-0250 0255-0256 0259 0261 0265 0271 0274 0277 0289 0292 0299 0302 0304

NOTE : Config. 01 concerns all A/C model B4-100 types, (MSN 0035-0256). KIT No. QTY PER A/C CONFIGURATION 530350A01R00 1 01 530350A02R00 1 01 530350A03R00 1 01 530350A04R00 1 01 530350A05R01 1 01 530350A06R00 1 01 530350A07R00 1 01 530350A08R00 2 01 530350A09R00 2 01 530350A10R00 2 01

KIT No. QTY PER A/C CONFIGURATION 530350A01R00 1 02 530350A02R00 1 02 530350A03R00 1 02 530350A04R00 1 02 530350A05R01 1 02 530350A06R00 1 02 530350A07R00 1 02 530350A08R00 2 02 530350A09R00 2 02 530350A10R00 2 02

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Config. 02 concerns all A/C model B4-200 types, (MSN 0019-0305). NOTE : Kit 530350A01R00 : In case of no crack findings at holes A to N. Valid A/C having basic splice A53834139200/201/202/203 or Service Bulletin No. A300-53-0199 not embodied. NOTE : Kit 530350A02R00 : In case of no crack findings at holes A to N. Valid A/C having new splice A53812635200/201 (installed by Service Bulletin No.A300-53-0199 or Modification No.05890S6739). NOTE : Kit 530350A03R00 : In case of no crack findings at holes A to N. Valid A/C having new splice A53812635200/201 (replaced by Repair Instruction R53810422 SOL. A). NOTE : Kit 530350A04R00 : In case of no crack findings at holes A to N. Valid A/C having new splice A53812635200/201 (replaced by Repair Instruction R53810422 SOL. B). NOTE : Kit 530350A05R01 : In case of crack findings less than or equal to 0.8 mm (0.315in.) at holes A to N. — Valid A/C having basic splice A53834139200/201/202/203. — Valid A/C having new splice A53812635200/201 (installed by Service Bulletin No. 53-0199 or Modification No. 05890S6739 or Repair Instruction R53810422 SOL. A). — Valid A/C having new splice A53812635200/201 (replaced by Repair Instruction R53810422 SOL. B). NOTE : Kit 530350A06R00 : In case of crack findings more than 0.8 mm (0.315 in.) at holes A to N. Replacement splice, LH side. NOTE : Kit 530350A07R00 : In case of crack findings more than 0.8 mm (0.315 in.) at holes A to N. Replacement splice, RH side. NOTE : Kit 530350A08R00 : In case of crack findings more than 0.8 mm (0.315 in.) at holes A to N. Bolts for replacement splice with Repair Instruction R53810422 SOL. A. NOTE : Kit 530350A09R00 : In case of crack findings more than 0.8 mm (0.315 in.) at holes A to N. Bolts for replacement splice with Repair Instruction R53810422 SOL. B.

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Kit 530350A10R00 : In case of no crack findings in the adjacent holes. Valid all A/C. (3) Spares None B. CONCURRENT REQUIREMENTS None C. REASON (1) History Service Bulletin No. A300-53-0199 and Service Bulletin A300-53-6131 (A300-600), modification No. 05890S6739, specifies cold working of fastener holes in the splice fitting at FR47. The Service Bulletin No. A300-53-0199 currently terminates the inspection requirements of Service Bulletin No. A300-53-0200. Cracks have been found on post Service Bulletin No. A300-53-0199 aircraft in the fastener holes which attach the splice fitting to FR47 (ref. A300 SRM 53-15-00 Fig. 112 item 39 and A300-600 SRM 57-10-24 Fig. 8 item 125A). A laboratory investigation has been performed on a cracked splice fitting, and the analysis of the crack growth rate shows that an inspection program is required for post Service Bulletin No. A300-53-0199 B4/C4/F4 aircraft. Due to the structural similarity, the inspection is also required on A300-600 aircraft. AOT A300-53A350 and A300-600 53A6123 were issued to call for a one-time inspection of the splice fitting between stringers 24 and 26, LH and RH sides. This Service Bulletin has been created to define a new inspection program for the pre-mod. and post-mod. 05890S6739 aircraft (FUSELAGE - FRAME 47 - REINFORCE LATERAL SECTION BY STRENTHENED FISH PLATE) and supersede previous inspection Service Bulletin A300-53-0200. The equivalent of this Service Bulletin has been validated on A300-600 aircraft MSN 0635. (2) Objective/Action This Service Bulletin recommends an HFEC rotating probe inspection after bolt removals of the splice fitting between stringers 24 and 26 and subsequent action in case of findings.

5

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (3) Advantages Accomplishment of this Service Bulletin permits early detection of cracking in the splice fitting to avoid cracking in the FR47 which would require extensive repairs. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : On LH and RH sides, at FR47 (1) Config. 01 thru Config. 02 (a) Get access to the working area. (b) Remove fasteners A, B, C, D, E, F, G, H, I, J, K, L, M, N. (c) Perform rotating probe inspection. (d) If crack, repair and inspect the adjacent holes. (e) Close-up. E. COMPLIANCE (1) Classification Mandatory (2) Accomplishment Timescale This Service Bulletin is mandatory at the threshold and inteval given in the Figure 1, Sheet 1. Grace period for A/C model A300B4 post Mod. No. 05890S6739 For aircraft above 20000 FC : Next C-check but not exceeding 750 FC / 1500 FH, from reception date of the Revision No. 01. For other aircraft : Next C-check but not exceeding 1800FC / 3000 FH. Accomplishment of this Service Bulletin has been rendered 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 mandatory accomplishment timescale. F. APPROVAL Approved under EASA Design Organisation Approval No. EASA 21J.031.

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 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 thru Config. 02 INSPECTION Kit 530350A01R00 thru Kit 530350A04R00 Inspect fastener holes A to N (holes without crack), LH and RH sides:

Config. 01 thru Config. 02 REPAIR Kit 530350A05R01 and Kit 530350A10R00

Config. 01 thru Config. 02 Kit 530350A06R00 with Kit 530350A08R00 or Kit 530350A09R00 Replace splice LH side Gain access 4.0 Remove fasteners A to N 10.0 Inspect holes A to N 2.0 Install new fasteners 8.0 Close-up 4.0 TOTAL MANHOURS 28.0 ELAPSED TIME (HOURS) 14.0

Eliminate crack 2.0 inspect adjacent holes 2.0 Install new fasteners 8.0 TOTAL MANHOURS 12.0 ELAPSED TIME (HOURS) 6.0

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Config. 01 thru Config. 02 Kit 530350A07R00 with Kit 530350A08R00 or Kit 530350A09R00 Replace splice RH side

H. WEIGHT AND BALANCE Not changed I. ELECTRICAL LOAD DATA Not changed J. REFERENCES

Consumable Material List (CML) Nondestructive Testing Manual (NTM) 51-30-10 Part 1 Nondestructive Testing Manual (NTM) 51-31-04 Part 1. Repair Instruction R53810422 Service Bulletin No. A300-53-0199 Service Bulletin No. A300-53-0200 Standards Manual (SM) Remove splice 5.0 Install new splice 8.0 Do cold expansion 3.0 Install fasteners A to N 10.0 TOTAL MANHOURS 26.0 ELAPSED TIME (HOURS) 20.0

Remove splice 5.0 Install new splice 8.0 Do cold expansion 3.0 Install fasteners A to N 10.0 TOTAL MANHOURS 26.0 ELAPSED TIME (HOURS) 20.0

Aircraft Maintenance Manual (AMM) : 20-21-12 24-00-00 25-21-00 25-22-11 25-23-31 51-12-00 Elec. Std. Practices Manual (ESPM) : 20-55-00

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Appendix 1 K. PUBLICATIONS AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not applicable

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved

This Page Intentionally Left Blank

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 2. MATERIAL INFORMATION A. MATERIAL — PRICE AND AVAILABILITY (1) Material Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is : AIRBUS Spares Support and Services Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet : http://spares.airbus.com For ordering by fax : +49 40 50 76 25 90 (2) Price and Availability Kit 530350A01R00 Cost : 2,404.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A02R00 Cost : 2,051.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A03R00 Cost : 1,816.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A04R00

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Cost : 3,868.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A05R01 Cost : 9,170.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A06R00 Cost : 1,570.00 US Dollars Availability : 120 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A07R00 Cost : 1,570.00 US Dollars Availability : 120 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A08R00 Cost : 9,450.00 US Dollars Availability : 120 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A09R00

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Cost : 4,370.00 US Dollars Availability : 120 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. Kit 530350A10R00 Cost : 4,660.00 US Dollars Availability : 150 calendar days from receipt of order The Kit availability given above is the standard lead time from the date of your purchase order. If you require the Kit(s) before this time, please include a retrofit planning schedule with your order so that we can try to comply with your requirements. The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 530350A01R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-4 30 Nut NSA5351-4-12 14 Pin NSA5351-4-13 2 Pin NSA5351-4-15 6 Pin NSA5351-4-19 6 Pin NSA5357-4-12 14 Pin NSA5357-4-13 2 Pin NSA5357-4-15 6 Pin NSA5357-4-19 6 Pin NSA5359-4-12 14 Pin NSA5359-4-13 2 Pin NSA5359-4-15 6 Pin NSA5359-4-19 6 Pin NSA5368PD416A 30 Washer

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A02R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A03R00 ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5351-4-12 2 Pin NSA5351-4-13 2 Pin NSA5351-4-15 6 Pin NSA5351-4-19 6 Pin NSA5351-5-12 8 Pin NSA5351-5-13 2 Pin NSA5351-5-14 2 Pin NSA5357-5-12 8 Pin NSA5357-5-13 2 Pin NSA5357-5-14 2 Pin NSA5357-5-15 4 Pin NSA5359-5-12 8 Pin NSA5359-5-13 2 Pin NSA5359-5-14 2 Pin NSA5359-5-15 4 Pin NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5351-5-11 2 Pin NSA5351-5-12 10 Pin NSA5351-5-13 2 Pin NSA5351-5-14 8 Pin NSA5351-5-18 6 Pin NSA5357-4-12 2 Pin NSA5357-4-13 2 Pin NSA5357-4-15 6 Pin

14

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A04R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. NSA5357-4-19 6 Pin NSA5359-4-12 2 Pin NSA5359-4-13 2 Pin NSA5359-4-15 6 Pin NSA5359-4-19 6 Pin NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5050-6 30 Nut NSA5351-6-11 8 Pin NSA5351-6-12 2 Pin NSA5351-6-13 2 Pin NSA5351-6-14 4 Pin NSA5357-4-11 2 Pin NSA5357-4-12 2 Pin NSA5357-4-14 6 Pin NSA5357-4-18 6 Pin NSA5357-5-11 8 Pin NSA5357-5-12 2 Pin NSA5357-5-13 2 Pin NSA5359-5-11 8 Pin NSA5359-5-12 2 Pin NSA5359-5-13 2 Pin NSA5359-5-14 4 Pin NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer NSA5368PD616A 30 Washer ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

15

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Kit 530350A05R01 ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5050-6 30 Nut NSA5351-5-11 2 Pin NSA5351-5-12 14 Pin NSA5351-5-13 2 Pin NSA5351-5-14 6 Pin NSA5351-5-15 6 Pin NSA5351-5-18 6 Pin NSA5351-5-19 6 Bolt NSA5351-6-11 8 Pin NSA5351-6-12 12 Pin NSA5351-6-13 2 Pin NSA5351-6-14 2 Pin NSA5357-4-12 14 Pin NSA5357-4-13 2 Pin NSA5357-4-15 6 Pin NSA5357-4-19 6 Pin NSA5357-5-11 2 Pin NSA5357-5-12 14 Pin NSA5357-5-13 2 Pin NSA5357-5-14 2 Pin NSA5357-5-15 6 Pin NSA5357-5-18 6 Pin NSA5357-5-19 6 Pin NSA5359-4-11 2 Pin NSA5359-4-12 14 Pin NSA5359-4-13 2 Pin NSA5359-4-14 6 Pin-Hi l NSA5359-4-15 6 Pin NSA5359-4-18 6 Pin NSA5359-4-19 6 Pin NSA5359-5-11 8 Pin NSA5359-5-12 12 Pin NSA5359-5-13 2 Pin NSA5359-5-14 2 Pin NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer NSA5368PD616A 30 Washer

16

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A06R00

Kit 530350A07R00

Kit 530350A08R00 ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP A5381263520096 1 Splice

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP A5381263520196 1 Splice

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NAS1726-3E 18 Nut NAS1726-4E 42 Nut NAS1726-5E 14 Nut NAS1727-4E 8 Nut NSA5050-3 18 Nut NSA5050-4 42 Nut NSA5050-5 14 Nut NSA5351-4-11 6 Pin NSA5351-4-12 8 Pin NSA5351-4-13 12 Pin NSA5351-4-14 2 Pin NSA5351-4-15 5 Pin NSA5351-4-16 1 Pin NSA5351-5-11 1 Pin NSA5351-5-12 5 Pin NSA5351-5-13 1 Pin NSA5351-5-14 4 Pin NSA5351-5-18 3 Pin NSA5357-3-10 7 Pin NSA5357-3-12 15 Pin NSA5357-3-14 2 Pin NSA5357-4-10 1 Pin NSA5357-4-12 4 Pin NSA5357-4-13 2 Pin NSA5357-4-15 4 Pin NSA5357-4-16 1 Pin

17

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A09R00 NSA5357-4-19 3 Pin NSA5359-4-12 1 Pin NSA5359-4-13 1 Pin NSA5359-4-15 4 Pin NSA5359-4-19 3 Pin

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NAS1726-4E 42 Nut NAS1726-5E 6 Nut NAS1726-6E 8 Nut NAS1727-3E 18 Nut NAS1727-5E 8 Nut NSA5050-3 18 Nut NSA5050-4 42 Nut NSA5050-5 14 Nut NSA5351-6-11 4 Pin NSA5351-6-12 1 Pin NSA5351-6-13 1 Pin NSA5351-6-14 2 Pin NSA5357-3-12 6 Pin NSA5357-4-10 1 Pin NSA5357-4-11 7 Pin NSA5357-4-12 12 Pin NSA5357-4-13 13 Pin NSA5357-4-14 5 Pin NSA5357-4-15 6 Pin NSA5357-4-16 2 Pin NSA5357-4-18 3 Pin NSA5357-5-11 4 Pin NSA5357-5-12 1 Pin NSA5357-5-13 1 Pin NSA5359-3-10 7 Pin NSA5359-3-12 9 Pin NSA5359-3-14 2 Pin NSA5359-4-15 2 Pin NSA5359-5-11 4 Pin ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

18

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 530350A10R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS — OPERATOR SUPPLIED (1) Consumable Materials NSA5359-5-12 1 Pin NSA5359-5-13 1 Pin NSA5359-5-14 2 Pin

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP NSA5050-3 12 Nut NSA5050-4 10 Nut NSA5330-6 2 Nut NSA5351-3-10 1 Pin NSA5351-3-12 1 Pin NSA5351-3-13 9 Pin NSA5351-3-16 1 Pin NSA5351-4-13 5 Pin NSA5351-4-15 4 Pin NSA5351-4-16 1 Pin NSA5357-3-10 1 Pin NSA5357-3-12 1 Pin

DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C INST DISP Corrosion Inhibiting Brush Consistency 09-013 As required Solvant General Purpose 11-026 As required Anti-Corrosion Primer (Polyurethane) 16-001 As required Polyurethane Topcoat grey (For Internal Applic.) 16-002 As required Wash Primer 16-020 As required ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

19

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (2) Components None E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR None F. TOOLING — PRICE AND AVAILABILITY (1) To accomplish this Service Bulletin it is necessary to use the following tools and equipment listed in Nondestructive Testing Manual (NTM) 51-30-10 Part 1 and Nondestructive Testing Manual (NTM) 51-31-04 Part 1. (2) Fatigue Technology Incorporated (FTI) has allocated tool kit number FTI-A300-53-0350-1 for accomplishment of this Service Bulletin. Operators interested in obtaining the FTI tool kit should contact : Fatigue Technology Inc. 401 ANDOVER PARK EAST SEATTLE, WA 98188-7605 USA E.mail : sales@fatiguetech.com aog@fatiguetech.com Phone : (1) 206 2462010 Fax : (1) 206 2449886 G. SPECIAL TOOLS None

20

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 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. 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 thru Config. 02 1 Electrically ground the aircraft (Refer to AMM 24-00-00 Page block 301). 2 Put the access platforms in position. 3 Remove row of passenger seats at FR47 on LH and RH sides (Refer to AMM 25-21-00 Page block 401). 4 Remove lower sidewall panels at FR47 on LH and RH sides (Refer to AMM 25-23-31 Page block 401). 5 Remove heat and sound insulation blankets at FR47 on LH and RH sides (Refer to AMM 25-22-11 Page block 401). (2) Standard Practices (a) For inspection 1 For the specification of the material numbers (Mat. No.), refer to the CML. 2 Clean surfaces to be sealed with Solvant General Purpose (Mat No. 11-026) .

21

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 3 Apply sealant Corrosion Inhibiting Brush Consistency (Mat No. 09-013) . 4 Torque the standard threaded fasteners (Refer to AMM 20-21-12). (b) For repair only 1 Renew protective finish (Refer to AMM 51-12-00) using Wash Primer (Mat No. 16-020) , Anti-Corrosion Primer (Polyurethane) (Mat No. 16-001) and Polyurethane Topcoat grey (For Internal Applic.) (Mat No. 16-002) . B. INSPECTION (1) Config. 01 thru Config. 02 (a) For the inspection area, refer to figure 3 , sheets 1 and 2 . (b) Do a rotating probe inspection,NTM 51-30-10 Part 1 , NTM 51-31-04 Part 1 , refer to figure 4 , sheets 1 and 2 . (c) For the Inspection Report, refer to Appendix 01 . C. REPAIR (1) Config. 01 thru Config. 02 (a) Kit 530350A01R00 1 Install new fasteners same diameter, refer to figure 5 , figure 6 and figure 11 .

NOTE: Use washer NSA5368 only if the fasteners are too long. (b) Kit 530350A02R00 14 Pin-Hi Lok NSA5351-4-12 14 Pin-Hi Lok NSA5357-4-12 14 Pin-Hi Lok NSA5359-4-12

2 Pin-Hi Lok NSA5351-4-13 2 Pin-Hi Lok NSA5357-4-13 2 Pin-Hi Lok NSA5359-4-13 6 Pin-Hi Lok NSA5351-4-15 6 Pin-Hi Lok NSA5357-4-15 6 Pin-Hi Lok NSA5359-4-15 6 Pin-Hi Lok NSA5351-4-19 6 Pin-Hi Lok NSA5357-4-19 6 Pin-Hi Lok NSA5359-4-19 30 Nut NSA5050-4 30 Washer NSA5368PD416A

22

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved 1 Install new fasteners of same diameter, refer to figure 5 , figure 7 and figure 11 .

NOTE: Use washer NSA5368 only if the fasteners are too long. (c) Kit 530350A03R00 1 Install new fasteners of same diameter, refer to figure 5 , figure 8 and figure 11 .

NOTE: Use washer NSA5368 only if the fasteners are too long. 2 Pin-Hi Lok NSA5351-4-12 8 Pin-Hi Lok NSA5351-5-12 8 Pin-Hi Lok NSA5357-5-12 8 Pin-Hi Lok NSA5359-5-12 2 Pin-Hi Lok NSA5351-4-13 2 Pin-Hi Lok NSA5351-5-13 2 Pin-Hi Lok NSA5357-5-13 2 Pin-Hi Lok NSA5359-5-13 6 Pin-Hi Lok NSA5351-4-15 4 Pin-Hi Lok NSA5357-5-15 4 Pin-Hi Lok NSA5359-5-15 6 Pin-Hi Lok NSA5351-4-19 2 Pin-Hi Lok NSA5351-5-14 2 Pin-Hi Lok NSA5357-5-14 2 Pin-Hi Lok NSA5359-5-14 30 Nut NSA5050-4 30 Nut NSA5050-5 30 Washer NSA5368PD416A 30 Washer NSA5368PD516A

2 Pin-Hi Lok NSA5357-4-12 2 Pin-Hi Lok NSA5359-4-12 2 Pin NSA5351-5-11 8 Pin-Hi Lok NSA5351-5-12 2 Pin-Hi Lok NSA5357-4-13 2 Pin-Hi Lok NSA5359-4-13 2 Pin-Hi Lok NSA5351-5-12 2 Pin-Hi Lok NSA5351-5-13 6 Pin-Hi Lok NSA5357-4-15 6 Pin-Hi Lok NSA5359-4-15 6 Pin-Hi Lok NSA5351-5-14 6 Pin-Hi Lok NSA5357-4-19 6 Pin-Hi Lok NSA5359-4-19 6 Pin NSA5351-5-18 2 Pin-Hi Lok NSA5351-5-14 30 Nut NSA5050-4 30 Nut NSA5050-5 30 Washer NSA5368PD416A 30 Washer NSA5368PD516A

23

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (d) Kit 530350A04R00 1 Install new fasteners of same diameter, refer to figure 5 , figure 9 and figure 11 .

NOTE: Use washer NSA5368 only if the fasteners are too long. (e) Kit 530350A05R01 1 Install new fasteners, refer to figure 5 , figure 10 , sheets 1 to 3 and figure 11 . 2 Pin-Hi Lok NSA5357-4-11 8 Pin-Hi Lok NSA5357-5-11 8 Pin-Hi Lok NSA5359-5-11 8 Pin NSA5351-6-11 2 Pin-Hi Lok NSA5357-4-12 2 Pin-Hi Lok NSA5357-5-12 2 Pin-Hi Lok NSA5359-5-12 2 Pin NSA5351-6-12 6 Pin-Hi Lok NSA5357-4-14 4 Pin-Hi Lok NSA5359-5-14 4 Pin-Hi Lok NSA5351-6-14 6 Pin-Threaded NSA5357-4-18 2 Pin-Hi Lok NSA5357-5-13 2 Pin-Hi Lok NSA5359-5-13 2 Pin NSA5351-6-13 30 Nut NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5050-6 30 Washer NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer NSA5368PD616A

14 Pin-Hi Lok NSA5357-4-12 14 Pin-Hi Lok NSA5359-4-12 14 Pin-Hi Lok NSA5351-5-12 14 Pin-Hi Lok NSA5357-5-12 12 Pin-Hi Lok NSA5359-5-12 12 Pin NSA5351-6-12

6 Pin-Hi Lok NSA5357-4-15 6 Pin-Hi Lok NSA5359-4-15 6 Pin-Hi Lok NSA5351-5-15 6 Pin-Hi Lok NSA5357-5-15 6 Pin-Hi Lok NSA5357-4-19 6 Pin-Hi Lok NSA5359-4-19 6 Pin NSA5351-5-19 6 Pin-Hi Lok NSA5357-5-19 2 Pin-Hi Lok NSA5357-4-13 2 Pin-Hi Lok NSA5359-4-13 2 Pin-Hi Lok NSA5351-5-13

24

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved NOTE: Use washer NSA5368 only if the fasteners are too long. (f) Kit 530350A06R00 and Kit 530350A08R00 1 Replace splice, LH side, by Repair Instruction R53810422 , SOL.A. 2 Pin-Hi Lok NSA5357-5-13 8 Pin-Hi Lok NSA5359-5-11 8 Pin NSA5351-6-11 2 Pin-Threaded NSA5359-4-11 2 Pin NSA5351-5-11 2 Pin-Hi Lok NSA5357-5-11 6 Pin-Threaded NSA5359-4-18 6 Pin NSA5351-5-18 6 Pin-Hi Lok NSA5357-5-18 2 Pin-Hi Lok NSA5357-5-14 2 Pin-Hi Lok NSA5359-5-14 2 Pin-Hi Lok NSA5351-6-14 2 Pin-Hi Lok NSA5359-5-13 2 Pin NSA5351-6-13 6 Pin-Hi Lok NSA5351-5-14 6 Pin-Hi lok NSA5359-4-14 30 Nut NSA5050-4 30 Nut NSA5050-5 30 Nut NSA5050-6 30 Washer NSA5368PD416A 30 Washer NSA5368PD516A 30 Washer NSA5368PD616A

1 Splice A5381263520096 1 Pin-Hi Lok NSA5357-4-12 1 Pin-Hi Lok NSA5357-4-13 3 Pin-Hi Lok NSA5357-4-15 3 Pin-Hi Lok NSA5357-4-19 1 Pin-Hi Lok NSA5359-4-12 1 Pin-Hi Lok NSA5359-4-13 3 Pin-Hi Lok NSA5359-4-15 3 Pin-Hi Lok NSA5359-4-19 1 Pin NSA5351-5-11 5 Pin-Hi Lok NSA5351-5-12 1 Pin-Hi Lok NSA5351-5-13 4 Pin-Hi Lok NSA5351-5-14 3 Pin NSA5351-5-18 7 Pin-Hi Lok NSA5357-3-10 9 Pin-Hi lok NSA5357-3-12 2 Pin-Hi Lok NSA5357-3-14 6 Pin-Hi-Lok NSA5351-4-11 8 Pin-Hi Lok NSA5351-4-12 12 Pin-Hi Lok NSA5351-4-13

2 Pin-Hi Lok NSA5351-4-14

25

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (g) Kit 530350A07R00 and Kit 530350A08R00 1 Replace splice, RH side, by Repair Instruction R53810422 , SOL.A.

NOTE: For the hardware use the Kit 530350A08R00 . (h) Kit 530350A06R00 and Kit 530350A09R00 1 Replace splice, LH side, by Repair Instruction R53810422 , SOL.B. 1 Pin-Hi Lok NSA5357-4-13 1 Pin-Hi Lok NSA5357-4-10 3 Pin-Hi Lok NSA5357-4-12 6 Pin-Hi lok NSA5357-3-12 1 Pin-Hi Lok NSA5357-4-15 1 Pin-Hi Lok NSA5357-4-16 5 Pin-Hi Lok NSA5351-4-15 1 Pin-Hi Lok NSA5351-4-16 18 Nuts NSA5050-3 42 Nut NSA5050-4 14 Nut NSA5050-5 18 Nut NAS1726-3E 42 Nut NAS1726-4E 14 Nut NAS1726-5E

8 Nut NAS1727-4E 1 Pin-Hi Lok NSA5359-4-15

1 Splice A5381263520196

1 splice A5381263520096 7 Pin-Hi Lok NSA5357-4-11 9 Pin-Hi Lok NSA5357-4-12 5 Pin-Hi Lok NSA5357-4-14 3 Pin-Threaded NSA5357-4-18 4 Pin-Hi Lok NSA5357-5-11 1 Pin-Hi Lok NSA5357-5-12 1 Pin-Hi Lok NSA5357-5-13 4 Pin-Hi Lok NSA5359-5-11 1 Pin-Hi Lok NSA5359-5-12 1 Pin-Hi Lok NSA5359-5-13 2 Pin-Hi Lok NSA5359-5-14 4 Pin NSA5351-6-11 1 Pin NSA5351-6-12 1 Pin NSA5351-6-13 2 Pin-Hi Lok NSA5351-6-14 7 Pin-Hi Lok NSA5359-3-10 9 Pin,Threaded NSA5359-3-12 2 Pin,Threaded NSA5359-3-14 12 Pin-Hi Lok NSA5357-4-13

5 Pin-Hi Lok NSA5357-4-15

26

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (i) Kit 530350A07R00 and Kit 530350A09R00 1 Replace splice, RH side, by Repair Instruction R53810422 , SOL.B.

NOTE: For the hardware use the Kit 530350A09R00 . (j) Kit 530350A10R00 1 Fasteners for the adjacent holes.

D. TEST None E. CLOSE UP (1) Config. 01 thru Config. 02 (a) Install heat and sound insulation blankets (Refer to AMM 25-22-11 Page block 401).

1 Pin-Hi Lok NSA5357-4-16 1 Pin-Hi Lok NSA5357-4-13 1 Pin-Hi Lok NSA5357-4-10 3 Pin-Hi Lok NSA5357-4-12 6 Pin-Hi lok NSA5357-3-12 2 Pin-Hi Lok NSA5359-4-15 1 Pin-Hi Lok NSA5357-4-15 1 Pin-Hi Lok NSA5357-4-16 42 Nut NAS1726-4E

6 Nut NAS1726-5E 8 Nut NAS1726-6E 18 Nut NAS1727-3E

8 Nut NAS1727-5E 18 Nuts NSA5050-3 42 Nut NSA5050-4 14 Nut NSA5050-5

1 splice A5381263520196

1 Pin-Hi lok NSA5351-3-10 1 Pin-Hi lok NSA5351-3-12 9 Pin-Hi lok NSA5351-3-13 1 Pin-Hi lok NSA5351-3-16 12 Nuts NSA5050-3

5 Pin-Hi Lok NSA5351-4-13 4 Pin-Hi Lok NSA5351-4-15 1 Pin-Hi Lok NSA5351-4-16 10 Nut NSA5050-4

1 Pin-Hi Lok NSA5357-3-10 1 Pin-Hi lok NSA5357-3-12 2 Nuts NSA5330-6

27

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved (b) Install lower sidewall panels (Refer to AMM 25-23-31 Page block 401). (c) Install row of passenger seats (Refer to AMM 25-21-00 Page block 401). (d) Remove the access platforms. (e) Restore the systems and the aircraft to normal operating condition. F. DOCUMENTATION Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

28

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 1 Config. 01 thru 02 : Threshold and Interval of Inspection

29

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 2 Sheet 1 Config. 01 thru 02 : Identification Splice

30

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 2 Sheet 2 Config. 01 thru 02 : Identification Splice

31

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 3 Sheet 1 Config. 01 thru 02 : Location of Fastener Holes to be Inspected

32

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 3 Sheet 2 Config. 01 thru 02 : Location of Fastener Holes to be Inspected

33

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 4 Sheet 1 Config. 01 thru 02 : Flow Chart

34

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 4 Sheet 2 Config. 01 thru 02 : Flow Chart

35

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 5 Sheet 1 Config. 01 thru 02 : Replacement of Fasteners

36

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 6 Sheet 1 Config. 01 thru 02 : Install new Fasteners, KIT A01

37

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 7 Sheet 1 Config. 01 thru 02 : Install new Fasteners, KIT A02

38

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 8 Sheet 1 Config. 01 thru 02 : Install new Fasteners, KIT A03

39

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 9 Sheet 1 Config. 01 thru 02 : Install new Fasteners, KIT A04

40

# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 10 Sheet 1 Config. 01 thru 02 : Install new Fasteners, KIT A05

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 10 Sheet 2 Config. 01 thru 02 : Install new Fasteners, KIT A05

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 10 Sheet 3 Config. 01 thru 02 : Install new Fasteners, KIT A05

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# @ A300 SERVICE BULLETIN

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 11 Sheet 1 Config. 01 thru 02 : Hole Tolerances in case the Splice is not replaced.

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# @ A300 SERVICE BULLETIN APPENDIX 01

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : 1 of 5 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 DEPT. SEE81 AND AI/SM-K, ON THE ATTACHED INSPECTION REPORT SHEET.

# @ A300 SERVICE BULLETIN APPENDIX 01

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 1 Config. 01 thru 02 : Inspection Report

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# @ A300 SERVICE BULLETIN APPENDIX 01

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 2 Config. 01 thru 02 : Inspection Report

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# @ A300 SERVICE BULLETIN APPENDIX 01

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 3 Config. 01 thru 02 : Inspection Report

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# @ A300 SERVICE BULLETIN APPENDIX 01

DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : Printed in FRANCE © AIRBUS, 2007 All rights reserved Figure 1 Sheet 4 Config. 01 thru 02 : Inspection Report

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# @ A300 SERVICE BULLETIN REPORTING SHEET

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 Page : 1 of 1 Printed in FRANCE © AIRBUS, 2007 All rights reserved TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES. 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:..........................

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........................................ B - SB HAS BEEN embodied on aircraft:.....................

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........................................ Operator comments:..............................

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....................................... 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

5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300—53—0350 REVISION No. : 03 — Jul 26/07 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.