@A340

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

This page transmits Revision No.01 of Service Bulletin No.A340-33-4026

ADDITIONAL WORK

**CONF ALL

REASON

The Revision No.01 issued to:

- update the effectivity.

- amend the KitD02.

CHANGES

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

R

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 1

6

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS

Kit 334026D02R01 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 334026- 831-848-001-Modification

Subtask 334026-831-205-002 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

MATERIAL LIST UPDATED

R

Subtask 334026-831-205-002 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

MATERIAL LIST 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Jan 03/12

REVISION No. : 01 - Jul 10/12

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201683D46730

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

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19 (5LJ, 6LJ, 7LJ

and 8LJ) are to be removed.

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

The affected circuit breakers are to be opened and safetied. Related wires and connections that

are no longer used are to be stowed properly. Installation positions (for unit installation and ground

connections) must be protected with sealants and anti-corrosion treatments as applicable.

With the accomplishment of this Service Bulletin the applicable aircraft obey the instructions of SFAR88

for the de-activation of maintenance maintenance lights 5LJ, 6LJ, 7LJ and 8LJ.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 1

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@A340

SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 334026D01R02 1 242.00 Caps, clip, placard set and ties

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 334026D01R02 1 242.00 Caps, clip, placard set and ties

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 334026D01R02 1 242.00 Caps, clip, placard set and ties

Kit 334026D02R01 1 37.00 Clamp, washer, screw and spacer

TOTAL 279.00

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 334026D01R02 1 242.00 Caps, clip, placard set and ties

Kit 334026D02R01 1 37.00 Clamp, washer, screw and spacer

TOTAL 279.00

EFFECTIVITY

**CONF ALL

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

47W 56W 83V AAW AFR ALK ARG CAL CCA CES CPA DGA DLH

FIN GAF GFA HFY IBE IRC KAC KNE LAN M3R MAU MDG MSR

NMB PAL QAF RJA S3R SAA SAS SFB SLM SVW SWR TAP THT

THY UAE VCV VIR XAX

CONCURRENT REQUIREMENTS

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 2

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

SUMMARY

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 334026-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 334026-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Task 334026-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 004

Task 334026-831-848-001: Modification

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

APPENDICES

**CONF ALL

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 3

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z270

A

FR77

FR75

FR72

5005VE

FR76

A

Z310

FR83

FR87

4LJ

FR84

5872VB /2M

FR85

BEFORE

6LJ

5012VN /DC2 FR88

7LJ

8LJ

5315VN /DC2

5420VN /DC2

5LJ

5011VN /DC2

B

C

B C

D

D

D

D

5LJ

6LJ

7LJ

8LJ

LH

RH

LH

RH

D

TYPICAL

AFTER

TYPICAL

E

E

5872VB /2M

F_SB_334026_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 33

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

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

This modification is applicable by Service Bulletin only.

(1) Models

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002-0006 0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044

0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131

0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233

0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270

0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325

0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374

0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424

0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528

0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646

0651 0668 0793 0800 0835 0844 0921 0938 0955

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 1

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@A340

SERVICE BULLETIN

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

47W 0009

56W 0003 0013 0015

83V 0235 0239 0280 0292

AAW 0151

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

ALK 0032 0033 0034 0367 0374 0381

ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126 0128 0373

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233

0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390

0434 0447

FIN 0058 0168 0174 0835 0844 0921 0938

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133

IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318

0329 0332 0387 0414 0459 0474 0483

IRC 0002

KAC 0089 0090 0101 0104

KNE 0004

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0210 0319

MSR 0156 0159 0178

NMB 0047 0051

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0011 0018 0019 0021 0197 0378 0544 0582 0590 0643 0646

0651

SAS 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 2

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@A340

SERVICE BULLETIN

OPERATOR MSN

SVW 0955

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0216 0257 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0236

VCV 0031

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0003 0004 0006 0013 0015 0020 0024 0026 0027 0028

0031 0032 0033 0034 0035 0038 0041 0043 0044 0046 0047

0048 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074

0075 0076 0078 0079 0080 0081 0084 0085 0088 0089 0090

0091 0093 0094 0101 0104 0114 0115 0117 0123 0125 0126

0128 0129 0131 0133 0134 0135 0136 0137 0139 0141 0142

0145 0146 0147 0149 0150 0151 0152 0154 0156 0157 0158

0159 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173

0174 0175 0176 0178 0179 0180 0182 0185 0186 0187 0190

0192 0193 0194 0354

003

0005 0009 0011 0014 0018 0019 0021 0022 0023 0025 0029 004

0196 0197 0199 0201 0202 0204 0207 0208 0210 0212 0213

0214 0215 0216 0217 0218 0220 0221 0225 0227 0228

001

0233 0235 0236 0237 0239 0242 0243 0245 0246 0252 0257

0260 0263 0264 0268 0270 0273 0274 0278 0280 0282 0292

0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329

0331 0332 0335 0347 0352 0355 0359 0363 0367 0373 0374

0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406

0411 0413 0414 0415 0424 0429 0430 0433 0434 0435 0438

0442 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538

0541 0544 0545 0546 0554 0556 0559 0561 0562 0582 0585

0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921

0938 0955

002

(5) Configuration definition

**CONF 001

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

standard configuration.

**CONF 002

Config. 002 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 3

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@A340

SERVICE BULLETIN

**CONF 003

Config. 003 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

**CONF 004

Config. 004 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

NOTE: The Kit 334026D01R02 and the Kit 334026D02R01 are not necessary, if

Service Bulletin No. A340-33-4027 will be embodied at the same time.

**CONF 001 thru 002

MATERIAL QTY PER A/C SEE NOTES

Kit 334026D01R02 1

Consumable CMLD01 1

**CONF 003 thru 004

MATERIAL QTY PER A/C SEE NOTES

Kit 334026D01R02 1

Kit 334026D02R01 1

Consumable CMLD01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

To obey SFAR88 instructions for in-service aircraft, the maintenance lights in section 19

(5LJ, 6LJ, 7LJ and 8LJ) are to be removed.

(2) Objective/Action

This Service Bulletin gives the procedure to remove the maintenance lights 5LJ, 6LJ,

7LJ and 8LJ. The affected circuit breakers are to be opened and safetied. Related wires

and connections that are no longer used are to be stowed properly. Installation positions

(for unit installation and ground connections) must be protected with sealants and anticorrosion treatments as applicable.

(3) Advantages

With the accomplishment of this Service Bulletin the applicable aircraft obey the

instructions of SFAR88 for the de-activation of maintenance maintenance lights 5LJ, 6LJ,

7LJ and 8LJ.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 4

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@A340

SERVICE BULLETIN

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 334026-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF 002

Task 334026-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF 003

Task 334026-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 5

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@A340

SERVICE BULLETIN

**CONF 004

Task 334026-831-848-001: Modification

(1) Modify the circuit breaker panel 5005VE

(2) Modify the electrical wiring of the button toggle 4LJ

(3) Remove the maintenance light 5LJ and modify the electrical wire

(4) Remove the maintenance light 6LJ and modify the electrical wire

(5) Remove the maintenance lights 7LJ and 8LJ and modify the electrical wires

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

F. APPROVAL

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

Organisation 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 334026-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 6

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@A340

SERVICE BULLETIN

Task 334026-831-848-001: Modification

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 002

Task 334026-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Task 334026-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 7

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@A340

SERVICE BULLETIN

Task 334026-831-848-001: Modification

ELAPSED TIME (HOURS) 5.75

**CONF 004

Task 334026-831-848-001: Modification

Get Access 0.25

On Aircraft

Modify the circuit breaker panel 5005VE 0.25

Modify the electrical wiring of the button toggle 4LJ 0.50

Remove the maintenance light 5LJ and modify the

electrical wire

1.00

Remove the maintenance light 6LJ and modify the

electrical wire

1.00

Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

2.00

Tests 0.50

Close-Up 0.25

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001 thru 002

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Only for aircraft model A340-200

Manufactures Empty Weight -1.558 KG -3.4347 LB

Effect on Balance -90.220 KGM -652.561 LB.FT

Only for aircraft model A340-300

Manufactures Empty Weight -1.558 KG -3.4347 LB

Effect on Balance -96,870 KGM -700.660 LB.FT

**CONF 003 thru 004

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 8

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@A340

SERVICE BULLETIN

Only for aircraft model A340-200

Manufactures Empty Weight -1.550 KG -3.4171 LB

Effect on Balance -89.741 KGM -649.096 LB.FT

Only for aircraft model A340-300

Manufactures Empty Weight -1.550 KG -3.4171 LB

Effect on Balance -96.356 KGM -696.943 LB.FT

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

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

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A340-33-4027

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

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

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A340-33-4027

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 003

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 9

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SERVICE BULLETIN

Consumable Material List (CML)

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

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A340-33-4027

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF 004

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-16-00 20-28-00

24-41-00 31-18-00 33-31-00

33-31-11 52-10-00

Consumable Material List (CML)

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

20-42-13 20-51-21 20-51-22

20-54-55 20-55-00

Service Bulletin (SB) A340-33-4027

Standards Manual (SM)

Weight and Balance Manual (WBM) Weight and Balance Manual

(WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 33-31-00 33-31-11

Aircraft Schematic Manual (ASM) 33-31-00

Illustrated Parts Catalog (IPC) 33-31-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 334026D01R02

Kit 334026D02R01

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:

AIRBUS Material, Logistics and Suppliers

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

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 334026D01R02

Cost 242.00 USD

Availability 45 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 Kits 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

Kit 334026D02R01

Cost 37.00 USD

Availability 45 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 Kits 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. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

C. LIST OF COMPONENTS

Kit 334026D01R02

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

NOTES

1 NSA936603CC0100 5 CAP

2 NSA935401-03 15 TIE

3 ABS0772A01A 1 CLIP

9 F9239025710100 1 PLCRDSET

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 334026D02R01

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

NOTES

5 MS21919WCH2 2 CLAMP

6 NAS1149C0332R 2 WASHER

7 NAS1096-2-12 2 SCREW

8 NSA5527-03-01 2 SPACER

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Electrical Bonding Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

Lockwire Stainlss Stl Or Nickel Alloy 19-018 As required

(2) Components

None

(3) Equipment

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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This Page Intentionally Left Blank

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 334026-831-848-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE

LANDING GEAR.

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START A TASK ON OR NEAR :

- THE FLIGHT CONTROLS

- THE FLIGHT CONTROL SURFACES

- THE LANDING GEAR AND THE RELATED DOORS

- COMPONENTS THAT MOVE.

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS LIGHT

BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN YOU IF YOU

TOUCH IT.

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 ELECTRICAL 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

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 002

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 003

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF 004

Zone

270 310

Modified FIN

4LJ 5LJ 6LJ 7LJ 8LJ

Manpower

TOTAL MANHOURS 5.75

ELAPSED TIME (HOURS) 5.75

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 334026-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 16

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, 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

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 334026-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 334026-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

20-28-00, Page Block 201

Consumable Material List (CML)

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 17

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SERVICE BULLETIN

References

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

20-33-00

20-33-44

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 334026-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 003

(1) Subtask 334026-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, 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

20-51-21

Standards Manual (SM)

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 18

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SERVICE BULLETIN

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 334026-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 334026-910-201-001 - Standard Practices

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, 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

20-51-21

Standards Manual (SM)

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

Consumable Materials List (CML)).

(b) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(c) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

(d) For the identification of the access panels (Refer to AMM 06-41-53, Page Block

001).

(e) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201 and ESPM

20-51-21).

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

(g) For the cable tie application and tooling (Refer to ESPM 20-25-51 and ESPM

20-33-44).

(2) Subtask 334026-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 334026-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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SERVICE BULLETIN

**CONF 002

(1) Subtask 334026-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

**CONF 003

(1) Subtask 334026-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

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**CONF 004

(1) Subtask 334026-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 24-41-00-861-801

Task 52-10-00-010-801

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).

(c) Put access platform(s) in position below the access door 312AR.

(d) Open the access door 312AR.

(e) Put access platform(s) in position below the AFT passenger/crew door 833.

(f) Open the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-010-801).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 334026-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

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Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE.

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 334026-831-202-001 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

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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 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAA

Modification of the Electrical Wiring of

the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ.

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAA Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

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3 Install:

1 Placard set F9239025710100 Item 9

(3) Subtask 334026-831-203-001 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAA

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wire

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

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WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAA Sheet 01, View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAA Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 26

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@A340

SERVICE BULLETIN

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(4) Subtask 334026-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 27

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014.

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 28

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(5) Subtask 334026-831-205-001 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

9 F9239025710100 2 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAA

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 29

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance lights 7LJ and 8LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAA Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017.

Refer to Fig. A-GBEAA Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 30

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710100 Item 9

**CONF 002

(1) Subtask 334026-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 31

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE.

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 334026-831-202-001 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 32

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAA

Modification of the Electrical Wiring of

the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ.

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAA Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710100 Item 9

(3) Subtask 334026-831-203-002 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 33

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAB

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ:

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAB Sheet 01, View B.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 34

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@A340

SERVICE BULLETIN

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAB Sheet 02.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 35

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(4) Subtask 334026-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 36

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014.

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 37

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(5) Subtask 334026-831-205-001 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

9 F9239025710100 2 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAA

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 38

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

(a) Remove the maintenance lights 7LJ and 8LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAA Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017.

Refer to Fig. A-GBEAA Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 39

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

1 Install:

2 Placard set F9239025710100 Item 9

**CONF 003

(1) Subtask 334026-831-201-001 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAA

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAA

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE.

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

1 Open, safety/lock and tag this circuit breaker:

Refer to AMM Task 31-18-00-010-801.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 40

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAA Sheet 01, View C and D.

Refer to Fig. A-GWCAA Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT SEC19 1LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 334026-831-202-002 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAB

Modification of the Electrical Wire 5003

of the Button Toggle 4LJ

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 41

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

References

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ.

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAB Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710100 Item 9

(3) Subtask 334026-831-203-003 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 42

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAC

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAC Sheet 01, View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAC Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 43

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SERVICE BULLETIN

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

Fig. A-GBCAC Sheet 02, View D.

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 44

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SERVICE BULLETIN

(4) Subtask 334026-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 45

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SERVICE BULLETIN

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014.

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(5) Subtask 334026-831-205-002 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 46

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@A340

SERVICE BULLETIN

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

9 F9239025710100 2 PLCRDSET

Kit 334026D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

5 MS21919WCH2 2 CLAMP

6 NAS1149C0332R 2 WASHER

7 NAS1096-2-12 2 SCREW

8 NSA5527-03-01 2 SPACER

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAB

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance lights 7LJ and 8LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAB Sheet 01, View B.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 47

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SERVICE BULLETIN

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017.

Refer to Fig. A-GBEAB Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

3 Install:

2 Clamp MS21919WCH2 Item 5

2 Washer NAS1149C0332R Item 6

2 Screw NAS1096-2-12 Item 7

2 Spacer NSA5527-03-01 Item 8

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 48

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@A340

SERVICE BULLETIN

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710100 Item 9

**CONF 004

(1) Subtask 334026-831-201-002 - Modify the circuit breaker panel 5005VE

Work Zones and Access Panels

Zone Access/Work location

270

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 ABS0772A01A 1 CLIP

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Lockwire Stainlss Stl Or

Nickel Alloy

19-018 As required

References

Aircraft Maintenance Manual (AMM) Task 20-16-00-912-801

Task 31-18-00-010-801

Fig. A-GBAAB

Modification of the Circuit Breaker Panel

5005VE

Sheet 01

Fig. A-GWCAB

Wiring 3

Sheet 01

(a) Modify the circuit breaker panel 5005VE.

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS

YOU DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND

YOU.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 49

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SERVICE BULLETIN

1 Open, safety/lock and tag this (these) circuit breaker(s):

Refer to AMM Task 31-18-00-010-801.

Refer to AMM Task 20-16-00-912-801.

Refer to Fig. A-GBAAB Sheet 01, View C and D.

Refer to Fig. A-GWCAB Sheet 01.

PANEL DESIGNATION FIN LOCATION SEE

NOTES

5005VE LIGHT APU 2LJ D06

and install:

1 Clip-Locking ABS0772A01A Item 3

with:

Lockwire Stainlss

Stl Or Nickel Alloy

19-018 As required

(2) Subtask 334026-831-202-002 - Modify the electrical wiring of the button toggle 4LJ

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBBAB

Modification of the Electrical Wire 5003

of the Button Toggle 4LJ

Sheet 01

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 50

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SERVICE BULLETIN

References

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

(a) Modify the electrical wire 5003 and the button toggle 4LJ.

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GBBAB Sheet 01, View B to D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 1 and 2.

1 Remove the electrical wire 5003 from the button toggle 4LJ.

2 Stow the electrical wire 5003, install:

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

3 Install:

1 Placard set F9239025710100 Item 9

(3) Subtask 334026-831-203-003 - Remove the maintenance light 5LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 51

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@A340

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Electrical Coating (Blue

Color)

07-001 As required

Sealant 09-007 As required

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-51-22

20-54-55

Fig. A-GBCAC

Removal of the Maintenance Light 5LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

Fig. A-GHAAA

Hookup Chart

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 5LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBCAC Sheet 01, View B.

1 Remove:

FIN 5LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 52

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SERVICE BULLETIN

(b) Remove the electrical wire 5016.

Refer to Fig. A-GBCAC Sheet 02, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 13.

1 Remove the bonding connection of the maintenance light 5LJ and the

maintenance socket 11LJ:

Fig. A-GBCAC Sheet 02, View D.

1 Nut MS21042-08 Item (17) Retain

1 Washer NAS1149C0332R Item (6) Retain

1 Screw NAS1096-3-8 Item (16) Retain

2 Remove the electrical wire 5016.

3 Re-install the bonding connection of the maintenance socket 11LJ:

1 Nut MS21042-08 Item (17) Retained at

removal

1 Washer NAS1149C0332R Item (6) Retained at

removal

1 Screw NAS1096-3-8 Item (16) Retained at

removal

4 Apply to the bonding connection 5011VN/DC2:

Refer to ESPM 20-51-22.

Sealant 09-007 As required

and

Electrical Coating

(Blue Color)

07-001 As required

(c) Stow the electrical wire 5008, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 9 and 10.

1 Cap NSA936603CC0100 Item 1

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 53

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SERVICE BULLETIN

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

(4) Subtask 334026-831-204-001 - Remove the maintenance light 6LJ and modify the

electrical wire

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 1 CAP

2 NSA935401-03 3 TIE

9 F9239025710100 1 PLCRDSET

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBDAA

Removal of the Maintenance Light 6LJ

and Modification of the Electrical Wiring

Sheet 01

Sheet 02

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

(a) Remove the maintenance light 6LJ.

Refer to AMM Task 33-31-11-000-801.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 54

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@A340

SERVICE BULLETIN

Refer to Fig. A-GBDAA Sheet 01, View B.

1 Remove:

FIN 6LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

4 Screw NAS1096-3-7 Item (12) Discard

4 Washer NAS1149DN816K Item (13) Discard

2 Nut Item (14) Discard

2 Washer Item (15) Discard

(b) Remove the electrical wire 5014.

Refer to Fig. A-GBDAA Sheet 02, View D.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Line 11.

1 Remove the bonding connection of the maintenance light 6LJ:

1 Nut MS21042-08 Item (17) Discard

1 Washer NAS1149C0332R Item (6) Discard

1 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wire 5014.

(c) Stow the electrical wire 5005, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 3 and 4.

1 Cap NSA936603CC0100 Item 1

3 Tie-Cable NSA935401-03 Item 2

1 Install:

1 Placard set F9239025710100 Item 9

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 55

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@A340

SERVICE BULLETIN

(5) Subtask 334026-831-205-002 - Remove the maintenance lights 7LJ and 8LJ and

modify the electrical wires

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills ELECTRICAL

Material necessary to do the job

Kit 334026D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA936603CC0100 2 CAP

2 NSA935401-03 6 TIE

9 F9239025710100 2 PLCRDSET

Kit 334026D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

5 MS21919WCH2 2 CLAMP

6 NAS1149C0332R 2 WASHER

7 NAS1096-2-12 2 SCREW

8 NSA5527-03-01 2 SPACER

References

Aircraft Maintenance Manual (AMM) Task 33-31-11-000-801

Elec. Std. Practices Manual (ESPM) 20-42-13

20-54-55

Fig. A-GBEAB

Removal of the Maintenance Light 7LJ

and 8LJ and Modification of the

Electrical Wiring

Sheet 01

Sheet 02

Sheet 03

Fig. A-GHAAA

Hookup Chart

Sheet 01

Fig. A-GWAAA

Wiring 1

Sheet 01

Fig. A-GWBAA

Wiring 2

Sheet 01

WARNING: LET THE LIGHT BECOME COOL BEFORE YOU TOUCH IT. THIS

LIGHT BECOMES VERY HOT WHEN IT IS ON, AND IT CAN BURN

YOU IF YOU TOUCH IT.

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 56

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@A340

SERVICE BULLETIN

(a) Remove the maintenance lights 7LJ and 8LJ.

Refer to AMM Task 33-31-11-000-801.

Refer to Fig. A-GBEAB Sheet 01, View B.

1 Remove:

FIN 7LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

FIN 8LJ

1 Light-Service Area 2LA002606-01 Item (11) Discard

8 Screw NAS1096-3-7 Item (12) Discard

8 Washer NAS1149DN816K Item (13) Discard

4 Nut Item (14) Discard

4 Washer Item (15) Discard

(b) Remove the electrical wires 5015 and 5017.

Refer to Fig. A-GBEAB Sheet 01, View E to G.

Refer to Fig. A-GWAAA Sheet 01.

Refer to Fig. A-GWBAA Sheet 01.

Refer to Fig. A-GHAAA Sheet 01, Lines 12 and 14.

1 Remove the bonding connection of the maintenance lights 7LJ and 8LJ:

2 Nut MS21042-08 Item (17) Discard

2 Washer NAS1149C0332R Item (6) Discard

2 Screw NAS1096-3-8 Item (16) Discard

2 Remove the electrical wires 5015 and 5017.

3 Install:

2 Clamp MS21919WCH2 Item 5

2 Washer NAS1149C0332R Item 6

2 Screw NAS1096-2-12 Item 7

2 Spacer NSA5527-03-01 Item 8

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 57

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@A340

SERVICE BULLETIN

(c) Stow the electrical wires 5007 and 5006, install:

Refer to ESPM 20-42-13 and ESPM 20-54-55.

Refer to Fig. A-GHAAA Sheet 01, Lines 5, 6, 7 and 8.

2 Cap NSA936603CC0100 Item 1

6 Tie-Cable NSA935401-03 Item 2

1 Install:

2 Placard set F9239025710100 Item 9

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 334026-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF 002

(1) Subtask 334026-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 58

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@A340

SERVICE BULLETIN

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF 003

(1) Subtask 334026-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

**CONF 004

(1) Subtask 334026-700-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

310

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 33-31-00-720-801

(a) Make sure that the resistance (ohmic) of the bonding connection 5011VN/DC2 of

the maintenance socket 11LJ is correct.

(b) Do the functional test of the maintenance socket 11LJ (Refer to AMM Task

33-31-00-720-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 59

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@A340

SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 334026-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

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

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

**CONF 002

(1) Subtask 334026-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

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

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 60

6

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@A340

SERVICE BULLETIN

**CONF 003

(1) Subtask 334026-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

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

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

**CONF 004

(1) Subtask 334026-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 52-10-00-410-801

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

equipment.

(b) Close the access door 312AR.

(c) De-energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-862-801).

(d) Remove the access platform(s).

(e) Close the AFT passenger/crew door 833 (Refer to AMM Task 52-10-00-410-801).

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 61

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001 thru 003

LIGHT

C

NOTE:

01 SAFETY THE CLIP WITH LOCKWIRE (MAT. NO. 19−018)

3 01

D

SEC19

1LJ

A

B

FR77

FR75

FR72 5005VE

FR76 C

APU

LAV

AFT&MID PAX & CABIN ATTND

D

B

F_SB_334026_6_BAAA_01_00

Z270

A

Figure A-GBAAA - Sheet 01

Modification of the Circuit Breaker Panel 5005VE

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 62

6

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@A340

SERVICE BULLETIN

**CONF 004

LIGHT

C

NOTE:

01 SAFETY THE CLIP WITH LOCKWIRE (MAT. NO. 19−018)

3 01

D

SEC19

2LJ

A

B

FR77

FR75

FR72 5005VE

FR76 C

APU

LAV

AFT&MID PAX & CABIN ATTND

D

B

Z270

A

F_SB_334026_6_BAAB_01_00

Figure A-GBAAB - Sheet 01

Modification of the Circuit Breaker Panel 5005VE

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 63

6

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@A340

SERVICE BULLETIN

**CONF 001 thru 002

Z310

5872VB /2M

FR83

FR87

A

4LJ

FR84

B C

BEFORE

AFTER

5872VB /2M

FR84

4LJ

B

F

W

D

4LJ C F

W

D

FR84

D

MOD. 201683

SB33−4026

2

1

9

D

AFTER

TO

4LJ

A

F_SB_334026_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Modification of the Electrical Wiring of the Button Toggle 4LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 64

6

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@A340

SERVICE BULLETIN

**CONF 003 thru 004

FR83

FR87

A

4LJ

FR84

B C

BEFORE

5872VB /2M

FR84

4LJ

B

VIEW LOOKING FWD

VIEW LOOKING FWD

AFTER

C

4LJ

5872VB /2M

FR84

STGR33RH

STGR34RH

STGR33RH

STGR34RH

D

Z310

A

F_SB_334026_6_BBAB_01_01

MOD. 201683

SB33−4026

2

1

9

D

AFTER

TO

4LJ

Figure A-GBBAB - Sheet 01

Modification of the Electrical Wire 5003 of the Button Toggle 4LJ

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 65

6

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@A340

SERVICE BULLETIN

**CONF 001

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

Z310

A

F_SB_334026_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 66

6

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@A340

SERVICE BULLETIN

**CONF 001

5872VB /2M 5LJ

BEFORE

AFTER

FR85

C F

W

D

D

5011VN /DC2

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

F

W

D

E

5872VB /2M

5011VN /DC2

BEFORE

TO 11LJ

AFTER

F

F

G

(16)

(6)

(17)

AFTER

FR85

MOD. 201683

SB33−4026

2

1

9

G

F_SB_334026_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wire

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 67

6

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@A340

SERVICE BULLETIN

**CONF 002

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

Z310

A

F_SB_334026_6_BCAB_01_01

Figure A-GBCAB - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 68

6

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@A340

SERVICE BULLETIN

**CONF 002

5LJ

BEFORE

AFTER

FR85

C F

W

D

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

BEFORE

TO 11LJ

AFTER

F (16)

(6)

(17)

D

G F

FR85

F

W

D

E

5011VN /DC2

5011VN /DC2

F_SB_334026_6_BCAB_02_02

MOD. 201683

SB33−4026

2

1

9

AFTER

G

5872VB /2M

5872VB /2M

Figure A-GBCAB - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 69

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003 thru 004

B

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

5LJ

11LJ

FR83

FR85

FR87

FR85

B

A

C E

5011VN /DC2

5LJ

Z310

A

F_SB_334026_6_BCAC_01_01

Figure A-GBCAC - Sheet 01

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 70

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 003 thru 004

5872VB /2M

5LJ

BEFORE

AFTER

FR85

C F

W

D

5011VN /DC2

TO 5LJ

TO 11LJ

(16)

(6)

(17)

D

F

W

D

E

5872VB /2M

5011VN /DC2

BEFORE

TO 11LJ

AFTER

F (16)

(6)

(17)

D

11LJ

G

F

11LJ

FR85

F_SB_334026_6_BCAC_02_02

MOD. 201683

SB33−4026

2

1

9

AFTER

G

Figure A-GBCAC - Sheet 02

Removal of the Maintenance Light 5LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 71

6

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@A340

SERVICE BULLETIN

**CONF ALL

(14) B (15)

(11)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

FR83

FR85

FR87

FR85

A

6LJ

5012VN /DC2

B

C E

6LJ

Z310

A

F_SB_334026_6_BDAA_01_01

Figure A-GBDAA - Sheet 01

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 72

6

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@A340

SERVICE BULLETIN

**CONF ALL

5872VB /2M

BEFORE

AFTER

D

5872VB /2M

TO 6LJ (16)

(6)

(17) 6LJ

STGR18RH

STGR20RH

STGR20RH

STGR18RH

C

VIEW LOOKING FWD

5012VN /DC2

D

BEFORE

E

VIEW LOOKING FWD

F

FR83

FR83

MOD. 201683

SB33−4026

2

1

9

AFTER

F

F_SB_334026_6_BDAA_02_02

Figure A-GBDAA - Sheet 02

Removal of the Maintenance Light 6LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 73

6

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@A340

SERVICE BULLETIN

**CONF 001 thru 002

B

(11)

5872VB /2M

TYPICAL

FR83

FR85

FR88

A

7LJ

8LJ

B

C E

Z310

A

5315VN /DC2

5420VN /DC2

(14)

(15)

(11)

(12)

(13)

(4 POS)

(4 POS)

7LJ

8LJ

LH

RH

F_SB_334026_6_BEAA_01_02

Figure A-GBEAA - Sheet 01

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 74

6

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@A340

SERVICE BULLETIN

**CONF 001 thru 002

5872VB /2M

C

(16)

(6)

(17)

BEFORE

D

5315VN /DC2

5420VN /DC2

7LJ

8LJ

LH

RH

TYPICAL

RH

LH

F

W

D

FR88

BEFORE

D

F_SB_334026_6_BEAA_02_01

TYPICAL

TO 7LJ LH

TO 8LJ RH

Figure A-GBEAA - Sheet 02

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 75

6

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@A340

SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL

F

W

D

E

AFTER

F

FR80

5872VB /2M

MOD. 201683

SB33−4026

2

1

9

AFTER

F_SB_334026_6_BEAA_03_02

F

Figure A-GBEAA - Sheet 03

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 76

6

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@A340

SERVICE BULLETIN

**CONF 003 thru 004

B

(14)

(15)

(12)

(13)

(4 POS)

(4 POS)

5872VB /2M

TYPICAL

C E

FR83

FR85

FR87

A

7LJ

8LJ

B

Z310

A

5315VN /DC2

5420VN /DC2

(11) 7LJ

8LJ

LH

RH

F_SB_334026_6_BEAB_01_02

Figure A-GBEAB - Sheet 01

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 77

6

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@A340

SERVICE BULLETIN

**CONF 003 thru 004

5872VB /2M

5315VN /DC2

5420VN /DC2

C

VIEW LOOKING FWD

BEFORE

TO 7LJ LH

(16)

(6)

(17)

TO 8LJ RH

TYPICAL

D

D

7LJ

8LJ

LH

RH

TYPICAL

RH

LH

BEFORE

F_SB_334026_6_BEAB_02_00

Figure A-GBEAB - Sheet 02

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 78

6

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@A340

SERVICE BULLETIN

**CONF 003 thru 004

AFTER

6

E

VIEW LOOKING FWD

TYPICAL

F

G

8 5

7

AFTER

G

5872VB /2M

MOD. 201683

SB33−4026

2

1

9

AFTER

F_SB_334026_6_BEAB_03_02

F

Figure A-GBEAB - Sheet 03

Removal of the Maintenance Light 7LJ and 8LJ and Modification of the Electrical Wiring

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 79

6

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@A340

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

BEFORE

5003

NOTE:

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

6LJ

312

5014

8LJ

312

5015

2

1

2

1

1

2

1

2

5012VN

DC2

5420VN

DC2

50165017

5011VN

DC2

5315VN

DC2

EXISTING WIRE

5LJ

311

7LJ

311

F_SB_334026_6_WAAA_01_00

Figure A-GWAAA - Sheet 01

Wiring 1

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 80

6

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@A340

SERVICE BULLETIN

**CONF ALL

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

1

5200VT

312

AFTER

5003

NOTE:

F

G

H

J

K

B

C

A

D

E

1

2

4LJ

312

5005

5006

5007

5008

EXISTING WIRE

REROUTED WIRE

STOWED WIRE

F_SB_334026_6_WBAA_01_00

Figure A-GWBAA - Sheet 01

Wiring 2

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 81

6

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@A340

SERVICE BULLETIN

**CONF 001 thru 003

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

BEFORE

NOTE:

EXISTING WIRE

1 2

7.5A

1LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

AFTER

1 2

7.5A

1LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

28V DC

GROUND

BUS

28V DC

GROUND

BUS

F_SB_334026_6_WCAA_01_01

Figure A-GWCAA - Sheet 01

Wiring 3

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 82

6

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@A340

SERVICE BULLETIN

**CONF 004

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE IDENTIFICATION WITH ATA−NO.3331

UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF18 GAUGE

UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2M

BEFORE

NOTE:

EXISTING WIRE

1 2

7.5A

2LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

AFTER

1 2

7.5A

2LJ

1 2

4LJ

312

5040

5005VE

AFT CIRCUIT BREAKER PANEL

28V DC

GROUND

BUS

28V DC

GROUND

BUS

F_SB_334026_6_WCAB_01_01

Figure A-GWCAB - Sheet 01

Wiring 3

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 83

6

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@A340

SERVICE BULLETIN

**CONF ALL

L

I

N

E ZONE OR

PANEL TERM. TERMINAL P/N WIREIDENT C0L ROUTE GAUGE

LENGTH

MM INCH

ZONE OR

PANEL

ELEC.

IDENT TERM. TERMINAL P/N

INSTRUCTIONS

END 1 LEAD END 2

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

1

2

3

4

5

6

7

8

9

ELEC.

IDENT.

3331−5003

3331−5003

3331−5005

3331−5005

3331−5006

3331−5006

3331−5007

3331−5007

3331−5008

3331−5008

312 4LJ

312

2

STOW

2M CF18

2M

2M

2M

2M

2M

2M

2M

2M

2M

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

CF18

312

312

5200VT

5200VT

312

312

311

311

6LJ

8LJ

7LJ

5LJ

1A

1A

STOW

STOW

STOW

STOW

1

1

1

1

312

312

312

312

312

312

312

312

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

5200VT

1B

1B

1C

1C

1D

1E

1D

1E

NSA936501TA1602

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

EN3155−016M2018

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

NSA936603CC0100

BEFORE

AFTER

BEFORE

BEFORE

BEFORE

BEFORE

AFTER

AFTER

AFTER

AFTER

312

312

311

311

6LJ

8LJ

5LJ

7LJ

2

2

2

2

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

NSA936501TA1602

3331−5014

3331−5015

3331−5016

3331−5017

2M

2M

2M

2M

CF18

CF18

CF18

CF18

312

312

311

311

5012VN

5420VN

5011VN

5315VN

DC2

DC2

DC2

DC2

DELETE

DELETE

DELETE

DELETE

F929−97007−000−00

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

NSA936501TA1604

312 6LJ

312 8LJ

311 7LJ

311 5LJ

Figure A-GHAAA - Sheet 01

Hookup Chart

DATE: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 84

6

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@A340

SERVICE BULLETIN

REPORTING SHEET

TITLE: LIGHTS - SERVICE AREA LIGHTING - REMOVE SERVICE AREA

LIGHTS IN SECTION 19 ACCORDING TO SFAR 88 REQUIREMENTS.

MODIFICATION No.: 201683D46730

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: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 1

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Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

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: Jan 03/12 SERVICE BULLETIN No.: A340-33-4026

REVISION No.: 01 - Jul 10/12 Page: 1

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