C @A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - INSPECTION

OF DEUTSCH DEFECTIVE MODULES NSA 937901M1604

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The manufacturer Deutsch has identified a manufacturing quality issue on some terminal modules

having standard Part Number NSA937901M1604 and date code 08-14 (corresponds manufacturing

date from the 31st March 2008 to the 04th April 2008) and 08-18 (corresponds manufacturing date from

the 28th March 2008 to the 02nd May 2008). This could result in the intermittent or the permanent loss

of the affected aircraft systems power supply and their related functions and possible terminal modules

overheating.

The Service Bulletin recommends to inspect some terminal modules FIN positions and to replace those

manufactured by Deutsch having the same Part Number.

The replacement of the potentially defective Deutsch terminal modules will prevent the possible

intermittent or permanent loss of the affected aircraft systems power supply, their related functions and

their potential overheating. This will restore the high aircraft systems reliability and avoid possible NO

GO flight conditions.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 002

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 003

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 004

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 005

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 006

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

**CONF 007

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 008

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

**CONF 009

MATERIAL PRICE INFORMATION TABLE

TYPE MATERIAL QUANTITY

PER A/C

PRICE PER

A/C (USD)

MAINPARTS

COMP Component

COMPA01

See SB See SB Module

EFFECTIVITY

**CONF ALL

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

60V 60X AAW ABY AFL AVA AXM BAW BER BKP CCA CES CSA

CSN CSZ DKH DLH EZY GOW IAC IGO JBU LAN QTR THY USA

VOI

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHERS None

NATURE OF THE WORK

AIRCRAFT YES

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 6.25

ELAPSED TIME (HOURS) 6.25

**CONF 002

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 9.50

ELAPSED TIME (HOURS) 7.75

**CONF 003

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 20.25

ELAPSED TIME (HOURS) 12.25

**CONF 004

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 10.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 4

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SERVICE BULLETIN

SUMMARY

**CONF 005

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 21.50

ELAPSED TIME (HOURS) 14.75

**CONF 006

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 28.50

ELAPSED TIME (HOURS) 14.00

**CONF 007

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 19.75

ELAPSED TIME (HOURS) 13.25

**CONF 008

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 16.25

ELAPSED TIME (HOURS) 11.25

**CONF 009

Task 921072-832-801-001: INSPECTION

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

Task 921072-833-801-001: REPAIR

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

APPENDICES

**CONF ALL

Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

**CONF ALL

N_SB_921072_5_SAAA_01_01

Z220

Z250

Z260

Z120

Z150

Z420

Z410

MODULE

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

Figure A-FSAAA - Sheet 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 8

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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: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - INSPECTION

OF DEUTSCH DEFECTIVE MODULES NSA 937901M1604

MODIFICATION No.: None

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

318-112 319-111 319-112 319-115 319-132 319-133 320-214 320-216

320-232 320-233 321-211 321-213 321-231

(2) Effectivity by MSN

3603 3605 3607 3610 3613 3615-3619 3622-3627 3629 3631-3634 3636 3639 3645

3647 3653 3655 3657 3660-3661 3663 3671 3675 3687 3689 3691 3694 3696 3700

3702 3704-3705

(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

60V 3632

60X 3617

AAW 3615 3657

ABY 3626

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OPERATOR MSN

AFL 3627 3631

AVA 3647 3691

AXM 3610

BAW 3607

BER 3661 3689 3700 3704

BKP 3694

CCA 3623 3653 3655

CES 3613 3639

CSA 3660

CSN 3645

CSZ 3696

DKH 3605

DLH 3625

EZY 3634 3675 3702

GOW 3616

IAC 3619 3687

IGO 3618

JBU 3622

LAN 3663 3671

QTR 3636

THY 3603

USA 3629 3633

VOI 3624 3705

(4) Configuration by MSN

MSN CONFIGURATION

3603 3605 3607 3610 3613 3615 3616 3617 3618 3619 3622

3624 3625 3626 3627 3629 3631 3632 3633 3634

001

3623 3636 002

3639 003

3645 004

3647 005

3653 3655 006

3657 3660 3661 3663 007

3671 008

3675 3687 3689 3691 3694 3696 3700 3702 3704 3705 009

(5) Configuration definition

**CONF 001

Conf. 001 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1 and 450VT2-2.

**CONF 002

Conf. 002 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2 and 7430VT32.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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**CONF 003

Conf. 003 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1156VT3, 1156VT5, 6701VT18, 7222VT10, 7430VT32 and

7506VT13.

**CONF 004

Conf. 004 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1156VT3, 1156VT5, 6701VT18, 7222VT10 and 7506VT13.

**CONF 005

Conf. 005 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1833VT69, 1837VT17, 1842VT3, 1846VT5, 1846VT16, 1890VT3,

7492VT22 and 7506VT13.

**CONF 006

Conf. 006 is valid for aircraft fitted with Deutsch modules, 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1833VT69, 1837VT17, 1842VT3, 1846VT5, 1846VT16, 1890VT3,

1156VT3, 1156VT5, 6701VT18, 7222VT10 and 7506VT13.

**CONF 007

Conf. 007 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1833VT69, 1837VT17, 1842VT3, 1846VT5, 1846VT16, 1890VT3

and 7506VT13.

**CONF 008

Conf. 008 is valid for aircraft fitted with Deutsch modules 450VT1-1, 450VT1-2,

450VT2-1, 450VT2-2, 1833VT69, 1837VT17, 1842VT3, 1846VT5, 1846VT16 and

1890VT3.

**CONF 009

Conf. 009 is valid for aircraft fitted with Deutsch modules 1833VT69, 1837VT17,

1842VT3, 1846VT5, 1846VT16 and 1890VT3.

(6) Material Effectivity

MATERIAL QTY PER A/C REMARK

Component COMPA01

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The manufacturer Deutsch has identified a manufacturing quality issue on some

terminal modules having standard Part Number NSA937901M1604 and date code 08-14

(corresponds manufacturing date from the 31st March 2008 to the 04th April 2008)

and 08-18 (corresponds manufacturing date from the 28th March 2008 to the 02nd

May 2008). This could result in the intermittent or the permanent loss of the affected

aircraft systems power supply and their related functions and possible terminal modules

overheating.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 3

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(2) Objective/Action

The Service Bulletin recommends to inspect some terminal modules FIN positions and to

replace those manufactured by Deutsch having the same Part Number.

(3) Advantages

The replacement of the potentially defective Deutsch terminal modules will prevent the

possible intermittent or permanent loss of the affected aircraft systems power supply,

their related functions and their potential overheating. This will restore the high aircraft

systems reliability and avoid possible NO GO flight conditions.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 921072-832-801-001: INSPECTION

(1) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change modules in Pylons

**CONF 002

Task 921072-832-801-001: INSPECTION

(1) Inspection of 7430VT32

(2) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7430VT32

(2) Change modules in Pylons

**CONF 003

Task 921072-832-801-001: INSPECTION

(1) Inspection of 7430VT32

(2) Inspection of 7222VT10

(3) Inspection of the 7506VT13

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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(4) Inspection of the 6701VT18

(5) Inspection of modules in Electronics Rack 103VU

(6) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7430VT32

(2) Change the module 7222VT10

(3) Change the module 7506VT13

(4) Change the module 6701VT18

(5) Change modules in Electronics Rack 103VU

(6) Change modules in Pylons

**CONF 004

Task 921072-832-801-001: INSPECTION

(1) Inspection of 7222VT10

(2) Inspection of the 7506VT13

(3) Inspection of the 6701VT18

(4) Inspection of modules in Electronics Rack 103VU

(5) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7222VT10

(2) Change the module 7506VT13

(3) Change the module 6701VT18

(4) Change modules in Electronics Rack 103VU

(5) Change modules in Pylons

**CONF 005

Task 921072-832-801-001: INSPECTION

(1) Inspection of the 7506VT13

(2) Inspection of the 7492VT22

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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(3) Inspection of modules in the Electronics Rack 80VU

(4) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7506VT13

(2) Change the module 7492VT22

(3) Change the modules in the Electronics Rack 80VU

(4) Change modules in Pylons

**CONF 006

Task 921072-832-801-001: INSPECTION

(1) Inspection of 7222VT10

(2) Inspection of the 7506VT13

(3) Inspection of the 6701VT18

(4) Inspection of the modules in Electronics Racks 80VU and 103VU

(5) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7222VT10

(2) Change the module 7506VT13

(3) Change the module 6701VT18

(4) Change the modules in Electronics Rack 80VU and 103VU

(5) Change modules in Pylons

**CONF 007

Task 921072-832-801-001: INSPECTION

(1) Inspection of the 7506VT13

(2) Inspection of modules in the Electronics Rack 80VU

(3) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the module 7506VT13

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 6

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(2) Change the modules in the Electronics Rack 80VU

(3) Change modules in Pylons

**CONF 008

Task 921072-832-801-001: INSPECTION

(1) Inspection of modules in the Electronics Rack 80VU

(2) Inspection of modules in Pylons

Task 921072-833-801-001: REPAIR

(1) Change the modules in the Electronics Rack 80VU

(2) Change modules in Pylons

**CONF 009

Task 921072-832-801-001: INSPECTION

(1) Inspection of modules in the Electronics Rack 80VU

Task 921072-833-801-001: REPAIR

(1) Change the modules in the Electronics Rack 80VU

**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED

(2) Accomplishment Timescale

It is recommended to accomplish this Service Bulletin before 600FH from the date of the

SB issuance.

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). It is anticipated that the AD will confirm the thresholds given above but

reference should be made to the AD for confirmation of the mandated accomplishment

timescale.

F. APPROVAL

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

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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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.

**CONF 001

Task 921072-832-801-001: INSPECTION

Get Access 0.50

On Aircraft

Inspection of modules in Pylons 1.00

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

Task 921072-833-801-001: REPAIR

Get Access 0.50

On Aircraft

Change modules in Pylons 4.00

Tests 1.25

Close-Up 0.50

TOTAL MANHOURS 6.25

ELAPSED TIME (HOURS) 6.25

**CONF 002

Task 921072-832-801-001: INSPECTION

Get Access 0.75

On Aircraft

Inspection of 7430VT32 0.25

Inspection of modules in Pylons 1.00

Close-Up 1.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

Get Access 0.75

On Aircraft

Change the module 7430VT32 1.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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Task 921072-833-801-001: REPAIR

Change modules in Pylons 4.00

Tests 2.75

Close-Up 1.00

TOTAL MANHOURS 9.50

ELAPSED TIME (HOURS) 7.75

**CONF 003

Task 921072-832-801-001: INSPECTION

Get Access 1.75

On Aircraft

Inspection of 7430VT32 0.25

Inspection of 7222VT10 0.25

Inspection of the 7506VT13 0.25

Inspection of the 6701VT18 0.25

Inspection of modules in Electronics Rack 103VU 0.50

Inspection of modules in Pylons 1.00

Close-Up 2.75

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

Get Access 1.75

On Aircraft

Change the module 7430VT32 1.00

Change the module 7222VT10 1.00

Change the module 7506VT13 1.00

Change the module 6701VT18 1.00

Change modules in Electronics Rack 103VU 2.00

Change modules in Pylons 4.00

Tests 5.75

Close-Up 2.75

TOTAL MANHOURS 20.25

ELAPSED TIME (HOURS) 12.25

**CONF 004

Task 921072-832-801-001: INSPECTION

Get Access 1.50

On Aircraft

Inspection of 7222VT10 0.25

Inspection of the 7506VT13 0.25

Inspection of the 6701VT18 0.25

Inspection of modules in Electronics Rack 103VU 0.50

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 9

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Task 921072-832-801-001: INSPECTION

Inspection of modules in Pylons 1.00

Close-Up 2.25

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

Get Access 1.50

On Aircraft

Change the module 7222VT10 1.00

Change the module 7506VT13 1.00

Change the module 6701VT18 1.00

Change modules in Electronics Rack 103VU 2.00

Change modules in Pylons 4.00

Tests 5.75

Close-Up 2.25

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 10.00

**CONF 005

Task 921072-832-801-001: INSPECTION

Get Access 1.25

On Aircraft

Inspection of the 7506VT13 0.25

Inspection of the 7492VT22 0.25

Inspection of modules in the Electronics Rack 80VU 1.50

Inspection of modules in Pylons 1.00

Close-Up 1.75

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

Get Access 1.25

On Aircraft

Change the module 7506VT13 1.00

Change the module 7492VT22 1.00

Change the modules in the Electronics Rack 80VU 6.00

Change modules in Pylons 4.00

Tests 6.50

Close-Up 1.75

TOTAL MANHOURS 21.50

ELAPSED TIME (HOURS) 14.75

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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**CONF 006

Task 921072-832-801-001: INSPECTION

Get Access 1.75

On Aircraft

Inspection of 7222VT10 0.25

Inspection of the 7506VT13 0.25

Inspection of the 6701VT18 0.25

Inspection of the modules in Electronics Racks 80VU

and 103VU

2.00

Inspection of modules in Pylons 1.00

Close-Up 2.50

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

Get Access 1.75

On Aircraft

Change the module 7222VT10 1.00

Change the module 7506VT13 1.00

Change the module 6701VT18 1.00

Change the modules in Electronics Rack 80VU and

103VU

8.00

Change modules in Pylons 4.00

Tests 9.25

Close-Up 2.50

TOTAL MANHOURS 28.50

ELAPSED TIME (HOURS) 14.00

**CONF 007

Task 921072-832-801-001: INSPECTION

Get Access 1.00

On Aircraft

Inspection of the 7506VT13 0.25

Inspection of modules in the Electronics Rack 80VU 1.50

Inspection of modules in Pylons 1.00

Close-Up 1.25

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 3.00

Task 921072-833-801-001: REPAIR

Get Access 1.00

On Aircraft

Change the module 7506VT13 1.00

Change the modules in the Electronics Rack 80VU 6.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 11

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Task 921072-833-801-001: REPAIR

Change modules in Pylons 4.00

Tests 6.50

Close-Up 1.25

TOTAL MANHOURS 19.75

ELAPSED TIME (HOURS) 13.25

**CONF 008

Task 921072-832-801-001: INSPECTION

Get Access 0.75

On Aircraft

Inspection of modules in the Electronics Rack 80VU 1.50

Inspection of modules in Pylons 1.00

Close-Up 0.75

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

Get Access 0.75

On Aircraft

Change the modules in the Electronics Rack 80VU 6.00

Change modules in Pylons 4.00

Tests 4.75

Close-Up 0.75

TOTAL MANHOURS 16.25

ELAPSED TIME (HOURS) 11.25

**CONF 009

Task 921072-832-801-001: INSPECTION

Get Access 0.25

On Aircraft

Inspection of modules in the Electronics Rack 80VU 1.50

Close-Up 0.25

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 921072-833-801-001: REPAIR

Get Access 0.25

On Aircraft

Change the modules in the Electronics Rack 80VU 6.00

Tests 3.50

Close-Up 0.25

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 12

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**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 21-26-00 22-96-00 22-97-00

24-38-51 26-12-00 31-50-00

31-60-00 33-13-00 33-14-00

54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 002

Aircraft Maintenance Manual (AMM) 21-26-00 22-96-00 22-97-00

24-38-51 25-23-42 26-12-00

31-50-00 31-60-00 33-13-00

33-14-00 33-21-00 33-51-00

54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 003

Aircraft Maintenance Manual (AMM) 21-26-00 22-96-00 22-97-00

24-38-51 25-23-41 25-23-42

25-52-00 25-55-11 26-12-00

31-50-00 31-60-00 33-13-00

33-14-00 33-21-00 33-51-00

35-23-00 52-41-00 54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 13

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**CONF 004

Aircraft Maintenance Manual (AMM) 21-26-00 22-96-00 22-97-00

24-38-51 25-23-41 25-23-42

25-52-00 25-55-11 26-12-00

31-50-00 31-60-00 33-13-00

33-14-00 33-21-00 33-51-00

35-23-00 52-41-00 54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 005

Aircraft Maintenance Manual (AMM) 05-21-20 21-26-00 22-61-00

22-96-00 22-97-00 24-38-51

25-23-42 25-52-00 25-55-11

26-12-00 27-14-00 27-22-00

27-93-00 27-94-00 31-50-00

31-60-00 33-13-00 33-14-00

52-41-00 54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 006

Aircraft Maintenance Manual (AMM) 05-21-20 21-26-00 22-61-00

22-96-00 22-97-00 24-38-51

25-23-41 25-23-42 25-52-00

25-55-11 26-12-00 27-14-00

27-22-00 27-93-00 27-94-00

31-50-00 31-60-00 33-13-00

33-14-00 33-21-00 33-51-00

35-23-00 52-41-00 54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 14

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**CONF 007

Aircraft Maintenance Manual (AMM) 05-21-20 21-26-00 22-61-00

22-96-00 22-97-00 24-38-51

25-52-00 25-55-11 26-12-00

27-14-00 27-22-00 27-93-00

27-94-00 31-50-00 31-60-00

33-13-00 33-14-00 52-41-00

54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 008

Aircraft Maintenance Manual (AMM) 05-21-20 21-26-00 22-61-00

22-96-00 22-97-00 24-38-51

26-12-00 27-14-00 27-22-00

27-93-00 27-94-00 31-50-00

31-60-00 33-13-00 33-14-00

52-41-00 54-52-11

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF 009

Aircraft Maintenance Manual (AMM) 05-21-20 21-26-00 22-61-00

22-96-00 22-97-00 24-38-51

27-14-00 27-22-00 27-93-00

27-94-00 31-50-00 31-60-00

33-13-00 33-14-00 52-41-00

Aircraft Wiring List (AWL)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-25-51 20-33-00 20-33-44

20-52-10 20-55-00

Standards Manual (SM)

**CONF ALL

K. PUBLICATION AFFECTED

None

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 15

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L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 005

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 006

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 16

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NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 007

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 008

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 009

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY REMARK

Module NSA937901M16-04 NSA937901M16-04 01 Not

Applicable

(1)

NOTE (1): For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF ALL

M. SPARES

None

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 17

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This Page Intentionally Left Blank

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 18

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Component COMPA01 Vendor parts are to be purchased from:

Connecteurs Electriques DEUTSCH

17 Rue Lavoisier

BP117

27091 EVREUX Cedex 9

(2) Price and Availability

Component COMPA01

Refer to the paragraph: ’Price and Availability’.

B. INDUSTRY SUPPORT INFORMATION

Refer to the paragraph: ’Price and Availability’.

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

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

operator’s agreed in-house warranty labor rate. Claims for labor allowance should be received

not later than 90 days after completion of the last affected warranted aircraft.

For those aircraft with findings further to inspection as per this Service Bulletin, AIRBUS

will provide the kits at no charge, and will credit the manhours for the correction at the

operator’s agreed in-house warranty labor rate for claims received not later than 90 days after

completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

Component COMPA01

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

NSA937901M16-04 MODULE NSA937901M16-04 01

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

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 19

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

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

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

correct part number to part number relationship.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 20

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 921072-832-801-001 - INSPECTION

Task Associated Data

**CONF 001

Zone 410 420

Modified FIN 450VT1 450VT2

Access Panel 414AR 424AR

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 1.00

**CONF 002

Zone 220 410 420

Modified FIN 450VT1 450VT2 7430VT32

Access Door 831

Panel 221BC 414AR 424AR

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.00

**CONF 003

Zone 120 150 220 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

6701VT18 7222VT10 7430VT32 7506VT13

Access Door 822 824 826 831 832

Panel 152DW 221BC 251LC 261BC 414AR

424AR

Manpower

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 3.00

**CONF 004

Zone 120 150 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

6701VT18 7222VT10 7506VT13

Access Door 822 824 826 831 832

Panel 152DW 251LC 261BC 414AR 424AR

Manpower

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 2.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 21

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**CONF 005

Zone 120 150 260 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

7492VT22 7506VT13

Access Door 824 826 832

Panel 152DW 261CC 414AR 424AR

Manpower

TOTAL MANHOURS 6.00

ELAPSED TIME (HOURS) 3.00

**CONF 006

Zone 120 150 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

1833VT69 1837VT17 1842VT3 1846VT5

1846VT16 1890VT3 6701VT18 7222VT10

7506VT13

Access Door 822 824 826 831 832

Panel 152DW 251LC 261BC 414AR 424AR

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 3.00

**CONF 007

Zone 120 150 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

7506VT13

Access Door 824 826

Panel 152DW 414AR 424AR

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 3.00

**CONF 008

Zone 120 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

Access Door 824

Panel 414AR 424AR

Manpower

TOTAL MANHOURS 4.00

ELAPSED TIME (HOURS) 2.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 22

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**CONF 009

Zone 120

Modified FIN 1833VT69 1837VT17 1842VT3 1846VT5

1846VT16 1890VT3

Access Door 824

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

A. GENERAL

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND 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. IF THERE IS CONTAMINATION, REFER TO ESPM

20-55-00.

**CONF 001

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 23

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**CONF 003

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 005

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 006

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 007

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 24

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**CONF 008

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 009

(1) Subtask 921072-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

**CONF 001

(1) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 002

(1) Subtask 921072-941-001-001 - Get access to 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Panel 221BC

Work location Electrical panel 2000VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 25

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-001

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 221BC (Refer to AMM Task 25-23-42-000-001 and to figure Fig.

A-FGAAA Sheet 01).

(2) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 003

(1) Subtask 921072-941-001-001 - Get access to 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Panel 221BC

Work location Electrical panel 2000VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-001

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Put the access platform in position.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 26

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(b) Open the passenger/crew door 831.

(c) Remove the panel 221BC (Refer to AMM Task 25-23-42-000-001 and to figure Fig.

A-FGAAA Sheet 01).

(2) Subtask 921072-941-002-001 - Get access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

(3) Subtask 921072-941-003-001 - Get access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 27

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(4) Subtask 921072-941-004-001 - Get access to 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

(5) Subtask 921072-941-008-003 - Get access to 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824, Door 822

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access door 822(Refer to AMM Task 52-41-00-010-002 and to figure Fig. AFBAAA Sheet 01).

(6) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 28

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References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 004

(1) Subtask 921072-941-002-001 - Get access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

(2) Subtask 921072-941-003-001 - Get access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 29

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(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(3) Subtask 921072-941-004-001 - Get access to 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

(4) Subtask 921072-941-008-003 - Get access to 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824, Door 822

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access door 822(Refer to AMM Task 52-41-00-010-002 and to figure Fig. AFBAAA Sheet 01).

(5) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 30

5

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 005

(1) Subtask 921072-941-003-001 - Get access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(2) Subtask 921072-941-005-001 - Get access to 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261CC

Work location Stringer 2LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGJAA Sheet 01 - Location of module 7492VT22

(a) Put the access platform in position.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 31

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(b) Open the passenger/crew door 832.

(c) Remove the panel 261CC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGJAA Sheet 01).

(3) Subtask 921072-941-007-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824 (Refer to AMM Task 52-41-00-010-002 and to figure

Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(4) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 32

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SERVICE BULLETIN

**CONF 006

(1) Subtask 921072-941-002-001 - Get access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

(2) Subtask 921072-941-003-001 - Get access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(3) Subtask 921072-941-004-001 - Get access to 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Panel 251LC

Work location Stringer 5LH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 33

5

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

(4) Subtask 921072-941-008-001 - Get access to Electronics Racks 80VU and 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824, Door 822

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access doors 824 and 822 (Refer to AMM Task 52-41-00-010-002 and to

figure Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(5) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 34

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SERVICE BULLETIN

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 007

(1) Subtask 921072-941-003-001 - Get access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(2) Subtask 921072-941-007-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824 (Refer to AMM Task 52-41-00-010-002 and to figure

Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 35

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SERVICE BULLETIN

(3) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 008

(1) Subtask 921072-941-007-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824 (Refer to AMM Task 52-41-00-010-002 and to figure

Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(2) Subtask 921072-941-009-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

420 Access to open Panel 424AR

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 36

5

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SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-052

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-052 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 009

(1) Subtask 921072-941-007-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824 (Refer to AMM Task 52-41-00-010-002 and to figure

Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

C. PROCEDURE

**CONF 001

(1) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 37

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 002

(1) Subtask 921072-832-001-001 - Inspection of 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Panel 221BC

Work location Electrical panel 2000VU

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Do the inspection of the Date Code for the module 7430VT32 (Refer to figures Fig.

A-FGAAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 38

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SERVICE BULLETIN

(2) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 003

(1) Subtask 921072-832-001-001 - Inspection of 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Panel 221BC

Work location Electrical panel 2000VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 39

5

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SERVICE BULLETIN

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Do the inspection of the Date Code for the module 7430VT32 (Refer to figures Fig.

A-FGAAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(2) Subtask 921072-832-002-001 - Inspection of 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Do the inspection of the Date Code for the module 7222VT10 (Refer to figures Fig.

A-FGCAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(3) Subtask 921072-832-003-001 - Inspection of the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 40

5

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C @A318/A319/A320/A321

SERVICE BULLETIN

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Do the inspection of the Date Code for the module 7506VT13 (Refer to figures Fig.

A-FGEAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(4) Subtask 921072-832-004-001 - Inspection of the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Do the inspection of the Date Code for the module 6701VT18 (Refer to figures Fig.

A-FGGAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(5) Subtask 921072-832-010-001 - Inspection of modules in Electronics Rack 103VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 41

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SERVICE BULLETIN

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA Sheet 01):

- 1156VT3

- 1156VT5

(b) For the Inspection Report, refer to Appendix 01

(6) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 42

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**CONF 004

(1) Subtask 921072-832-002-001 - Inspection of 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Do the inspection of the Date Code for the module 7222VT10 (Refer to figures Fig.

A-FGCAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(2) Subtask 921072-832-003-001 - Inspection of the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Do the inspection of the Date Code for the module 7506VT13 (Refer to figures Fig.

A-FGEAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 43

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SERVICE BULLETIN

(3) Subtask 921072-832-004-001 - Inspection of the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Do the inspection of the Date Code for the module 6701VT18 (Refer to figures Fig.

A-FGGAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(4) Subtask 921072-832-010-001 - Inspection of modules in Electronics Rack 103VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA Sheet 01):

- 1156VT3

- 1156VT5

(b) For the Inspection Report, refer to Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 44

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(5) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 005

(1) Subtask 921072-832-003-001 - Inspection of the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 45

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Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Do the inspection of the Date Code for the module 7506VT13 (Refer to figures Fig.

A-FGEAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(2) Subtask 921072-832-006-001 - Inspection of the 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261CC

Work location Stringer 2LH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGJAA Sheet 01 - Location of module 7492VT22

(a) Do the inspection of the Date Code for the module 7492VT22 (Refer to figuresFig.

A-FGJAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(3) Subtask 921072-832-007-001 - Inspection of modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 46

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Fig. A-FAAAA Sheet 01 - Flow Chart.

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA):

- 1833VT69

- 1842VT3

- 1846VT5

- 1846VT16

- 1837VT17

- 1890VT3

(b) For the Inspection Report, refer to Appendix 01

(4) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 47

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(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 006

(1) Subtask 921072-832-002-001 - Inspection of 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Panel 261BC

Work location Frame 66

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Do the inspection of the Date Code for the module 7222VT10 (Refer to figures Fig.

A-FGCAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(2) Subtask 921072-832-003-001 - Inspection of the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 48

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Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Do the inspection of the Date Code for the module 7506VT13 (Refer to figures Fig.

A-FGEAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(3) Subtask 921072-832-004-001 - Inspection of the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Do the inspection of the Date Code for the module 6701VT18 (Refer to figures Fig.

A-FGGAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

(4) Subtask 921072-832-008-001 - Inspection of the modules in Electronics Racks 80VU

and 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822, Door 824

Work location Electrical panel 103VU

Electrical panel 80VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 49

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Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Fig. A-FAAAA Sheet 01 - Flow Chart.

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA).

For modules in Electronics Rack 80VU:

- 1833VT69

- 1842VT3

- 1846VT5

- 1846VT16

- 1837VT17

- 1890VT3

For modules in Electronics Rack 103VU:

- 1156VT3

- 1156VT5

(b) For the Inspection Report, refer to Appendix 01

(5) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 50

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References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 007

(1) Subtask 921072-832-003-001 - Inspection of the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Do the inspection of the Date Code for the module 7506VT13 (Refer to figures Fig.

A-FGEAA Sheet 01 and Fig. A-FAAAA).

(b) For the Inspection Report, refer to Appendix 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 51

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(2) Subtask 921072-832-007-001 - Inspection of modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Fig. A-FAAAA Sheet 01 - Flow Chart.

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA):

- 1833VT69

- 1842VT3

- 1846VT5

- 1846VT16

- 1837VT17

- 1890VT3

(b) For the Inspection Report, refer to Appendix 01

(3) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 52

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References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 008

(1) Subtask 921072-832-007-001 - Inspection of modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Fig. A-FAAAA Sheet 01 - Flow Chart.

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA):

- 1833VT69

- 1842VT3

- 1846VT5

- 1846VT16

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 53

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- 1837VT17

- 1890VT3

(b) For the Inspection Report, refer to Appendix 01

(2) Subtask 921072-832-009-001 - Inspection of modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

References

Fig. A-FAAAA Sheet 01 - Flow Chart.

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBBAA Sheet 01 and Fig. A-FAAAA).

On Pylon 1:

- 450VT1-1

- 450VT1-2

On Pylon 2 for modules on :

- 450VT2-1

- 450VT2-2

(b) For the Inspection Report, refer to Appendix 01

**CONF 009

(1) Subtask 921072-832-007-001 - Inspection of modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 54

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills NON SPECIFIC

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Fig. A-FAAAA Sheet 01 - Flow Chart.

(a) Do the inspection of the Date Code for the following modules (Refer to figures Fig.

A-FBAAA Sheet 01 and Fig. A-FAAAA):

- 1833VT69

- 1842VT3

- 1846VT5

- 1846VT16

- 1837VT17

- 1890VT3

(b) For the Inspection Report, refer to Appendix 01

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

**CONF 004

None

**CONF 005

None

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 55

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**CONF 006

None

**CONF 007

None

**CONF 008

None

**CONF 009

None

E. CLOSE-UP

**CONF 001

(1) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 002

(1) Subtask 921072-942-001-001 - Close access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 56

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-001

(a) Install the access panel 221BC (Refer to AMM Task 25-23-42-400-001).

(2) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 003

(1) Subtask 921072-942-001-001 - Close access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-001

(a) Install the access panel 221BC (Refer to AMM Task 25-23-42-400-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 57

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(2) Subtask 921072-942-002-001 - Close the access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(3) Subtask 921072-942-003-001 - Close the access to the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(4) Subtask 921072-942-004-001 - Close the access to the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 58

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(5) Subtask 921072-942-009-001 - Close the access to the Electronics Rack 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002

(a) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(6) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 004

(1) Subtask 921072-942-002-001 - Close the access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 59

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References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(2) Subtask 921072-942-003-001 - Close the access to the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(3) Subtask 921072-942-004-001 - Close the access to the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

(4) Subtask 921072-942-009-001 - Close the access to the Electronics Rack 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 60

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(a) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(5) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 005

(1) Subtask 921072-942-003-001 - Close the access to the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(2) Subtask 921072-942-005-001 - Close the access to the 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261CC

Work location Stringer 2LH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 61

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261CC (Refer to AMM Task 25-23-42-400-002).

(3) Subtask 921072-942-007-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(4) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 62

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**CONF 006

(1) Subtask 921072-942-002-001 - Close the access to 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(2) Subtask 921072-942-003-001 - Close the access to the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(3) Subtask 921072-942-004-001 - Close the access to the 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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(4) Subtask 921072-942-008-001 - Close the access to Electronics Racks 80VU and 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822, Door 824

Work location Electrical panel 103VU

Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(c) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(5) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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**CONF 007

(1) Subtask 921072-942-003-001 - Close the access to the 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(2) Subtask 921072-942-007-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(3) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 65

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References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 008

(1) Subtask 921072-942-007-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(2) Subtask 921072-942-009-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 66

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**CONF 009

(1) Subtask 921072-942-007-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 67

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This Page Intentionally Left Blank

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 68

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Task 921072-833-801-001 - REPAIR

**CONF ALL

Task Associated Data

**CONF 001

Zone 410 420

Modified FIN 450VT1 450VT2

Access Panel 414AR 424AR

Manpower

TOTAL MANHOURS 6.25

ELAPSED TIME (HOURS) 6.25

**CONF 002

Zone 220 410 420

Modified FIN 450VT1 450VT2 7430VT32

Access Door 831

Panel 221BC 414AR 424AR

Manpower

TOTAL MANHOURS 9.50

ELAPSED TIME (HOURS) 7.75

**CONF 003

Zone 120 150 220 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

6701VT18 7222VT10 7430VT32 7506VT13

Access Door 822 826 831 832

Panel 152DW 221BC 251LC 261BC 414AR

424AR

Manpower

TOTAL MANHOURS 20.25

ELAPSED TIME (HOURS) 12.25

**CONF 004

Zone 120 150 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

6701VT18 7222VT10 7506VT13

Access Door 822 826 831 832

Panel 152DW 251LC 261BC 414AR 424AR

Manpower

TOTAL MANHOURS 18.50

ELAPSED TIME (HOURS) 10.00

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 69

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**CONF 005

Zone 120 150 260 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

7492VT22 7506VT13

Access Door 822 824 826 832

Panel 152DW 261CC 414AR 424AR

Manpower

TOTAL MANHOURS 21.50

ELAPSED TIME (HOURS) 14.75

**CONF 006

Zone 120 150 250 260 410 420

Modified FIN 450VT1 450VT2 1156VT3 1156VT5

1833VT69 1837VT17 1842VT3 1846VT5

1846VT16 1890VT3 6701VT18 7222VT10

7506VT13

Access Door 822 824 826 831 832

Panel 152DW 251LC 261BC 414AR 424AR

Manpower

TOTAL MANHOURS 28.50

ELAPSED TIME (HOURS) 14.00

**CONF 007

Zone 120 150 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

7506VT13

Access Door 822 824 826

Panel 152DW 414AR 424AR

Manpower

TOTAL MANHOURS 19.75

ELAPSED TIME (HOURS) 13.25

**CONF 008

Zone 120 410 420

Modified FIN 450VT1 450VT2 1833VT69 1837VT17

1842VT3 1846VT5 1846VT16 1890VT3

Access Door 822 824

Panel 414AR 424AR

Manpower

TOTAL MANHOURS 16.25

ELAPSED TIME (HOURS) 11.25

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 70

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**CONF 009

Zone 120

Modified FIN 1833VT69 1837VT17 1842VT3 1846VT5

1846VT16 1890VT3

Access Door 822 824

Manpower

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

A. GENERAL

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND 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. IF THERE IS CONTAMINATION, REFER TO ESPM

20-55-00.

**CONF 001

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 71

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(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 72

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**CONF 003

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 73

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(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 005

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 74

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**CONF 006

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 007

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 75

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(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 008

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 76

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**CONF 009

(1) Subtask 921072-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-00

20-33-44

(a) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(b) Do a continuity test of the modified wires.

(c) For the cable tie application and tooling, refer to ESPM 20-33-44 and ESPM

20-25-51.

(d) Before removing modules witch have to be changed, note the position of the

connected wires and/or control its connections with the Aircraft Wiring List (AWL).

(e) After installation of the modules, connect the wires in the position that you noted

before the removal or following the Aircraft Wiring List (AWL).

(2) Subtask 921072-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

**CONF 001

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 77

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(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 78

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**CONF 002

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-010-001 - Get access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 79

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References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-001

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 221BC (Refer to AMM Task 25-23-42-000-001 and to figure Fig.

A-FGAAA Sheet 01).

(3) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 003

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 80

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SERVICE BULLETIN

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-010-001 - Get access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-001

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 221BC (Refer to AMM Task 25-23-42-000-001 and to figure Fig.

A-FGAAA Sheet 01).

(3) Subtask 921072-941-011-001 - Get access to the module 7222VT10

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 81

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SERVICE BULLETIN

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

(4) Subtask 921072-941-012-001 - Get access to the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(5) Subtask 921072-941-013-001 - Get access to the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 82

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SERVICE BULLETIN

(6) Subtask 921072-941-009-001 - Get access to the Electronics Rack 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access door 822 (Refer to AMM Task 52-41-00-010-002 and to figure Fig. AFBAAA Sheet 01).

(7) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 004

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 83

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-011-001 - Get access to the module 7222VT10

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 84

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SERVICE BULLETIN

(3) Subtask 921072-941-012-001 - Get access to the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(4) Subtask 921072-941-013-001 - Get access to the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

(5) Subtask 921072-941-009-001 - Get access to the Electronics Rack 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 85

5

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C @A318/A319/A320/A321

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access door 822 (Refer to AMM Task 52-41-00-010-002 and to figure Fig. AFBAAA Sheet 01).

(6) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 005

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 86

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SERVICE BULLETIN

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-012-001 - Get access to the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 87

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SERVICE BULLETIN

(3) Subtask 921072-941-014-001 - Get access to the module 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261CC

Work location Stringer 2LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGJAA Sheet 01 - Location of module 7492VT22

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261CC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGJAA Sheet 01).

(4) Subtask 921072-941-016-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824.(Refer to AMM Task 52-41-00-010-002 and to figure Fig.

A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 88

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SERVICE BULLETIN

(5) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 006

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 89

5

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SERVICE BULLETIN

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-011-001 - Get access to the module 7222VT10

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-000-002

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

(a) Put the access platform in position.

(b) Open the passenger/crew door 832.

(c) Remove the panel 261BC (Refer to AMM Task 25-23-42-000-002 and to figure Fig.

A-FGCAA Sheet 01).

(3) Subtask 921072-941-012-001 - Get access to the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 90

5

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SERVICE BULLETIN

(4) Subtask 921072-941-013-001 - Get access to the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-000-001

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

(a) Put the access platform in position.

(b) Open the passenger/crew door 831.

(c) Remove the panel 251LC (Refer to AMM Task 25-23-41-000-001 and to figure Fig.

A-FGGAA Sheet 01).

(5) Subtask 921072-941-017-001 - Get access to Electronics Racks 80VU and 103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822, Door 824

Work location Electrical panel 80VU

Electrical panel 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open access doors 824 and 826 (Refer to AMM Task 52-41-00-010-002 and to

figure Fig. A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 91

5

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SERVICE BULLETIN

(6) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 007

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 92

5

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SERVICE BULLETIN

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-012-001 - Get access to the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-000-003

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

(a) Put the access platform in position.

(b) Open the door 826.

(c) Remove the panel 152DW (Refer to AMM Task 25-55-11-000-003 and to figure Fig.

A-FGEAA Sheet 01).

(3) Subtask 921072-941-016-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 93

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SERVICE BULLETIN

(b) Open the access door 824.(Refer to AMM Task 52-41-00-010-002 and to figure Fig.

A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(4) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 008

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 94

5

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C @A318/A319/A320/A321

SERVICE BULLETIN

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

(2) Subtask 921072-941-016-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824.(Refer to AMM Task 52-41-00-010-002 and to figure Fig.

A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(3) Subtask 921072-941-018-001 - Get access to modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 95

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References

Aircraft Maintenance Manual (AMM) Task 54-52-11-000-002

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

(a) Put the access platform in position.

(b) Remove skin panels 414AR and 424AR (Refer to AMM Task 54-52-11-000-002 and

to figure Fig. A-FBBAA Sheet 01).

**CONF 009

(1) Subtask 921072-941-019-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-000-001

(a) Make sure that the external connectors are not connected to the aircraft

receptacles EXT PW.

(b) Make sure that there are warning notices on external power receptacles to tell

persons not to connect an external power source.

(c) Make sure that the EMER EXIT LT pushbutton switch on 25VU is on OFF position.

(d) In the cockpit, on the overhead panel 35VU release BAT pushbutton switches.

(e) Put a warning notice on the panel 35VU to tell persons not to operate the batteries.

(f) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the

NORMAL BATTERY switch.

(g) Put a warning notice in the cockpit to tell persons not to start the APU.

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1 and the

ENG2.

(i) Disconnect the Batteries:

- for Job Set-up, refer to Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-000-001).

- turn the knurled nut a quarter turn

- disconnect the connectors

- put blanking caps on the disconnected electrical connectors.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 96

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SERVICE BULLETIN

(2) Subtask 921072-941-016-001 - Get access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-010-002

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

(a) Put the access platform in position.

(b) Open the access door 824.(Refer to AMM Task 52-41-00-010-002 and to figure Fig.

A-FBAAA Sheet 01).

(c) Remove the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

C. PROCEDURE

**CONF 001

(1) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 97

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References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 002

(1) Subtask 921072-912-001-001 - Change the module 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

Refer to figure Fig. A-FGAAA Sheet 01.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 98

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(a) Remove the faulty module :

FIN 7430VT32

1 Module NSA937901M16-04

(b) Install module:

FIN 7430VT32

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 99

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(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 003

(1) Subtask 921072-912-001-001 - Change the module 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGAAA Sheet 01 - Location of module 7430VT32

Refer to figure Fig. A-FGAAA Sheet 01.

(a) Remove the faulty module :

FIN 7430VT32

1 Module NSA937901M16-04

(b) Install module:

FIN 7430VT32

As

required

Module NSA937901M16-04

(2) Subtask 921072-900-001-001 - Change the module 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 100

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

Refer to figure Fig. A-FGCAA Sheet 01.

(a) Remove the faulty module :

FIN 7222VT10

1 Module NSA937901M16-04

(b) Install module:

FIN 7222VT10

As

required

Module NSA937901M16-04

(3) Subtask 921072-912-002-001 - Change the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 101

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References

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

Refer to figure Fig. A-FGEAA Sheet 01.

(a) Remove the faulty module :

FIN 7506VT13

1 Module NSA937901M16-04

(b) Install module:

FIN 7506VT13

As

required

Module NSA937901M16-04

(4) Subtask 921072-912-003-001 - Change the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

Refer to figure Fig. A-FGGAA Sheet 01.

(a) Remove the faulty module :

FIN 6701VT18

1 Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 102

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(b) Install module:

FIN 6701VT18

As

required

Module NSA937901M16-04

(5) Subtask 921072-912-009-001 - Change modules in Electronics Rack 103VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1156VT3

1 Module NSA937901M16-04

FIN 1156VT5

1 Module NSA937901M16-04

(b) Install modules:

FIN 1156VT3

As

required

Module NSA937901M16-04

FIN 1156VT5

As

required

Module NSA937901M16-04

(6) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 103

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Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 004

(1) Subtask 921072-900-001-001 - Change the module 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 104

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Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

Refer to figure Fig. A-FGCAA Sheet 01.

(a) Remove the faulty module :

FIN 7222VT10

1 Module NSA937901M16-04

(b) Install module:

FIN 7222VT10

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-002-001 - Change the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

Refer to figure Fig. A-FGEAA Sheet 01.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 105

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(a) Remove the faulty module :

FIN 7506VT13

1 Module NSA937901M16-04

(b) Install module:

FIN 7506VT13

As

required

Module NSA937901M16-04

(3) Subtask 921072-912-003-001 - Change the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

Refer to figure Fig. A-FGGAA Sheet 01.

(a) Remove the faulty module :

FIN 6701VT18

1 Module NSA937901M16-04

(b) Install module:

FIN 6701VT18

As

required

Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 106

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(4) Subtask 921072-912-009-001 - Change modules in Electronics Rack 103VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1156VT3

1 Module NSA937901M16-04

FIN 1156VT5

1 Module NSA937901M16-04

(b) Install modules:

FIN 1156VT3

As

required

Module NSA937901M16-04

FIN 1156VT5

As

required

Module NSA937901M16-04

(5) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 107

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Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 005

(1) Subtask 921072-912-002-001 - Change the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 108

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

Refer to figure Fig. A-FGEAA Sheet 01.

(a) Remove the faulty module :

FIN 7506VT13

1 Module NSA937901M16-04

(b) Install module:

FIN 7506VT13

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-004-001 - Change the module 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261CC

Work location Stringer 2LH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 109

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References

Fig. A-FGJAA Sheet 01 - Location of module 7492VT22

Refer to figure Fig. A-FGJAA Sheet 01.

(a) Remove the faulty module :

FIN 7492VT22

1 Module NSA937901M16-04

(b) Install module:

FIN 7492VT22

As

required

Module NSA937901M16-04

(3) Subtask 921072-912-006-001 - Change the modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 80VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1833VT69

1 Module NSA937901M16-04

FIN 1842VT3

1 Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 110

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FIN 1846VT5

1 Module NSA937901M16-04

FIN 1846VT16

1 Module NSA937901M16-04

FIN 1837VT17

1 Module NSA937901M16-04

FIN 1890VT3

1 Module NSA937901M16-04

(b) Install modules:

FIN 1833VT69

As

required

Module NSA937901M16-04

FIN 1842VT3

As

required

Module NSA937901M16-04

FIN 1846VT5

As

required

Module NSA937901M16-04

FIN 1846VT16

As

required

Module NSA937901M16-04

FIN 1837VT17

As

required

Module NSA937901M16-04

FIN 1890VT3

As

required

Module NSA937901M16-04

(4) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 111

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Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 006

(1) Subtask 921072-900-001-001 - Change the module 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 112

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Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGCAA Sheet 01 - Location of module 7222VT10

Refer to figure Fig. A-FGCAA Sheet 01.

(a) Remove the faulty module :

FIN 7222VT10

1 Module NSA937901M16-04

(b) Install module:

FIN 7222VT10

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-002-001 - Change the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

Refer to figure Fig. A-FGEAA Sheet 01.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 113

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(a) Remove the faulty module :

FIN 7506VT13

1 Module NSA937901M16-04

(b) Install module:

FIN 7506VT13

As

required

Module NSA937901M16-04

(3) Subtask 921072-912-003-001 - Change the module 6701VT18

Work Zones and Access Panels

Zone Access/Work location

250 Access to open Door 831

Panel 251LC

Work location Stringer 5LH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGGAA Sheet 01 - Location of module 6701VT18

Refer to figure Fig. A-FGGAA Sheet 01.

(a) Remove the faulty module :

FIN 6701VT18

1 Module NSA937901M16-04

(b) Install module:

FIN 6701VT18

As

required

Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 114

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(4) Subtask 921072-912-007-001 - Change the modules in Electronics Rack 80VU and

103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822, Door 824

Work location Electrical panel 103VU

Electrical panel 80VU

Manpower Resources

Manhours 8.00

Minimum number of person 1

Subtask elapsed time 8.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1833VT69

1 Module NSA937901M16-04

FIN 1842VT3

1 Module NSA937901M16-04

FIN 1846VT5

1 Module NSA937901M16-04

FIN 1846VT16

1 Module NSA937901M16-04

FIN 1837VT17

1 Module NSA937901M16-04

FIN 1890VT3

1 Module NSA937901M16-04

FIN 1156VT3

1 Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 115

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FIN 1156VT5

1 Module NSA937901M16-04

(b) Install modules:

FIN 1833VT69

As

required

Module NSA937901M16-04

FIN 1842VT3

As

required

Module NSA937901M16-04

FIN 1846VT5

As

required

Module NSA937901M16-04

FIN 1846VT16

As

required

Module NSA937901M16-04

FIN 1837VT17

As

required

Module NSA937901M16-04

FIN 1890VT3

As

required

Module NSA937901M16-04

FIN 1156VT3

As

required

Module NSA937901M16-04

FIN 1156VT5

As

required

Module NSA937901M16-04

(5) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 116

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Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 007

(1) Subtask 921072-912-002-001 - Change the module 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 117

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Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FGEAA Sheet 01 - Location of module 7506VT13

Refer to figure Fig. A-FGEAA Sheet 01.

(a) Remove the faulty module :

FIN 7506VT13

1 Module NSA937901M16-04

(b) Install module:

FIN 7506VT13

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-006-001 - Change the modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 80VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 118

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(a) Remove faulty modules :

FIN 1833VT69

1 Module NSA937901M16-04

FIN 1842VT3

1 Module NSA937901M16-04

FIN 1846VT5

1 Module NSA937901M16-04

FIN 1846VT16

1 Module NSA937901M16-04

FIN 1837VT17

1 Module NSA937901M16-04

FIN 1890VT3

1 Module NSA937901M16-04

(b) Install modules:

FIN 1833VT69

As

required

Module NSA937901M16-04

FIN 1842VT3

As

required

Module NSA937901M16-04

FIN 1846VT5

As

required

Module NSA937901M16-04

FIN 1846VT16

As

required

Module NSA937901M16-04

FIN 1837VT17

As

required

Module NSA937901M16-04

FIN 1890VT3

As

required

Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 119

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(3) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 008

(1) Subtask 921072-912-006-001 - Change the modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 80VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 120

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Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1833VT69

1 Module NSA937901M16-04

FIN 1842VT3

1 Module NSA937901M16-04

FIN 1846VT5

1 Module NSA937901M16-04

FIN 1846VT16

1 Module NSA937901M16-04

FIN 1837VT17

1 Module NSA937901M16-04

FIN 1890VT3

1 Module NSA937901M16-04

(b) Install modules:

FIN 1833VT69

As

required

Module NSA937901M16-04

FIN 1842VT3

As

required

Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 121

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FIN 1846VT5

As

required

Module NSA937901M16-04

FIN 1846VT16

As

required

Module NSA937901M16-04

FIN 1837VT17

As

required

Module NSA937901M16-04

FIN 1890VT3

As

required

Module NSA937901M16-04

(2) Subtask 921072-912-008-001 - Change modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBBAA Sheet 01 - Location of modules in Pylons

Refer to figure Fig. A-FBBAA Sheet 01.

(a) On Pylon 1, Remove faulty modules 450VT1-1 and 450VT1-2:

2 Module NSA937901M16-04

(b) On Pylon 1, Install modules 450VT1-1 and 450VT1-2:

As

required

Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 122

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(c) On Pylon 2, Remove faulty modules 450VT2-1 and 450VT2-2:

2 Module NSA937901M16-04

(d) On Pylon 2, Install modules 450VT2-1 and 450VT2-2:

As

required

Module NSA937901M16-04

**CONF 009

(1) Subtask 921072-912-006-001 - Change the modules in the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 80VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD

NSA937901M16-04 As required MODULE

References

Fig. A-FBAAA Sheet 01 - Location of modules in 80VU and

103VU

Refer to figure Fig. A-FBAAA Sheet 01.

(a) Remove faulty modules :

FIN 1833VT69

1 Module NSA937901M16-04

FIN 1842VT3

1 Module NSA937901M16-04

FIN 1846VT5

1 Module NSA937901M16-04

FIN 1846VT16

1 Module NSA937901M16-04

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 123

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FIN 1837VT17

1 Module NSA937901M16-04

FIN 1890VT3

1 Module NSA937901M16-04

(b) Install modules:

FIN 1833VT69

As

required

Module NSA937901M16-04

FIN 1842VT3

As

required

Module NSA937901M16-04

FIN 1846VT5

As

required

Module NSA937901M16-04

FIN 1846VT16

As

required

Module NSA937901M16-04

FIN 1837VT17

As

required

Module NSA937901M16-04

FIN 1890VT3

As

required

Module NSA937901M16-04

D. TEST

**CONF 001

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 124

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- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 125

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(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

**CONF 002

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 126

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References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-004-003 - Test of modules 7430VT32

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 33-21-00-710-001

Task 33-51-00-710-001

(a) Do the Operational Test of the general illumination (Refer to AMM Task

33-21-00-710-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 127

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(b) Do the Operational Test of emergency lights (Refer to AMM Task

33-51-00-710-001).

(4) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

**CONF 003

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 128

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References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-004-001 - Test of modules 7430VT32, 7222VT10 and 6701VT18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 33-21-00-710-001

Task 33-51-00-710-001

(a) Do the Operational Test of the general illumination (Refer to AMM Task

33-21-00-710-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 129

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(b) Do the Operational Test of emergency lights (Refer to AMM Task

33-51-00-710-001).

(4) Subtask 921072-710-005-003 - Test of modules 7506VT13

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-710-003

Task 25-52-00-710-004

Task 25-52-00-710-005

(a) Do the Operational Test of the proximity switches (Refer to AMM Task

25-52-00-710-003).

(b) Do the Operational Test of the Door Sill Latches in the FWD Cargo Compartment

(2004VU1 and 2004VU2) and in the AFT Cargo Compartment (2004VU3 and

2004VU4) (Refer to AMM Task 25-52-00-710-004).

(c) Do the Operational Test of the power drive units (Refer to AMM Task

25-52-00-710-005)

(5) Subtask 921072-710-007-001 - Test of modules in Electronics Rack 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 35-23-00-710-001

Task 35-23-00-720-002

(a) Do the Operational Check of manual mask release (Refer to AMM Task

35-23-00-710-001).

(b) Do the Functional Test of the passenger emergency-oxygen system (Refer to AMM

Task 35-23-00-720-002).

(6) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 130

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**CONF 004

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 131

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NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-004-004 - Test of modules 7222VT10 and 6701VT18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 33-21-00-710-001

Task 33-51-00-710-001

(a) Do the Operational Test of the general illumination (Refer to AMM Task

33-21-00-710-001).

(b) Do the Operational Test of emergency lights (Refer to AMM Task

33-51-00-710-001).

(4) Subtask 921072-710-005-003 - Test of modules 7506VT13

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-710-003

Task 25-52-00-710-004

Task 25-52-00-710-005

(a) Do the Operational Test of the proximity switches (Refer to AMM Task

25-52-00-710-003).

(b) Do the Operational Test of the Door Sill Latches in the FWD Cargo Compartment

(2004VU1 and 2004VU2) and in the AFT Cargo Compartment (2004VU3 and

2004VU4) (Refer to AMM Task 25-52-00-710-004).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 132

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(c) Do the Operational Test of the power drive units (Refer to AMM Task

25-52-00-710-005)

(5) Subtask 921072-710-007-001 - Test of modules in Electronics Rack 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 35-23-00-710-001

Task 35-23-00-720-002

(a) Do the Operational Check of manual mask release (Refer to AMM Task

35-23-00-710-001).

(b) Do the Functional Test of the passenger emergency-oxygen system (Refer to AMM

Task 35-23-00-720-002).

(6) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

**CONF 005

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 133

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- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 134

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(3) Subtask 921072-710-005-001 - Test of modules 7506VT13 and 7492VT22

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-710-003

Task 25-52-00-710-004

Task 25-52-00-710-005

(a) Do the Operational Test of the proximity switches (Refer to AMM Task

25-52-00-710-003).

(b) Do the Operational Test of the Door Sill Latches in the FWD Cargo Compartment

(2004VU1 and 2004VU2) and in the AFT Cargo Compartment (2004VU3 and

2004VU4) (Refer to AMM Task 25-52-00-710-004).

(c) Do the Operational Test of the power drive units (Refer to AMM Task

25-52-00-710-005)

(4) Subtask 921072-710-006-001 - Test of modules in Electronics Rack 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-61-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 27-14-00-710-001

Task 27-22-00-710-002

Task 27-93-00-710-001

Task 27-93-00-710-002

Task 27-94-00-710-002

Task 27-94-00-710-003

(a) Do the Operational Test of AFS (Refer to AMM Task 22-96-00-710-001).

(b) Do the Operational Test of the Rudder Travel Limiting Function (Refer to AMM

Task 22-61-00-710-001).

(c) Do the Operational Test of the Rudder Trim Actuation (Refer to AMM Task

27-22-00-710-002).

(d) Do the Operational Test of the Aileron and Hydraulic Actuation (Refer to AMM Task

27-14-00-710-001).

(e) Do the Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of

loss of Blue Hydraulic Pressure (to be done before revenue flight landing gear

down) (Refer to AMM Task 27-93-00-710-002).

(f) Do the Operational Test of the Elevator and Aileron Computers (ELACs) (Refer to

AMM Task 27-93-00-710-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

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(g) Do the Operational Test of the Spoiler Elevator Computer 2 (SEC 2) (Refer to AMM

Task 27-94-00-710-003).

(h) Do the Operational Test of the Spoiler Elevator Computer 1 (SEC 1) (Refer to AMM

Task 27-94-00-710-002).

(i) Do the Operational Test of the LAND CAT III Capability (Refer to AMM Task

22-97-00-710-001).

(5) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

**CONF 006

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 136

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(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-004-004 - Test of modules 7222VT10 and 6701VT18

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 137

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References

Aircraft Maintenance Manual (AMM) Task 33-21-00-710-001

Task 33-51-00-710-001

(a) Do the Operational Test of the general illumination (Refer to AMM Task

33-21-00-710-001).

(b) Do the Operational Test of emergency lights (Refer to AMM Task

33-51-00-710-001).

(4) Subtask 921072-710-005-003 - Test of modules 7506VT13

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-710-003

Task 25-52-00-710-004

Task 25-52-00-710-005

(a) Do the Operational Test of the proximity switches (Refer to AMM Task

25-52-00-710-003).

(b) Do the Operational Test of the Door Sill Latches in the FWD Cargo Compartment

(2004VU1 and 2004VU2) and in the AFT Cargo Compartment (2004VU3 and

2004VU4) (Refer to AMM Task 25-52-00-710-004).

(c) Do the Operational Test of the power drive units (Refer to AMM Task

25-52-00-710-005)

(5) Subtask 921072-710-006-001 - Test of modules in Electronics Rack 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-61-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 27-14-00-710-001

Task 27-22-00-710-002

Task 27-93-00-710-001

Task 27-93-00-710-002

Task 27-94-00-710-002

Task 27-94-00-710-003

(a) Do the Operational Test of AFS (Refer to AMM Task 22-96-00-710-001).

(b) Do the Operational Test of the Rudder Travel Limiting Function (Refer to AMM

Task 22-61-00-710-001).

(c) Do the Operational Test of the Rudder Trim Actuation (Refer to AMM Task

27-22-00-710-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 138

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(d) Do the Operational Test of the Aileron and Hydraulic Actuation (Refer to AMM Task

27-14-00-710-001).

(e) Do the Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of

loss of Blue Hydraulic Pressure (to be done before revenue flight landing gear

down) (Refer to AMM Task 27-93-00-710-002).

(f) Do the Operational Test of the Elevator and Aileron Computers (ELACs) (Refer to

AMM Task 27-93-00-710-001).

(g) Do the Operational Test of the Spoiler Elevator Computer 2 (SEC 2) (Refer to AMM

Task 27-94-00-710-003).

(h) Do the Operational Test of the Spoiler Elevator Computer 1 (SEC 1) (Refer to AMM

Task 27-94-00-710-002).

(i) Do the Operational Test of the LAND CAT III Capability (Refer to AMM Task

22-97-00-710-001).

(6) Subtask 921072-710-007-001 - Test of modules in Electronics Rack 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 35-23-00-710-001

Task 35-23-00-720-002

(a) Do the Operational Check of manual mask release (Refer to AMM Task

35-23-00-710-001).

(b) Do the Functional Test of the passenger emergency-oxygen system (Refer to AMM

Task 35-23-00-720-002).

(7) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 139

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**CONF 007

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 140

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NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-005-003 - Test of modules 7506VT13

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-52-00-710-003

Task 25-52-00-710-004

Task 25-52-00-710-005

(a) Do the Operational Test of the proximity switches (Refer to AMM Task

25-52-00-710-003).

(b) Do the Operational Test of the Door Sill Latches in the FWD Cargo Compartment

(2004VU1 and 2004VU2) and in the AFT Cargo Compartment (2004VU3 and

2004VU4) (Refer to AMM Task 25-52-00-710-004).

(c) Do the Operational Test of the power drive units (Refer to AMM Task

25-52-00-710-005)

(4) Subtask 921072-710-006-001 - Test of modules in Electronics Rack 80VU

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 141

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References

Aircraft Maintenance Manual (AMM) Task 22-61-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 27-14-00-710-001

Task 27-22-00-710-002

Task 27-93-00-710-001

Task 27-93-00-710-002

Task 27-94-00-710-002

Task 27-94-00-710-003

(a) Do the Operational Test of AFS (Refer to AMM Task 22-96-00-710-001).

(b) Do the Operational Test of the Rudder Travel Limiting Function (Refer to AMM

Task 22-61-00-710-001).

(c) Do the Operational Test of the Rudder Trim Actuation (Refer to AMM Task

27-22-00-710-002).

(d) Do the Operational Test of the Aileron and Hydraulic Actuation (Refer to AMM Task

27-14-00-710-001).

(e) Do the Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of

loss of Blue Hydraulic Pressure (to be done before revenue flight landing gear

down) (Refer to AMM Task 27-93-00-710-002).

(f) Do the Operational Test of the Elevator and Aileron Computers (ELACs) (Refer to

AMM Task 27-93-00-710-001).

(g) Do the Operational Test of the Spoiler Elevator Computer 2 (SEC 2) (Refer to AMM

Task 27-94-00-710-003).

(h) Do the Operational Test of the Spoiler Elevator Computer 1 (SEC 1) (Refer to AMM

Task 27-94-00-710-002).

(i) Do the Operational Test of the LAND CAT III Capability (Refer to AMM Task

22-97-00-710-001).

(5) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 142

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**CONF 008

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 143

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NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-006-001 - Test of modules in Electronics Rack 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-61-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 27-14-00-710-001

Task 27-22-00-710-002

Task 27-93-00-710-001

Task 27-93-00-710-002

Task 27-94-00-710-002

Task 27-94-00-710-003

(a) Do the Operational Test of AFS (Refer to AMM Task 22-96-00-710-001).

(b) Do the Operational Test of the Rudder Travel Limiting Function (Refer to AMM

Task 22-61-00-710-001).

(c) Do the Operational Test of the Rudder Trim Actuation (Refer to AMM Task

27-22-00-710-002).

(d) Do the Operational Test of the Aileron and Hydraulic Actuation (Refer to AMM Task

27-14-00-710-001).

(e) Do the Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of

loss of Blue Hydraulic Pressure (to be done before revenue flight landing gear

down) (Refer to AMM Task 27-93-00-710-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 144

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(f) Do the Operational Test of the Elevator and Aileron Computers (ELACs) (Refer to

AMM Task 27-93-00-710-001).

(g) Do the Operational Test of the Spoiler Elevator Computer 2 (SEC 2) (Refer to AMM

Task 27-94-00-710-003).

(h) Do the Operational Test of the Spoiler Elevator Computer 1 (SEC 1) (Refer to AMM

Task 27-94-00-710-002).

(i) Do the Operational Test of the LAND CAT III Capability (Refer to AMM Task

22-97-00-710-001).

(4) Subtask 921072-710-008-001 - Test of modules in Pylons

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 26-12-00-710-001

Task 26-12-00-710-002

(a) Do the Operational Test of loop/squib (Refer to AMM Task 26-12-00-710-001).

(b) Do the Operational Test of the Engine Fire and Overheat Detection with the

Centralized Fault Display System (CFDS) (Refer to AMM Task 26-12-00-710-002).

**CONF 009

(1) Subtask 921072-710-002-001 - Job Set-up.

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001

(a) Reconnect the batteries:

- for Job Set-up, refer to the Removal/Installation of the Batteries (Refer to AMM

Task 24-38-51-400-001)

- remove the blanking caps from the electrical connectors

- make sure that the electrical connectors are clean and in correct condition

- connect the connector on the battery

- turn the knurled nut a quarter turn

(b) Remove all warning notices

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

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 145

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(2) Subtask 921072-710-003-001 - Preliminary tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-26-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 31-50-00-710-001

Task 31-50-00-710-004

Task 31-60-00-710-001

Task 33-13-00-710-001

Task 33-14-00-710-001

Elec. Std. Practices Manual (ESPM) 20-52-10

NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the

Operational Test of the LAND CAT III Capability, Refer to AMM Task

22-97-00-710-001.

(a) On each connector which was disconnected:

- do the checks as defined by ESPM 20-52-10.

NOTE: The functional test and/or operational test requested by this ESPM

procedure is given hereafter.

(b) Do the Operational Test of the Instrument and Panel Integral Lightning (Refer to

AMM Task 33-13-00-710-001).

(c) Do the Operational Test of the Light (Refer to AMM Task 33-14-00-710-001).

(d) Do the Operational Check of the System via MCDU (Refer to AMM Task

21-26-00-710-001).

(e) Do the Operational Test of the AFS (Refer to AMM Task 22-96-00-710-001).

(f) Do the Operational Test of the EIS (Refer to AMM Task 31-60-00-710-001).

(g) Do the Operational Test of the ECAM Control Panel (Refer to AMM Task

31-50-00-710-004).

(h) Do the Ground Scanning of the Central Warning System (Refer to AMM Task

31-50-00-710-001).

(3) Subtask 921072-710-006-001 - Test of modules in Electronics Rack 80VU

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 146

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References

Aircraft Maintenance Manual (AMM) Task 22-61-00-710-001

Task 22-96-00-710-001

Task 22-97-00-710-001

Task 27-14-00-710-001

Task 27-22-00-710-002

Task 27-93-00-710-001

Task 27-93-00-710-002

Task 27-94-00-710-002

Task 27-94-00-710-003

(a) Do the Operational Test of AFS (Refer to AMM Task 22-96-00-710-001).

(b) Do the Operational Test of the Rudder Travel Limiting Function (Refer to AMM

Task 22-61-00-710-001).

(c) Do the Operational Test of the Rudder Trim Actuation (Refer to AMM Task

27-22-00-710-002).

(d) Do the Operational Test of the Aileron and Hydraulic Actuation (Refer to AMM Task

27-14-00-710-001).

(e) Do the Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of

loss of Blue Hydraulic Pressure (to be done before revenue flight landing gear

down) (Refer to AMM Task 27-93-00-710-002).

(f) Do the Operational Test of the Elevator and Aileron Computers (ELACs) (Refer to

AMM Task 27-93-00-710-001).

(g) Do the Operational Test of the Spoiler Elevator Computer 2 (SEC 2) (Refer to AMM

Task 27-94-00-710-003).

(h) Do the Operational Test of the Spoiler Elevator Computer 1 (SEC 1) (Refer to AMM

Task 27-94-00-710-002).

(i) Do the Operational Test of the LAND CAT III Capability (Refer to AMM Task

22-97-00-710-001).

E. CLOSE-UP

**CONF 001

(1) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 147

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 002

(1) Subtask 921072-942-010-001 - Close the access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Work location Electrical panel 2000VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-001

(a) Install the access panel 221BC (Refer to AMM Task 25-23-42-400-001).

(2) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 148

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**CONF 003

(1) Subtask 921072-942-010-001 - Close the access to the 7430VT32

Work Zones and Access Panels

Zone Access/Work location

220 Access to open Door 831

Panel 221BC

Work location Electrical panel 2000VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-001

(a) Install the access panel 221BC (Refer to AMM Task 25-23-42-400-001).

(2) Subtask 921072-942-011-001 - Close the access to the 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(3) Subtask 921072-942-012-001 - Close the access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 149

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(4) Subtask 921072-942-013-001 - Close the access to 6701VT18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

(5) Subtask 921072-942-010-001 - Close the access to the modules in Electronics Rack

103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002

(a) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(6) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 150

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**CONF 004

(1) Subtask 921072-942-011-001 - Close the access to the 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(2) Subtask 921072-942-012-001 - Close the access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(3) Subtask 921072-942-013-001 - Close the access to 6701VT18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

(4) Subtask 921072-942-010-001 - Close the access to the modules in Electronics Rack

103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822

Work location Electrical panel 103VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 151

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Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002

(a) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(5) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 005

(1) Subtask 921072-942-012-001 - Close the access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 152

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(2) Subtask 921072-942-014-001 - Close the access to 7492VT22

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261CC

Work location Stringer 2LH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261CC (Refer to AMM Task 25-23-42-400-002).

(3) Subtask 921072-942-016-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(4) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 153

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(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 006

(1) Subtask 921072-942-011-001 - Close the access to the 7222VT10

Work Zones and Access Panels

Zone Access/Work location

260 Access to open Door 832

Panel 261BC

Work location Frame 66

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-42-400-002

(a) Install the access panel 261BC (Refer to AMM Task 25-23-42-400-002).

(2) Subtask 921072-942-012-001 - Close the access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(3) Subtask 921072-942-013-001 - Close the access to 6701VT18

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-001

(a) Install the access panel 251LC (Refer to AMM Task 25-23-41-400-001).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 154

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(4) Subtask 921072-942-017-001 - Close the access to the Electronics Racks 80VU and

103VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 822, Door 824

Work location Electrical panel 103VU

Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(c) Close the access door 822 (Refer to AMM Task 52-41-00-410-002).

(5) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 155

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**CONF 007

(1) Subtask 921072-942-012-001 - Close the access to 7506VT13

Work Zones and Access Panels

Zone Access/Work location

150 Access to open Door 826

Panel 152DW

Work location Stringer 31RH

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-55-11-400-003

(a) Install the access panel 152DW (Refer to AMM Task 25-55-11-400-003).

(2) Subtask 921072-942-016-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(3) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 156

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References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

**CONF 008

(1) Subtask 921072-942-016-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

(2) Subtask 921072-942-018-001 - Close the access to the modules in Pylons

Work Zones and Access Panels

Zone Access/Work location

410 Access to open Panel 414AR

Work location Pylon 1

420 Access to open Panel 424AR

Work location Pylon 2

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-52-11-400-002

(a) Install the skin panels (Refer to AMM Task 54-52-11-400-002):

- 414AR for Pylon 1

- 424AR for Pylon 2

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 157

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**CONF 009

(1) Subtask 921072-942-016-001 - Close the access to the Electronics Rack 80VU

Work Zones and Access Panels

Zone Access/Work location

120 Access to open Door 824

Work location Electrical panel 80VU

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 05-21-20, Page Block 601

Task 52-41-00-410-002

(a) Install the partition panels 131DW, 131CW and 132EW (Refer to AMM 05-21-20,

Page Block 601).

(b) Close the access door 824 (Refer to AMM Task 52-41-00-410-002).

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 158

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SERVICE BULLETIN

**CONF 002 thru 003

MODULE 32

MODULE 32

NSA 937901 M1604

MODULE 32

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

C

TYPICAL

7430VT

7430VT

B

FR18

FR20 FR21

FR12

( 2000VU)

B

C

Z220

A

A

N_SB_921072_5_GAAA_01_00

Figure A-FGAAA - Sheet 01

Location of module 7430VT32

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 159

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SERVICE BULLETIN

**CONF 003 thru 004, 006

MODULE 10

Z260

MODULE 10

NSA 937901 M1604

MODULE 10

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

C

A

TYPICAL

FR66

FR65

FR64

FR70

B

A

B C

7222VT

7222VT

N_SB_921072_5_GCAA_01_00

Figure A-FGCAA - Sheet 01

Location of module 7222VT10

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 160

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**CONF 003 thru 007

Z150

A

FR52

FR51

FR50

FR56

7506VT

MODULE 13

B

A

B

TYPICAL

7506VT

MODULE 13

NSA 937901 M1604

C

MODULE 13

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

STGR31RH

C

N_SB_921072_5_GEAA_01_00

Figure A-FGEAA - Sheet 01

Location of module 7506VT13

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 161

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**CONF 003 thru 004, 006

MODULE 18

MODULE 18

NSA 937901 M1604

MODULE 18

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

C

TYPICAL

C

Z250

A

B

STGR5LH

FR47.1

FR47.4

FR47.5

FR48

6701VT

6701VT

A

B

N_SB_921072_5_GGAA_01_00

Figure A-FGGAA - Sheet 01

Location of module 6701VT18

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 162

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**CONF 005

FR64

FR65

FR66

MODULE 22

STGR2LH

CL

Z260

7492VT

MODULE 22

NSA 937901 M1604

B

C

MODULE 22

NSA 937901 M1604

DATE CODE

TO BE INSPECTED

C

A

A

B TYPICAL

7492VT

FR70

N_SB_921072_5_GJAA_01_00

Figure A-FGJAA - Sheet 01

Location of module 7492VT22

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 163

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**CONF 003 thru 009

C A

1156VT

103VU

1890VT

187VU

80VU

B

N_SB_921072_5_BAAA_01_02

A

1833VT

1837VT

1842VT

1846VT

B C

Figure A-FBAAA - Sheet 01

Location of modules in 80VU and 103VU

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 164

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**CONF 001 thru 008

Z410

A

B

Z420

414AR

424AR

A

B

C

C

C

RIB04

RIB05

RIB06

RIB07

RIB08

RIB09

450VT

N_SB_921072_5_BBAA_01_01

Figure A-FBBAA - Sheet 01

Location of modules in Pylons

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 165

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**CONF ALL

QUESTION

ACTION

FINDING

NO FURTHER ACTION

DATE CODE

08−14 AND 08−18 YES NO

REMOVE AND REPLACE BY NSA

937901M1604 WITH DATE CODE

DIFFERENT FROM 08−14 AND 08−18

TESTING OF

TERMINAL MODULE

REPLACED

NO FURTHER ACTION

CHECK DEUTSCH MODULES

NSA 937901M1604 DATE CODE

08−14 ON 103VU, PYLON HARNESSES,

S15/19 HARNESSES AND DATE CODE

08−14 AND 08−18 ON 80VU

THRESHOLD: NOT LATER THAN 600FH

N_SB_921072_5_AAAA_01_01

Figure A-FAAAA - Sheet 01

Flow Chart.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 166

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Appendix 01

**CONF ALL

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1, Rond point Maurice BELLONTE

31707 BLAGNAC CEDEX

FRANCE

Tel: (33)-5-61-93-33-33

Telex: AIRBU 530526 F

Fax: (33)-5-61-93-42-51

ATA SYSTEM: 92

ELECTRIC AND ELECTRONIC COMMON INSTALLATION - INSPECTION OF DEUTSCH DEFECTIVE

MODULES NSA 937901M1604

MODIFICATION No.: NONE

(1) Inspection Report

The results of the Inspection, including no findings, replacement or actions to be done must be

forwarded to AIRBUS department SEEEA6, on the attached inspection report sheet.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 1

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Appendix 01

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. : A320−92−1072

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

DATE OF INSPECTION :

INSPECTION METHOD :

MARK THE CORRESPONDING BOX

DETAILED

VISUAL

INSPECTED

MODULE

7430VT32

7222VT10

7506VT13

6701VT18

7492VT22

1833VT69

1842VT3

1846VT5

1846VT16

1837VT17

1890VT3

1156VT3

1156VT5

450VT1 1

450VT1 2

450VT2 1

450VT2 2

N_SB_921072_5_AKAA_01_00

DATE CODE 08−14

(TO BE REPLACED)

NOT TO BE

INSPECTED

OTHER

DATE CODE

Figure A-FAKAA - Sheet 01

Inspection Report Sheet

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 2

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Appendix 01

**CONF 001

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

TEST AFTER REMOVAL

GET ACCESS TO Z414

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

7.25

7.25

STEPS

1.25

0.25 0.25

1.25

1

1

0 2 4 6 8

INSPECT AND REPAIR

MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR

MODULES IN Z424

CLOSE ACCESS TO Z424

1

1

1

1

1

2.50 2.50

0.25 0.25

0.25

0.25

2.50

0.25

0.25

2.50

N_SB_921072_5_ABAA_01_02

OF MODULES IN PYLONS

1357

Figure A-FABAA - Sheet 01

Elapsed time assumptions (Conf. 001)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 3

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Appendix 01

**CONF 002

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

STEPS MH ET PER

0

GET ACCESS TO Z220

INSPECT AND REPAIR MODULES IN Z220

CLOSE ACCESS TO Z220

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

TEST AFTER REMOVAL OF MODULE IN 7430VT32

TEST AFTER REMOVAL OF MODULES IN PYLONS

0.25 0.25 1.00

1 2 3 4 5 6 7 8 9

1.25 1.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

1.50 1.50 1.00

1.25 1.25 1.00

N_SB_921072_5_ACAA_01_01

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

MH: TO DO THE WORK IS MORE SUITABLE FOR THEM.

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

0.50 0.50 1.00

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

10.75

8.75 ELAPSED TIME

(HOURS)

Figure A-FACAA - Sheet 01

Elapsed time assumptions (Conf. 002)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 4

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Appendix 01

**CONF 003

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

MH ET PER

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

22.75

12.75

STEPS

0

TEST AFTER REMOVAL OF MODULES IN PYLONS

GET ACCESS TO Z220

INSPECT AND REPAIR MODULES IN Z220

CLOSE ACCESS TO Z220

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

GET ACCESS TO Z150

INSPECT AND REPAIR MODULES IN Z150

CLOSE ACCESS TO Z150

GET ACCESS TO 103VU

INSPECT AND REPAIR MODULES IN 103VU

CLOSE ACCESS TO 103VU

GET ACCESS TO Z250

INSPECT AND REPAIR MODULES IN Z250

CLOSE ACCESS TO Z250

GET ACCESS TO Z260

INSPECT AND REPAIR MODULES IN Z260

CLOSE ACCESS TO Z260

TEST AFTER REMOVAL OF MODULE IN 103 VU

TEST AFTER REMOVAL OF MODULES 7222VT10,

TEST AFTER REMOVAL OF MODULE 7506VT13

0.25 0.25 1.00

2 3 4 5 6 7 8 9 10 11 12 13

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

1.25 1.25 1.00

1.25 1.25 1.00

1.50 1.50 1.00

N_SB_921072_5_ADAA_01_02

1

7430VT32 AND 6701VT18

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

ELAPSED TIME

(HOURS)

1.75 1.75 1.00

Figure A-FADAA - Sheet 01

Elapsed time assumptions (Conf. 003)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 5

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Appendix 01

**CONF 004

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

MH ET PER

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

20.75

10.75

STEPS

0

TEST AFTER REMOVAL OF MODULES IN PYLONS

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

GET ACCESS TO Z150

INSPECT AND REPAIR MODULES IN Z150

CLOSE ACCESS TO Z150

GET ACCESS TO 103VU

INSPECT AND REPAIR MODULES IN 103VU

CLOSE ACCESS TO 103VU

GET ACCESS TO Z250

INSPECT AND REPAIR MODULES IN Z250

CLOSE ACCESS TO Z250

GET ACCESS TO Z260

INSPECT AND REPAIR MODULES IN Z260

CLOSE ACCESS TO Z260

TEST AFTER REMOVAL OF MODULE IN 103 VU

TEST AFTER REMOVAL OF MODULES 7222VT10,

2 3 4 5 6 7 8 9 10 11

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

1.25 1.25 1.00

1.25 1.25 1.00

1.50 1.50 1.00

1

AND 6701VT18

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

ELAPSED TIME

(HOURS)

TEST AFTER REMOVAL OF MODULES 7506VT13 1.75 1.75 1.00

N_SB_921072_5_AEAA_01_02

Figure A-FAEAA - Sheet 01

Elapsed time assumptions (Conf. 004)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 6

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SERVICE BULLETIN

Appendix 01

**CONF 005

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

STEPS MH ET PER

0

GET ACCESS TO Z150

INSPECT AND REPAIR MODULES IN Z150

CLOSE ACCESS TO Z150

GET ACCESS TO 80VU

INSPECT AND REPAIR MODULES IN 80VU

CLOSE ACCESS TO 80VU

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

GET ACCESS TO Z260

INSPECT AND REPAIR MODULES IN Z260

CLOSE ACCESS TO Z260

TEST AFTER REMOVAL OF MODULE IN 80VU

TEST AFTER REMOVAL OF MODULE IN PYLONS

TEST AFTER REMOVAL OF MODULES 7506VT13

0.25 0.25 1.00

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

7.50 7.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

3.50 3.50 1.00

1.25 1.25 1.00

1.75 1.75 1.00

N_SB_921072_5_AFAA_01_01

AND 7492VT22

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

24.50

16.50 ELAPSED TIME

(HOURS)

17

Figure A-FAFAA - Sheet 01

Elapsed time assumptions (Conf. 005)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 7

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Appendix 01

**CONF 006

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

ELAPSED TIME (HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

32.25

18.25

STEPS

0

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

GET ACCESS TO 103VU

INSPECT AND REPAIR MODULES IN 103VU

CLOSE ACCESS TO 103VU

GET ACCESS TO Z250

INSPECT AND REPAIR MODULES IN Z250

CLOSE ACCESS TO Z250

GET ACCESS TO Z260

INSPECT AND REPAIR MODULES IN Z260

CLOSE ACCESS TO Z260

GET ACCESS TO 80VU

INSPECT AND REPAIR MODULES IN 80VU

CLOSE ACCESS TO 80VU

GET ACCESS TO Z150

INSPECT AND REPAIR MODULES IN Z150

CLOSE ACCESS TO Z150

0.25

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18

2.50

0.25

0.25

2.50

0.25

0.25

2.50

0.25

0.25

1.25

0.50

0.25

1.25

0.50

0.25

7.50

0.25

0.25

1.25

0.50

TEST AFTER REMOVAL OF MODULES 7222VT10

AND 6701VT18

TEST AFTER REMOVAL OF MODULE 7506VT13

1.50

1.75

TEST AFTER REMOVAL OF MODULES IN 80VU 3.50

TEST AFTER REMOVAL OF MODULES IN PYLONS 1.25

TEST AFTER REMOVAL OF MODULES IN 103VU 1.25

0.25 1.00

2.50 1.00

0.25 1.00

0.25 1.00

2.50 1.00

0.25 1.00

0.25 1.00

2.50 1.00

0.25 1.00

0.25 1.00

1.25 1.00

0.50 1.00

0.25 1.00

1.25 1.00

0.50 1.00

0.25 1.00

7.50 1.00

0.25 1.00

0.25 1.00

1.25 1.00

0.50 1.00

1.50 1.00

1.75 1.00

3.50 1.00

1.25 1.00

1.25 1.00

N_SB_921072_5_AGAA_01_03

Figure A-FAGAA - Sheet 01

Elapsed time assumptions (Conf. 006)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 8

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Appendix 01

**CONF 007

ELAPSED TIME (HOURS)

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

22.50

14.50

STEPS

0

GET ACCESS TO Z150

INSPECT AND REPAIR MODULES IN Z150

CLOSE ACCESS TO Z150

GET ACCESS TO 80VU

INSPECT AND REPAIR MODULES IN 80VU

CLOSE ACCESS TO 80VU

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

TEST AFTER REMOVAL OF MODULE 7506VT13

TEST AFTER REMOVAL OF MODULES IN 80VU

TEST AFTER REMOVAL OF MODULES IN PYLONS

15

N_SB_921072_5_AHAA_01_02

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

MH: TO DO THE WORK IS MORE SUITABLE FOR THEM.

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

1 2 3 4 5 6 7 8 9 10 11 12 13 14

MH ET PER

0.25 0.25 1.00

1.25 1.25 1.00

0.50 0.50 1.00

0.25 0.25 1.00

7.50 7.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

0.25 0.25 1.00

2.50 2.50 1.00

0.25 0.25 1.00

1.75 1.75 1.00

3.50 3.50 1.00

1.25 1.25 1.00

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

Figure A-FAHAA - Sheet 01

Elapsed time assumptions (Conf. 007)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 9

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Appendix 01

**CONF 008

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

MH: TO DO THE WORK IS MORE SUITABLE FOR THEM.

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

18.75

12.75

1 2 3 4 5 6 7 8 9 10 11 12 13

GET ACCESS TO 80VU

INSPECT AND REPAIR MODULES IN 80VU

CLOSE ACCESS TO 80VU

GET ACCESS TO Z414

INSPECT AND REPAIR MODULES IN Z414

CLOSE ACCESS TO Z414

GET ACCESS TO Z424

INSPECT AND REPAIR MODULES IN Z424

CLOSE ACCESS TO Z424

TEST AFTER REMOVAL OF MODULES IN 80VU

TEST AFTER REMOVAL OF MODULES IN PYLONS

0.25

7.50

0.25

0.25

7.50

0.25

1.00

1.00

1.00

0.25

2.50

0.25

0.25

2.50

0.25

1.00

1.00

1.00

0.25

2.50

0.25

0.25

2.50

0.25

1.00

1.00

1.00

3.50

1.25

3.50

1.25

1.00

1.00

STEPS MH ET PER

0

N_SB_921072_5_AJAA_01_01

Figure A-FAJAA - Sheet 01

Elapsed time assumptions (Conf. 008)

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 10

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Appendix 01

**CONF 009

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−92−1072

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

MH: TO DO THE WORK IS MORE SUITABLE FOR THEM.

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

11.50

11.50

1 2 3 4 5 6 7 8 9 10 11 12 13

GET ACCESS TO 80VU

INSPECT AND REPAIR MODULES IN 80VU

CLOSE ACCESS TO 80VU

TEST AFTER REMOVAL OF MODULES IN 80VU

0.25

7.50

0.25

0.25

7.50

0.25

1.00

1.00

1.00

3.50 3.50 1.00

STEPS MH ET PER

0

N_SB_921072_5_ALAA_01_00

Figure A-FALAA - Sheet 01

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 11

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SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - INSPECTION

OF DEUTSCH DEFECTIVE MODULES NSA 937901M1604

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 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: Mar 13/09 SERVICE BULLETIN No.: A320-92A1072

REVISION No.: 00 - Mar 13/09 Page: 1

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