@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.

ATA SYSTEM: 31

TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN

35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13590S22843 13634S22870

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

Following report of events of rapid alternating and large rudder pedal inputs that resulted in high vertical

stabilizer loads, a new Flight Warning Computer (FWC) standard S17 has been mainly developed

to generate the new "STOP RUDDER INPUTS" synthetic voice audio warning associated with the

detection of rudder reversal. This warning is generated by the Flight Control Computer (FCC).

This Service Bulletin is issued to inform all operators of A310 aircraft of the issue of AIRBUS FRANCE

Avionics and Simulation Products Service Bulletin No. 35-0B5-31-027.

The modification consists in upgrading two FWC standard S15 PN 35-0B5-3006-318 installed by Mod.

No. 13271S22526 (Service Bulletin No. A310-31-2135) in two FWC standard S17 PN 35-0B5-3008-320.

Accomplishment of this Service Bulletin primarily incorporates the following evolutions to FWC software:

- New synthetic voice "STOP RUDDER INPUTS":

The purpose of this alert is to inform pilots of excessive rudder pedal inputs at high airspeeds.

Conditions to generate this alert are triggered by the FCC.

NOTE: When Service Bulletin No. A310-22-2063 Mod. No. 13592S22487, Service Bulletin No.

A310-22-2064 Mod. No. 13593S22853, Service Bulletin No. A310-22-2065 Mod. No.

13591S22844 and Service Bulletin No. A310-31-2144 Mod. No. 13590S22843 and

13634S22870 are embodied, in case of excessive rudder pedal reversal inputs, visual

and aural warnings are triggered in the cockpit.

Accomplishment of this Service Bulletin further incorporates the following evolutions to FWC software:

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 1

5

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

SERVICE BULLETIN

SUMMARY

- New Traffic Alert and Collision Avoidance System (TCAS) monitoring:

. Creation of two new amber ECAM cautions logics: "NAV ADC TCAS FAULT", "NAV ADC

TCAS STBY" and "* NAV ADC TCAS FAULT" secondary alert.

. Creation of a new status logic: "TCAS INOP".

. Provision for creation of a new memo by EFIS-Symbol Generator Units (SGU) ECAM: "TCAS

STBY".

The TCAS evolution requires the embodiment of a SGU ECAM standard W33. As a consequence,

"TCAS INSTALLED" hard pin program should not be activated while aircraft is not fitted with a SGU

ECAM able to support the display of TCAS messages.

- Modification of ’fuel consumption increase’ logic to cover spoiler failure cases.

- Improvement of FWC input test to avoid spurious fault triggering.

- ROM LU1 margin memory increase.

- Inhibition of the single chime associated to the "FUEL CTR TK L+R PUMPS LO PR" alert during

phase 3.

- Improvement of sound emission associated to the following ECAM alerts:

. "CONFIG SLATS NOT IN T.O CONFIG" and "CONFIG FLAPS NOT IN T.O CONFIG"

. "CONFIG SPD BRK NOT RETRACTED" and "CONFIG PITCH TRIM NOT IN T.O RANGE".

. "ELEC BAT 1(2)(3) OVHT".

. "FLT CTL FLAPS SYS 1+2 FAULT" and "FLT CTL FLAPS STUCK".

. "FLT CTL SLATS SYS 1+2 FAULT" and "FLT CTL SLATS STUCK".

. OVERSPEED red alerts.

The operational consequences of this Service Bulletin are the modification of the Flight Crew Operating

Manual (FCOM) and the Master Minimum Equipment List (MMEL).

NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17.

NOTE: For a full improvements description, refer to Modification Operational Impact (MOI)

No.13590 and 13634.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED YES

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 2

5

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

SERVICE BULLETIN

SUMMARY

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

disruptions.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB FWC

EFFECTIVITY

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

18T 19U 52X 58X 82Z 83V 85W 85Z 99Y AFG AIB AIC AMV

BAF BBC C9L CFC DAH DGA FDX G2X G8E GAF HFY HJI IRA

IRM IYE JAV K1P KAC KZU MGL PCA PIA QAF R1T RJA ROT

RZO SBI SGX THY TSC UBD UZB WHT

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s) or the equivalent production modification(s):

Service Bulletin No. A310-31-2135 Mod. No. 13271S22526

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 YES

OBRM NO

MANPOWER

Task 312144-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 3

5

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

SERVICE BULLETIN

SUMMARY

Task 312144-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

Modify the two FWCs (FINs 1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. 35-0B5-31-027

Task 312144-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and

1WW2) as per AMM.

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

APPENDICES

None

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 4

5

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

1WW1

1WW2

90VU

FR1

FR20

Z120

A

A

B_SB_312144_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 5

5

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

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 6

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

ATA SYSTEM: 31

TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN

35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING

MODIFICATION No.: 13590S22843 13634S22870

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: These modifications are applicable by Service Bulletin only.

(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 0278 0281 0283 0288 0291 0293 0297 0303 0313 0316 0318 0326

0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362

0364 0367 0369-0370 0372 0375 0378-0379 0389-0390 0392 0394 0397 0399-0400

0406-0407 0410 0413 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

0480-0485 0488-0492 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 0642 0644 0646-0654 0656 0658 0660-0661 0663 0667 0669 0671-0672 0674

0676 0678 0682 0684 0686-0687 0689 0691 0693 0697 0700 0702 0704 0706

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 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

18T 0473

19U 0399

52X 0410

58X 0431

82Z 0550 0551

83V 0427

85W 0684 0693 0697

85Z 0547

99Y 0489

AFG 0496 0497

AIB 0650 0686

AIC 0392 0406 0407 0428 0429 0538 0544 0654 0669

AMV 0437

BAF 0367 0372

BBC 0594 0642 0700

C9L 0652

CFC 0425 0441 0444 0446 0482

DAH 0291 0293

DGA 0418 0421 0422

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

0254 0257 0260 0264 0267 0273 0278 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

G2X 0573

G8E 0475

GAF 0434 0484 0498 0499 0503 0522 0523

HFY 0495 0565

HJI 0413

IRA 0338 0370 0375 0379 0389 0390 0436 0671

IRM 0488 0524 0537 0564 0567 0586 0595 0620

IYE 0568 0702 0704

JAV 0357 0481

K1P 0648

KAC 0647 0649 0663

KZU 0592 0622 0646

MGL 0526

PCA 0419

PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 2

5

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

SERVICE BULLETIN

OPERATOR MSN

QAF 0667

R1T 0591

RJA 0445 0490 0491 0531

ROT 0636 0644

RZO 0571 0624 0651 0661

SBI 0520

SGX 0519 0562

THY 0476 0478 0480 0502

TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658

UBD 0672 0674

UZB 0574 0576 0706

WHT 0448 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 0278 0281 0283 0288

0291 0293 0297 0303 0313 0316 0318 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 0389

0390 0392 0394 0397 0399 0400 0406 0407 0410 0413 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 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 0642

0644 0646 0647 0648 0649 0650 0651 0652 0653 0654 0656

0658 0660 0661 0663 0667 0669 0671 0672 0674 0676 0678

0682 0684 0686 0687 0689 0691 0693 0697 0700 0702 0704

0706

001

(5) Configuration definition

**CONF 001

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

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 3

5

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

SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin(s) or the equivalent production modification(s):

Service Bulletin No. A310-31-2135 Mod. No. 13271S22526

C. REASON

(1) History

Following report of events of rapid alternating and large rudder pedal inputs that resulted

in high vertical stabilizer loads, a new Flight Warning Computer (FWC) standard S17

has been mainly developed to generate the new "STOP RUDDER INPUTS" synthetic

voice audio warning associated with the detection of rudder reversal. This warning is

generated by the Flight Control Computer (FCC).

(2) Objective/Action

This Service Bulletin is issued to inform all operators of A310 aircraft of the issue of

AIRBUS FRANCE Avionics and Simulation Products Service Bulletin No. 35-0B5-31-027.

The modification consists in upgrading two FWC standard S15 PN 35-0B5-3006-318

installed by Mod. No. 13271S22526 (Service Bulletin No. A310-31-2135) in two FWC

standard S17 PN 35-0B5-3008-320.

(3) Advantages

Accomplishment of this Service Bulletin primarily incorporates the following evolutions to

FWC software:

- New synthetic voice "STOP RUDDER INPUTS":

The purpose of this alert is to inform pilots of excessive rudder pedal inputs at high

airspeeds.

Conditions to generate this alert are triggered by the FCC.

NOTE: When Service Bulletin No. A310-22-2063 Mod. No. 13592S22487,

Service Bulletin No. A310-22-2064 Mod. No. 13593S22853, Service

Bulletin No. A310-22-2065 Mod. No. 13591S22844 and Service Bulletin

No. A310-31-2144 Mod. No. 13590S22843 and 13634S22870 are

embodied, in case of excessive rudder pedal reversal inputs, visual and

aural warnings are triggered in the cockpit.

Accomplishment of this Service Bulletin further incorporates the following evolutions to

FWC software:

- New Traffic Alert and Collision Avoidance System (TCAS) monitoring:

. Creation of two new amber ECAM cautions logics: "NAV ADC TCAS FAULT",

"NAV ADC TCAS STBY" and "* NAV ADC TCAS FAULT" secondary alert.

. Creation of a new status logic: "TCAS INOP".

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 4

5

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

SERVICE BULLETIN

. Provision for creation of a new memo by EFIS-Symbol Generator Units (SGU)

ECAM: "TCAS STBY".

The TCAS evolution requires the embodiment of a SGU ECAM standard W33. As

a consequence, "TCAS INSTALLED" hard pin program should not be activated

while aircraft is not fitted with a SGU ECAM able to support the display of TCAS

messages.

- Modification of ’fuel consumption increase’ logic to cover spoiler failure cases.

- Improvement of FWC input test to avoid spurious fault triggering.

- ROM LU1 margin memory increase.

- Inhibition of the single chime associated to the "FUEL CTR TK L+R PUMPS LO PR"

alert during phase 3.

- Improvement of sound emission associated to the following ECAM alerts:

. "CONFIG SLATS NOT IN T.O CONFIG" and "CONFIG FLAPS NOT IN T.O

CONFIG"

. "CONFIG SPD BRK NOT RETRACTED" and "CONFIG PITCH TRIM NOT IN

T.O RANGE".

. "ELEC BAT 1(2)(3) OVHT".

. "FLT CTL FLAPS SYS 1+2 FAULT" and "FLT CTL FLAPS STUCK".

. "FLT CTL SLATS SYS 1+2 FAULT" and "FLT CTL SLATS STUCK".

. OVERSPEED red alerts.

(4) Operational/Maintenance Consequences

The operational consequences of this Service Bulletin are the modification of the Flight

Crew Operating Manual (FCOM) and the Master Minimum Equipment List (MMEL).

NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17.

NOTE: For a full improvements description, refer to Modification Operational

Impact (MOI) No.13590 and 13634.

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, two possibilities are available:

- Either modify the two FWCs (FINs 1WW1 and 1WW2) as described in

TASK 312144-831-801 001 Modification of the two FWCs (FINs 1WW1

and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No.

35-0B5-31-027.

- Or replace them as described in TASK 312144-831-802 001 Modification

by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM.

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 5

5

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

SERVICE BULLETIN

To accomplish this Service Bulletin it is necessary to :

Task 312144-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by

Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

(1) In the Electronics Rack 90VU, remove the two FWCs (FINs 1WW1 and 1WW2).

(2) Modify the two FWCs (FINs 1WW1 and 1WW2).

(3) In the Electronics Rack 90VU, install the two FWCs (FINs 1WW1 and 1WW2).

Task 312144-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and

1WW2) as per AMM.

(1) In the Electronics Rack 90VU, replace the two FWCs (FINs 1WW1 and 1WW2).

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

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.

Task 312144-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

Get Access 0.50

On Aircraft

In the Electronics Rack 90VU, remove the two FWCs

(FINs 1WW1 and 1WW2).

0.50

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 6

5

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

SERVICE BULLETIN

Task 312144-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

In the Electronics Rack 90VU, install the two FWCs

(FINs 1WW1 and 1WW2).

0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

Modify the two FWCs (FINs 1WW1 and 1WW2). AIRBUS FRANCE SAS Service

Bulletin No. 35-0B5-31-027

Task 312144-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and

1WW2) as per AMM.

Get Access 0.50

On Aircraft

In the Electronics Rack 90VU, replace the two FWCs

(FINs 1WW1 and 1WW2).

1.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

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

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Modification Operational Impact (MOI) 13590

13634

Service Bulletin (SB) A310-31-2135

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service

Bulletin No. 35-0B5-31-027

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM)

Illustrated Parts Catalog (IPC) 31-53-08

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 7

5

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

SERVICE BULLETIN

Master Minimum Equipment List (MMEL)

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in

advance, in case you need your operational documentation to be amended by a revision prior

to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to :

SEDOR4 - AIRBUS Customer Services Technical Data

Fax No.: (33) 5 61 93 28 06

E-mail: sb.reporting@airbus.com

SB Reporting service is accessible on-line through AIRBUSWorld from :

My on-line services’ section, available on all AIRBUSWorld pages.

The Maintenance and Engineering Community, in :

- Modify and Upgrade page,

- Access SB and VSB section.

These amendments will be confirmed by the next normal revision of operational

documentation, once your Service Bulletin accomplishment report has been sent, as usual, to

our Customer Services Aircraft In-Service Data (SEDOR4).

NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17.

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FWC 35-0B5-3008-318 35-0B5-3008-320 03 NO (1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Mixability not authorized. Replacement of the two old FWCs has to be done

as a set.

M. SPARES

FWC 35-0B5-3008-318

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 8

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

Equipment BFEA01 The material is included in the commercial

offer of the Letter Agreement, and as

such will be supplied by AIRBUS Upgrade

Services.

Airline Customers are requested to contact:

AIRBUS Upgrade Services

Attn KAM Manager

(2) Price and Availability

Sales terms must be agreed between the Customer and AIRBUS in accordance with the

RFC (or RFC/RMO) procedure in the framework of the Stop Rudder Inputs Warning

retrofit.

B. INDUSTRY SUPPORT INFORMATION

Refer to the paragraph: ’Price and Availability’.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

None

(3) Equipment

Equipment BFEA01

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

NOTES

35-0B5-3008-320 2 FWC 35-0B5-3008-318 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 9

5

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

SERVICE BULLETIN

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 10

5

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

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 312144-831-801-001 - Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

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

120

Modified FIN

1WW1 1WW2

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

Additional manhours related to Vendor SB; refer to:

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027

A. GENERAL

(1) Subtask 312144-839-001-001 - 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: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 11

5

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

SERVICE BULLETIN

B. PREPARATION

(1) Subtask 312144-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

31-53-34, Page Block 401

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

Block 301).

(b) Do the Job Set-up procedure as specified in the removal of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

C. PROCEDURE

(1) Subtask 312144-831-004-001 - In the Electronics Rack 90VU, remove the two FWCs

(FINs 1WW1 and 1WW2).

Work Zones and Access Panels

Zone Access/Work location

120

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

(a) Remove:

Refer to AMM 31-53-34, Page Block 401

FIN 1WW1

1 FWC 35-0B5-3008-318

and

FIN 1WW2

1 FWC 35-0B5-3008-318

(2) Subtask 312144-831-002-001 - Modify the two FWCs (FINs 1WW1 and 1WW2).

References

Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS 35-0B5-31-027

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 12

5

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

SERVICE BULLETIN

(a) Modify the two FWCs (FINs 1WW1 and 1WW2) as per instructions given in

AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027.

(3) Subtask 312144-831-003-001 - In the Electronics Rack 90VU, install the two FWCs

(FINs 1WW1 and 1WW2).

Work Zones and Access Panels

Zone Access/Work location

120

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

35-0B5-3008-320 2 FWC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

(a) Install:

Refer to AMM 31-53-34, Page Block 401

FIN 1WW1

1 FWC 35-0B5-3008-320

and

FIN 1WW2

1 FWC 35-0B5-3008-320

D. TEST

(1) Subtask 312144-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

(a) Remove the safety clips and/or tags and close/unlock the circuit breakers as

specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to

AMM 31-53-34, Page Block 401).

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 13

5

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

SERVICE BULLETIN

(b) Do the test procedure as specified after the installation of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

E. CLOSE-UP

(1) Subtask 312144-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

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

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 14

5

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

SERVICE BULLETIN

Task 312144-831-802-001 - Modification by replacement of the two FWCs (FINs 1WW1 and

1WW2) as per AMM.

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

120

Modified FIN

1WW1 1WW2

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

A. GENERAL

(1) Subtask 312144-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 312144-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 15

5

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

SERVICE BULLETIN

References

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

31-53-34, Page Block 401

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

Block 301).

(b) Do the Job Set-up procedure as specified in the removal of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

C. PROCEDURE

(1) Subtask 312144-831-005-001 - In the Electronics Rack 90VU, replace the two FWCs

(FINs 1WW1 and 1WW2).

Work Zones and Access Panels

Zone Access/Work location

120

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

35-0B5-3008-320 2 FWC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

(a) Remove:

Refer to AMM 31-53-34, Page Block 401

FIN 1WW1

1 FWC 35-0B5-3008-318

and

FIN 1WW2

1 FWC 35-0B5-3008-318

(b) Install:

Refer to AMM 31-53-34, Page Block 401

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 16

5

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

SERVICE BULLETIN

FIN 1WW1

1 FWC 35-0B5-3008-320

and

FIN 1WW1

1 FWC 35-0B5-3008-320

D. TEST

(1) Subtask 312144-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

(a) Remove the safety clips and/or tags and close/unlock the circuit breakers as

specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to

AMM 31-53-34, Page Block 401).

(b) Do the test procedure as specified after the installation of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

E. CLOSE-UP

(1) Subtask 312144-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401

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

equipment.

(b) Do the Close-up procedure as specified in the installation of the two FWCs (FINs

1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401).

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

DATE: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 17

5

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN

35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING

MODIFICATION No.: 13590S22843 13634S22870

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: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 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 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: May 04/12 SERVICE BULLETIN No.: A310-31-2144

REVISION No.: 00 - May 04/12 Page: 1

5

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