A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 57

TITLE : WINGS - INSPECTION OF THE OUTER SHROUD BOX HINGE BRACKETS

MODIFICATION No. : NONE

This page transmits revision No. 04 of Service BuLletin A300-57-0142.

ADDITIONAL WORK

No additional work is required by this revision for aircraft inspected by any

previous revision.

REASON

This Service BuLLetin has been issued to inform Operators that Flight Hours (FH)

conversion figures have been added to the AccompLishment TimescaLe. In addition, a

maximum crack length has been incLuded.

CHANGES

SUMMARY:

. AIRBUS address has been amended.

- REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

• Text has been amended.

- EFFECTIVITY

• Effectivity has been updated.

- REFERENCES/REPERCUSSIONS

. TFU has been amended.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 1

Printed in France
A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

SERVICE BULLETIN:

• AIRBUS address has been amended.

• Copyright statement has been moved below TITLE.

PLANNING INFORMATION

EFFECTIVITY

. Para. (1) Aircraft models have been updated.

. Para. (2)(a) Effectivity has been updated.

. Para. (2)(b) Effectivity has been updated.

Para. (2)(c) Effectivity by MSN and kit/configuration has been

added.

- REASON

- Para B. (5) AccompLishment TimescaLe

Text has been amended and TabLe has been added to show the inspection

thresholds and intervals with FH conversion figures.

- APPROVAL

Approval statement has been amended.

- MATERIAL - COST AND AVAILABILITY

. AIRBUS address has been amended.

- REFERENCES

. AD has been removed.

- ACCOMPLISHMENT INSTRUCTIONS

- INSPECTION

. Para. (4) Text has been amended.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 2

Printed in France
. A300

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- CLOSE-UP

Para. (6) Airbus Industrie has been changed to Airbus.

ACCEPTANCE/REJECTION SHEET:

. AIRBUS address has been amended.

FILING INSTRUCTIONS

1. Remove and destroy pages 1 and 2 of the Summary, pages 1, 2, 3, 4, 5, 6, 7, 8,

9, 10 and 11 of this Service BuLLetin and page 1 of the Acceptance/Rejection

sheet.

2. Insert pages 1, 2, 3 and 4 of the Summary, pages 1, 2, 3, 4, 5, 6, 7, 8, 9, 10,

11, 12 and 13/14 of this Service BuLLetin and page 1 of the Acceptance/Rejection

sheet.

Put this Revision TransmittaL Sheet in front of the Service BuLLetin.

HISTORY OF PREVIOUS REVISIONS

This is only appLicabLe for Revision 04 and subsequent. If information is required

for revisions issued previous to this, pLease check your copies of Revision

TransmittaL Sheet or contact AIRBUS.

REVISION SEQUENCE

ORIGINAL : Dec 17/86

REVISION No. : 01 - Apr 09/90

REVISION No. : 02 - Jan 16/91

REVISION No. : 03 - Feb 22/99

REVISION No. : 04 - Mar 30/11

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 3/4

Printed in France
A300

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice BELLONTE

31707 BLAGNAC CEDEX FRANCE

Tel : (33) 5 61 93 33 33

TeLex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only

and is not approved for modification of the aircraft

MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 57

TITLE : WINGS — INSPECTION OF THE OUTER SHROUD BOX HINGE BRACKETS

MODIFICATION No. : NONE

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

An ALL Operator TeLex (AOT) 57/86/01 has been issued to aLL A300 Operators

requesting inspection of the aft hinge brackets of the outer shroud box. This

inspection revealed that approximately half of aLL the brackets inspected were

cracked.

This Inspection Service BuLLetin introduces a visuaL inspection of the forward and

aft outer shroud box hinge brackets for cracks or complete fracture of the bracket.

AccompLishment of this Service BulLetin wiLL Lead to the early detection of the

cracks in the shroud box hinge brackets and wiLL prevent the fracture of the

brackets. Fracture of a bracket wouLd allow vertical movement of the inner shroud

box structure in the immediate area which could resuLt in damage to the top skin of

the inboard flap. Additionally, the Loads carried through the brackets will be

transferred to the remaining supports which may also crack and cause extensive

structural damage.

A detailed visuaL inspection is necessary of the shroud box hinge brackets. The

inspection thresholds and repeat inspection intervaLs are given in this Service

BuLLetin. In addition, a maximum crack Length is incLuded.

This Service BuLLetin has been classified Mandatory by the issue of an

Airworthiness Directive (AD) published by the European Aviation Safety Agency

(EASA). The AD must be used as the reference document for the mandated

accomplishment timescaLe.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I REVISION No. : 04 Mar 30/11 PAGE : 1

Printed in France
A300

SERVICE BULLETIN

SUMMARY

EFFECTIVITY

This Service BuLLetin is appLicabLe to these operators:

30V, 50W, 69X, A2S, AFG, BCS, DHL, F21, FLM, IAC, IAW, IRA, IRB, IRM, KZU, MIX,

MNB, MSR, NTR, OHY, RUN, SOP, TDX, TNO, TSY

SERVICE BULLETIN TO BE ACCOMPLISHED PREVIOUSLY OR SIMULTANEOUSLY

None

REFERENCES/REPERCUSSIONS

TFU : 572200001

OEB : None

AOT : 57/86/01

SIL : None

LIFE LIMIT : None

LINE MAINTENANCE AFFECTED : No

OTHER : None

NATURE OF WORK

AIRCRAFT Yes

EQUIPMENT No

HARD : No

SOFT : No

OBRM : No

COMPLIANCE

Mandatory

MANPOWER

Manhours

TOTAL MANHOURS 8.0

ELAPSED TIME (HOURS) 4.0

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 2

Printed in France
^A300

SERVICE BULLETIN

SUMMARY

MATERIAL INFORMATION

AIRCRAFT DATA

None

EQUIPMENT DATA

None

APPENDICES

None

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I REVISION No. : 04 Mar 30/11 PAGE : 3

Printed in France
S A300

SERVICE BULLETIN

SUMMARY

JOINT LINE USUAL STARTING POINT

I OF CRACKS

CRACK IN VERTICAL

WEB RADIUS

CRACK IN VERTICAL FLANGE

UNDER BEARING ASSY. NUT

EXAMPLE 'A'

EXAMPLE 'B'

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. . 04 - Mar 30/11 PAGE : 4

Printed in France
A3 0 0

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice BeLLonte

31707 BLAGNAC CEDEX FRANCE

TeL : (33) 5 61 93 33 33

TeLex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM : 57

TITLE : WINGS - INSPECTION OF THE OUTER SHROUD BOX HINGE BRACKETS

MODIFICATION No. : NONE

This document contains AIRBUS PROPRIETARY INFORMATION and shaLL at aLL times remain

the property of AIRBUS; no inteLLectual property right or License is granted by

AIRBUS in connection with any information contained in it. It is deLivered on the

express condition that said document and the information contained in it shaLL be

treated as confidential, shaLL not be used for any purpose other than that for which

it is hereby deLivered. It shall not be discLosed in whole or in part to third

parties and shall not be duplicated in any manner (except for the purposes of

performing the tasks described hereunder and provided that any recipient of such

document shall comply with the conditions herein), without AIRBUS prior written

consent.

1. PLANNING INFORMATION

A.

EFFECTIVITY

(1) ModeLs

B2-1C, B2.203, B2K-3C, B4-103, B4-120, 64-203, B4-2C, C4-203,

F4-203

(2) Aircraft

(a) Effectivity by MSN

The Service Bulletin is appLicabLe to aircraft MSN:

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 1

Printed in France
5A300

SERVICE BULLETIN

0003 0019 0041 0044 0045 0047 0053 0055 0063 0073 0074 0075 0078

0079 0080 0082 0083 0084 0085 0090 0093 0094 0095 0100 0101 0105

0107 0116 0117 0121 0123 0124 0125 0126 0128 0129 0133 0134 0135

0136 0137 0138 0139 0141 0147 0148 0149 0150 0151 0152 0154 0155

0156 0157 0160 0170 0173 0175 0176 0180 0181 0182 0183 0184 0185

0187 0189 0190 0192 0196 0199 0200 0203 0204 0207 0208 0210 0211

0212 0216 0218 0219 0220 0226 0227 0234 0235 0236 0239 0240 0243

0244 0247 0249 0250 0255 0256 0259 0261 0265 0271 0274 0277 0289

0292 0299 0302 0304

(b) 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 further changes resuLting from transfer

of an aircraft one Operator to another will not be reflected in

this List unless the Service Bulletin is revised for another

reason.

OPERATOR MSN

30V 0083

50W 0003

69X 0073

A2S 0063

AFG 0180 0190

BCS 0095 0116 0148 0150 0152 0184 0189

0199 0208 0219 0220 0234 0235 0236

0250 0259 0274 0289

DHL 0084 0085 0141 0149 0249 0265

F21 0079 0093 0094 0128 0133 0135 0136

0137 0156 0170 0243

FLM 0082 0151 0176 0256

IAC 0181 0182 0240

IAW 0239

IRA 0080 0139 0173 0185 0187 0226

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 2

Printed in France
A300

SERVICE BULLETIN

OPERATOR MSN

IRB 0299 0302

IRM 0055 0090 0160 0175 0204 0244

KZU 0041 0044 0101 0117

MIX 0125 0134 0157 0196 0203 0218

MNB 0019 0047 0123 0212 0277 0292 0304

MSR 0200 0255

NTR 0124 0155 0210 0227 0247 0261

OHY 0138 0192

RUN 0075 0105 0107 0121 0147 0154 0183

SOP 0126

TDX 0053 0100 0207 0211 0216 0271

TNO 0045 0074 0078

TSY 0129

Cc) Effectivity by MSN and Kit/Configuration

None

(3) SPARES

None

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 64 Mar 30/11 PAGE : 3

Printed in France
1A300

SERVICE BULLETIN

B.REASON

(1) History

An ALL Operator Telex (AOT) 57/86/01 has been issued to aLL A300

Operators requesting inspection of the aft hinge brackets of the outer

shroud box. This inspection revealed that approximately half of aLL the

brackets inspected were cracked or compLeteLy fractured. Fracture of the

bracket would aLLow vertical movement of the inner shroud box structure

in the immediate area which couLd result in damage to the top skin of the

inboard flap. Additionally, the Loads carried through the brackets will

be transferred to the remaining supports which may also crack and cause

extensive structural damage.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

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REVISION No. : 04 Mar 30/11 PAGE : 4

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S A3 00

SERVICE BULLETIN

There is also some evidence of un- reported fractures of the forward hinge

bracket of the outer shroud box.

Modification No. 06661H1033 (Service Bulletin A300-57-0143) has been

introduced which repLaces the aLuminum aLLoy aft bracket with a steeL

bracket.

(2) Objective/Action

To do a mandatory detailed visuaL inspection of the LH and RH outer shroud

box hinge brackets to detect any cracks or the complete fracture of the

brackets.

(3) Advantages

Accomplishment of this Service BuLLetin wiLL Lead to the early detection

of the cracks in the shroud box hinge brackets and wiLL prevent the

fracture of the brackets.

(4) Operational/Maintenance Consequences

None

(5) AccompLishment Timescale

This Service BuLLetin has been classified Mandatory by the issue of an

Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). The AD must be used as the reference document for the

mandated accomplishment timescaLe.

A detailed visuaL inspection and repeat inspections are to be done on the

forward and aft hinge brackets of the outer shroud-box. For aircraft

already within the inspection program, the next inspection must be

compLeted within the next interval period. However, where the FH Limit

only has been exceeded the inspection may be extended to the previousLy

planned FC inspection.

The inspection thresholds and repeat inspection intervals are detaiLed in

TabLe 1.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57.0142

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REVISION No. : 04 Mar 30/11 PAGE : 5

Printed in France
A300

SERVICE BULLETIN

TabLe 1

REPEAT REPEAT

THRESHOLD INTERVAL (IF

MODIFICATION INSPECTION INSPECTION INTERVAL

CRACK IS AIRCRAFT (IF CRACKS STANDARD METHOD BEFORE FOUND IN ONE ARE NOT

EMBODIMENT HALF FOUND) BRACKET)

FC FH FC FH FC FH

A300B2 Pre-Mod. 06661 DVI 5,000 5,400 1,000 1,000 50** 50**

Post Mod. 06661* N/A N/A N/A N/A N/A N/A N/A

A300B4-100 Pre-Mod. 06661 DVI 5,000 6,600 1,000 1,300 50** 65**

Post Mod. 06661* N/A N/A N/A N/A N/A N/A N/A

A300 B4-200 Pre-Mod. 06661 DVI 5,000 10,400 1,000 2,000 50** 100**

C4-200

F4-200

Post Mod. 06661* N/A N/A N/A N/A N/A N/A N/A

NOTE: (*) : If Modification 06661H1033 (Service Bulletin A300.57.0143) is embodied

then no further inspections are necessary.

NOTE: (**) : If a crack is found in one haLf bracket, repeat intervals can only be

carried out for crack Lengths Less than 8mm.

For aircraft subject to short-range missions only, the inspections are identicaL to

those for normaL operation.

For aircraft with cracks greater than 8mm, hinge bracket fractured or with cracks in

both haLf brackets repLace the bracket before the next flight.

NOTE : Each hinge bracket (forward and aft) is manufactured from two haLf

brackets joined at the vertical face of the fLange which supports

its bearing assembLyDATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I

REVISION No. : 04 Mar 30/11 PAGE : 6

Printed in France
© A300

SERVICE BULLETIN

C. DESCRIPTION

To accompLish this Service BuLLetin it is necessary to:

(1) Get access to both the LH and RH outer shroud boxes, fwd and aft

hinge brackets.

(2) Do a detailed visual inspection of the hinge brackets.

(3) Repair by replacement, as necessary.

(4) If a bracket is cracked, do additionaL visual inspections for

secondary damage of the support structure, attachment brackets and

the top skin of the inboard flap in the area of the inner and outer

shroud boxes.

(5) CLose—up.

D. APPROVAL

The technical content of this document is approved under the authority

of Design Organization Approval No. EASA.21J.031.

E. MANPOWER

This Service BuLLetin is written for an aircraft in a maintenance

status. The manhours/elapsed time estimates do not include the time to

prepare for the inspection, non—productive elapsed time or

administration.

Manhours (both wings)

Get access 2.0

Inspection 4.0

Close—up 2.0

TOTAL MANHOURS 8.0

ELAPSED TIME (HOURS) 4.0

F. MATERIAL — COST AND AVAILABILITY

If replacement brackets are required send a Spares Purchase Order,

quoting this Service Bulletin number, to:

AIRBUS

MATERIAL SUPPORT CENTER

P.O. Box 630262

22312 HAMBURG

GERMANY

G. TOOLING - PRICE AND AVAILABILITY

None

H. WEIGHT AND BALANCE

Not changed

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I

REVISION No. : 04 — Mar 30/11 PAGE : 7

Printed in France
Sj A300

SERVICE BULLETIN

I. REFERENCES

Aircraft Maintenance Manual (AMM)

Service Bulletin

J. PUBLICATIONS AFFECTED

None

06-21-57, 24-00-00, 27-51-65,

27-51-65,

A300-57-0143

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 — Mar 30/11 PAGE : 8

Printed in France
A300

SERVICE BULLETIN

2. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE

CAUTIONS LISTED IN THE REFERENCED PROCEDURES.

WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL

SURFACES ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A

HYDRAULIC SYSTEM.

(1) Preparation

(a) Make sure that the aircraft is electrically grounded (Refer to

AMM: 24-00-00, P. Block 301).

(b) To get access to the outer shroud box fwd and aft hinge

brackets, extend the flaps (Refer to AMM: 27-51-65, P. Block

401) and the inner airbrakes (Refer to AMM: 27-61-54, P. Block

401).

(c) Put warning notices in position in the flight compartment to

tell persons not to operate the flight controls.

(d) To get access to the inner shroud box, inner attachment

brackets, remove and retain the access panels 577CT, 577DT(LH),

677CT and 677DT(RH) (Refer to AMM: 06-21-57, P. Block 1).

(e) Get access to the inner shroud-box fwd attachments through the

Main Landing Gear Bays (LH and RH).

(2) Standard Practices

None

B. INSPECTION

The procedures that follow are applicable to the (LH) and (RH) wings,

Refer to Figure 1 .

(1) Clean the inspection area with cleaning agent (Mat. No. 11 -026)

(2) Get access from the top surface of the wing through the gap between

the inner and outer shroud boxes. Move the seal between the shroud

boxes, as necessary, to visually inspect the top of the outer

shroud-box hinge brackets.

(3) Do a detailed inspection of the outer shroud-box forward and aft

hinge bracket assemblies, as follows:

(a) Inspect the small radius between the top flange and the

vertical fLange, as shown in example 'A and example 'B' of

Figure 1, for signs of cracks on the hinge bracket.

(b) Get access from the Lower surface of the wing and with the use

of an inspection mirror, visually inspect both halves of the

hinge brackets for signs of cracks or fracture of the bracket.

NOTE 1 :Each hinge bracket (forward and aft) is manufactured

from two half brackets joined at the vertical face of

the fLange which supports its bearing assembly.

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 - Mar 30/11 PAGE : 9

Printed in France
A300

SERVICE BULLETIN

NOTE 2 : The cracks can start in either of the two haLf brackets and run

down the verticaL web radium (example 'A' of Figure 1), or run

through the verticaL flange under the bearing assembLy

attachment nut (example 'B' of Figure 1).

(4) Use the results of the inspection to do one or more of the worksteps that

foLLow:

(a) If cracks are not found on either the forward or aft hinge brackets,

do repeat inspections as detailed in TabLe 1 untiL Modification

06661H1033 (Service Bulletin A300-57-0143) is embodied.

(b) If a crack is found in one half bracket, do repeat inspections as

detaiLed in Table 1 until a repair is done, as detailed in Para. C.

REPAIR. The repeat intervaLs can only be carried out for crack

Lengths Less than 8mm.

(c) If both half brackets are cracked or a hinge bracket has fractured,

then do a repair as detaiLed in Para. C. REPAIR.

Cd) If a crack is found in one half bracket or both half brackets, do a

visual inspection for secondary damage in the areas that follows:

1 The inner shroud-box forward attachments and the attachment

brackets at the inboard end.

2 The inner and out shroud-box structure, adjacent to the

fractured bracket.

3 The top skin of the inboard flap.

NOTE : If any damage is found contact AIRBUS for an

applicable repair procedure.

(5) If Modification 06661H1033 (Service BuLLetin A300-57-0143) has been

embodied after the fracture of the aft hinge bracket, then visualLy

inspect the forward hinge bracket for cracks immediately after the

embodiment of the modification.

C.

REPAIR

(1) If a crack is found in one half bracket, Less than 8mm, the bracket should

be:

replaced as soon as a replacement part is available, or

embody Modification No. 06661H1033 (Service Bulletin A300-57-0143).

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I

REVISION No. : 04 Mar 30/11 PAGE : 10

Printed in France
A300

SERVICE BULLETIN

(2) If both half brackets are cracked or the hinge bracket has fractured or

cracks are greater than 8mm in one half bracket:

replace the damaged hinge bracket before the next fLight, or

embody Modification No. 06661H1033 (Service Bulletin A300-57-0143)

before the next fLight.

D. TEST

None

E. CLOSE-UP

(1) Make sure that the work areas are clean and clear of tools and other items

of equipment.

(2) Install the access panels 577CT, 577DT(LH), 677CT and 677DT(RH) (Refer to

AMM: 06-21-57, P. Block 1).

(3) Retract the inner airbrakes (Refer to AMM: 27-61-54, P Block 401).

(4) Retract the fLaps (Refer to AMM: 27-51-65, P BLock 401).

(5) Send the results of aLL the inspections to AIRBUS.

(6) AIRBUS requires the return of any failed brackets for investigation.

F.

DOCUMENTATION

Write in the applicabLe aircraft records that you have done aLL the work given

in this Service Bulletin.

DATE: Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 11

Printed in France
S A300

SERVICE BULLETIN

JOINT LINE USUAL STARTING POINT I I

OF CRACKS

CRACK IN VERTICAL

WEB RADIUS

CRACK IN VERTICAL FLANGE

UNDER BEARING ASSY. NUT

EXAMPLE 'B'

Inspection Areas

Figure 1 Sheet 1

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

I REVISION No. : 04 Mar 30/11 PAGE : 12

 Printed in France
S A300

SERVICE BULLETIN

3. MATERIAL INFORMATION

A. LIST OF C OMPONENTS

None

B. SPECIAL TOOLS

None

C. LIST OF MATERIAL - OPERATOR SUPPLI ED

DESCRIPTION REFERENCE TO CML

Cleaning agent (Mat. No. 11-026)

D. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

QTY PER A/C

As Required

DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

REVISION No. : 04 Mar 30/11 PAGE : 13/14

Printed in France
j A300

SERVICE BULLETIN

ACCEPTANCE/REJECTION SHEET I AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice BELLONTE

31707 BLAGNAC CEDEX FRANCE

TeL: (33) 5 61-93-33-33

Telex: AIRBU 530526 F

TITLE : WINGS — INSPECTION OF OUTER SHROUD BOX HINGE BRACKETS

MODIFICATION No. : NONE ATA SYSTEM : 57

IS BEING HEREWITH SUBMITTED TO YOU FOR REVIEW

Please fill : ...REJECTED

...WILL BE EMBODIED

...EFFECTIVITY

This SB can only be incorporated in your "customized"

documentation within the agreed time schedule in so far as this

sheet returned to us on purchase date and signed by a duly

authorized and empowered officer or representative.

FROM : Please return to

AIRLINE : AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

NAME 31707 BLAGNAC CEDEX FRANCE

Attn : AI/SE—D32 Technical Data

DATE : and Documentation Services

FAX : (+33) 5 61 93 28 06

7 DATE : Dec 17/86 SERVICE BULLETIN No. : A300-57-0142

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REVISION No. : 04 Mar 30/11 PAGE : 1 of 1

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