@A318/A319/A320/A321

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 - SECTION 21 - INSPECT LOWER SURFACE PANEL BETWEEN

FRAME 41 AND 42.

MODIFICATION No.: None

This page transmits Revision No.04 of Service Bulletin No.A320-57-1082

ADDITIONAL WORK

**CONF ALL

For aircraft in Config. 001, additional work is required by this revision for aircraft which have already

applied the repair instruction through any previous issue of this Service Bulletin. This additional work

consists in contacting AIRBUS within 30 days for further instruction.

For aircraft in Config. 002, additional work is required by this revision for aircraft which have not applied

Service Bulletin No. A320-57-1043 at Rev. No. 06. This additional work consists in repeating the HFEC

inspection of the lower surface panel of the center wing box.

REASON

Revision No. 04 issued to delete the repair and to update the threshold, interval and grace period for

the inspection.

CHANGES

The main changes of this revision are:

- to create Config. 001 for aircraft on which Service Bulletin No. A320-57-1043 is not accomplished,

and Config. 002 for aircraft on which Service Bulletin No. A320-57-1043 Rev. No 00 to Rev. No. 05

is accomplished.

- to delete repair instructions,

- to delete all the AIRBUS Kits (571082A01R00, 571082A02R00, 571082A03R01, 571082A04R01,

571082A05R01, 571082A06R01, 571082A07R01 and 571082A08R02),

- to modify the Flow Charts,

- to update threshold, interval and grace period values.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 1

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REVISION TRANSMITTAL SHEET

NOTE: Revised text and layout changes of this revision are not identified with revision bars.

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

Minor editorial or document structure change N

GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

APPENDICES Minor editorial or document structure change N

Fig. A-FSAAA Minor editorial or document structure change N

Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N

PLANNING INFORMATION

EFFECTIVITY Effectivity updated N

Configuration definition Config. 002 added for the aircraft on which Service

Bulletin No. A320-57-1043 Rev. 00 to 05 is

accomplished.

N

CONF 001 Minor editorial or document structure change N

CONF 002 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

History Minor editorial or document structure change N

Objective/Action Minor editorial or document structure change N

Advantages Minor editorial or document structure change N

Operational/Maintenance

Consequences

Minor editorial or document structure change N

DESCRIPTION Minor editorial or document structure change N

COMPLIANCE ACCOMPLISHMENT TIMESCALE updated. N

Classification Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

APPROVAL Sentence updated. N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 2

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REVISION TRANSMITTAL SHEET

WEIGHT AND BALANCE WEIGHT AND BALANCE updated. N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES REFERENCES updated. N

Minor editorial or document structure change N

Minor editorial or document structure change N

PUBLICATION AFFECTED PUBLICATIONS AFFECTED updated. N

INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N

SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N

Procurement Addresses Kits A01 to A08 deleted. N

Price and Availability Kits A01 to A08 deleted. N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Kits A01 to A08 deleted. N

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

Minor editorial or document structure change N

TOOLING Minor editorial or document structure change N

Tooling - Price and Availability Tooling concerning the REPAIR deleted. N

Tools Minor editorial or document structure change N

Special Tools Minor editorial or document structure change N

ACCOMPLISHMENT INSTRUCTIONS

TASK 571082- 832-801-001-INSPECTION Paragraph REPAIR deleted. N

Task associated data - 001 Minor editorial or document structure change N

Task associated data - 002 Minor editorial or document structure change N

Subtask 571082-910-001-001 Standard Practices modified. N

Subtask 571082-839-001-001 Minor editorial or document structure change N

Subtask 571082-910-001-001 Standard Practices modified. N

Subtask 571082-839-001-001 Minor editorial or document structure change N

Subtask 571082-941-001-001 Steps concerning the REPAIR deleted. N

Subtask 571082-941-001-001 Steps concerning the REPAIR deleted. N

Subtask 571082-832-006-001 Paragraph REPAIR deleted. N

Subtask 571082-832-006-002 Paragraph REPAIR deleted. N

Subtask 571082-942-009-001 Steps concerning the REPAIR deleted. N

Subtask 571082-942-009-001 Steps concerning the REPAIR deleted. N

Fig. A-FBAAA Minor editorial or document structure change N

Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FFAAA Minor editorial or document structure change N

Fig. A-FFAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FFAAB Minor editorial or document structure change N

Fig. A-FFAAB Sheet 01 Minor editorial or document structure change N

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 3

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REVISION TRANSMITTAL SHEET

Fig. A-FRAAA Minor editorial or document structure change N

Fig. A-FRAAA Sheet 01 Minor editorial or document structure change N

FILLING 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 of a fuel leak test to be performed in the case of

crack detection. This Service Bulletin is rendered mandatory by Airworthiness Directive (Consigne de

Navigabilite) No. 97-309-104(B).

Revision No. 02 issued to inform the operators of technical changes in the repair procedure.

Furthermore, Kits A07R01 and A08R02 are added to include the new parts necessary for this Revision.

Revision No. 03 issued to modify the threshold and interval related to the embodiment of this Service

Bulletin. The threshold and interval figures indicated in the previous issues of this Service Bulletin have

been defined on the basis of full scale fatigue test. Since then, a survey, carried out on the A320 family

fleet, has highlighted some differences between the mission parameters of in service aircraft and those

initially considered. The differences are mainly on the weight of fuel at landing and on the average flight

time which are higher than those defined for the analysis of the fatigue related tasks. This has led to an

adjustment of the A320 family reference fatigue mission. Consequently, the threshold and intervals

related to the embodiment of this Service Bulletin have been revised and a new limit, expressed in flight

hours has been introduced.

REVISION SEQUENCE

ORIGINAL: Oct 31/96

REVISION No.: 01 - Dec 10/97

REVISION No.: 02 - Jul 26/99

REVISION No.: 03 - Apr 30/02

REVISION No. : 04 - Dec 05/13

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 4

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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 - SECTION 21 - INSPECT LOWER SURFACE PANEL BETWEEN

FRAME 41 AND 42.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During full scale fatigue tests, cracks were detected on the center wing box lower panel, in the

radius of the milling step between stiffener 13 and 14 near the fuel pump aperture. Related

modification Service Bulletin No. A320-57-1043 (Mod. No. 22418P2408) recommends a shot peening

on the affected areas to prevent from crack initiation. However, on aircraft on which modification

Service Bulletin No. A320-57-1043 (Mod. No.22418P2408) before revision 06 is accomplished, the shot

peening could have been uncorrectly done on the CAA protection, which has no fatigue benefit effect.

Therefore, the inspection is required again on these aircraft. Moreover, the repair solution provided on

previous revisions of this Inspection Service Bulletin is no more applicable and has been removed from

Inspection Service Bulletin A320-57-1082 revision 04.

For aircraft on which Modification Service Bulletin No. A320-57-1043 revision 06 or any subsequent

revision (Mod. No. 22418P2408) is not accomplished, this Inspection Service Bulletin calls for repetitive

High Frequency Eddy Current (HFEC) inspection on the external face of the center wing box lower

panel.

Accomplishment of this Inspection Service Bulletin will enable detection of cracks at an early stage,

thus avoiding further damage on the center wing box lower panel. Accomplishment of this Inspection

Service Bulletin is cancelled by accomplishment of the Modification Service Bulletin A320-57-1043

revision 06 or any subsequent revision (Mod. No 22418P2408).

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 1

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SUMMARY

EVALUATION TABLE

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

26S 29S 31V 35U 56W 66X 69X 73W 85T 86Z ACA AFR AGC

AHY AIB ANA ART B2V BGH C9G CTN CYP D2F DAL DLH ETD

ETJ F2I FPY G2X GWI HRM IAC IBE IBS IRA JAV KAC KHO

MMA MSR MXA NVD RNV SGL SKU SNX SOL SVR TAM TAR TBZ

ULG USA VLG WRC XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 571082-832-801-001: INSPECTION

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 2

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SUMMARY

**CONF 002

Task 571082-832-801-001: INSPECTION

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

APPENDICES

**CONF ALL

None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

B

A

INSPECTION AREA

NOTE:

FR41

FR42

A

FUEL PUMP APERTURE FUEL PUMP APERTURE

B

F

W

D

VIEW LOOKING UP

FR42

FR41

STGR14

STGR13

N_SB_571082_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 4

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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 - SECTION 21 - INSPECT LOWER SURFACE PANEL BETWEEN

FRAME 41 AND 42.

MODIFICATION No.: None

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This Inspection Service Bulletin is only applicable to aircraft on which Service

Bulletin No. A320-57-1043 revision No. 06 or any subsequent revision (Mod.

No. 22418P2408) is not accomplished.

(1) Models

320-211 320-212 320-231

(2) Effectivity by MSN

0029 0045-0059 0061 0063-0078 0080-0090 0093-0097 0099 0104 0110-0119

0121-0127 0135 0137-0138 0140-0142 0147-0150 0152-0155 0157-0162 0164-0168

0171-0176 0178-0179 0181-0183 0185 0189-0190 0192 0194-0195 0197-0203

0205-0214 0216-0220 0223-0224 0229-0235 0237 0239-0246 0248-0256 0258-0270

0272-0279 0281-0282 0284-0285 0287 0289-0303 0306-0309 0311-0312 0314

0316-0325 0328-0335 0339-0343 0345-0347 0349-0351 0353-0358 0360-0362

0366-0368 0370 0372-0373 0375-0376

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 1

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(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

26S 0368

29S 0291 0292

31V 0164 0332

35U 0088 0199

56W 0250 0335

66X 0230

69X 0219

73W 0087

85T 0234

86Z 0168

ACA 0059 0068 0073 0084 0122 0126 0127 0141 0149 0150 0154 0159

0174 0175 0183 0210 0231 0232 0233 0242 0248 0253 0254 0255

0265 0277 0284 0290 0309 0324 0330 0341

AFR 0061 0063 0115 0155 0214 0237 0239 0278 0285 0287

AGC 0190

AHY 0331

AIB 0138

ANA 0167 0212 0245 0300 0328

ART 0142 0244 0279 0311 0333

B2V 0185

BGH 0349

C9G 0246

CTN 0258

CYP 0256

D2F 0243 0251

DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213

0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319

0329 0339 0340 0355 0358 0360 0367 0372

DLH 0069 0070 0071 0072 0078 0083 0086 0093 0094 0104 0110 0111

0116 0117 0135 0137 0147 0161 0172 0200 0201 0202 0209 0216

0217 0218 0267 0268 0269 0346

ETD 0350

ETJ 0325

F2I 0085 0148 0220 0249 0270 0294 0301 0373

FPY 0112 0189 0342

G2X 0347

GWI 0162

HRM 0293

IAC 0045 0046 0047 0048 0049 0050 0051 0056 0057 0058 0074 0075

0080 0089 0090 0095 0096 0097

IBE 0158 0173 0176 0207 0223 0224 0274 0323 0356

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 2

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OPERATOR MSN

IBS 0266

IRA 0303 0312 0345

JAV 0029

KAC 0181 0182 0195

KHO 0354 0376

MMA 0113 0114 0295 0316

MSR 0165 0166 0178 0194 0198 0322 0351 0366

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353

NVD 0211 0299 0375

RNV 0229

SGL 0357

SKU 0179

SNX 0289

SOL 0302

SVR 0140 0157 0203

TAM 0334

TAR 0119 0123 0124 0205 0370

TBZ 0361 0362

ULG 0308 0314

USA 0052 0053 0054 0055 0064 0065 0066 0067 0076 0077 0081 0082

0099 0317

VLG 0240 0241 0264

WRC 0235

XLF 0343

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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(4) Configuration by MSN

MSN CONFIGURATION

0029 0045 0046 0047 0048 0049 0050 0051 0052 0053 0054

0055 0056 0057 0058 0059 0061 0063 0064 0065 0066 0067

0068 0069 0070 0071 0072 0073 0074 0075 0076 0077 0078

0080 0081 0082 0083 0084 0085 0086 0087 0088 0089 0090

0093 0094 0095 0096 0097 0099 0104 0110 0111 0112 0113

0114 0115 0116 0117 0118 0119 0121 0122 0123 0124 0125

0126 0127 0135 0137 0138 0140 0141 0142 0147 0148 0149

0150 0152 0153 0154 0155 0157 0158 0159 0160 0161 0162

0164 0165 0166 0167 0168 0171 0172 0173 0174 0175 0176

0178 0179 0181 0182 0183 0185 0189 0190 0192 0194 0195

0197 0198 0199 0200 0201 0202 0203 0205 0206 0207 0208

0209 0210 0211 0212 0213 0214 0216 0217 0218 0219 0220

0223 0224 0229 0230 0231 0232 0233 0234 0235 0237 0239

0240 0241 0242 0243 0244 0245 0246 0248 0249 0250 0251

0252 0253 0254 0255 0256 0258 0259 0260 0261 0262 0263

0264 0265 0266 0267 0268 0269 0270 0272 0273 0274 0275

0276 0277 0278 0279 0281 0282 0284 0285 0287 0289 0290

0291 0292 0293 0294 0295 0296 0297 0298 0299 0300 0301

0302 0303 0306 0307 0308 0309 0311 0312 0314 0316 0317

0318 0319 0320 0321 0322 0323 0324 0325 0328 0329 0330

0331 0332 0333 0334 0335 0339 0340 0341 0342 0343 0345

0346 0347 0349 0350 0351 0353 0354 0355 0356 0357 0358

0360 0361 0362 0366 0367 0368 0370 0372 0373 0375 0376

001 002

(5) Configuration definition

**CONF 001

Config. 001 concerns aircraft on which Service Bulletin No. A320-57-1043 is not

accomplished.

**CONF 002

Config. 002 concerns aircraft on which Service Bulletin No. A320-57-1043 Rev. 00 to 05

is accomplished.

(6) Material Effectivity

No Material Set

B. CONCURRENT REQUIREMENTS

None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 4

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C. REASON

(1) History

During full scale fatigue tests, cracks were detected on the center wing box lower panel,

in the radius of the milling step between stiffener 13 and 14 near the fuel pump aperture.

Related modification Service Bulletin No. A320-57-1043 (Mod. No. 22418P2408)

recommends a shot peening on the affected areas to prevent from crack initiation.

However, on aircraft on which modification Service Bulletin No. A320-57-1043 (Mod.

No.22418P2408) before revision 06 is accomplished, the shot peening could have been

uncorrectly done on the CAA protection, which has no fatigue benefit effect. Therefore,

the inspection is required again on these aircraft. Moreover, the repair solution provided

on previous revisions of this Inspection Service Bulletin is no more applicable and has

been removed from Inspection Service Bulletin A320-57-1082 revision 04.

(2) Objective/Action

For aircraft on which Modification Service Bulletin No. A320-57-1043 revision 06 or

any subsequent revision (Mod. No. 22418P2408) is not accomplished, this Inspection

Service Bulletin calls for repetitive High Frequency Eddy Current (HFEC) inspection on

the external face of the center wing box lower panel.

(3) Advantages

Accomplishment of this Inspection Service Bulletin will enable detection of cracks at

an early stage, thus avoiding further damage on the center wing box lower panel.

Accomplishment of this Inspection Service Bulletin is cancelled by accomplishment of

the Modification Service Bulletin A320-57-1043 revision 06 or any subsequent revision

(Mod. No 22418P2408).

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 571082-832-801-001: INSPECTION

(1) Do a HFEC Inspection on the Lower Surface Panel of the Center Wing Box

**CONF 002

Task 571082-832-801-001: INSPECTION

(1) Do a HFEC Inspection on the Lower Surface Panel of the Center Wing Box

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 5

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**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

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.

Table 1, Config. 001 - Special Detailed Inspection of the Lower Surface panel of the Center Wing Box

Compliance Time (whichever occurs

later)

Condition Action

Threshold from

first flight

(whichever occurs

first)

Grace period

(whichever occurs

first)

Repetitive Interval

(whichever occurs

first)

All aircraft Check that ISB No.

A320-57-1082 Rev.

00 to 03 is

accomplished, refer

to TASK

571082-832-801-001

20700 FC / 41400

FH

7200 FC / 14400

FH since last

inspection

according to ISB

No. A320-57-1082

at revision up to

03

None

Repair according

to ISB No.

A320-57-1082

Rev. No. 00 to 03

accomplished on

aircraft

Contact AIRBUS and

apply actions

provided by AIRBUS

Within 30 days None None

Repair according

to ISB No.

A320-57-1082

Rev. No. 00 to 03

not accomplished

on aircraft

Do a HFEC

inspection of the

lower surface panel

of the center wing

box, refer to

SUBTASK

571082-832-006-001

Before next flight None None

Crack found Contact AIRBUS and

apply actions

provided by AIRBUS

Before next flight None None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 6

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Table 1, Config. 001 - Special Detailed Inspection of the Lower Surface panel of the Center Wing Box

Compliance Time (whichever occurs

later)

Condition Action

Threshold from

first flight

(whichever occurs

first)

Grace period

(whichever occurs

first)

Repetitive Interval

(whichever occurs

first)

Repeat the HFEC

inspection of the

lower surface panel

of the center wing

box, refer to TASK

571082-832-801-001

None None 7200 FC / 14400

FH

OR

No crack found

Accomplish the MSB

No. A320-57-1043

Rev.06

None None None

**CONF 002

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.

Table 1, Config. 002 - Special Detailed Inspection of the Lower Surface panel of the Center Wing Box

Compliance Time (whichever occurs

later)

Condition Action

Threshold from

first flight

(whichever occurs

first)

Grace period

(whichever occurs

first)

Repetitive Interval

(whichever occurs

first)

All aircraft Do a special detailed

inspection (HFEC) of

the lower surface

panel of the center

wing box, refer to

TASK

571082-832-801-001

7200 FC / 14400

FH from MSB No.

A320-57-1043

embodiment

Within 850 FC /

1700 FH from this

Service Bulletin

issuance date

NOTE*

None

Crack found Contact AIRBUS and

apply actions provided

by AIRBUS

Before next flight None None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 7

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Table 1, Config. 002 - Special Detailed Inspection of the Lower Surface panel of the Center Wing Box

Compliance Time (whichever occurs

later)

Condition Action

Threshold from

first flight

(whichever occurs

first)

Grace period

(whichever occurs

first)

Repetitive Interval

(whichever occurs

first)

Repeat the HFEC

inspection of the lower

surface panel of the

center wing box, refer

to TASK

571082-832-801-001

None None 7200 FC / 14400

FH

OR

No crack found

Accomplish the MSB

No. A320-57-1043

Rev.06

None None None

NOTE*: A grace period of 3750 FC or 7500 FH whichever occurs first from Jul 31/12 has been

defined and will be readjusted from SB issuance date with the assumption of an average accumulation

of 2500 FC / 5000 FH per year.

**CONF ALL

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organization Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

**CONF 001

Task 571082-832-801-001: INSPECTION

Get Access 0.50

On Aircraft

Do a HFEC Inspection on the Lower Surface Panel of

the Center Wing Box

2.00

Close-Up 0.50

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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Task 571082-832-801-001: INSPECTION

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

**CONF 002

Task 571082-832-801-001: INSPECTION

Get Access 0.50

On Aircraft

Do a HFEC Inspection on the Lower Surface Panel of

the Center Wing Box

2.00

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24

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

Non Destructive Test Manual (NTM) 57-11-95

Service Bulletin (SB) A320-57-1043

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24

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

Non Destructive Test Manual (NTM) 57-11-95

Service Bulletin (SB) A320-57-1043

**CONF ALL

K. PUBLICATION AFFECTED

None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

None

(2) Price and Availability

None

B. INDUSTRY SUPPORT INFORMATION

None

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Service Bulletin it is necessary to use the tools listed in the

subsequent referenced AMM and/or NTM tasks:

- NTM 57-11-95 Part 6

(3) Special Tools

None

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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This Page Intentionally Left Blank

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 571082-832-801-001 - INSPECTION

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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Task Associated Data

**CONF 001

Zone

195 196

Access

Panel 195BB 196BB

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

**CONF 002

Zone

195 196

Access

Panel 195BB 196BB

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 571082-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(2) Subtask 571082-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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**CONF 002

(1) Subtask 571082-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(2) Subtask 571082-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 571082-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-802

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-869-802.

(c) Put an access platform(s) in position at zone 195 and 196.

(d) Open the access doors 195BB and 196BB, refer to AMM 06-41-53 Page Block 001.

**CONF 002

(1) Subtask 571082-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-802

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety locks and the

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

(b) Make sure that the aircraft is electrically grounded, refer to AMM Task

12-34-24-869-802.

(c) Put an access platform(s) in position at zone 195 and 196.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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(d) Open the access doors 195BB and 196BB, refer to AMM 06-41-53 Page Block 001.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 571082-832-006-001 - Do a HFEC Inspection on the Lower Surface Panel

of the Center Wing Box

Work Zones and Access Panels

Zone Access/Work location

195 Access Panel 195BB

196 Access Panel 196BB

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Non Destructive Test Manual (NTM) 57-11-95 Part 6

Service Bulletin (SB) A320-57-1043

Fig. A-FBAAA

Inspection of the Lower Surface Panel of

the Center Wing Box

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

At the threshold given in the PLANNING INFORMATION paragraph E.(2).

(a) Check that Inspection Service Bulletin No. A320-57-1082 Rev. No. 00 to Rev. No.

03 is accomplished.

Refer to Fig. A-FFAAA Sheet 01

1 If the aircraft has been repaired according to Inspection Service Bulletin No.

A320-57-1082 revision No. 00 to 03, contact AIRBUS within 30 days and

apply actions provided by AIRBUS.

2 If the aircraft has not been repaired according to Inspection Service Bulletin

No. A320-57-1082 revision No. 00 to 03:

a Do a HFEC inspection of the lower surface panel of the center wing box

at the threshold given in the PLANNING INFORMATION paragraph E.(2).

Refer to Fig. A-FBAAA and Fig. A-FFAAA

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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Refer to NTM 57-11-95 Part 6

<1> If crack is found:

<a> Contact AIRBUS and apply actions provided by AIRBUS before

next flight.

<2> If no crack is found:

<a> Repeat the HFEC inspection of the lower surface panel of

the center wing box as specified in NTM 57-11-95 Part 6,

refer to TASK 571082-832-801-001 at the interval given in the

PLANNING INFORMATION paragraph E.(2).

<b> Or, accomplish Service Bulletin No. A320-57-1043 revision No.

06.

<c> No further action is necessary.

3 For the Inspection Report, refer to Fig. A-FRAAA.

**CONF 002

(1) Subtask 571082-832-006-002 - Do a HFEC Inspection on the Lower Surface Panel

of the Center Wing Box

Work Zones and Access Panels

Zone Access/Work location

195 Access Panel 195BB

196 Access Panel 196BB

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Non Destructive Test Manual (NTM) 57-11-95 Part 6

Service Bulletin (SB) A320-57-1043

Fig. A-FBAAA

Inspection of the Lower Surface Panel of

the Center Wing Box

Sheet 01

Fig. A-FFAAB

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

At the threshold given in the PLANNING INFORMATION paragraph E.(2).

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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(a) Do a HFEC inspection of the lower surface panel of the center wing box.

Refer to Fig. A-FBAAA and Fig. A-FFAAB Sheet 01

Refer to NTM 57-11-95 Part 6

1 If crack is found:

a Contact AIRBUS and apply actions provided by AIRBUS before next

flight.

2 If no crack is found:

a Repeat the HFEC inspection of the lower surface panel of the

center wing box as specified in NTM 57-11-95 Part 6, refer to

TASK 571082-832-801-001 at the interval given in the PLANNING

INFORMATION paragraph E.(2).

b Or, accomplish Service Bulletin No. A320-57-1043 revision No. 06.

c No further action is necessary.

3 For the Inspection Report, refer to Fig. A-FRAAA.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 571082-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

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

equipment.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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(b) Close the access doors 195BB and 196BB, refer to AMM 06-41-53 Page Block

001.

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 571082-942-009-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

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

equipment.

(b) Close the access doors 195BB and 196BB, refer to AMM 06-41-53 Page Block

001.

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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**CONF ALL

PUMP AXIS

DATUM

Y−1292

Y−254Y−765

TYPICAL CRACK HYDRAULIC BULKHEAD FUEL PUMP APERTURE

TYPICAL CRACK

B

A

FR41

FR42

INSPECTION AREA

A A

A A

STGR14

STGR13

STGR12

STGR15

DATUM

DATUM

DATUM

B

F

W

D

A

NOTE:

01 RH SHOWN, LH SYMMETRICAL

01

N_SB_571082_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Inspection of the Lower Surface Panel of the Center Wing Box

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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**CONF 001

QUESTION

ACTION

FINDING

YES NO

CHECK THAT ISB No A320−57−1082 REV. 00 TO 03 IS ACCOMPLISHED 

AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2) 

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.

REPAIR ACCORDING TO

ISB No. A320−57−1082 REV. 00 TO 03

ACCOMPLISHED ON THE AIRCRAFT

DO THE HFEC INSPECTION OF THE LOWER SURFACE PANEL OF THE CENTER WING BOX

AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2)

REFER TO SUBTASK 571082−832−006−001

NO CRACK FOUND YES

OR CONTACT AIRBUS AND APPLY ACTIONS

PROVIDED BY AIRBUS BEFORE NEXT FLIGHT

ACCOMPLISH THE MSB No A320−57−1043 Rev. 06

REPEAT THE HFEC INSPECTION OF THE LOWER SURFACE PANEL OF THE CENTER WING BOX

AT INTERVAL GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2).

REFER TO TASK 571082−832−801−001

NO FURTHER ACTION

CONTACT AIRBUS WITHIN 30 DAYS

AND APPLY ACTIONS PROVIDED BY AIRBUS

REFER TO TASK 571082−832−801−001

N_SB_571082_5_FAAA_01_01

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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**CONF 002

QUESTION

ACTION

FINDING

NO CRACK FOUND YES

OR

REFER TO TASK 571082−832−801−001

CONTACT AIRBUS AND APPLY ACTIONS

PROVIDED BY AIRBUS BEFORE NEXT FLIGHT

ACCOMPLISH THE MSB No A320−57−1043 Rev. 06

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.

REPEAT THE HFEC INSPECTION OF THE LOWER SURFACE

PANEL OF THE CENTER WING BOX AT INTERVAL GIVEN IN 

NO FURTHER ACTION

PLANNING INFORMATION PARAGRAPH E.(2).

REFER TO TASK 571082−832−801−001

DO A SPECIAL DETAILED INSPECTION (HFEC) OF THE LOWER SURFACE PANEL OF THE CENTER WING

BOX AT THE THRESHOLD GIVEN IN PLANNING INFORMATION PARAGRAPH E.(2).

N_SB_571082_5_FAAB_01_00

Figure A-FFAAB - Sheet 01

Flow Chart

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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**CONF ALL

PLEASE PRECISE OTHER FINDINGS:

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−57−1082

DATE OF INSPECTION :

RETURN TO :

INSPECTION METHOD : SPECIAL DETAILED INSPECTION

NO

CRACK DEPTH

CRACK

LENGTH

HFEC

INSPECTION

RIGHT SIDE OF THE

LOWER SURFACE PANEL

OF THE CENTER WING BOX

LEFT SIDE OF THE

LOWER SURFACE PANEL

OF THE CENTER WING BOX

RH LOOKING UP SHOWN

(LH SYMMETRICAL)

INSPECTION AREA ON THE LOWER

SURFACE ON LOWER SURFACE PANEL

OF THE CENTER WING BOX

PUMP AXIS

DATUM

STGR14

STGR13

STGR12

STGR15

DATUM

DATUM

DATUM

F

W

D

A

A

INSPECTION AREA

NOTE:

A A

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES4

PAX DOORS − FUSELAGE (SA/LA) − WINDOWS − CENTER WING BOX (SA/LA)

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: structure.sbinspectionresult@airbus.com

FAX +33 (0)5 61 93 36 14

N_SB_571082_5_RAAA_01_01

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

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REPORTING SHEET

TITLE: WINGS - SECTION 21 - INSPECT LOWER SURFACE PANEL BETWEEN

FRAME 41 AND 42.

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

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.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- 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 Operator Supplied X Mod/Inspection

X Manpower X Industry support 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 CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Oct 31/96 SERVICE BULLETIN No.: A320-57-1082

REVISION No.: 04 - Dec 05/13 Page: 1

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