@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.

ATA SYSTEM: 22

TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF

RUDDER REVERSAL WARNING.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13591S22844

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 function has been developed in the Flight Control Computer (FCC) to

detect excessive pedal reversal inputs in order to trigger visual and aural warnings via Flight Warning

Computer (FWC).

This Service Bulletin is published to advise all operator of A300-600 aircraft of the issue of THALES

AVIONICS S.A. Service Bulletin No. B470ADM-22-006.

This Service Bulletin upgrades the two FCC PN B470ADM2 by new FCC PN B470ADM3 capable of

rudder reversal warning modified as per instructions given in the THALES AVIONICS S.A. Service

Bulletin No. B470ADM-22-006.

When Service Bulletin No. A300-22-6054, Service Bulletin No. A300-22-6055, Service Bulletin No.

A300-22-6056 and Service Bulletin No. A300-31-6140 are embodied, in case of excessive rudder pedal

reversal inputs, visual and aural warnings are triggered in the cockpit:

- The FWC provides audio "STOP RUDDER INPUT" messages.

- STOP rudder inputs lights are illuminated.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

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 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 FCCs

EFFECTIVITY

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

34Z 77T 83V AAL ABD AHK AIB AMU BCS CES F2I FDX G8E

GBG IRA IRM JAL KAC KAL MNB MON MSR MXU OHY QTR RUN

SUD TAR THA TMA UPS URS UZB

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. A300-22-6053 Mod. No. 13262S22684

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

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SERVICE BULLETIN

SUMMARY

MANPOWER

Task 226056-831-801-001: Modification of the two FCCs by replacement or by reprogramming

of their cards.

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

Additional manhours related to Vendor SB; refer to:

Modify the two FCCs (FINs 301CA1 and 301CA2). THALES AVIONICS S.A. Service

Bulletin No. B470ADM-22-006

Task 226056-831-802-001: Modification by replacement of the two FCCs.

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

APPENDICES

None

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR17

FR20

121BL

80VU

LH ELECTRONICS RACK

FCC1

FCC2

A

A

301CA1

301CA2

D_SB_226056_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 22

TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF

RUDDER REVERSAL WARNING.

MODIFICATION No.: 13591S22844

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This modification is applicable by Service Bulletin only.

(1) Models

B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R

F4-622R

(2) Effectivity by MSN

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0358 0361 0365 0380

0388 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470 0474 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 0602-0615 0617-0618 0621 0623

0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670

0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705

0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794

0797 0799-0841 0845-0878

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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

34Z 0685

77T 0838

83V 0423 0459 0460 0463 0466 0470 0474 0510 0511 0512 0615 0639

0675

AAL 0517 0612

ABD 0529 0557

AHK 0855 0856 0857 0858 0859 0860 0870 0871

AIB 0507 0508 0515

AMU 0677

BCS 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730 0737 0740

0753 0770

CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0461 0518

0606 0610 0645

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 0735 0736 0738 0742 0745

0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774

0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799

0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878

G8E 0462 0465 0469 0506 0509 0513 0514 0516

GBG 0626 0643

IRA 0632 0696 0723 0727

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

0750 0762 0773

JAL 0602 0617 0683 0783

KAC 0344 0673 0694 0699 0719 0721

KAL 0582 0609 0627 0631 0662 0692 0731

MNB 0734 0739 0755 0756 0758

MON 0540 0556 0604 0605

MSR 0561 0607

MXU 0767 0788 0797 0836 0837

OHY 0584 0603 0744 0747 0749 0764

QTR 0554 0560 0614

RUN 0743

SUD 0666 0775

TAR 0505 0558 0563

THA 0464 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785

0786 0787

TMA 0872

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SERVICE BULLETIN

OPERATOR MSN

UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816

0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 0845 0846

0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864

0865 0866 0867 0868 0869

URS 0733

UZB 0717 0722

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351

0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417

0423 0459 0460 0461 0462 0463 0464 0465 0466 0469 0470

0474 0477 0479 0505 0506 0507 0508 0509 0510 0511 0512

0513 0514 0515 0516 0517 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 0602 0603 0604 0605 0606 0607 0608 0609 0610 0611

0612 0613 0614 0615 0617 0618 0621 0623 0625 0626 0627

0628 0629 0630 0631 0632 0633 0635 0637 0639 0641 0643

0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 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

0735 0736 0737 0738 0739 0740 0741 0742 0743 0744 0745

0746 0747 0748 0749 0750 0752 0753 0754 0755 0756 0757

0758 0759 0760 0761 0762 0763 0764 0766 0767 0768 0769

0770 0771 0772 0773 0774 0775 0777 0778 0779 0780 0781

0782 0783 0784 0785 0786 0787 0788 0789 0790 0791 0792

0793 0794 0797 0799 0800 0801 0802 0803 0804 0805 0806

0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817

0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0836 0837 0838 0839

0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853

0854 0855 0856 0857 0858 0859 0860 0861 0862 0863 0864

0865 0866 0867 0868 0869 0870 0871 0872 0873 0874 0875

0876 0877 0878

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.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

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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. A300-22-6053 Mod. No. 13262S22684

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 function has been developed in the Flight Control

Computer (FCC) to detect excessive pedal reversal inputs in order to trigger visual and

aural warnings via Flight Warning Computer (FWC).

(2) Objective/Action

This Service Bulletin is published to advise all operator of A300-600 aircraft of the issue

of THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006.

This Service Bulletin upgrades the two FCC PN B470ADM2 by new FCC PN B470ADM3

capable of rudder reversal warning modified as per instructions given in the THALES

AVIONICS S.A. Service Bulletin No. B470ADM-22-006.

(3) Advantages

When Service Bulletin No. A300-22-6054, Service Bulletin No. A300-22-6055, Service

Bulletin No. A300-22-6056 and Service Bulletin No. A300-31-6140 are embodied, in

case of excessive rudder pedal reversal inputs, visual and aural warnings are triggered

in the cockpit:

- The FWC provides audio "STOP RUDDER INPUT" messages.

- STOP rudder inputs lights are illuminated.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, you have two possibilities:

- either you modify the two FCCs by replacement or by reprogramming

their cards as described in TASK 226056-831-801 001 Modification of the

two FCCs by replacement or by reprogramming of their cards.

- or you replace them as described in TASK 226056-831-802 001

Modification by replacement of the two FCCs.

To accomplish this Service Bulletin it is necessary to :

Task 226056-831-801-001: Modification of the two FCCs by replacement or by

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SERVICE BULLETIN

reprogramming of their cards.

(1) In the LH electronics rack 80VU, remove the two FCCs (FINs 301CA1 and 301CA2).

(2) Modify the two FCCs (FINs 301CA1 and 301CA2).

(3) In the LH electronics rack 80VU, install the two FCCs (FINs 301CA1 and 301CA2).

Task 226056-831-802-001: Modification by replacement of the two FCCs.

(1) In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2).

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 226056-831-801-001: Modification of the two FCCs by replacement or by reprogramming

of their cards.

Get Access 1.00

On Aircraft

In the LH electronics rack 80VU, remove the two FCCs

(FINs 301CA1 and 301CA2).

1.00

In the LH electronics rack 80VU, install the two FCCs

(FINs 301CA1 and 301CA2).

1.00

Tests 1.00

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Task 226056-831-801-001: Modification of the two FCCs by replacement or by reprogramming

of their cards.

Close-Up 1.00

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

Additional manhours related to Vendor SB; refer to:

Modify the two FCCs (FINs 301CA1 and 301CA2). THALES AVIONICS S.A. Service

Bulletin No. B470ADM-22-006

Task 226056-831-802-001: Modification by replacement of the two FCCs.

Get Access 1.00

On Aircraft

In the LH electronics rack 80VU, replace the two FCCs

(FINs 301CA1 and 301CA2).

2.00

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 22-18-34 24-00-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A300-22-6053

A300-22-6054

A300-22-6055

A300-22-6056

A300-31-6140

Vendor Service Bulletin (VSB) THALES AVIONICS S.A. Service

Bulletin No. B470ADM-22-006

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 22-18-08

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FCC B470ADM2 B470ADM3 03 NO (1)

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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 FCC has to be done

simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph 3.C

of this Service Bulletin.

M. SPARES

FCC B470ADM2

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This Page Intentionally Left Blank

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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

B470ADM3 2 FCC B470ADM2 03

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

Common Support Data Dictionary (CSDD), Chapter 2.

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 226056-831-801-001 - Modification of the two FCCs by replacement or by

reprogramming of their cards.

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.

NOTE: This Task concerns the modification of the FCCs by replacement or by

reprogramming their cards.

Task Associated Data

Zone

120

Modified FIN

301CA1 301CA2

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

Additional manhours related to Vendor SB; refer to:

THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006

A. GENERAL

(1) Subtask 226056-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

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B. PREPARATION

(1) Subtask 226056-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

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 in position below the door 121BL and the door 831 or 841.

(c) Open the door 121BL and the door 831 or 841.

(d) Do the Job Set-Up as specified in the removal/installation of the FCCs (FINs

301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

C. PROCEDURE

(1) Subtask 226056-020-001-002 - In the LH electronics rack 80VU, remove the two

FCCs (FINs 301CA1 and 301CA2).

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

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

(a) Remove the two FCCs (FINs 301CA1 and 301CA2):

Refer to AMM 22-18-34, Page Block 401

FIN 301CA1

1 FCC B470ADM2

and

FIN 301CA2

1 FCC B470ADM2

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(2) Subtask 226056-831-001-001 - Modify the two FCCs (FINs 301CA1 and 301CA2).

References

Vendor Service Bulletin (VSB) THALES AVIONICS S.A. B470ADM-22-006

(a) Modify the two FCCs (FINs 301CA1 and 301CA2) (Refer to THALES AVIONICS

S.A. Service Bulletin No. B470ADM-22-006).

(3) Subtask 226056-420-001-001 - In the LH electronics rack 80VU, install the two

FCCs (FINs 301CA1 and 301CA2).

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

B470ADM3 2 FCC

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

(a) Install the two FCCs (FINs 301CA1 and 301CA2):

Refer to AMM 22-18-34, Page Block 401

FIN 301CA1

1 FCC B470ADM3

and

FIN 301CA2

1 FCC B470ADM3

D. TEST

(1) Subtask 226056-700-001-001 - Test

Work Zones and Access Panels

Zone Access/Work location

120

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

(a) Job Set-Up:

1 Remove the safety clips and/or tags and close/unlock the circuit breakers as

specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer

to AMM 22-18-34, Page Block 401).

(b) Procedure:

1 Do the test procedure as specified after the installation of the FCCs (FINs

301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

E. CLOSE-UP

(1) Subtask 226056-942-001-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

120

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-18-34, 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 removal/installation of the FCCs

(FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

(c) Close the access doors.

(d) Remove the access platform(s).

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

DATE: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 14

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SERVICE BULLETIN

Task 226056-831-802-001 - Modification by replacement of the two FCCs.

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.

NOTE: This Task concerns the replacement of the two FCCs.

Task Associated Data

Zone

120

Modified FIN

301CA1 301CA2

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

A. GENERAL

(1) Subtask 226056-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 226056-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 15

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

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 in position below the door 121BL and the door 831 or 841.

(c) Open the door 121BL and the door 831 or 841.

(d) Do the Job Set-Up as specified in the removal/installation of the FCCs (FINs

301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

C. PROCEDURE

(1) Subtask 226056-960-001-001 - In the LH electronics rack 80VU, replace the two

FCCs (FINs 301CA1 and 301CA2).

Work Zones and Access Panels

Zone Access/Work location

120

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

B470ADM3 2 FCC

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

(a) Remove the two FCCs (FINs 301CA1 and 301CA2):

Refer to AMM 22-18-34, Page Block 401

FIN 301CA1

1 FCC B470ADM2

and

FIN 301CA2

1 FCC B470ADM2

DATE: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 16

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@A300-600

SERVICE BULLETIN

(b) Install the two FCCs (FINs 301CA1 and 301CA2):

Refer to AMM 22-18-34, Page Block 401

FIN 301CA1

1 FCC B470ADM3

and

FIN 301CA2

1 FCC B470ADM3

D. TEST

(1) Subtask 226056-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

(a) Job Set-Up:

1 Remove the safety clips and/or tags and close/unlock the circuit breakers as

specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer

to AMM 22-18-34, Page Block 401).

(b) Procedure:

1 Do the test procedure as specified after the installation of the FCCs (FINs

301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

E. CLOSE-UP

(1) Subtask 226056-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 22-18-34, 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 removal/installation of the FCCs

(FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

(c) Close the access doors.

(d) Remove the access platform(s).

DATE: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 17

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@A300-600

SERVICE BULLETIN

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

DATE: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 18

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@A300-600

SERVICE BULLETIN

REPORTING SHEET

TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF

RUDDER REVERSAL WARNING.

MODIFICATION No.: 13591S22844

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: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 1

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@A300-600

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: Apr 25/12 SERVICE BULLETIN No.: A300-22-6056

REVISION No.: 00 - Apr 25/12 Page: 1

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