@A300-600

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.: A300-25-6217

REVISION No.: 00 - Aug 31/09 Page: 1

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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 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

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

AAW ABD AMU BKV CES CSN DLH F2I FDX IRA JAL KAC KAL

LAA MON MSR OHY QTR SUD TAR THA UZB

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

MANPOWER

Task 256217-831-801-001: Modification

TOTAL MANHOURS 2.50

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SERVICE BULLETIN

SUMMARY

Task 256217-831-801-001: Modification

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.: A300-25-6217

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@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

5MS

B C

4MS

Z210

A

D_SB_256217_5_SAAA_01_00

C

B

A

FR1

FR11

Figure A-FSAAA - Sheet 01

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

REVISION No.: 00 - Aug 31/09 Page: 4

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@A300-600

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

B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620

F4-605R

(2) Effectivity by MSN

0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358 0361

0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 0464 0477 0479 0505

0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563 0566 0569

0572 0575 0577 0579 0581-0582 0584 0601-0605 0607-0609 0611 0613-0614

0616-0618 0621 0623 0625 0627-0633 0635 0637 0641 0657 0659 0662 0664 0666

0668 0670 0673 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703

0705 0707 0709 0711 0713 0715 0717 0719 0721-0734 0737 0739-0741 0743-0744

0746-0747 0749-0750 0753-0756 0762-0764 0770 0773

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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

AAW 0354

ABD 0529 0557 0755

AMU 0677 0743

BKV 0411 0414 0546 0553 0608

CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763

CSN 0733 0734 0739 0750 0756 0762

DLH 0380 0401 0405 0408 0618 0623 0701 0773

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0341 0348 0351

FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559

0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664

0668 0688 0709 0713 0715 0726 0728

IRA 0632 0696 0723 0727

JAL 0602 0617 0621 0637 0641 0670 0679 0683 0703 0711 0724 0729

0730 0737 0740 0753 0770

KAC 0344 0673 0694 0699 0719 0721

KAL 0582 0609 0627 0631 0662 0685 0692 0731

LAA 0601 0616

MON 0540 0556 0604 0605

MSR 0561 0607

OHY 0584 0603 0744 0747 0749 0764

QTR 0554 0560 0614

SUD 0666

TAR 0505 0558 0563

THA 0368 0398 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705

UZB 0717 0722

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

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@A300-600

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348

0351 0354 0358 0361 0365 0368 0380 0388 0398 0401 0405

0408 0411 0414 0417 0464 0477 0479 0505 0518 0521 0525

0529 0530 0532 0536 0540 0543 0546 0553 0554 0555 0556

0557 0558 0559 0560 0561 0563 0566 0569 0572 0575 0577

0579 0581 0582 0584 0601 0602 0603 0604 0605 0607 0608

0609 0611 0613 0614 0616 0617 0618 0621 0623 0625 0627

0628 0629 0630 0631 0632 0633 0635 0637 0641 0657 0659

0662 0664 0666 0668 0670 0673 0677 0679 0681 0683 0685

0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711

0713 0715 0717 0719 0721 0722 0723 0724 0725 0726 0727

0728 0729 0730 0731 0732 0733 0734 0737 0739 0740 0741

0743 0744 0746 0747 0749 0750 0753 0754 0755 0756 0762

0763 0764 0770 0773

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

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.

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

REVISION No.: 00 - Aug 31/09 Page: 3

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@A300-600

SERVICE BULLETIN

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 256217-831-801-001: Modification

(1) Modify the captain seat 4MS

(2) Modify the first officer seat 5MS

E. COMPLIANCE

(1) Classification

MANDATORY

(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.

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

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SERVICE BULLETIN

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 256217-831-801-001: 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

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

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SERVICE BULLETIN

M. SPARES

None

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

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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

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This Page Intentionally Left Blank

DATE: Aug 31/09 SERVICE BULLETIN No.: A300-25-6217

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 256217-831-801-001 - 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 256217-839-001-001 - 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.: A300-25-6217

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B. PREPARATION

(1) Subtask 256217-941-001-001 - 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 256217-831-001-001 - 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 256217-831-002-001 - 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.: A300-25-6217

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

Bulletin No. 2510112-25-813.

D. TEST

(1) Subtask 256217-700-001-001 - 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 256217-942-001-001 - 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.: A300-25-6217

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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.: A300-25-6217

REVISION No.: 00 - Aug 31/09 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 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.: A300-25-6217

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