@A318/A319/A320/A321

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.

ATA SYSTEM: 53

TITLE: FUSELAGE - MAIN STRUCTURE - INSPECTION FOR MISSING

FASTENERS AT FR24 BETWEEN STR17 & STR18

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

On MSN 5255, at VIP cabin customization at manufacturers site, several fasteners and an angle PN

D5323006520103 were found missing at right hand side on FR24 between STR17 and STR18 during

inspections.

An inspection is therefore needed on 70 Aircraft potentially impacted by this issue.

This Service Bulletin recommends doing special detailed inspections for missing fasteners and missing

splice. The special detailed inspections consists in rototest under insulation blankets in case of missing

parts.

Accomplishment of this Service Bulletin will clarify the build status at the identified location and restore

it conform to the applicable design standard when needed.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational

disruptions.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Rivet, Bush.

Component COMPA02 1 See SB Splice

EFFECTIVITY

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

54S AAR ABY AFL AXM AZA BER CCA CEB CES CRK CSC CSN

DLH EZY GFA GOW HKE HVN IAW IGO JJP JST LAN MEA ONE

QTR RJD SLK SVA TAI TAM TBA THA THY USA

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 531285-832-801-001: Inspection

TOTAL MANHOURS 39.00

ELAPSED TIME (HOURS) 39.00

APPENDICES

None

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF ALL

AREA TO BE INSPECTED

A

Z232

NOTE:

A FR24

STGR18

B

N_SB_531285_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF ALL

C

FR23 FR24 FR25

STGR17

STGR18

STGR17

STGR18

FR24

FWD

B

C

E

D

N_SB_531285_5_SAAA_02_01

Figure A-FSAAA - Sheet 02

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF ALL

STGR17

STGR18

FR24

VIEW LOOKING AFT

D

NOTE:

MISSING FASTENERS

STGR18

FR24

PART MISSING

E

N_SB_531285_5_SAAA_03_01

Figure A-FSAAA - Sheet 03

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

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

ATA SYSTEM: 53

TITLE: FUSELAGE - MAIN STRUCTURE - INSPECTION FOR MISSING

FASTENERS AT FR24 BETWEEN STR17 & STR18

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

(1) Models

319-111 319-112 319-115 319-132 319-133 320-214 320-216 320-232

320-233 321-211 321-231 321-232

(2) Effectivity by MSN

5230-5294 5296-5300

(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

54S 5261

AAR 5287

ABY 5276

AFL 5271

AXM 5272 5283

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

AZA 5294

BER 5246 5252

CCA 5265

CEB 5250

CES 5242 5267 5273

CRK 5260

CSC 5233 5286

CSN 5237 5268 5279 5288

DLH 5239 5284 5293

EZY 5236 5249 5289

GFA 5257

GOW 5232

HKE 5264 5266

HVN 5241 5247 5251 5275 5297

IAW 5290

IGO 5230 5231 5259 5262 5291 5298

JJP 5245 5274 5281

JST 5270

LAN 5234 5263

MEA 5253

ONE 5278 5299

QTR 5255

RJD 5277

SLK 5296

SVA 5285

TAI 5238 5243 5280

TAM 5240

TBA 5256

THA 5248 5258

THY 5254

USA 5235 5244 5269 5282 5292 5300

(4) Configuration by MSN

MSN CONFIGURATION

5230 5231 5232 5233 5234 5235 5236 5237 5238 5239 5240

5241 5242 5243 5244 5245 5246 5247 5248 5249 5250 5251

5252 5253 5254 5255 5256 5257 5258 5259 5260 5261 5262

5263 5264 5265 5266 5267 5268 5269 5270 5271 5272 5273

5274 5275 5276 5277 5278 5279 5280 5281 5282 5283 5284

5285 5286 5287 5288 5289 5290 5291 5292 5293 5294 5296

5297 5298 5299 5300

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA02 1

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

On MSN 5255, at VIP cabin customization at manufacturers site, several fasteners and

an angle PN D5323006520103 were found missing at right hand side on FR24 between

STR17 and STR18 during inspections.

An inspection is therefore needed on 70 Aircraft potentially impacted by this issue.

(2) Objective/Action

This Service Bulletin recommends doing special detailed inspections for missing

fasteners and missing splice. The special detailed inspections consists in rototest under

insulation blankets in case of missing parts.

(3) Advantages

Accomplishment of this Service Bulletin will clarify the build status at the identified

location and restore it conform to the applicable design standard when needed.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 531285-832-801-001: Inspection

(1) Do a General Visual Inspection of FR 24 between STGR 17 and 18 RH side.

(2) Depending on Inspection Results: Remove the Fasteners of FR 24 between STGR

17 and 18 RH side.

(3) Do a Rototest Inspection of the Fastener Holes at FR 24 between STGR 17 and 18

RH side.

(4) Depending on Inspection Results: Reinstall Fasteners and Splice at FR 24 between

STGR 17 and 18 RH side.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

This Service Bulletin has been classified Recommended. It is expected that an

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

will be issued to change this classification to Mandatory. It is anticipated that the AD

will confirm the thresholds given below but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

Table 1, Config.001: Inspection of Frame 24 between stringer 17 and stringer 18 RH side

Condition Action Compliance Time Repetitive Interval

All Aircraft Do a General Visual

Inspection of Frame 24

between stringer 17 and

stringer 18 RH side, refer

to TASK 531285-832-801

001 Inspection

Within 5000 FC from

entry into service

None

No missing fasteners

and/or splice

No further action None None

Remove fasteners of holes

1 to 44, refer to SUBTASK

531285-831-001 001

Depending on Inspection

Results: Remove the

Fasteners of FR 24

between STGR 17 and 18

RH side.

and

Missing fasteners Before next flight None

and/or splice

Do the rototest inspection

of all holes, refer to

SUBTASK 531285-832-002

001 Do a Rototest

Inspection of the Fastener

Holes at FR 24 between

STGR 17 and 18 RH side.

Before next flight None

If crack is found Contact Airbus for further

action

Before next flight None

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Table 1, Config.001: Inspection of Frame 24 between stringer 17 and stringer 18 RH side

Condition Action Compliance Time Repetitive Interval

Reinstall fasteners and

splice, refer to SUBTASK

531285-831-002 001

Depending on Inspection

Results: Reinstall

Fasteners and Splice at FR

24 between STGR 17 and

18 RH side. SUBTASK

531285-831-002-001

and

If no crack is found Before next flight None

No further action None None

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

Task 531285-832-801-001: Inspection

Get Access 4.00

On Aircraft

Do a General Visual Inspection of FR 24 between

STGR 17 and 18 RH side.

0.25

Depending on Inspection Results: Remove the

Fasteners of FR 24 between STGR 17 and 18 RH

side.

6.50

Do a Rototest Inspection of the Fastener Holes at FR

24 between STGR 17 and 18 RH side.

12.00

Depending on Inspection Results: Reinstall Fasteners

and Splice at FR 24 between STGR 17 and 18 RH

side.

12.00

Close-Up 4.25

TOTAL MANHOURS 39.00

ELAPSED TIME (HOURS) 39.00

NOTE: The minimum manhours necessary to accomplish this Service Bulletin are

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

those for the Inspection. Depending on the inspection result, additional

manhours can apply.

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 12-34-24

20-21-11 25-21-41 25-23-43

25-23-44 25-80-00 52-10-00

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

Non Destructive Test Manual (NTM) 51-10-01

Standards Manual (SM)

Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00

51-44-00

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 53-21-00

Impact on scheduled maintenance: Refer to Maintenance Planning Document (MPD).

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive

multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers

with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to

B/E Aerospace. The address is:

Component COMPA01 B/E AEROSPACE INC.

CONSUMABLES MANAGEMENT

10000 NW 15th Terrace Miami

FL 33172

USA

Tel EMEA: +49 (0) 822 285 31500

Tel US: +1 305 925 2600

Tel ASIA: +1 310 900 1300

Fax EMEA: +49 (0) 822 285 31010

Fax US: +1 305 507 7191

Fax ASIA: +1 310 819 1200

SITA: MIAMMCR

E-mail: AOGdesk_CMG@beaerospace.com

internet: http://www.beconsumables.com

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Component COMPA02 AIRBUS Material, Logistics and suppliers

IFD - In Flight Desk

Weg Beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 4012

For ordering by E-mail:

ifd.spares@airbus.com

(2) Price and Availability

No AIRBUS kit will be provided.

Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be

purchased by a spares purchase order.

Operator supplied standard hardware parts required to accomplish this Service Bulletin

are to be supplied from the Operator’s stock.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will credit the man hours indicated in this Service Bulletin for inspections that are

performed on aircraft in warranty at the time of such inspection. Credit will be at the agreed

inhouse warranty labour rate. Claims for labour allowance should be received not later than

90 days after completion of the last affected warranted aircraft.

For those aircraft in warranty at the time of such inspection with findings further to inspection

as per this Service Bulletin, AIRBUS will share the costs of accomplishment of this Service

Bulletin by crediting the operator supplied AIRBUS parts for orders placed before Sep 30/17.

Claims for this allowance should be received not later than 90 days after completion of the

last affected aircraft of your fleet.

For the accomplishment of this Service Bulletin before Sep 30/17, AIRBUS will share the

costs by crediting the operator supplied standard hardware parts. Claims for this allowance

should be received not later than 90 days after completion of the last affected aircraft of your

fleet.

Airbus will credit the man hours indicated in this Service Bulletin for corrections that are

performed on aircraft in warranty at the time of such correction. Credit will be at the agreed

inhouse warranty labour rate. Claims for labour allowance should be received not later than

90 days after completion of the last affected warranted aircraft.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint--

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane-- External

Structure

04JAA3 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

(2) Components

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

2 ASNA2536-3 55 NUT

3 ASNA2657V3-5Y 6 BOLT

4 EN6114V3-5 6 BOLT

5 EN6114V3-4 6 BOLT

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

6 EN6114V3-3 8 BOLT

7 EN6114V3-6 10 BOLT

9 EN6115V3-8 16 BOLT

10 EN6114V3-7 3 BOLT

11 ASNA2050DXJ4020 10 RIVET

NOTE: If you find part numbers of hardware components in the related kit(s)

which you cannot identify in the LIST OF COMPONENTS of this Service

Bulletin, refer to Standards Manual (SM). The SM will give you the

correct part number to part number relationship.

NOTE: The above list of components is not AIRBUS Kit, the required parts shall

be ordered as necessary through the given channel.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 D5323006520103 1 SPLICE

NOTE: The above list of components is not AIRBUS Kit, the required parts shall

be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 9

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 10

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 531285-832-801-001 - 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 KEEPELECTRICAL 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: 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.

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.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 11

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Task Associated Data

Zone

232

Access

Door 831

Manpower

TOTAL MANHOURS 39.00

ELAPSED TIME (HOURS) 39.00

A. GENERAL

(1) Subtask 531285-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-24-00

51-42-00

51-43-00

51-44-00

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

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

(c) Remove and install fasteners in accordance with SRM 51-42-00.

(d) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

(e) Obtain alternative and substitute fastener data, in accordance with SRM 51-43-00.

(f) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Materials List (CML).

(2) Subtask 531285-839-002-001 - 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: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 12

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

B. PREPARATION

(1) Subtask 531285-941-002-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

232 Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-21-41-000-001

Task 25-23-43-000-001

Task 25-23-44-000-001

25-80-00, Page Block 201

Task 52-10-00-010-001

(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

12-34-24-860-802.

(c) Put an access platform(s) in position at door 831.

(d) Open the passenger/crew door 831, refer to AMM Task 52-10-00-010-001.

(e) If necessary, remove the passenger seats around Frame 24, refer to AMM Task

25-21-41-000-001.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 13

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(f) Remove the sidewall panels 232DW, 232EW, 232GW and 232HW, refer to AMM

Task 25-23-43-000-001 and AMM Task 25-23-44-000-001.

(g) Move insulation blankets around the Frame 24, refer to AMM 25-80-00, Page Block

201.

C. PROCEDURE

(1) Subtask 531285-832-001-001 - Do a General Visual Inspection of FR 24 between

STGR 17 and 18 RH side.

Work Zones and Access Panels

Zone Access/Work location

232 Access Door 831

Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

Sheet 02

Fig. A-FBAAA

Area to be Inspected

Sheet 01

Sheet 02

Sheet 03

(a) At the threshold given in the Planning Information paragraph E.(2):

Do a General Visual Inspection of Frame 24 between stringer 17 and stringer 18

RH side.

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

1 If there are no missing fasteners and/or splice:

a No further action.

2 If there are missing fasteners and/or splice:

a Do SUBTASK 531285-831-001 001 Depending on Inspection Results:

Remove the Fasteners of FR 24 between STGR 17 and 18 RH side.

and

Do SUBTASK 531285-832-002 001 Do a Rototest Inspection of the

Fastener Holes at FR 24 between STGR 17 and 18 RH side.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 14

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(b) For the Inspection Report, refer to Fig. A-FRAAA.

(2) Subtask 531285-831-001-001 - Depending on Inspection Results: Remove the

Fasteners of FR 24 between STGR 17 and 18 RH side.

Work Zones and Access Panels

Zone Access/Work location

232 Access Door 831

Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Manhours 6.50

Minimum number of person 1

Subtask elapsed time 6.50

Skills NON SPECIFIC

References

Structural Repair Manual (SRM) 51-42-00

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove fasteners of holes 1 to 44:

Refer to Fig. A-FBCAA.

In accordance with SRM 51-42-00.

6 Bush Item (2) Discard

3 Rivet Item (3) Discard

6 Rivet Item (4) Discard

22 Bush Item (5) Discard

6 Rivet Item (6) Discard

8 Rivet Item (7) Discard

3 Rivet Item (8) Discard

2 Rivet Item (9) Discard

16 Rivet Item (10) Discard

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 15

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(3) Subtask 531285-832-002-001 - Do a Rototest Inspection of the Fastener Holes at

FR 24 between STGR 17 and 18 RH side.

Work Zones and Access Panels

Zone Access/Work location

232 Access Door 831

Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills NON DESTRUCTIVE

TESTING

References

Non Destructive Test Manual (NTM) 51-10-01

Fig. A-FBBAA

Rototest Inspection of Fasteners Holes

Sheet 01

Sheet 02

Sheet 03

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report

Sheet 01

Sheet 02

(a) Do the rototest inspection of all holes:

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

Refer to NTM 51-10-01.

1 If crack is found:

a Contact Airbus for further instruction.

2 If no crack is found:

a Do SUBTASK 531285-831-002 001 Depending on Inspection Results:

Reinstall Fasteners and Splice at FR 24 between STGR 17 and 18 RH

side.

(b) For the Inspection Report, refer to Fig. A-FRAAA.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 16

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(4) Subtask 531285-831-002-001 - Depending on Inspection Results: Reinstall

Fasteners and Splice at FR 24 between STGR 17 and 18 RH side.

Work Zones and Access Panels

Zone Access/Work location

232 Access Door 831

Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Manhours 12.00

Minimum number of person 1

Subtask elapsed time 12.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 ASNA2536-3 55 NUT

3 ASNA2657V3-5Y 6 BOLT

4 EN6114V3-5 6 BOLT

5 EN6114V3-4 6 BOLT

6 EN6114V3-3 8 BOLT

7 EN6114V3-6 10 BOLT

9 EN6115V3-8 16 BOLT

10 EN6114V3-7 3 BOLT

11 ASNA2050DXJ4020 10 RIVET

NOTE: The above list of components is not AIRBUS Kit, the required parts shall

be ordered as necessary through the given channel.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D5323006520103 1 SPLICE

NOTE: The above list of components is not AIRBUS Kit, the required parts shall

be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Primer Polyurethane Paint--

Corrosion Inhibiting

04EAC2 As required

Top Coat Polyurethane--

External Structure

04JAA3 As required

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 17

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-24-00

51-42-00

51-43-00

51-44-00

Fig. A-FBCAA

Removal/Installation of Fasteners

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-FRAAA

Inspection Report

Sheet 01

Sheet 02

(a) Install fasteners of holes 1 to 44:

Refer to Fig. A-FBCAA.

In accordance with SRM 51-42-00 and SRM 51-43-00.

Refer to AMM Task 20-21-11-911-001.

44 Nut ASNA2536-3 Item 2

6 Bolt ASNA2657V3-5Y Item 3

6 Bolt EN6114V3-5 Item 4

6 Bolt EN6114V3-4 Item 5

8 Bolt EN6114V3-3 Item 6

2 Bolt EN6114V3-6 Item 7

16 Bolt EN6115V3-8 Item 9

(b) Install the missing splice and fasteners:

Refer to Fig. A-FBCAA.

In accordance with SRM 51-42-00, SRM 51-43-00 and SRM 51-44-00.

Refer to AMM Task 20-21-11-911-001.

1 Temporarily, put the Splice Item 1 in position as shown on Fig. A-FBCAA

Sheet 03 and Fig. A-FBCAA Sheet 04.

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 18

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

2 Drill eleven holes on the structure to align with the holes of the splice Item 1 to

the diameter given in Fig. A-FBCAA Sheet 03 and Fig. A-FBCAA Sheet 04.

3 Drill ten holes on the splice Item 1 to align with the holes of the structure to

the diameter given in Fig. A-FBCAA Sheet 04.

4 Remove the splice Item 1 and deburr the holes.

5 Between the splice Item 1 and the structure apply:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

Refer to SRM 51-24-00

6 Install:

Refer to Fig. A-FBCAA Sheet 03 and Fig. A-FBCAA Sheet 04.

1 Splice D5323006520103 Item 1

8 Bolt EN6114V3-6 Item 7

3 Bolt EN6114V3-7 Item 10

11 Nut ASNA2536-3 Item 2

10 Rivet ASNA2050DXJ4020 Item 11

7 Do a sealant bead around the splice Item 1 with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

8 On the splice apply:

Primer

Polyurethane Paint-

- Corrosion

Inhibiting

04EAC2 As required

Top Coat

Polyurethane--

External Structure

04JAA3 As required

D. TEST

(1) Subtask 531285-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 19

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 25-21-41, Page Block 401

NOTE: This Service Bulletin requires the accomplishment of the following Tests

which are given in subtasks included in the topic Close-up. The

manhours for the tests are included in the referenced Service Bulletin

subtasks.

If necessary, do the test procedure as specified in the SEAT - PASSENGER -

REMOVAL/INSTALLATION, refer to AMM 25-21-41, Page Block 401.

E. CLOSE-UP

(1) Subtask 531285-942-001-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

232 Access Door 831

Work location Frame 24

from Stringer 17 to Stringer 18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-001

Task 25-23-43-400-001

Task 25-23-44-400-001

Task 25-80-00-400-001

Task 52-10-00-410-001

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

equipment.

(b) Install insulation blankets, refer to AMM Task 25-80-00-400-001.

(c) Install the sidewall panels 232DW, 232EW, 232GW and 232HW, refer to AMM

Task 25-23-43-400-001 and AMM Task 25-23-44-400-001.

(d) If removed, install the passenger seats, refer to AMM Task 25-21-41-400-001.

(e) Close passenger/crew door, refer to AMM Task 52-10-00-410-001.

(f) Remove the access platform(s).

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

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 20

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

AREA TO BE INSPECTED

A

Z232

NOTE:

A FR24

STGR18

B

N_SB_531285_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Area to be Inspected

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 21

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

C

FR23 FR24 FR25

STGR17

STGR18

STGR17

STGR18

FR24

FWD

B

C

E

D

N_SB_531285_5_BAAA_02_01

Figure A-FBAAA - Sheet 02

Area to be Inspected

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 22

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

STGR17

STGR18

FR24

VIEW LOOKING AFT

D

NOTE:

MISSING FASTENERS

STGR18

FR24

PART MISSING

E

N_SB_531285_5_BAAA_03_01

Figure A-FBAAA - Sheet 03

Area to be Inspected

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 23

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

AREA TO BE INSPECTED

A

Z232

NOTE:

A FR24

STGR18

B

N_SB_531285_5_BBAA_01_01

Figure A-FBBAA - Sheet 01

Rototest Inspection of Fasteners Holes

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 24

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

C

FR23 FR24 FR25

STGR17

STGR18

STGR17

STGR18

FR24

FWD

B

C

F

E D

N_SB_531285_5_BBAA_02_01

Figure A-FBBAA - Sheet 02

Rototest Inspection of Fasteners Holes

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 25

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

STGR17

STGR18

FR24

VIEW LOOKING AFT

STGR18

FR24

E

STGR18

FR24

D

NOTE:

HOLE WITH FASTENER TO BE INSPECTED

HOLE WITHOUT FASTENER TO BE INSPECTED

F

G

FR24

FWD

G

N_SB_531285_5_BBAA_03_01

Figure A-FBBAA - Sheet 03

Rototest Inspection of Fasteners Holes

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 26

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

AREA TO BE INSPECTED

A

Z232

NOTE:

A FR24

STGR18

B

N_SB_531285_5_BCAA_01_01

Figure A-FBCAA - Sheet 01

Removal/Installation of Fasteners

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 27

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

C

FR23 FR24 FR25

STGR17

STGR18

STGR17

STGR18

FR24

FWD

B

C

F

E D

N_SB_531285_5_BCAA_02_01

Figure A-FBCAA - Sheet 02

Removal/Installation of Fasteners

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 28

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

STGR18

FR24

E

STGR18

FR24

D

NOTE:

BETWEEN THE SPLICE AND THE 

1 01

01

STRUCTURE APPLY MAT. No 06AAB1.

H8 H16

H15

H6 H14

H7

H5

H4

H13

H12

H3

H2

H1

H11

H10

H9

H20

H19

H28

H27

H26

H25

H24

H23

H22

H21

H17

H18

20.33 mm

(0.8 in)

02

03

02 DO A SEALANT BEAD AROUND THE SPLICE WITH MAT. No 06AAB1.

03 ON THE SPLICE APPLY MAT. No 04EAC2

AND MAT. No 04JAA2. N_SB_531285_5_BCAA_03_01

Figure A-FBCAA - Sheet 03

Removal/Installation of Fasteners

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 29

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

STGR17

STGR18

FR24

NOTE: VIEW LOOKING AFT

HOLE 

SYMBOLE

OLD

ITEM ITEM PN DESCRIPTION HOLE DIAMETER

MIN MAX

EN6114V3−5

ASNA2657V3−5Y

ASNA2536−3

ASNA2536−3

EN6114V3−4

ASNA2536−3

EN6114V3−3

ASNA2536−3

ASNA2657V3−5Y

ASNA2536−3

EN6114V3−6

ASNA2536−3

EN6115V3−8

EN6114V3−6

ASNA2536−3

EN6114V3−7

ASNA2536−3

ASNA2050DXJ4020

NUT

BOLT

BOLT

NUT

BOLT

NUT

BOLT

NUT

BOLT

NUT

BOLT

NUT

BOLT

4.14 mm

(0.163 in)

4.14 mm

(0.163 in)

3.94 mm

(0.155 in)

4.15 mm

(0.164 in)

4.15 mm

(0.164 in)

4 mm

(0.157 in)

2

3

4

2

5

2

6

2

3

2

7

2

9

7

2

10

2

11

(2)

(3)

(4)

(5)

(6)

(5)

(7)

(5)

(8)

(2)

(9)

(5)

(10)

H32

H31

H36

H40

H35

H39

H34

H38

H37

H33

H30

H29

2 ASNA2536−3 NUT

BOLT

NUT

BOLT

NUT

RIVET

FR24

FWD

H44

H43

H42

H41

F G

G

N_SB_531285_5_BCAA_04_01

Figure A-FBCAA - Sheet 04

Removal/Installation of Fasteners

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 30

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

INFORMATION PARAGRAPH E.(2).

REFER TO TASK 531285−832−801−001.

MISSING FASTENERS AND/OR NO YES

REMOVE FASTENERS FROM HOLES 1 TO 44

REFER TO SUBTASK 531285−831−001−001

& RH SIDE. STGR18

AT THE THRESHOLD GIVEN IN THE PLANNING

REPORT RESULTS TO AIRBUS

NO CRACKS? YES

CONTACT AIRBUS FOR

FURTHER INSTRUCTION

DO A GENERAL VISUAL INSPECTION OF BETWEEN FR24 STGR17

SPLICE

DO A ROTOTEST INSPECTION OF ALL HOLES

REFER TO SUBTASK 531285−832−002−001

REINSTALL FASTENERS AND SPLICE

REFER TO SUBTASK 531285−831−002−001

NO FURTHER ACTION

NO FURTHER ACTION

REPORT RESULTS TO AIRBUS

QUESTION

ACTION

FINDING

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.

N_SB_531285_5_FAAA_01_01

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 31

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−53−1285

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES4

PAX DOORS − FUSELAGE (SA/LA) − WINDOWS −

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

E−mail: Structure.sbinspectionresult@airbus.com GENERAL VISUAL

SPECIAL DETAILED

INSPECTION

INSPECTION

MISSING FASTENERS AND/OR SPLICE ? YES NO

CRACK FOUND ON THE FASTENERS HOLES ? YES NO

HOLE NUMBER(S) FOUND WITH CRACK ?

MISSING FASTENERS AND SPLICE INSTALLED ? YES NO

CENTER WING BOX (SA/LA)

FAX +33 (0)5 61 93 36 14

N_SB_531285_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 32

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

STGR17

STGR18

FR24

VIEW LOOKING AFT

STGR18

FR24

E

STGR18

FR24

D

NOTE:

HOLE WITH FASTENER TO BE INSPECTED

HOLE WITHOUT FASTENER TO BE INSPECTED

H8 H16

H15

H6 H14

H7

H5

H4

H13

H12

H3

H2

H1

H11

H10

H9

H20

H19

H28

H27

H26

H25

H24

H23

H22

H21

H17

H18

H32

H31

H36

H40

H35

H39

H34

H38

H37

H33

H30

H29

F

G

FR24

FWD

H44

H43

H42

H41

G

N_SB_531285_5_RAAA_02_01

Figure A-FRAAA - Sheet 02

Inspection Report

DATE: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 33

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - MAIN STRUCTURE - INSPECTION FOR MISSING

FASTENERS AT FR24 BETWEEN STR17 & STR18

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: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

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: Jan 29/14 SERVICE BULLETIN No.: A320-53-1285

REVISION No.: 00 - Jan 29/14 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.