@A310

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: 25

TITLE: EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT SEATS -

INSTALL ENLARGED SHIM FOR HORIZONTAL SWITCH ACTUATION

MODIFICATION No.: 13500S22802

This page transmits Revision No.01 of Service Bulletin No.A310-25-2205

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision 01 issued to add MSN 0367 and 0372 in the effectivity.

CHANGES

SUMMARY

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

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

No previous revision

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Aug 31/09

REVISION No. : 01 - Nov 19/10

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

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: 25

TITLE: EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT SEATS -

INSTALL ENLARGED SHIM FOR HORIZONTAL SWITCH ACTUATION

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13500S22802

MINOR None

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Powered captain and first officer seats are equipped with an actuator for the horizontal displacement

limited by an end switch, which detects the end seat displacement and stops the actuator thanks to a

cam detecting device.

An A300-600 aircraft operator reported that during take-off roll, the first officer seat PN 2510113-05-14,

manufactured by SOGERMA, slid back by itself to the end stop position. Command was transferred to

the captain and flight continued uneventful.

As wide body model families can be installed with SOGERMA seats PN 2510113 and 2510112 series,

the above conditions might also exist on the model family addressed in the Service Bulletin.

This Service Bulletin is published to advise all operators of A310/A300-600 (or A300-600 ST) aircraft of

the issue of SOGERMA-SOCEA Service Bulletin No. 2510112-25-813.

This Service Bulletin requires to change the cam by a new larger one and the switch S4 bracket.

The reason of the seat slippage is due to the misalignment of an electrical stop switch that causes the

actuator failure.

The reason of this misalignment is due to a bad adjustment of the seat pan.

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

SUMMARY

An actuator failure of this kind will allow uncommanded longitudinal movements of the seat.

A potential seat movement during landing/take-off may cause inadvertent actions on control column,

pedals or throttles.

Accomplishment of this Service Bulletin will ensure a correct stopping of the actuator.

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

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

19U 52X 58X 82Z 83V 98W 99Y ACQ AFG AIB AIC BAF BBC

BLE CFC DAH DEC DGA F2I FDX G8E GAF HFY I2L IRA IRM

IYE JAB JAV K1P KAC KTC KYV KZU MGL MWA PIA QAF R1T

RJA ROT RZO SBI SGX SUD THY TSC UZB WHT WTJ

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 NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

SUMMARY

MANPOWER

Task 252205-831-801-001: Modification

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the captain seat 4MS SOGERMA-SOCEA Service Bulletin

No. 2510112-25-813

Modify the first officer seat 5MS SOGERMA-SOCEA Service Bulletin

No. 2510112-25-813

APPENDICES

None

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z210

A

C

B

A

FR1

FR11

5MS

B C

4MS

B_SB_252205_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

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: 25

TITLE: EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT SEATS -

INSTALL ENLARGED SHIM FOR HORIZONTAL SWITCH ACTUATION

MODIFICATION No.: 13500S22802

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

310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324

310-325

(2) Effectivity by MSN

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260

0264 0267 0273 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320

0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360

0362 0364 0367 0369-0370 0372 0375 0378-0379 0386 0389-0390 0392 0394 0397

0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425 0427-0429 0431

0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473

0475-0476 0478 0480-0492 0494-0500 0502-0503 0519-0520 0522-0524 0526-0527

0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562 0564-0565

0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600 0620 0622

0624 0636 0638 0640 0642 0644 0646-0654 0656 0658 0660-0661 0663 0665 0667

0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691 0693 0697

0700

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

(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

19U 0399

52X 0410

58X 0431

82Z 0550 0551

83V 0427

98W 0672

99Y 0489

ACQ 0538 0544

AFG 0496 0497

AIB 0686

AIC 0392 0406 0407 0413 0428 0429 0654 0665 0669 0680

BAF 0367 0372

BBC 0594 0642 0700

BLE 0650 0674

CFC 0425 0441 0444 0446 0482

DAH 0291 0293

DEC 0684 0693 0697

DGA 0418 0421 0422

F2I 0309 0487

FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251

0254 0257 0260 0264 0267 0273 0281 0283 0288 0297 0303 0313

0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353

0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400 0439

0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542

0549 0552 0593 0638

G8E 0475

GAF 0434 0484 0498 0499 0503 0522 0523

HFY 0495 0565

I2L 0640

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0488 0537 0564 0586 0595

IYE 0568

JAB 0320 0419

JAV 0357 0481

K1P 0648

KAC 0647 0649 0663

KTC 0524 0567 0620

KYV 0386

KZU 0592 0622 0646

MGL 0526

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 2

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

OPERATOR MSN

MWA 0652

PIA 0473 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689

0691

QAF 0667

R1T 0591

RJA 0416 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

SBI 0486 0520

SGX 0519 0562

SUD 0437

THY 0476 0478 0480 0502

TSC 0447 0472 0483 0485 0527 0541 0545 0547 0588 0597 0599 0600

0658

UZB 0574 0576

WHT 0448 0573

WTJ 0494

(4) Configuration by MSN

MSN CONFIGURATION

0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248

0251 0254 0257 0260 0264 0267 0273 0281 0283 0288 0291

0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333

0335 0338 0339 0342 0343 0345 0346 0353 0355 0356 0357

0359 0360 0362 0364 0367 0369 0370 0372 0375 0378 0379

0386 0389 0390 0392 0394 0397 0399 0400 0406 0407 0410

0413 0416 0418 0419 0421 0422 0425 0427 0428 0429 0431

0434 0436 0437 0439 0441 0444 0445 0446 0447 0448 0449

0452 0454 0456 0457 0458 0467 0472 0473 0475 0476 0478

0480 0481 0482 0483 0484 0485 0486 0487 0488 0489 0490

0491 0492 0494 0495 0496 0497 0498 0499 0500 0502 0503

0519 0520 0522 0523 0524 0526 0527 0531 0534 0537 0538

0539 0541 0542 0544 0545 0547 0549 0550 0551 0552 0562

0564 0565 0567 0568 0571 0573 0574 0576 0585 0586 0587

0588 0590 0591 0592 0593 0594 0595 0597 0599 0600 0620

0622 0624 0636 0638 0640 0642 0644 0646 0647 0648 0649

0650 0651 0652 0653 0654 0656 0658 0660 0661 0663 0665

0667 0669 0671 0672 0674 0676 0678 0680 0682 0684 0686

0687 0689 0691 0693 0697 0700

001

(5) Configuration definition

**CONF 001

Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

None

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 3

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Powered captain and first officer seats are equipped with an actuator for the horizontal

displacement limited by an end switch, which detects the end seat displacement and

stops the actuator thanks to a cam detecting device.

An A300-600 aircraft operator reported that during take-off roll, the first officer seat PN

2510113-05-14, manufactured by SOGERMA, slid back by itself to the end stop position.

Command was transferred to the captain and flight continued uneventful.

As wide body model families can be installed with SOGERMA seats PN 2510113 and

2510112 series, the above conditions might also exist on the model family addressed in

the Service Bulletin.

(2) Objective/Action

This Service Bulletin is published to advise all operators of A310/A300-600 (or A300-600

ST) aircraft of the issue of SOGERMA-SOCEA Service Bulletin No. 2510112-25-813.

This Service Bulletin requires to change the cam by a new larger one and the switch S4

bracket.

The reason of the seat slippage is due to the misalignment of an electrical stop switch

that causes the actuator failure.

The reason of this misalignment is due to a bad adjustment of the seat pan.

An actuator failure of this kind will allow uncommanded longitudinal movements of the

seat.

A potential seat movement during landing/take-off may cause inadvertent actions on

control column, pedals or throttles.

(3) Advantages

Accomplishment of this Service Bulletin will ensure a correct stopping of the actuator.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 252205-831-801-001: Modification

(1) Modify the captain seat 4MS

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

(2) Modify the first officer seat 5MS

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is requested within 12 months after the issue

date of this Service Bulletin.

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

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

The AD must be used as the reference document for the mandatory accomplishment

timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA 21J.031.

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 252205-831-801-001: Modification

Get Access 1.00

Tests 0.50

Close-Up 1.00

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the captain seat 4MS SOGERMA-SOCEA Service Bulletin

No. 2510112-25-813

Modify the first officer seat 5MS SOGERMA-SOCEA Service Bulletin

No. 2510112-25-813

H. WEIGHT AND BALANCE

Not Changed

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 5

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 24-00-00 25-11-11 25-11-12

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

Vendor Service Bulletin (VSB) SOGERMA-SOCEA Service

Bulletin No. 2510112-25-813

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 25-11-01 25-11-11 25-11-12

25-11-21

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 6

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with SOGERMASOCEA as per instructions given in Service Bulletin No. 2510112-25-813.

(2) Price and Availability

Refer to the vendor Service Bulletin No. 2510112-25-813 for the equipment modification

sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin (VSB) for the industry support terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Refer to SOGERMA-SOCEA Service Bulletin No. 2510112-25-813.

F. TOOLING

None

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 7

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 8

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 252205-831-801-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS :

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

210

Modified FIN

4MS 5MS

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

SOGERMA-SOCEA Service Bulletin No. 2510112-25-813

A. GENERAL

(1) Subtask 252205-839-001-001 - 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: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 9

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

B. PREPARATION

(1) Subtask 252205-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position.

(c) Open, safety and tag this (these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

125VU SEATS/CAPT 1MS 502/J53

125VU SEATS/F/O 2MS 503/H53

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU SEATS/CAPT 1MS 326/J71

132VU SEATS/F/O 2MS 326/J74

C. PROCEDURE

(1) Subtask 252205-831-001-001 - Modify the captain seat 4MS

Work Zones and Access Panels

Zone Access/Work location

210

References

Vendor Service Bulletin (VSB) SOGERMA-SOCEA 2510112-25-813

(a) Modify the captain seat 4MS as described in SOGERMA-SOCEA Service Bulletin

No. 2510112-25-813.

(2) Subtask 252205-831-002-001 - Modify the first officer seat 5MS

Work Zones and Access Panels

Zone Access/Work location

210

References

Vendor Service Bulletin (VSB) SOGERMA-SOCEA 2510112-25-813

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 10

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

(a) Modify the first officer seat 5MS as described in SOGERMA-SOCEA Service

Bulletin No. 2510112-25-813.

D. TEST

(1) Subtask 252205-700-001-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-11, Page Block 501

25-11-12, Page Block 501

(a) Remove the safety clip(s) and tag(s) and close this (these) circuit breaker(s) :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

125VU SEATS/CAPT 1MS 502/J53

125VU SEATS/F/O 2MS 503/H53

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU SEATS/CAPT 1MS 326/J71

132VU SEATS/F/O 2MS 326/J74

(b) Procedure :

1 Do the Operational Test of the captain seat (Refer to AMM 25-11-11, Page

Block 501).

2 Do the Operational Test of the first officer seat (Refer to AMM 25-11-12, Page

Block 501).

E. CLOSE-UP

(1) Subtask 252205-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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

equipment.

(b) Restore the systems and the aircraft to normal operating conditions.

(c) Remove the access platform(s).

DATE: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 11

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

SERVICE BULLETIN

REPORTING SHEET

TITLE: EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT SEATS -

INSTALL ENLARGED SHIM FOR HORIZONTAL SWITCH ACTUATION

MODIFICATION No.: 13500S22802

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: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 1

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A310

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 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials 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: Aug 31/09 SERVICE BULLETIN No.: A310-25-2205

REVISION No.: 01 - Nov 19/10 Page: 1

5

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