@A318/A319/A320/A321

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 32

TITLE: LANDING GEAR - EXTENSION AND RETRACTION- INTRODUCE

POWER INTERRUPT PROTECTION CIRCUIT FOR LGCIUS ON A319CJ

AIRCRAFT

MODIFICATION No.: 30248P10949 37866J2818

This page transmits Revision No.03 of Service Bulletin No.A320-32-1349

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 03 issued to update the INDUSTRY SUPPORT INFORMATION and to amend a Tooling

reference.

The opportunity has been taken to:

- update the test procedure for the Test of Battery Relief Relay 60GA

- update the test procedure for the Test of System 2 Battery Relief Relay 61GA

- update the effectivity.

CHANGES

SUMMARY

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

APPROVAL APPROVAL UPDATED R

MATERIAL INFORMATION

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 1

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REVISION TRANSMITTAL SHEET

Consumable CMLA11 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

R

TOOLING

Tools TOOLS UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 321349- 831-896-001-

MODIFICATION

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Subtask 321349-910-001-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 321349-910-001-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 321349-910-001-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 321349-910-001-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 321349-720-402-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PANEL UPDATED

CIRCUIT BREAKER UPDATED

REFERENCES UPDATED

R

Subtask 321349-720-403-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

Subtask 321349-720-402-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PANEL UPDATED

CIRCUIT BREAKER UPDATED

REFERENCES UPDATED

R

Subtask 321349-720-403-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

Subtask 321349-720-402-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PANEL UPDATED

CIRCUIT BREAKER UPDATED

REFERENCES UPDATED

R

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 2

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REVISION TRANSMITTAL SHEET

Subtask 321349-720-403-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

Subtask 321349-720-402-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PANEL UPDATED

CIRCUIT BREAKER UPDATED

REFERENCES UPDATED

R

Subtask 321349-720-403-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

REFERENCES UPDATED

NOTE UPDATED

R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision 01 has been issued:

to update the Industry Support paragraph

Replace P/N D9251719400195 by D9251719400195 for the LGCIU plate in Kit 321349A01R01,

Add Kit 321349A06R00 which contains one bundle (modification of the wiring in 93VU),

Update the effectivity.

This Service Bulletin has been validated on A320 aircraft MSN 2760.

The opportunity has also been taken to include changes to the test procedures that were found

necessary following the validation of the Service Bulletin A320-32-1346 on MSN 2760.

Revision 02 has been issued to:

update the Relay 62GA Test requirements

modify the pin of the relay 53GA (A1, A2, A3 become B1, B2, B3 in Fig. A-FBBAA).

REVISION SEQUENCE

ORIGINAL: Dec 04/08

REVISION No. : 01 - Aug 31/09

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REVISION No. : 02 - Jun 16/10

REVISION No. : 03 - Oct 05/11

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 4

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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: 32

TITLE: LANDING GEAR - EXTENSION AND RETRACTION- INTRODUCE

POWER INTERRUPT PROTECTION CIRCUIT FOR LGCIUS ON A319CJ

AIRCRAFT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 37866J2818

MINOR 30248P10949

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

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

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

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Uncommanded Nose Landing Gear (NLG) retraction can occur when there is a dormant seal failure in

the Landing Gear Retract Valve (causing retraction pressure to be applied to the gear) and a Landing

Gear Control and Interface Unit (LGCIU) power interrupt occurs. Under normal circumstances the NLG

is held in the downlock position by the doors closed hydraulic pressure to the NLG downlock actuator.

In the failure condition, doors closed pressure might be lost if the LGCIU suffers a power supply

interrupt longer than 3mSec, thus allowing, under certain circumstances, the dormant seal failure to

retract the NLG.

This Service Bulletin provides a power interrupt protection for the LGCIU(s) using diodes (Power Supply

De-coupling Unit (PSDU)) to split the LGCIU 28V supply between the transformer rectifiers and the

batteries. This will enable the battery bus 7PP to supply LGCIU(s) in the event of an interrupt on the

normal LGCIU supply. A time delay relay will also be installed so that the battery cannot be drained.

The safety valve relay (pre mod 48GA) will be changed from a normal type to a 1 second delay on

energization (post mod 62GA). This one-second delay will give the LGCIU time to power up and

energise the doors closed valve.

Accomplishment of this modification will ensure the door closed pressure remains, and thus downlock

pressure, even in the case of LGCIU power interrupt. The LG safety valve 49GA will be controlled by a

1 second time delay relay 62GA to allow time for the LGCIU(s) to power up. The LG leg extension will

be delayed by one second due to the delay relay 62GA.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 1

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SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED YES

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

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

disruptions.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 321349A01R01 1 8,110.00 Bundle, placard set, LGCIU plate, C/B,

relay, fasteners

Kit 321349A02R00 1 128.00 Placard

Kit 321349A06R00 1 82.00 Bundle

TOTAL 8,320.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 321349A01R01 1 8,110.00 Bundle, placard set, LGCIU plate, C/B,

relay, fasteners

Kit 321349A03R00 1 128.00 Placard

Kit 321349A06R00 1 82.00 Bundle

TOTAL 8,320.00

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 321349A01R01 1 8,110.00 Bundle, placard set, LGCIU plate, C/B,

relay, fasteners

Kit 321349A04R00 1 128.00 Placard

Kit 321349A06R00 1 82.00 Bundle

TOTAL 8,320.00

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 2

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SERVICE BULLETIN

SUMMARY

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 321349A01R01 1 8,110.00 Bundle, placard set, LGCIU plate, C/B,

relay, fasteners

Kit 321349A05R00 1 128.00 Placard

Kit 321349A06R00 1 82.00 Bundle

TOTAL 8,320.00

EFFECTIVITY

**CONF ALL

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

01Z 03X 17W 31X 53Z 59U 59Z 80X 91X 95W AEE AHY BRS

CEF DCS G4I KFR MLM PVJ QAF QTR R1T SHJ SND SVW TBJ

THY TWJ UKN WGT WHT

The equivalent of this Service Bulletin has been validated on A320 aircraft MSN 2760.

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU 32.31.00.009

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 321349-831-896-001: MODIFICATION

TOTAL MANHOURS 48.00

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 3

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SUMMARY

Task 321349-831-896-001: MODIFICATION

ELAPSED TIME (HOURS) 33.50

**CONF 002

Task 321349-831-896-001: MODIFICATION

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF 003

Task 321349-831-896-001: MODIFICATION

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF 004

Task 321349-831-896-001: MODIFICATION

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

APPENDICES

**CONF ALL

Appendix 1

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 4

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SUMMARY

**CONF ALL

MODIFICATION OF THE EQUIPMENT

AND THE WIRING IN 121VU

2M

1M

MODIFICATION OF THE EQUIPMENT

AND THE WIRING IN 93VU

INSTALLATION OF THE

LGCIU PLATE IN 91VU

120VU

90VU

N_SB_321349_5_SUAA_01_00

Figure A-FSUAA - Sheet 01

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 5

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SUMMARY

This Page Intentionally Left Blank

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 6

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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: 32

TITLE: LANDING GEAR - EXTENSION AND RETRACTION- INTRODUCE

POWER INTERRUPT PROTECTION CIRCUIT FOR LGCIUS ON A319CJ

AIRCRAFT

MODIFICATION No.: 30248P10949 37866J2818

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

319-115 319-132 319-133

(2) Effectivity by MSN

0910 1002 1053 1157 1212 1256 1335 1468 1485 1556 1589 1656 1727 1795 1880

1908 1999 2192 2263 2341 2421 2440 2487 2507 2550 2592 2650 2675 2706 2748

2801 2837 2921 2949 3046 3073 3085 3133 3243 3260 3356 3542

(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

01Z 1589

03X 2421

17W 3046

31X 2192

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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OPERATOR MSN

53Z 1468

59U 2706 3073

59Z 1556

80X 2748

91X 2837

95W 2949

AEE 1727 1880

AHY 2487

BRS 2263

CEF 2801 3085

DCS 1053 3243

G4I 1157 1795 2507

KFR 2650

MLM 2592 3356

PVJ 3542

QAF 1335

QTR 1656 2341

R1T 1908

SHJ 0910

SND 1999

SVW 2921 3133

TBJ 1485

THY 1002

TWJ 2550

UKN 3260

WGT 1212

WHT 1256 2440 2675

(4) Configuration by MSN

MSN CONFIGURATION

0910 1002 1053 1157 001

1212 1256 1335 1468 1485 1556 1589 002

1656 1727 2263 2341 003

1795 1880 1908 1999 2192 2421 2440 2487 2507 2550 2592

2650 2675 2706 2748 2801 2837 2921 2949 3046 3073 3085

3133 3243 3260 3356 3542

004

(5) Configuration definition

The intent of this Service Bulletin has been validated on A320 aircraft MSN 2760 by

Service Bulletin A320-32-1346.

NOTE: Modification Nos. 37866J2818 and 30248P10949 are embodied before

delivery on A319CJ aircraft MSN 3513, 3632 and subsequent.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 2

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**CONF 001

Config. 01 is valid for aircraft on which Mod. No. 28655P6042 is not embodied, Mod. No.

31063P6940 is not embodied, Mod. No. 31051P6983 is not embodied.

**CONF 002

Config. 02 is valid for aircraft on which Mod. No. 28655P6042 is embodied, Mod. No.

31063P6940 is not embodied, Mod. No. 31051P6983 is not embodied.

**CONF 003

Config. 03 is valid for aircraft on which Mod. No. 28655P6042 is embodied, Mod. No.

31063P6940 is embodied, Mod. No. 31051P6983 is not embodied.

**CONF 004

Config. 04 is valid for aircraft on which Mod. No. 28655P6042 is embodied, Mod. No.

31063P6940 is embodied, Mod. No. 31051P6983 is embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 321349A01R01 1

Kit 321349A02R00 1

Kit 321349A06R00 1

Consumable CMLA11 As required

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 321349A01R01 1

Kit 321349A03R00 1

Kit 321349A06R00 1

Consumable CMLA11 As required

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 321349A01R01 1

Kit 321349A04R00 1

Kit 321349A06R00 1

Consumable CMLA11 As required

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Kit 321349A01R01 1

Kit 321349A05R00 1

Kit 321349A06R00 1

Consumable CMLA11 As required

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 3

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**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Uncommanded Nose Landing Gear (NLG) retraction can occur when there is a dormant

seal failure in the Landing Gear Retract Valve (causing retraction pressure to be applied

to the gear) and a Landing Gear Control and Interface Unit (LGCIU) power interrupt

occurs. Under normal circumstances the NLG is held in the downlock position by the

doors closed hydraulic pressure to the NLG downlock actuator. In the failure condition,

doors closed pressure might be lost if the LGCIU suffers a power supply interrupt longer

than 3mSec, thus allowing, under certain circumstances, the dormant seal failure to

retract the NLG.

(2) Objective/Action

This Service Bulletin provides a power interrupt protection for the LGCIU(s) using diodes

(Power Supply De-coupling Unit (PSDU)) to split the LGCIU 28V supply between the

transformer rectifiers and the batteries. This will enable the battery bus 7PP to supply

LGCIU(s) in the event of an interrupt on the normal LGCIU supply. A time delay relay

will also be installed so that the battery cannot be drained.

The safety valve relay (pre mod 48GA) will be changed from a normal type to a 1

second delay on energization (post mod 62GA). This one-second delay will give the

LGCIU time to power up and energise the doors closed valve.

(3) Advantages

Accomplishment of this modification will ensure the door closed pressure remains, and

thus downlock pressure, even in the case of LGCIU power interrupt. The LG safety valve

49GA will be controlled by a 1 second time delay relay 62GA to allow time for the

LGCIU(s) to power up. The LG leg extension will be delayed by one second due to the

delay relay 62GA.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 321349-831-896-001: MODIFICATION

(1) Remove the equipment for access in the cockpit.

(2) Remove the equipment for access in the avionics compartment.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 4

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(3) Install the new grounding points in the avionics compartment at FR10.

(4) Modify the equipment and the wiring in the C/B panel 121VU.

(5) Modify the equipment and the wiring in the shelf 93VU.

(6) Modify the wiring in the shelf 94VU.

(7) Modify the equipment in the shelf 91VU.

(8) Modify the wiring between the shelves 91VU and 93VU.

(9) Modify the wiring between the shelves 91VU and 94VU.

(10) Modify the wiring between the shelf 91VU and the avionics compartment.

(11) Modify the wiring between the rear panel 120VU and the FWD electronics rack

90VU.

(12) Modify the wiring between the rear panel 120VU and the shelf 91VU.

(13) Install the equipment removed for access in the cockpit.

(14) Install the equipment removed for access in the avionics compartment.

**CONF 002

Task 321349-831-896-001: MODIFICATION

(1) Remove the equipment for access in the cockpit.

(2) Remove the equipment for access in the avionics compartment.

(3) Install the new grounding points in the avionics compartment at FR10.

(4) Modify the equipment and the wiring in the C/B panel 121VU.

(5) Modify the equipment and the wiring in the shelf 93VU.

(6) Modify the wiring in the shelf 94VU.

(7) Modify the equipment in the shelf 91VU.

(8) Modify the wiring between the shelves 91VU and 93VU.

(9) Modify the wiring between the shelves 91VU and 94VU.

(10) Modify the wiring between the shelf 91VU and the avionics compartment.

(11) Modify the wiring between the rear panel 120VU and the FWD electronics rack

90VU.

(12) Modify the wiring between the rear panel 120VU and the shelf 91VU.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 5

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(13) Install the equipment removed for access in the cockpit.

(14) Install the equipment removed for access in the avionics compartment.

**CONF 003

Task 321349-831-896-001: MODIFICATION

(1) Remove the equipment for access in the cockpit.

(2) Remove the equipment for access in the avionics compartment.

(3) Install the new grounding points in the avionics compartment at FR10.

(4) Modify the equipment and the wiring in the C/B panel 121VU.

(5) Modify the equipment and the wiring in the shelf 93VU.

(6) Modify the wiring in the shelf 94VU.

(7) Modify the equipment in the shelf 91VU.

(8) Modify the wiring between the shelves 91VU and 93VU.

(9) Modify the wiring between the shelves 91VU and 94VU.

(10) Modify the wiring between the shelf 91VU and the avionics compartment.

(11) Modify the wiring between the rear panel 120VU and the FWD electronics rack

90VU.

(12) Modify the wiring between the rear panel 120VU and the shelf 91VU.

(13) Install the equipment removed for access in the cockpit.

(14) Install the equipment removed for access in the avionics compartment.

**CONF 004

Task 321349-831-896-001: MODIFICATION

(1) Remove the equipment for access in the cockpit.

(2) Remove the equipment for access in the avionics compartment.

(3) Install the new grounding points in the avionics compartment at FR10.

(4) Modify the equipment and the wiring in the C/B panel 121VU.

(5) Modify the equipment and the wiring in the shelf 93VU.

(6) Modify the wiring in the shelf 94VU.

(7) Modify the equipment in the shelf 91VU.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 6

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(8) Modify the wiring between the shelves 91VU and 93VU.

(9) Modify the wiring between the shelves 91VU and 94VU.

(10) Modify the wiring between the shelf 91VU and the avionics compartment.

(11) Modify the wiring between the rear panel 120VU and the FWD electronics rack

90VU.

(12) Modify the wiring between the rear panel 120VU and the shelf 91VU.

(13) Install the equipment removed for access in the cockpit.

(14) Install the equipment removed for access in the avionics compartment.

**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

F. APPROVAL

This technical content of this document is approved under the authority of Design

Organization Approval No. EASA 21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

**CONF 001

Task 321349-831-896-001: MODIFICATION

Get Access 3.00

On Aircraft

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 7

7

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Task 321349-831-896-001: MODIFICATION

Remove the equipment for access in the cockpit. 2.00

Remove the equipment for access in the avionics

compartment.

4.00

Install the new grounding points in the avionics

compartment at FR10.

1.00

Modify the equipment and the wiring in the C/B panel

121VU.

3.00

Modify the equipment and the wiring in the shelf 93VU. 5.00

Modify the wiring in the shelf 94VU. 0.50

Modify the equipment in the shelf 91VU. 1.00

Modify the wiring between the shelves 91VU and

93VU.

2.00

Modify the wiring between the shelves 91VU and

94VU.

2.00

Modify the wiring between the shelf 91VU and the

avionics compartment.

1.00

Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

3.00

Modify the wiring between the rear panel 120VU and

the shelf 91VU.

4.00

Install the equipment removed for access in the

cockpit.

3.00

Install the equipment removed for access in the

avionics compartment.

5.00

Tests 4.50

Close-Up 4.00

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 1 .

**CONF 002

Task 321349-831-896-001: MODIFICATION

Get Access 3.00

On Aircraft

Remove the equipment for access in the cockpit. 2.00

Remove the equipment for access in the avionics

compartment.

4.00

Install the new grounding points in the avionics

compartment at FR10.

1.00

Modify the equipment and the wiring in the C/B panel

121VU.

3.00

Modify the equipment and the wiring in the shelf 93VU. 5.00

Modify the wiring in the shelf 94VU. 0.50

Modify the equipment in the shelf 91VU. 1.00

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 8

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SERVICE BULLETIN

Task 321349-831-896-001: MODIFICATION

Modify the wiring between the shelves 91VU and

93VU.

2.00

Modify the wiring between the shelves 91VU and

94VU.

2.00

Modify the wiring between the shelf 91VU and the

avionics compartment.

1.00

Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

3.00

Modify the wiring between the rear panel 120VU and

the shelf 91VU.

4.00

Install the equipment removed for access in the

cockpit.

3.00

Install the equipment removed for access in the

avionics compartment.

5.00

Tests 4.50

Close-Up 4.00

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 1 .

**CONF 003

Task 321349-831-896-001: MODIFICATION

Get Access 3.00

On Aircraft

Remove the equipment for access in the cockpit. 2.00

Remove the equipment for access in the avionics

compartment.

4.00

Install the new grounding points in the avionics

compartment at FR10.

1.00

Modify the equipment and the wiring in the C/B panel

121VU.

3.00

Modify the equipment and the wiring in the shelf 93VU. 5.00

Modify the wiring in the shelf 94VU. 0.50

Modify the equipment in the shelf 91VU. 1.00

Modify the wiring between the shelves 91VU and

93VU.

2.00

Modify the wiring between the shelves 91VU and

94VU.

2.00

Modify the wiring between the shelf 91VU and the

avionics compartment.

1.00

Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

3.00

Modify the wiring between the rear panel 120VU and

the shelf 91VU.

4.00

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 9

7

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SERVICE BULLETIN

Task 321349-831-896-001: MODIFICATION

Install the equipment removed for access in the

cockpit.

3.00

Install the equipment removed for access in the

avionics compartment.

5.00

Tests 4.50

Close-Up 4.00

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 1 .

**CONF 004

Task 321349-831-896-001: MODIFICATION

Get Access 3.00

On Aircraft

Remove the equipment for access in the cockpit. 2.00

Remove the equipment for access in the avionics

compartment.

4.00

Install the new grounding points in the avionics

compartment at FR10.

1.00

Modify the equipment and the wiring in the C/B panel

121VU.

3.00

Modify the equipment and the wiring in the shelf 93VU. 5.00

Modify the wiring in the shelf 94VU. 0.50

Modify the equipment in the shelf 91VU. 1.00

Modify the wiring between the shelves 91VU and

93VU.

2.00

Modify the wiring between the shelves 91VU and

94VU.

2.00

Modify the wiring between the shelf 91VU and the

avionics compartment.

1.00

Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

3.00

Modify the wiring between the rear panel 120VU and

the shelf 91VU.

4.00

Install the equipment removed for access in the

cockpit.

3.00

Install the equipment removed for access in the

avionics compartment.

5.00

Tests 4.50

Close-Up 4.00

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 1 .

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 10

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SERVICE BULLETIN

**CONF ALL

H. WEIGHT AND BALANCE

Manufacturers Empty Weight +1.060 KG (+2.3368 LB)

Effect on Balance +5.647 KGM (+40.844 LB.FT )

I. ELECTRICAL LOAD DATA

The values given below show the increase (+) or decrease (-) of the electrical load resulting

from the accomplishment of this Service Bulletin.

(1) Direct Current (DC) Load Changes

- Circuit Breaker: 58GA (New)

Designation: LGCIU/BAT SPLY/SYS 1

Busbar: 701PP

Nominal Power: 103.8W

Electrical Load Delta: +103.8W

- Circuit Breaker: 59GA (New)

Designation: LGCIU/BAT SPLY/SYS 2

Busbar: 702PP

Nominal Power: 69.8W

Electrical Load Delta: +69.8W

(2) Alternating Current (AC) Load Changes

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-11 20-21-15

20-28-00 21-26-00 21-43-00

21-43-34 21-63-00 21-63-34

22-96-00 22-97-00 24-22-34

24-23-34 24-38-51 24-41-00

25-11-41 25-13-41 26-16-00

26-17-00 26-17-34 27-94-00

27-94-34 28-51-35 31-50-00

31-60-00 32-00-00 32-30-00

32-31-00 32-31-71 32-42-34

32-46-00 32-49-00 32-49-34

32-69-00 33-13-00 33-14-00

52-10-00 52-41-00

Consumable Material List (CML)

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

20-52-10 20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-11

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 11

7

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SERVICE BULLETIN

**CONF 002

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-11 20-21-15

20-28-00 21-26-00 21-43-00

21-43-34 21-63-00 21-63-34

22-96-00 22-97-00 24-22-34

24-23-34 24-38-51 24-41-00

25-11-41 25-13-41 26-16-00

26-17-00 26-17-34 27-94-00

27-94-34 28-51-35 31-50-00

31-60-00 32-00-00 32-30-00

32-31-00 32-31-71 32-42-34

32-46-00 32-49-00 32-49-34

32-69-00 33-13-00 33-14-00

52-10-00 52-41-00

Consumable Material List (CML)

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

20-52-10 20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-11

**CONF 003

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-11 20-21-15

20-28-00 21-26-00 21-43-00

21-43-34 21-63-00 21-63-34

22-96-00 22-97-00 24-22-34

24-23-34 24-38-51 24-41-00

25-11-41 25-13-41 26-16-00

26-17-00 26-17-34 27-94-00

27-94-34 28-51-35 31-50-00

31-60-00 32-00-00 32-30-00

32-31-00 32-31-71 32-42-34

32-46-00 32-49-00 32-49-34

32-69-00 33-13-00 33-14-00

52-10-00 52-41-00

Consumable Material List (CML)

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

20-52-10 20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-11

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 12

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**CONF 004

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 11-00-00

12-34-24 20-21-11 20-21-15

20-28-00 21-26-00 21-43-00

21-43-34 21-63-00 21-63-34

22-96-00 22-97-00 24-22-34

24-23-34 24-38-51 24-41-00

25-11-41 25-13-41 26-16-00

26-17-00 26-17-34 27-94-00

27-94-34 28-51-35 31-50-00

31-60-00 32-00-00 32-30-00

32-31-00 32-31-71 32-42-34

32-46-00 32-49-00 32-49-34

32-69-00 33-13-00 33-14-00

52-10-00 52-41-00

Consumable Material List (CML)

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

20-52-10 20-52-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-11

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Schematic Manual (ASM) 31-54-00

Aircraft Wiring Manual (AWM) 24-68-12 24-68-13 31-54-94

32-31-02 32-31-03 32-31-04

32-31-09 32-31-10 32-31-11

93-01-21

Flight Crew Operating Manual (FCOM) FCOM Vol. 3

Illustrated Parts Catalog (IPC) 32-31-08

MMEL

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

in advance, in case you need your operational documentation to be amended by an

intermediate revision prior to Service Bulletin embodiment. For this purpose, please request

the intermediate revision by fax, telex or mail to:

SEDCC, AIRBUS - Customer Services Directorate

Fax No.: 33 (0) 5 61 93 28 06

Sita No.: TLSBP7X

E-mail: sb.reporting@airbus.com

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

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

our Customer Services Directorate (SEDCC).

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 13

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SERVICE BULLETIN

M. SPARES

Placard D11311171A00

Placard D11311293A00

Placard D11311356A00

Placard D11311370A00

Plate-Assy D9251335500000

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 14

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 321349A01R01

Kit 321349A02R00

Kit 321349A03R00

Kit 321349A04R00

Kit 321349A05R00

Kit 321349A06R00

AIRBUS

Spares Support and Services

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 25 90

(2) Price and Availability

Kit 321349A01R01

Cost 8,110.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 321349A02R00

Cost 128.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 321349A03R00

Cost 128.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 15

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The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 321349A04R00

Cost 128.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 321349A05R00

Cost 128.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

Kit 321349A06R00

Cost 82.00 USD

Availability 60 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kit(s) before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

For Kit 321349A01R01, AIRBUS will provide a 15% reduction to the applicable sales prices

given in paragraph 2 A (2) for orders placed before Dec 31/14.

C. LIST OF COMPONENTS

Kit 321349A01R01

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

NOTES

1 NSA931324-075 2 C/B

3 ASNA2080G01 5 Button

4 ASNA2080G04 5 Button

13 E0217XUU001A 1 Relay

14 E0219ASXUU 1 Base

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 16

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

NOTES

15 MS21042-04 3 Nut

16 E0425A2001 1 Module

21 D9251719400095 1 Plate

22 NAS1801-3-8 8 Screw

23 NAS1149F0332P 10 Washer

24 NSA5050-3 10 Nut

25 NSA935504-01 2 Mount

26 NSA5515-11 2 Clamp

27 NAS1801-3-13 2 Screw

36 EN3646A61210BW 1 CNCTR

37 ABS0638A12 2 BACKSHLL

38 EN3646A61210BN 1 CNCTR

D9000095223495 1 Bundle

D9100095213795 1 Set

NSA935401-03 850 Tie

NSA935401-05 850 Tie

NSA935401-08 600 Tie

NSA937901FM 2 Module

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.

Kit 321349A02R00

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

NOTES

2 D11311628A00 1 Placard (2) D11311171A00

Kit 321349A03R00

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

NOTES

2 D11311631A00 1 Placard (2) D11311293A00

Kit 321349A04R00

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

NOTES

2 D11311636A00 1 Placard (2) D11311356A00

Kit 321349A05R00

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

NOTES

2 D11312010A00 1 Placard (2) D11311370A00

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 17

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Kit 321349A06R00

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

NOTES

D9000095224595 1 Bundle

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA11

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petrolatum

04-012 As required

Electrical Bonding Coating (Blue

Color)

07-001 As required

Dry Cleaning Solvent (Varsol/White

Spirit)

11-002 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

To accomplish this Service Bulletin it will be necessary to use the tooling listed in AMM

32-31-00, Page Block 501.

(3) Special Tools

None

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 18

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 321349-831-896-001 - MODIFICATION

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.

Task Associated Data

**CONF 001

Zone

120 210

From 210 to 120

Modified FIN

48GA 48GAA 48GAA8 56GA 57GA 58GA 59GA 62GA 62GAA 31LM 201VCA

201VCA1 203VCA 203VCA1 679VG 217VT 217VT9 217VT10 217VT91

Access

Door 811 812 822 831

Manpower

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF 002

Zone

120 210

From 210 to 120

Modified FIN

48GA 48GAA 48GAA8 56GA 57GA 58GA 59GA 62GA 62GAA 31LM 201VCA

201VCA1 203VCA 203VCA1 679VG 217VT 217VT9 217VT10 217VT91

Access

Door 811 812 822 831

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 19

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Manpower

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF 003

Zone

120 210

From 210 to 120

Modified FIN

48GA 48GAA 48GAA8 56GA 57GA 58GA 59GA 62GA 62GAA 31LM 201VCA

201VCA1 203VCA 203VCA1 679VG 217VT 217VT9 217VT10 217VT91

Access

Door 811 812 822 831

Manpower

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF 004

Zone

120 210

From 210 to 120

Modified FIN

48GA 48GAA 48GAA8 56GA 57GA 58GA 59GA 62GA 62GAA 31LM 201VCA

201VCA1 203VCA 203VCA1 679VG 217VT 217VT9 217VT10 217VT91

Access

Door 811 812 822 831

Manpower

TOTAL MANHOURS 48.00

ELAPSED TIME (HOURS) 33.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 321349-910-001-001 - STANDARD PRACTICES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 20

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Material necessary to do the job

Consumable CMLA11

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petrolatum

04-012 As required

Electrical Bonding Coating

(Blue Color)

07-001 As required

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-11, Page Block 201

20-21-15, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

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

20-33-00

20-33-44

20-52-21

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11

51-44-11

(a) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin, refer to the Consumable Material List (CML).

(b) For the frames (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of the access panels, refer to AMM 06-41-53, Page Block 001.

(d) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(e) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(f) 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 the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(g) Drill and deburr the holes (Refer to SRM 51-44-11).

(h) Remove/install the fasteners (Refer to SRM 51-42-11).

(i) Torque the standard threaded fasteners (Refer to AMM 20-21-11, Page Block 201).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 21

7

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SERVICE BULLETIN

(j) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 001.

(k) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201) with

Pure Mineral

Vaseline Or

Petrolatum

04-012 As required

and

Electrical Bonding

Coating (Blue

Color)

07-001 As required

(l) For the installation of the placards, refer to AMM 11-00-00, Page Block 201.

(m) Clean the surfaces at the location of the placards with

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(n) Obey the instructions for the general installation of electrical wire harness (Refer to

ESPM 20-33-00).

(o) Put blanking caps on the disconnected electrical connectors.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(q) Route the new wires with the wires that are in the aircraft.

(r) Use existing spare conduits to route wires in locations difficult to get access to.

(s) Do a continuity test of the modified and the new wires (Refer to ESPM 20-52-21).

(t) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(2) Subtask 321349-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 321349-910-001-001 - STANDARD PRACTICES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 22

7

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

Material necessary to do the job

Consumable CMLA11

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petrolatum

04-012 As required

Electrical Bonding Coating

(Blue Color)

07-001 As required

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-11, Page Block 201

20-21-15, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

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

20-33-00

20-33-44

20-52-21

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11

51-44-11

(a) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin, refer to the Consumable Material List (CML).

(b) For the frames (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of the access panels, refer to AMM 06-41-53, Page Block 001.

(d) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(e) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(f) 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 the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(g) Drill and deburr the holes (Refer to SRM 51-44-11).

(h) Remove/install the fasteners (Refer to SRM 51-42-11).

(i) Torque the standard threaded fasteners (Refer to AMM 20-21-11, Page Block 201).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 23

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(j) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 001.

(k) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201) with

Pure Mineral

Vaseline Or

Petrolatum

04-012 As required

and

Electrical Bonding

Coating (Blue

Color)

07-001 As required

(l) For the installation of the placards, refer to AMM 11-00-00, Page Block 201.

(m) Clean the surfaces at the location of the placards with

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(n) Obey the instructions for the general installation of electrical wire harness (Refer to

ESPM 20-33-00).

(o) Put blanking caps on the disconnected electrical connectors.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(q) Route the new wires with the wires that are in the aircraft.

(r) Use existing spare conduits to route wires in locations difficult to get access to.

(s) Do a continuity test of the modified and the new wires (Refer to ESPM 20-52-21).

(t) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(2) Subtask 321349-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 321349-910-001-001 - STANDARD PRACTICES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 24

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA11

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petrolatum

04-012 As required

Electrical Bonding Coating

(Blue Color)

07-001 As required

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-11, Page Block 201

20-21-15, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

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

20-33-00

20-33-44

20-52-21

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11

51-44-11

(a) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin, refer to the Consumable Material List (CML).

(b) For the frames (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of the access panels, refer to AMM 06-41-53, Page Block 001.

(d) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(e) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(f) 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 the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(g) Drill and deburr the holes (Refer to SRM 51-44-11).

(h) Remove/install the fasteners (Refer to SRM 51-42-11).

(i) Torque the standard threaded fasteners (Refer to AMM 20-21-11, Page Block 201).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 25

7

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@A318/A319/A320/A321

SERVICE BULLETIN

(j) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 001.

(k) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201) with

Pure Mineral

Vaseline Or

Petrolatum

04-012 As required

and

Electrical Bonding

Coating (Blue

Color)

07-001 As required

(l) For the installation of the placards, refer to AMM 11-00-00, Page Block 201.

(m) Clean the surfaces at the location of the placards with

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(n) Obey the instructions for the general installation of electrical wire harness (Refer to

ESPM 20-33-00).

(o) Put blanking caps on the disconnected electrical connectors.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(q) Route the new wires with the wires that are in the aircraft.

(r) Use existing spare conduits to route wires in locations difficult to get access to.

(s) Do a continuity test of the modified and the new wires (Refer to ESPM 20-52-21).

(t) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(2) Subtask 321349-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 321349-910-001-001 - STANDARD PRACTICES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 26

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA11

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Pure Mineral Vaseline Or

Petrolatum

04-012 As required

Electrical Bonding Coating

(Blue Color)

07-001 As required

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

20-21-11, Page Block 201

20-21-15, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

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

20-33-00

20-33-44

20-52-21

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11

51-44-11

(a) For the specification of the material numbers (Mat. No.) that you must use in this

Service Bulletin, refer to the Consumable Material List (CML).

(b) For the frames (FR) identification, refer to AMM 06-31-53, Page Block 001.

(c) For the identification of the access panels, refer to AMM 06-41-53, Page Block 001.

(d) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(e) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(f) 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 the

Standards Manual (SM). The SM will give you the correct part number to part

number relationship.

(g) Drill and deburr the holes (Refer to SRM 51-44-11).

(h) Remove/install the fasteners (Refer to SRM 51-42-11).

(i) Torque the standard threaded fasteners (Refer to AMM 20-21-11, Page Block 201).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 27

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(j) To torque tighten the electrical component fasteners, refer to AMM 20-21-15, Page

Block 001.

(k) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201) with

Pure Mineral

Vaseline Or

Petrolatum

04-012 As required

and

Electrical Bonding

Coating (Blue

Color)

07-001 As required

(l) For the installation of the placards, refer to AMM 11-00-00, Page Block 201.

(m) Clean the surfaces at the location of the placards with

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(n) Obey the instructions for the general installation of electrical wire harness (Refer to

ESPM 20-33-00).

(o) Put blanking caps on the disconnected electrical connectors.

(p) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(q) Route the new wires with the wires that are in the aircraft.

(r) Use existing spare conduits to route wires in locations difficult to get access to.

(s) Do a continuity test of the modified and the new wires (Refer to ESPM 20-52-21).

(t) For the cable tie application and tooling (Refer to ESPM 20-33-44 and ESPM

20-25-51).

(2) Subtask 321349-839-001-001 - DOCUMENTATION

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 28

7

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SERVICE BULLETIN

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 321349-941-001-001 - JOB SET-UP

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

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

(2) Subtask 321349-010-001-001 - REMOVE/OPEN FOR ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) Open the FWD passenger/crew door 831 (Refer to AMM 52-10-00, Page Block

201).

(b) Open the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(c) In the cockpit, remove the sidewall panels 212JW and 212HW (Refer to AMM

25-13-41, Page Block 401).

(d) In the cockpit, remove the ceiling panels 212FC and 211HC (Refer to AMM

25-13-41, Page Block 401).

(e) In the cockpit, remove the third occupant seat 14MM (Refer to AMM 25-11-41,

Page Block 401).

(3) Subtask 321349-862-001-001 - DE-ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 29

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(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on the external power receptacle to

tell persons not to connect an external power source.

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

position.

(d) In the cockpit, on the overhead panel 35VU release the 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 the 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 Auxiliary Power

Unit (APU).

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1, 2.

(i) Battery de-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Turn the knurled nut a quarter turn.

3 Disconnect the connectors.

4 Put blanking caps on the disconnected electrical connectors.

(4) Subtask 321349-941-002-001 - PREPARATION PROCEDURES

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the preparation procedure as specified in the removal/installation of the

Generator Control Units 1 and 2 (GCU 1 and 2) FIN 1XU1 and 1XU2 (if installed)

(Refer to AMM 24-22-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 30

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SERVICE BULLETIN

(b) Do the preparation procedure as specified in the removal/installation of the GCU

APU FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the preparation procedure as specified in the removal/installation of the Spoiler

Elevator Computer 3 (SEC 3) FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

(d) Do the preparation procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the preparation procedure as specified in the removal/installation of the LGCIU

1 and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block

401).

(f) Do the preparation procedure as specified in the removal/installation of the Tire

Pressure Indicating Computer (TPIS) detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

(g) Do the preparation procedure as specified in the removal/installation of the Smoke

Detection Control Unit (SDCU) FIN 10WQ (if installed) (Refer to AMM 26-17-34,

Page Block 401).

(h) Do the preparation procedure as specified in the removal/installation of the

Braking/Steering Control Unit (BSCU) FIN 10GG (if installed) (Refer to AMM

32-42-34, Page Block 401).

(i) Do the preparation procedure as specified in the removal/installation of the aft

cargo heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block

401).

(j) Do the preparation procedure as specified in the removal/installation of the

Auxiliary Fuel Management Computer (AFMC) FIN 2QN (if installed) (Refer to AMM

28-51-35, Page Block 401).

**CONF 002

(1) Subtask 321349-941-001-001 - JOB SET-UP

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

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

(2) Subtask 321349-010-001-001 - REMOVE/OPEN FOR ACCESS

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 31

7

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) Open the FWD passenger/crew door 831 (Refer to AMM 52-10-00, Page Block

201).

(b) Open the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(c) In the cockpit, remove the sidewall panels 212JW and 212HW (Refer to AMM

25-13-41, Page Block 401).

(d) In the cockpit, remove the ceiling panels 212FC and 211HC (Refer to AMM

25-13-41, Page Block 401).

(e) In the cockpit, remove the third occupant seat 14MM (Refer to AMM 25-11-41,

Page Block 401).

(3) Subtask 321349-862-001-001 - DE-ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on the external power receptacle to

tell persons not to connect an external power source.

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

position.

(d) In the cockpit, on the overhead panel 35VU release the 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 the 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 Auxiliary Power

Unit (APU).

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1, 2.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 32

7

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SERVICE BULLETIN

(i) Battery de-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Turn the knurled nut a quarter turn.

3 Disconnect the connectors.

4 Put blanking caps on the disconnected electrical connectors.

(4) Subtask 321349-941-002-001 - PREPARATION PROCEDURES

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the preparation procedure as specified in the removal/installation of the

Generator Control Units 1 and 2 (GCU 1 and 2) FIN 1XU1 and 1XU2 (if installed)

(Refer to AMM 24-22-34, Page Block 401).

(b) Do the preparation procedure as specified in the removal/installation of the GCU

APU FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the preparation procedure as specified in the removal/installation of the Spoiler

Elevator Computer 3 (SEC 3) FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

(d) Do the preparation procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the preparation procedure as specified in the removal/installation of the LGCIU

1 and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block

401).

(f) Do the preparation procedure as specified in the removal/installation of the Tire

Pressure Indicating Computer (TPIS) detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

(g) Do the preparation procedure as specified in the removal/installation of the Smoke

Detection Control Unit (SDCU) FIN 10WQ (if installed) (Refer to AMM 26-17-34,

Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 33

7

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@A318/A319/A320/A321

SERVICE BULLETIN

(h) Do the preparation procedure as specified in the removal/installation of the

Braking/Steering Control Unit (BSCU) FIN 10GG (if installed) (Refer to AMM

32-42-34, Page Block 401).

(i) Do the preparation procedure as specified in the removal/installation of the aft

cargo heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block

401).

(j) Do the preparation procedure as specified in the removal/installation of the

Auxiliary Fuel Management Computer (AFMC) FIN 2QN (if installed) (Refer to AMM

28-51-35, Page Block 401).

**CONF 003

(1) Subtask 321349-941-001-001 - JOB SET-UP

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

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

(2) Subtask 321349-010-001-001 - REMOVE/OPEN FOR ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) Open the FWD passenger/crew door 831 (Refer to AMM 52-10-00, Page Block

201).

(b) Open the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(c) In the cockpit, remove the sidewall panels 212JW and 212HW (Refer to AMM

25-13-41, Page Block 401).

(d) In the cockpit, remove the ceiling panels 212FC and 211HC (Refer to AMM

25-13-41, Page Block 401).

(e) In the cockpit, remove the third occupant seat 14MM (Refer to AMM 25-11-41,

Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 34

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(3) Subtask 321349-862-001-001 - DE-ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

(b) Make sure that there is (are) warning notice(s) on the external power receptacle to

tell persons not to connect an external power source.

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

position.

(d) In the cockpit, on the overhead panel 35VU release the 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 the 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 Auxiliary Power

Unit (APU).

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1, 2.

(i) Battery de-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Turn the knurled nut a quarter turn.

3 Disconnect the connectors.

4 Put blanking caps on the disconnected electrical connectors.

(4) Subtask 321349-941-002-001 - PREPARATION PROCEDURES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 35

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References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the preparation procedure as specified in the removal/installation of the

Generator Control Units 1 and 2 (GCU 1 and 2) FIN 1XU1 and 1XU2 (if installed)

(Refer to AMM 24-22-34, Page Block 401).

(b) Do the preparation procedure as specified in the removal/installation of the GCU

APU FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the preparation procedure as specified in the removal/installation of the Spoiler

Elevator Computer 3 (SEC 3) FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

(d) Do the preparation procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the preparation procedure as specified in the removal/installation of the LGCIU

1 and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block

401).

(f) Do the preparation procedure as specified in the removal/installation of the Tire

Pressure Indicating Computer (TPIS) detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

(g) Do the preparation procedure as specified in the removal/installation of the Smoke

Detection Control Unit (SDCU) FIN 10WQ (if installed) (Refer to AMM 26-17-34,

Page Block 401).

(h) Do the preparation procedure as specified in the removal/installation of the

Braking/Steering Control Unit (BSCU) FIN 10GG (if installed) (Refer to AMM

32-42-34, Page Block 401).

(i) Do the preparation procedure as specified in the removal/installation of the aft

cargo heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block

401).

(j) Do the preparation procedure as specified in the removal/installation of the

Auxiliary Fuel Management Computer (AFMC) FIN 2QN (if installed) (Refer to AMM

28-51-35, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 36

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**CONF 004

(1) Subtask 321349-941-001-001 - JOB SET-UP

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24, Page

Block 201).

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

(2) Subtask 321349-010-001-001 - REMOVE/OPEN FOR ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) Open the FWD passenger/crew door 831 (Refer to AMM 52-10-00, Page Block

201).

(b) Open the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(c) In the cockpit, remove the sidewall panels 212JW and 212HW (Refer to AMM

25-13-41, Page Block 401).

(d) In the cockpit, remove the ceiling panels 212FC and 211HC (Refer to AMM

25-13-41, Page Block 401).

(e) In the cockpit, remove the third occupant seat 14MM (Refer to AMM 25-11-41,

Page Block 401).

(3) Subtask 321349-862-001-001 - DE-ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PW.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(b) Make sure that there is (are) warning notice(s) on the external power receptacle to

tell persons not to connect an external power source.

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

position.

(d) In the cockpit, on the overhead panel 35VU release the 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 the 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 Auxiliary Power

Unit (APU).

(h) Put a warning notice in the cockpit to tell persons not to start the ENG1, 2.

(i) Battery de-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Turn the knurled nut a quarter turn.

3 Disconnect the connectors.

4 Put blanking caps on the disconnected electrical connectors.

(4) Subtask 321349-941-002-001 - PREPARATION PROCEDURES

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the preparation procedure as specified in the removal/installation of the

Generator Control Units 1 and 2 (GCU 1 and 2) FIN 1XU1 and 1XU2 (if installed)

(Refer to AMM 24-22-34, Page Block 401).

(b) Do the preparation procedure as specified in the removal/installation of the GCU

APU FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(c) Do the preparation procedure as specified in the removal/installation of the Spoiler

Elevator Computer 3 (SEC 3) FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

(d) Do the preparation procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the preparation procedure as specified in the removal/installation of the LGCIU

1 and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block

401).

(f) Do the preparation procedure as specified in the removal/installation of the Tire

Pressure Indicating Computer (TPIS) detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

(g) Do the preparation procedure as specified in the removal/installation of the Smoke

Detection Control Unit (SDCU) FIN 10WQ (if installed) (Refer to AMM 26-17-34,

Page Block 401).

(h) Do the preparation procedure as specified in the removal/installation of the

Braking/Steering Control Unit (BSCU) FIN 10GG (if installed) (Refer to AMM

32-42-34, Page Block 401).

(i) Do the preparation procedure as specified in the removal/installation of the aft

cargo heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block

401).

(j) Do the preparation procedure as specified in the removal/installation of the

Auxiliary Fuel Management Computer (AFMC) FIN 2QN (if installed) (Refer to AMM

28-51-35, Page Block 401).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 321349-010-002-001 - Remove the equipment for access in the cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Remove as shown in detail B :

1 Panel-RH Lateral Item (28) Retain

attached with :

1 Screw Item (29) Retain

1 Nut Item (30) Retain

2 Screw Item (31) Retain

(b) Remove as shown in detail C :

FIN 702VU

1 Console Item (32) Retain

attached with :

4 Screw Item (33) Retain

4 Washer Item (34) Retain

(2) Subtask 321349-010-003-001 - Remove the equipment for access in the avionics

compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Panel 90VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 40

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References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Remove the shelf 91VU.

1 Remove and retain the GCU 1 and 2 FIN 1XU1 and 1XU2 (if installed) (Refer

to AMM 24-22-34, Page Block 401).

2 Remove and retain the GCU APU FIN 1XS (if installed) (Refer to AMM

24-23-34, Page Block 401).

3 Disconnect the shelf cut-off connectors and install protective caps.

4 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(b) Remove the shelf 93VU.

1 Remove and retain the SEC 3 FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

2 Remove and retain the zone controller FIN 8HK (if installed) (Refer to AMM

21-63-34, Page Block 401).

3 Remove and retain the LGCIU 1 FIN 5GA1 (if installed) (Refer to AMM

32-31-71, Page Block 401).

4 Disconnect the shelf cut-off connectors and install protective caps.

5 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(c) Remove the shelf 94VU.

1 Remove and retain the LGCIU 2 FIN 5GA2 (if installed) (Refer to AMM

32-31-71, Page Block 401).

2 Remove and retain the TPIS detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

3 Remove and retain the SDCU FIN 10WQ (if installed) (Refer to AMM

26-17-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 41

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4 Remove and retain the BSCU FIN 10GG (if installed) (Refer to AMM 32-42-34,

Page Block 401).

5 Remove and retain the aft cargo heat controller FIN 10HC (if installed) (Refer

to AMM 21-43-34, Page Block 401).

6 Remove and retain the AFMC FIN 2QN (if installed) (Refer to AMM 28-51-35,

Page Block 401).

7 Disconnect the shelf cut-off connectors and install protective caps.

8 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(3) Subtask 321349-831-001-001 - Install the new grounding points in the avionics

compartment at FR10.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811, Door 812

Work location Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9100095213795 Set

References

Fig. A-FACAA

Installation of the New Grounding Points

at FR10 in AVNCS Compartment

Sheet 01

Sheet 02

(a) Drill 2 holes on the structure at FR10 to the dimensions given in Fig. A-FACAA

Sheet 01 and Fig. A-FACAA Sheet 02.

(b) Do 2 stripping dia. 14mm (0.551in.) as shown in Fig. A-FACAA Sheet 02.

(c) Near the new holes, as shown in Fig. A-FACAA Sheet 02, bond the placards

identified 1037VN and 1039VN, supplied in :

Placard Set D9100095213795

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 42

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(4) Subtask 321349-831-002-001 - Modify the equipment and the wiring in the C/B

panel 121VU.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Work location Electrical panel 121VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA931324-075 2 C/B

3 ASNA2080G01 5 Button

4 ASNA2080G04 5 Button

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 50 Tie

NSA935401-05 50 Tie

Kit 321349A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 D11311628A00 1 Placard

References

Fig. A-FADAA

Modification of the Equipment in the C/B

Panel 121VU

Sheet 01

Fig. A-FBAAA

Modification of the Wiring in the C/B

Panel 121VU

Sheet 01

Sheet 02

Sheet 03

(a) Install the C/B 58GA and 59GA.

1 At position R25, install :

FIN 58GA

1 Circuit Breaker NSA931324-075 Item 1

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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2 At position R26, install :

FIN 59GA

1 Circuit Breaker NSA931324-075 Item 1

3 Near the new C/B, bond the placards identified 58GA and 59GA, supplied in :

Placard Set D9100095213795

(b) Replace the placard 31LM (line R).

1 Remove :

FIN 31LM

1 Placard D11311171A00 Item (2) Discard

attached with :

5 Button-Rivet Plastic ASNA2080G01 Item (3) Discard

or

5 Button-Rivet Plastic ASNA2080G04 Item (4) Discard

2 Install :

FIN 31LM

1 Placard D11311628A00 Item 2

attach with :

5 Button-Rivet Plastic ASNA2080G01 Item 3

or

5 Button-Rivet Plastic ASNA2080G04 Item 4

(c) Modify the wiring.

1 Modify the connections of the wires as shown on the wiring diagram Fig. AFBAAA Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBAAA Sheet 03).

2 Install the wires as shown on the wiring diagrams Fig. A-FBAAA Sheet 01 and

Fig. A-FBAAA Sheet 02 and as given in the hook-up chart lines :

- 8 thru 13 (Refer to Fig. A-FBAAA Sheet 03), supplied in :

Bundle D9000095223495

3 Attach the wires with :

50 Tie-Cable NSA935401-03

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 44

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50 Tie-Cable NSA935401-05

(5) Subtask 321349-831-003-001 - Modify the equipment and the wiring in the shelf

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 93VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 E0217XUU001A 1 Relay

14 E0219ASXUU 1 Base

15 MS21042-04 3 Nut

16 E0425A2001 1 Module

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA937901FM 2 Module

Kit 321349A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095224595 Bundle

References

Fig. A-FAEAA

Modification of the Equipment in the

Shelf 93VU

Sheet 01

Sheet 02

Fig. A-FBBAA

Modification of the Wiring in the Shelf

93VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(a) Remove the relay 48GA.

1 Remove as shown in Fig. A-FAEAA Sheet 01 :

FIN 48GA

1 Relay Item (5) Discard

FIN 48GAA

1 Base Item (6) Discard

FIN 48GAA8

1 Retainer Assy Item (7) Discard

2 Remove the placard identified 48GA.

(b) Modify the terminal block 217VT.

1 Remove from position 9, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT9

1 Module Item (10) Discard

and

FIN 57GA

1 Capacitor Item (9) Discard

2 Remove from position 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT10

1 Module Item (12) Discard

and

FIN 56GA

1 Resistor Item (8) Discard

3 Remove between positions 9 and 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT91

1 Plate-Module Item (11) Discard

4 Install in replacement at positions 9 and 10 :

2 Module-False NSA937901FM

(c) Install the relay 62GA.

1 Install at position B23, as shown in Fig. A-FAEAA Sheet 02 :

FIN 62GA

1 Relay E0217XUU001A Item 13

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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FIN 62GAA

1 Base E0219ASXUU Item 14

attach with :

3 Nut MS21042-04 Item 15

2 Near the new relay, bond the placard identified 62GA, supplied in :

Placard Set D9100095213795

(d) Install the grounding module 679VG.

1 Install as shown in Fig. A-FAEAA Sheet 02 :

FIN 679VG

1 Module-Grounding E0425A2001 Item 16

2 Near the new grounding module, bond the placard identified 679VG, supplied

in :

Placard Set D9100095213795

(e) Modify the wiring.

1 Remove the wires as shown on the wiring diagram Fig. A-FBBAA Sheet 01,

Fig. A-FBBAA Sheet 03 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FBBAA Sheet 04).

2 Install the wires as shown on the wiring diagrams Fig. A-FBBAA Sheet 02 and

Fig. A-FBBAA Sheet 03 and as given in the hook-up charts lines :

- 17 thru 23 (Refer to Fig. A-FBBAA Sheet 04), supplied in :

Bundle D9000095223495

Bundle D9000095224595

3 Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

(6) Subtask 321349-831-004-001 - Modify the wiring in the shelf 94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 47

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FBCAA

Modification of the Wiring in the Shelf

94VU

Sheet 01

Sheet 02

(a) Install the wire as shown on the wiring diagram Fig. A-FBCAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBCAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(7) Subtask 321349-831-005-001 - Modify the equipment in the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 91VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 48

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Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 D9251719400095 1 Plate

22 NAS1801-3-8 6 Screw

23 NAS1149F0332P 8 Washer

24 NSA5050-3 8 Nut

25 NSA935504-01 2 Mount

26 NSA5515-11 2 Clamp

27 NAS1801-3-13 2 Screw

36 EN3646A61210BW 1 CNCTR

37 ABS0638A12 2 BACKSHLL

38 EN3646A61210BN 1 CNCTR

References

Fig. A-FAFAA

Modification of the Equipment in the

Shelf 91VU

Sheet 01

Sheet 02

Fig. A-FBJAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

Fig. A-FBKAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

(a) Disconnect the draining pipe from the blanking plate Item (17).

NOTE: Discard the attachment parts.

(b) Remove as shown in Fig. A-FAFAA Sheet 01 detail B :

1 Plate-Assy D9251335500000 Item (17) Discard

attached with :

6 Screw Item (22) Discard

6 Washer Item (23) Discard

6 Nut Item (24) Discard

(c) Install as shown in Fig. A-FAFAA Sheet 02 detail C :

1 Plate-LGCIU D9251719400095 Item 21

attach with :

6 Screw NAS1801-3-8 Item 22

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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6 Washer NAS1149F0332P Item 23

6 Nut NSA5050-3 Item 24

NOTE: For the internal wiring of the LGCIU plate, refer to Fig. A-FBJAA

Sheet 01 and Fig. A-FBKAA Sheet 01.

Install at the rear of the new LGCIU plate Item 21 :

FIN 201VCA

1 Connector-Plug EN3646A61210BW Item 36

FIN 201VCA1

1 Backshell-Connector ABS0638A12 Item 37

FIN 203VCA

1 Connector-Plug EN3646A61210BN Item 38

FIN 203VCA1

1 Backshell-Connector ABS0638A12 Item 37

(d) Install as shown in Fig. A-FAFAA Sheet 02 detail D :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

(e) Install as shown in Fig. A-FAFAA Sheet 02 detail E :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 50

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SERVICE BULLETIN

(8) Subtask 321349-831-006-001 - Modify the wiring between the shelves 91VU and

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

93VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBDAA

Modification of the Wiring between the

Shelves 91VU and 93VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 3 (Refer to Fig. A-FBDAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 51

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SERVICE BULLETIN

(9) Subtask 321349-831-007-001 - Modify the wiring between the shelves 91VU and

94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

94VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBEAA

Modification of the Wiring between the

Shelves 91VU and 94VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBEAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 52

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SERVICE BULLETIN

(10) Subtask 321349-831-008-001 - Modify the wiring between the shelf 91VU and the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

22 NAS1801-3-8 2 Screw

23 NAS1149F0332P 2 Washer

24 NSA5050-3 2 Nut

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBFAA

Modification of the Wiring between the

Shelf 91VU and the AVNCS

Compartment

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBFAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBFAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Connect the bonding points, as shown in Fig. A-FAGAA Sheet 01, with :

2 Screw NAS1801-3-8 Item 22

2 Washer NAS1149F0332P Item 23

2 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 53

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(c) Together with the new wires, install the identification plates 1037VN and 1039VN,

supplied in :

Bundle D9000095223495

(d) Attach the wires with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(11) Subtask 321349-831-009-001 - Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 90VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBGAA

Modification of the Wiring between the

Rear Panel 120VU and the FWD

Electronics Rack 90VU

Sheet 01

Sheet 02

(a) Remove the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBGAA Sheet 02).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 54

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(b) Install the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 2 (Refer to Fig. A-FBGAA Sheet 02), supplied in :

Bundle D9000095223495

(c) Attach the wire with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

(12) Subtask 321349-831-010-001 - Modify the wiring between the rear panel 120VU and

the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 91VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 300 Tie

NSA935401-05 300 Tie

NSA935401-08 300 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBHAA

Modification of the Wiring between the

Rear Panel 120VU and the Shelf 91VU

Sheet 01

Sheet 02

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 55

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(a) Install the wires as shown on the wiring diagram Fig. A-FBHAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBHAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Together with the new wires, install the identification plates 201VC-A and 203VC-A,

supplied in :

Bundle D9000095223495

(c) Attach the wires with :

300 Tie-Cable NSA935401-03

300 Tie-Cable NSA935401-05

300 Tie-Cable NSA935401-08

(13) Subtask 321349-410-001-001 - Install the equipment removed for access in the

cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Install as shown in detail B :

1 Panel-RH Lateral Item (28)

attach with :

1 Screw Item (29)

1 Nut Item (30)

2 Screw Item (31)

NOTE: All these items were retained at the removal.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 56

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(b) Install as shown in detail C :

FIN 702VU

1 Console Item (32)

attach with :

4 Screw Item (33)

4 Washer Item (34)

NOTE: All these items were retained at the removal.

(14) Subtask 321349-410-002-001 - Install the equipment removed for access in the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 90VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Install the shelf 91VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the GCU 1 and 2 FIN 1XU1 and 1XU2 (if removed) (Refer to AMM

24-22-34, Page Block 401).

3 Install the GCU APU FIN 1XS (if removed) (Refer to AMM 24-23-34, Page

Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 57

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4 Remove the protective caps and connect the shelf cut-off connectors.

(b) Install the shelf 93VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the SEC 3 FIN 1CE3 (if removed) (Refer to AMM 27-94-34, Page Block

401).

3 Install the zone controller FIN 8HK (if removed) (Refer to AMM 21-63-34,

Page Block 401.

4 Install the LGCIU 1 FIN 5GA1 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

5 Remove the protective caps and connect the shelf cut-off connectors.

(c) Install the shelf 94VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the LGCIU 2 FIN 5GA2 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

3 Install the TPIS detection unit FIN 2GV (if removed) (Refer to AMM 32-49-34,

Page Block 401).

4 Install the SDCU FIN 10WQ (if removed) (Refer to AMM 26-17-34, Page Block

401).

5 Install the BSCU FIN 10GG (if removed) (Refer to AMM 32-42-34, Page Block

401).

6 Install the aft cargo heat controller FIN 10HC (if removed) (Refer to AMM

21-43-34, Page Block 401).

7 Install the AFMC FIN 2QN (if removed) (Refer to AMM 28-51-35, Page Block

401).

8 Remove the protective caps and connect the shelf cut-off connectors.

**CONF 002

(1) Subtask 321349-010-002-001 - Remove the equipment for access in the cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 58

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Remove as shown in detail B :

1 Panel-RH Lateral Item (28) Retain

attached with :

1 Screw Item (29) Retain

1 Nut Item (30) Retain

2 Screw Item (31) Retain

(b) Remove as shown in detail C :

FIN 702VU

1 Console Item (32) Retain

attached with :

4 Screw Item (33) Retain

4 Washer Item (34) Retain

(2) Subtask 321349-010-003-001 - Remove the equipment for access in the avionics

compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Panel 90VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 59

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Remove the shelf 91VU.

1 Remove and retain the GCU 1 and 2 FIN 1XU1 and 1XU2 (if installed) (Refer

to AMM 24-22-34, Page Block 401).

2 Remove and retain the GCU APU FIN 1XS (if installed) (Refer to AMM

24-23-34, Page Block 401).

3 Disconnect the shelf cut-off connectors and install protective caps.

4 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(b) Remove the shelf 93VU.

1 Remove and retain the SEC 3 FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

2 Remove and retain the zone controller FIN 8HK (if installed) (Refer to AMM

21-63-34, Page Block 401).

3 Remove and retain the LGCIU 1 FIN 5GA1 (if installed) (Refer to AMM

32-31-71, Page Block 401).

4 Disconnect the shelf cut-off connectors and install protective caps.

5 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(c) Remove the shelf 94VU.

1 Remove and retain the LGCIU 2 FIN 5GA2 (if installed) (Refer to AMM

32-31-71, Page Block 401).

2 Remove and retain the TPIS detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

3 Remove and retain the SDCU FIN 10WQ (if installed) (Refer to AMM

26-17-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 60

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4 Remove and retain the BSCU FIN 10GG (if installed) (Refer to AMM 32-42-34,

Page Block 401).

5 Remove and retain the aft cargo heat controller FIN 10HC (if installed) (Refer

to AMM 21-43-34, Page Block 401).

6 Remove and retain the AFMC FIN 2QN (if installed) (Refer to AMM 28-51-35,

Page Block 401).

7 Disconnect the shelf cut-off connectors and install protective caps.

8 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(3) Subtask 321349-831-001-001 - Install the new grounding points in the avionics

compartment at FR10.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811, Door 812

Work location Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9100095213795 Set

References

Fig. A-FACAA

Installation of the New Grounding Points

at FR10 in AVNCS Compartment

Sheet 01

Sheet 02

(a) Drill 2 holes on the structure at FR10 to the dimensions given in Fig. A-FACAA

Sheet 01 and Fig. A-FACAA Sheet 02.

(b) Do 2 stripping dia. 14mm (0.551in.) as shown in Fig. A-FACAA Sheet 02.

(c) Near the new holes, as shown in Fig. A-FACAA Sheet 02, bond the placards

identified 1037VN and 1039VN, supplied in :

Placard Set D9100095213795

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 61

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SERVICE BULLETIN

(4) Subtask 321349-831-002-002 - Modify the equipment and the wiring in the C/B

panel 121VU.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Work location Electrical panel 121VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA931324-075 2 C/B

3 ASNA2080G01 5 Button

4 ASNA2080G04 5 Button

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 50 Tie

NSA935401-05 50 Tie

Kit 321349A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 D11311631A00 1 Placard

References

Fig. A-FADAA

Modification of the Equipment in the C/B

Panel 121VU

Sheet 01

Fig. A-FBAAA

Modification of the Wiring in the C/B

Panel 121VU

Sheet 01

Sheet 02

Sheet 03

(a) Install the C/B 58GA and 59GA.

1 At position R25, install :

FIN 58GA

1 Circuit Breaker NSA931324-075 Item 1

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 62

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2 At position R26, install :

FIN 59GA

1 Circuit Breaker NSA931324-075 Item 1

3 Near the new C/B, bond the placards identified 58GA and 59GA, supplied in :

Placard Set D9100095213795

(b) Replace the placard 31LM (line R).

1 Remove :

FIN 31LM

1 Placard D11311293A00 Item (2) Discard

attached with :

5 Button-Rivet Plastic ASNA2080G01 Item (3) Discard

or

5 Button-Rivet Plastic ASNA2080G04 Item (4) Discard

2 Install :

FIN 31LM

1 Placard D11311631A00 Item 2

attach with :

5 Button-Rivet Plastic ASNA2080G01 Item 3

or

5 Button-Rivet Plastic ASNA2080G04 Item 4

(c) Modify the wiring.

1 Modify the connections of the wires as shown on the wiring diagram Fig. AFBAAA Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBAAA Sheet 03).

2 Install the wires as shown on the wiring diagrams Fig. A-FBAAA Sheet 01 and

Fig. A-FBAAA Sheet 02 and as given in the hook-up chart lines :

- 8 thru 13 (Refer to Fig. A-FBAAA Sheet 03), supplied in :

Bundle D9000095223495

3 Attach the wires with :

50 Tie-Cable NSA935401-03

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 63

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50 Tie-Cable NSA935401-05

(5) Subtask 321349-831-003-001 - Modify the equipment and the wiring in the shelf

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 93VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 E0217XUU001A 1 Relay

14 E0219ASXUU 1 Base

15 MS21042-04 3 Nut

16 E0425A2001 1 Module

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA937901FM 2 Module

Kit 321349A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095224595 Bundle

References

Fig. A-FAEAA

Modification of the Equipment in the

Shelf 93VU

Sheet 01

Sheet 02

Fig. A-FBBAA

Modification of the Wiring in the Shelf

93VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 64

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(a) Remove the relay 48GA.

1 Remove as shown in Fig. A-FAEAA Sheet 01 :

FIN 48GA

1 Relay Item (5) Discard

FIN 48GAA

1 Base Item (6) Discard

FIN 48GAA8

1 Retainer Assy Item (7) Discard

2 Remove the placard identified 48GA.

(b) Modify the terminal block 217VT.

1 Remove from position 9, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT9

1 Module Item (10) Discard

and

FIN 57GA

1 Capacitor Item (9) Discard

2 Remove from position 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT10

1 Module Item (12) Discard

and

FIN 56GA

1 Resistor Item (8) Discard

3 Remove between positions 9 and 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT91

1 Plate-Module Item (11) Discard

4 Install in replacement at positions 9 and 10 :

2 Module-False NSA937901FM

(c) Install the relay 62GA.

1 Install at position B23, as shown in Fig. A-FAEAA Sheet 02 :

FIN 62GA

1 Relay E0217XUU001A Item 13

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 65

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FIN 62GAA

1 Base E0219ASXUU Item 14

attach with :

3 Nut MS21042-04 Item 15

2 Near the new relay, bond the placard identified 62GA, supplied in :

Placard Set D9100095213795

(d) Install the grounding module 679VG.

1 Install as shown in Fig. A-FAEAA Sheet 02 :

FIN 679VG

1 Module-Grounding E0425A2001 Item 16

2 Near the new grounding module, bond the placard identified 679VG, supplied

in :

Placard Set D9100095213795

(e) Modify the wiring.

1 Remove the wires as shown on the wiring diagram Fig. A-FBBAA Sheet 01,

Fig. A-FBBAA Sheet 03 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FBBAA Sheet 04).

2 Install the wires as shown on the wiring diagrams Fig. A-FBBAA Sheet 02 and

Fig. A-FBBAA Sheet 03 and as given in the hook-up charts lines :

- 17 thru 23 (Refer to Fig. A-FBBAA Sheet 04), supplied in :

Bundle D9000095223495

Bundle D9000095224595

3 Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

(6) Subtask 321349-831-004-001 - Modify the wiring in the shelf 94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 66

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FBCAA

Modification of the Wiring in the Shelf

94VU

Sheet 01

Sheet 02

(a) Install the wire as shown on the wiring diagram Fig. A-FBCAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBCAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(7) Subtask 321349-831-005-001 - Modify the equipment in the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 91VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 67

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Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 D9251719400095 1 Plate

22 NAS1801-3-8 6 Screw

23 NAS1149F0332P 8 Washer

24 NSA5050-3 8 Nut

25 NSA935504-01 2 Mount

26 NSA5515-11 2 Clamp

27 NAS1801-3-13 2 Screw

36 EN3646A61210BW 1 CNCTR

37 ABS0638A12 2 BACKSHLL

38 EN3646A61210BN 1 CNCTR

References

Fig. A-FAFAA

Modification of the Equipment in the

Shelf 91VU

Sheet 01

Sheet 02

Fig. A-FBJAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

Fig. A-FBKAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

(a) Disconnect the draining pipe from the blanking plate Item (17).

NOTE: Discard the attachment parts.

(b) Remove as shown in Fig. A-FAFAA Sheet 01 detail B :

1 Plate-Assy D9251335500000 Item (17) Discard

attached with :

6 Screw Item (22) Discard

6 Washer Item (23) Discard

6 Nut Item (24) Discard

(c) Install as shown in Fig. A-FAFAA Sheet 02 detail C :

1 Plate-LGCIU D9251719400095 Item 21

attach with :

6 Screw NAS1801-3-8 Item 22

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 68

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6 Washer NAS1149F0332P Item 23

6 Nut NSA5050-3 Item 24

NOTE: For the internal wiring of the LGCIU plate, refer to Fig. A-FBJAA

Sheet 01 and Fig. A-FBKAA Sheet 01.

Install at the rear of the new LGCIU plate Item 21 :

FIN 201VCA

1 Connector-Plug EN3646A61210BW Item 36

FIN 201VCA1

1 Backshell-Connector ABS0638A12 Item 37

FIN 203VCA

1 Connector-Plug EN3646A61210BN Item 38

FIN 203VCA1

1 Backshell-Connector ABS0638A12 Item 37

(d) Install as shown in Fig. A-FAFAA Sheet 02 detail D :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

(e) Install as shown in Fig. A-FAFAA Sheet 02 detail E :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 69

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SERVICE BULLETIN

(8) Subtask 321349-831-006-001 - Modify the wiring between the shelves 91VU and

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

93VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBDAA

Modification of the Wiring between the

Shelves 91VU and 93VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 3 (Refer to Fig. A-FBDAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 70

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SERVICE BULLETIN

(9) Subtask 321349-831-007-001 - Modify the wiring between the shelves 91VU and

94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

94VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBEAA

Modification of the Wiring between the

Shelves 91VU and 94VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBEAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 71

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SERVICE BULLETIN

(10) Subtask 321349-831-008-001 - Modify the wiring between the shelf 91VU and the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

22 NAS1801-3-8 2 Screw

23 NAS1149F0332P 2 Washer

24 NSA5050-3 2 Nut

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBFAA

Modification of the Wiring between the

Shelf 91VU and the AVNCS

Compartment

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBFAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBFAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Connect the bonding points, as shown in Fig. A-FAGAA Sheet 01, with :

2 Screw NAS1801-3-8 Item 22

2 Washer NAS1149F0332P Item 23

2 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 72

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(c) Together with the new wires, install the identification plates 1037VN and 1039VN,

supplied in :

Bundle D9000095223495

(d) Attach the wires with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(11) Subtask 321349-831-009-001 - Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 90VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBGAA

Modification of the Wiring between the

Rear Panel 120VU and the FWD

Electronics Rack 90VU

Sheet 01

Sheet 02

(a) Remove the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBGAA Sheet 02).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 73

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(b) Install the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 2 (Refer to Fig. A-FBGAA Sheet 02), supplied in :

Bundle D9000095223495

(c) Attach the wire with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

(12) Subtask 321349-831-010-001 - Modify the wiring between the rear panel 120VU and

the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 91VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 300 Tie

NSA935401-05 300 Tie

NSA935401-08 300 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBHAA

Modification of the Wiring between the

Rear Panel 120VU and the Shelf 91VU

Sheet 01

Sheet 02

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 74

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(a) Install the wires as shown on the wiring diagram Fig. A-FBHAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBHAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Together with the new wires, install the identification plates 201VC-A and 203VC-A,

supplied in :

Bundle D9000095223495

(c) Attach the wires with :

300 Tie-Cable NSA935401-03

300 Tie-Cable NSA935401-05

300 Tie-Cable NSA935401-08

(13) Subtask 321349-410-001-001 - Install the equipment removed for access in the

cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Install as shown in detail B :

1 Panel-RH Lateral Item (28)

attach with :

1 Screw Item (29)

1 Nut Item (30)

2 Screw Item (31)

NOTE: All these items were retained at the removal.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 75

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(b) Install as shown in detail C :

FIN 702VU

1 Console Item (32)

attach with :

4 Screw Item (33)

4 Washer Item (34)

NOTE: All these items were retained at the removal.

(14) Subtask 321349-410-002-001 - Install the equipment removed for access in the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 90VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Install the shelf 91VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the GCU 1 and 2 FIN 1XU1 and 1XU2 (if removed) (Refer to AMM

24-22-34, Page Block 401).

3 Install the GCU APU FIN 1XS (if removed) (Refer to AMM 24-23-34, Page

Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 76

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4 Remove the protective caps and connect the shelf cut-off connectors.

(b) Install the shelf 93VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the SEC 3 FIN 1CE3 (if removed) (Refer to AMM 27-94-34, Page Block

401).

3 Install the zone controller FIN 8HK (if removed) (Refer to AMM 21-63-34,

Page Block 401.

4 Install the LGCIU 1 FIN 5GA1 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

5 Remove the protective caps and connect the shelf cut-off connectors.

(c) Install the shelf 94VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the LGCIU 2 FIN 5GA2 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

3 Install the TPIS detection unit FIN 2GV (if removed) (Refer to AMM 32-49-34,

Page Block 401).

4 Install the SDCU FIN 10WQ (if removed) (Refer to AMM 26-17-34, Page Block

401).

5 Install the BSCU FIN 10GG (if removed) (Refer to AMM 32-42-34, Page Block

401).

6 Install the aft cargo heat controller FIN 10HC (if removed) (Refer to AMM

21-43-34, Page Block 401).

7 Install the AFMC FIN 2QN (if removed) (Refer to AMM 28-51-35, Page Block

401).

8 Remove the protective caps and connect the shelf cut-off connectors.

**CONF 003

(1) Subtask 321349-010-002-001 - Remove the equipment for access in the cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 77

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Remove as shown in detail B :

1 Panel-RH Lateral Item (28) Retain

attached with :

1 Screw Item (29) Retain

1 Nut Item (30) Retain

2 Screw Item (31) Retain

(b) Remove as shown in detail C :

FIN 702VU

1 Console Item (32) Retain

attached with :

4 Screw Item (33) Retain

4 Washer Item (34) Retain

(2) Subtask 321349-010-003-001 - Remove the equipment for access in the avionics

compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Panel 90VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 78

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References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Remove the shelf 91VU.

1 Remove and retain the GCU 1 and 2 FIN 1XU1 and 1XU2 (if installed) (Refer

to AMM 24-22-34, Page Block 401).

2 Remove and retain the GCU APU FIN 1XS (if installed) (Refer to AMM

24-23-34, Page Block 401).

3 Disconnect the shelf cut-off connectors and install protective caps.

4 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(b) Remove the shelf 93VU.

1 Remove and retain the SEC 3 FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

2 Remove and retain the zone controller FIN 8HK (if installed) (Refer to AMM

21-63-34, Page Block 401).

3 Remove and retain the LGCIU 1 FIN 5GA1 (if installed) (Refer to AMM

32-31-71, Page Block 401).

4 Disconnect the shelf cut-off connectors and install protective caps.

5 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(c) Remove the shelf 94VU.

1 Remove and retain the LGCIU 2 FIN 5GA2 (if installed) (Refer to AMM

32-31-71, Page Block 401).

2 Remove and retain the TPIS detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

3 Remove and retain the SDCU FIN 10WQ (if installed) (Refer to AMM

26-17-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 79

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4 Remove and retain the BSCU FIN 10GG (if installed) (Refer to AMM 32-42-34,

Page Block 401).

5 Remove and retain the aft cargo heat controller FIN 10HC (if installed) (Refer

to AMM 21-43-34, Page Block 401).

6 Remove and retain the AFMC FIN 2QN (if installed) (Refer to AMM 28-51-35,

Page Block 401).

7 Disconnect the shelf cut-off connectors and install protective caps.

8 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(3) Subtask 321349-831-001-001 - Install the new grounding points in the avionics

compartment at FR10.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811, Door 812

Work location Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9100095213795 Set

References

Fig. A-FACAA

Installation of the New Grounding Points

at FR10 in AVNCS Compartment

Sheet 01

Sheet 02

(a) Drill 2 holes on the structure at FR10 to the dimensions given in Fig. A-FACAA

Sheet 01 and Fig. A-FACAA Sheet 02.

(b) Do 2 stripping dia. 14mm (0.551in.) as shown in Fig. A-FACAA Sheet 02.

(c) Near the new holes, as shown in Fig. A-FACAA Sheet 02, bond the placards

identified 1037VN and 1039VN, supplied in :

Placard Set D9100095213795

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 80

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SERVICE BULLETIN

(4) Subtask 321349-831-002-003 - Modify the equipment and the wiring in the C/B

panel 121VU.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Work location Electrical panel 121VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA931324-075 2 C/B

3 ASNA2080G01 5 Button

4 ASNA2080G04 5 Button

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 50 Tie

NSA935401-05 50 Tie

Kit 321349A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 D11311636A00 1 Placard

References

Fig. A-FADAA

Modification of the Equipment in the C/B

Panel 121VU

Sheet 01

Fig. A-FBAAA

Modification of the Wiring in the C/B

Panel 121VU

Sheet 01

Sheet 02

Sheet 03

(a) Install the C/B 58GA and 59GA.

1 At position R25, install :

FIN 58GA

1 Circuit Breaker NSA931324-075 Item 1

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 81

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2 At position R26, install :

FIN 59GA

1 Circuit Breaker NSA931324-075 Item 1

3 Near the new C/B, bond the placards identified 58GA and 59GA, supplied in :

Placard Set D9100095213795

(b) Replace the placard 31LM (line R).

1 Remove :

FIN 31LM

1 Placard D11311356A00 Item (2) Discard

attached with :

5 Button-Rivet Plastic ASNA2080G01 Item (3) Discard

or

5 Button-Rivet Plastic ASNA2080G04 Item (4) Discard

2 Install :

FIN 31LM

1 Placard D11311636A00 Item 2

attach with :

5 Button-Rivet Plastic ASNA2080G01 Item 3

or

5 Button-Rivet Plastic ASNA2080G04 Item 4

(c) Modify the wiring.

1 Modify the connections of the wires as shown on the wiring diagram Fig. AFBAAA Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBAAA Sheet 03).

2 Install the wires as shown on the wiring diagrams Fig. A-FBAAA Sheet 01 and

Fig. A-FBAAA Sheet 02 and as given in the hook-up chart lines :

- 8 thru 13 (Refer to Fig. A-FBAAA Sheet 03), supplied in :

Bundle D9000095223495

3 Attach the wires with :

50 Tie-Cable NSA935401-03

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 82

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SERVICE BULLETIN

50 Tie-Cable NSA935401-05

(5) Subtask 321349-831-003-001 - Modify the equipment and the wiring in the shelf

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 93VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 E0217XUU001A 1 Relay

14 E0219ASXUU 1 Base

15 MS21042-04 3 Nut

16 E0425A2001 1 Module

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA937901FM 2 Module

Kit 321349A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095224595 Bundle

References

Fig. A-FAEAA

Modification of the Equipment in the

Shelf 93VU

Sheet 01

Sheet 02

Fig. A-FBBAA

Modification of the Wiring in the Shelf

93VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 83

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(a) Remove the relay 48GA.

1 Remove as shown in Fig. A-FAEAA Sheet 01 :

FIN 48GA

1 Relay Item (5) Discard

FIN 48GAA

1 Base Item (6) Discard

FIN 48GAA8

1 Retainer Assy Item (7) Discard

2 Remove the placard identified 48GA.

(b) Modify the terminal block 217VT.

1 Remove from position 9, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT9

1 Module Item (10) Discard

and

FIN 57GA

1 Capacitor Item (9) Discard

2 Remove from position 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT10

1 Module Item (12) Discard

and

FIN 56GA

1 Resistor Item (8) Discard

3 Remove between positions 9 and 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT91

1 Plate-Module Item (11) Discard

4 Install in replacement at positions 9 and 10 :

2 Module-False NSA937901FM

(c) Install the relay 62GA.

1 Install at position B23, as shown in Fig. A-FAEAA Sheet 02 :

FIN 62GA

1 Relay E0217XUU001A Item 13

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 84

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FIN 62GAA

1 Base E0219ASXUU Item 14

attach with :

3 Nut MS21042-04 Item 15

2 Near the new relay, bond the placard identified 62GA, supplied in :

Placard Set D9100095213795

(d) Install the grounding module 679VG.

1 Install as shown in Fig. A-FAEAA Sheet 02 :

FIN 679VG

1 Module-Grounding E0425A2001 Item 16

2 Near the new grounding module, bond the placard identified 679VG, supplied

in :

Placard Set D9100095213795

(e) Modify the wiring.

1 Remove the wires as shown on the wiring diagram Fig. A-FBBAA Sheet 01,

Fig. A-FBBAA Sheet 03 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FBBAA Sheet 04).

2 Install the wires as shown on the wiring diagrams Fig. A-FBBAA Sheet 02 and

Fig. A-FBBAA Sheet 03 and as given in the hook-up charts lines :

- 17 thru 23 (Refer to Fig. A-FBBAA Sheet 04), supplied in :

Bundle D9000095223495

Bundle D9000095224595

3 Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

(6) Subtask 321349-831-004-001 - Modify the wiring in the shelf 94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 85

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FBCAA

Modification of the Wiring in the Shelf

94VU

Sheet 01

Sheet 02

(a) Install the wire as shown on the wiring diagram Fig. A-FBCAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBCAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(7) Subtask 321349-831-005-001 - Modify the equipment in the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 91VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 86

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Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 D9251719400095 1 Plate

22 NAS1801-3-8 6 Screw

23 NAS1149F0332P 8 Washer

24 NSA5050-3 8 Nut

25 NSA935504-01 2 Mount

26 NSA5515-11 2 Clamp

27 NAS1801-3-13 2 Screw

36 EN3646A61210BW 1 CNCTR

37 ABS0638A12 2 BACKSHLL

38 EN3646A61210BN 1 CNCTR

References

Fig. A-FAFAA

Modification of the Equipment in the

Shelf 91VU

Sheet 01

Sheet 02

Fig. A-FBJAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

Fig. A-FBKAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

(a) Disconnect the draining pipe from the blanking plate Item (17).

NOTE: Discard the attachment parts.

(b) Remove as shown in Fig. A-FAFAA Sheet 01 detail B :

1 Plate-Assy D9251335500000 Item (17) Discard

attached with :

6 Screw Item (22) Discard

6 Washer Item (23) Discard

6 Nut Item (24) Discard

(c) Install as shown in Fig. A-FAFAA Sheet 02 detail C :

1 Plate-LGCIU D9251719400095 Item 21

attach with :

6 Screw NAS1801-3-8 Item 22

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 87

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6 Washer NAS1149F0332P Item 23

6 Nut NSA5050-3 Item 24

NOTE: For the internal wiring of the LGCIU plate, refer to Fig. A-FBJAA

Sheet 01 and Fig. A-FBKAA Sheet 01.

Install at the rear of the new LGCIU plate Item 21 :

FIN 201VCA

1 Connector-Plug EN3646A61210BW Item 36

FIN 201VCA1

1 Backshell-Connector ABS0638A12 Item 37

FIN 203VCA

1 Connector-Plug EN3646A61210BN Item 38

FIN 203VCA1

1 Backshell-Connector ABS0638A12 Item 37

(d) Install as shown in Fig. A-FAFAA Sheet 02 detail D :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

(e) Install as shown in Fig. A-FAFAA Sheet 02 detail E :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 88

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SERVICE BULLETIN

(8) Subtask 321349-831-006-001 - Modify the wiring between the shelves 91VU and

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

93VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBDAA

Modification of the Wiring between the

Shelves 91VU and 93VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 3 (Refer to Fig. A-FBDAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 89

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SERVICE BULLETIN

(9) Subtask 321349-831-007-001 - Modify the wiring between the shelves 91VU and

94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

94VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBEAA

Modification of the Wiring between the

Shelves 91VU and 94VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBEAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 90

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SERVICE BULLETIN

(10) Subtask 321349-831-008-001 - Modify the wiring between the shelf 91VU and the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

22 NAS1801-3-8 2 Screw

23 NAS1149F0332P 2 Washer

24 NSA5050-3 2 Nut

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBFAA

Modification of the Wiring between the

Shelf 91VU and the AVNCS

Compartment

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBFAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBFAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Connect the bonding points, as shown in Fig. A-FAGAA Sheet 01, with :

2 Screw NAS1801-3-8 Item 22

2 Washer NAS1149F0332P Item 23

2 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 91

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(c) Together with the new wires, install the identification plates 1037VN and 1039VN,

supplied in :

Bundle D9000095223495

(d) Attach the wires with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(11) Subtask 321349-831-009-001 - Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 90VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBGAA

Modification of the Wiring between the

Rear Panel 120VU and the FWD

Electronics Rack 90VU

Sheet 01

Sheet 02

(a) Remove the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBGAA Sheet 02).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 92

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(b) Install the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 2 (Refer to Fig. A-FBGAA Sheet 02), supplied in :

Bundle D9000095223495

(c) Attach the wire with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

(12) Subtask 321349-831-010-001 - Modify the wiring between the rear panel 120VU and

the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 91VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 300 Tie

NSA935401-05 300 Tie

NSA935401-08 300 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBHAA

Modification of the Wiring between the

Rear Panel 120VU and the Shelf 91VU

Sheet 01

Sheet 02

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 93

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(a) Install the wires as shown on the wiring diagram Fig. A-FBHAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBHAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Together with the new wires, install the identification plates 201VC-A and 203VC-A,

supplied in :

Bundle D9000095223495

(c) Attach the wires with :

300 Tie-Cable NSA935401-03

300 Tie-Cable NSA935401-05

300 Tie-Cable NSA935401-08

(13) Subtask 321349-410-001-001 - Install the equipment removed for access in the

cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Install as shown in detail B :

1 Panel-RH Lateral Item (28)

attach with :

1 Screw Item (29)

1 Nut Item (30)

2 Screw Item (31)

NOTE: All these items were retained at the removal.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 94

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(b) Install as shown in detail C :

FIN 702VU

1 Console Item (32)

attach with :

4 Screw Item (33)

4 Washer Item (34)

NOTE: All these items were retained at the removal.

(14) Subtask 321349-410-002-001 - Install the equipment removed for access in the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 90VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Install the shelf 91VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the GCU 1 and 2 FIN 1XU1 and 1XU2 (if removed) (Refer to AMM

24-22-34, Page Block 401).

3 Install the GCU APU FIN 1XS (if removed) (Refer to AMM 24-23-34, Page

Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 95

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4 Remove the protective caps and connect the shelf cut-off connectors.

(b) Install the shelf 93VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the SEC 3 FIN 1CE3 (if removed) (Refer to AMM 27-94-34, Page Block

401).

3 Install the zone controller FIN 8HK (if removed) (Refer to AMM 21-63-34,

Page Block 401.

4 Install the LGCIU 1 FIN 5GA1 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

5 Remove the protective caps and connect the shelf cut-off connectors.

(c) Install the shelf 94VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the LGCIU 2 FIN 5GA2 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

3 Install the TPIS detection unit FIN 2GV (if removed) (Refer to AMM 32-49-34,

Page Block 401).

4 Install the SDCU FIN 10WQ (if removed) (Refer to AMM 26-17-34, Page Block

401).

5 Install the BSCU FIN 10GG (if removed) (Refer to AMM 32-42-34, Page Block

401).

6 Install the aft cargo heat controller FIN 10HC (if removed) (Refer to AMM

21-43-34, Page Block 401).

7 Install the AFMC FIN 2QN (if removed) (Refer to AMM 28-51-35, Page Block

401).

8 Remove the protective caps and connect the shelf cut-off connectors.

**CONF 004

(1) Subtask 321349-010-002-001 - Remove the equipment for access in the cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 96

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Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Remove as shown in detail B :

1 Panel-RH Lateral Item (28) Retain

attached with :

1 Screw Item (29) Retain

1 Nut Item (30) Retain

2 Screw Item (31) Retain

(b) Remove as shown in detail C :

FIN 702VU

1 Console Item (32) Retain

attached with :

4 Screw Item (33) Retain

4 Washer Item (34) Retain

(2) Subtask 321349-010-003-001 - Remove the equipment for access in the avionics

compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Panel 90VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills AIRFRAME

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 97

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Remove the shelf 91VU.

1 Remove and retain the GCU 1 and 2 FIN 1XU1 and 1XU2 (if installed) (Refer

to AMM 24-22-34, Page Block 401).

2 Remove and retain the GCU APU FIN 1XS (if installed) (Refer to AMM

24-23-34, Page Block 401).

3 Disconnect the shelf cut-off connectors and install protective caps.

4 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(b) Remove the shelf 93VU.

1 Remove and retain the SEC 3 FIN 1CE3 (if installed) (Refer to AMM 27-94-34,

Page Block 401).

2 Remove and retain the zone controller FIN 8HK (if installed) (Refer to AMM

21-63-34, Page Block 401).

3 Remove and retain the LGCIU 1 FIN 5GA1 (if installed) (Refer to AMM

32-31-71, Page Block 401).

4 Disconnect the shelf cut-off connectors and install protective caps.

5 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(c) Remove the shelf 94VU.

1 Remove and retain the LGCIU 2 FIN 5GA2 (if installed) (Refer to AMM

32-31-71, Page Block 401).

2 Remove and retain the TPIS detection unit FIN 2GV (if installed) (Refer to

AMM 32-49-34, Page Block 401).

3 Remove and retain the SDCU FIN 10WQ (if installed) (Refer to AMM

26-17-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 98

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4 Remove and retain the BSCU FIN 10GG (if installed) (Refer to AMM 32-42-34,

Page Block 401).

5 Remove and retain the aft cargo heat controller FIN 10HC (if installed) (Refer

to AMM 21-43-34, Page Block 401).

6 Remove and retain the AFMC FIN 2QN (if installed) (Refer to AMM 28-51-35,

Page Block 401).

7 Disconnect the shelf cut-off connectors and install protective caps.

8 Disconnect the bonding strap and remove the shelf from the aircraft.

NOTE: Retain the hardware.

(3) Subtask 321349-831-001-001 - Install the new grounding points in the avionics

compartment at FR10.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811, Door 812

Work location Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9100095213795 Set

References

Fig. A-FACAA

Installation of the New Grounding Points

at FR10 in AVNCS Compartment

Sheet 01

Sheet 02

(a) Drill 2 holes on the structure at FR10 to the dimensions given in Fig. A-FACAA

Sheet 01 and Fig. A-FACAA Sheet 02.

(b) Do 2 stripping dia. 14mm (0.551in.) as shown in Fig. A-FACAA Sheet 02.

(c) Near the new holes, as shown in Fig. A-FACAA Sheet 02, bond the placards

identified 1037VN and 1039VN, supplied in :

Placard Set D9100095213795

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 99

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SERVICE BULLETIN

(4) Subtask 321349-831-002-004 - Modify the equipment and the wiring in the C/B

panel 121VU.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Work location Electrical panel 121VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA931324-075 2 C/B

3 ASNA2080G01 5 Button

4 ASNA2080G04 5 Button

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 50 Tie

NSA935401-05 50 Tie

Kit 321349A05R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 D11312010A00 1 Placard

References

Fig. A-FADAA

Modification of the Equipment in the C/B

Panel 121VU

Sheet 01

Fig. A-FBAAA

Modification of the Wiring in the C/B

Panel 121VU

Sheet 01

Sheet 02

Sheet 03

(a) Install the C/B 58GA and 59GA.

1 At position R25, install :

FIN 58GA

1 Circuit Breaker NSA931324-075 Item 1

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 100

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2 At position R26, install :

FIN 59GA

1 Circuit Breaker NSA931324-075 Item 1

3 Near the new C/B, bond the placards identified 58GA and 59GA, supplied in :

Placard Set D9100095213795

(b) Replace the placard 31LM (line R).

1 Remove :

FIN 31LM

1 Placard D11311370A00 Item (2) Discard

attached with :

5 Button-Rivet Plastic ASNA2080G01 Item (3) Discard

or

5 Button-Rivet Plastic ASNA2080G04 Item (4) Discard

2 Install :

FIN 31LM

1 Placard D11312010A00 Item 2

attach with :

5 Button-Rivet Plastic ASNA2080G01 Item 3

or

5 Button-Rivet Plastic ASNA2080G04 Item 4

(c) Modify the wiring.

1 Modify the connections of the wires as shown on the wiring diagram Fig. AFBAAA Sheet 01 and as given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBAAA Sheet 03).

2 Install the wires as shown on the wiring diagrams Fig. A-FBAAA Sheet 01 and

Fig. A-FBAAA Sheet 02 and as given in the hook-up chart lines :

- 8 thru 13 (Refer to Fig. A-FBAAA Sheet 03), supplied in :

Bundle D9000095223495

3 Attach the wires with :

50 Tie-Cable NSA935401-03

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 101

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50 Tie-Cable NSA935401-05

(5) Subtask 321349-831-003-001 - Modify the equipment and the wiring in the shelf

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 93VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 E0217XUU001A 1 Relay

14 E0219ASXUU 1 Base

15 MS21042-04 3 Nut

16 E0425A2001 1 Module

D9000095223495 Bundle

D9100095213795 Set

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA937901FM 2 Module

Kit 321349A06R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095224595 Bundle

References

Fig. A-FAEAA

Modification of the Equipment in the

Shelf 93VU

Sheet 01

Sheet 02

Fig. A-FBBAA

Modification of the Wiring in the Shelf

93VU

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 102

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(a) Remove the relay 48GA.

1 Remove as shown in Fig. A-FAEAA Sheet 01 :

FIN 48GA

1 Relay Item (5) Discard

FIN 48GAA

1 Base Item (6) Discard

FIN 48GAA8

1 Retainer Assy Item (7) Discard

2 Remove the placard identified 48GA.

(b) Modify the terminal block 217VT.

1 Remove from position 9, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT9

1 Module Item (10) Discard

and

FIN 57GA

1 Capacitor Item (9) Discard

2 Remove from position 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT10

1 Module Item (12) Discard

and

FIN 56GA

1 Resistor Item (8) Discard

3 Remove between positions 9 and 10, as shown in Fig. A-FAEAA Sheet 01 :

FIN 217VT91

1 Plate-Module Item (11) Discard

4 Install in replacement at positions 9 and 10 :

2 Module-False NSA937901FM

(c) Install the relay 62GA.

1 Install at position B23, as shown in Fig. A-FAEAA Sheet 02 :

FIN 62GA

1 Relay E0217XUU001A Item 13

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 103

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FIN 62GAA

1 Base E0219ASXUU Item 14

attach with :

3 Nut MS21042-04 Item 15

2 Near the new relay, bond the placard identified 62GA, supplied in :

Placard Set D9100095213795

(d) Install the grounding module 679VG.

1 Install as shown in Fig. A-FAEAA Sheet 02 :

FIN 679VG

1 Module-Grounding E0425A2001 Item 16

2 Near the new grounding module, bond the placard identified 679VG, supplied

in :

Placard Set D9100095213795

(e) Modify the wiring.

1 Remove the wires as shown on the wiring diagram Fig. A-FBBAA Sheet 01,

Fig. A-FBBAA Sheet 03 and as given in the hook-up chart lines :

- 1 thru 13 (Refer to Fig. A-FBBAA Sheet 04).

2 Install the wires as shown on the wiring diagrams Fig. A-FBBAA Sheet 02 and

Fig. A-FBBAA Sheet 03 and as given in the hook-up charts lines :

- 17 thru 23 (Refer to Fig. A-FBBAA Sheet 04), supplied in :

Bundle D9000095223495

Bundle D9000095224595

3 Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

(6) Subtask 321349-831-004-001 - Modify the wiring in the shelf 94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 104

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FBCAA

Modification of the Wiring in the Shelf

94VU

Sheet 01

Sheet 02

(a) Install the wire as shown on the wiring diagram Fig. A-FBCAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBCAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wire with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(7) Subtask 321349-831-005-001 - Modify the equipment in the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 91VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 105

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Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

21 D9251719400095 1 Plate

22 NAS1801-3-8 6 Screw

23 NAS1149F0332P 8 Washer

24 NSA5050-3 8 Nut

25 NSA935504-01 2 Mount

26 NSA5515-11 2 Clamp

27 NAS1801-3-13 2 Screw

36 EN3646A61210BW 1 CNCTR

37 ABS0638A12 2 BACKSHLL

38 EN3646A61210BN 1 CNCTR

References

Fig. A-FAFAA

Modification of the Equipment in the

Shelf 91VU

Sheet 01

Sheet 02

Fig. A-FBJAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

Fig. A-FBKAA

Wiring Diagram of the New LGCIU Plate

(For Information Only)

Sheet 01

(a) Disconnect the draining pipe from the blanking plate Item (17).

NOTE: Discard the attachment parts.

(b) Remove as shown in Fig. A-FAFAA Sheet 01 detail B :

1 Plate-Assy D9251335500000 Item (17) Discard

attached with :

6 Screw Item (22) Discard

6 Washer Item (23) Discard

6 Nut Item (24) Discard

(c) Install as shown in Fig. A-FAFAA Sheet 02 detail C :

1 Plate-LGCIU D9251719400095 Item 21

attach with :

6 Screw NAS1801-3-8 Item 22

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 106

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6 Washer NAS1149F0332P Item 23

6 Nut NSA5050-3 Item 24

NOTE: For the internal wiring of the LGCIU plate, refer to Fig. A-FBJAA

Sheet 01 and Fig. A-FBKAA Sheet 01.

Install at the rear of the new LGCIU plate Item 21 :

FIN 201VCA

1 Connector-Plug EN3646A61210BW Item 36

FIN 201VCA1

1 Backshell-Connector ABS0638A12 Item 37

FIN 203VCA

1 Connector-Plug EN3646A61210BN Item 38

FIN 203VCA1

1 Backshell-Connector ABS0638A12 Item 37

(d) Install as shown in Fig. A-FAFAA Sheet 02 detail D :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

(e) Install as shown in Fig. A-FAFAA Sheet 02 detail E :

1 Mount NSA935504-01 Item 25

and

1 Clamp NSA5515-11 Item 26

attach with :

1 Screw NAS1801-3-13 Item 27

1 Washer NAS1149F0332P Item 23

1 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 107

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SERVICE BULLETIN

(8) Subtask 321349-831-006-001 - Modify the wiring between the shelves 91VU and

93VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

93VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBDAA

Modification of the Wiring between the

Shelves 91VU and 93VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBDAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 3 (Refer to Fig. A-FBDAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 108

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(9) Subtask 321349-831-007-001 - Modify the wiring between the shelves 91VU and

94VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Electrical panel

94VU

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBEAA

Modification of the Wiring between the

Shelves 91VU and 94VU

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBEAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBEAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Attach the wires with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 109

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(10) Subtask 321349-831-008-001 - Modify the wiring between the shelf 91VU and the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location from Electrical panel 91VU to Frame 10

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

22 NAS1801-3-8 2 Screw

23 NAS1149F0332P 2 Washer

24 NSA5050-3 2 Nut

D9000095223495 Bundle

NSA935401-03 50 Tie

NSA935401-05 50 Tie

References

Fig. A-FAGAA

Modification of the Routing behind the

Shelf 91VU

Sheet 01

Fig. A-FBFAA

Modification of the Wiring between the

Shelf 91VU and the AVNCS

Compartment

Sheet 01

Sheet 02

(a) Install the wires as shown on the wiring diagram Fig. A-FBFAA Sheet 01 and as

given in the hook-up chart lines :

- 1 and 2 (Refer to Fig. A-FBFAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Connect the bonding points, as shown in Fig. A-FAGAA Sheet 01, with :

2 Screw NAS1801-3-8 Item 22

2 Washer NAS1149F0332P Item 23

2 Nut NSA5050-3 Item 24

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 110

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(c) Together with the new wires, install the identification plates 1037VN and 1039VN,

supplied in :

Bundle D9000095223495

(d) Attach the wires with :

50 Tie-Cable NSA935401-03

50 Tie-Cable NSA935401-05

(11) Subtask 321349-831-009-001 - Modify the wiring between the rear panel 120VU and

the FWD electronics rack 90VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 90VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 100 Tie

NSA935401-05 100 Tie

NSA935401-08 100 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBGAA

Modification of the Wiring between the

Rear Panel 120VU and the FWD

Electronics Rack 90VU

Sheet 01

Sheet 02

(a) Remove the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 1 (Refer to Fig. A-FBGAA Sheet 02).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 111

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(b) Install the wire as shown on the wiring diagram Fig. A-FBGAA Sheet 01 and as

given in the hook-up chart line :

- 2 (Refer to Fig. A-FBGAA Sheet 02), supplied in :

Bundle D9000095223495

(c) Attach the wire with :

100 Tie-Cable NSA935401-03

100 Tie-Cable NSA935401-05

100 Tie-Cable NSA935401-08

(12) Subtask 321349-831-010-001 - Modify the wiring between the rear panel 120VU and

the shelf 91VU.

Work Zones and Access Panels

Zone Access/Work location

From 210 Access Door 831

Work location Electrical panel 120VU

To 120 Access Door 811, Door 822

Work location Electrical panel 91VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 321349A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

D9000095223495 Bundle

NSA935401-03 300 Tie

NSA935401-05 300 Tie

NSA935401-08 300 Tie

References

Fig. A-FAAAA

Location of the Working Area

Sheet 01

Fig. A-FBHAA

Modification of the Wiring between the

Rear Panel 120VU and the Shelf 91VU

Sheet 01

Sheet 02

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 112

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(a) Install the wires as shown on the wiring diagram Fig. A-FBHAA Sheet 01 and as

given in the hook-up chart lines :

- 1 thru 4 (Refer to Fig. A-FBHAA Sheet 02), supplied in :

Bundle D9000095223495

(b) Together with the new wires, install the identification plates 201VC-A and 203VC-A,

supplied in :

Bundle D9000095223495

(c) Attach the wires with :

300 Tie-Cable NSA935401-03

300 Tie-Cable NSA935401-05

300 Tie-Cable NSA935401-08

(13) Subtask 321349-410-001-001 - Install the equipment removed for access in the

cockpit.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills AIRFRAME

References

Fig. A-FABAA

Removal/Installation of the Equipment in

the Cockpit (For Access)

Sheet 01

(a) Install as shown in detail B :

1 Panel-RH Lateral Item (28)

attach with :

1 Screw Item (29)

1 Nut Item (30)

2 Screw Item (31)

NOTE: All these items were retained at the removal.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 113

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(b) Install as shown in detail C :

FIN 702VU

1 Console Item (32)

attach with :

4 Screw Item (33)

4 Washer Item (34)

NOTE: All these items were retained at the removal.

(14) Subtask 321349-410-002-001 - Install the equipment removed for access in the

avionics compartment.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 811

Work location Electrical panel 90VU

Manpower Resources

Manhours 5.00

Minimum number of person 1

Subtask elapsed time 5.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Install the shelf 91VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the GCU 1 and 2 FIN 1XU1 and 1XU2 (if removed) (Refer to AMM

24-22-34, Page Block 401).

3 Install the GCU APU FIN 1XS (if removed) (Refer to AMM 24-23-34, Page

Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 114

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4 Remove the protective caps and connect the shelf cut-off connectors.

(b) Install the shelf 93VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the SEC 3 FIN 1CE3 (if removed) (Refer to AMM 27-94-34, Page Block

401).

3 Install the zone controller FIN 8HK (if removed) (Refer to AMM 21-63-34,

Page Block 401.

4 Install the LGCIU 1 FIN 5GA1 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

5 Remove the protective caps and connect the shelf cut-off connectors.

(c) Install the shelf 94VU.

1 Install the shelf and connect the bonding straps.

NOTE: Attach with the fasteners retained at removal.

2 Install the LGCIU 2 FIN 5GA2 (if removed) (Refer to AMM 32-31-71, Page

Block 401).

3 Install the TPIS detection unit FIN 2GV (if removed) (Refer to AMM 32-49-34,

Page Block 401).

4 Install the SDCU FIN 10WQ (if removed) (Refer to AMM 26-17-34, Page Block

401).

5 Install the BSCU FIN 10GG (if removed) (Refer to AMM 32-42-34, Page Block

401).

6 Install the aft cargo heat controller FIN 10HC (if removed) (Refer to AMM

21-43-34, Page Block 401).

7 Install the AFMC FIN 2QN (if removed) (Refer to AMM 28-51-35, Page Block

401).

8 Remove the protective caps and connect the shelf cut-off connectors.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 115

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SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 321349-861-001-001 - ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Battery re-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Remove the blanking cap(s) from the electrical connectors.

3 Make sure that the electrical connectors are clean and in correct condition.

4 Connect the connector on the battery.

5 Turn the knurled nut a quarter turn.

(b) Remove all the warning notices.

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

(2) Subtask 321349-700-001-001 - PRELIMINARY TESTS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-26-00, Page Block 501

22-96-00, Page Block 501

22-97-00, Page Block 501

31-50-00, Page Block 501

31-60-00, Page Block 501

33-13-00, Page Block 501

33-14-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-10

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 116

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(a) Preliminary tests

1 Initial conditions :

a On each connectors that you disconnected, do a visual check as defined

in ESPM 20-52-10 to make sure that :

- The label of the plug is the same as the label on the receptacle.

- The plug is correctly locked.

2 Preliminary tests

NOTE: If the aircraft is operated in CAT3 conditions, you must also do

the Land CAT3 capability test (Refer to AMM 22-97-00, Page

Block 501).

a Do an operational test of the instrument and panel integral lighting (Refer

to AMM 33-13-00, Page Block 501).

b Do an operational test of the annunciator light test system in the cockpit

(Refer to AMM 33-14-00, Page Block 501).

c Do an operational test of the avionics equipment ventilation system

(Refer to AMM 21-26-00, Page Block 501).

d Do an operational test of the Automatic Flight System (AFS) (Refer to

AMM 22-96-00, Page Block 501).

e Do an operational test of the Electronic Instrument System (EIS) (Refer

to AMM 31-60-00, Page Block 501).

f Do an operational test of the Electronic Centralized Aircraft Monitoring

(ECAM) control panel (Refer to AMM 31-50-00, Page Block 501).

g Do a ground scanning of the central warning system (Refer to AMM

31-50-00, Page Block 501).

(3) Subtask 321349-700-002-001 - TESTING

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 117

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References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 501

21-43-00, Page Block 501

21-63-00, Page Block 501

24-41-00, Page Block 501

26-16-00, Page Block 501

26-17-00, Page Block 501

27-94-00, Page Block 501

31-50-00, Page Block 501

32-46-00, Page Block 501

32-49-00, Page Block 501

(a) Tests after disconnection/re-connection of the connectors and the terminal blocks

1 Connectors 282VC, 283VC, 2254VC, 2206VC, 201VC and 203VC

a None, included in the system test.

2 Terminal blocks 213VT and 206VT

a None, included in the system test.

(b) Tests after disconnection/re-connection of the shelves 91VU, 93VU and 94VU

1 Shelf 91VU

a Do an operational test of the Ground Power Control Unit (GPCU) (Refer

to AMM 24-41-00, Page Block 501).

2 Shelf 93VU

a Do an operational test of the SEC 3 (Refer to AMM 27-94-00, Page Block

501).

b Do an operational test of the cockpit and cabin temperature control with

Centralized Fault Display (CFDS)/Multipurpose Control and Display Unit

(MCDU) (Refer to AMM 21-63-00, Page Block 501).

3 Shelf 94VU

a Do the cross-check of TPIS reading and tire pressure gauge (Refer to

AMM 32-49-00, Page Block 501).

b Do an operational test of the lavatory smoke-detection system (Refer to

AMM 26-16-00, Page Block 501).

c Do an operational check of the cargo-compartment smoke-detection by

Push To Test (PTT) (Refer to AMM 26-17-00, Page Block 501).

d Do the BITE test of the BSCU (Refer to AMM 32-46-00, Page Block 501).

e Do an operational test of the aft cargo-compartment heating system

(Refer to AMM 21-43-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(c) Tests after installation of the new C/B

1 Do a voltage check at pin 1 of these C/B to make sure that there is 28VDC :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/A

1WE1 43 Q

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/B

2WE1 44 Q

121VU LGCIU/BAT SPLY/SYS1 58GA 32 R

121VU LGCIU/BAT SPLY/SYS2 59GA 33 R

2 Do an operational test of the circuit breaker monitoring system for the panel

121VU (Refer to AMM 31-50-00, Page Block 501).

(d) Test of the electrical bonding

1 Do a check of the electrical bonding (Refer to AMM 20-28-00, Page Block

501).

NOTE: For the maximum permissible resistance values (Refer to AMM

20-28-00, Page Block 501).

(4) Subtask 321349-720-401-001 - Preparation

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-00-00, Page Block 201

(a) On the overhead panel 35GU switch the batteries ’ON’.

(b) On the overhead panel 35GU switch the external power ’ON’.

(c) Put the aircraft to Flight Configurations Precautions with Electrical Power (Refer to

AMM 32-00-00, Page Block 201).

(5) Subtask 321349-720-402-001 - Test of Battery Relief Relay 60GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(a) Switch off LGCIU2:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

121VU LGCIU SYS 2 BAT SPLY 59GA R33

(b) LGCIU1 only powered from ground supply:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

49VU LGCIU SYS 1 1GA C09

Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(c) On the ECAM wheel page check that the indications that follow are displayed:

1 The MLG Left, MLG Right, Nose LG symbols on the right hand side on the

Wheel page are amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02 for EIS 1

(Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD

screens).

(d) Do a BITE TEST on the LGCIU1 from the MCDU, the result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(e) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

Check that the ECAM Wheel page shows all amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 120

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(f) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02

OR

Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(h) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(i) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check that the ECAM Wheel page remains the same as above, 1GA and 52GA are

already open at this stage:

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(6) Subtask 321349-720-403-001 - Test of System 2 Battery Relief Relay 61GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Make sure that 59GA is still open.

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(b) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 BAT SPLY 59GA R33

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(c) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(d) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

(e) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

NOTE: To do a BITE test on LGCIU SYS 2 the CFDS must receive a ground

signal from LGCIU1.

(f) On LGCIU2 do a ’BITE’ test from the MCDU, the test result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

(h) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(7) Subtask 321349-720-404-001 - Modified Safety Valve Circuit Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-30-00, Page Block 201

NOTE: Diode 1VD 2/17 provides a feed back loop around Relay 62GA and must

be tested, otherwise the Landing Gear will not retract. The test below

avoids jacking the aircraft and swinging the gear.

(a) Make sure that the LG ground locks are fitted and hydraulic systems are

depressurized (Refer to AMM 32-30-00, Page Block 201).

(b) Open the connector 49GA-A Landing Gear Safety Valve (LGSV) and connect a

Portable Voltmeter between pin B and ground.

(c) On the overhead panel 35GU switch the external power ’ON’.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 123

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(d) Check that 28 volts appears on the Portable Voltmeter.

(e) Simulate the MLG left, MLG right and NLG to extend by:

1 For Pre-Mod 37831J2877 - Ultra LGCIU P/N 664700500A4x:

Enter interactive mode LGCIU2 use MCDU, go to page 2 of the main menu

and use ’LG SIMULATION MODE’.

2 For Post-Mod 37831J2877 NEW LGCIU P/N 80-178-02-88xxx:

It will be necessary to use false targets (steel) on proximity sensors 22GA,

23GA and 25GA to perform this simulation.

(f) Set the LG control lever 6GA to ’UP’ check that 28V remains indicated on the

Portable Voltmeter, then set the lever to ’DOWN’.

(g) Set the EXT PWR to ’OFF’

(h) Remove the Portable Voltmeter.

(i) Reconnect the 49GA-A connector to the LGSV.

(8) Subtask 321349-720-405-001 - Relay 62GA Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-005

(a) Perform an operational test of the safety valves (Refer to AMM

Task 32-31-00-710-005, or AMM Task 32-31-00-710-005-01 or AMM Task

32-31-00-710-005-02) ’Operational Check to Ensure Safety Valve Close at 260kts’.

**CONF 002

(1) Subtask 321349-861-001-001 - ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Battery re-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Remove the blanking cap(s) from the electrical connectors.

3 Make sure that the electrical connectors are clean and in correct condition.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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4 Connect the connector on the battery.

5 Turn the knurled nut a quarter turn.

(b) Remove all the warning notices.

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

(2) Subtask 321349-700-001-001 - PRELIMINARY TESTS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-26-00, Page Block 501

22-96-00, Page Block 501

22-97-00, Page Block 501

31-50-00, Page Block 501

31-60-00, Page Block 501

33-13-00, Page Block 501

33-14-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Preliminary tests

1 Initial conditions :

a On each connectors that you disconnected, do a visual check as defined

in ESPM 20-52-10 to make sure that :

- The label of the plug is the same as the label on the receptacle.

- The plug is correctly locked.

2 Preliminary tests

NOTE: If the aircraft is operated in CAT3 conditions, you must also do

the Land CAT3 capability test (Refer to AMM 22-97-00, Page

Block 501).

a Do an operational test of the instrument and panel integral lighting (Refer

to AMM 33-13-00, Page Block 501).

b Do an operational test of the annunciator light test system in the cockpit

(Refer to AMM 33-14-00, Page Block 501).

c Do an operational test of the avionics equipment ventilation system

(Refer to AMM 21-26-00, Page Block 501).

d Do an operational test of the Automatic Flight System (AFS) (Refer to

AMM 22-96-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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e Do an operational test of the Electronic Instrument System (EIS) (Refer

to AMM 31-60-00, Page Block 501).

f Do an operational test of the Electronic Centralized Aircraft Monitoring

(ECAM) control panel (Refer to AMM 31-50-00, Page Block 501).

g Do a ground scanning of the central warning system (Refer to AMM

31-50-00, Page Block 501).

(3) Subtask 321349-700-002-001 - TESTING

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 501

21-43-00, Page Block 501

21-63-00, Page Block 501

24-41-00, Page Block 501

26-16-00, Page Block 501

26-17-00, Page Block 501

27-94-00, Page Block 501

31-50-00, Page Block 501

32-46-00, Page Block 501

32-49-00, Page Block 501

(a) Tests after disconnection/re-connection of the connectors and the terminal blocks

1 Connectors 282VC, 283VC, 2254VC, 2206VC, 201VC and 203VC

a None, included in the system test.

2 Terminal blocks 213VT and 206VT

a None, included in the system test.

(b) Tests after disconnection/re-connection of the shelves 91VU, 93VU and 94VU

1 Shelf 91VU

a Do an operational test of the Ground Power Control Unit (GPCU) (Refer

to AMM 24-41-00, Page Block 501).

2 Shelf 93VU

a Do an operational test of the SEC 3 (Refer to AMM 27-94-00, Page Block

501).

b Do an operational test of the cockpit and cabin temperature control with

Centralized Fault Display (CFDS)/Multipurpose Control and Display Unit

(MCDU) (Refer to AMM 21-63-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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3 Shelf 94VU

a Do the cross-check of TPIS reading and tire pressure gauge (Refer to

AMM 32-49-00, Page Block 501).

b Do an operational test of the lavatory smoke-detection system (Refer to

AMM 26-16-00, Page Block 501).

c Do an operational check of the cargo-compartment smoke-detection by

Push To Test (PTT) (Refer to AMM 26-17-00, Page Block 501).

d Do the BITE test of the BSCU (Refer to AMM 32-46-00, Page Block 501).

e Do an operational test of the aft cargo-compartment heating system

(Refer to AMM 21-43-00, Page Block 501).

(c) Tests after installation of the new C/B

1 Do a voltage check at pin 1 of these C/B to make sure that there is 28VDC :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/A

1WE1 43 Q

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/B

2WE1 44 Q

121VU LGCIU/BAT SPLY/SYS1 58GA 32 R

121VU LGCIU/BAT SPLY/SYS2 59GA 33 R

2 Do an operational test of the circuit breaker monitoring system for the panel

121VU (Refer to AMM 31-50-00, Page Block 501).

(d) Test of the electrical bonding

1 Do a check of the electrical bonding (Refer to AMM 20-28-00, Page Block

501).

NOTE: For the maximum permissible resistance values (Refer to AMM

20-28-00, Page Block 501).

(4) Subtask 321349-720-401-001 - Preparation

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-00-00, Page Block 201

(a) On the overhead panel 35GU switch the batteries ’ON’.

(b) On the overhead panel 35GU switch the external power ’ON’.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(c) Put the aircraft to Flight Configurations Precautions with Electrical Power (Refer to

AMM 32-00-00, Page Block 201).

(5) Subtask 321349-720-402-001 - Test of Battery Relief Relay 60GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Switch off LGCIU2:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

121VU LGCIU SYS 2 BAT SPLY 59GA R33

(b) LGCIU1 only powered from ground supply:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

49VU LGCIU SYS 1 1GA C09

Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(c) On the ECAM wheel page check that the indications that follow are displayed:

1 The MLG Left, MLG Right, Nose LG symbols on the right hand side on the

Wheel page are amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02 for EIS 1

(Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD

screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(d) Do a BITE TEST on the LGCIU1 from the MCDU, the result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(e) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

Check that the ECAM Wheel page shows all amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(f) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02

OR

Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(h) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(i) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check that the ECAM Wheel page remains the same as above, 1GA and 52GA are

already open at this stage:

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(6) Subtask 321349-720-403-001 - Test of System 2 Battery Relief Relay 61GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Make sure that 59GA is still open.

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 130

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(b) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 BAT SPLY 59GA R33

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(c) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(d) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

(e) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

NOTE: To do a BITE test on LGCIU SYS 2 the CFDS must receive a ground

signal from LGCIU1.

(f) On LGCIU2 do a ’BITE’ test from the MCDU, the test result should be test OK

(Refer to AMM Task 32-69-00-740-001).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 131

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(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

(h) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(7) Subtask 321349-720-404-001 - Modified Safety Valve Circuit Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-30-00, Page Block 201

NOTE: Diode 1VD 2/17 provides a feed back loop around Relay 62GA and must

be tested, otherwise the Landing Gear will not retract. The test below

avoids jacking the aircraft and swinging the gear.

(a) Make sure that the LG ground locks are fitted and hydraulic systems are

depressurized (Refer to AMM 32-30-00, Page Block 201).

(b) Open the connector 49GA-A Landing Gear Safety Valve (LGSV) and connect a

Portable Voltmeter between pin B and ground.

(c) On the overhead panel 35GU switch the external power ’ON’.

(d) Check that 28 volts appears on the Portable Voltmeter.

(e) Simulate the MLG left, MLG right and NLG to extend by:

1 For Pre-Mod 37831J2877 - Ultra LGCIU P/N 664700500A4x:

Enter interactive mode LGCIU2 use MCDU, go to page 2 of the main menu

and use ’LG SIMULATION MODE’.

2 For Post-Mod 37831J2877 NEW LGCIU P/N 80-178-02-88xxx:

It will be necessary to use false targets (steel) on proximity sensors 22GA,

23GA and 25GA to perform this simulation.

(f) Set the LG control lever 6GA to ’UP’ check that 28V remains indicated on the

Portable Voltmeter, then set the lever to ’DOWN’.

(g) Set the EXT PWR to ’OFF’

(h) Remove the Portable Voltmeter.

(i) Reconnect the 49GA-A connector to the LGSV.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 132

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(8) Subtask 321349-720-405-001 - Relay 62GA Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-005

(a) Perform an operational test of the safety valves (Refer to AMM

Task 32-31-00-710-005, or AMM Task 32-31-00-710-005-01 or AMM Task

32-31-00-710-005-02) ’Operational Check to Ensure Safety Valve Close at 260kts’.

**CONF 003

(1) Subtask 321349-861-001-001 - ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Battery re-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Remove the blanking cap(s) from the electrical connectors.

3 Make sure that the electrical connectors are clean and in correct condition.

4 Connect the connector on the battery.

5 Turn the knurled nut a quarter turn.

(b) Remove all the warning notices.

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

(2) Subtask 321349-700-001-001 - PRELIMINARY TESTS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-26-00, Page Block 501

22-96-00, Page Block 501

22-97-00, Page Block 501

31-50-00, Page Block 501

31-60-00, Page Block 501

33-13-00, Page Block 501

33-14-00, Page Block 501

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 133

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References

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Preliminary tests

1 Initial conditions :

a On each connectors that you disconnected, do a visual check as defined

in ESPM 20-52-10 to make sure that :

- The label of the plug is the same as the label on the receptacle.

- The plug is correctly locked.

2 Preliminary tests

NOTE: If the aircraft is operated in CAT3 conditions, you must also do

the Land CAT3 capability test (Refer to AMM 22-97-00, Page

Block 501).

a Do an operational test of the instrument and panel integral lighting (Refer

to AMM 33-13-00, Page Block 501).

b Do an operational test of the annunciator light test system in the cockpit

(Refer to AMM 33-14-00, Page Block 501).

c Do an operational test of the avionics equipment ventilation system

(Refer to AMM 21-26-00, Page Block 501).

d Do an operational test of the Automatic Flight System (AFS) (Refer to

AMM 22-96-00, Page Block 501).

e Do an operational test of the Electronic Instrument System (EIS) (Refer

to AMM 31-60-00, Page Block 501).

f Do an operational test of the Electronic Centralized Aircraft Monitoring

(ECAM) control panel (Refer to AMM 31-50-00, Page Block 501).

g Do a ground scanning of the central warning system (Refer to AMM

31-50-00, Page Block 501).

(3) Subtask 321349-700-002-001 - TESTING

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 134

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References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 501

21-43-00, Page Block 501

21-63-00, Page Block 501

24-41-00, Page Block 501

26-16-00, Page Block 501

26-17-00, Page Block 501

27-94-00, Page Block 501

31-50-00, Page Block 501

32-46-00, Page Block 501

32-49-00, Page Block 501

(a) Tests after disconnection/re-connection of the connectors and the terminal blocks

1 Connectors 282VC, 283VC, 2254VC, 2206VC, 201VC and 203VC

a None, included in the system test.

2 Terminal blocks 213VT and 206VT

a None, included in the system test.

(b) Tests after disconnection/re-connection of the shelves 91VU, 93VU and 94VU

1 Shelf 91VU

a Do an operational test of the Ground Power Control Unit (GPCU) (Refer

to AMM 24-41-00, Page Block 501).

2 Shelf 93VU

a Do an operational test of the SEC 3 (Refer to AMM 27-94-00, Page Block

501).

b Do an operational test of the cockpit and cabin temperature control with

Centralized Fault Display (CFDS)/Multipurpose Control and Display Unit

(MCDU) (Refer to AMM 21-63-00, Page Block 501).

3 Shelf 94VU

a Do the cross-check of TPIS reading and tire pressure gauge (Refer to

AMM 32-49-00, Page Block 501).

b Do an operational test of the lavatory smoke-detection system (Refer to

AMM 26-16-00, Page Block 501).

c Do an operational check of the cargo-compartment smoke-detection by

Push To Test (PTT) (Refer to AMM 26-17-00, Page Block 501).

d Do the BITE test of the BSCU (Refer to AMM 32-46-00, Page Block 501).

e Do an operational test of the aft cargo-compartment heating system

(Refer to AMM 21-43-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 135

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(c) Tests after installation of the new C/B

1 Do a voltage check at pin 1 of these C/B to make sure that there is 28VDC :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/A

1WE1 43 Q

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/B

2WE1 44 Q

121VU LGCIU/BAT SPLY/SYS1 58GA 32 R

121VU LGCIU/BAT SPLY/SYS2 59GA 33 R

2 Do an operational test of the circuit breaker monitoring system for the panel

121VU (Refer to AMM 31-50-00, Page Block 501).

(d) Test of the electrical bonding

1 Do a check of the electrical bonding (Refer to AMM 20-28-00, Page Block

501).

NOTE: For the maximum permissible resistance values (Refer to AMM

20-28-00, Page Block 501).

(4) Subtask 321349-720-401-001 - Preparation

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-00-00, Page Block 201

(a) On the overhead panel 35GU switch the batteries ’ON’.

(b) On the overhead panel 35GU switch the external power ’ON’.

(c) Put the aircraft to Flight Configurations Precautions with Electrical Power (Refer to

AMM 32-00-00, Page Block 201).

(5) Subtask 321349-720-402-001 - Test of Battery Relief Relay 60GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 136

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(a) Switch off LGCIU2:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

121VU LGCIU SYS 2 BAT SPLY 59GA R33

(b) LGCIU1 only powered from ground supply:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

49VU LGCIU SYS 1 1GA C09

Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(c) On the ECAM wheel page check that the indications that follow are displayed:

1 The MLG Left, MLG Right, Nose LG symbols on the right hand side on the

Wheel page are amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02 for EIS 1

(Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD

screens).

(d) Do a BITE TEST on the LGCIU1 from the MCDU, the result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(e) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

Check that the ECAM Wheel page shows all amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 137

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(f) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02

OR

Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(h) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(i) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check that the ECAM Wheel page remains the same as above, 1GA and 52GA are

already open at this stage:

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 138

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refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(6) Subtask 321349-720-403-001 - Test of System 2 Battery Relief Relay 61GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Make sure that 59GA is still open.

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(b) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 BAT SPLY 59GA R33

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(c) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 139

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refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(d) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

(e) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

NOTE: To do a BITE test on LGCIU SYS 2 the CFDS must receive a ground

signal from LGCIU1.

(f) On LGCIU2 do a ’BITE’ test from the MCDU, the test result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

(h) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(7) Subtask 321349-720-404-001 - Modified Safety Valve Circuit Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-30-00, Page Block 201

NOTE: Diode 1VD 2/17 provides a feed back loop around Relay 62GA and must

be tested, otherwise the Landing Gear will not retract. The test below

avoids jacking the aircraft and swinging the gear.

(a) Make sure that the LG ground locks are fitted and hydraulic systems are

depressurized (Refer to AMM 32-30-00, Page Block 201).

(b) Open the connector 49GA-A Landing Gear Safety Valve (LGSV) and connect a

Portable Voltmeter between pin B and ground.

(c) On the overhead panel 35GU switch the external power ’ON’.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 140

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(d) Check that 28 volts appears on the Portable Voltmeter.

(e) Simulate the MLG left, MLG right and NLG to extend by:

1 For Pre-Mod 37831J2877 - Ultra LGCIU P/N 664700500A4x:

Enter interactive mode LGCIU2 use MCDU, go to page 2 of the main menu

and use ’LG SIMULATION MODE’.

2 For Post-Mod 37831J2877 NEW LGCIU P/N 80-178-02-88xxx:

It will be necessary to use false targets (steel) on proximity sensors 22GA,

23GA and 25GA to perform this simulation.

(f) Set the LG control lever 6GA to ’UP’ check that 28V remains indicated on the

Portable Voltmeter, then set the lever to ’DOWN’.

(g) Set the EXT PWR to ’OFF’

(h) Remove the Portable Voltmeter.

(i) Reconnect the 49GA-A connector to the LGSV.

(8) Subtask 321349-720-405-001 - Relay 62GA Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-005

(a) Perform an operational test of the safety valves (Refer to AMM

Task 32-31-00-710-005, or AMM Task 32-31-00-710-005-01 or AMM Task

32-31-00-710-005-02) ’Operational Check to Ensure Safety Valve Close at 260kts’.

**CONF 004

(1) Subtask 321349-861-001-001 - ENERGIZE ELECTRICAL NETWORK

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-38-51, Page Block 401

(a) Battery re-connection :

1 For the job set-up, refer to the removal/installation of the batteries (Refer to

AMM 24-38-51, Page Block 401).

2 Remove the blanking cap(s) from the electrical connectors.

3 Make sure that the electrical connectors are clean and in correct condition.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 141

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4 Connect the connector on the battery.

5 Turn the knurled nut a quarter turn.

(b) Remove all the warning notices.

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

(2) Subtask 321349-700-001-001 - PRELIMINARY TESTS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-26-00, Page Block 501

22-96-00, Page Block 501

22-97-00, Page Block 501

31-50-00, Page Block 501

31-60-00, Page Block 501

33-13-00, Page Block 501

33-14-00, Page Block 501

Elec. Std. Practices Manual (ESPM) 20-52-10

(a) Preliminary tests

1 Initial conditions :

a On each connectors that you disconnected, do a visual check as defined

in ESPM 20-52-10 to make sure that :

- The label of the plug is the same as the label on the receptacle.

- The plug is correctly locked.

2 Preliminary tests

NOTE: If the aircraft is operated in CAT3 conditions, you must also do

the Land CAT3 capability test (Refer to AMM 22-97-00, Page

Block 501).

a Do an operational test of the instrument and panel integral lighting (Refer

to AMM 33-13-00, Page Block 501).

b Do an operational test of the annunciator light test system in the cockpit

(Refer to AMM 33-14-00, Page Block 501).

c Do an operational test of the avionics equipment ventilation system

(Refer to AMM 21-26-00, Page Block 501).

d Do an operational test of the Automatic Flight System (AFS) (Refer to

AMM 22-96-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 142

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e Do an operational test of the Electronic Instrument System (EIS) (Refer

to AMM 31-60-00, Page Block 501).

f Do an operational test of the Electronic Centralized Aircraft Monitoring

(ECAM) control panel (Refer to AMM 31-50-00, Page Block 501).

g Do a ground scanning of the central warning system (Refer to AMM

31-50-00, Page Block 501).

(3) Subtask 321349-700-002-001 - TESTING

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 20-28-00, Page Block 501

21-43-00, Page Block 501

21-63-00, Page Block 501

24-41-00, Page Block 501

26-16-00, Page Block 501

26-17-00, Page Block 501

27-94-00, Page Block 501

31-50-00, Page Block 501

32-46-00, Page Block 501

32-49-00, Page Block 501

(a) Tests after disconnection/re-connection of the connectors and the terminal blocks

1 Connectors 282VC, 283VC, 2254VC, 2206VC, 201VC and 203VC

a None, included in the system test.

2 Terminal blocks 213VT and 206VT

a None, included in the system test.

(b) Tests after disconnection/re-connection of the shelves 91VU, 93VU and 94VU

1 Shelf 91VU

a Do an operational test of the Ground Power Control Unit (GPCU) (Refer

to AMM 24-41-00, Page Block 501).

2 Shelf 93VU

a Do an operational test of the SEC 3 (Refer to AMM 27-94-00, Page Block

501).

b Do an operational test of the cockpit and cabin temperature control with

Centralized Fault Display (CFDS)/Multipurpose Control and Display Unit

(MCDU) (Refer to AMM 21-63-00, Page Block 501).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 143

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3 Shelf 94VU

a Do the cross-check of TPIS reading and tire pressure gauge (Refer to

AMM 32-49-00, Page Block 501).

b Do an operational test of the lavatory smoke-detection system (Refer to

AMM 26-16-00, Page Block 501).

c Do an operational check of the cargo-compartment smoke-detection by

Push To Test (PTT) (Refer to AMM 26-17-00, Page Block 501).

d Do the BITE test of the BSCU (Refer to AMM 32-46-00, Page Block 501).

e Do an operational test of the aft cargo-compartment heating system

(Refer to AMM 21-43-00, Page Block 501).

(c) Tests after installation of the new C/B

1 Do a voltage check at pin 1 of these C/B to make sure that there is 28VDC :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/A

1WE1 43 Q

121VU ENGINE/ENG1 AND 2 FIRE

EXTIG/BTL1/SQUIB/B

2WE1 44 Q

121VU LGCIU/BAT SPLY/SYS1 58GA 32 R

121VU LGCIU/BAT SPLY/SYS2 59GA 33 R

2 Do an operational test of the circuit breaker monitoring system for the panel

121VU (Refer to AMM 31-50-00, Page Block 501).

(d) Test of the electrical bonding

1 Do a check of the electrical bonding (Refer to AMM 20-28-00, Page Block

501).

NOTE: For the maximum permissible resistance values (Refer to AMM

20-28-00, Page Block 501).

(4) Subtask 321349-720-401-001 - Preparation

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-00-00, Page Block 201

(a) On the overhead panel 35GU switch the batteries ’ON’.

(b) On the overhead panel 35GU switch the external power ’ON’.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 144

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(c) Put the aircraft to Flight Configurations Precautions with Electrical Power (Refer to

AMM 32-00-00, Page Block 201).

(5) Subtask 321349-720-402-001 - Test of Battery Relief Relay 60GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Switch off LGCIU2:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

121VU LGCIU SYS 2 BAT SPLY 59GA R33

(b) LGCIU1 only powered from ground supply:

Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

49VU LGCIU SYS 1 1GA C09

Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(c) On the ECAM wheel page check that the indications that follow are displayed:

1 The MLG Left, MLG Right, Nose LG symbols on the right hand side on the

Wheel page are amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02 for EIS 1

(Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD

screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

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(d) Do a BITE TEST on the LGCIU1 from the MCDU, the result should be test OK

(Refer to AMM Task 32-69-00-740-001).

(e) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

Check that the ECAM Wheel page shows all amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(f) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 01 and Fig. A-UBAAA Sheet 02

OR

Fig. A-UBAAA Sheet 04 and Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check on the ECAM Wheel page that the LGCIU is on:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(h) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 146

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OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(i) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

Check that the ECAM Wheel page remains the same as above, 1GA and 52GA are

already open at this stage:

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(6) Subtask 321349-720-403-001 - Test of System 2 Battery Relief Relay 61GA

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-69-00-740-001

Fig. A-UBAAA

LGCIU Location and Display

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Make sure that 59GA is still open.

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 147

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(b) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 BAT SPLY 59GA R33

Check on the ECAM Wheel page that the LGCIU2 only is energized:

refer to Fig. A-UBAAA Sheet 02 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 05 for EIS 2 (LCD screens).

(c) Open

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

Check on the ECAM Wheel page that after TEN seconds all the gear symbols are

amber ’XX’ (crosses):

refer to Fig. A-UBAAA Sheet 03 for EIS 1 (Cathode Ray Display Screens)

OR

refer to Fig. A-UBAAA Sheet 06 for EIS 2 (LCD screens).

(d) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 2 2GA Q35

(e) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU LGCIU SYS 1 1GA C09

NOTE: To do a BITE test on LGCIU SYS 2 the CFDS must receive a ground

signal from LGCIU1.

(f) On LGCIU2 do a ’BITE’ test from the MCDU, the test result should be test OK

(Refer to AMM Task 32-69-00-740-001).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 148

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(g) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 BAT SPLY 58GA R32

(h) Close

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU LGCIU SYS 1 GND SPLY 52GA Q34

(7) Subtask 321349-720-404-001 - Modified Safety Valve Circuit Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 32-30-00, Page Block 201

NOTE: Diode 1VD 2/17 provides a feed back loop around Relay 62GA and must

be tested, otherwise the Landing Gear will not retract. The test below

avoids jacking the aircraft and swinging the gear.

(a) Make sure that the LG ground locks are fitted and hydraulic systems are

depressurized (Refer to AMM 32-30-00, Page Block 201).

(b) Open the connector 49GA-A Landing Gear Safety Valve (LGSV) and connect a

Portable Voltmeter between pin B and ground.

(c) On the overhead panel 35GU switch the external power ’ON’.

(d) Check that 28 volts appears on the Portable Voltmeter.

(e) Simulate the MLG left, MLG right and NLG to extend by:

1 For Pre-Mod 37831J2877 - Ultra LGCIU P/N 664700500A4x:

Enter interactive mode LGCIU2 use MCDU, go to page 2 of the main menu

and use ’LG SIMULATION MODE’.

2 For Post-Mod 37831J2877 NEW LGCIU P/N 80-178-02-88xxx:

It will be necessary to use false targets (steel) on proximity sensors 22GA,

23GA and 25GA to perform this simulation.

(f) Set the LG control lever 6GA to ’UP’ check that 28V remains indicated on the

Portable Voltmeter, then set the lever to ’DOWN’.

(g) Set the EXT PWR to ’OFF’

(h) Remove the Portable Voltmeter.

(i) Reconnect the 49GA-A connector to the LGSV.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 149

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(8) Subtask 321349-720-405-001 - Relay 62GA Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-31-00-710-005

(a) Perform an operational test of the safety valves (Refer to AMM

Task 32-31-00-710-005, or AMM Task 32-31-00-710-005-01 or AMM Task

32-31-00-710-005-02) ’Operational Check to Ensure Safety Valve Close at 260kts’.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 321349-410-003-001 - INSTALL/CLOSE ITEMS REMOVED/OPENED FOR

ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) In the cockpit, install the sidewall panels 212JW an 212HW (Refer to AMM

25-13-41, Page Block 401).

(b) In the cockpit, install the ceiling panels 212FC and 211HC (Refer to AMM 25-13-41,

Page Block 401).

(c) In the cockpit, install the third occupant seat 14MM (Refer to AMM 25-11-41, Page

Block 401).

(d) Close the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(e) Close the FWD passenger/crew door(s) (Refer to AMM 52-10-00, Page Block 201).

(2) Subtask 321349-942-001-001 - CLOSE-UP PROCEDURES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 150

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References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the close-up procedure as specified in the removal/installation of the GCU 1 and

2 FIN 1XU1 and 1XU2 (if installed) (Refer to AMM 24-22-34, Page Block 401).

(b) Do the close-up procedure as specified in the removal/installation of the GCU APU

FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the close-up procedure as specified in the removal/installation of the SEC 3 FIN

1CE3 (if installed) (Refer to AMM 27-94-34, Page Block 401).

(d) Do the close-up procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the close-up procedure as specified in the removal/installation of the LGCIU 1

and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block 401).

(f) Do the close-up procedure as specified in the removal/installation of the TPIS

detection unit FIN 2GV (if installed) (Refer to AMM 32-49-34, Page Block 401).

(g) Do the close-up procedure as specified in the removal/installation of the SDCU FIN

10WQ (if installed) (Refer to AMM 26-17-34, Page Block 401).

(h) Do the close-up procedure as specified in the removal/installation of the BSCU FIN

10GG (if installed) (Refer to AMM 32-42-34, Page Block 401).

(i) Do the close-up procedure as specified in the removal/installation of the aft cargo

heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block 401).

(j) Do the close-up procedure as specified in the removal/installation of the AFMC FIN

2QN (if installed) (Refer to AMM 28-51-35, Page Block 401).

(3) Subtask 321349-942-002-001 - CLOSE-UP

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

(c) Remove the access platform(s).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 151

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**CONF 002

(1) Subtask 321349-410-003-001 - INSTALL/CLOSE ITEMS REMOVED/OPENED FOR

ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) In the cockpit, install the sidewall panels 212JW an 212HW (Refer to AMM

25-13-41, Page Block 401).

(b) In the cockpit, install the ceiling panels 212FC and 211HC (Refer to AMM 25-13-41,

Page Block 401).

(c) In the cockpit, install the third occupant seat 14MM (Refer to AMM 25-11-41, Page

Block 401).

(d) Close the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(e) Close the FWD passenger/crew door(s) (Refer to AMM 52-10-00, Page Block 201).

(2) Subtask 321349-942-001-001 - CLOSE-UP PROCEDURES

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the close-up procedure as specified in the removal/installation of the GCU 1 and

2 FIN 1XU1 and 1XU2 (if installed) (Refer to AMM 24-22-34, Page Block 401).

(b) Do the close-up procedure as specified in the removal/installation of the GCU APU

FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the close-up procedure as specified in the removal/installation of the SEC 3 FIN

1CE3 (if installed) (Refer to AMM 27-94-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 152

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(d) Do the close-up procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the close-up procedure as specified in the removal/installation of the LGCIU 1

and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block 401).

(f) Do the close-up procedure as specified in the removal/installation of the TPIS

detection unit FIN 2GV (if installed) (Refer to AMM 32-49-34, Page Block 401).

(g) Do the close-up procedure as specified in the removal/installation of the SDCU FIN

10WQ (if installed) (Refer to AMM 26-17-34, Page Block 401).

(h) Do the close-up procedure as specified in the removal/installation of the BSCU FIN

10GG (if installed) (Refer to AMM 32-42-34, Page Block 401).

(i) Do the close-up procedure as specified in the removal/installation of the aft cargo

heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block 401).

(j) Do the close-up procedure as specified in the removal/installation of the AFMC FIN

2QN (if installed) (Refer to AMM 28-51-35, Page Block 401).

(3) Subtask 321349-942-002-001 - CLOSE-UP

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

(c) Remove the access platform(s).

**CONF 003

(1) Subtask 321349-410-003-001 - INSTALL/CLOSE ITEMS REMOVED/OPENED FOR

ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) In the cockpit, install the sidewall panels 212JW an 212HW (Refer to AMM

25-13-41, Page Block 401).

(b) In the cockpit, install the ceiling panels 212FC and 211HC (Refer to AMM 25-13-41,

Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 153

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(c) In the cockpit, install the third occupant seat 14MM (Refer to AMM 25-11-41, Page

Block 401).

(d) Close the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(e) Close the FWD passenger/crew door(s) (Refer to AMM 52-10-00, Page Block 201).

(2) Subtask 321349-942-001-001 - CLOSE-UP PROCEDURES

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the close-up procedure as specified in the removal/installation of the GCU 1 and

2 FIN 1XU1 and 1XU2 (if installed) (Refer to AMM 24-22-34, Page Block 401).

(b) Do the close-up procedure as specified in the removal/installation of the GCU APU

FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the close-up procedure as specified in the removal/installation of the SEC 3 FIN

1CE3 (if installed) (Refer to AMM 27-94-34, Page Block 401).

(d) Do the close-up procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the close-up procedure as specified in the removal/installation of the LGCIU 1

and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block 401).

(f) Do the close-up procedure as specified in the removal/installation of the TPIS

detection unit FIN 2GV (if installed) (Refer to AMM 32-49-34, Page Block 401).

(g) Do the close-up procedure as specified in the removal/installation of the SDCU FIN

10WQ (if installed) (Refer to AMM 26-17-34, Page Block 401).

(h) Do the close-up procedure as specified in the removal/installation of the BSCU FIN

10GG (if installed) (Refer to AMM 32-42-34, Page Block 401).

(i) Do the close-up procedure as specified in the removal/installation of the aft cargo

heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block 401).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 154

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(j) Do the close-up procedure as specified in the removal/installation of the AFMC FIN

2QN (if installed) (Refer to AMM 28-51-35, Page Block 401).

(3) Subtask 321349-942-002-001 - CLOSE-UP

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

(c) Remove the access platform(s).

**CONF 004

(1) Subtask 321349-410-003-001 - INSTALL/CLOSE ITEMS REMOVED/OPENED FOR

ACCESS

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 25-11-41, Page Block 401

25-13-41, Page Block 401

52-10-00, Page Block 201

52-41-00, Page Block 201

(a) In the cockpit, install the sidewall panels 212JW an 212HW (Refer to AMM

25-13-41, Page Block 401).

(b) In the cockpit, install the ceiling panels 212FC and 211HC (Refer to AMM 25-13-41,

Page Block 401).

(c) In the cockpit, install the third occupant seat 14MM (Refer to AMM 25-11-41, Page

Block 401).

(d) Close the access doors 811, 812 and 822 (Refer to AMM 52-41-00, Page Block

201).

(e) Close the FWD passenger/crew door(s) (Refer to AMM 52-10-00, Page Block 201).

(2) Subtask 321349-942-001-001 - CLOSE-UP PROCEDURES

Manpower Resources

Skills NON SPECIFIC

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 155

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References

Aircraft Maintenance Manual (AMM) 21-43-34, Page Block 401

21-63-34, Page Block 401

24-22-34, Page Block 401

24-23-34, Page Block 401

26-17-34, Page Block 401

27-94-34, Page Block 401

28-51-35, Page Block 401

32-31-71, Page Block 401

32-42-34, Page Block 401

32-49-34, Page Block 401

(a) Do the close-up procedure as specified in the removal/installation of the GCU 1 and

2 FIN 1XU1 and 1XU2 (if installed) (Refer to AMM 24-22-34, Page Block 401).

(b) Do the close-up procedure as specified in the removal/installation of the GCU APU

FIN 1XS (if installed) (Refer to AMM 24-23-34, Page Block 401).

(c) Do the close-up procedure as specified in the removal/installation of the SEC 3 FIN

1CE3 (if installed) (Refer to AMM 27-94-34, Page Block 401).

(d) Do the close-up procedure as specified in the removal/installation of the zone

controller FIN 8HK (if installed) (Refer to AMM 21-63-34, Page Block 401).

(e) Do the close-up procedure as specified in the removal/installation of the LGCIU 1

and 2 FIN 5GA1 and 5GA2 (if installed) (Refer to AMM 32-31-71, Page Block 401).

(f) Do the close-up procedure as specified in the removal/installation of the TPIS

detection unit FIN 2GV (if installed) (Refer to AMM 32-49-34, Page Block 401).

(g) Do the close-up procedure as specified in the removal/installation of the SDCU FIN

10WQ (if installed) (Refer to AMM 26-17-34, Page Block 401).

(h) Do the close-up procedure as specified in the removal/installation of the BSCU FIN

10GG (if installed) (Refer to AMM 32-42-34, Page Block 401).

(i) Do the close-up procedure as specified in the removal/installation of the aft cargo

heat controller FIN 10HC (if installed) (Refer to AMM 21-43-34, Page Block 401).

(j) Do the close-up procedure as specified in the removal/installation of the AFMC FIN

2QN (if installed) (Refer to AMM 28-51-35, Page Block 401).

(3) Subtask 321349-942-002-001 - CLOSE-UP

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

(c) Remove the access platform(s).

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 156

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**CONF ALL

UP

DOWN

6GA

N_SB_321349_7_BAAA_01_01

A B

Figure A-UBAAA - Sheet 01

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 157

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**CONF ALL

NLG

MLG LEFT MLG RIGHT

VIEW OF THE WHEEL PAGE WITH ONE LGCIU POWERED.

AMBER

GREEN

AMBER

GREEN

AMBER

GREEN

A

N_SB_321349_7_BAAA_02_02

Figure A-UBAAA - Sheet 02

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 158

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**CONF ALL

NLG

MLG LEFT MLG RIGHT

VIEW OF THE WHEEL PAGE WITH BOTH LGCIU OFF.

AMBER

AMBER AMBER

N_SB_321349_7_BAAA_03_03

B

Figure A-UBAAA - Sheet 03

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 159

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**CONF ALL

UP

DOWN

6GA

C D E

N_SB_321349_7_BAAA_04_01

Figure A-UBAAA - Sheet 04

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 160

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**CONF ALL

NLG

MLG LEFT MLG RIGHT

VIEW OF THE WHEEL PAGE WITH LGCIU1 ’ON’.

GREEN AMBER

GREEN AMBER GREEN AMBER

N_SB_321349_7_BAAA_05_00

C

Figure A-UBAAA - Sheet 05

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 161

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**CONF ALL

NLG

MLG LEFT MLG RIGHT

VIEW ON MCDU WITH BOTH LGCIU OFF

AMBER

AMBER AMBER

N_SB_321349_7_BAAA_06_00

D

Figure A-UBAAA - Sheet 06

LGCIU Location and Display

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 162

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**CONF ALL

MODIFICATION OF THE EQUIPMENT

AND THE WIRING IN 121VU

2M

1M

MODIFICATION OF THE EQUIPMENT

AND THE WIRING IN 93VU

INSTALLATION OF THE

LGCIU PLATE IN 91VU

120VU

90VU

N_SB_321349_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Location of the Working Area

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 163

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**CONF ALL

B

(28)

(31)

(30)

(29)

(2 POS)

Z210

FR1

FR24A

120VU

C

A

(32)

(33)

(34)

(4 POS)

702VU

A

B

C

N_SB_321349_5_ABAA_01_00

Figure A-FABAA - Sheet 01

Removal/Installation of the Equipment in the Cockpit (For Access)

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 164

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**CONF ALL

FR9 A

FR20

FR9 FR10 FR12 FR14 FR16 FR18 FR20

B

A

A/C CL

1031VN

1009VN

1005VN

C

FWD

B

N_SB_321349_5_ACAA_01_00

Figure A-FACAA - Sheet 01

Installation of the New Grounding Points at FR10 in AVNCS Compartment

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 165

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**CONF ALL

1005VN 1037VN 1039VN

50 mm

(1.969 in)

150 mm

(5.906 in)

60 mm

(2.362 in)

A/C CL

2 STRIPPING DIA. 14 mm (0.551 in)

ELECTRICAL BONDING

HOLE

HOLE DIA

MIN.

mm in

MAX.

mm in

5 0.197 5.1 0.201

AFTER

C

N_SB_321349_5_ACAA_02_00

Figure A-FACAA - Sheet 02

Installation of the New Grounding Points at FR10 in AVNCS Compartment

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 166

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**CONF ALL

A

Z210

FR1

FR24A

FR13

120VU

B

A

2

(2)

3

4

(3)

(4)

OR

(5 POS)

(5 POS)

1

121VU

C

C

R

BAT

SPLY

LGCIU

SYS2

SYS1

58GA

59GA

B

C

N_SB_321349_5_ADAA_01_00

23

25

26

27

28

24

3

4

Figure A-FADAA - Sheet 01

Modification of the Equipment in the C/B Panel 121VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 167

7

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SERVICE BULLETIN

**CONF ALL

FR1

FR24A

Z120

A B

E

C

48GA

217VT

93VU

(8)

(12)

(10)

(11)

(9)

(5)

(6)

(7)

90VU

A

B

C

56GA 57GA

D

BEFORE

D

N_SB_321349_5_AEAA_01_00

Figure A-FAEAA - Sheet 01

Modification of the Equipment in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 168

7

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@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

93VU

G

F

POSITION B23

FOOL PROOFING

15 (3 POS)

14

13

679VG

16

62GA

ELECTRICAL BONDING

217VT

679VG

639VG

637VG

H

F

AFTER

E

G

H

N_SB_321349_5_AEAA_02_00

Figure A-FAEAA - Sheet 02

Modification of the Equipment in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 169

7

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SERVICE BULLETIN

**CONF ALL

90VU

A

B

1XU2

GCU−2

1XS

GCU−APU

1XU1

GCU−1

(OPTIONAL)

BEFORE

DISCARD THE ATTACHMENT PARTS 91VU

(22) (17)

(23)

(24)

(6 POS)

C

B

F

W

D

DRAINING PIPE

FR1

FR24A

Z120

A

NOTE :

01

01 01

N_SB_321349_5_AFAA_01_00

Figure A-FAFAA - Sheet 01

Modification of the Equipment in the Shelf 91VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 170

7

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SERVICE BULLETIN

**CONF ALL

AFTER

22

23

24

(6 POS)

21

1XU2

GCU−2

1XS

GCU−APU

1XU1

GCU−1

(OPTIONAL)

91VU

27

23

25

21

26

24

E D

C

D E

F

W

D

DRAINING PIPE

DRAINING PIPE

ELECTRICAL BONDING

27

23

25

21

26

24

38

37 36

37

N_SB_321349_5_AFAA_02_00

Figure A-FAFAA - Sheet 02

Modification of the Equipment in the Shelf 91VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 171

7

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SERVICE BULLETIN

**CONF ALL

91VU

3E

1M

1XS (IF EXISTING)

1037VN 1039VN

FR10

FR9

FR8

2E

2M

203VC−A

(2M)

201VC−A

(1M)

A/C CL

1XU2

GCU−2

1XS

GCU−APU

1XU1

GCU−1

(OPTIONAL)

24

23

22

FR10

A

A

ELECTRICAL BONDING

B

1XU2

FR1

FR24A

Z120

B

N_SB_321349_5_AGAA_01_00

Figure A-FAGAA - Sheet 01

Modification of the Routing behind the Shelf 91VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 172

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBAAA - Sheet 01

Modification of the Wiring in the C/B Panel 121VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 173

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBAAA - Sheet 02

Modification of the Wiring in the C/B Panel 121VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 174

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 121VU 4KS1 3 3154−1565 B PG24 121VU 2803GE 3 M1O

 2 121VU 58GA 3 EN3155−016M2018 3154−1565 B PG24 121VU 2803GE 3 M1N

 3 121VU 4KS1 4 3154−1565 R PG24 121VU 2803GE 4 M1O

 4 121VU 58GA 4 EN3155−016M2018 3154−1565 R PG24 121VU 2803GE 4 M1N

 5

 6

 7

 8 121VU 59GA 1 NSA936501TA1003 2468−0490 DK10 1200 48 121VU 2WE1 1 NSA936501TA1003 (a) A

 9 121VU 59GA 3 EN3155−016M2018 3154−2895 B PG24 500 20 121VU 4KS1 3 EN3155−016M2018 (a) A

10 121VU 59GA 4 EN3155−016M2018 3154−2895 R PG24 500 20 121VU 4KS1 4 EN3155−016M2018 (a) A

11 121VU 59GA 3 EN3155−016M2018 3154−2896 B PG24 500 20 121VU 58GA 3 EN3155−016M2018 (a) A

12 121VU 59GA 4 EN3155−016M2018 3154−2896 R PG24 500 20 121VU 58GA 4 EN3155−016M2018 (a) A

13 121VU 58GA 1 NSA936501TA1003 2468−0489 DK10 900 36 121VU 2803GE 1 NSA936501TA1003 (a) A

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495 M1N = NEW HOOK−UP ON END 1

 A = ADDED WIRE

 M1O = OLD HOOK−UP ON END 1

Figure A-FBAAA - Sheet 03

Modification of the Wiring in the C/B Panel 121VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 175

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBBAA - Sheet 01

Modification of the Wiring in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 176

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBBAA - Sheet 02

Modification of the Wiring in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 177

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBBAA - Sheet 03

Modification of the Wiring in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 178

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 93VU 217VT 8A 3231−0401 1M CF22 93VU 48GA−A B D

 2 93VU 217VT 8B 3231−0405 1M CF22 93VU 48GA−A X D

 3 93VU 217VT 10A 3231−0438 1M CF22 93VU 56GA 2 D

 4 93VU 217VT 10E 3231−0439 1M CF22 93VU 56GA 1 D

 5 93VU 217VT 9A 3231−0440 1M CF22 93VU 57GA + D

 6 93VU 217VT 9E 3231−0441 1M CF22 93VU 57GA − D

 7 93VU 217VT 9K 3231−0442 1M CF22 93VU 621VG GND D

 8 93VU 217VT 10D 3231−0443 1M CF22 93VU 217VT 9F D

 9 93VU 217VT 10F 3231−0446 1M CF22 93VU 48GA−A 4 D

10 93VU 217VT 8C 3231−0447 1M CF20 93VU 48GA−A 2 D

11 93VU 48GA−A A 3231−0400 1M CF20 93VU 213VT 2J D

12 93VU 48GA−A Z 3231−0422 1M CF22 93VU 213VT 5G D

13 93VU 213VT 8H 3231−0433 1M CF20 93VU 53GA−A B2 D

14

15

16

17 93VU 62GA−A A1 EN3155−017F1616 3231−0400 1M CF20 1600 64 93VU 213VT 2J EN3155−016M2018 (a) A

18 93VU 62GA−A X1 EN3155−017F1620 3231−0405 1M CF22 1200 48 93VU 217VT 8B EN3155−016M2018 (a) A

19 93VU 62GA−A X2 EN3155−017F1620 3231−0422 1M CF22 1400 56 93VU 213VT 5G EN3155−016M2222 (a) A

20 93VU 62GA−A A2 EN3155−017F1616 3231−0447 1M CF20 1200 48 93VU 217VT 8C EN3155−016M2018 (a) A

21 93VU 213VT 8H EN3155−016M2018 3231−0433 1M CF20 1000 40 93VU 283VC 45 EN3155−008M1614 (b) A

22 93VU 283VC 44 EN3155−008M1614 3231−0487 1M CF20 2000 80 93VU 53GA−A B2 EN3155−017F1216 (a) A

23 93VU 283VC 47 EN3155−008M1614 3231−0525 1M CF20 2000 80 93VU 679VG GND EN3155−015F2018 (a) A

24

25

 (a) = BUNDLE D9000095223495 D = DELETED WIRE

 (b) = BUNDLE D9000095224595

 A = ADDED WIRE

Figure A-FBBAA - Sheet 04

Modification of the Wiring in the Shelf 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 179

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBCAA - Sheet 01

Modification of the Wiring in the Shelf 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 180

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 94VU 284VC 40 EN3155−008M1614 3231−0532 CF20 2000 80 94VU 654VG GND EN3155−015F2018 (a) A

 2

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

 GND = GROUND

Figure A-FBCAA - Sheet 02

Modification of the Wiring in the Shelf 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 181

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBDAA - Sheet 01

Modification of the Wiring between the Shelves 91VU and 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 182

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 91VU 201VC−A E EN3155−019F2018 3231−0488 1M CF20 5000 200 93VU 283VC−A 44 EN3155−003F1614 (a) A

 2 91VU 201VC−A B EN3155−019F2018 3231−0489 1M CF20 5000 200 93VU 283VC−A 45 EN3155−003F1614 (a) A

 3 91VU 201VC−A C EN3155−019F2018 3231−0526 1M CF20 5000 200 93VU 283VC−A 47 EN3155−003F1614 (a) A

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

Figure A-FBDAA - Sheet 02

Modification of the Wiring between the Shelves 91VU and 93VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 183

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBEAA - Sheet 01

Modification of the Wiring between the Shelves 91VU and 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 184

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 91VU 203VC−A D EN3155−019F2018 3231−0502 2M CF20 6000 240 94VU 284VC−A 40 EN3155−015F2018 (a) A

 2 91VU 203VC−A C EN3155−019F2018 3231−0533 2M CF20 6000 240 94VU 282VC−A 11 EN3155−015F2018 (a) A

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

Figure A-FBEAA - Sheet 02

Modification of the Wiring between the Shelves 91VU and 94VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 185

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBFAA - Sheet 01

Modification of the Wiring between the Shelf 91VU and the AVNCS Compartment

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 186

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 91VU 201VC−A J EN3155−019F2018 3231−0527 1M CF20 1500 60 125 1039VN GND NSA936501TA2004 (a) A

 2 91VU 203VC−A J EN3155−019F2018 3231−0530 2M CF20 2000 80 125 1037VN GND NSA936501TA2004 (a) A

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

 GND = GROUND

Figure A-FBFAA - Sheet 02

Modification of the Wiring between the Shelf 91VU and the AVNCS Compartment

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 187

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBGAA - Sheet 01

Modification of the Wiring between the Rear Panel 120VU and the FWD Electronics Rack 90VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 188

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 94VU 282VC−A 11 3231−0074 2M CF20 120VU 2206VC−A 4 D

 2 91VU 203VC−A B EN3155−019F2018 3231−0074 2M CF20 14000 560 120VU 2206VC−A 4 EN3155−014M2018 (a) A

 3

 4

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FBGAA - Sheet 02

Modification of the Wiring between the Rear Panel 120VU and the FWD Electronics Rack 90VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 189

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBHAA - Sheet 01

Modification of the Wiring between the Rear Panel 120VU and the Shelf 91VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 190

7

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SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 120VU 2254VC Y EN3155−019F2018 3231−0496 1M DK20 4000 160 121VU 58GA 2 NSA936501TA2003 (a) A

 2 120VU 2254VC Z EN3155−019F2018 3231−0509 1M DK20 4000 160 121VU 59GA 2 NSA936501TA2003 (a) A

 3 120VU 2254VC−A Y EN3155−018M2018 3231−0497 1M CF20 20000 800 91VU 201VC−A A EN3155−019F2018 (a) A

 4 120VU 2254VC−A Z EN3155−018M2018 3231−0510 1M CF20 20000 800 91VU 201VC−A D EN3155−019F2018 (a) A

 5

 6

 7

 8

 9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

 (a) = BUNDLE D9000095223495

 A = ADDED WIRE

Figure A-FBHAA - Sheet 02

Modification of the Wiring between the Rear Panel 120VU and the Shelf 91VU

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 191

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBJAA - Sheet 01

Wiring Diagram of the New LGCIU Plate (For Information Only)

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 192

7

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SERVICE BULLETIN

**CONF ALL

Figure A-FBKAA - Sheet 01

Wiring Diagram of the New LGCIU Plate (For Information Only)

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 193

7

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 194

7

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SERVICE BULLETIN

Appendix 1

**CONF ALL

Refer to the subsequent Gantt Chart for the detail concerning the elapsed time assumptions.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 1

7

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SERVICE BULLETIN

Appendix 1

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A320−32−1349

46.0

33.5

3

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

NUMBER OF PEOPLE

NOTE :

STEPS

HOURS

0

CLOSE−UP

GET ACCESS

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

1 5

1 4.0

3.0

X Y

X : NUMBER OF WORKERS

Y : MANHOURS REQUIRED FOR THE TASK

TEST 1 2.5

INSTL OF EQPT IN AVNCS 1 5.0

INSTL OF EQPT IN CKPT 1 3.0

MODIF. OF WIRING 120VU/91VU 1 4.0

1 3.0

1 1.0

1 2.0

MODIF. OF WIRING 120VU/AVNCS

MODIF. OF WIRING 91VU/AVNCS

MODIF. OF WIRING 91VU/94VU

1 2.0

1.0

MODIF. OF EQPT 94VU 0.5

5.0

3.0

1.0

4.0

2.0

INSTL OF GND POINTS

REMOVAL OF EQPT IN AVNCS

REMOVAL OF EQPT IN CKPT

MODIF. OF WIRING 91VU/93VU

MODIF. OF EQPT 91VU

MODIF. OF EQPT/WIRING 93VU

MODIF. OF EQPT/WIRING 121VU

10 15 20 25 30 33.5

1

1

1

1

1

1

1

1

N_SB_321349_5_XXAA_01_01

Figure A-FXXAA - Sheet 01

Elapsed Time Assumptions

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 2

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - EXTENSION AND RETRACTION- INTRODUCE

POWER INTERRUPT PROTECTION CIRCUIT FOR LGCIUS ON A319CJ

AIRCRAFT

MODIFICATION No.: 30248P10949 37866J2818

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: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Dec 04/08 SERVICE BULLETIN No.: A320-32-1349

REVISION No.: 03 - Oct 05/11 Page: 1

7

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