5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 53

TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAM

FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES.

MODIFICATION No. : NONE

This page transmits Revision No. 03 of Service Bulletin No. A300-

ADDITIONAL WORK

No additional work is required by this revision for aircraft m

previous issue.

REASON

Revision No. 03 issued to update the effectivity, to update th

Kit A05, A08, A09 and A10, to add the reference of the existi

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 del

MSN 0177 deleted for operator AIC. Operator BAE, aircraft 

deleted. Operator CAL, aircraft 0193, 0197, 0221, 0232 del

MSN 0023 deleted for operator C2A. Operator E4G, aircraft 

deleted. Operator F2I, aircraft MSN 0033, 0145 deleted. A

0131 deleted for operator HLA. Aircraft MSN 0262 deleted 

IAC. Aircraft MSN 0110, 0169, 0174, 0178, 0194 deleted for 

Operator LFA, aircraft MSN 0066 deleted. Operator NTL, ai
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

. Para. 1.E. Sentence updated.

— APPROVAL

. Para. 1.F. Sentence updated.

— REFERENCES

. Para. 1.J. Reference of the ESPM 20-55-00 added. Referenc

24-40-00 becomes 24-00-00.

MATERIAL INFORMATION :

— MATERIAL - PRICE AND AVAILABILITY

. Para. 2.A. Address updated. Price updated for Kit A05, A0

— 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 ad

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.

2
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

Revision No. 01 issued to inform the operators that Service B

A300-53-0350 replaces the All Operator Telex (AOT) A300-53A03

The All Operator Telex (AOT) requires the inspection of one h

Service Bulletin requires the inspection of the 14 holes.

Revision No.02 is issued to inform the operators of the SB upd

the validation of the equivalent A300-600 Service Bulletin on 

Service Bulletin becomes mandatory and The Airworthiness Dire

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

3
5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved

This summary is for information only

and is not approved for modification of the aircraf

MANDATORY MANDATORY MAND

ATA SYSTEM : 53

TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAM

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 A30

(A300-600), modification No. 05890S6739, specifies cold working o

holes in the splice fitting at FR47.

The Service Bulletin No. A300-53-0199 currently terminates the in

requirements of Service Bulletin No. A300-53-0200. Cracks have be

post Service Bulletin No. A300-53-0199 aircraft in the fastener h

attach the splice fitting to FR47 (ref. A300 SRM 53-15-00 Fig. 11

A300-600 SRM 57-10-24 Fig. 8 item 125A).

A laboratory investigation has been performed on a cracked splice 

the analysis of the crack growth rate shows that an inspection pr

required for post Service Bulletin No. A300-53-0199 B4/C4/F4 airc

Due to the structural similarity, the inspection is also required 

aircraft.

AOT A300-53A350 and A300-600-53A6123 were issued to call for a on

inspection of the splice fitting between stringers 24 and 26, LH 

This Service Bulletin has been created to define a new inspection 

the pre-mod. and post-mod. 05890S6739 aircraft (FUSELAGE - FRAME 

LATERAL SECTION BY STRENTHENED FISH PLATE) and supersede previous 

Service Bulletin A300-53-0200.

This Service Bulletin recommends an HFEC rotating probe inspectio

removals of the splice fitting between stringers 24 and 26 and sub

in case of findings.

Accomplishment of this Service Bulletin permits early detection o

the splice fitting to avoid cracking in the FR47 which would requ

repairs.
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

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 NT

TDX TNO TSY

NOTE : This Inspection Service Bulletin is applicable on all A/C m

F4 pre or post Mod. 05890S6739, with or without Service Bu

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

AD Yes A/C OPERATION AFFECT

RELIABILITY AFFECTED No PAX COMFORT AFFECTED 

COST SAVING No ETOPS AFFECTED 

STRUCTURAL LIFE EXTN No VENDOR SB INVOLVED 

KIT PRICE (USD) See SB . 

2
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

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

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 

ELAPSED TIME (HOURS) 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

3
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

4
5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved

MANDATORY MANDATORY MAND

ATA SYSTEM : 53

TITLE : FUSELAGE - CENTER SECTION - INSPECTION HOLES FUSELAGE FRAM

FITTING BETWEEN STRINGERS 24 AND 26 LH AND RH SIDES.

MODIFICATION No. : NONE

This document contains AIRBUS PROPRIETARY INFORMATION and shall a

remain the property of AIRBUS; no intellectual property right or 

granted by AIRBUS in connection with any information contained in 

delivered on the express condition that said document and the inf

contained in it shall be treated as confidential, shall not be us

purpose other than that for which it is hereby delivered. It shal

disclosed in whole or in part to third parties and shall not be d

any manner (except for the purposes of performing the tasks descr

and provided that any recipient of such document shall comply wit

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 

0019 0023 0033 0035 0041 0042 0044-0047 0053 00

0066 0069 0073-0075 0078 0079 0083-0087 0091 009

0098-0101 0105-0107 0110 0114 0116 0117 0121 01

0133-0142 0144-0152 0154-0158 0161 0169 0170 01

0178 0180-0184 0189 0190 0192-0197 0199 0200 020

0208 0210-0212 0216 0218-0222 0227 0232 0234-02

0243 0247 0249 0250 0255 0256 0259 0261 0262 02

0274 0277 0289 0292 0299 0302 0304 0305

NOTE : This Inspection Service Bulletin is appli

A/C model B4, C4, F4 pre or post Mod. 058
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

from transfer of an aircraft from one operator t

not be reflected in this list unless the Service 

revised for another reason.

(c) Effectivity by MSN and Kit/Configuration

The kits and configurations applicable to these 

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 0

0236 0250 0259 0274 0289

BLM 0239

DHL 0084 0085 0141 0149 0249 0265

F2I 0079 0093 0094 0128 0133 0135 0136 0

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 0

MSR 0200 0255

NTR 0124 0155 0210 0227 0247 0261

OHY 0138 0192

RUN 0075 0083 0105 0107 0121 0147 0154 0

TCN 0125

TDX 0053 0100 0207 0211 0216 0271

TNO 0045 0074 0078

TSY 0129

2
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

The kits and configurations applicable to these 

at the end of this list:

0019 0045 0047 0053 0073-0075 0078 0083-0085 009

0100-0101 0107 0116-0117 0121 0123 0125-0126 01

0137-0139 0141 0147 0149-0150 0152 0154-0155 01

0180-0183 0190 0192 0196 0199-0200 0203-0204 020

0210-0212 0216 0218-0220 0222 0227 0234-0236 024

0249-0250 0255-0256 0259 0261 0265 0271 0274 02

0299 0302 0304

NOTE : Config. 01 concerns all A/C model B4-100 

0035-0256).

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

3
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

NOTE : Kit 530350A02R00 : In case of no crack f

holes A to N. Valid A/C having new splice

A53812635200/201 (installed by Service Bu

No.A300-53-0199 or Modification No.05890S

NOTE : Kit 530350A03R00 : In case of no crack f

holes A to N. Valid A/C having new splice

A53812635200/201 (replaced by Repair Inst

R53810422 SOL. A).

NOTE : Kit 530350A04R00 : In case of no crack f

holes A to N. Valid A/C having new splice

A53812635200/201 (replaced by Repair Inst

R53810422 SOL. B).

NOTE : Kit 530350A05R01 : In case of crack find

or equal to 0.8 mm (0.315in.) at holes A 

— Valid A/C having basic splice

A53834139200/201/202/203.

— Valid A/C having new splice A5381263520

(installed by Service Bulletin No. 53-0

Modification No. 05890S6739 or Repair I

R53810422 SOL. A).

— Valid A/C having new splice A5381263520

(replaced by Repair Instruction R538104

NOTE : Kit 530350A06R00 : In case of crack find

0.8 mm (0.315 in.) at holes A to N. Repla

LH side.

NOTE : Kit 530350A07R00 : In case of crack find

0.8 mm (0.315 in.) at holes A to N. Repla

RH side.

NOTE : Kit 530350A08R00 : In case of crack find

0.8 mm (0.315 in.) at holes A to N. Bolt

replacement splice with Repair Instructio

SOL. A.

NOTE : Kit 530350A09R00 : In case of crack find

0.8 mm (0.315 in.) at holes A to N. Bolt

replacement splice with Repair Instructio

SOL. B.

4
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

None

C. REASON

(1) History

Service Bulletin No. A300-53-0199 and Service Bulleti

(A300-600), modification No. 05890S6739, specifies co

fastener holes in the splice fitting at FR47.

The Service Bulletin No. A300-53-0199 currently term

inspection requirements of Service Bulletin No. A300

Cracks have been found on post Service Bulletin No. A

aircraft in the fastener holes which attach the spli

FR47 (ref. A300 SRM 53-15-00 Fig. 112 item 39 and A30

57-10-24 Fig. 8 item 125A).

A laboratory investigation has been performed on a c

fitting, and the analysis of the crack growth rate s

inspection program is required for post Service Bull

A300-53-0199 B4/C4/F4 aircraft.

Due to the structural similarity, the inspection is a

on A300-600 aircraft.

AOT A300-53A350 and A300-600 53A6123 were issued to 

one-time inspection of the splice fitting between st

26, LH and RH sides.

This Service Bulletin has been created to define a n

program for the pre-mod. and post-mod. 05890S6739 ai

(FUSELAGE - FRAME 47 - REINFORCE LATERAL SECTION BY 

FISH PLATE) and supersede previous inspection Servic

A300-53-0200.

The equivalent of this Service Bulletin has been val

A300-600 aircraft MSN 0635.

(2) Objective/Action

This Service Bulletin recommends an HFEC rotating pro

after bolt removals of the splice fitting between st

26 and subsequent action in case of findings.

5
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

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, 

(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 a

given in the Figure 1, Sheet 1.

Grace period for A/C model A300B4 post Mod. No. 05890

For aircraft above 20000 FC : Next C-check but not ex

/ 1500 FH, from reception date of the Revision No. 0

For other aircraft : Next C-check but not exceeding 

FH.

Accomplishment of this Service Bulletin has been rend

by the issue of an Airworthiness Directive (AD) publ

European Aviation Safety Agency (EASA). The AD must 

reference document for the mandatory accomplishment t

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 

6
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

The manpower estimates given in this Service Bulletin are 

direct labor cost to do the work. These estimates assume 

will be done by experienced personnel, and may need to be 

upwards to suit operator's circumstances. The estimates do 

the time to prepare, plan or inspect the work. Manufactur

procurement of parts and tools, drying times for paints, 

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 a

Config. 01 thru Config. 02

REPAIR

Kit 530350A05R01 and Kit 530350A10R00

Config. 01 thru Config. 02

Kit 530350A06R00 with Kit 530350A08R00 or Kit 530350A09

Replace splice LH side

Gain access 

Remove fasteners A to N 

Inspect holes A to N 

Install new fasteners 

Close-up 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Eliminate crack 

inspect adjacent holes 

Install new fasteners 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

7
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 530350A09

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)

ELAPSED TIME (HOURS) 

Remove splice 

Install new splice 

Do cold expansion 

Install fasteners A to N 

TOTAL MANHOURS 

ELAPSED TIME (HOURS) 

Aircraft Maintenance Manual (AMM) : 20-21-12 24-00-00 

25-22-11 25-23-31 

Elec. Std. Practices Manual (ESPM) : 20-55-00

8
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

Not applicable

9
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

This Page Intentionally Left Blank

10
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

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://spa

For ordering by fax : +49 40 50 76 2

(2) Price and Availability

Kit 530350A01R00

Cost : 2,404.00 US Dollars

Availability : 150 calendar days from receipt of orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

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 orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

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 orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

so that we can try to comply with your requirements.

Kit 530350A04R00

11
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

Kit 530350A05R01

Cost : 9,170.00 US Dollars

Availability : 150 calendar days from receipt of orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

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 orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

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 orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

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 orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

so that we can try to comply with your requirements.

Kit 530350A09R00

12
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

Kit 530350A10R00

Cost : 4,660.00 US Dollars

Availability : 150 calendar days from receipt of orde

The Kit availability given above is the standard lead 

date of your purchase order. If you require the Kit(

time, please include a retrofit planning schedule wit

so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimat

to economic conditions at the issue date of the Serv

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishme

Service Bulletin.

C. LIST OF COMPONENTS

Kit 530350A01R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you f

numbers of hardware components in the related kit(

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

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

13
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 f

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

Kit 530350A03R00

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. 

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 f

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

Kit 530350A04R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you f

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

NSA5368PD416A 30 Washer

NSA5368PD516A 30 Washer

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

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

15
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

Kit 530350A07R00

Kit 530350A08R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

A5381263520096 1 Splice

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

A5381263520196 1 Splice

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 f

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

Kit 530350A09R00

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

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

18
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

Kit 530350A10R00

NOTE : Refer to the AIRBUS Standards Manual (SM) if you f

numbers of hardware components in the related kit(

cannot identify in the LIST OF COMPONENTS of this 

Bulletin. The SM will give you the correct part num

number relationship.

D. LIST OF MATERIALS — OPERATOR SUPPLIED

(1) Consumable Materials

ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. 

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 

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

19
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

F. TOOLING — PRICE AND AVAILABILITY

(1) To accomplish this Service Bulletin it is necessary t

following tools and equipment listed in Nondestructiv

Manual (NTM) 51-30-10 Part 1 and Nondestructive Test

(NTM) 51-31-04 Part 1.

(2) Fatigue Technology Incorporated (FTI) has allocated t

FTI-A300-53-0350-1 for accomplishment of this Servic

Operators interested in obtaining the FTI tool kit s

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY 

MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENAN

REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICA

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIB

:

— PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOT

AS NECESSARY ON WIRING AND COMPONENTS.

— REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CO

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLAT

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-0

(1) Preparation

(a) Config. 01 thru Config. 02

1 Electrically ground the aircraft (Refer to AM

Page block 301).

2 Put the access platforms in position.

3 Remove row of passenger seats at FR47 on LH a

(Refer to AMM 25-21-00 Page block 401).

4 Remove lower sidewall panels at FR47 on LH a

(Refer to AMM 25-23-31 Page block 401).

5 Remove heat and sound insulation blankets at 

RH sides (Refer to AMM 25-22-11 Page block 40

(2) Standard Practices

(a) For inspection

1 For the specification of the material number

refer to the CML.

2 Clean surfaces to be sealed with Solvant Gene

(Mat No. 11-026) .

21
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

1 Renew protective finish (Refer to AMM 51-12-0

Primer (Mat No. 16-020) , Anti-Corrosion Prim

(Polyurethane) (Mat No. 16-001) and Polyuret

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 , she

(b) Do a rotating probe inspection,NTM 51-30-10 Part 

51-31-04 Part 1 , refer to figure 4 , sheets 1 

(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 6 and figure 11 .

NOTE: Use washer NSA5368 only if the fastene

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

NOTE: Use washer NSA5368 only if the fastene

long.

(c) Kit 530350A03R00

1 Install new fasteners of same diameter, refer 

figure 8 and figure 11 .

NOTE: Use washer NSA5368 only if the fastene

long.

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

NOTE: Use washer NSA5368 only if the fastene

long.

(e) Kit 530350A05R01

1 Install new fasteners, refer to figure 5 , f

sheets 1 to 3 and figure 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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

NOTE: Use washer NSA5368 only if the fastene

long.

(f) Kit 530350A06R00 and Kit 530350A08R00

1 Replace splice, LH side, by Repair Instructio

SOL.A.

6 Pin NSA5351518

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 Instructio

SOL.A.

NOTE: For the hardware use the Kit 530350A08

(h) Kit 530350A06R00 and Kit 530350A09R00

1 Replace splice, LH side, by Repair Instructio

SOL.B.

1 PinHi Lok NSA5351416

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 Instructio

SOL.B.

NOTE: For the hardware use the Kit 530350A09

(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 (Refe

25-22-11 Page block 401).

1 PinHi Lok NSA5357416

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page :

Printed in FRANCE © AIRBUS, 2007 All rights reserved

(e) Restore the systems and the aircraft to normal o

condition.

F. DOCUMENTATION

Write in the applicable aircraft records that you have don

given in the Service Bulletin.

28
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 Inspect

29
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 Ins

32
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 Ins

33
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

41
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

42
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

43
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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 no

44
5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

2
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

3
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

4
DATE : Oct 25/99 SERVICE BULLETIN No. : A300

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

5
5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved

A - SB WILL BE embodied............. YES/NO (if NO p

If YES, aircraft concerned (as per SB effectivity by default) and 

(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 th

information is needed prior to next normal revision or prior to S

please indicate required service:

Either: Modification Operational Impact (MOI), if available. . YE

Or : Intermediate revision. ................ YE

Important Information: This SB will only be incorporated in your m

operational documentation if this sheet is returned to Airbus and 

duly authorised representative. With the next feasible revision, 

result in

- updating of maintenance documentation to show pre and post S

- updating of maintenance and operational documentation to show 

after embodiment.

If this SB requires previous or simultaneous accomplishment of ot

Airbus shall automatically include them in the manual revisions. 

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.
5 DATE : Oct 25/99 SERVICE BULLETIN No. : A300

REVISION No. : 03 — Jul 26/07 Page : 1 of 

Printed in FRANCE © AIRBUS, 2007 All rights reserved

(Please rate on a scale of 1 to 4, with 4 being the 

- Quality rating of this SB 

- Quality rating of the Accomplishment Instructions 

- Quality rating of the Illustrations 

- Is this SB easy to understand ? 

If you have had difficulties in the accomplishment of this SB plea

the area(s) and give a short description of the issue.

Planning Material Instruct

X Effectivity X Kit content X Preparat

X Reason X List of Materials X Mod/Insp

X Manpower Operator Supplied X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustra

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.