# @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 ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE ADAPTED DUAL LOOP OVERHEAT LEAK DETECTION APU BLEED AIR DUCT MODIFICATION No.: 55198D46290 55198D46286 55961D46493 55962D46494 58529D46961 58530D46962 This page transmits Revision No.01 of Service Bulletin No.A340-36-4033 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to: - integrate the results of the validation of the equivalent of this Service Bulletin, accomplished on A330 aircraft MSN 0389, - introduce minor changes. 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 MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET CONF 001 CONFIGURATION DEFINITION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED MATERIAL SET QUANTITY UPDATED R
MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED MATERIAL SET QUANTITY UPDATED R
MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED MATERIAL SET QUANTITY UPDATED R
MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED MATERIAL SET QUANTITY UPDATED R
MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED MATERIAL SET QUANTITY UPDATED R
MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL SET UPDATED R LIST OF COMPONENTS Kit 364033A01R02 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED PART NUMBER UPDATED R

Kit 364033D01R02 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D02R04 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D10R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 2 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Kit 364033D11R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D12R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D13R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D14R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

Kit 364033D15R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

ACCOMPLISHMENT INSTRUCTIONS TASK 364033- 831-848-001-Modification Subtask 364033-831-001-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-002-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-003-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-004-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-006-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-007-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-008-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-009-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 3 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-010-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-011-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-012-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-013-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-201-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-202-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-204-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-207-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-209-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-001-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-002-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-003-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-004-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-006-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-007-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 4 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-008-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-009-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-010-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-011-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-012-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-013-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-201-003 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-202-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-204-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-207-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-209-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-001-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-002-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-003-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-004-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 5 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-006-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-007-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-008-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-009-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-010-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-011-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-012-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-013-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-201-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-202-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-204-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-207-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-209-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-001-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-002-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 6 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-003-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-004-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-006-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-007-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-008-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-009-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-010-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-011-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-012-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-013-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-201-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-202-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-204-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-207-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-209-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 7 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-001-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-002-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-003-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-004-001 SUBTASK SOLUTION UPDATED PART NUMBER DESCRIPTION UPDATED R Subtask 364033-831-006-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-007-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-008-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-009-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-010-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-011-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-012-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED MATERIAL LIST UPDATED R
Subtask 364033-831-013-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-201-002 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-202-002 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 364033-831-204-002 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-207-003 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Subtask 364033-831-211-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 8 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Subtask 364033-831-209-003 SUBTASK SOLUTION UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED PART NUMBER DESCRIPTION UPDATED MATERIAL LIST UPDATED R

Fig. A-FBCAA Fig. A-FBCAA Sheet 01 SHEET UPDATED R Fig. A-FBCAA Sheet 02 SHEET UPDATED R Fig. A-FBNAA Fig. A-FBNAA Sheet 01 SHEET UPDATED R Fig. A-FBNAA Sheet 02 SHEET UPDATED R Fig. A-FBNAA Sheet 03 SHEET UPDATED R Fig. A-FBNAA Sheet 04 SHEET UPDATED R Fig. A-FBNAA Sheet 05 SHEET UPDATED R Fig. A-FBJAA Fig. A-FBJAA Sheet 02 SHEET UPDATED R Fig. A-FBJAA Sheet 03 SHEET UPDATED R Fig. A-FBJAA Sheet 04 SHEET UPDATED R Fig. A-FBMAA Fig. A-FBMAA Sheet 01 SHEET UPDATED R Fig. A-FBMAA Sheet 02 SHEET UPDATED R Fig. A-FBMAA Sheet 03 SHEET UPDATED R Fig. A-FBMAA Sheet 04 SHEET UPDATED R Fig. A-FBMAA Sheet 05 SHEET UPDATED R Fig. A-FBMAA Sheet 06 SHEET UPDATED R Fig. A-FBMAA Sheet 08 SHEET UPDATED R Fig. A-FBMAA Sheet 09 SHEET UPDATED R Fig. A-FBMAA Sheet 11 SHEET UPDATED R Fig. A-FBMAA Sheet 12 SHEET UPDATED R Fig. A-FBMAA Sheet 13 SHEET UPDATED R Fig. A-FBMAA Sheet 14 SHEET UPDATED R Fig. A-FBMAA Sheet 15 SHEET UPDATED R Fig. A-FBMAA Sheet 16 SHEET UPDATED R Fig. A-FBMAA Sheet 17 SHEET UPDATED R Fig. A-FBMAA Sheet 18 SHEET UPDATED R Fig. A-FBMAA Sheet 19 SHEET UPDATED R Fig. A-FBMAA Sheet 20 SHEET UPDATED R Fig. A-FBMAA Sheet 21 SHEET UPDATED R Fig. A-FBMAA Sheet 22 SHEET UPDATED R Fig. A-FAAAA FIGURE SOLUTION ADDED N DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 9 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-FAAAA Sheet 01 SHEET ADDED N Fig. A-GBDAA Fig. A-GBDAA Sheet 08 SHEET UPDATED R Fig. A-GBDAE Fig. A-GBDAE Sheet 07 SHEET UPDATED R Fig. A-GBGAA Fig. A-GBGAA Sheet 01 SHEET UPDATED R Fig. A-GBGAA Sheet 02 SHEET UPDATED R Fig. A-GBGAA Sheet 03 SHEET UPDATED R Fig. A-GBGAA Sheet 04 SHEET UPDATED R Fig. A-GBGAA Sheet 05 SHEET UPDATED R Fig. A-GBGAA Sheet 06 SHEET UPDATED R Fig. A-GBGAA Sheet 07 SHEET UPDATED R Fig. A-GBGAA Sheet 08 SHEET UPDATED R Fig. A-GBGAB Fig. A-GBGAB Sheet 01 SHEET UPDATED R Fig. A-GBGAB Sheet 02 SHEET UPDATED R Fig. A-GBGAB Sheet 03 SHEET UPDATED R Fig. A-GBGAB Sheet 04 SHEET UPDATED R Fig. A-GBGAB Sheet 05 SHEET UPDATED R Fig. A-GBGAB Sheet 06 SHEET UPDATED R Fig. A-GBGAB Sheet 07 SHEET UPDATED R Fig. A-GBGAB Sheet 08 SHEET UPDATED R Fig. A-GBGAB Sheet 09 SHEET UPDATED R Fig. A-GBGAE Fig. A-GBGAE Sheet 01 SHEET UPDATED R Fig. A-GBGAE Sheet 02 SHEET UPDATED R Fig. A-GBGAE Sheet 03 SHEET UPDATED R Fig. A-GBGAE Sheet 04 SHEET UPDATED R Fig. A-GBGAE Sheet 05 SHEET UPDATED R Fig. A-GBGAE Sheet 06 SHEET UPDATED R Fig. A-GBGAE Sheet 07 SHEET UPDATED R Fig. A-GBGAE Sheet 08 SHEET UPDATED R Fig. A-GBGAE Sheet 09 SHEET UPDATED R Fig. A-GBJAA Fig. A-GBJAA Sheet 01 SHEET UPDATED R Fig. A-GBJAA Sheet 02 SHEET UPDATED R Fig. A-GBJAA Sheet 03 SHEET UPDATED R Fig. A-GBJAA Sheet 04 SHEET UPDATED R Fig. A-GBJAA Sheet 05 SHEET UPDATED R Fig. A-GBJAA Sheet 06 SHEET UPDATED R DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 10 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Fig. A-GBJAA Sheet 07 SHEET UPDATED R Fig. A-GBJAA Sheet 08 SHEET UPDATED R Fig. A-GBJAC Fig. A-GBJAC Sheet 01 SHEET UPDATED R Fig. A-GBJAC Sheet 02 SHEET UPDATED R Fig. A-GBJAC Sheet 03 SHEET UPDATED R Fig. A-GBJAC Sheet 04 SHEET UPDATED R Fig. A-GBJAC Sheet 05 SHEET UPDATED R Fig. A-GBJAC Sheet 06 SHEET UPDATED R Fig. A-GBJAC Sheet 07 SHEET UPDATED R Fig. A-GBJAC Sheet 08 SHEET UPDATED R Fig. A-GBJAE Fig. A-GBJAE Sheet 01 SHEET UPDATED R Fig. A-GBJAE Sheet 02 SHEET UPDATED R Fig. A-GBJAE Sheet 04 SHEET UPDATED R Fig. A-GBJAE Sheet 05 SHEET UPDATED R Fig. A-GBJAE Sheet 06 SHEET UPDATED R Fig. A-GBJAE Sheet 07 SHEET UPDATED R Fig. A-GBJAE Sheet 08 SHEET 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: Sep 23/11 REVISION No. : 01 - Jan 28/13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 11 6

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 12 6

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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. ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE ADAPTED DUAL LOOP OVERHEAT LEAK DETECTION APU BLEED AIR DUCT **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None 55198D46290 55198D46286 55961D46493 55962D46494 58529D46961 MINOR 58530D46962 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 The Auxiliary Power Unit (APU) bleed leak detection system detects any ambient overheat in the vicinity of the APU bleed air ducts. This system is made of a single overheat detection loop which runs along the APU bleed air ducts in section 15/21 and sections 16 thru 19.1. The SFAR88 requirements introduced Master Minimum Equipment List(MMEL) restrictions on this system. This Service Bulletin details the installation of a second APU bleed leak detection loop (APU LOOP A) in parallel to the current APU loop (which consequently becomes APU LOOP B) in section 15/21 and sections 16 thru 19.1. After installation of the second loop, the design and philosophy ofthe APU bleed leak detection system will be similar to the wing bleed leak detection system (dual loop). This allows to dispatch the aircraft with one loop inoperative for 800 FH. The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the affected publications detailed in ’PLANNING INFORMATION’. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD NO A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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# @A340 SERVICE BULLETIN SUMMARY EVALUATION TABLE COST SAVING NO LROPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033A01R02 1 28,600.00 Sensing element Kit 364033A02R01 1 4,370.00 Bundle, Clamp, Hardware Kit364033D01R02 1 2,570.00 Electrical Equipment, Fitting, Protection System, Clamp, Spacer, Strip, Splice, Support, Placard Set, Cable Tie, Spring, Tube and Attaching Parts Kit 364033D03R00 1 106.00 Section and Attaching Parts Kit364033D10R01 1 13,750.00 Attaching Element, Sensing Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit364033D13R01 1 10,070.00 Cable, Cable Tie, Attaching Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit 364033D16R00 1 3,780.00 Sleeve TOTAL 63,246.00 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033A01R02 1 28,600.00 Sensing element Kit 364033A02R01 1 4,370.00 Bundle, Clamp, Hardware Kit364033D01R02 1 2,570.00 Electrical Equipment, Fitting, Protection System, Clamp, Spacer, Strip, Splice, Support, Placard Set, Cable Tie, Spring, Tube and Attaching Parts Kit 364033D03R00 1 106.00 Section and Attaching Parts Kit364033D11R01 1 15,540.00 Attaching Element, Sensing Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 2 6

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# @A340 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033D13R01 1 10,070.00 Cable, Cable Tie, Attaching Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit 364033D16R00 1 3,780.00 Sleeve TOTAL 65,036.00 **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033A01R02 1 28,600.00 Sensing element Kit 364033A02R01 1 4,370.00 Bundle, Clamp, Hardware Kit364033D01R02 1 2,570.00 Electrical Equipment, Fitting, Protection System, Clamp, Spacer, Strip, Splice, Support, Placard Set, Cable Tie, Spring, Tube and Attaching Parts Kit 364033D03R00 1 106.00 Section and Attaching Parts Kit364033D10R01 1 13,750.00 Attaching Element, Sensing Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit364033D14R01 1 7,790.00 Cable, Cable Tie, Attaching Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit 364033D17R00 1 3,720.00 Sleeve TOTAL 60,906.00 **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033A01R02 1 28,600.00 Sensing element Kit 364033A02R01 1 4,370.00 Bundle, Clamp, Hardware Kit364033D01R02 1 2,570.00 Electrical Equipment, Fitting, Protection System, Clamp, Spacer, Strip, Splice, Support, Placard Set, Cable Tie, Spring, Tube and Attaching Parts Kit 364033D03R00 1 106.00 Section and Attaching Parts

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 3 6

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# @A340 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033D11R01 1 15,540.00 Attaching Element, Sensing Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit364033D14R01 1 7,790.00 Cable, Cable Tie, Attaching Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit 364033D17R00 1 3,720.00 Sleeve TOTAL 62,696.00 **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit364033A01R02 1 28,600.00 Sensing element Kit 364033A02R01 1 4,370.00 Bundle, Clamp, Hardware Kit364033D02R04 1 2,660.00 Fitting, Protection System, Clamp, Spacer, Strip, Support, Spring, Cable Tie, Placard Set, Electrical Equipment and Attaching Parts Kit 364033D03R00 1 106.00 Section and Attaching Parts Kit364033D12R01 1 15,540.00 Attaching Element, Sensing Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit364033D15R01 1 8,010.00 Sensing Element, Bracket, Cable, Cable Tie, Attaching Element, Sleeve, Spacer, Angle, Connector, Clamp, Ring, Placard and Attaching Parts Kit 364033D17R00 1 3,720.00 Sleeve TOTAL 63,006.00 EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

47W 56W 83V AAW AFR AIB 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 SWR TAP THT THY UAE VCV VIR XAX The equivalent of this Service Bulletin has been validated on A330 aircraft MSN 0389. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 4 6

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# @A340 SERVICE BULLETIN SUMMARY CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A340-31-4083 Mod. No. 52306S16981 53296S18162 A340-31-4111 55981S18827 A340-36-4028 51789S17829 NOTE: Make sure that either the Flight Warning Computer (FWC) L10 (Service Bulletin No. A340-31-4083, Mod. No. 52306S16981, Mod. No. 53296S18162) or the FWC L10-1 (Service Bulletin No. A340-31-4111, Mod. No. 55981S18827 ) is embodied. REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER OIT SE 999.0063/06 OTHER O/REF SBIT-11-0009 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT YES HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 364033-831-848-001: Modification TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 002 Task 364033-831-848-001: Modification TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 003 Task 364033-831-848-001: Modification TOTAL MANHOURS 268.75 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 5 6

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# @A340 SERVICE BULLETIN SUMMARY Task 364033-831-848-001: Modification ELAPSED TIME (HOURS) 144.0 **CONF 004 Task 364033-831-848-001: Modification TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 005 Task 364033-831-848-001: Modification TOTAL MANHOURS 273.00 ELAPSED TIME (HOURS) 144.0 APPENDICES **CONF ALL Appendix 01: Elapsed Time Assumptions

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 6 6

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# @A340 SERVICE BULLETIN SUMMARY **CONF 001, 003


### B

**A** Z310 Z170 Z160 Z150

Z130 Z120 FR56

FR39.2 FR39.1 FR37

FR19

FR56 FR65 FR72
FR80 FR95

/82 FR101

800VU 

## A

**B** SECOND SENSING ELEMENT (APU LOOP B) AND ASSOCIATED WIRING

Z140

F_SB_364033_6_SAAA_01_01 SECOND SENSING ELEMENT (APU LOOP B) AND ASSOCIATED WIRING

Figure A-GSAAA - Sheet 01
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 7 6

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# @A340 SERVICE BULLETIN SUMMARY **CONF 002, 004 thru 005


### B

**A** Z310 Z170 Z160 Z150

Z130 Z120 FR56

FR39.2 FR39.1

FR19

FR56 FR65 FR72
FR80 FR95

/82 FR101

800VU 

## A

**B** Z140

FR37.4

F_SB_364033_6_SAAB_01_01 SECOND SENSING ELEMENT (APU LOOP B) AND ASSOCIATED WIRING

SECOND SENSING ELEMENT (APU LOOP B) AND ASSOCIATED WIRING

Figure A-GSAAB - Sheet 01
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 8 6

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# @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 ATA SYSTEM: 36 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE ADAPTED DUAL LOOP OVERHEAT LEAK DETECTION APU BLEED AIR DUCT MODIFICATION No.: 55198D46290 55198D46286 55961D46493 55962D46494 58529D46961 58530D46962 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 The equivalent of this Service Bulletin has been validated on A330 aircraft MSN 0389. NOTE: The intent of this modification is achieved in production on MSN 0793 and subsequent through modification Mod. No. 52260D44330. (1) Models 340-211 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 0002-0006 00090011 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 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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# @A340 SERVICE BULLETIN
0651 0668 (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 0011 0013 0015 001800190021 83V 0235023902800292 AAW 0151 AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377 0399 AIB 0332 ALK 0032 0033 0034 0367 0374 0381 ARG 0048 0063 0074 0080 0085 0093 0094 0123012601280373 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 GAF 0274 0355 GFA 021202150282 0554 HFY 0117 0133 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318 0329 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 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 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0413 0424 0430 0435 04500467 0470 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 2 6

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# @A340 SERVICE BULLETIN
OPERATOR MSN SFB 0046 SLM 0049 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 0005 0013 0015 0020 0023 0024 0025 0027 0028 0029 0032 0033 0034 0035 0041 0044 0047 0048 0049 0051 0052 0053 0056 0057 0058 0076 0078 0079 0084 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 0152 0154 0157 0158 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 002

0004 0006 0009 0011 0014 0018 0019 0021 0022 0026 0031 0038 0043 0046 0061 0063 0074 0075 0080 0081 0085 0151 0156 0159 0178 001
0196 0197 0199 0201 0202 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0225 0227 0228 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 0354 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 0545 0546 0554 0556 0559 0561 0562 004

0204 003 0544 0582 0585 0590 0598 0643 0646 0651 0668 005 (5) Configuration definition **CONF 001 Config. 001 is valid for all A340-200 aircraft given in the effectivity of this Service Bulletin without the Modification No. 44579D40539, Modification No. 48980D42587 and Modification No.55961D46493. **CONF 002 Config. 002 is valid for all A340-300 aircraft given in the effectivity of this Service Bulletin without the Modification No. 44579D40539, Modification No. 48980D42587 and Modification No.55961D46493. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 3 6

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# @A340 SERVICE BULLETIN
**CONF 003 Config. 003 is valid for all A340-200 aircraft given in the effectivity of this Service Bulletin on which the Modification No. 44579D40539 is embodied. **CONF 004 Config. 004 is valid for all A340-300 aircraft given in the effectivity of this Service Bulletin on which the Modification No. 44579D40539 is embodied. **CONF 005 Config. 005 valid for all A340-300 aircraft given in the effectivity of this Service Bulletin on which the Modification No. 44579D40539 and the Modification No. 48980D42587 are embodied. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Kit364033A01R02 1 Kit 364033A02R01 1 Kit364033D01R02 1 Kit 364033D03R00 1 Kit364033D10R01 1 Kit364033D13R01 1 Kit 364033D16R00 1 Reidentified part set REIDA01 1 Consumable CMLD01 1 Consumable CMLA01 As required **CONF 002 MATERIAL QTY PER A/C SEE NOTES Kit364033A01R02 1 Kit 364033A02R01 1 Kit364033D01R02 1 Kit 364033D03R00 1 Kit364033D11R01 1 Kit364033D13R01 1 Kit 364033D16R00 1 Reidentified part set REIDA01 1 Consumable CMLD01 1 Consumable CMLA01 As required **CONF 003 MATERIAL QTY PER A/C SEE NOTES Kit364033A01R02 1 Kit 364033A02R01 1 Kit364033D01R02 1 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 4 6

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# @A340 SERVICE BULLETIN
MATERIAL QTY PER A/C SEE NOTES Kit 364033D03R00 1 Kit364033D10R01 1 Kit364033D14R01 1 Kit 364033D17R00 1 Reidentified part set REIDA01 1 Consumable CMLD01 1 Consumable CMLA01 As required **CONF 004 MATERIAL QTY PER A/C SEE NOTES Kit364033A01R02 1 Kit 364033A02R01 1 Kit364033D01R02 1 Kit 364033D03R00 1 Kit364033D11R01 1 Kit364033D14R01 1 Kit 364033D17R00 1 Reidentified part set REIDA01 1 Consumable CMLD01 1 Consumable CMLA01 As required **CONF 005 MATERIAL QTY PER A/C SEE NOTES Kit364033A01R02 1 Kit 364033A02R01 1 Kit364033D02R04 1 Kit 364033D03R00 1 Kit364033D12R01 1 Kit364033D15R01 1 Kit 364033D17R00 1 Reidentified part set REIDA01 1 Consumable CMLD01 1 Consumable CMLA01 As required **CONF ALL B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A340-31-4083 Mod. No. 52306S16981 53296S18162 A340-31-4111 55981S18827 A340-36-4028 51789S17829 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 5 6

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# @A340 SERVICE BULLETIN
NOTE: Make sure that either the Flight Warning Computer (FWC) L10 (Service Bulletin No. A340-31-4083, Mod. No. 52306S16981, Mod. No. 53296S18162) or the FWC L10-1 (Service Bulletin No. A340-31-4111, Mod. No. 55981S18827 ) is embodied. C. REASON (1) History The Auxiliary Power Unit (APU) bleed leak detection system detects any ambient overheat in the vicinity of the APU bleed air ducts. This system is made of a single overheat detection loop which runs along the APU bleed air ducts in section 15/21 and sections 16 thru 19.1. The SFAR88 requirements introduced Master Minimum Equipment List (MMEL) restrictions on this system. (2) Objective/Action This Service Bulletin details the installation of a second APU bleed leak detection loop (APU LOOP A) in parallel to the current APU loop (which consequently becomes APU LOOP B) in section 15/21 and sections 16 thru 19.1. (3) Advantages After installation of the second loop, the design and philosophy of the APU bleed leak detection system will be similar to the wing bleed leak detection system (dual loop). This allows to dispatch the aircraft with one loop inoperative for 800 FH. (4) Operational/Maintenance Consequences The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the affected publications detailed in ’PLANNING INFORMATION’. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 364033-831-848-001: Modification (1) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (2) Modify the Wiring in the Main rack 800VU. (3) Remove the sensing elements and the supports between FR39 and FR44. (4) Remove the sensing elements and the supports between FR44 and FR51. (5) Remove the sensing elements and the supports between FR51 and FR53.6. (6) Remove the sensing elements and the supports between FR53.6 and FR55. (7) If necessary, remove the ducts between FR53.5 and FR53.6 for access. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 6 6

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# @A340 SERVICE BULLETIN (8) Drill a new hole in the structure between FR53.5 and FR53.6. (9) Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. (10) If removed, install the ducts between FR53.5 and FR53.6. (11) If necessary, remove the ducts between FR43 and FR45 for access. (12) Replace the web assy and the half clamp assy at FR44. (13) Install the new brackets for the routing of the sensing elements at FR44. (14) If removed, install the ducts between FR43 and FR45. (15) Install the sensing elements and the supports between FR39 and FR44. (16) Install the sensing elements and the supports between FR44 and FR50. (17) Install the sensing elements and the supports between FR50 and FR53.6. (18) Install the sensing elements and the supports between FR53.6 and FR55. (19) If necessary, remove the ducts between FR39 and FR40 for access. (20) Install the new supports for the new harness between FR39.1 and FR39.2. (21) Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (22) Install the new Harness 2SG. (23) Install the electrical wiring in the FWD cargo compartment (24) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment (25) Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section (26) Install an additional profile in the Rear fuselage section (27) Install the electrical wiring in the rear fuselage section (28) Remove the sensing elements in the AFT and Bulk cargo compartments (29) Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead (30) Install the sensing elements in the AFT and Bulk cargo compartments (31) If removed, install the ducts between FR39 and FR40. (32) Remove the sensing elements in the rear fuselage DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 7 6

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# @A340 SERVICE BULLETIN (33) Install the sensing elements in the rear fuselage (34) Install the sleeves at the APU Bleed Air Duct **CONF 002 Task 364033-831-848-001: Modification (1) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (2) Modify the Wiring in the Main rack 800VU. (3) Remove the sensing elements and the supports between FR39 and FR44. (4) Remove the sensing elements and the supports between FR44 and FR51. (5) Remove the sensing elements and the supports between FR51 and FR53.6. (6) Remove the sensing elements and the supports between FR53.6 and FR55. (7) If necessary, remove the ducts between FR53.5 and FR53.6 for access. (8) Drill a new hole in the structure between FR53.5 and FR53.6. (9) Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. (10) If removed, install the ducts between FR53.5 and FR53.6. (11) If necessary, remove the ducts between FR43 and FR45 for access. (12) Replace the web assy and the half clamp assy at FR44. (13) Install the new brackets for the routing of the sensing elements at FR44. (14) If removed, install the ducts between FR43 and FR45. (15) Install the sensing elements and the supports between FR39 and FR44. (16) Install the sensing elements and the supports between FR44 and FR50. (17) Install the sensing elements and the supports between FR50 and FR53.6. (18) Install the sensing elements and the supports between FR53.6 and FR55. (19) If necessary, remove the ducts between FR39 and FR40 for access. (20) Install the new supports for the new harness between FR39.1 and FR39.2. (21) Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (22) Install the new Harness 2SG. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 8 6

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# @A340 SERVICE BULLETIN (23) Install the electrical wiring in the FWD cargo compartment (24) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment (25) Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section (26) Install an additional profile in the Rear fuselage section (27) Install the electrical wiring in the rear fuselage section (28) Remove the sensing elements in the AFT and Bulk cargo compartments (29) Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead (30) Install the sensing elements in the AFT and Bulk cargo compartments (31) If removed, install the ducts between FR39 and FR40. (32) Remove the sensing elements in the rear fuselage (33) Install the sensing elements in the rear fuselage (34) Install the sleeves at the APU Bleed Air Duct **CONF 003 Task 364033-831-848-001: Modification (1) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (2) Modify the Wiring in the Main rack 800VU. (3) Remove the sensing elements and the supports between FR39 and FR44. (4) Remove the sensing elements and the supports between FR44 and FR51. (5) Remove the sensing elements and the supports between FR51 and FR53.6. (6) Remove the sensing elements and the supports between FR53.6 and FR55. (7) If necessary, remove the ducts between FR53.5 and FR53.6 for access. (8) Drill a new hole in the structure between FR53.5 and FR53.6. (9) Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. (10) If removed, install the ducts between FR53.5 and FR53.6. (11) If necessary, remove the ducts between FR43 and FR45 for access. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 9 6

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# @A340 SERVICE BULLETIN (12) Replace the web assy and the half clamp assy at FR44. (13) Install the new brackets for the routing of the sensing elements at FR44. (14) If removed, install the ducts between FR43 and FR45. (15) Install the sensing elements and the supports between FR39 and FR44. (16) Install the sensing elements and the supports between FR44 and FR50. (17) Install the sensing elements and the supports between FR50 and FR53.6. (18) Install the sensing elements and the supports between FR53.6 and FR55. (19) If necessary, remove the ducts between FR39 and FR40 for access. (20) Install the new supports for the new harness between FR39.1 and FR39.2. (21) Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (22) Install the new Harness 2SG. (23) Install the electrical wiring in the FWD cargo compartment (24) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment (25) Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section (26) Install an additional profile in the Rear fuselage section (27) Install the electrical wiring in the rear fuselage section (28) Remove the sensing elements in the AFT and Bulk cargo compartments (29) Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead (30) Install the sensing elements in the AFT and Bulk cargo compartments (31) If removed, install the ducts between FR39 and FR40. (32) Remove the sensing elements in the rear fuselage (33) Install the sensing elements in the rear fuselage (34) Install the sleeves at the APU Bleed Air Duct

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 10 6

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# @A340 SERVICE BULLETIN
**CONF 004 Task 364033-831-848-001: Modification (1) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (2) Modify the Wiring in the Main rack 800VU. (3) Remove the sensing elements and the supports between FR39 and FR44. (4) Remove the sensing elements and the supports between FR44 and FR51. (5) Remove the sensing elements and the supports between FR51 and FR53.6. (6) Remove the sensing elements and the supports between FR53.6 and FR55. (7) If necessary, remove the ducts between FR53.5 and FR53.6 for access. (8) Drill a new hole in the structure between FR53.5 and FR53.6. (9) Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. (10) If removed, install the ducts between FR53.5 and FR53.6. (11) If necessary, remove the ducts between FR43 and FR45 for access. (12) Replace the web assy and the half clamp assy at FR44. (13) Install the new brackets for the routing of the sensing elements at FR44. (14) If removed, install the ducts between FR43 and FR45. (15) Install the sensing elements and the supports between FR39 and FR44. (16) Install the sensing elements and the supports between FR44 and FR50. (17) Install the sensing elements and the supports between FR50 and FR53.6. (18) Install the sensing elements and the supports between FR53.6 and FR55. (19) If necessary, remove the ducts between FR39 and FR40 for access. (20) Install the new supports for the new harness between FR39.1 and FR39.2. (21) Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (22) Install the new Harness 2SG. (23) Install the electrical wiring in the FWD cargo compartment (24) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 11 6

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# @A340 SERVICE BULLETIN (25) Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section (26) Install an additional profile in the Rear fuselage section (27) Install the electrical wiring in the rear fuselage section (28) Remove the sensing elements in the AFT and Bulk cargo compartments (29) Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead (30) Install the sensing elements in the AFT and Bulk cargo compartments (31) If removed, install the ducts between FR39 and FR40. (32) Remove the sensing elements in the rear fuselage (33) Install the sensing elements in the rear fuselage (34) Install the sleeves at the APU Bleed Air Duct **CONF 005 Task 364033-831-848-001: Modification (1) Modify the Wiring between the Avionics Compartment and the Cargo Compartment. (2) Modify the Wiring in the Main rack 800VU. (3) Remove the sensing elements and the supports between FR39 and FR44. (4) Remove the sensing elements and the supports between FR44 and FR51. (5) Remove the sensing elements and the supports between FR51 and FR53.6. (6) Remove the sensing elements and the supports between FR53.6 and FR55. (7) If necessary, remove the ducts between FR53.5 and FR53.6 for access. (8) Drill a new hole in the structure between FR53.5 and FR53.6. (9) Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. (10) If removed, install the ducts between FR53.5 and FR53.6. (11) If necessary, remove the ducts between FR43 and FR45 for access. (12) Replace the web assy and the half clamp assy at FR44. (13) Install the new brackets for the routing of the sensing elements at FR44. (14) If removed, install the ducts between FR43 and FR45. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 12 6

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# @A340 SERVICE BULLETIN (15) Install the sensing elements and the supports between FR39 and FR44. (16) Install the sensing elements and the supports between FR44 and FR50. (17) Install the sensing elements and the supports between FR50 and FR53.6. (18) Install the sensing elements and the supports between FR53.6 and FR55. (19) If necessary, remove the ducts between FR39 and FR40 for access. (20) Install the new supports for the new harness between FR39.1 and FR39.2. (21) Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. (22) Install the new Harness 2SG. (23) Install the electrical wiring in the FWD cargo compartment (24) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment (25) Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section (26) Install an additional profile in the Rear fuselage section (27) Install the electrical wiring in the rear fuselage section (28) Remove the sensing elements in the AFT and Bulk cargo compartments (29) Drill an additional hole for the dual loop overheat leak detection in the CFK pressure bulkhead (30) Install the sensing elements in the AFT and Bulk cargo compartments (31) If removed, install the ducts between FR39 and FR40. (32) Remove the sensing elements in the rear fuselage (33) Remove the sensing element, FIN 149HF, previously installed with Service Bulletin No. A340-36-4028 (34) Install the sensing elements in the rear fuselage (35) Install the sleeves at the APU Bleed Air Duct

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 13 6

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# @A340 SERVICE BULLETIN
**CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL 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 364033-831-848-001: Modification Get Access 27.75 On Aircraft Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 2.00 Modify the Wiring in the Main rack 800VU. 4.00 Remove the sensing elements and the supports between FR39 and FR44. 4.00 Remove the sensing elements and the supports between FR44 and FR51. 4.00 Remove the sensing elements and the supports between FR51 and FR53.6. 4.00 Remove the sensing elements and the supports between FR53.6 and FR55. 4.00 If necessary, remove the ducts between FR53.5 and FR53.6 for access. 1.00
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 14 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Drill a new hole in the structure between FR53.5 and FR53.6. 1.00 Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. 1.00 If removed, install the ducts between FR53.5 and FR53.6. 2.00 If necessary, remove the ducts between FR43 and FR45 for access. 1.00 Replace the web assy and the half clamp assy at FR44. 3.00 Install the new brackets for the routing of the sensing elements at FR44. 1.00 If removed, install the ducts between FR43 and FR45. 2.00 Install the sensing elements and the supports between FR39 and FR44. 14.00 Install the sensing elements and the supports between FR44 and FR50. 14.00 Install the sensing elements and the supports between FR50 and FR53.6. 21.00 Install the sensing elements and the supports between FR53.6 and FR55. 14.00 If necessary, remove the ducts between FR39 and FR40 for access. 1.00 Install the new supports for the new harness between FR39.1 and FR39.2. 3.00 Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Install the new Harness 2SG. 26.00 Install the electrical wiring in the FWD cargo compartment 7.50 Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 11.00 Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section 4.50 Install an additional profile in the Rear fuselage section 3.00 Install the electrical wiring in the rear fuselage section 14.00 Remove the sensing elements in the AFT and Bulk cargo compartments 5.25 Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead 0.75 Install the sensing elements in the AFT and Bulk cargo compartments 11.25 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sensing elements in the rear fuselage 2.75 Install the sensing elements in the rear fuselage 5.75 Install the sleeves at the APU Bleed Air Duct 0.50 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 15 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Tests 5.00 Close-Up 37.75 TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 002 Task 364033-831-848-001: Modification Get Access 27.75 On Aircraft Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 2.00 Modify the Wiring in the Main rack 800VU. 4.00 Remove the sensing elements and the supports between FR39 and FR44. 4.00 Remove the sensing elements and the supports between FR44 and FR51. 4.00 Remove the sensing elements and the supports between FR51 and FR53.6. 4.00 Remove the sensing elements and the supports between FR53.6 and FR55. 4.00 If necessary, remove the ducts between FR53.5 and FR53.6 for access. 1.00 Drill a new hole in the structure between FR53.5 and FR53.6. 1.00 Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. 1.00 If removed, install the ducts between FR53.5 and FR53.6. 2.00 If necessary, remove the ducts between FR43 and FR45 for access. 1.00 Replace the web assy and the half clamp assy at FR44. 3.00 Install the new brackets for the routing of the sensing elements at FR44. 1.00 If removed, install the ducts between FR43 and FR45. 2.00 Install the sensing elements and the supports between FR39 and FR44. 14.00 Install the sensing elements and the supports between FR44 and FR50. 14.00 Install the sensing elements and the supports between FR50 and FR53.6. 21.00 Install the sensing elements and the supports between FR53.6 and FR55. 14.00 If necessary, remove the ducts between FR39 and FR40 for access. 1.00 Install the new supports for the new harness between FR39.1 and FR39.2. 3.00 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 16 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Install the new Harness 2SG. 26.00 Install the electrical wiring in the FWD cargo compartment 7.50 Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 11.00 Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section 4.50 Install an additional profile in the Rear fuselage section 3.00 Install the electrical wiring in the rear fuselage section 14.00 Remove the sensing elements in the AFT and Bulk cargo compartments 5.25 Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead 0.75 Install the sensing elements in the AFT and Bulk cargo compartments 11.25 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sensing elements in the rear fuselage 2.75 Install the sensing elements in the rear fuselage 5.75 Install the sleeves at the APU Bleed Air Duct 0.50 Tests 5.00 Close-Up 37.75 TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 003 Task 364033-831-848-001: Modification Get Access 27.75 On Aircraft Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 2.00 Modify the Wiring in the Main rack 800VU. 4.00 Remove the sensing elements and the supports between FR39 and FR44. 4.00 Remove the sensing elements and the supports between FR44 and FR51. 4.00 Remove the sensing elements and the supports between FR51 and FR53.6. 4.00 Remove the sensing elements and the supports between FR53.6 and FR55. 4.00 If necessary, remove the ducts between FR53.5 and FR53.6 for access. 1.00
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 17 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Drill a new hole in the structure between FR53.5 and FR53.6. 1.00 Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. 1.00 If removed, install the ducts between FR53.5 and FR53.6. 2.00 If necessary, remove the ducts between FR43 and FR45 for access. 1.00 Replace the web assy and the half clamp assy at FR44. 3.00 Install the new brackets for the routing of the sensing elements at FR44. 1.00 If removed, install the ducts between FR43 and FR45. 2.00 Install the sensing elements and the supports between FR39 and FR44. 14.00 Install the sensing elements and the supports between FR44 and FR50. 14.00 Install the sensing elements and the supports between FR50 and FR53.6. 21.00 Install the sensing elements and the supports between FR53.6 and FR55. 14.00 If necessary, remove the ducts between FR39 and FR40 for access. 1.00 Install the new supports for the new harness between FR39.1 and FR39.2. 3.00 Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Install the new Harness 2SG. 26.00 Install the electrical wiring in the FWD cargo compartment 7.50 Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 11.00 Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section 4.50 Install an additional profile in the Rear fuselage section 3.00 Install the electrical wiring in the rear fuselage section 14.00 Remove the sensing elements in the AFT and Bulk cargo compartments 5.25 Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead 0.75 Install the sensing elements in the AFT and Bulk cargo compartments 11.25 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sensing elements in the rear fuselage 2.75 Install the sensing elements in the rear fuselage 5.75 Install the sleeves at the APU Bleed Air Duct 0.50 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 18 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Tests 5.00 Close-Up 37.75 TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 004 Task 364033-831-848-001: Modification Get Access 27.75 On Aircraft Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 2.00 Modify the Wiring in the Main rack 800VU. 4.00 Remove the sensing elements and the supports between FR39 and FR44. 4.00 Remove the sensing elements and the supports between FR44 and FR51. 4.00 Remove the sensing elements and the supports between FR51 and FR53.6. 4.00 Remove the sensing elements and the supports between FR53.6 and FR55. 4.00 If necessary, remove the ducts between FR53.5 and FR53.6 for access. 1.00 Drill a new hole in the structure between FR53.5 and FR53.6. 1.00 Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. 1.00 If removed, install the ducts between FR53.5 and FR53.6. 2.00 If necessary, remove the ducts between FR43 and FR45 for access. 1.00 Replace the web assy and the half clamp assy at FR44. 3.00 Install the new brackets for the routing of the sensing elements at FR44. 1.00 If removed, install the ducts between FR43 and FR45. 2.00 Install the sensing elements and the supports between FR39 and FR44. 14.00 Install the sensing elements and the supports between FR44 and FR50. 14.00 Install the sensing elements and the supports between FR50 and FR53.6. 21.00 Install the sensing elements and the supports between FR53.6 and FR55. 14.00 If necessary, remove the ducts between FR39 and FR40 for access. 1.00 Install the new supports for the new harness between FR39.1 and FR39.2. 3.00 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 19 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Install the new Harness 2SG. 26.00 Install the electrical wiring in the FWD cargo compartment 7.50 Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 11.00 Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section 4.50 Install an additional profile in the Rear fuselage section 3.00 Install the electrical wiring in the rear fuselage section 14.00 Remove the sensing elements in the AFT and Bulk cargo compartments 5.25 Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead 0.75 Install the sensing elements in the AFT and Bulk cargo compartments 11.25 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sensing elements in the rear fuselage 2.75 Install the sensing elements in the rear fuselage 5.75 Install the sleeves at the APU Bleed Air Duct 0.50 Tests 5.00 Close-Up 37.75 TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 005 Task 364033-831-848-001: Modification Get Access 27.75 On Aircraft Modify the Wiring between the Avionics Compartment and the Cargo Compartment. 2.00 Modify the Wiring in the Main rack 800VU. 4.00 Remove the sensing elements and the supports between FR39 and FR44. 4.00 Remove the sensing elements and the supports between FR44 and FR51. 4.00 Remove the sensing elements and the supports between FR51 and FR53.6. 4.00 Remove the sensing elements and the supports between FR53.6 and FR55. 4.00 If necessary, remove the ducts between FR53.5 and FR53.6 for access. 1.00
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 20 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Drill a new hole in the structure between FR53.5 and FR53.6. 1.00 Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. 1.00 If removed, install the ducts between FR53.5 and FR53.6. 2.00 If necessary, remove the ducts between FR43 and FR45 for access. 1.00 Replace the web assy and the half clamp assy at FR44. 3.00 Install the new brackets for the routing of the sensing elements at FR44. 1.00 If removed, install the ducts between FR43 and FR45. 2.00 Install the sensing elements and the supports between FR39 and FR44. 14.00 Install the sensing elements and the supports between FR44 and FR50. 14.00 Install the sensing elements and the supports between FR50 and FR53.6. 21.00 Install the sensing elements and the supports between FR53.6 and FR55. 14.00 If necessary, remove the ducts between FR39 and FR40 for access. 1.00 Install the new supports for the new harness between FR39.1 and FR39.2. 3.00 Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. 3.00 Install the new Harness 2SG. 26.00 Install the electrical wiring in the FWD cargo compartment 7.50 Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 11.00 Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section 4.50 Install an additional profile in the Rear fuselage section 3.00 Install the electrical wiring in the rear fuselage section 14.00 Remove the sensing elements in the AFT and Bulk cargo compartments 5.25 Drill an additional hole for the dual loop overheat leak detection in the CFK pressure bulkhead 0.75 Install the sensing elements in the AFT and Bulk cargo compartments 11.25 If removed, install the ducts between FR39 and FR40. 2.00 Remove the sensing elements in the rear fuselage 2.75 Remove the sensing element, FIN 149HF, previously installed with Service Bulletin No. A340-36-4028 4.25 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 21 6

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# @A340 SERVICE BULLETIN
Task 364033-831-848-001: Modification Install the sensing elements in the rear fuselage 5.75 Install the sleeves at the APU Bleed Air Duct 0.50 Tests 5.00 Close-Up 37.75 TOTAL MANHOURS 273.00 ELAPSED TIME (HOURS) 144.0 **CONF ALL H. WEIGHT AND BALANCE **CONF 001 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. Manufacturers Empty Weight +8.315 KG (+18.3312 LB) Effect on Balance +425.254 KGM (+3075.862 LB.FT ) **CONF 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. Manufacturers Empty Weight +8.470 KG (+18.6729 LB) Effect on Balance +461.230 KGM (+3336.076 LB.FT ) **CONF 003 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. Manufacturers Empty Weight +6.722 KG (+14.8193 LB) Effect on Balance +331.166 KGM (+2395.323 LB.FT ) **CONF 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. Manufacturers Empty Weight +6.877 KG (+15.1610 LB) Effect on Balance +360.343 KGM (+2606.360 LB.FT )

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 22 6

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# @A340 SERVICE BULLETIN
**CONF 005 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. Manufacturers Empty Weight +7.027 KG (+15.4917 LB) Effect on Balance +369.588 KGM (+2673.230 LB.FT ) **CONF ALL I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-21-41 25-28-41 25-52-00 25-53-00 25-54-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-33-00 52-52-00 53-00-00 53-35-11 53-35-13 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-10 20-42-12 20-43-10 20-43-42 20-48-00 20-52-10 20-55-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-42-11 51-42-21 51-43-00 51-47-00 51-75-12 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 23 6

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# @A340 SERVICE BULLETIN
**CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-21-41 25-28-41 25-52-00 25-53-00 25-54-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-33-00 52-52-00 53-00-00 53-35-11 53-35-13 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-10 20-42-12 20-43-10 20-43-42 20-48-00 20-52-10 20-55-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-42-11 51-42-21 51-43-00 51-47-00 51-75-12 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 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-21-41 25-28-41 25-52-00 25-53-00 25-54-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-33-00 52-52-00 53-00-00 53-35-11 53-35-13 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-10 20-42-12 20-43-10 20-43-42 20-48-00 20-52-10 20-55-00
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 24 6

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# @A340 SERVICE BULLETIN Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-42-11 51-42-21 51-43-00 51-47-00 51-75-12 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 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-21-41 25-28-41 25-52-00 25-53-00 25-54-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-33-00 52-52-00 53-00-00 53-35-11 53-35-13 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-10 20-42-12 20-43-10 20-43-42 20-48-00 20-52-10 20-55-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-42-11 51-42-21 51-43-00 51-47-00 51-75-12 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 25 6

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# @A340 SERVICE BULLETIN
**CONF 005 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 11-00-00 12-34-24 20-21-15 21-20-00 21-26-00 22-96-00 22-97-00 24-41-00 25-21-41 25-28-41 25-52-00 25-53-00 25-54-00 25-75-41 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 36-11-34 36-12-00 36-12-41 36-22-00 36-22-17 52-10-00 52-30-00 52-33-00 52-52-00 53-00-00 53-35-11 53-35-13 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-10 20-42-12 20-43-10 20-43-42 20-48-00 20-52-10 20-55-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-42-11 51-42-21 51-43-00 51-47-00 51-75-12 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 **CONF ALL K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 36-12-00 36-22-00 36-22-17 Aircraft Schematic Manual (ASM) 36-22-00 Aircraft Wiring List (AWL) Aircraft Wiring Manual (AWM) 36-12-04 36-22-05 91-03-06 91-03-07 Illustrated Parts Catalog (IPC) 24-92-02 24-92-04 24-92-32 25-14-01 25-71-01 25-92-31 36-12-04 36-22-03 36-22-04 53-36-03 Minimum Equipment List (MMEL) Trouble Shooting Manual (TSM) 36-22-00 This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in advance, in case you need your operational documentation to be amended by a revision priorto Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 26 6

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# @A340 SERVICE BULLETIN
SEDOR4 - AIRBUS Customer Services Technical Data Fax No.: (33) 5 61 93 28 06 E-mail: sb.reporting@airbus.com SB Reporting service is accessible on-line through AIRBUSWorld from: - My on-line services’ section, available on all AIRBUSWorld pages - The Maintenance & Engineering Community, in: . Modify and Upgrade page . Access SB and VSB section. These amendments will be confirmed by the next normal revision of operational documentation, once your Service Bulletin accomplishment report has been sent, as usual, to our Customer Services Aircraft In-Service Data (SEDOR4). L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35605-2-255 35597-2-255 03 Not Applicable Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35624-2-255 35620-2-255 03 Not Applicable Sensing element 35612-2-255 35618-2-255 03 Not Applicable Sensing element 35600-2-255 35595-2-255 03 Not Applicable Sensing element 35571-2-255 35568-4-255 03 Not Applicable Sensing element 35580-2-255 35597-3-255 03 Not Applicable Sensing element 35611-3-255 35627-2-255 03 Not Applicable Blanket-Insulation F2581571700000 F0041196200000 03 Not Applicable Blanket-Insulation F2582261900000 F0041196200000 03 Not Applicable Blanket-Insulation F2581566600000 F0041196300000 03 Not Applicable Blanket-Insulation F2581666600000 F0041196400000 03 Not Applicable
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 27 6

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# @A340 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable Blanket-Insulation F2582242300000 F0041196700000 03 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35605-2-255 35597-2-255 03 Not Applicable Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35624-2-255 35620-2-255 03 Not Applicable Sensing element 35612-2-255 35618-2-255 03 Not Applicable Sensing element 35600-2-255 35595-2-255 03 Not Applicable Sensing element 35571-2-255 35568-4-255 03 Not Applicable Sensing element 35580-2-255 35597-3-255 03 Not Applicable Sensing element 35611-3-255 35627-2-255 03 Not Applicable Blanket-Insulation F2581571700000 F0041196200000 03 Not Applicable Blanket-Insulation F2582261900000 F0041196200000 03 Not Applicable Blanket-Insulation F2581566600000 F0041196300000 03 Not Applicable Blanket-Insulation F2581666600000 F0041196400000 03 Not Applicable Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable Blanket-Insulation F2582242300000 F0041196700000 03 Not Applicable
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 28 6

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# @A340 SERVICE BULLETIN
NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF 003 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35605-2-255 35597-2-255 03 Not Applicable Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35624-2-255 35620-2-255 03 Not Applicable Sensing element 35612-2-255 35618-2-255 03 Not Applicable Sensing element 35600-2-255 35595-2-255 03 Not Applicable Sensing element 35571-2-255 35568-4-255 03 Not Applicable Sensing element 35580-2-255 35597-3-255 03 Not Applicable Sensing element 35611-3-255 35627-2-255 03 Not Applicable Blanket-Insulation F2581571700000 F0041196200000 03 Not Applicable Blanket-Insulation F2582261900000 F0041196200000 03 Not Applicable Blanket-Insulation F2581566600000 F0041196300000 03 Not Applicable Blanket-Insulation F2581666600000 F0041196400000 03 Not Applicable Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable Blanket-Insulation F2582242300000 F0041196700000 03 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF 004 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35605-2-255 35597-2-255 03 Not Applicable
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 29 6

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# @A340 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35624-2-255 35620-2-255 03 Not Applicable Sensing element 35612-2-255 35618-2-255 03 Not Applicable Sensing element 35600-2-255 35595-2-255 03 Not Applicable Sensing element 35571-2-255 35568-4-255 03 Not Applicable Sensing element 35580-2-255 35597-3-255 03 Not Applicable Sensing element 35611-3-255 35627-2-255 03 Not Applicable Blanket-Insulation F2581571700000 F0041196200000 03 Not Applicable Blanket-Insulation F2582261900000 F0041196200000 03 Not Applicable Blanket-Insulation F2581566600000 F0041196300000 03 Not Applicable Blanket-Insulation F2581666600000 F0041196400000 03 Not Applicable Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable Blanket-Insulation F2582242300000 F0041196700000 03 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF 005 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35605-2-255 35597-2-255 03 Not Applicable Sensing element 35610-2-255 35606-2-255 03 Not Applicable Sensing element 35624-2-255 35620-2-255 03 Not Applicable Sensing element 35612-2-255 35618-2-255 03 Not Applicable
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 30 6

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# @A340 SERVICE BULLETIN
DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES Sensing element 35600-2-255 35595-2-255 03 Not Applicable Sensing element 35571-2-255 35568-4-255 03 Not Applicable Sensing element 35580-2-255 35597-3-255 03 Not Applicable Sensing element 35611-3-255 35627-2-255 03 Not Applicable Blanket-Insulation F2581571700000 F0041196200000 03 Not Applicable Blanket-Insulation F2582261900000 F0041196200000 03 Not Applicable Blanket-Insulation F2581566600000 F0041196300000 03 Not Applicable Blanket-Insulation F2581666600000 F0041196400000 03 Not Applicable Blanket-Insulation F2581677800000 F0041196500000 03 Not Applicable Blanket-Insulation F2581677900000 F0041196600000 03 Not Applicable Blanket-Insulation F2582242300000 F0041196700000 03 Not Applicable NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **CONF ALL M. SPARES None

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 31 6

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# @A340 SERVICE BULLETIN

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DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 32 6

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# @A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit364033A01R02 Kit 364033A02R01 Kit364033D01R02 Kit364033D02R04 Kit 364033D03R00 Kit364033D10R01 Kit364033D11R01 Kit364033D12R01 Kit364033D13R01 Kit364033D14R01 Kit364033D15R01 Kit 364033D16R00 Kit 364033D17R00 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

Kit364033A01R02 Cost 28,600.00 USD Availability 90 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. Kit 364033A02R01 Cost 4,370.00 USD Availability 90 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. Kit364033D01R02 Cost 2,570.00 USD Availability 90 calendar days from receipt of order
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 33 6

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# @A340 SERVICE BULLETIN 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. Kit364033D02R04 Cost 2,660.00 USD Availability 90 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. Kit 364033D03R00 Cost 106.00 USD Availability 90 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. Kit364033D10R01 Cost 13,750.00 USD Availability 90 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. Kit364033D11R01 Cost 15,540.00 USD Availability 90 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.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 34 6

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# @A340 SERVICE BULLETIN
Kit364033D12R01 Cost 15,540.00 USD Availability 90 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. Kit364033D13R01 Cost 10,070.00 USD Availability 90 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. Kit364033D14R01 Cost 7,790.00 USD Availability 90 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. Kit364033D15R01 Cost 8,010.00 USD Availability 90 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. Kit 364033D16R00 Cost 3,780.00 USD Availability 90 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. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 35 6

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# @A340 SERVICE BULLETIN The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. Kit 364033D17R00 Cost 3,720.00 USD Availability 90 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. B. INDUSTRY SUPPORT INFORMATION As a special policy applied to this Service Bulletin, AIRBUS will provide a 15% reduction to the applicable kits sales prices given in the paragraph Price and Availability for orders placed before 31st December 2017. C. LIST OF COMPONENTS Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 10 NSA5543-00 123 CLAMP 11 ASNA0342T04-01 16 BOLT 13 NSA5539S 249 SLEEVE 14 ASNA2397-10L 152 WASHER 15 NSA5542-00 20 NUT 16 NSA5527-03-01 41 SPACER 17 NSA5527-03-10 3 SPACER 18 NSA5527-03-11 15 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 73 BOLT 21 NAS6603-9 34 BOLT 22 NSA5527-03-15 1 SPACER 23 NAS6603-16 1 BOLT 24 NAS6603-15 7 BOLT 25 NSA5545-00 1 ANGLE 26 NAS6603-32 3 BOLT 28 NAS6603-12 1 BOLT 29 NAS6603-2 22 BOLT 30 NSA5546-00 7 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 2 PLACARD 35 F1131031623800 2 PLACARD 36 F1131031623900 2 PLACARD DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 36 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 2 PLACARD 41 F1131031624100 2 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 70 F3611548300000 3 SUPPORT 71 F3611548800000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 9 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 18 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT 100 35606-2-255 1 SNSGELEM (1) 35610-2-255 03 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM (2) 35624-2-255 03 103 35618-2-255 2 SNSGELEM (3) 35612-2-255 03 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 37 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 104 35567-3-255 1 SNSGELEM 105 35598-2-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM (6) 35600-2-255 03 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM (7) 35571-2-255 03 109 35597-3-255 1 SNSGELEM (8) 35580-2-255 03 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM (9) 35611-3-255 03 112 35625-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM (4) 35605-2-255 03 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. 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 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 14 ASNA2397-10L 5 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 2 SPACER 22 NSA5527-03-15 1 SPACER 92 NSA57304-643ADL 1 PLATE 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 155 NSA5516-04ND 1 CLAMP 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 38 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 358 TIE 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 2 CABLE 175 35301-75 2 CABLE 35301-74 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 182 NSA5050-4 1 NUT 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F1131031522100 1 PLACARD F9000095227895 1 BUNDLE F9100095005595 1 PLACARD NSA935401-06 50 TIE NSA935401-08 300 TIE NSA935401-13 350 TIE 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 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 8 PLCRDSET 404 NSA935401-03 300 TIE DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 39 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 405 NSA935401-04 300 TIE 406 NSA935401-05 250 TIE 407 NSA935401-10 200 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 24 WASHER 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 10 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 (ME) TUBING 480 NSA937210MB0300 0.1 (ME) TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.1 (ME) TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 (ME) TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 40 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 843 MS21919WCH12 1 CLAMP 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 364033D02R04 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 401 F9297000500200 1 EQUIPMNT 402 F9237000207400 9 PLCRDSET 404 NSA935401-03 300 TIE 405 NSA935401-04 300 TIE 406 NSA935401-05 250 TIE 407 NSA935401-10 200 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 32 WASHER 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 18 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW 426 NAS6703U4 6 BOLT 427 NAS6703U5 2 BOLT 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 41 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 479 E0718-01 0.12 (ME) TUBING 480 NSA937210MB0300 0.2 (ME) TUBING 481 NSA936809RG0001 4 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.1 (ME) TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 (ME) TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP 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 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER 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 364033D10R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 42 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 6 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 152 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 12 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW 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 364033D11R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 358 35587-2-255 2 SNSGELEM 389 F3627011520000 1 PLACARD 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 43 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 591 F3627011520600 1 PLACARD 592 NSA5546-00 7 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 176 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 14 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW 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 364033D12R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 27 CLAMP 358 35587-2-255 2 SNSGELEM 389 F3627011520000 1 PLACARD 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 7 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 176 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 44 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 607 NAS1919C04S02U 14 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW 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 364033D13R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 40 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 364 35566-2-310 2 ELEMENT 366 35624-2-310 2 ELEMENT 371 35661-2-310 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 398 35659-3-310 1 ELEMENT 405 NSA935401-04 2 TIE 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 2 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 104 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 4 SPACER 610 NSA5538-00 4 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 45 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 805 NAS1802-3-13 2 SCREW 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 364033D14R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 314 NAS1801-3-8 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 37 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 362 35563-2-255 1 ELEMENT 363 35566-2-255 1 ELEMENT 365 35616-2-255 2 ELEMENT 369 35641-3-255 1 ELEMENT 370 35642-2-255 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 397 NSA5527-03-04 2 SPACER 405 NSA935401-04 TIE 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 1 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 94 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 3 SPACER 610 NSA5538-00 2 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 46 6

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# @A340 SERVICE BULLETIN
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 364033D15R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 314 NAS1801-3-8 5 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 38 CLAMP 359 F3627014700200 1 BRACKET 360 35301-74 1 CABLE 361 35301-75 1 CABLE 362 35563-2-255 1 ELEMENT 363 35566-2-255 1 ELEMENT 365 35616-2-255 2 ELEMENT 367 35637-3-255 1 ELEMENT 368 35640-2-255 1 SNSGELEM 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 396 NAS1149F0332P 5 WASHER 397 NSA5527-03-04 2 SPACER 405 NSA935401-04 TIE 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 92 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 3 SPACER 610 NSA5538-00 2 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 47 6

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# @A340 SERVICE BULLETIN
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 364033D16R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 375 F3617062400000 1 SLEEVE 376 F3617062400200 1 SLEEVE 377 F3617062400400 1 SLEEVE 378 F3617062400600 1 SLEEVE 379 F3617062400800 1 SLEEVE 380 F3617062401000 1 SLEEVE 381 F3617062401200 1 SLEEVE 382 F3617062401400 1 SLEEVE 384 F3617062401800 1 SLEEVE Kit 364033D17R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 377 F3617062400400 1 SLEEVE 380 F3617062401600 1 SLEEVE 382 F3617062402200 1 SLEEVE 383 F3617062403200 1 SLEEVE 384 F3617062403400 1 SLEEVE 385 F3617062403600 1 SLEEVE 386 F3617062403800 1 SLEEVE 387 F3617062404000 1 SLEEVE 602 NSA5539S 6 SLEEVE 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 CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Brush Consistency 09-013B 0 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 48 6

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# @A340 SERVICE BULLETIN
ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required Solvent General Purpose 11-026 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required External Top Coat (polyurethane) 16-018 As required Lint-Free Cotton Cloth 19-003 As required Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibitive interfay Sealant 09-005 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Corrosion Preventive Temporary Protective Compound 15-005 As required Corrosion Preventive Temporary Protective Compound 15-007 As required Corrosion Preventive Temporary Protective Compound 15-009 As required Anti-Corrosion Primer (polyurethane) 16-001 As requiredAnti-Corrosion Primer (EpoxyImproved Adhesion) 16-006 As required External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required Lockwire 0.6 Mm 19-018 As required (2) Components None DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 49 6

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# @A340 SERVICE BULLETIN (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 F. TOOLING (1) Tooling - Price and Availability None (2) Tools To accomplish this Service Bulletin it is necessary to use the tools listed in AMM 52-30-00, Page Block 201. (3) Special Tools None

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 50 6

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 364033-831-848-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: YOU MUST MAKE SURE THAT THE LANDING GEAR GROUND SAFETY LOCKS ARE INSTALLED AND THE WHEEL CHOCKS ARE IN POSITION. WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE 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. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM. AUTOMATIC MOVEMENT OF THE FLIGHT CONTROL SURFACES CAN BE DANGEROUS AND/OR CAUSE DAMAGE. WARNING: CLEANING SOLVENTS ARE FLAMMABLE, VOLATILE, TOXIC. THEY SHOULD BE USED WITH ADEQUATE VENTILATION. AVOID PROLONGED BREATHING OF VAPORS AND REPEATED OR PROLONGED CONTACT WITH THE SKIN, OR CLOTHING. WARNING: USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS ONLY WITH A GOOD SUPPLY OF AIR THROUGH THE WORK AREA. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. CAUTION: MAKE SURE THAT THE MAINTENANCE DEVICES OF THE WING TIP BRAKES ARE IN THE ’O’ (OPERATION) POSITION. THIS PREVENTS THE MOVEMENT OF THE FLAP/SLAT TRANSMISSION SYSTEM DURING MAINTENANCE. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 51 6

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# @A340 SERVICE BULLETIN
CAUTION: MAKE SURE THAT THE CLEANING AGENTS OR SOLVENTS DO NOT GET IN OR ON: - COMPONENT PARTS - PROTECTIVE COVERS - ELECTRICAL WIRING AND CONNECTORS. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION (REFER TO ESPM 20-55-00). Task Associated Data **CONF 001 Zone 120 130 150 160 190 310 From 150 to 170 From 160 to 310 Modified FIN 23HF 24HF 25HF 27HF 28HF 29HF 30HF 31HF 32HF 33HF 34HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 139HF 140HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 358HF 359HF 360HF 361HF 5865VB 5866VB 5886VB 5215VC 5208VP 3503VS 3591VS 3593VS 5151VSA 5410VS Access Door 313AL 821 822 831 Manpower TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 52 6

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# @A340 SERVICE BULLETIN
**CONF 002 Zone 120 130 150 160 190 310 From 150 to 170 From 160 to 310 Modified FIN 23HF 24HF 25HF 26HF 27HF 28HF 29HF 30HF 31HF 32HF 33HF 34HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 139HF 140HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 358HF 359HF 360HF 361HF 5865VB 5866VB 5886VB 5215VC 5208VP 3503VS 3591VS 3593VS 5151VSA 5410VS Access Door 313AL 821 822 831 Manpower TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 003 Zone 120 130 150 160 190 310 From 150 to 170 From 160 to 310 Modified FIN 23HF 24HF 25HF 27HF 28HF 29HF 30HF 31HF 32HF 33HF 34HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 139HF 140HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 358HF 359HF 360HF 361HF 5865VB 5866VB 5886VB 5215VC 5208VP 3503VS 3591VS 3593VS 5151VSA 5410VS Access Door 313AL 821 822 831 Manpower TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 004 Zone 120 130 150 160 190 310 From 150 to 170 From 160 to 310 Modified FIN 23HF 24HF 25HF 26HF 27HF 28HF 29HF 30HF 31HF 32HF 33HF 34HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 139HF 140HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 358HF 359HF 360HF 361HF 5865VB 5866VB 5886VB 5215VC 5208VP 3503VS 3591VS 3593VS 5151VSA 5410VS
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 53 6

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# @A340 SERVICE BULLETIN
Access Door 313AL 821 822 831 Manpower TOTAL MANHOURS 268.75 ELAPSED TIME (HOURS) 144.0 **CONF 005 Zone 120 130 150 160 190 310 From 150 to 170 From 160 to 310 Modified FIN 23HF 24HF 25HF 26HF 27HF 28HF 29HF 30HF 31HF 32HF 33HF 34HF 97HF 98HF 99HF 100HF 101HF 102HF 137HF 139HF 140HF 149HF 150HF 151HF 301HF 302HF 303HF 304HF 305HF 306HF 307HF 308HF 309HF 310HF 311HF 312HF 358HF 359HF 360HF 361HF 5865VB 5866VB 5886VB 5215VC 5208VP 3503VS 3591VS 3593VS 5151VSA 5410VS 5865VSA 5865VSB Access Door 313AL 821 822 831 Manpower TOTAL MANHOURS 273.00 ELAPSED TIME (HOURS) 144.0 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 364033-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 54 6

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# @A340 SERVICE BULLETIN
ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Preventive Temporary Protective Compound 15-005 As required
Corrosion Preventive Temporary Protective Compound 15-007 As required
Corrosion Preventive Temporary Protective Compound 15-009 As required
Anti-Corrosion Primer (polyurethane) 16-001 As required Anti-Corrosion Primer (Epoxy-Improved Adhesion) 16-006 As required External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 11-00-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-33-10 20-42-12 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-42-11 51-42-21 51-75-12 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to the Consumable Materials List (CML)). (b) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001). (c) For the application of low adhesion sealants (Refer to Process and Material Specification (PMS) 01-02-36). (d) Renew the protective finish (Refer to SRM 51-75-12).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 55 6

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# @A340 SERVICE BULLETIN (e) Apply: Low Adhesion Polysulfide Sealant 09-019 As required to the interfaces of the structure and the mew parts. (f) Fill gaps between the structure with: Corrosion Inhibiting, Fillet Consistency 09-016 As required
Low Adhesion Polysulfide Sealant 09-019 As required Adhesive Sealant 08-004 As required (g) Protect the spot facing area with: Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (h) For the drilling of rivet holes: - Use a soft lead pencil and make marks to show the position of the rivet holes. - Make sure that you have the correct edge clearance before you drill the fastener holes. - If not shown otherwise the tolerance for rivet holes is + 0.1 mm (+ 0.004 in.). - Transfer-drill the existing holes with a pilot drill and a drill bush. - Deburr the holes after you have drilled them. - Cut the rivets to the correct length, as necessary. - When you remove fasteners you must be careful that you do not damage the holes in the structure. - Drill new fastener holes with a pilot drill of 2.5 mm (0.098 in.) diameter. Increase the hole diameter to the correct size for the fastener which you must install.
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 56 6

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# @A340 SERVICE BULLETIN (i) Apply: Wash Primer 16-020 As required Anti-CorrosionPrimer (EpoxyImproved Adhesion) 16-006 As required

to the new drilled holes. (j) Before riveting apply to all contact surfaces and components (Refer to SRM 51-24-00): Corrosion Inhibiting Brush Consistency 09-013 As required (k) Install rivets immediately after you position the components with sealant. If not, tacking pins must be installed temporarily in every third hole. (l) After riveting, remove unwanted sealant from the work area and apply to the rivets: Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (m) Where locking facilities exist, make sure that the electrical connector is correctly locked with: Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
(n) For the protective treatment in the upper area between Frame 80/82 thru Frame 91A, use: Corrosion Preventive Temporary Protective Compound 15-005 As required

Corrosion Preventive Temporary Protective Compound 15-007 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 57 6

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# @A340 SERVICE BULLETIN
Corrosion Preventive Temporary Protective Compound 15-009 As required

(o) For wiring and routing (Refer to ESPM 20-33-10). (p) Do not fully tighten the attachment parts and ties until all the wire harnesses are checked by a continuity test. NOTE: To prevent chaffing, make sure that the cable harness does not sag between the attachment points. (q) Do not shrink the sleeves and shrinkable parts until you do a continuity test of the new wires. (r) For sleeve shrinking (Refer to ESPM 20-42-12). (s) For the installation of sleeves and shrinkable parts (Refer to Process and Material Specification (PMS) 01-07-06 and Process and Material Specification (PMS) 01-07-89). (t) For fastener installation and removal (metallic structure) (Refer to SRM 51-42-11). (u) For fastener installation and removal (composite structure) (Refer to SRM 51-42-21). (v) For the installation of placards (Refer to AMM 11-00-00, Page Block 001). (w) Install Service Bulletin identification placards at each end of new or modified electrical wires in a position where they can be easily seen and at approximately every 1.50 m (59.0 in.). (2) Subtask 364033-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 58 6

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# @A340 SERVICE BULLETIN
References Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-43-42 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required

and Lint-Free Cotton Cloth 19-003 As required (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 59 6

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# @A340 SERVICE BULLETIN (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the pressure seals (Refer to ESPM 20-43-42). (o) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (p) Make sure that the electrical connectors are serviceable before you connect them again. (q) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (r) Put blanking plugs on the disconnected line ends. (3) Subtask 364033-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 364033-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Corrosion Preventive Temporary Protective Compound 15-005 As required
Corrosion Preventive Temporary Protective Compound 15-007 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 60 6

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

# @A340 SERVICE BULLETIN
ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Preventive Temporary Protective Compound 15-009 As required
Anti-Corrosion Primer (polyurethane) 16-001 As required Anti-Corrosion Primer (Epoxy-Improved Adhesion) 16-006 As required External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 11-00-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-33-10 20-42-12 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-42-11 51-42-21 51-75-12 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to the Consumable Materials List (CML)). (b) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001). (c) For the application of low adhesion sealants (Refer to Process and Material Specification (PMS) 01-02-36). (d) Renew the protective finish (Refer to SRM 51-75-12). (e) Apply: Low Adhesion Polysulfide Sealant 09-019 As required to the interfaces of the structure and the mew parts.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 61 6

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# @A340 SERVICE BULLETIN (f) Fill gaps between the structure with: Corrosion Inhibiting, Fillet Consistency 09-016 As required
Low Adhesion Polysulfide Sealant 09-019 As required Adhesive Sealant 08-004 As required (g) Protect the spot facing area with: Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (h) For the drilling of rivet holes: - Use a soft lead pencil and make marks to show the position of the rivet holes. - Make sure that you have the correct edge clearance before you drill the fastener holes. - If not shown otherwise the tolerance for rivet holes is + 0.1 mm (+ 0.004 in.). - Transfer-drill the existing holes with a pilot drill and a drill bush. - Deburr the holes after you have drilled them. - Cut the rivets to the correct length, as necessary. - When you remove fasteners you must be careful that you do not damage the holes in the structure. - Drill new fastener holes with a pilot drill of 2.5 mm (0.098 in.) diameter. Increase the hole diameter to the correct size for the fastener which you must install. (i) Apply: Wash Primer 16-020 As required Anti-CorrosionPrimer (EpoxyImproved Adhesion) 16-006 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 62 6

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# @A340 SERVICE BULLETIN
to the new drilled holes. (j) Before riveting apply to all contact surfaces and components (Refer to SRM 51-24-00): Corrosion Inhibiting Brush Consistency 09-013 As required (k) Install rivets immediately after you position the components with sealant. If not, tacking pins must be installed temporarily in every third hole. (l) After riveting, remove unwanted sealant from the work area and apply to the rivets: Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (m) Where locking facilities exist, make sure that the electrical connector is correctly locked with: Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
(n) For the protective treatment in the upper area between Frame 80/82 thru Frame 91A, use: Corrosion Preventive Temporary Protective Compound 15-005 As required

Corrosion Preventive Temporary Protective Compound 15-007 As required

Corrosion Preventive Temporary Protective Compound 15-009 As required

(o) For wiring and routing (Refer to ESPM 20-33-10).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 63 6

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# @A340 SERVICE BULLETIN (p) Do not fully tighten the attachment parts and ties until all the wire harnesses are checked by a continuity test. NOTE: To prevent chaffing, make sure that the cable harness does not sag between the attachment points. (q) Do not shrink the sleeves and shrinkable parts until you do a continuity test of the new wires. (r) For sleeve shrinking (Refer to ESPM 20-42-12). (s) For the installation of sleeves and shrinkable parts (Refer to Process and Material Specification (PMS) 01-07-06 and Process and Material Specification (PMS) 01-07-89). (t) For fastener installation and removal (metallic structure) (Refer to SRM 51-42-11). (u) For fastener installation and removal (composite structure) (Refer to SRM 51-42-21). (v) For the installation of placards (Refer to AMM 11-00-00, Page Block 001). (w) Install Service Bulletin identification placards at each end of new or modified electrical wires in a position where they can be easily seen and at approximately every 1.50 m (59.0 in.). (2) Subtask 364033-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-43-42 20-48-00 Standards Manual (SM)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 64 6

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# @A340 SERVICE BULLETIN
References Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required

and Lint-Free Cotton Cloth 19-003 As required (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the pressure seals (Refer to ESPM 20-43-42). (o) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 65 6

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

# @A340 SERVICE BULLETIN (p) Make sure that the electrical connectors are serviceable before you connect them again. (q) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (r) Put blanking plugs on the disconnected line ends. (3) Subtask 364033-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 364033-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Corrosion Preventive Temporary Protective Compound 15-005 As required
Corrosion Preventive Temporary Protective Compound 15-007 As required
Corrosion Preventive Temporary Protective Compound 15-009 As required
Anti-Corrosion Primer (polyurethane) 16-001 As required Anti-Corrosion Primer (Epoxy-Improved Adhesion) 16-006 As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 66 6

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

# @A340 SERVICE BULLETIN
ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 11-00-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-33-10 20-42-12 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-42-11 51-42-21 51-75-12 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to the Consumable Materials List (CML)). (b) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001). (c) For the application of low adhesion sealants (Refer to Process and Material Specification (PMS) 01-02-36). (d) Renew the protective finish (Refer to SRM 51-75-12). (e) Apply: Low Adhesion Polysulfide Sealant 09-019 As required to the interfaces of the structure and the mew parts. (f) Fill gaps between the structure with: Corrosion Inhibiting, Fillet Consistency 09-016 As required
Low Adhesion Polysulfide Sealant 09-019 As required Adhesive Sealant 08-004 As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 67 6

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# @A340 SERVICE BULLETIN (g) Protect the spot facing area with: Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (h) For the drilling of rivet holes: - Use a soft lead pencil and make marks to show the position of the rivet holes. - Make sure that you have the correct edge clearance before you drill the fastener holes. - If not shown otherwise the tolerance for rivet holes is + 0.1 mm (+ 0.004 in.). - Transfer-drill the existing holes with a pilot drill and a drill bush. - Deburr the holes after you have drilled them. - Cut the rivets to the correct length, as necessary. - When you remove fasteners you must be careful that you do not damage the holes in the structure. - Drill new fastener holes with a pilot drill of 2.5 mm (0.098 in.) diameter. Increase the hole diameter to the correct size for the fastener which you must install. (i) Apply: Wash Primer 16-020 As required Anti-CorrosionPrimer (EpoxyImproved Adhesion) 16-006 As required

to the new drilled holes. (j) Before riveting apply to all contact surfaces and components (Refer to SRM 51-24-00): Corrosion Inhibiting Brush Consistency 09-013 As required (k) Install rivets immediately after you position the components with sealant. If not, tacking pins must be installed temporarily in every third hole. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 68 6

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

# @A340 SERVICE BULLETIN (l) After riveting, remove unwanted sealant from the work area and apply to the rivets: Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (m) Where locking facilities exist, make sure that the electrical connector is correctly locked with: Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
(n) For the protective treatment in the upper area between Frame 80/82 thru Frame 91A, use: Corrosion Preventive Temporary Protective Compound 15-005 As required

Corrosion Preventive Temporary Protective Compound 15-007 As required

Corrosion Preventive Temporary Protective Compound 15-009 As required

(o) For wiring and routing (Refer to ESPM 20-33-10). (p) Do not fully tighten the attachment parts and ties until all the wire harnesses are checked by a continuity test. NOTE: To prevent chaffing, make sure that the cable harness does not sag between the attachment points. (q) Do not shrink the sleeves and shrinkable parts until you do a continuity test of the new wires. (r) For sleeve shrinking (Refer to ESPM 20-42-12). (s) For the installation of sleeves and shrinkable parts (Refer to Process and Material Specification (PMS) 01-07-06 and Process and Material Specification (PMS) 01-07-89). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 69 6

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

# @A340 SERVICE BULLETIN (t) For fastener installation and removal (metallic structure) (Refer to SRM 51-42-11). (u) For fastener installation and removal (composite structure) (Refer to SRM 51-42-21). (v) For the installation of placards (Refer to AMM 11-00-00, Page Block 001). (w) Install Service Bulletin identification placards at each end of new or modified electrical wires in a position where they can be easily seen and at approximately every 1.50 m (59.0 in.). (2) Subtask 364033-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-43-42 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 70 6

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

# @A340 SERVICE BULLETIN (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required

and Lint-Free Cotton Cloth 19-003 As required (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the pressure seals (Refer to ESPM 20-43-42). (o) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (p) Make sure that the electrical connectors are serviceable before you connect them again. (q) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (r) Put blanking plugs on the disconnected line ends. (3) Subtask 364033-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 71 6

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# @A340 SERVICE BULLETIN
**CONF 004 (1) Subtask 364033-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Corrosion Preventive Temporary Protective Compound 15-005 As required
Corrosion Preventive Temporary Protective Compound 15-007 As required
Corrosion Preventive Temporary Protective Compound 15-009 As required
Anti-Corrosion Primer (polyurethane) 16-001 As required Anti-Corrosion Primer (Epoxy-Improved Adhesion) 16-006 As required External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 11-00-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-33-10 20-42-12

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 72 6

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

# @A340 SERVICE BULLETIN
References Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-42-11 51-42-21 51-75-12 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to the Consumable Materials List (CML)). (b) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001). (c) For the application of low adhesion sealants (Refer to Process and Material Specification (PMS) 01-02-36). (d) Renew the protective finish (Refer to SRM 51-75-12). (e) Apply: Low Adhesion Polysulfide Sealant 09-019 As required to the interfaces of the structure and the mew parts. (f) Fill gaps between the structure with: Corrosion Inhibiting, Fillet Consistency 09-016 As required
Low Adhesion Polysulfide Sealant 09-019 As required Adhesive Sealant 08-004 As required (g) Protect the spot facing area with: Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 73 6

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# @A340 SERVICE BULLETIN (h) For the drilling of rivet holes: - Use a soft lead pencil and make marks to show the position of the rivet holes. - Make sure that you have the correct edge clearance before you drill the fastener holes. - If not shown otherwise the tolerance for rivet holes is + 0.1 mm (+ 0.004 in.). - Transfer-drill the existing holes with a pilot drill and a drill bush. - Deburr the holes after you have drilled them. - Cut the rivets to the correct length, as necessary. - When you remove fasteners you must be careful that you do not damage the holes in the structure. - Drill new fastener holes with a pilot drill of 2.5 mm (0.098 in.) diameter. Increase the hole diameter to the correct size for the fastener which you must install. (i) Apply: Wash Primer 16-020 As required Anti-CorrosionPrimer (EpoxyImproved Adhesion) 16-006 As required

to the new drilled holes. (j) Before riveting apply to all contact surfaces and components (Refer to SRM 51-24-00): Corrosion Inhibiting Brush Consistency 09-013 As required (k) Install rivets immediately after you position the components with sealant. If not, tacking pins must be installed temporarily in every third hole. (l) After riveting, remove unwanted sealant from the work area and apply to the rivets: Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 74 6

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# @A340 SERVICE BULLETIN (m) Where locking facilities exist, make sure that the electrical connector is correctly locked with: Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
(n) For the protective treatment in the upper area between Frame 80/82 thru Frame 91A, use: Corrosion Preventive Temporary Protective Compound 15-005 As required

Corrosion Preventive Temporary Protective Compound 15-007 As required

Corrosion Preventive Temporary Protective Compound 15-009 As required

(o) For wiring and routing (Refer to ESPM 20-33-10). (p) Do not fully tighten the attachment parts and ties until all the wire harnesses are checked by a continuity test. NOTE: To prevent chaffing, make sure that the cable harness does not sag between the attachment points. (q) Do not shrink the sleeves and shrinkable parts until you do a continuity test of the new wires. (r) For sleeve shrinking (Refer to ESPM 20-42-12). (s) For the installation of sleeves and shrinkable parts (Refer to Process and Material Specification (PMS) 01-07-06 and Process and Material Specification (PMS) 01-07-89). (t) For fastener installation and removal (metallic structure) (Refer to SRM 51-42-11). (u) For fastener installation and removal (composite structure) (Refer to SRM 51-42-21). (v) For the installation of placards (Refer to AMM 11-00-00, Page Block 001).
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 75 6

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# @A340 SERVICE BULLETIN (w) Install Service Bulletin identification placards at each end of new or modified electrical wires in a position where they can be easily seen and at approximately every 1.50 m (59.0 in.). (2) Subtask 364033-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-43-42 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required

and Lint-Free Cotton Cloth 19-003 As required
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 76 6

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# @A340 SERVICE BULLETIN (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the pressure seals (Refer to ESPM 20-43-42). (o) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (p) Make sure that the electrical connectors are serviceable before you connect them again. (q) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (r) Put blanking plugs on the disconnected line ends. (3) Subtask 364033-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 005 (1) Subtask 364033-910-201-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 77 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Sealant 08-004 As required Corrosion Inhibiting Brush Consistency 09-013 As required Corrosion Inhibiting, Fillet Consistency 09-016 As required Low Adhesion Polysulfide Sealant 09-019 As required Chemical Conversion Coating Yellow Aluminum 13-002 As required Corrosion Preventive Temporary Protective Compound 15-005 As required
Corrosion Preventive Temporary Protective Compound 15-007 As required
Corrosion Preventive Temporary Protective Compound 15-009 As required
Anti-Corrosion Primer (polyurethane) 16-001 As required Anti-Corrosion Primer (Epoxy-Improved Adhesion) 16-006 As required External Top Coat (polyurethane) 16-018 As required Wash Primer 16-020 As required Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required
References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 11-00-00, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-33-10 20-42-12 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-02-36 Process and Material Specification (PMS) 01-07-06 Process and Material Specification (PMS) 01-07-89 Standards Manual (SM)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 78 6

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# @A340 SERVICE BULLETIN
References Structural Repair Manual (SRM) 51-24-00 51-42-11 51-42-21 51-75-12 (a) For the specification of the materials (Mat. No.) given in this Service Bulletin (Refer to the Consumable Materials List (CML)). (b) For the identification of Zones (Refer to AMM 06-20-00, Page Block 001). (c) For the application of low adhesion sealants (Refer to Process and Material Specification (PMS) 01-02-36). (d) Renew the protective finish (Refer to SRM 51-75-12). (e) Apply: Low Adhesion Polysulfide Sealant 09-019 As required to the interfaces of the structure and the mew parts. (f) Fill gaps between the structure with: Corrosion Inhibiting, Fillet Consistency 09-016 As required
Low Adhesion Polysulfide Sealant 09-019 As required Adhesive Sealant 08-004 As required (g) Protect the spot facing area with: Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (h) For the drilling of rivet holes: - Use a soft lead pencil and make marks to show the position of the rivet holes. - Make sure that you have the correct edge clearance before you drill the fastener holes. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 79 6

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# @A340 SERVICE BULLETIN - If not shown otherwise the tolerance for rivet holes is + 0.1 mm (+ 0.004 in.). - Transfer-drill the existing holes with a pilot drill and a drill bush. - Deburr the holes after you have drilled them. - Cut the rivets to the correct length, as necessary. - When you remove fasteners you must be careful that you do not damage the holes in the structure. - Drill new fastener holes with a pilot drill of 2.5 mm (0.098 in.) diameter. Increase the hole diameter to the correct size for the fastener which you must install. (i) Apply: Wash Primer 16-020 As required Anti-CorrosionPrimer (EpoxyImproved Adhesion) 16-006 As required

to the new drilled holes. (j) Before riveting apply to all contact surfaces and components (Refer to SRM 51-24-00): Corrosion Inhibiting Brush Consistency 09-013 As required (k) Install rivets immediately after you position the components with sealant. If not, tacking pins must be installed temporarily in every third hole. (l) After riveting, remove unwanted sealant from the work area and apply to the rivets: Anti-Corrosion Primer (polyurethane) 16-001 As required
External Top Coat (polyurethane) 16-018 As required (m) Where locking facilities exist, make sure that the electrical connector is correctly locked with: Lockwire, Stainless Steel, Annealed, 0.8mm Dia. 19-010 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 80 6

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# @A340 SERVICE BULLETIN (n) For the protective treatment in the upper area between Frame 80/82 thru Frame 91A, use: Corrosion Preventive Temporary Protective Compound 15-005 As required

Corrosion Preventive Temporary Protective Compound 15-007 As required

Corrosion Preventive Temporary Protective Compound 15-009 As required

(o) For wiring and routing (Refer to ESPM 20-33-10). (p) Do not fully tighten the attachment parts and ties until all the wire harnesses are checked by a continuity test. NOTE: To prevent chaffing, make sure that the cable harness does not sag between the attachment points. (q) Do not shrink the sleeves and shrinkable parts until you do a continuity test of the new wires. (r) For sleeve shrinking (Refer to ESPM 20-42-12). (s) For the installation of sleeves and shrinkable parts (Refer to Process and Material Specification (PMS) 01-07-06 and Process and Material Specification (PMS) 01-07-89). (t) For fastener installation and removal (metallic structure) (Refer to SRM 51-42-11). (u) For fastener installation and removal (composite structure) (Refer to SRM 51-42-21). (v) For the installation of placards (Refer to AMM 11-00-00, Page Block 001). (w) Install Service Bulletin identification placards at each end of new or modified electrical wires in a position where they can be easily seen and at approximately every 1.50 m (59.0 in.). (2) Subtask 364033-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 81 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Lint-Free Cotton Cloth 19-003 As required References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-53, Page Block 001 11-00-00, Page Block 201 Task 20-21-15-912-801 Elec. Std. Practices Manual (ESPM) 20-33-00 20-43-10 20-43-42 20-48-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-24-00 51-43-00 51-47-00 (a) Use a non metallic spatula to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (b) For fasteners spacing and margin (Refer to SRM 51-47-00). (c) To torque tighten the electrical component fasteners (Refer to AMM Task 20-21-15-912-801). (d) Clean the areas where you will install the placards with : Solvent General Purpose 11-026 As required

and Lint-Free Cotton Cloth 19-003 As required (e) Apply the sealant (Refer to SRM 51-24-00). (f) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block 001). (h) Tag all the parts you must remove and retain to make the subsequent installation easier. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 82 6

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# @A340 SERVICE BULLETIN (i) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (j) If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to the Standards Manual (SM). The SM will give you the correct part number to part number relationship. (k) For the installation of the placards, (Refer to AMM 11-00-00, Page Block 201). (l) Apply a special protection on new parts (Refer to SRM 51-23-12). (m) Obey the instructions for the general wiring installation, (Refer to ESPM 20-33-00). (n) Obey the instructions of the pressure seals (Refer to ESPM 20-43-42). (o) Obey the instructions of the splices installation (Refer to ESPM 20-43-10). (p) Make sure that the electrical connectors are serviceable before you connect them again. (q) To install new wires, cut them to the necessary length, crimp the terminals and connect them (Referto ESPM 20-48-00). (r) Put blanking plugs on the disconnected line ends. (3) Subtask 364033-839-201-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 364033-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 831, Door 821 Work location from Frame 20 to Frame 39.2 Panel 132CC Panel 132GC Panel 132KC Panel 132MC Panel 132PC Panel 132RC Panel 132TC DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 83 6

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# @A340 SERVICE BULLETIN
150 Access Door 822 160 Access Door 313AL Work location Panel 161BC Panel 161EC Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-33-00, Page Block 001 (a) In the FWD cargo compartment remove the ceiling panels 132CC, 132GC, 132KC, 132MC, 132PC, 132RC and 132TC for access as necessary (Refer to AMM 25-52-00, Page Block 201). (b) Open the Bulk cargo compartment door (Refer to AMM 52-33-00, Page Block 001). (c) In the BULK cargo compartment remove the ceiling panels 161BC and 161EC for access as necessary (Refer to AMM 25-54-00, Page Block 201). (2) Subtask 364033-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 84 6

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# @A340 SERVICE BULLETIN (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (3) Subtask 364033-010-001-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-000-801 Task 25-28-41-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Seats (Refer to AMM Task 25-21-41-000-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 85 6

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# @A340 SERVICE BULLETIN (g) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Textile Floor (TF) Covering for access to the spare conduits (Refer to AMM Task 25-28-41-000-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the floor panel 252LG for access to the spare conduits (Refer to AMM Task 53-00-00-000-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (k) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (l) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (m) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (4) Subtask 364033-862-001-001 - De-energize Electrical Network (Safety Precautions). Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 86 6

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# @A340 SERVICE BULLETIN (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s). **CONF 002 (1) Subtask 364033-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 831, Door 821 Work location from Frame 20 to Frame 39.2 Panel 132CC Panel 132GC Panel 132KC Panel 132MC Panel 132PC Panel 132RC Panel 132TC 150 Access Door 822 160 Access Door 313AL Work location Panel 161BC Panel 161EC Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-33-00, Page Block 001 (a) In the FWD cargo compartment remove the ceiling panels 132CC, 132GC, 132KC, 132MC, 132PC, 132RC and 132TC for access as necessary (Refer to AMM 25-52-00, Page Block 201). (b) Open the Bulk cargo compartment door (Refer to AMM 52-33-00, Page Block 001). (c) In the BULK cargo compartment remove the ceiling panels 161BC and 161EC for access as necessary (Refer to AMM 25-54-00, Page Block 201). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 87 6

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# @A340 SERVICE BULLETIN (2) Subtask 364033-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (3) Subtask 364033-010-001-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 88 6

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# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-000-801 Task 25-28-41-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Seats (Refer to AMM Task 25-21-41-000-801). (g) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Textile Floor (TF) Covering for access to the spare conduits (Refer to AMM Task 25-28-41-000-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the floor panel 252LG for access to the spare conduits (Refer to AMM Task 53-00-00-000-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 89 6

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# @A340 SERVICE BULLETIN(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (k) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (l) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (m) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (4) Subtask 364033-862-001-001 - De-energize Electrical Network (Safety Precautions). Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B).
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 90 6

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# @A340 SERVICE BULLETIN (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s). **CONF 003 (1) Subtask 364033-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 831, Door 821 Work location from Frame 20 to Frame 39.2 Panel 132CC Panel 132GC Panel 132KC Panel 132MC Panel 132PC Panel 132RC Panel 132TC 150 Access Door 822 160 Access Door 313AL Work location Panel 161BC Panel 161EC Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-33-00, Page Block 001 (a) In the FWD cargo compartment remove the ceiling panels 132CC, 132GC, 132KC, 132MC, 132PC, 132RC and 132TC for access as necessary (Refer to AMM 25-52-00, Page Block 201). (b) Open the Bulk cargo compartment door (Refer to AMM 52-33-00, Page Block 001). (c) In the BULK cargo compartment remove the ceiling panels 161BC and 161EC for access as necessary (Refer to AMM 25-54-00, Page Block 201). (2) Subtask 364033-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 91 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (3) Subtask 364033-010-001-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-000-801 Task 25-28-41-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 92 6

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

# @A340 SERVICE BULLETIN (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Seats (Refer to AMM Task 25-21-41-000-801). (g) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Textile Floor (TF) Covering for access to the spare conduits (Refer to AMM Task 25-28-41-000-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the floor panel 252LG for access to the spare conduits (Refer to AMM Task 53-00-00-000-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (k) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (l) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (m) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 93 6

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

# @A340 SERVICE BULLETIN (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (4) Subtask 364033-862-001-001 - De-energize Electrical Network (Safety Precautions). Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 94 6

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

# @A340 SERVICE BULLETIN
**CONF 004 (1) Subtask 364033-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 831, Door 821 Work location from Frame 20 to Frame 39.2 Panel 132CC Panel 132GC Panel 132KC Panel 132MC Panel 132PC Panel 132RC Panel 132TC 150 Access Door 822 160 Access Door 313AL Work location Panel 161BC Panel 161EC Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-33-00, Page Block 001 (a) In the FWD cargo compartment remove the ceiling panels 132CC, 132GC, 132KC, 132MC, 132PC, 132RC and 132TC for access as necessary (Refer to AMM 25-52-00, Page Block 201). (b) Open the Bulk cargo compartment door (Refer to AMM 52-33-00, Page Block 001). (c) In the BULK cargo compartment remove the ceiling panels 161BC and 161EC for access as necessary (Refer to AMM 25-54-00, Page Block 201). (2) Subtask 364033-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 95 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (3) Subtask 364033-010-001-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-000-801 Task 25-28-41-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 96 6

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

# @A340 SERVICE BULLETIN (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Seats (Refer to AMM Task 25-21-41-000-801). (g) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Textile Floor (TF) Covering for access to the spare conduits (Refer to AMM Task 25-28-41-000-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the floor panel 252LG for access to the spare conduits (Refer to AMM Task 53-00-00-000-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (k) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (l) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (m) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 97 6

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

# @A340 SERVICE BULLETIN (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (4) Subtask 364033-862-001-001 - De-energize Electrical Network (Safety Precautions). Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 98 6

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

# @A340 SERVICE BULLETIN
**CONF 005 (1) Subtask 364033-941-201-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 831, Door 821 Work location from Frame 20 to Frame 39.2 Panel 132CC Panel 132GC Panel 132KC Panel 132MC Panel 132PC Panel 132RC Panel 132TC 150 Access Door 822 160 Access Door 313AL Work location Panel 161BC Panel 161EC Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-33-00, Page Block 001 (a) In the FWD cargo compartment remove the ceiling panels 132CC, 132GC, 132KC, 132MC, 132PC, 132RC and 132TC for access as necessary (Refer to AMM 25-52-00, Page Block 201). (b) Open the Bulk cargo compartment door (Refer to AMM 52-33-00, Page Block 001). (c) In the BULK cargo compartment remove the ceiling panels 161BC and 161EC for access as necessary (Refer to AMM 25-54-00, Page Block 201). (2) Subtask 364033-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 99 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 36-11-34-000-802 Task 36-22-17-000-801 Task 36-22-17-000-802 Task 52-10-00-010-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put access platform(s) in position. (c) Open the passenger/crew door(s) (Refer to AMM Task 52-10-00-010-801). (d) Open the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (f) Open the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-010-801). (g) Do the Job Set-up procedure as specified in the removal of the sensing elements (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802). (h) Do the Job Set-up procedure as specified in the removal of the Bleed Monitoring Computer (BMC) (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (3) Subtask 364033-010-001-001 - Remove/Open for Access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-000-801 Task 25-28-41-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-53-00-000-801 Task 25-75-41-000-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 100 6

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

# @A340 SERVICE BULLETIN (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, remove the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-000-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, remove (if necessary) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (d) At Frame 39.2 in the FWD cargo-compartment, remove (if necessary) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (e) At Frame 20 in the FWD cargo-compartment, remove the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-000-801). (f) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Seats (Refer to AMM Task 25-21-41-000-801). (g) On the RH side only, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the Textile Floor (TF) Covering for access to the spare conduits (Refer to AMM Task 25-28-41-000-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, remove (if necessary) the floor panel 252LG for access to the spare conduits (Refer to AMM Task 53-00-00-000-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, remove (if necessary) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, remove (if necessary) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (k) At Frame 53.2 in the AFT cargo-compartment, remove the partition panel 152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-000-801). (l) On the LH side of the belly fairing, remove (if necessary) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). (m) On the RH side of the belly fairing, remove the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-000-801 and AMM Task 53-35-13-000-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 101 6

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# @A340 SERVICE BULLETIN (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-000-801). (4) Subtask 364033-862-001-001 - De-energize Electrical Network (Safety Precautions). Manpower Resources Skills NON SPECIFIC (a) In the cockpit, on the panel 235VU, make sure that these pushbutton switches are released : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Open, safety and tags the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S (c) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the pushbutton switches on the overhead panel : - 211VU (EMER ELEC PWR), - 235VU (ELEC). (d) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (e) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (f) Make sure that there is a warning notice at the access door 121EL to tell persons not to connect the external power connector (s). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 364033-831-016-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 102 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 300 TIE F9000095227895 BUNDLE NSA935401-08 300 TIE NSA935401-13 300 TIE References Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01 Sheet 02
(a) As shown in Fig. A-FBMAA Sheet 01, install the wire, using spares conduits between Frame 37 and Frame 53.2, as shown on the wiring diagram, Fig. AFCBAA Sheet 01 and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FCBAA Sheet 02) supplied in :
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 103 6

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# @A340 SERVICE BULLETIN
Bundle F9000095227895 NOTE: The spares conduits is divided in two parts. The first parts go away from Frame 40 to Frame 47 and the second parts go away from Frame 48 to Frame 53.2 (b) Attach the wires with : 300 Tie-Cable NSA935401-03 Item 169 300 Tie-Cable NSA935401-08 300 Tie-Cable NSA935401-13

(2) Subtask 364033-831-017-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 50 TIE F9000095227895 BUNDLE NSA935401-06 50 TIE NSA935401-13 50 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Fig. A-FCAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove and retain the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wires as shown on the wiring diagram Fig. A-FCAAA Sheet 01, and as given in the Hook-up Chart lines : - 1 thru 5 (Refer to Fig. A-FCAAA Sheet 04). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 104 6

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# @A340 SERVICE BULLETIN (c) Install the wires as shown on the wiring diagrams, Fig. A-FCAAA Sheet 02and Fig. A-FCAAA Sheet 03and as given in the Hook-up Chart lines : - 9 thru 19 (Refer to Fig. A-FCAAA Sheet 04) supplied in : Bundle F9000095227895 (d) Attach the wires with : 50 Tie-Cable NSA935401-03 Item 169 50 Tie-Cable NSA935401-06 50 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (3) Subtask 364033-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 02 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 22 Screw Item (20) Discard 32 Washer Item (14) Discard 32 Clamp Item (86) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 105 6

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# @A340 SERVICE BULLETIN 32 Sleeve Item (13) Discard 5 Screw Item (91) Discard 10 Spacer Item (16) Discard 5 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 97HF 1 Sensing Element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing Element 35624-2-255 Item (2) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(4) Subtask 364033-831-002-001 - Remove the sensing elements and the supports between FR44 and FR51. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 51 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 03 (Refer to AMM Task 36-22-17-000-801) 18 Screw Item (21) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 106 6

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# @A340 SERVICE BULLETIN 30 Washer Item (14) Discard 30 Clamp Item (86) Discard 30 Sleeve Item (13) Discard 18 Spacer Item (16) Discard 12 Screw Item (20) Discard 2 Nut Item (15) Discard FIN 99HF 1 Sensing Element 35612-2-255 Item (3) Discard FIN 100HF 1 Sensing Element 35605-2-255 Item (6) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(5) Subtask 364033-831-003-001 - Remove the sensing elements and the supports between FR51 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 51 to Frame 53.6 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 04 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 107 6

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# @A340 SERVICE BULLETIN 18 Screw Item (21) Discard 37 Washer Item (14) Discard 37 Clamp Item (86) Discard 37 Sleeve Item (13) Discard 23 Spacer Item (16) Discard 16 Screw Item (20) Discard 1 Screw Item (93) Discard 1 Spacer Item (18) Discard 2 Screw Item (91) Discard 3 Nut Item (15) Discard FIN 101HF 1 Sensing Element 35603-2-255 Item (4) Discard FIN 102HF 1 Sensing Element 35600-2-255 Item (5) Discard FIN 23HF 1 Sensing Element 35571-2-255 Item (7) Discard 6 Rivet Item (11) Discard 3 Support Item (10) Discard

(6) Subtask 364033-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 108 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 05 (Refer to AMM Task 36-22-17-000-801) 19 Screw Item (20) Discard 27 Washer Item (14) Discard 27 Clamp Item (86) Discard 27 Sleeve Item (13) Discard 4 Screw Item (91) Discard 12 Spacer Item (16) Discard 4 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 24HF 1 Sensing Element 35580-2-255 Item (8) Discard FIN 25HF 1 Sensing Element 35611-3-255 Item (9) Discard 2 Rivet Item (11) Discard 1 Support Item (10) Discard

(7) Subtask 364033-010-002-001 - If necessary, remove the ducts between FR53.5 and FR53.6 for access. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 109 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (112) Retain 1 Duct assy Item (114) Retain

(8) Subtask 364033-831-005-001 - Drill a new hole in the structure between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required Polyurethane Finnish Paint 16-018 As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 110 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Drill one hole on the structure between FR53.5 and FR53.6 to a diameter comprised between 13.5mm (0.531in.) Min. and 13.7mm (0.539 in.) Max. as shown on Fig. A-FBCAA

. (b) Do a spotfacing on the structure between FR53.5 and 53.6 to a diameter of 24mm (0.944 in.) with a radius of 2mm (0.078in.) NOTE: Be careful at the depth : 2mm (0.078 in.) Min. and 3mm (0.118 in.) Max. (c) Protect the hole and the spotfacing with : Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
Polyurethane Finnish Paint 16-018 As required (9) Subtask 364033-831-006-001 - Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 111 6

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# @A340 SERVICE BULLETIN Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBFAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02 (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBFAA

. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Fig. A-FBFAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required
(e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581571700000 or 1 Blanket-Insulation F2582261900000 becomes DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 112 6

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# @A340 SERVICE BULLETIN
1 Blanket-Insulation F0041196200000 or 1 Blanket-Insulation F2581566600000 becomes 1 Blanket-Insulation F0041196300000 or 1 Blanket-Insulation F2581666600000 becomes 1 Blanket-Insulation F0041196400000 or 1 Blanket-Insulation F2581677800000 becomes 1 Blanket-Insulation F0041196500000 or 1 Blanket-Insulation F2581677900000 becomes 1 Blanket-Insulation F0041196600000 or 1 Blanket-Insulation F2582242300000 becomes 1 Blanket-Insulation F0041196700000 (f) Install : Fig. A-FBFAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure, apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with :
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 113 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (g) Install the insulation blanket. (10) Subtask 364033-410-001-001 - If removed, install the ducts between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (114) Retained at removal (11) Subtask 364033-010-003-001 - If necessary, remove the ducts between FR43 and FR45 for access. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 114 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Remove : (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(12) Subtask 364033-831-007-001 - Replace the web assy and the half clamp assy at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 115 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBEAA Replacement of the Web Assy at FR44 on the LH side Sheet 01 Sheet 02 (a) Remove : Fig. A-FBEAA 17 Screw Item (119) Retain 17 Washer Item (124) Retain 1 Strip cover assy Item (122) Retain 2 Screw Item (120) Retain 1 Half clamp assy F5331583500000 Item (118) Discard 1 Half clamp assy Item (121) Retain 1 Bracket Item (123) Retain 1 Web Assy F5331591000000 Item (117) Discard NOTE: It is not necessary to remove completely the bracket Item (123). (b) Install : Fig. A-FBEAA 1 Web Assy F5331591000200 Item 117 1 Bracket Item (123) Retained at removal 1 Half clamp assy Item (121) Retained at removal 1 Half clamp assy F5331583500200 Item 118 2 Screw Item (120) Retained at removal 1 Strip cover assy Item (122) Retained at removal 17 Washer Item (124) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 116 6

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# @A340 SERVICE BULLETIN 17 Screw Item (119) Retained at removal NOTE: Install the new web assy with : Corrosion Inhibiting Fillet Consistency 09-016B As required

and Low Adhesion Polysulfide Sealant 09-019B As required (13) Subtask 364033-831-008-001 - Install the new brackets for the routing of the sensing elements at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBGAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBGAA

.
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 117 6

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# @A340 SERVICE BULLETIN (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBGAA

. (c) Install : 1 Support F0041178800000 Item 98 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (14) Subtask 364033-410-002-001 - If removed, install the ducts between FR43 and FR45. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 118 6

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# @A340 SERVICE BULLETIN 1 Duct assy Item (116) Retained at removal (15) Subtask 364033-831-009-001 - Install the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 119 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBHAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 120 6

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# @A340 SERVICE BULLETIN
3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 121 6

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# @A340 SERVICE BULLETIN
FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

(16) Subtask 364033-831-010-001 - Install the sensing elements and the supports between FR44 and FR50. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 11 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 3 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 14 BOLT 21 NAS6603-9 9 BOLT 23 NAS6603-16 1 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 122 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM References Fig. A-FBJAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46. 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 3 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 5 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 123 6

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# @A340 SERVICE BULLETIN
FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 124 6

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# @A340 SERVICE BULLETIN
3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105 24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (17) Subtask 364033-831-011-001 - Install the sensing elements and the supports between FR50 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 125 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM References Fig. A-FBKAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 126 6

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# @A340 SERVICE BULLETIN
7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 306HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13 2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548620000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 127 6

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# @A340 SERVICE BULLETIN
4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 128 6

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# @A340 SERVICE BULLETIN
NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (18) Subtask 364033-831-012-001 - Install the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 129 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 112 35625-2-255 1 SNSGELEM References Fig. A-FBLAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200095 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 130 6

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# @A340 SERVICE BULLETIN
2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (19) Subtask 364033-010-004-001 - If necessary, remove the ducts between FR39 and FR40 for access. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 131 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain 1 Duct assy Item (127) Retain

(20) Subtask 364033-831-013-001 - Install the new supports for the new harness between FR39.1 and FR39.2. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 97 ASNA2050DCJ3215 14 RIVET Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required
References Fig. A-FBNAA Installation of the Supports for the New Harness Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 132 6

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# @A340 SERVICE BULLETIN (a) At FR39.1, remove a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (88) Retain 2 Install : 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (b) At FR39.1, install a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Put the support Item (88) in position as shown on Fig. A-FBNAA Sheet 03

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item (88). 3 Install : 1 Support Item (88) Retained at removal 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (c) At FR39.2, install a plate between STGR 46 and STGR 47. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (89) Retain 2 Put the plate Item 64 in position as shown on Fig. A-FBNAA Sheet 04

. 3 Drill one hole on the plate Item 64 to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the hole of the structure. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 133 6

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# @A340 SERVICE BULLETIN
4 Drill three holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the plate Item (64). 5 Install : 1 Plate F5391094700095 Item 64 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (d) At FR39.2, install two supports between STGR46 and STGR48. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Put the supports Item 63 in position as shown on Fig. A-FBNAA Sheet 04

. 2 Drill four holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the supports Item 63. 3 Install : 2 Support ASNA2327-3-8 Item 63 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (e) At FR39.1, install a support between STGR 39 and STGR 40. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 05 1 Put the support Item 65 in position as shown on Fig. A-FBNAA Sheet 05

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item 65. 3 Install : 1 Support NSA5456-3-8 Item 65 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 134 6

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# @A340 SERVICE BULLETIN (21) Subtask 364033-831-014-001 - Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 18 NSA5527-03-11 1 SPACER 92 NSA57304-643ADL 1 PLATE 155 NSA5516-04ND 1 CLAMP 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 2 CABLE 182 NSA5050-4 1 NUT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F9000095227895 BUNDLE F9100095005595 1 PLACARD References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 135 6

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# @A340 SERVICE BULLETIN (b) Put in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item 175 (c) Install the splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095227895 (d) Identify the splice FIN 3593VS with the identification sleeves and the identification label supplied in : 1 Placard F9100095005595 and Bundle F9000095227895 (e) On the fuselage close to the plugs, identify the FIN 309HF and the FIN 310HF with : 1 Placard F1131031521900 and 1 Placard F1131031522000 (f) Identify the wire No. 3622-0543 of the FIN 310HF and the wire No. 3622-0544 of the FIN 309HF with the identification sleeves supplied in : 1 Placard F9100095005595 (g) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 136 6

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# @A340 SERVICE BULLETIN
4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175)
5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175
6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095227895 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (h) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer NSA5527-03-11 Item 18 1 Clamp NSA5516-04ND Item (155) Retained at removal 1 Clamp NSA5516-04ND Item 155 1 Washer ASNA2397-10L Item 14 1 Screw NAS1801-3-22 Item 168 and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (i) Secure the FIN 310HF : Refer to Fig. A-FBCAA Sheet 04

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 137 6

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# @A340 SERVICE BULLETIN
1 Remove : 1 Nut Discard 2 Install : 1 Plate-Attachment NSA57304-643ADL Item 92 With : 1 Nut NSA5050-4 Item 182 3 Secure the new nut and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (22) Subtask 364033-831-015-001 - Install the new Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 26.00 Minimum number of person 2 Subtask elapsed time 13.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 4 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 138 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 1 CABLE 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031522100 1 PLACARD F9000095227895 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-42 Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 139 6

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# @A340 SERVICE BULLETIN (a) Install supports of new routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 7 Screw Item (130) Discard 7 Washer Item (131) Discard 7 Clamp Item (150) Retain 2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section B-B : 7 Stud NSA5159-17 Item 151 7 Clamp Item (150) Retained at removal 7 Spacer NSA5527-03-08 Item 152 7 Clamp NSA935807-04 Item 150 7 Washer NSA935808-03 Item 131 7 Nut NSA5050-3 Item 154 b For Section C-C : 1 Stud NSA5159-17 Item 151 1 Clamp NSA935807-04 Item 150 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 65 installed DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 140 6

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# @A340 SERVICE BULLETIN previously. 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section F-F : 1 Screw Item (130) Discard 1 Washer Item (131) Discard 1 Clamp Item (150) Retain b For Section G-G : 1 Screw Item (132) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section H-H : 1 Stud NSA5159-17 Item 151 1 Clamp Item (150) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 b For Section J-J : 1 Stud NSA5159-17 Item 151 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 141 6

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# @A340 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Screw Item (136) Discard 2 Washer Item (137) Discard 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud NSA5159-17 Item 151 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section K-K : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 142 6

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# @A340 SERVICE BULLETIN 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section M-M : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 143 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Screw Item (130) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 144 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section P-P : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 145 6

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# @A340 SERVICE BULLETIN
12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 146 6

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# @A340 SERVICE BULLETIN
13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section Q-Q : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (152) Retain 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (135) Retain 1 Spacer Item (152) Discard 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (144) Discard 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section S-S : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 147 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (134) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 15 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Screw Item (132) Discard 2 Washer Item (153) Discard 2 Clamp Item (138) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 148 6

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# @A340 SERVICE BULLETIN
16 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud NSA5159-17 Item 151 2 Clamp Item (138) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 17 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, remove for Section T-T : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 18 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, install for Section U-U : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 149 6

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# @A340 SERVICE BULLETIN
1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Screw Item (142) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud NSA5159-17 Item 151 1 Clamp Item (138) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (142) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp NSA935807-04 Item 150 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 150 6

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# @A340 SERVICE BULLETIN
3 Screw NAS1801-3-9 Item 158 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for detail S : 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Screw NAS1801-3-8 Item 159 NOTE: Install this hardware on the support Item 63 installed previously. 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND for Item 170. NOTE: Install this hardware on the support Item 64 installed previously. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section V-V : 1 Stud NSA5159-27 Item 163 1 Spacer NSA5527-03-01 Item 16 1 Clamp NSA935807-16 Item 134 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 151 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-20 Item 135 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 64 installed previously. 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail T : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail U : 1 Stud NSA5159-17 Item 151 1 Spacer NSA5527-03-02 Item 141 1 Clamp Item (134) Retained at removal 1 Spacer NSA5527-03-05 Item 165 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Screw Item (143) Discard 1 Washer Item (133) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 152 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 29 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud NSA5159-27 Item 163 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Spacer NSA5527-03-15 Item 22 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 30 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 31 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X : 1 Stud NSA5159-10 Item 157 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 153 6

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# @A340 SERVICE BULLETIN
Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 32 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 33 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud NSA5159-17 Item 151 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 154 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 34 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (136) Discard 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 35 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 Or 3 Clamp NSA5516-22ND Item 177 Or 3 Clamp NSA5516-23ND Item 178 And 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-10 Item 167 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 155 6

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# @A340 SERVICE BULLETIN
36 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, along the Frame 39.1 and between Stringers 38 and 37, remove for detail AE : 1 Screw Item (153) Discard 1 Washer Item (142) Discard 1 Clamp Item (135) Retain 37 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 38 and 37, install for detail AF : 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Screw NAS1801-3-9 Item 158 NOTE: Install this hardware on the support Item (88) installed previously. (b) Install the new route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : 1 Remove the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Remove : 2 Fitting-Seal NSA934710T11 Item (184) Discard And 3 Spring NSA934710E20 Item (183) Discard Attached with : 4 Screw NAS1801-3-12 Item (166) Discard 4 Washer ASNA2397-10L Item (14) Discard 4 Nut MS21042-3 Item (170) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 156 6

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# @A340 SERVICE BULLETIN
2 Put in position : FIN 301HF 1 Cable-Electrical Interconnecting 35301-74 Item 174
3 Install : 20 (M) Conduit E0432A04 4 Using supports installed at paragraph 3.C.(20).(a), route the wire No. 3622-0540 spliced at paragraph 3.C.(20).(b).2, from FIN 301HF located on the left hand side at stringer 36 and at Frame 40, through pressure seal 3520VP, to 3520VC located in avionics compartment as shown in Fig. A-FCCAA Sheet 01 and in Fig. A-FBMAA Sheet 01

. NOTE: The route 2SG rejoins route 2S on the right hand side at stringer 46 between Frame 39.1 and Frame 39.2 as shown in Fig. A-FBMAA Sheet 17

. 5 Connect the wire No. 3622-0540 as shown on the wiring diagram, Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines : - 1 and 2 (Refer to Fig. A-FCCAA Sheet 02). NOTE: Use the contacts supplied in : Bundle F9000095227895 6 Install the splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540 supplied in : Bundle F9000095227895 NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C32 item 27. 7 Install the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Install : 2 Fitting-Seal NSA934710T11 Item 184 And 3 Spring NSA934710E20 Item 183 Attach with : 4 Screw NAS1801-3-12 Item 166 4 Washer ASNA2397-10L Item 14 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 157 6

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# @A340 SERVICE BULLETIN
4 Nut MS21042-3 Item 170 8 Identify the splice FIN 3591VS with the identification sleeves and the identification label supplied in : Bundle F9000095227895 9 On the fuselage close to the plugs, identify the FIN 301HF with : 1 Placard F1131031522100

(23) Subtask 364033-831-201-001 - Install the electrical wiring in the FWD cargo compartment Work Zones and Access Panels Zone Access/Work location 130 Work location from Frame 19 to Frame 37.1 Manpower Resources Manhours 7.50 Minimum number of person 2 Subtask elapsed time 3.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 2 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBAAA Installation of the Electrical Wiring in the FWD Cargo Compartment Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 158 6

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# @A340 SERVICE BULLETIN (a) Install the electrical wiring in the FWD cargo compartment 1 Install the electrical wires: Refer to Fig. A-GBAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 2, END 1, Refer to Fig. A-GWAAA Sheet 01 supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBAAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 2 Placard Set F9237000207400 Item 402

(24) Subtask 364033-831-202-001 - Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment Work Zones and Access Panels Zone Access/Work location From 150 Work location Frame 55 To 170 Work location Frame 80 Manpower Resources Manhours 11.00 Minimum number of person 2 Subtask elapsed time 5.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 159 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 402 F9237000207400 4 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBBAA Installation of the Electrical Wiring in the AFT Cargo Compartment Sheet 01 Sheet 02 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01 (a) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 1 Install the electrical wires on 5866VB between Frame 55 thru Frame 80/82: Refer to Fig. A-GBBAA Sheet 01 Refer to Fig. A-GWAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 3, END 1, supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBBAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 4 Placard Set F9237000207400 Item 402
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 160 6

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# @A340 SERVICE BULLETIN
3 Route the electrical wires through the thermal insulator at Frame 80/82: Refer to Fig. A-GBBAA Sheet 02 1 Insulator-Cable Protection ABS0596S006 Item (403) (25) Subtask 364033-831-203-001 - Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills ELECTRICAL References Fig. A-GBCAA Preparation for the Electrical Wiring Installation in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Remove the pressure seal 5208VP from the pressure Frame at Frame 80/82 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03 Remove: 1 Plate F9249011000200 Item (410) Retain 1 Plate F9249011000400 Item (411) Retain 2 Bulkhead Item (415) Discard 8 Screw Item (416) Discard 12 Washer Item (417) Discard 4 Washer Item (418) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 161 6

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# @A340 SERVICE BULLETIN 4 Nut Item (419) Discard or if alternate installed remove: 12 Washer Item (417) Discard 4 Washer Item (418) Discard 4 Nut Item (419) Discard 4 Screw Item (420) Discard 2 Screw Item (423) Discard (b) Remove the lightning protection of the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 08 1 At Frame 90 loosen the electrical receptacle 5215VC, Item (435). Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 4 Screw Item (430) Discard 4 Washer Item (431) Discard 4 Nut Item (432) Discard 2 Disconnect the electrical wires end from the electrical receptacle 5215VC. Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 thru 25 Fig. A-GHBAA Sheet 01 END 2, Line 1 and 2 Remove: 1 Receptacle Item (435) Retain 3 Remove from Frame 91 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 1 Screw Item (314) Discard 1 Washer Item (417) Discard 1 Clamp Item (437) Discard 1 Clip nut Item (353) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 162 6

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# @A340 SERVICE BULLETIN
4 Remove the lightning protection from the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 08 8 Screw Item (314) Discard 12 Washer Item (417) Discard 3 Nut Item (419) Discard 21 Clamp Item (437) Retain 3 Spacer Item (442) Retain 1 Clamp Item (443) Retain 4 Screw Item (444) Discard 1 Clip nut Item (448) Discard or if alternate installed remove: 1 Washer Item (417) Discard 2 Spacer Item (442) Retain 3 Clamp Item (437) Retain 1 Clip nut Item (439) Discard 1 Screw Item (501) Discard (c) Disconnect the electrical wiring 5865VB from the APU overhead leak detection system at Frame 93 Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 09 thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 1 Remove between Frame 92 thru Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 1 Washer Item (417) Discard 1 Nut Item (419) Discard 2 Clamp Item (437) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 163 6

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# @A340 SERVICE BULLETIN 1 Screw Item (449) Discard 1 Spacer Item (464) Retain 1 Screw Item (465) Discard 1 Nut Item (470) Discard 1 Washer Item (471) Discard 2 Remove from Frame 93: Refer to Fig. A-GBCAA Sheet 09 2 Washer Item (417) Discard 4 Spacer Item (442) Retain 2 Clamp Item (437) Retain 2 Clip nut Item (448) Discard 2 Screw Item (501) Discard 3 Remove the electrical splice 5151VSA from Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 and 5 1 Sleeve Item (479) Discard 1 Sleeve Item (480) Discard 1 Splice Item (481) Discard

(26) Subtask 364033-831-205-001 - Install an additional profile in the Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 90 to Frame 91 Stringer 6RH Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 164 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibitive interfay Sealant 09-005 Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018
References Fig. A-GBEAA Installation of the Bracket between FR90 and FR91 Sheet 01
(a) Install an additional profile in the Rear fuselage section 1 Between Frame 90 thru Frame 91, at RH STGR6, temporarily put into position Refer to Fig. A-GBEAA Sheet 01 1 Section Assy F5397083308600 Item 460 2 Transfer drill the holes and open holes to final dimension and install: 1 Nut MS21047L3 Item 461 with: 2 Rivet EN6101AD3-08 Item 462 NOTE: For dimensions refer to the table on Fig. A-GBEAA Sheet 01

. 3 Between Frame 90 thru Frame 91, at RH STGR6, install: 1 Section Assy F5397083308600 Item 460 with: 2 Screw NAS1801-3-8 Item 314 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 165 6

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# @A340 SERVICE BULLETIN
2 Washer NAS1149D0332J Item 463 and protect the surface with: Corrosion Inhibitive interfay Sealant 09-005 As required
and Corrosion Inhibiting, Fillet Consistency 09-016 As required , and seal the edges with: Corrosion Inhibiting low Adhesion Sealant 09-018 As required
(27) Subtask 364033-831-204-001 - Install the electrical wiring in the rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80/82 to Frame 93 Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 10 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 50 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 24 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 166 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 10 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.2 TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 167 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBDAA Installation of the Electrical Wiring in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 (a) Install the electrical wire in the rear fuselage section 1 Install the electrical wire, Item 400, on 5866VB between Frame 80/82 thru Frame 90 Refer to Fig. A-GBDAA Sheet 011 Equipment AssyElectrical F9297000500000 Item 400 Attach the wire with: 2 Placard Set F9237000207400 Item 402 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 50 Tie-Cable NSA935401-05 Item 406 2 Install the electrical wire on 5866VB with the pressure seal 5208VP at Frame 80/82 Refer to Fig. A-GBDAA Sheet 01 thru Fig. A-GBDAA Sheet 03 Install: 1 Plate F9249011000200 Item (410) Retained at removal 1 Plate F9249011000400 Item (411) Retained at removal with: 2 Fitting-Seal NSA934710T14 Item 415 8 Screw NAS1801-3-9 Item 416 12 Washer NAS1149C0332R Item 417 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 168 6

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# @A340 SERVICE BULLETIN
4 Washer NAS1149D0363K Item 418 4 Nut NAS1291C3M Item 419 4 Screw NAS1102-3-10 Item 420 2 Screw NAS1801-3-10 Item 423 NOTE: Alternative to two of the, Item 416. 3 Spring NSA934710E20 Item 485 3 Install the lightning protection of the electrical bundle 5886VB at Frame 90. Attach to the wires on 5866VB leaving thru the 3 way transition at Frame 90 Refer to Fig. A-GBDAA Sheet 04 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 NOTE: Cut the sleeve to the necessary length. 4 Route the wires on 5866VB between Frame 90 thru Frame 91 Refer to Fig. A-GBDAA Sheet 04, Fig. A-GBDAA Sheet 08thru Fig. A-GBDAA Sheet 09 Install:1 Protection SystemLightning F9249016510800 Item 489
with: 1 Washer NAS1149C0332R Item 417 1 Screw NAS1801-3-18 Item 444 1 Clamp AS21919WCH13 Item 350 1 Clamp Item (437) Retained at removal 1 Spacer Item (442) Retained at removal 5 Route the electrical wires: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 08 1 Fitting-Conduit ABS0580A17P Item 492 and install, Item 492, at Frame 90 with: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 169 6

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# @A340 SERVICE BULLETIN
1 Clamp MS21919WCH14 Item 351 2 Nut NAS1291C3M Item 419 1 Strip ASNA0182-4ADL Item 469 2 Screw NAS1801-3-21 Item 493 2 Washer NSA935808C03 Item 494 2 Spacer NSA5527-03-08D Item 496 1 Clamp MS21919WCH12 Item 843 6 Route the electrical wires on 5866VB between Frame 90 thru Frame 91 to connector 5215VC Refer to Fig. A-GBDAA Sheet 04thru Fig. A-GBDAA Sheet 08 Reinstall the connector 5215VC 1 Receptacle Item (435) Retained at removal attached with: 4 Screw NAS1100-04-6 Item 430 4 Washer NAS1149CN416R Item 431 4 Nut MS21042-04 Item 432 and install: 1 Screw NAS1801-3-8 Item 314 1 Washer NAS1149C0332R Item 417 2 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-2 Item 448 or alternative install: 1 Washer NAS1149C0332R Item 417 3 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-1 Item 439
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 170 6

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# @A340 SERVICE BULLETIN 2 Spacer Item (442) Retained at removal 1 Screw NAS1801-3-27 Item 501 and install: 12 Clamp Item (437) Retained at removal 2 Spacer Item (442) Retained at removal 5 Clamp AS21919WCH13 Item 350 8 Washer NAS1149C0332R Item 417 7 Screw NAS1801-3-8 Item 314 1 Screw NAS1801-3-27 Item 501 2 Spacer NSA5527-03-02 Item 320 3 Nut NAS1291C3M Item 419 2 Screw NAS1801-3-18 Item 444 1 Nut NSA5067-3-1 Item 353 7 Route the wire, Item 400, from the 3 way transition, Item 492, to the splice 5410VS and route to the wire 5866VB with: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 081 Protection SystemLightning F9249016013200 Item 4511 Protection SystemLightning F9249016510800 Item 4891 Protection SystemLightning F9249016110900 Item 511 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 0.35 Tubing-Heat-Shrinkable E0126-01L Item 510 NOTE: Cut the sleeve to the necessary length. and install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 171 6

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# @A340 SERVICE BULLETIN
8 Placard Set F9237000207400 Item 402 8 Install the protection, Item 511, at Frame 93 with: 1 Nut ABS0520-07P Item 518 1 Support-Strain Relief ABS0513-09 Item 517 9 Install the electrical wire at Frame 93on 5865VB and 5866VB with: Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 10 thru Fig. AGBDAA Sheet 11 Install: 3 Spacer NSA5527-03-02 Item 320 1 Clamp MS21919WCH8 Item 352 1 Washer NAS1149C0332R Item 417 1 Nut NAS1291C3M Item 419 6 Clamp Item (437) Retained at removal 5 Spacer Item (442) Retained at removal 2 Screw NAS1801-08-8 Item 449 1 Screw NAS1801-3-15 Item 465 1 Strip ASNA0182-4ADL Item 469 3 Nut NAS1291C08M Item 470 5 Washer NAS1149CN816R Item 471 1 Strip-Bonding ASNA0182-3ADL Item 472 2 Screw NAS1801-08-36 Item 475 2 Nut-Clip NSA5066-08-1 Item 476 1 Clamp AS21919WCH07 Item 515 1 Clamp AS21919WCH14 Item 521 1 Screw NAS1801-08-12 Item 528 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 172 6

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# @A340 SERVICE BULLETIN 3 Clamp AS21919WCH02 Item 536 1 Clamp AS21919WCH09 Item 537 for the wire connection install: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481

(28) Subtask 364033-831-206-001 - Remove the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 5.25 Minimum number of person 1 Subtask elapsed time 5.25 Skills ELECTRICAL References Fig. A-GBFAA Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 (a) Remove the sensing elements from the APU bleed air duct in the AFT and Bulk cargo compartments 1 Remove the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBFAA Sheet 01 thru Fig. A-GBFAA Sheet 03 Remove: FIN 27HF 1 Sensing Element 35609-2-255 Item (562) FIN 28HF 1 Sensing Element 35593-2-255 Item (564) FIN 29HF 1 Sensing Element 35593-2-255 Item (566)
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 173 6

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# @A340 SERVICE BULLETIN
FIN 30HF 1 Sensing Element 35609-2-255 Item (563) FIN 31HF 1 Sensing Element 35609-2-255 Item (570) FIN 32HF 1 Sensing Element 35609-2-255 Item (572) attached with: 6 Nut Item (612) Retain 5 Flange Item (592) Discard 15 Sleeve Item (602) Discard 15 Clamp Item (357) Discard 8 Screw Item (408) Retain 8 Spacer Item (609) Discard 16 Clip Nut Item (399) Retain 16 Screw Item (601) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 03 Remove: 1 Connector Item (355) Discard 3 Washer Item (596) Discard

(29) Subtask 364033-831-212-001 - Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead Manpower Resources Manhours 0.75 Minimum number of person 1 Subtask elapsed time 0.75 Skills AIRFRAME

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 174 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBMAA Hole Location and Dimensions for the sensing element Installation in the Sheet Metal Pressure Bulkhead Sheet 01

(a) Drill the hole for the dual loop overheat leak detection in the pressure bulkhead For dimensions refer to Fig. A-GBMAA Sheet 01 1 Drill the additional sensing element hole into the pressure bulkhead Frame 80/82 with a diameter of 13.5mm (0.53in.) (30) Subtask 364033-831-207-001 - Install the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 11.25 Minimum number of person 1 Subtask elapsed time 11.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D10R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 6 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 175 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 602 NSA5539S 152 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 12 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBGAA Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GBNAA Tolerances for the Waviness and Bend in the Electrical Wiring Sheet 01 Sheet 02 (a) Install the sensing elements in the AFT and Bulk cargo compartments Refer to AMM Task 36-22-17-400-801 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 08 Put the angles, Item 592, in position within the given tolerance area, transfer drill the rivet holes to the duct-brackets with the diameter between 3.28 mm and 3.35 mm (0.129 in and 0.132 in) and install: 6 Angle NSA5546-00 Item 592 with: 12 Rivet-Blind NAS1919C04S02U Item 607

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 176 6

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# @A340 SERVICE BULLETIN
2 Install the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 08 For the tolerances for waviness and bend in wires, refer to Fig. A-GBNAA Sheet 01 thru Fig. A-GBNAA Sheet 02

. NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: 2 Sensing Element 35602-2-255 Item 562 2 Sensing Element 35600-2-255 Item 563 2 Sensing Element 35586-2-255 Item 564 2 Sensing Element 35594-2-255 Item 566 2 Sensing Element 35604-2-255 Item 570 1 Sensing Element 35597-2-255 Item 572 1 Sensing Element 35599-3-255 Item 574 with: 1 Connector NSA5549-00 Item 355 22 Clamp NSA5543-00 Item 357 16 Clip Nut Item (399) Retained at removal 6 Screw Item (408) Retained at removal 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0832R Item 597 16 Screw Item (601) Retained at removal 152 Sleeve-Protective NSA5539S Item 602 1 Washer NAS1149C0863R Item 604 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 177 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 6 Nut NSA5542-00 Item 612 6 Nut Item (612) Retained at removal 1 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 07 Install: 1 Placard F3627011520400 Item 356 1 Placard F3627011520600 Item 591 2 Placard F3627011520800 Item 594 1 Placard F3627011522200 Item 593 1 Placard F3627011521000 Item 611 2 Placard F3627011520200 Item 606 1 Placard D3627006026600 Item 57

(31) Subtask 364033-410-003-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 178 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Install : Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (32) Subtask 364033-831-208-001 - Remove the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 2.75 Minimum number of person 1 Subtask elapsed time 2.75 Skills ELECTRICAL References Fig. A-GBHAA Removal of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the sensing elements in the rear fuselage 1 Remove the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBHAA Sheet 01 thru Fig. A-GBHAA Sheet 04 Remove: FIN 33HF 1 Sensing Element 35660-2-310 Item (371) Discard FIN 34HF 1 Sensing Element 35301-75 Item (361) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 179 6

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# @A340 SERVICE BULLETIN
FIN 139HF 1 Sensing Element 35558-2-310 Item (364) Discard FIN 140HF 1 Sensing Element 35636-2-310 Item (366) Discard attached with: 3 Screw Item (601) Discard 35 Screw Item (601) Retain 39 Sleeve Item (602) Discard 6 Screw Item (620) Retain 6 Spacer Item (609) Retain 38 Clamp Item (610) Discard 37 Nut-Clip Item (399) Retain 1 Nut-Clip Item (399) Discard 3 Flange Item (59) Discard 3 Nut Item (612) Retain 2 Clamp Item (621) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBHAA Sheet 01 thru Fig. A-GBHAA Sheet 04 Remove: 1 Connector Item (355) Discard 1 Washer Item (596) Discard 1 Washer Item (604) Discard

(33) Subtask 364033-831-209-001 - Install the sensing elements in the rear fuselage Manpower Resources Manhours 5.75 Minimum number of person 1 Subtask elapsed time 5.75 Skills ELECTRICAL DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 180 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D13R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 40 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 364 35566-2-310 2 ELEMENT 366 35624-2-310 2 ELEMENT 371 35661-2-310 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 398 35659-3-310 1 ELEMENT 405 NSA935401-04 2 TIE 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 2 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 104 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 4 SPACER 610 NSA5538-00 4 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 181 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBJAA Installation of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 (a) Install the sensing elements in the rear fuselage 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 Install: 3 Connection Flanges NSA5545-00 Item 59 with: 6 Rivet-Blind NAS1919C04S02U Item 607 2 Install the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: FIN 359HF 1 Sensing Element 35566-2-310 Item 364 FIN 139HF 1 Sensing Element 35566-2-310 Item 364 FIN 361HF 1 Cable-Electrical Interconnecting 35301-74 Item 360
FIN 34HF 1 Cable-Electrical Interconnecting 35301-75 Item 361
FIN 360HF 1 Sensing Element 35624-2-310 Item 366 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 182 6

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# @A340 SERVICE BULLETIN
FIN 140HF 1 Sensing Element 35624-2-310 Item 366 FIN 358HF 1 Sensing Element 35659-3-310 Item 398 FIN 33HF 1 Sensing Element 35661-2-310 Item 371 with: 1 Connector NSA5549-00 Item 355 1 Washer NAS1149C0832R Item 597 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0863R Item 604 attached with: 37 Nut-Clip Item (399) Retained at removal 35 Screw Item (601) Retained at removal 6 Spacer Item (609) Retained at removal 3 Nut Item (612) Retained at removal 6 Screw Item (620) Retained at removal 2 Clamp Item (621) Retained at removal 2 Screw NAS1801-3-19 Item 313 40 Clamp NSA5543-00 Item 357 12 Clamp AS21919WCH04 Item 372 2 Clamp AS21919WCH10 Item 373 5 Screw NAS1801-3-9 Item 416 2 Spacer NSA5527-03-08D Item 496 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 183 6

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# @A340 SERVICE BULLETIN
104 Sleeve-Protective NSA5539S Item 602 4 Spacer NSA5527-03-01 Item 609 4 Clamp NSA5538-00 Item 610 3 Nut NSA5542-00 Item 612 5 Nut MS21042-3 Item 640 7 Washer NAS1149D0332K Item 682 2 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 Install: 1 Placard F3617052620200 Item 374 1 Placard F3627011521400 Item 392 2 Placard F3627011521600 Item 393 2 Placard F3627011521800 Item 394 2 Tie-Cable NSA935401-04 Item 405 1 Placard F3617052620000 Item 591 1 Placard D3627006026800 Item 608

(34) Subtask 364033-831-210-001 - Install the sleeves at the APU Bleed Air Duct Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 184 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D16R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 375 F3617062400000 1 SLEEVE 376 F3617062400200 1 SLEEVE 377 F3617062400400 1 SLEEVE 378 F3617062400600 1 SLEEVE 379 F3617062400800 1 SLEEVE 380 F3617062401000 1 SLEEVE 381 F3617062401200 1 SLEEVE 382 F3617062401400 1 SLEEVE 384 F3617062401800 1 SLEEVE References Fig. A-GBKAA Installation of the Sleeves at the APU Bleed Air Duct Sheet 01
(a) Install the sleeves at the APU Bleed Air Duct between Frame 80/82 thru Frame 95 Refer to Fig. A-GBKAA Sheet 01 install the sleeves: 1 Sleeve Assy F3617062400000 Item 375 1 Sleeve Assy F3617062400200 Item 376 1 Sleeve Assy F3617062400400 Item 377 1 Sleeve Assy F3617062400600 Item 378 1 Sleeve Assy F3617062400800 Item 379 1 Sleeve Assy F3617062401000 Item 380 1 Sleeve Assy F3617062401200 Item 381 1 Sleeve Assy F3617062401400 Item 382 1 Sleeve Assy F3617062401800 Item 384 NOTE: Make sure that the blowout apertures of the blankets are close to (under) the sensing elements.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 185 6

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# @A340 SERVICE BULLETIN
**CONF 002 (1) Subtask 364033-831-016-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 300 TIE F9000095227895 BUNDLE NSA935401-08 300 TIE NSA935401-13 300 TIE References Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 186 6

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# @A340 SERVICE BULLETIN
References Fig. A-FCBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01 Sheet 02
(a) As shown in Fig. A-FBMAA Sheet 01, install the wire, using spares conduits between Frame 37 and Frame 53.2, as shown on the wiring diagram, Fig. AFCBAA Sheet 01 and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FCBAA Sheet 02) supplied in : Bundle F9000095227895 NOTE: The spares conduits is divided in two parts. The first parts go away from Frame 40 to Frame 47 and the second parts go away from Frame 48 to Frame 53.2 (b) Attach the wires with : 300 Tie-Cable NSA935401-03 Item 169 300 Tie-Cable NSA935401-08 300 Tie-Cable NSA935401-13

(2) Subtask 364033-831-017-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 50 TIE F9000095227895 BUNDLE NSA935401-06 50 TIE NSA935401-13 50 TIE

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 187 6

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# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Fig. A-FCAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove and retain the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wires as shown on the wiring diagram Fig. A-FCAAA Sheet 01, and as given in the Hook-up Chart lines : - 1 thru 5 (Refer to Fig. A-FCAAA Sheet 04). (c) Install the wires as shown on the wiring diagrams, Fig. A-FCAAA Sheet 02and Fig. A-FCAAA Sheet 03and as given in the Hook-up Chart lines : - 9 thru 19 (Refer to Fig. A-FCAAA Sheet 04) supplied in : Bundle F9000095227895 (d) Attach the wires with : 50 Tie-Cable NSA935401-03 Item 169 50 Tie-Cable NSA935401-06 50 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (3) Subtask 364033-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 188 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 02 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 22 Screw Item (20) Discard 32 Washer Item (14) Discard 32 Clamp Item (86) Discard 32 Sleeve Item (13) Discard 5 Screw Item (91) Discard 10 Spacer Item (16) Discard 5 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 97HF 1 Sensing Element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing Element 35624-2-255 Item (2) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(4) Subtask 364033-831-002-001 - Remove the sensing elements and the supports between FR44 and FR51. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 51

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 189 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 03 (Refer to AMM Task 36-22-17-000-801) 18 Screw Item (21) Discard 30 Washer Item (14) Discard 30 Clamp Item (86) Discard 30 Sleeve Item (13) Discard 18 Spacer Item (16) Discard 12 Screw Item (20) Discard 2 Nut Item (15) Discard FIN 99HF 1 Sensing Element 35612-2-255 Item (3) Discard FIN 100HF 1 Sensing Element 35605-2-255 Item (6) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 190 6

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# @A340 SERVICE BULLETIN (5) Subtask 364033-831-003-001 - Remove the sensing elements and the supports between FR51 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 51 to Frame 53.6 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 04 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 18 Screw Item (21) Discard 37 Washer Item (14) Discard 37 Clamp Item (86) Discard 37 Sleeve Item (13) Discard 23 Spacer Item (16) Discard 16 Screw Item (20) Discard 1 Screw Item (93) Discard 1 Spacer Item (18) Discard 2 Screw Item (91) Discard 3 Nut Item (15) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 191 6

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# @A340 SERVICE BULLETIN
FIN 101HF 1 Sensing Element 35603-2-255 Item (4) Discard FIN 102HF 1 Sensing Element 35600-2-255 Item (5) Discard FIN 23HF 1 Sensing Element 35571-2-255 Item (7) Discard 6 Rivet Item (11) Discard 3 Support Item (10) Discard

(6) Subtask 364033-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 05 (Refer to AMM Task 36-22-17-000-801) 19 Screw Item (20) Discard 27 Washer Item (14) Discard 27 Clamp Item (86) Discard 27 Sleeve Item (13) Discard 4 Screw Item (91) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 192 6

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# @A340 SERVICE BULLETIN 12 Spacer Item (16) Discard 4 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 24HF 1 Sensing Element 35580-2-255 Item (8) Discard FIN 25HF 1 Sensing Element 35611-3-255 Item (9) Discard 2 Rivet Item (11) Discard 1 Support Item (10) Discard

(7) Subtask 364033-010-002-001 - If necessary, remove the ducts between FR53.5 and FR53.6 for access. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (112) Retain 1 Duct assy Item (114) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 193 6

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# @A340 SERVICE BULLETIN (8) Subtask 364033-831-005-001 - Drill a new hole in the structure between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required Polyurethane Finnish Paint 16-018 As required References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Drill one hole on the structure between FR53.5 and FR53.6 to a diameter comprised between 13.5mm (0.531in.) Min. and 13.7mm (0.539 in.) Max. as shown on Fig. A-FBCAA

. (b) Do a spotfacing on the structure between FR53.5 and 53.6 to a diameter of 24mm (0.944 in.) with a radius of 2mm (0.078in.) NOTE: Be careful at the depth : 2mm (0.078 in.) Min. and 3mm (0.118 in.) Max. (c) Protect the hole and the spotfacing with : Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 194 6

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# @A340 SERVICE BULLETIN Polyurethane Finnish Paint 16-018 As required (9) Subtask 364033-831-006-001 - Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBFAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 195 6

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# @A340 SERVICE BULLETIN (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBFAA

. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Fig. A-FBFAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required
(e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581571700000 or 1 Blanket-Insulation F2582261900000 becomes 1 Blanket-Insulation F0041196200000 or 1 Blanket-Insulation F2581566600000 becomes 1 Blanket-Insulation F0041196300000 or 1 Blanket-Insulation F2581666600000 becomes 1 Blanket-Insulation F0041196400000 or 1 Blanket-Insulation F2581677800000 becomes 1 Blanket-Insulation F0041196500000 or 1 Blanket-Insulation F2581677900000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 196 6

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# @A340 SERVICE BULLETIN
becomes 1 Blanket-Insulation F0041196600000 or 1 Blanket-Insulation F2582242300000 becomes 1 Blanket-Insulation F0041196700000 (f) Install : Fig. A-FBFAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure, apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (g) Install the insulation blanket. (10) Subtask 364033-410-001-001 - If removed, install the ducts between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 197 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (114) Retained at removal (11) Subtask 364033-010-003-001 - If necessary, remove the ducts between FR43 and FR45 for access. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Remove : (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 198 6

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# @A340 SERVICE BULLETIN (12) Subtask 364033-831-007-001 - Replace the web assy and the half clamp assy at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required
References Fig. A-FBEAA Replacement of the Web Assy at FR44 on the LH side Sheet 01 Sheet 02 (a) Remove : Fig. A-FBEAA 17 Screw Item (119) Retain 17 Washer Item (124) Retain 1 Strip cover assy Item (122) Retain 2 Screw Item (120) Retain 1 Half clamp assy F5331583500000 Item (118) Discard 1 Half clamp assy Item (121) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 199 6

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# @A340 SERVICE BULLETIN 1 Bracket Item (123) Retain 1 Web Assy F5331591000000 Item (117) Discard NOTE: It is not necessary to remove completely the bracket Item (123). (b) Install : Fig. A-FBEAA 1 Web Assy F5331591000200 Item 117 1 Bracket Item (123) Retained at removal 1 Half clamp assy Item (121) Retained at removal 1 Half clamp assy F5331583500200 Item 118 2 Screw Item (120) Retained at removal 1 Strip cover assy Item (122) Retained at removal 17 Washer Item (124) Retained at removal 17 Screw Item (119) Retained at removal NOTE: Install the new web assy with : Corrosion Inhibiting Fillet Consistency 09-016B As required

and Low Adhesion Polysulfide Sealant 09-019B As required (13) Subtask 364033-831-008-001 - Install the new brackets for the routing of the sensing elements at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 200 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBGAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBGAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBGAA

. (c) Install : 1 Support F0041178800000 Item 98 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 201 6

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# @A340 SERVICE BULLETIN Interfay Sealant 09-005A As required (14) Subtask 364033-410-002-001 - If removed, install the ducts between FR43 and FR45. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal (15) Subtask 364033-831-009-001 - Install the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 202 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 203 6

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# @A340 SERVICE BULLETIN
8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 204 6

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# @A340 SERVICE BULLETIN (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

(16) Subtask 364033-831-010-001 - Install the sensing elements and the supports between FR44 and FR50. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 205 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 11 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 3 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 14 BOLT 21 NAS6603-9 9 BOLT 23 NAS6603-16 1 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM References Fig. A-FBJAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46. 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 206 6

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# @A340 SERVICE BULLETIN
9 Spacer NSA5527-03-01 Item 16 3 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 5 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 207 6

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# @A340 SERVICE BULLETIN 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105 24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (17) Subtask 364033-831-011-001 - Install the sensing elements and the supports between FR50 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 208 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 209 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBKAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 306HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 210 6

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# @A340 SERVICE BULLETIN
2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548620000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 211 6

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# @A340 SERVICE BULLETIN
2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (18) Subtask 364033-831-012-001 - Install the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 212 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM 112 35625-2-255 1 SNSGELEM References Fig. A-FBLAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200095 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 213 6

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# @A340 SERVICE BULLETIN
2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 214 6

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# @A340 SERVICE BULLETIN
2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (19) Subtask 364033-010-004-001 - If necessary, remove the ducts between FR39 and FR40 for access. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain 1 Duct assy Item (127) Retain

(20) Subtask 364033-831-013-001 - Install the new supports for the new harness between FR39.1 and FR39.2. Work Zones and Access Panels Zone Access/Work location 190

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 215 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 97 ASNA2050DCJ3215 14 RIVET Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required
References Fig. A-FBNAA Installation of the Supports for the New Harness Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) At FR39.1, remove a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (88) Retain 2 Install : 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (b) At FR39.1, install a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 216 6

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# @A340 SERVICE BULLETIN
1 Put the support Item (88) in position as shown on Fig. A-FBNAA Sheet 03

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item (88). 3 Install : 1 Support Item (88) Retained at removal 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (c) At FR39.2, install a plate between STGR 46 and STGR 47. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (89) Retain 2 Put the plate Item 64 in position as shown on Fig. A-FBNAA Sheet 04

. 3 Drill one hole on the plate Item 64 to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the hole of the structure. 4 Drill three holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the plate Item (64). 5 Install : 1 Plate F5391094700095 Item 64 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (d) At FR39.2, install two supports between STGR46 and STGR48. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Put the supports Item 63 in position as shown on Fig. A-FBNAA Sheet 04

. 2 Drill four holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the supports Item 63. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 217 6

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# @A340 SERVICE BULLETIN
3 Install : 2 Support ASNA2327-3-8 Item 63 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (e) At FR39.1, install a support between STGR 39 and STGR 40. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 05 1 Put the support Item 65 in position as shown on Fig. A-FBNAA Sheet 05

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item 65. 3 Install : 1 Support NSA5456-3-8 Item 65 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (21) Subtask 364033-831-014-001 - Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 18 NSA5527-03-11 1 SPACER 92 NSA57304-643ADL 1 PLATE DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 218 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 155 NSA5516-04ND 1 CLAMP 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 2 CABLE 182 NSA5050-4 1 NUT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F9000095227895 BUNDLE F9100095005595 1 PLACARD References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 (b) Put in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item 175 (c) Install the splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095227895 (d) Identify the splice FIN 3593VS with the identification sleeves and the identification label supplied in : 1 Placard F9100095005595 and Bundle F9000095227895

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 219 6

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# @A340 SERVICE BULLETIN (e) On the fuselage close to the plugs, identify the FIN 309HF and the FIN 310HF with : 1 Placard F1131031521900 and 1 Placard F1131031522000 (f) Identify the wire No. 3622-0543 of the FIN 310HF and the wire No. 3622-0544 of the FIN 309HF with the identification sleeves supplied in : 1 Placard F9100095005595 (g) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard
4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175)
5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175
6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095227895 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 220 6

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# @A340 SERVICE BULLETIN
NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (h) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer NSA5527-03-11 Item 18 1 Clamp NSA5516-04ND Item (155) Retained at removal 1 Clamp NSA5516-04ND Item 155 1 Washer ASNA2397-10L Item 14 1 Screw NAS1801-3-22 Item 168 and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (i) Secure the FIN 310HF : Refer to Fig. A-FBCAA Sheet 04 1 Remove : 1 Nut Discard 2 Install : 1 Plate-Attachment NSA57304-643ADL Item 92 With : 1 Nut NSA5050-4 Item 182 3 Secure the new nut and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (22) Subtask 364033-831-015-001 - Install the new Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 221 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 26.00 Minimum number of person 2 Subtask elapsed time 13.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 4 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 1 CABLE 176 NSA5516-21ND 5 CLAMP 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031522100 1 PLACARD F9000095227895 BUNDLE DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 222 6

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# @A340 SERVICE BULLETIN
References Elec. Std. Practices Manual (ESPM) 20-43-42 Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Install supports of new routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 7 Screw Item (130) Discard 7 Washer Item (131) Discard 7 Clamp Item (150) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 223 6

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# @A340 SERVICE BULLETIN
2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section B-B : 7 Stud NSA5159-17 Item 151 7 Clamp Item (150) Retained at removal 7 Spacer NSA5527-03-08 Item 152 7 Clamp NSA935807-04 Item 150 7 Washer NSA935808-03 Item 131 7 Nut NSA5050-3 Item 154 b For Section C-C : 1 Stud NSA5159-17 Item 151 1 Clamp NSA935807-04 Item 150 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 65 installed previously. 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section F-F : 1 Screw Item (130) Discard 1 Washer Item (131) Discard 1 Clamp Item (150) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 224 6

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# @A340 SERVICE BULLETIN
b For Section G-G : 1 Screw Item (132) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section H-H : 1 Stud NSA5159-17 Item 151 1 Clamp Item (150) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 b For Section J-J : 1 Stud NSA5159-17 Item 151 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Screw Item (136) Discard 2 Washer Item (137) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 225 6

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# @A340 SERVICE BULLETIN 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud NSA5159-17 Item 151 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section K-K : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 226 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section M-M : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 227 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Screw Item (130) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 228 6

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# @A340 SERVICE BULLETIN
11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section P-P : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 229 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section Q-Q : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 230 6

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# @A340 SERVICE BULLETIN 1 Spacer Item (152) Retain 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (135) Retain 1 Spacer Item (152) Discard 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (144) Discard 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section S-S : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 231 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 15 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Screw Item (132) Discard 2 Washer Item (153) Discard 2 Clamp Item (138) Retain 16 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud NSA5159-17 Item 151 2 Clamp Item (138) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 232 6

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# @A340 SERVICE BULLETIN
2 Nut NSA5050-3 Item 154 17 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, remove for Section T-T : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 18 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, install for Section U-U : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Screw Item (142) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 233 6

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# @A340 SERVICE BULLETIN
20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud NSA5159-17 Item 151 1 Clamp Item (138) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (142) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp NSA935807-04 Item 150 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-9 Item 158 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for detail S : 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Screw NAS1801-3-8 Item 159 NOTE: Install this hardware on the support Item 63 installed previously. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 234 6

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# @A340 SERVICE BULLETIN
24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND for Item 170. NOTE: Install this hardware on the support Item 64 installed previously. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section V-V : 1 Stud NSA5159-27 Item 163 1 Spacer NSA5527-03-01 Item 16 1 Clamp NSA935807-16 Item 134 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-20 Item 135 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 64 installed previously.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 235 6

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# @A340 SERVICE BULLETIN
26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail T : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail U : 1 Stud NSA5159-17 Item 151 1 Spacer NSA5527-03-02 Item 141 1 Clamp Item (134) Retained at removal 1 Spacer NSA5527-03-05 Item 165 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Screw Item (143) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 29 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud NSA5159-27 Item 163
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 236 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Spacer NSA5527-03-15 Item 22 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 30 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 31 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X : 1 Stud NSA5159-10 Item 157 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 237 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 32 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 33 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud NSA5159-17 Item 151 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-11 Item 18 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 238 6

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# @A340 SERVICE BULLETIN
34 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (136) Discard 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 35 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 Or 3 Clamp NSA5516-22ND Item 177 Or 3 Clamp NSA5516-23ND Item 178 And 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-10 Item 167 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 36 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, along the Frame 39.1 and between Stringers 38 and 37, remove for detail AE : 1 Screw Item (153) Discard 1 Washer Item (142) Discard 1 Clamp Item (135) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 239 6

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# @A340 SERVICE BULLETIN
37 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 38 and 37, install for detail AF : 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Screw NAS1801-3-9 Item 158 NOTE: Install this hardware on the support Item (88) installed previously. (b) Install the new route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : 1 Remove the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Remove : 2 Fitting-Seal NSA934710T11 Item (184) Discard And 3 Spring NSA934710E20 Item (183) Discard Attached with : 4 Screw NAS1801-3-12 Item (166) Discard 4 Washer ASNA2397-10L Item (14) Discard 4 Nut MS21042-3 Item (170) Discard 2 Put in position : FIN 301HF 1 Cable-Electrical Interconnecting 35301-74 Item 174
3 Install : 20 (M) Conduit E0432A04

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 240 6

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# @A340 SERVICE BULLETIN
4 Using supports installed at paragraph 3.C.(20).(a), route the wire No. 3622-0540 spliced at paragraph 3.C.(20).(b).2, from FIN 301HF located on the left hand side at stringer 36 and at Frame 40, through pressure seal 3520VP, to 3520VC located in avionics compartment as shown in Fig. A-FCCAA Sheet 01 and in Fig. A-FBMAA Sheet 01

. NOTE: The route 2SG rejoins route 2S on the right hand side at stringer 46 between Frame 39.1 and Frame 39.2 as shown in Fig. A-FBMAA Sheet 17

. 5 Connect the wire No. 3622-0540 as shown on the wiring diagram, Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines : - 1 and 2 (Refer to Fig. A-FCCAA Sheet 02). NOTE: Use the contacts supplied in : Bundle F9000095227895 6 Install the splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540 supplied in : Bundle F9000095227895 NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C32 item 27. 7 Install the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Install : 2 Fitting-Seal NSA934710T11 Item 184 And 3 Spring NSA934710E20 Item 183 Attach with : 4 Screw NAS1801-3-12 Item 166 4 Washer ASNA2397-10L Item 14 4 Nut MS21042-3 Item 170 8 Identify the splice FIN 3591VS with the identification sleeves and the identification label supplied in : Bundle F9000095227895

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 241 6

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# @A340 SERVICE BULLETIN
9 On the fuselage close to the plugs, identify the FIN 301HF with : 1 Placard F1131031522100

(23) Subtask 364033-831-201-003 - Install the electrical wiring in the FWD cargo compartment Work Zones and Access Panels Zone Access/Work location 130 Work location from Frame 19 to Frame 37.1 Manpower Resources Manhours 7.50 Minimum number of person 2 Subtask elapsed time 3.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 2 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBAAB Installation of the Electrical Wiring in the FWD Cargo Compartment Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01 (a) Install the electrical wiring in the FWD cargo compartment 1 Install the electrical wires: Refer to Fig. A-GBAAB Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 2, END 1, Refer to Fig. A-GWAAA Sheet 01 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 242 6

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# @A340 SERVICE BULLETIN supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBAAB Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 2 Placard Set F9237000207400 Item 402

(24) Subtask 364033-831-202-001 - Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment Work Zones and Access Panels Zone Access/Work location From 150 Work location Frame 55 To 170 Work location Frame 80 Manpower Resources Manhours 11.00 Minimum number of person 2 Subtask elapsed time 5.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 4 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 243 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBBAA Installation of the Electrical Wiring in the AFT Cargo Compartment Sheet 01 Sheet 02 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01 (a) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 1 Install the electrical wires on 5866VB between Frame 55 thru Frame 80/82: Refer to Fig. A-GBBAA Sheet 01 Refer to Fig. A-GWAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 3, END 1, supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBBAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 4 Placard Set F9237000207400 Item 402 3 Route the electrical wires through the thermal insulator at Frame 80/82: Refer to Fig. A-GBBAA Sheet 02 1 Insulator-Cable Protection ABS0596S006 Item (403)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 244 6

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# @A340 SERVICE BULLETIN (25) Subtask 364033-831-203-001 - Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills ELECTRICAL References Fig. A-GBCAA Preparation for the Electrical Wiring Installation in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Remove the pressure seal 5208VP from the pressure Frame at Frame 80/82 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03 Remove: 1 Plate F9249011000200 Item (410) Retain 1 Plate F9249011000400 Item (411) Retain 2 Bulkhead Item (415) Discard 8 Screw Item (416) Discard 12 Washer Item (417) Discard 4 Washer Item (418) Discard 4 Nut Item (419) Discard or if alternate installed remove: 12 Washer Item (417) Discard 4 Washer Item (418) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 245 6

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# @A340 SERVICE BULLETIN 4 Nut Item (419) Discard 4 Screw Item (420) Discard 2 Screw Item (423) Discard (b) Remove the lightning protection of the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 08 1 At Frame 90 loosen the electrical receptacle 5215VC, Item (435). Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 4 Screw Item (430) Discard 4 Washer Item (431) Discard 4 Nut Item (432) Discard 2 Disconnect the electrical wires end from the electrical receptacle 5215VC. Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 thru 25 Fig. A-GHBAA Sheet 01 END 2, Line 1 and 2 Remove: 1 Receptacle Item (435) Retain 3 Remove from Frame 91 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 1 Screw Item (314) Discard 1 Washer Item (417) Discard 1 Clamp Item (437) Discard 1 Clip nut Item (353) Discard 4 Remove the lightning protection from the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 08 8 Screw Item (314) Discard 12 Washer Item (417) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 246 6

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# @A340 SERVICE BULLETIN 3 Nut Item (419) Discard 21 Clamp Item (437) Retain 3 Spacer Item (442) Retain 1 Clamp Item (443) Retain 4 Screw Item (444) Discard 1 Clip nut Item (448) Discard or if alternate installed remove: 1 Washer Item (417) Discard 2 Spacer Item (442) Retain 3 Clamp Item (437) Retain 1 Clip nut Item (439) Discard 1 Screw Item (501) Discard (c) Disconnect the electrical wiring 5865VB from the APU overhead leak detection system at Frame 93 Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 09 thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 1 Remove between Frame 92 thru Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 1 Washer Item (417) Discard 1 Nut Item (419) Discard 2 Clamp Item (437) Retain 1 Screw Item (449) Discard 1 Spacer Item (464) Retain 1 Screw Item (465) Discard 1 Nut Item (470) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 247 6

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# @A340 SERVICE BULLETIN 1 Washer Item (471) Discard 2 Remove from Frame 93: Refer to Fig. A-GBCAA Sheet 09 2 Washer Item (417) Discard 4 Spacer Item (442) Retain 2 Clamp Item (437) Retain 2 Clip nut Item (448) Discard 2 Screw Item (501) Discard 3 Remove the electrical splice 5151VSA from Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 and 5 1 Sleeve Item (479) Discard 1 Sleeve Item (480) Discard 1 Splice Item (481) Discard

(26) Subtask 364033-831-205-001 - Install an additional profile in the Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 90 to Frame 91 Stringer 6RH Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 248 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibitive interfay Sealant 09-005 Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018
References Fig. A-GBEAA Installation of the Bracket between FR90 and FR91 Sheet 01
(a) Install an additional profile in the Rear fuselage section 1 Between Frame 90 thru Frame 91, at RH STGR6, temporarily put into position Refer to Fig. A-GBEAA Sheet 01 1 Section Assy F5397083308600 Item 460 2 Transfer drill the holes and open holes to final dimension and install: 1 Nut MS21047L3 Item 461 with: 2 Rivet EN6101AD3-08 Item 462 NOTE: For dimensions refer to the table on Fig. A-GBEAA Sheet 01

. 3 Between Frame 90 thru Frame 91, at RH STGR6, install: 1 Section Assy F5397083308600 Item 460 with: 2 Screw NAS1801-3-8 Item 314 2 Washer NAS1149D0332J Item 463 and protect the surface with:

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 249 6

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# @A340 SERVICE BULLETIN
Corrosion Inhibitive interfay Sealant 09-005 As required
and Corrosion Inhibiting, Fillet Consistency 09-016 As required , and seal the edges with: Corrosion Inhibiting low Adhesion Sealant 09-018 As required
(27) Subtask 364033-831-204-001 - Install the electrical wiring in the rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80/82 to Frame 93 Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 10 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 50 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 24 WASHER 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 10 NUT 420 NAS1102-3-10 4 SCREW DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 250 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 423 NAS1801-3-10 2 SCREW 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.2 TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 251 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBDAA Installation of the Electrical Wiring in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 (a) Install the electrical wire in the rear fuselage section 1 Install the electrical wire, Item 400, on 5866VB between Frame 80/82 thru Frame 90 Refer to Fig. A-GBDAA Sheet 011 Equipment AssyElectrical F9297000500000 Item 400 Attach the wire with: 2 Placard Set F9237000207400 Item 402 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 50 Tie-Cable NSA935401-05 Item 406 2 Install the electrical wire on 5866VB with the pressure seal 5208VP at Frame 80/82 Refer to Fig. A-GBDAA Sheet 01 thru Fig. A-GBDAA Sheet 03 Install: 1 Plate F9249011000200 Item (410) Retained at removal 1 Plate F9249011000400 Item (411) Retained at removal with: 2 Fitting-Seal NSA934710T14 Item 415 8 Screw NAS1801-3-9 Item 416 12 Washer NAS1149C0332R Item 417 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 252 6

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# @A340 SERVICE BULLETIN
4 Washer NAS1149D0363K Item 418 4 Nut NAS1291C3M Item 419 4 Screw NAS1102-3-10 Item 420 2 Screw NAS1801-3-10 Item 423 NOTE: Alternative to two of the, Item 416. 3 Spring NSA934710E20 Item 485 3 Install the lightning protection of the electrical bundle 5886VB at Frame 90. Attach to the wires on 5866VB leaving thru the 3 way transition at Frame 90 Refer to Fig. A-GBDAA Sheet 04 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 NOTE: Cut the sleeve to the necessary length. 4 Route the wires on 5866VB between Frame 90 thru Frame 91 Refer to Fig. A-GBDAA Sheet 04, Fig. A-GBDAA Sheet 08thru Fig. A-GBDAA Sheet 09 Install:1 Protection SystemLightning F9249016510800 Item 489
with: 1 Washer NAS1149C0332R Item 417 1 Screw NAS1801-3-18 Item 444 1 Clamp AS21919WCH13 Item 350 1 Clamp Item (437) Retained at removal 1 Spacer Item (442) Retained at removal 5 Route the electrical wires: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 08 1 Fitting-Conduit ABS0580A17P Item 492 and install, Item 492, at Frame 90 with: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 253 6

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# @A340 SERVICE BULLETIN
1 Clamp MS21919WCH14 Item 351 2 Nut NAS1291C3M Item 419 1 Strip ASNA0182-4ADL Item 469 2 Screw NAS1801-3-21 Item 493 2 Washer NSA935808C03 Item 494 2 Spacer NSA5527-03-08D Item 496 1 Clamp MS21919WCH12 Item 843 6 Route the electrical wires on 5866VB between Frame 90 thru Frame 91 to connector 5215VC Refer to Fig. A-GBDAA Sheet 04thru Fig. A-GBDAA Sheet 08 Reinstall the connector 5215VC 1 Receptacle Item (435) Retained at removal attached with: 4 Screw NAS1100-04-6 Item 430 4 Washer NAS1149CN416R Item 431 4 Nut MS21042-04 Item 432 and install: 1 Screw NAS1801-3-8 Item 314 1 Washer NAS1149C0332R Item 417 2 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-2 Item 448 or alternative install: 1 Washer NAS1149C0332R Item 417 3 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-1 Item 439
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 254 6

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# @A340 SERVICE BULLETIN 2 Spacer Item (442) Retained at removal 1 Screw NAS1801-3-27 Item 501 and install: 12 Clamp Item (437) Retained at removal 2 Spacer Item (442) Retained at removal 5 Clamp AS21919WCH13 Item 350 8 Washer NAS1149C0332R Item 417 7 Screw NAS1801-3-8 Item 314 1 Screw NAS1801-3-27 Item 501 2 Spacer NSA5527-03-02 Item 320 3 Nut NAS1291C3M Item 419 2 Screw NAS1801-3-18 Item 444 1 Nut NSA5067-3-1 Item 353 7 Route the wire, Item 400, from the 3 way transition, Item 492, to the splice 5410VS and route to the wire 5866VB with: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 081 Protection SystemLightning F9249016013200 Item 4511 Protection SystemLightning F9249016510800 Item 4891 Protection SystemLightning F9249016110900 Item 511 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 0.35 Tubing-Heat-Shrinkable E0126-01L Item 510 NOTE: Cut the sleeve to the necessary length. and install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 255 6

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# @A340 SERVICE BULLETIN
8 Placard Set F9237000207400 Item 402 8 Install the protection, Item 511, at Frame 93 with: 1 Nut ABS0520-07P Item 518 1 Support-Strain Relief ABS0513-09 Item 517 9 Install the electrical wire at Frame 93on 5865VB and 5866VB with: Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 10 thru Fig. AGBDAA Sheet 11 Install: 3 Spacer NSA5527-03-02 Item 320 1 Clamp MS21919WCH8 Item 352 1 Washer NAS1149C0332R Item 417 1 Nut NAS1291C3M Item 419 6 Clamp Item (437) Retained at removal 5 Spacer Item (442) Retained at removal 2 Screw NAS1801-08-8 Item 449 1 Screw NAS1801-3-15 Item 465 1 Strip ASNA0182-4ADL Item 469 3 Nut NAS1291C08M Item 470 5 Washer NAS1149CN816R Item 471 1 Strip-Bonding ASNA0182-3ADL Item 472 2 Screw NAS1801-08-36 Item 475 2 Nut-Clip NSA5066-08-1 Item 476 1 Clamp AS21919WCH07 Item 515 1 Clamp AS21919WCH14 Item 521 1 Screw NAS1801-08-12 Item 528 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 256 6

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# @A340 SERVICE BULLETIN 3 Clamp AS21919WCH02 Item 536 1 Clamp AS21919WCH09 Item 537 for the wire connection install: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481

(28) Subtask 364033-831-206-002 - Remove the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 5.25 Minimum number of person 1 Subtask elapsed time 5.25 Skills ELECTRICAL References Fig. A-GBFAB Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 (a) Remove the sensing elements in the AFT and Bulk cargo compartments 1 Remove the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBFAB Sheet 01 thru Fig. A-GBFAB Sheet 03 Remove: FIN 26HF 1 Sensing Element 35593-2-255 Item (358) FIN 27HF 1 Sensing Element 35609-2-255 Item (562) FIN 28HF 1 Sensing Element 35593-2-255 Item (564) FIN 29HF 1 Sensing Element 35593-2-255 Item (566) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 257 6

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# @A340 SERVICE BULLETIN
FIN 30HF 1 Sensing Element 35609-2-255 Item (563) FIN 31HF 1 Sensing Element 35609-2-255 Item (570) FIN 32HF 1 Sensing Element 35609-2-255 Item (572) attached with: 7 Nut Item (599) Retain 7 Flange Item (592) Discard 17 Sleeve Item (602) Discard 17 Clamp Item (357) Discard 10 Screw Item (620) Retain 10 Spacer Item (609) Discard 16 Clip Nut Item (399) Retain 16 Screw Item (601) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 03 Remove: 1 Connector Item (355) Discard 2 Washer Item (596) Discard 1 Washer Item (597) Discard

(29) Subtask 364033-831-212-001 - Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead Manpower Resources Manhours 0.75 Minimum number of person 1 Subtask elapsed time 0.75 Skills AIRFRAME
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 258 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBMAA Hole Location and Dimensions for the sensing element Installation in the Sheet Metal Pressure Bulkhead Sheet 01

(a) Drill the hole for the dual loop overheat leak detection in the pressure bulkhead For dimensions refer to Fig. A-GBMAA Sheet 01 1 Drill the additional sensing element hole into the pressure bulkhead Frame 80/82 with a diameter of 13.5mm (0.53in.) (30) Subtask 364033-831-207-002 - Install the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 11.25 Minimum number of person 1 Subtask elapsed time 11.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D11R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 358 35587-2-255 2 SNSGELEM 389 F3627011520000 1 PLACARD 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 7 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 259 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 176 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 14 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBGAB Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GBNAA Tolerances for the Waviness and Bend in the Electrical Wiring Sheet 01 Sheet 02 (a) Install the sensing elements in the AFT and Bulk cargo compartments Refer to AMM Task 36-22-17-400-801 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 08 Put the angles, Item 592, in position within the given tolerance area, transfer drill the rivet holes to the duct-brackets with the diameter between 3.28 mm and 3.35 mm (0.129 in and 0.132 in) and install: 7 Angle NSA5546-00 Item 592 with: 14 Rivet-Blind NAS1919C04S02U Item 607 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 260 6

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# @A340 SERVICE BULLETIN
2 Install the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 08 For the tolerances for waviness and bend in wires, refer to Fig. A-GBNAA Sheet 01 thru Fig. A-GBNAA Sheet 02

. NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: 2 Sensing Element 35587-2-255 Item 358 2 Sensing Element 35602-2-255 Item 562 2 Sensing Element 35600-2-255 Item 563 2 Sensing Element 35586-2-255 Item 564 2 Sensing Element 35594-2-255 Item 566 2 Sensing Element 35604-2-255 Item 570 1 Sensing Element 35597-2-255 Item 572 1 Sensing Element 35599-3-255 Item 574 with: 1 Connector NSA5549-00 Item 355 22 Clamp NSA5543-00 Item 357 16 Clip Nut Item (399) Retained at removal 6 Screw Item (408) Retained at removal 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0832R Item 597 16 Screw Item (601) Retained at removal 176 Sleeve-Protective NSA5539S Item 602 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 261 6

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# @A340 SERVICE BULLETIN
1 Washer NAS1149C0863R Item 604 1 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 6 Nut NSA5542-00 Item 612 6 Nut Item (599) Retained at removal 1 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(599), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 07 Install: 1 Placard F3627011520400 Item 356 1 Placard F3627011520000 Item 389 1 Placard F3627011520600 Item 591 2 Placard F3627011520800 Item 594 1 Placard F3627011522200 Item 593 1 Placard F3627011521000 Item 611 2 Placard F3627011520200 Item 606 1 Placard D3627006026600 Item 57

(31) Subtask 364033-410-003-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 262 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Install : Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (32) Subtask 364033-831-208-001 - Remove the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 2.75 Minimum number of person 1 Subtask elapsed time 2.75 Skills ELECTRICAL References Fig. A-GBHAA Removal of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the sensing elements in the rear fuselage 1 Remove the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBHAA Sheet 01 thru Fig. A-GBHAA Sheet 04 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 263 6

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# @A340 SERVICE BULLETIN
Remove: FIN 33HF 1 Sensing Element 35660-2-310 Item (371) Discard FIN 34HF 1 Sensing Element 35301-75 Item (361) Discard FIN 139HF 1 Sensing Element 35558-2-310 Item (364) Discard FIN 140HF 1 Sensing Element 35636-2-310 Item (366) Discard attached with: 3 Screw Item (601) Discard 35 Screw Item (601) Retain 39 Sleeve Item (602) Discard 6 Screw Item (620) Retain 6 Spacer Item (609) Retain 38 Clamp Item (610) Discard 37 Nut-Clip Item (399) Retain 1 Nut-Clip Item (399) Discard 3 Flange Item (59) Discard 3 Nut Item (612) Retain 2 Clamp Item (621) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBHAA Sheet 01 thru Fig. A-GBHAA Sheet 04 Remove: 1 Connector Item (355) Discard 1 Washer Item (596) Discard 1 Washer Item (604) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 264 6

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# @A340 SERVICE BULLETIN (33) Subtask 364033-831-209-001 - Install the sensing elements in the rear fuselage Manpower Resources Manhours 5.75 Minimum number of person 1 Subtask elapsed time 5.75 Skills ELECTRICAL Material necessary to do the job Kit 364033D13R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 40 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 364 35566-2-310 2 ELEMENT 366 35624-2-310 2 ELEMENT 371 35661-2-310 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 398 35659-3-310 1 ELEMENT 405 NSA935401-04 2 TIE 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 2 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 104 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 4 SPACER 610 NSA5538-00 4 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 265 6

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# @A340 SERVICE BULLETIN
Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Fig. A-GBJAA Installation of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 (a) Install the sensing elements in the rear fuselage 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 Install: 3 Connection Flanges NSA5545-00 Item 59 with: 6 Rivet-Blind NAS1919C04S02U Item 607 2 Install the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: FIN 359HF 1 Sensing Element 35566-2-310 Item 364 FIN 139HF 1 Sensing Element 35566-2-310 Item 364 FIN 361HF 1 Cable-Electrical Interconnecting 35301-74 Item 360

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 266 6

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# @A340 SERVICE BULLETIN
FIN 34HF 1 Cable-Electrical Interconnecting 35301-75 Item 361
FIN 360HF 1 Sensing Element 35624-2-310 Item 366 FIN 140HF 1 Sensing Element 35624-2-310 Item 366 FIN 358HF 1 Sensing Element 35659-3-310 Item 398 FIN 33HF 1 Sensing Element 35661-2-310 Item 371 with: 1 Connector NSA5549-00 Item 355 1 Washer NAS1149C0832R Item 597 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0863R Item 604 attached with: 37 Nut-Clip Item (399) Retained at removal 35 Screw Item (601) Retained at removal 6 Spacer Item (609) Retained at removal 3 Nut Item (612) Retained at removal 6 Screw Item (620) Retained at removal 2 Clamp Item (621) Retained at removal 2 Screw NAS1801-3-19 Item 313 40 Clamp NSA5543-00 Item 357
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 267 6

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# @A340 SERVICE BULLETIN 12 Clamp AS21919WCH04 Item 372 2 Clamp AS21919WCH10 Item 373 5 Screw NAS1801-3-9 Item 416 2 Spacer NSA5527-03-08D Item 496 104 Sleeve-Protective NSA5539S Item 602 4 Spacer NSA5527-03-01 Item 609 4 Clamp NSA5538-00 Item 610 3 Nut NSA5542-00 Item 612 5 Nut MS21042-3 Item 640 7 Washer NAS1149D0332K Item 682 2 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAA Sheet 01 thru Fig. A-GBJAA Sheet 08 Install: 1 Placard F3617052620200 Item 374 1 Placard F3627011521400 Item 392 2 Placard F3627011521600 Item 393 2 Placard F3627011521800 Item 394 2 Tie-Cable NSA935401-04 Item 405 1 Placard F3617052620000 Item 591 1 Placard D3627006026800 Item 608

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 268 6

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# @A340 SERVICE BULLETIN (34) Subtask 364033-831-210-001 - Install the sleeves at the APU Bleed Air Duct Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D16R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 375 F3617062400000 1 SLEEVE 376 F3617062400200 1 SLEEVE 377 F3617062400400 1 SLEEVE 378 F3617062400600 1 SLEEVE 379 F3617062400800 1 SLEEVE 380 F3617062401000 1 SLEEVE 381 F3617062401200 1 SLEEVE 382 F3617062401400 1 SLEEVE 384 F3617062401800 1 SLEEVE References Fig. A-GBKAA Installation of the Sleeves at the APU Bleed Air Duct Sheet 01
(a) Install the sleeves at the APU Bleed Air Duct between Frame 80/82 thru Frame 95 Refer to Fig. A-GBKAA Sheet 01 install the sleeves: 1 Sleeve Assy F3617062400000 Item 375 1 Sleeve Assy F3617062400200 Item 376 1 Sleeve Assy F3617062400400 Item 377 1 Sleeve Assy F3617062400600 Item 378 1 Sleeve Assy F3617062400800 Item 379 1 Sleeve Assy F3617062401000 Item 380 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 269 6

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# @A340 SERVICE BULLETIN 1 Sleeve Assy F3617062401200 Item 381 1 Sleeve Assy F3617062401400 Item 382 1 Sleeve Assy F3617062401800 Item 384 NOTE: Make sure that the blowout apertures of the blankets are close to (under) the sensing elements. **CONF 003 (1) Subtask 364033-831-016-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 300 TIE F9000095227895 BUNDLE NSA935401-08 300 TIE NSA935401-13 300 TIE

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 270 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01 Sheet 02
(a) As shown in Fig. A-FBMAA Sheet 01, install the wire, using spares conduits between Frame 37 and Frame 53.2, as shown on the wiring diagram, Fig. AFCBAA Sheet 01 and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FCBAA Sheet 02) supplied in : Bundle F9000095227895 NOTE: The spares conduits is divided in two parts. The first parts go away from Frame 40 to Frame 47 and the second parts go away from Frame 48 to Frame 53.2 (b) Attach the wires with : 300 Tie-Cable NSA935401-03 Item 169 300 Tie-Cable NSA935401-08 300 Tie-Cable NSA935401-13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 271 6

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# @A340 SERVICE BULLETIN (2) Subtask 364033-831-017-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 50 TIE F9000095227895 BUNDLE NSA935401-06 50 TIE NSA935401-13 50 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Fig. A-FCAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove and retain the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wires as shown on the wiring diagram Fig. A-FCAAA Sheet 01, and as given in the Hook-up Chart lines : - 1 thru 5 (Refer to Fig. A-FCAAA Sheet 04). (c) Install the wires as shown on the wiring diagrams, Fig. A-FCAAA Sheet 02and Fig. A-FCAAA Sheet 03and as given in the Hook-up Chart lines : - 9 thru 19 (Refer to Fig. A-FCAAA Sheet 04) supplied in : Bundle F9000095227895 (d) Attach the wires with : 50 Tie-Cable NSA935401-03 Item 169 50 Tie-Cable NSA935401-06 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 272 6

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# @A340 SERVICE BULLETIN
50 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (3) Subtask 364033-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 02 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 22 Screw Item (20) Discard 32 Washer Item (14) Discard 32 Clamp Item (86) Discard 32 Sleeve Item (13) Discard 5 Screw Item (91) Discard 10 Spacer Item (16) Discard 5 Screw Item (21) Discard 2 Nut Item (15) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 273 6

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# @A340 SERVICE BULLETIN
FIN 97HF 1 Sensing Element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing Element 35624-2-255 Item (2) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(4) Subtask 364033-831-002-001 - Remove the sensing elements and the supports between FR44 and FR51. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 51 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 03 (Refer to AMM Task 36-22-17-000-801) 18 Screw Item (21) Discard 30 Washer Item (14) Discard 30 Clamp Item (86) Discard 30 Sleeve Item (13) Discard 18 Spacer Item (16) Discard 12 Screw Item (20) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 274 6

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# @A340 SERVICE BULLETIN 2 Nut Item (15) Discard FIN 99HF 1 Sensing Element 35612-2-255 Item (3) Discard FIN 100HF 1 Sensing Element 35605-2-255 Item (6) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(5) Subtask 364033-831-003-001 - Remove the sensing elements and the supports between FR51 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 51 to Frame 53.6 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 04 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 18 Screw Item (21) Discard 37 Washer Item (14) Discard 37 Clamp Item (86) Discard 37 Sleeve Item (13) Discard 23 Spacer Item (16) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 275 6

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# @A340 SERVICE BULLETIN 16 Screw Item (20) Discard 1 Screw Item (93) Discard 1 Spacer Item (18) Discard 2 Screw Item (91) Discard 3 Nut Item (15) Discard FIN 101HF 1 Sensing Element 35603-2-255 Item (4) Discard FIN 102HF 1 Sensing Element 35600-2-255 Item (5) Discard FIN 23HF 1 Sensing Element 35571-2-255 Item (7) Discard 6 Rivet Item (11) Discard 3 Support Item (10) Discard

(6) Subtask 364033-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 05 (Refer to AMM Task 36-22-17-000-801) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 276 6

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# @A340 SERVICE BULLETIN 19 Screw Item (20) Discard 27 Washer Item (14) Discard 27 Clamp Item (86) Discard 27 Sleeve Item (13) Discard 4 Screw Item (91) Discard 12 Spacer Item (16) Discard 4 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 24HF 1 Sensing Element 35580-2-255 Item (8) Discard FIN 25HF 1 Sensing Element 35611-3-255 Item (9) Discard 2 Rivet Item (11) Discard 1 Support Item (10) Discard

(7) Subtask 364033-010-002-001 - If necessary, remove the ducts between FR53.5 and FR53.6 for access. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 277 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (112) Retain 1 Duct assy Item (114) Retain

(8) Subtask 364033-831-005-001 - Drill a new hole in the structure between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required Polyurethane Finnish Paint 16-018 As required References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Drill one hole on the structure between FR53.5 and FR53.6 to a diameter comprised between 13.5mm (0.531in.) Min. and 13.7mm (0.539 in.) Max. as shown on Fig. A-FBCAA

.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 278 6

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# @A340 SERVICE BULLETIN (b) Do a spotfacing on the structure between FR53.5 and 53.6 to a diameter of 24mm (0.944 in.) with a radius of 2mm (0.078in.) NOTE: Be careful at the depth : 2mm (0.078 in.) Min. and 3mm (0.118 in.) Max. (c) Protect the hole and the spotfacing with : Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
Polyurethane Finnish Paint 16-018 As required (9) Subtask 364033-831-006-001 - Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 279 6

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# @A340 SERVICE BULLETIN
Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBFAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02 (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBFAA

. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Fig. A-FBFAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required
(e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581571700000 or 1 Blanket-Insulation F2582261900000 becomes 1 Blanket-Insulation F0041196200000 or 1 Blanket-Insulation F2581566600000 becomes 1 Blanket-Insulation F0041196300000 or 1 Blanket-Insulation F2581666600000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 280 6

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# @A340 SERVICE BULLETIN
becomes 1 Blanket-Insulation F0041196400000 or 1 Blanket-Insulation F2581677800000 becomes 1 Blanket-Insulation F0041196500000 or 1 Blanket-Insulation F2581677900000 becomes 1 Blanket-Insulation F0041196600000 or 1 Blanket-Insulation F2582242300000 becomes 1 Blanket-Insulation F0041196700000 (f) Install : Fig. A-FBFAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure, apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (g) Install the insulation blanket.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 281 6

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# @A340 SERVICE BULLETIN (10) Subtask 364033-410-001-001 - If removed, install the ducts between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (114) Retained at removal (11) Subtask 364033-010-003-001 - If necessary, remove the ducts between FR43 and FR45 for access. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 282 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Remove : (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(12) Subtask 364033-831-007-001 - Replace the web assy and the half clamp assy at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required
References Fig. A-FBEAA Replacement of the Web Assy at FR44 on the LH side Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 283 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBEAA 17 Screw Item (119) Retain 17 Washer Item (124) Retain 1 Strip cover assy Item (122) Retain 2 Screw Item (120) Retain 1 Half clamp assy F5331583500000 Item (118) Discard 1 Half clamp assy Item (121) Retain 1 Bracket Item (123) Retain 1 Web Assy F5331591000000 Item (117) Discard NOTE: It is not necessary to remove completely the bracket Item (123). (b) Install : Fig. A-FBEAA 1 Web Assy F5331591000200 Item 117 1 Bracket Item (123) Retained at removal 1 Half clamp assy Item (121) Retained at removal 1 Half clamp assy F5331583500200 Item 118 2 Screw Item (120) Retained at removal 1 Strip cover assy Item (122) Retained at removal 17 Washer Item (124) Retained at removal 17 Screw Item (119) Retained at removal NOTE: Install the new web assy with :
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 284 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Fillet Consistency 09-016B As required

and Low Adhesion Polysulfide Sealant 09-019B As required (13) Subtask 364033-831-008-001 - Install the new brackets for the routing of the sensing elements at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBGAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBGAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBGAA

. (c) Install : 1 Support F0041178800000 Item 98 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 285 6

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# @A340 SERVICE BULLETIN 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (14) Subtask 364033-410-002-001 - If removed, install the ducts between FR43 and FR45. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 286 6

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# @A340 SERVICE BULLETIN (15) Subtask 364033-831-009-001 - Install the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 287 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 288 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 289 6

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# @A340 SERVICE BULLETIN (16) Subtask 364033-831-010-001 - Install the sensing elements and the supports between FR44 and FR50. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 11 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 3 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 14 BOLT 21 NAS6603-9 9 BOLT 23 NAS6603-16 1 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 290 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBJAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46. 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 3 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 5 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 291 6

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# @A340 SERVICE BULLETIN (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 292 6

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# @A340 SERVICE BULLETIN
24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (17) Subtask 364033-831-011-001 - Install the sensing elements and the supports between FR50 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 293 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM References Fig. A-FBKAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 294 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 306HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13 2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548620000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 295 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (18) Subtask 364033-831-012-001 - Install the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 296 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM 112 35625-2-255 1 SNSGELEM References Fig. A-FBLAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 297 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200095 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 298 6

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# @A340 SERVICE BULLETIN
3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (19) Subtask 364033-010-004-001 - If necessary, remove the ducts between FR39 and FR40 for access. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 299 6

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# @A340 SERVICE BULLETIN 1 Duct assy Item (127) Retain

(20) Subtask 364033-831-013-001 - Install the new supports for the new harness between FR39.1 and FR39.2. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 97 ASNA2050DCJ3215 14 RIVET Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required
References Fig. A-FBNAA Installation of the Supports for the New Harness Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) At FR39.1, remove a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (88) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 300 6

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# @A340 SERVICE BULLETIN
2 Install : 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (b) At FR39.1, install a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Put the support Item (88) in position as shown on Fig. A-FBNAA Sheet 03

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item (88). 3 Install : 1 Support Item (88) Retained at removal 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (c) At FR39.2, install a plate between STGR 46 and STGR 47. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (89) Retain 2 Put the plate Item 64 in position as shown on Fig. A-FBNAA Sheet 04

. 3 Drill one hole on the plate Item 64 to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the hole of the structure. 4 Drill three holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the plate Item (64). 5 Install : 1 Plate F5391094700095 Item 64 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 301 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Brush Consistency 09-013B As required (d) At FR39.2, install two supports between STGR46 and STGR48. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Put the supports Item 63 in position as shown on Fig. A-FBNAA Sheet 04

. 2 Drill four holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the supports Item 63. 3 Install : 2 Support ASNA2327-3-8 Item 63 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (e) At FR39.1, install a support between STGR 39 and STGR 40. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 05 1 Put the support Item 65 in position as shown on Fig. A-FBNAA Sheet 05

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item 65. 3 Install : 1 Support NSA5456-3-8 Item 65 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (21) Subtask 364033-831-014-001 - Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 302 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 18 NSA5527-03-11 1 SPACER 92 NSA57304-643ADL 1 PLATE 155 NSA5516-04ND 1 CLAMP 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 2 CABLE 182 NSA5050-4 1 NUT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F9000095227895 BUNDLE F9100095005595 1 PLACARD References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 (b) Put in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item 175

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 303 6

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# @A340 SERVICE BULLETIN (c) Install the splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095227895 (d) Identify the splice FIN 3593VS with the identification sleeves and the identification label supplied in : 1 Placard F9100095005595 and Bundle F9000095227895 (e) On the fuselage close to the plugs, identify the FIN 309HF and the FIN 310HF with : 1 Placard F1131031521900 and 1 Placard F1131031522000 (f) Identify the wire No. 3622-0543 of the FIN 310HF and the wire No. 3622-0544 of the FIN 309HF with the identification sleeves supplied in : 1 Placard F9100095005595 (g) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard
4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 304 6

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# @A340 SERVICE BULLETIN
5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175
6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095227895 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (h) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer NSA5527-03-11 Item 18 1 Clamp NSA5516-04ND Item (155) Retained at removal 1 Clamp NSA5516-04ND Item 155 1 Washer ASNA2397-10L Item 14 1 Screw NAS1801-3-22 Item 168 and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (i) Secure the FIN 310HF : Refer to Fig. A-FBCAA Sheet 04 1 Remove : 1 Nut Discard 2 Install : 1 Plate-Attachment NSA57304-643ADL Item 92 With : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 305 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-4 Item 182 3 Secure the new nut and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (22) Subtask 364033-831-015-001 - Install the new Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 26.00 Minimum number of person 2 Subtask elapsed time 13.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 4 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 1 CABLE 176 NSA5516-21ND 5 CLAMP DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 306 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031522100 1 PLACARD F9000095227895 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-42 Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 307 6

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# @A340 SERVICE BULLETIN (a) Install supports of new routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 7 Screw Item (130) Discard 7 Washer Item (131) Discard 7 Clamp Item (150) Retain 2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section B-B : 7 Stud NSA5159-17 Item 151 7 Clamp Item (150) Retained at removal 7 Spacer NSA5527-03-08 Item 152 7 Clamp NSA935807-04 Item 150 7 Washer NSA935808-03 Item 131 7 Nut NSA5050-3 Item 154 b For Section C-C : 1 Stud NSA5159-17 Item 151 1 Clamp NSA935807-04 Item 150 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 65 installed DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 308 6

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# @A340 SERVICE BULLETIN previously. 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section F-F : 1 Screw Item (130) Discard 1 Washer Item (131) Discard 1 Clamp Item (150) Retain b For Section G-G : 1 Screw Item (132) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section H-H : 1 Stud NSA5159-17 Item 151 1 Clamp Item (150) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 b For Section J-J : 1 Stud NSA5159-17 Item 151 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 309 6

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# @A340 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Screw Item (136) Discard 2 Washer Item (137) Discard 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud NSA5159-17 Item 151 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section K-K : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 310 6

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# @A340 SERVICE BULLETIN 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section M-M : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 311 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Screw Item (130) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 312 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section P-P : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 313 6

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# @A340 SERVICE BULLETIN
12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 314 6

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# @A340 SERVICE BULLETIN
13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section Q-Q : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (152) Retain 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (135) Retain 1 Spacer Item (152) Discard 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (144) Discard 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section S-S : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 315 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (134) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 15 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Screw Item (132) Discard 2 Washer Item (153) Discard 2 Clamp Item (138) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 316 6

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# @A340 SERVICE BULLETIN
16 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud NSA5159-17 Item 151 2 Clamp Item (138) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 17 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, remove for Section T-T : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 18 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, install for Section U-U : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 317 6

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# @A340 SERVICE BULLETIN
1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Screw Item (142) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud NSA5159-17 Item 151 1 Clamp Item (138) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (142) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp NSA935807-04 Item 150 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 318 6

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# @A340 SERVICE BULLETIN
3 Screw NAS1801-3-9 Item 158 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for detail S : 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Screw NAS1801-3-8 Item 159 NOTE: Install this hardware on the support Item 63 installed previously. 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND for Item 170. NOTE: Install this hardware on the support Item 64 installed previously. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section V-V : 1 Stud NSA5159-27 Item 163 1 Spacer NSA5527-03-01 Item 16 1 Clamp NSA935807-16 Item 134 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 319 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-20 Item 135 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 64 installed previously. 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail T : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail U : 1 Stud NSA5159-17 Item 151 1 Spacer NSA5527-03-02 Item 141 1 Clamp Item (134) Retained at removal 1 Spacer NSA5527-03-05 Item 165 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Screw Item (143) Discard 1 Washer Item (133) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 320 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 29 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud NSA5159-27 Item 163 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Spacer NSA5527-03-15 Item 22 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 30 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 31 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X : 1 Stud NSA5159-10 Item 157 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 321 6

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# @A340 SERVICE BULLETIN
Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 32 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 33 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud NSA5159-17 Item 151 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 322 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 34 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (136) Discard 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 35 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 Or 3 Clamp NSA5516-22ND Item 177 Or 3 Clamp NSA5516-23ND Item 178 And 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-10 Item 167 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 323 6

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# @A340 SERVICE BULLETIN
36 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, along the Frame 39.1 and between Stringers 38 and 37, remove for detail AE : 1 Screw Item (153) Discard 1 Washer Item (142) Discard 1 Clamp Item (135) Retain 37 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 38 and 37, install for detail AF : 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Screw NAS1801-3-9 Item 158 NOTE: Install this hardware on the support Item (88) installed previously. (b) Install the new route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : 1 Remove the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Remove : 2 Fitting-Seal NSA934710T11 Item (184) Discard And 3 Spring NSA934710E20 Item (183) Discard Attached with : 4 Screw NAS1801-3-12 Item (166) Discard 4 Washer ASNA2397-10L Item (14) Discard 4 Nut MS21042-3 Item (170) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 324 6

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# @A340 SERVICE BULLETIN
2 Put in position : FIN 301HF 1 Cable-Electrical Interconnecting 35301-74 Item 174
3 Install : 20 (M) Conduit E0432A04 4 Using supports installed at paragraph 3.C.(20).(a), route the wire No. 3622-0540 spliced at paragraph 3.C.(20).(b).2, from FIN 301HF located on the left hand side at stringer 36 and at Frame 40, through pressure seal 3520VP, to 3520VC located in avionics compartment as shown in Fig. A-FCCAA Sheet 01 and in Fig. A-FBMAA Sheet 01

. NOTE: The route 2SG rejoins route 2S on the right hand side at stringer 46 between Frame 39.1 and Frame 39.2 as shown in Fig. A-FBMAA Sheet 17

. 5 Connect the wire No. 3622-0540 as shown on the wiring diagram, Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines : - 1 and 2 (Refer to Fig. A-FCCAA Sheet 02). NOTE: Use the contacts supplied in : Bundle F9000095227895 6 Install the splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540 supplied in : Bundle F9000095227895 NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C32 item 27. 7 Install the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Install : 2 Fitting-Seal NSA934710T11 Item 184 And 3 Spring NSA934710E20 Item 183 Attach with : 4 Screw NAS1801-3-12 Item 166 4 Washer ASNA2397-10L Item 14 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 325 6

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# @A340 SERVICE BULLETIN
4 Nut MS21042-3 Item 170 8 Identify the splice FIN 3591VS with the identification sleeves and the identification label supplied in : Bundle F9000095227895 9 On the fuselage close to the plugs, identify the FIN 301HF with : 1 Placard F1131031522100

(23) Subtask 364033-831-201-001 - Install the electrical wiring in the FWD cargo compartment Work Zones and Access Panels Zone Access/Work location 130 Work location from Frame 19 to Frame 37.1 Manpower Resources Manhours 7.50 Minimum number of person 2 Subtask elapsed time 3.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 2 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBAAA Installation of the Electrical Wiring in the FWD Cargo Compartment Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 326 6

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# @A340 SERVICE BULLETIN (a) Install the electrical wiring in the FWD cargo compartment 1 Install the electrical wires: Refer to Fig. A-GBAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 2, END 1, Refer to Fig. A-GWAAA Sheet 01 supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBAAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 2 Placard Set F9237000207400 Item 402

(24) Subtask 364033-831-202-001 - Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment Work Zones and Access Panels Zone Access/Work location From 150 Work location Frame 55 To 170 Work location Frame 80 Manpower Resources Manhours 11.00 Minimum number of person 2 Subtask elapsed time 5.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 327 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 402 F9237000207400 4 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBBAA Installation of the Electrical Wiring in the AFT Cargo Compartment Sheet 01 Sheet 02 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01 (a) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 1 Install the electrical wires on 5866VB between Frame 55 thru Frame 80/82: Refer to Fig. A-GBBAA Sheet 01 Refer to Fig. A-GWAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 3, END 1, supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBBAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 4 Placard Set F9237000207400 Item 402
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 328 6

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# @A340 SERVICE BULLETIN
3 Route the electrical wires through the thermal insulator at Frame 80/82: Refer to Fig. A-GBBAA Sheet 02 1 Insulator-Cable Protection ABS0596S006 Item (403) (25) Subtask 364033-831-203-001 - Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills ELECTRICAL References Fig. A-GBCAA Preparation for the Electrical Wiring Installation in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Remove the pressure seal 5208VP from the pressure Frame at Frame 80/82 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03 Remove: 1 Plate F9249011000200 Item (410) Retain 1 Plate F9249011000400 Item (411) Retain 2 Bulkhead Item (415) Discard 8 Screw Item (416) Discard 12 Washer Item (417) Discard 4 Washer Item (418) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 329 6

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# @A340 SERVICE BULLETIN 4 Nut Item (419) Discard or if alternate installed remove: 12 Washer Item (417) Discard 4 Washer Item (418) Discard 4 Nut Item (419) Discard 4 Screw Item (420) Discard 2 Screw Item (423) Discard (b) Remove the lightning protection of the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 08 1 At Frame 90 loosen the electrical receptacle 5215VC, Item (435). Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 4 Screw Item (430) Discard 4 Washer Item (431) Discard 4 Nut Item (432) Discard 2 Disconnect the electrical wires end from the electrical receptacle 5215VC. Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 thru 25 Fig. A-GHBAA Sheet 01 END 2, Line 1 and 2 Remove: 1 Receptacle Item (435) Retain 3 Remove from Frame 91 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 1 Screw Item (314) Discard 1 Washer Item (417) Discard 1 Clamp Item (437) Discard 1 Clip nut Item (353) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 330 6

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# @A340 SERVICE BULLETIN
4 Remove the lightning protection from the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 08 8 Screw Item (314) Discard 12 Washer Item (417) Discard 3 Nut Item (419) Discard 21 Clamp Item (437) Retain 3 Spacer Item (442) Retain 1 Clamp Item (443) Retain 4 Screw Item (444) Discard 1 Clip nut Item (448) Discard or if alternate installed remove: 1 Washer Item (417) Discard 2 Spacer Item (442) Retain 3 Clamp Item (437) Retain 1 Clip nut Item (439) Discard 1 Screw Item (501) Discard (c) Disconnect the electrical wiring 5865VB from the APU overhead leak detection system at Frame 93 Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 09 thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 1 Remove between Frame 92 thru Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 1 Washer Item (417) Discard 1 Nut Item (419) Discard 2 Clamp Item (437) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 331 6

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# @A340 SERVICE BULLETIN 1 Screw Item (449) Discard 1 Spacer Item (464) Retain 1 Screw Item (465) Discard 1 Nut Item (470) Discard 1 Washer Item (471) Discard 2 Remove from Frame 93: Refer to Fig. A-GBCAA Sheet 09 2 Washer Item (417) Discard 4 Spacer Item (442) Retain 2 Clamp Item (437) Retain 2 Clip nut Item (448) Discard 2 Screw Item (501) Discard 3 Remove the electrical splice 5151VSA from Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 and 5 1 Sleeve Item (479) Discard 1 Sleeve Item (480) Discard 1 Splice Item (481) Discard

(26) Subtask 364033-831-205-001 - Install an additional profile in the Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 90 to Frame 91 Stringer 6RH Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 332 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibitive interfay Sealant 09-005 Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018
References Fig. A-GBEAA Installation of the Bracket between FR90 and FR91 Sheet 01
(a) Install an additional profile in the Rear fuselage section 1 Between Frame 90 thru Frame 91, at RH STGR6, temporarily put into position Refer to Fig. A-GBEAA Sheet 01 1 Section Assy F5397083308600 Item 460 2 Transfer drill the holes and open holes to final dimension and install: 1 Nut MS21047L3 Item 461 with: 2 Rivet EN6101AD3-08 Item 462 NOTE: For dimensions refer to the table on Fig. A-GBEAA Sheet 01

. 3 Between Frame 90 thru Frame 91, at RH STGR6, install: 1 Section Assy F5397083308600 Item 460 with: 2 Screw NAS1801-3-8 Item 314 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 333 6

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# @A340 SERVICE BULLETIN
2 Washer NAS1149D0332J Item 463 and protect the surface with: Corrosion Inhibitive interfay Sealant 09-005 As required
and Corrosion Inhibiting, Fillet Consistency 09-016 As required , and seal the edges with: Corrosion Inhibiting low Adhesion Sealant 09-018 As required
(27) Subtask 364033-831-204-001 - Install the electrical wiring in the rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80/82 to Frame 93 Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 10 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 50 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 24 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 334 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 10 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.2 TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 335 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBDAA Installation of the Electrical Wiring in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 (a) Install the electrical wire in the rear fuselage section 1 Install the electrical wire, Item 400, on 5866VB between Frame 80/82 thru Frame 90 Refer to Fig. A-GBDAA Sheet 011 Equipment AssyElectrical F9297000500000 Item 400 Attach the wire with: 2 Placard Set F9237000207400 Item 402 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 50 Tie-Cable NSA935401-05 Item 406 2 Install the electrical wire on 5866VB with the pressure seal 5208VP at Frame 80/82 Refer to Fig. A-GBDAA Sheet 01 thru Fig. A-GBDAA Sheet 03 Install: 1 Plate F9249011000200 Item (410) Retained at removal 1 Plate F9249011000400 Item (411) Retained at removal with: 2 Fitting-Seal NSA934710T14 Item 415 8 Screw NAS1801-3-9 Item 416 12 Washer NAS1149C0332R Item 417 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 336 6

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# @A340 SERVICE BULLETIN
4 Washer NAS1149D0363K Item 418 4 Nut NAS1291C3M Item 419 4 Screw NAS1102-3-10 Item 420 2 Screw NAS1801-3-10 Item 423 NOTE: Alternative to two of the, Item 416. 3 Spring NSA934710E20 Item 485 3 Install the lightning protection of the electrical bundle 5886VB at Frame 90. Attach to the wires on 5866VB leaving thru the 3 way transition at Frame 90 Refer to Fig. A-GBDAA Sheet 04 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 NOTE: Cut the sleeve to the necessary length. 4 Route the wires on 5866VB between Frame 90 thru Frame 91 Refer to Fig. A-GBDAA Sheet 04, Fig. A-GBDAA Sheet 08thru Fig. A-GBDAA Sheet 09 Install:1 Protection SystemLightning F9249016510800 Item 489
with: 1 Washer NAS1149C0332R Item 417 1 Screw NAS1801-3-18 Item 444 1 Clamp AS21919WCH13 Item 350 1 Clamp Item (437) Retained at removal 1 Spacer Item (442) Retained at removal 5 Route the electrical wires: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 08 1 Fitting-Conduit ABS0580A17P Item 492 and install, Item 492, at Frame 90 with: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 337 6

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# @A340 SERVICE BULLETIN
1 Clamp MS21919WCH14 Item 351 2 Nut NAS1291C3M Item 419 1 Strip ASNA0182-4ADL Item 469 2 Screw NAS1801-3-21 Item 493 2 Washer NSA935808C03 Item 494 2 Spacer NSA5527-03-08D Item 496 1 Clamp MS21919WCH12 Item 843 6 Route the electrical wires on 5866VB between Frame 90 thru Frame 91 to connector 5215VC Refer to Fig. A-GBDAA Sheet 04thru Fig. A-GBDAA Sheet 08 Reinstall the connector 5215VC 1 Receptacle Item (435) Retained at removal attached with: 4 Screw NAS1100-04-6 Item 430 4 Washer NAS1149CN416R Item 431 4 Nut MS21042-04 Item 432 and install: 1 Screw NAS1801-3-8 Item 314 1 Washer NAS1149C0332R Item 417 2 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-2 Item 448 or alternative install: 1 Washer NAS1149C0332R Item 417 3 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-1 Item 439
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 338 6

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# @A340 SERVICE BULLETIN 2 Spacer Item (442) Retained at removal 1 Screw NAS1801-3-27 Item 501 and install: 12 Clamp Item (437) Retained at removal 2 Spacer Item (442) Retained at removal 5 Clamp AS21919WCH13 Item 350 8 Washer NAS1149C0332R Item 417 7 Screw NAS1801-3-8 Item 314 1 Screw NAS1801-3-27 Item 501 2 Spacer NSA5527-03-02 Item 320 3 Nut NAS1291C3M Item 419 2 Screw NAS1801-3-18 Item 444 1 Nut NSA5067-3-1 Item 353 7 Route the wire, Item 400, from the 3 way transition, Item 492, to the splice 5410VS and route to the wire 5866VB with: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 081 Protection SystemLightning F9249016013200 Item 4511 Protection SystemLightning F9249016510800 Item 4891 Protection SystemLightning F9249016110900 Item 511 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 0.35 Tubing-Heat-Shrinkable E0126-01L Item 510 NOTE: Cut the sleeve to the necessary length. and install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 339 6

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# @A340 SERVICE BULLETIN
8 Placard Set F9237000207400 Item 402 8 Install the protection, Item 511, at Frame 93 with: 1 Nut ABS0520-07P Item 518 1 Support-Strain Relief ABS0513-09 Item 517 9 Install the electrical wire at Frame 93on 5865VB and 5866VB with: Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 10 thru Fig. AGBDAA Sheet 11 Install: 3 Spacer NSA5527-03-02 Item 320 1 Clamp MS21919WCH8 Item 352 1 Washer NAS1149C0332R Item 417 1 Nut NAS1291C3M Item 419 6 Clamp Item (437) Retained at removal 5 Spacer Item (442) Retained at removal 2 Screw NAS1801-08-8 Item 449 1 Screw NAS1801-3-15 Item 465 1 Strip ASNA0182-4ADL Item 469 3 Nut NAS1291C08M Item 470 5 Washer NAS1149CN816R Item 471 1 Strip-Bonding ASNA0182-3ADL Item 472 2 Screw NAS1801-08-36 Item 475 2 Nut-Clip NSA5066-08-1 Item 476 1 Clamp AS21919WCH07 Item 515 1 Clamp AS21919WCH14 Item 521 1 Screw NAS1801-08-12 Item 528 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 340 6

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# @A340 SERVICE BULLETIN 3 Clamp AS21919WCH02 Item 536 1 Clamp AS21919WCH09 Item 537 for the wire connection install: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481

(28) Subtask 364033-831-206-001 - Remove the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 5.25 Minimum number of person 1 Subtask elapsed time 5.25 Skills ELECTRICAL References Fig. A-GBFAA Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 (a) Remove the sensing elements from the APU bleed air duct in the AFT and Bulk cargo compartments 1 Remove the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBFAA Sheet 01 thru Fig. A-GBFAA Sheet 03 Remove: FIN 27HF 1 Sensing Element 35609-2-255 Item (562) FIN 28HF 1 Sensing Element 35593-2-255 Item (564) FIN 29HF 1 Sensing Element 35593-2-255 Item (566)
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 341 6

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# @A340 SERVICE BULLETIN
FIN 30HF 1 Sensing Element 35609-2-255 Item (563) FIN 31HF 1 Sensing Element 35609-2-255 Item (570) FIN 32HF 1 Sensing Element 35609-2-255 Item (572) attached with: 6 Nut Item (612) Retain 5 Flange Item (592) Discard 15 Sleeve Item (602) Discard 15 Clamp Item (357) Discard 8 Screw Item (408) Retain 8 Spacer Item (609) Discard 16 Clip Nut Item (399) Retain 16 Screw Item (601) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBFAA Sheet 01 and Fig. A-GBFAA Sheet 03 Remove: 1 Connector Item (355) Discard 3 Washer Item (596) Discard

(29) Subtask 364033-831-212-001 - Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead Manpower Resources Manhours 0.75 Minimum number of person 1 Subtask elapsed time 0.75 Skills AIRFRAME

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 342 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBMAA Hole Location and Dimensions for the sensing element Installation in the Sheet Metal Pressure Bulkhead Sheet 01

(a) Drill the hole for the dual loop overheat leak detection in the pressure bulkhead For dimensions refer to Fig. A-GBMAA Sheet 01 1 Drill the additional sensing element hole into the pressure bulkhead Frame 80/82 with a diameter of 13.5mm (0.53in.) (30) Subtask 364033-831-207-001 - Install the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 11.25 Minimum number of person 1 Subtask elapsed time 11.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D10R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 6 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 343 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 602 NSA5539S 152 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 12 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBGAA Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Fig. A-GBNAA Tolerances for the Waviness and Bend in the Electrical Wiring Sheet 01 Sheet 02 (a) Install the sensing elements in the AFT and Bulk cargo compartments Refer to AMM Task 36-22-17-400-801 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 08 Put the angles, Item 592, in position within the given tolerance area, transfer drill the rivet holes to the duct-brackets with the diameter between 3.28 mm and 3.35 mm (0.129 in and 0.132 in) and install: 6 Angle NSA5546-00 Item 592 with: 12 Rivet-Blind NAS1919C04S02U Item 607

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 344 6

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# @A340 SERVICE BULLETIN
2 Install the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 08 For the tolerances for waviness and bend in wires, refer to Fig. A-GBNAA Sheet 01 thru Fig. A-GBNAA Sheet 02

. NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: 2 Sensing Element 35602-2-255 Item 562 2 Sensing Element 35600-2-255 Item 563 2 Sensing Element 35586-2-255 Item 564 2 Sensing Element 35594-2-255 Item 566 2 Sensing Element 35604-2-255 Item 570 1 Sensing Element 35597-2-255 Item 572 1 Sensing Element 35599-3-255 Item 574 with: 1 Connector NSA5549-00 Item 355 22 Clamp NSA5543-00 Item 357 16 Clip Nut Item (399) Retained at removal 6 Screw Item (408) Retained at removal 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0832R Item 597 16 Screw Item (601) Retained at removal 152 Sleeve-Protective NSA5539S Item 602 1 Washer NAS1149C0863R Item 604 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 345 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 6 Nut NSA5542-00 Item 612 6 Nut Item (612) Retained at removal 1 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAA Sheet 01 thru Fig. A-GBGAA Sheet 07 Install: 1 Placard F3627011520400 Item 356 1 Placard F3627011520600 Item 591 2 Placard F3627011520800 Item 594 1 Placard F3627011522200 Item 593 1 Placard F3627011521000 Item 611 2 Placard F3627011520200 Item 606 1 Placard D3627006026600 Item 57

(31) Subtask 364033-410-003-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 346 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Install : Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (32) Subtask 364033-831-208-002 - Remove the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 2.75 Minimum number of person 1 Subtask elapsed time 2.75 Skills ELECTRICAL References Fig. A-GBHAC Removal of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the sensing elements in the rear fuselage 1 Remove the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBHAC Sheet 01 thru Fig. A-GBHAC Sheet 04 Remove: FIN 34HF 1 Sensing Element 35301-75 Item (361) Discard FIN 139HF 1 Sensing Element 35558-2-310 Item (362) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 347 6

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# @A340 SERVICE BULLETIN
FIN 140HF 1 Sensing Element 35636-2-310 Item (365) Discard FIN 33HF 1 Sensing Element 35660-2-310 Item (370) Discard attached with: 3 Screw Item (601) Discard 33 Screw Item (601) Retain 47 Sleeve Item (602) Discard 1 Screw Item (603) Retain 4 Screw Item (620) Retain 5 Spacer Item (609) Retain 40 Clamp Item (357) Discard 37 Nut-Clip Item (399) Retain 3 Flange Item (59) Discard 3 Nut Item (612) Retain 2 Clamp Item (621) Discard 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBHAC Sheet 01 thru Fig. A-GBHAC Sheet 04 Remove: 1 Connector Item (355) Discard 1 Washer Item (596) Discard 1 Washer Item (604) Discard

(33) Subtask 364033-831-209-002 - Install the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 348 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 5.75 Minimum number of person 1 Subtask elapsed time 5.75 Skills ELECTRICAL Material necessary to do the job Kit 364033D14R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 314 NAS1801-3-8 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 37 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 362 35563-2-255 1 ELEMENT 363 35566-2-255 1 ELEMENT 365 35616-2-255 2 ELEMENT 369 35641-3-255 1 ELEMENT 370 35642-2-255 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 397 NSA5527-03-04 2 SPACER 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 1 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 94 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 3 SPACER 610 NSA5538-00 2 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 349 6

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# @A340 SERVICE BULLETIN
Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Fig. A-GBJAC Installation of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 (a) Install the sensing elements in the rear fuselage 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 Install: 3 Connection Flanges NSA5545-00 Item 59 with: 6 Rivet-Blind NAS1919C04S02U Item 607 2 Install the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: FIN 361HF 1 Cable-Electrical Interconnecting 35301-74 Item 360
FIN 34HF 1 Cable-Electrical Interconnecting 35301-75 Item 361
FIN 139HF 1 Sensing Element 35563-2-255 Item 362
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 350 6

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# @A340 SERVICE BULLETIN
FIN 359HF 1 Sensing Element 35566-2-255 Item 363 FIN 360HF 1 Sensing Element 35616-2-255 Item 365 FIN 140HF 1 Sensing Element 35616-2-255 Item 365 FIN 358HF 1 Sensing Element 35641-3-255 Item 369 FIN 33HF 1 Sensing Element 35642-2-255 Item 370 with: 1 Connector NSA5549-00 Item 355 1 Washer NAS1149C0832R Item 597 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0863R Item 604 attached with: 37 Nut-Clip Item (399) Retained at removal 33 Screw Item (601) Retained at removal 1 Screw Item (603) Retained at removal 5 Spacer Item (609) Retained at removal 3 Nut Item (612) Retained at removal 4 Screw Item (620) Retained at removal 2 Clamp Item (621) Retained at removal 2 Screw NAS1801-3-19 Item 313 2 Screw NAS1801-3-8 Item 314 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 351 6

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# @A340 SERVICE BULLETIN
37 Clamp NSA5543-00 Item 357 12 Clamp AS21919WCH04 Item 372 2 Clamp AS21919WCH10 Item 373 2 Spacer NSA5527-03-04 Item 397 5 Screw NAS1801-3-9 Item 416 1 Spacer NSA5527-03-08D Item 496 94 Sleeve-Protective NSA5539S Item 602 3 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 3 Nut NSA5542-00 Item 612 5 Nut MS21042-3 Item 640 7 Washer NAS1149D0332K Item 682 2 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 Install: 1 Placard F3617052620200 Item 374 1 Placard F3627011521400 Item 392 2 Placard F3627011521600 Item 393 2 Placard F3627011521800 Item 394 1 Placard F3617052620000 Item 591 1 Placard D3627006026800 Item 608

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 352 6

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# @A340 SERVICE BULLETIN (34) Subtask 364033-831-210-002 - Install the sleeves at the APU Bleed Air Duct Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D17R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 377 F3617062400400 1 SLEEVE 380 F3617062401600 1 SLEEVE 382 F3617062402200 1 SLEEVE 383 F3617062403200 1 SLEEVE 384 F3617062403400 1 SLEEVE 385 F3617062403600 1 SLEEVE 386 F3617062403800 1 SLEEVE 387 F3617062404000 1 SLEEVE 602 NSA5539S 6 SLEEVE References Fig. A-GBKAC Installation of the Sleeves at the APU Bleed Air Duct Sheet 01
(a) Install the sleeves at the APU Bleed Air Duct between Frame 80/82 thru Frame 95 Refer to Fig. A-GBKAC Sheet 01 install the sleeves and close them with the adhesive strips: 1 Sleeve Assy F3617062400400 Item 377 1 Sleeve Assy F3617062401600 Item 380 1 Sleeve Assy F3617062402200 Item 382 1 Sleeve F3617062403200 Item 383 1 Sleeve F3617062403400 Item 384 1 Sleeve F3617062403600 Item 385 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 353 6

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# @A340 SERVICE BULLETIN
1 Sleeve F3617062403800 Item 386 1 Sleeve F3617062404000 Item 387 Close the sleeves with: 6 Sleeve-Protective NSA5539S Item 602 NOTE: Make sure that the blowout apertures of the blankets are close to (under) the sensing elements. **CONF 004 (1) Subtask 364033-831-016-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 300 TIE F9000095227895 BUNDLE NSA935401-08 300 TIE NSA935401-13 300 TIE

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 354 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01 Sheet 02
(a) As shown in Fig. A-FBMAA Sheet 01, install the wire, using spares conduits between Frame 37 and Frame 53.2, as shown on the wiring diagram, Fig. AFCBAA Sheet 01 and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FCBAA Sheet 02) supplied in : Bundle F9000095227895 NOTE: The spares conduits is divided in two parts. The first parts go away from Frame 40 to Frame 47 and the second parts go away from Frame 48 to Frame 53.2 (b) Attach the wires with : 300 Tie-Cable NSA935401-03 Item 169 300 Tie-Cable NSA935401-08 300 Tie-Cable NSA935401-13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 355 6

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# @A340 SERVICE BULLETIN (2) Subtask 364033-831-017-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 50 TIE F9000095227895 BUNDLE NSA935401-06 50 TIE NSA935401-13 50 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Fig. A-FCAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove and retain the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wires as shown on the wiring diagram Fig. A-FCAAA Sheet 01, and as given in the Hook-up Chart lines : - 1 thru 5 (Refer to Fig. A-FCAAA Sheet 04). (c) Install the wires as shown on the wiring diagrams, Fig. A-FCAAA Sheet 02and Fig. A-FCAAA Sheet 03and as given in the Hook-up Chart lines : - 9 thru 19 (Refer to Fig. A-FCAAA Sheet 04) supplied in : Bundle F9000095227895 (d) Attach the wires with : 50 Tie-Cable NSA935401-03 Item 169 50 Tie-Cable NSA935401-06 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 356 6

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# @A340 SERVICE BULLETIN
50 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (3) Subtask 364033-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 02 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 22 Screw Item (20) Discard 32 Washer Item (14) Discard 32 Clamp Item (86) Discard 32 Sleeve Item (13) Discard 5 Screw Item (91) Discard 10 Spacer Item (16) Discard 5 Screw Item (21) Discard 2 Nut Item (15) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 357 6

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# @A340 SERVICE BULLETIN
FIN 97HF 1 Sensing Element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing Element 35624-2-255 Item (2) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(4) Subtask 364033-831-002-001 - Remove the sensing elements and the supports between FR44 and FR51. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 51 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 03 (Refer to AMM Task 36-22-17-000-801) 18 Screw Item (21) Discard 30 Washer Item (14) Discard 30 Clamp Item (86) Discard 30 Sleeve Item (13) Discard 18 Spacer Item (16) Discard 12 Screw Item (20) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 358 6

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# @A340 SERVICE BULLETIN 2 Nut Item (15) Discard FIN 99HF 1 Sensing Element 35612-2-255 Item (3) Discard FIN 100HF 1 Sensing Element 35605-2-255 Item (6) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(5) Subtask 364033-831-003-001 - Remove the sensing elements and the supports between FR51 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 51 to Frame 53.6 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 04 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 18 Screw Item (21) Discard 37 Washer Item (14) Discard 37 Clamp Item (86) Discard 37 Sleeve Item (13) Discard 23 Spacer Item (16) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 359 6

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# @A340 SERVICE BULLETIN 16 Screw Item (20) Discard 1 Screw Item (93) Discard 1 Spacer Item (18) Discard 2 Screw Item (91) Discard 3 Nut Item (15) Discard FIN 101HF 1 Sensing Element 35603-2-255 Item (4) Discard FIN 102HF 1 Sensing Element 35600-2-255 Item (5) Discard FIN 23HF 1 Sensing Element 35571-2-255 Item (7) Discard 6 Rivet Item (11) Discard 3 Support Item (10) Discard

(6) Subtask 364033-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 05 (Refer to AMM Task 36-22-17-000-801) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 360 6

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# @A340 SERVICE BULLETIN 19 Screw Item (20) Discard 27 Washer Item (14) Discard 27 Clamp Item (86) Discard 27 Sleeve Item (13) Discard 4 Screw Item (91) Discard 12 Spacer Item (16) Discard 4 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 24HF 1 Sensing Element 35580-2-255 Item (8) Discard FIN 25HF 1 Sensing Element 35611-3-255 Item (9) Discard 2 Rivet Item (11) Discard 1 Support Item (10) Discard

(7) Subtask 364033-010-002-001 - If necessary, remove the ducts between FR53.5 and FR53.6 for access. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 361 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (112) Retain 1 Duct assy Item (114) Retain

(8) Subtask 364033-831-005-001 - Drill a new hole in the structure between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required Polyurethane Finnish Paint 16-018 As required References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Drill one hole on the structure between FR53.5 and FR53.6 to a diameter comprised between 13.5mm (0.531in.) Min. and 13.7mm (0.539 in.) Max. as shown on Fig. A-FBCAA

.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 362 6

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# @A340 SERVICE BULLETIN (b) Do a spotfacing on the structure between FR53.5 and 53.6 to a diameter of 24mm (0.944 in.) with a radius of 2mm (0.078in.) NOTE: Be careful at the depth : 2mm (0.078 in.) Min. and 3mm (0.118 in.) Max. (c) Protect the hole and the spotfacing with : Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
Polyurethane Finnish Paint 16-018 As required (9) Subtask 364033-831-006-001 - Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 363 6

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# @A340 SERVICE BULLETIN
Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBFAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02 (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBFAA

. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Fig. A-FBFAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required
(e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581571700000 or 1 Blanket-Insulation F2582261900000 becomes 1 Blanket-Insulation F0041196200000 or 1 Blanket-Insulation F2581566600000 becomes 1 Blanket-Insulation F0041196300000 or 1 Blanket-Insulation F2581666600000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 364 6

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# @A340 SERVICE BULLETIN
becomes 1 Blanket-Insulation F0041196400000 or 1 Blanket-Insulation F2581677800000 becomes 1 Blanket-Insulation F0041196500000 or 1 Blanket-Insulation F2581677900000 becomes 1 Blanket-Insulation F0041196600000 or 1 Blanket-Insulation F2582242300000 becomes 1 Blanket-Insulation F0041196700000 (f) Install : Fig. A-FBFAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure, apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (g) Install the insulation blanket.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 365 6

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# @A340 SERVICE BULLETIN (10) Subtask 364033-410-001-001 - If removed, install the ducts between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (114) Retained at removal (11) Subtask 364033-010-003-001 - If necessary, remove the ducts between FR43 and FR45 for access. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 366 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Remove : (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(12) Subtask 364033-831-007-001 - Replace the web assy and the half clamp assy at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required
References Fig. A-FBEAA Replacement of the Web Assy at FR44 on the LH side Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 367 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBEAA 17 Screw Item (119) Retain 17 Washer Item (124) Retain 1 Strip cover assy Item (122) Retain 2 Screw Item (120) Retain 1 Half clamp assy F5331583500000 Item (118) Discard 1 Half clamp assy Item (121) Retain 1 Bracket Item (123) Retain 1 Web Assy F5331591000000 Item (117) Discard NOTE: It is not necessary to remove completely the bracket Item (123). (b) Install : Fig. A-FBEAA 1 Web Assy F5331591000200 Item 117 1 Bracket Item (123) Retained at removal 1 Half clamp assy Item (121) Retained at removal 1 Half clamp assy F5331583500200 Item 118 2 Screw Item (120) Retained at removal 1 Strip cover assy Item (122) Retained at removal 17 Washer Item (124) Retained at removal 17 Screw Item (119) Retained at removal NOTE: Install the new web assy with :
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 368 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Fillet Consistency 09-016B As required

and Low Adhesion Polysulfide Sealant 09-019B As required (13) Subtask 364033-831-008-001 - Install the new brackets for the routing of the sensing elements at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBGAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBGAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBGAA

. (c) Install : 1 Support F0041178800000 Item 98 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 369 6

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# @A340 SERVICE BULLETIN 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (14) Subtask 364033-410-002-001 - If removed, install the ducts between FR43 and FR45. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 370 6

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# @A340 SERVICE BULLETIN (15) Subtask 364033-831-009-001 - Install the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 371 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 372 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 373 6

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# @A340 SERVICE BULLETIN (16) Subtask 364033-831-010-001 - Install the sensing elements and the supports between FR44 and FR50. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 11 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 3 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 14 BOLT 21 NAS6603-9 9 BOLT 23 NAS6603-16 1 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 374 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBJAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46. 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 3 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 5 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 375 6

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# @A340 SERVICE BULLETIN (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 376 6

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# @A340 SERVICE BULLETIN
24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (17) Subtask 364033-831-011-001 - Install the sensing elements and the supports between FR50 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 377 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM References Fig. A-FBKAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 378 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 306HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13 2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548620000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 379 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (18) Subtask 364033-831-012-001 - Install the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 380 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM 112 35625-2-255 1 SNSGELEM References Fig. A-FBLAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 381 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200095 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 382 6

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# @A340 SERVICE BULLETIN
3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (19) Subtask 364033-010-004-001 - If necessary, remove the ducts between FR39 and FR40 for access. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 383 6

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# @A340 SERVICE BULLETIN 1 Duct assy Item (127) Retain

(20) Subtask 364033-831-013-001 - Install the new supports for the new harness between FR39.1 and FR39.2. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 97 ASNA2050DCJ3215 14 RIVET Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required
References Fig. A-FBNAA Installation of the Supports for the New Harness Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) At FR39.1, remove a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (88) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 384 6

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# @A340 SERVICE BULLETIN
2 Install : 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (b) At FR39.1, install a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Put the support Item (88) in position as shown on Fig. A-FBNAA Sheet 03

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item (88). 3 Install : 1 Support Item (88) Retained at removal 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (c) At FR39.2, install a plate between STGR 46 and STGR 47. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (89) Retain 2 Put the plate Item 64 in position as shown on Fig. A-FBNAA Sheet 04

. 3 Drill one hole on the plate Item 64 to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the hole of the structure. 4 Drill three holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the plate Item (64). 5 Install : 1 Plate F5391094700095 Item 64 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 385 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Brush Consistency 09-013B As required (d) At FR39.2, install two supports between STGR46 and STGR48. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Put the supports Item 63 in position as shown on Fig. A-FBNAA Sheet 04

. 2 Drill four holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the supports Item 63. 3 Install : 2 Support ASNA2327-3-8 Item 63 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (e) At FR39.1, install a support between STGR 39 and STGR 40. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 05 1 Put the support Item 65 in position as shown on Fig. A-FBNAA Sheet 05

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item 65. 3 Install : 1 Support NSA5456-3-8 Item 65 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (21) Subtask 364033-831-014-001 - Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 386 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 18 NSA5527-03-11 1 SPACER 92 NSA57304-643ADL 1 PLATE 155 NSA5516-04ND 1 CLAMP 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 2 CABLE 182 NSA5050-4 1 NUT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F9000095227895 BUNDLE F9100095005595 1 PLACARD References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 (b) Put in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item 175

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 387 6

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# @A340 SERVICE BULLETIN (c) Install the splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095227895 (d) Identify the splice FIN 3593VS with the identification sleeves and the identification label supplied in : 1 Placard F9100095005595 and Bundle F9000095227895 (e) On the fuselage close to the plugs, identify the FIN 309HF and the FIN 310HF with : 1 Placard F1131031521900 and 1 Placard F1131031522000 (f) Identify the wire No. 3622-0543 of the FIN 310HF and the wire No. 3622-0544 of the FIN 309HF with the identification sleeves supplied in : 1 Placard F9100095005595 (g) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard
4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 388 6

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# @A340 SERVICE BULLETIN
5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175
6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095227895 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (h) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer NSA5527-03-11 Item 18 1 Clamp NSA5516-04ND Item (155) Retained at removal 1 Clamp NSA5516-04ND Item 155 1 Washer ASNA2397-10L Item 14 1 Screw NAS1801-3-22 Item 168 and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (i) Secure the FIN 310HF : Refer to Fig. A-FBCAA Sheet 04 1 Remove : 1 Nut Discard 2 Install : 1 Plate-Attachment NSA57304-643ADL Item 92 With : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 389 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-4 Item 182 3 Secure the new nut and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (22) Subtask 364033-831-015-001 - Install the new Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 26.00 Minimum number of person 2 Subtask elapsed time 13.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 4 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 1 CABLE 176 NSA5516-21ND 5 CLAMP DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 390 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031522100 1 PLACARD F9000095227895 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-42 Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 391 6

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# @A340 SERVICE BULLETIN (a) Install supports of new routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 7 Screw Item (130) Discard 7 Washer Item (131) Discard 7 Clamp Item (150) Retain 2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section B-B : 7 Stud NSA5159-17 Item 151 7 Clamp Item (150) Retained at removal 7 Spacer NSA5527-03-08 Item 152 7 Clamp NSA935807-04 Item 150 7 Washer NSA935808-03 Item 131 7 Nut NSA5050-3 Item 154 b For Section C-C : 1 Stud NSA5159-17 Item 151 1 Clamp NSA935807-04 Item 150 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 65 installed DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 392 6

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# @A340 SERVICE BULLETIN previously. 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section F-F : 1 Screw Item (130) Discard 1 Washer Item (131) Discard 1 Clamp Item (150) Retain b For Section G-G : 1 Screw Item (132) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section H-H : 1 Stud NSA5159-17 Item 151 1 Clamp Item (150) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 b For Section J-J : 1 Stud NSA5159-17 Item 151 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 393 6

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# @A340 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Screw Item (136) Discard 2 Washer Item (137) Discard 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud NSA5159-17 Item 151 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section K-K : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 394 6

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# @A340 SERVICE BULLETIN 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section M-M : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 395 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Screw Item (130) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 396 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section P-P : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 397 6

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# @A340 SERVICE BULLETIN
12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 398 6

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# @A340 SERVICE BULLETIN
13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section Q-Q : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (152) Retain 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (135) Retain 1 Spacer Item (152) Discard 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (144) Discard 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section S-S : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 399 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (134) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 15 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Screw Item (132) Discard 2 Washer Item (153) Discard 2 Clamp Item (138) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 400 6

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# @A340 SERVICE BULLETIN
16 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud NSA5159-17 Item 151 2 Clamp Item (138) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 17 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, remove for Section T-T : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 18 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, install for Section U-U : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 401 6

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# @A340 SERVICE BULLETIN
1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Screw Item (142) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud NSA5159-17 Item 151 1 Clamp Item (138) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (142) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp NSA935807-04 Item 150 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 402 6

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# @A340 SERVICE BULLETIN
3 Screw NAS1801-3-9 Item 158 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for detail S : 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Screw NAS1801-3-8 Item 159 NOTE: Install this hardware on the support Item 63 installed previously. 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND for Item 170. NOTE: Install this hardware on the support Item 64 installed previously. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section V-V : 1 Stud NSA5159-27 Item 163 1 Spacer NSA5527-03-01 Item 16 1 Clamp NSA935807-16 Item 134 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 403 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-20 Item 135 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 64 installed previously. 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail T : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail U : 1 Stud NSA5159-17 Item 151 1 Spacer NSA5527-03-02 Item 141 1 Clamp Item (134) Retained at removal 1 Spacer NSA5527-03-05 Item 165 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Screw Item (143) Discard 1 Washer Item (133) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 404 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 29 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud NSA5159-27 Item 163 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Spacer NSA5527-03-15 Item 22 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 30 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 31 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X : 1 Stud NSA5159-10 Item 157 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 405 6

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# @A340 SERVICE BULLETIN
Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 32 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 33 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud NSA5159-17 Item 151 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 406 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 34 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (136) Discard 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 35 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 Or 3 Clamp NSA5516-22ND Item 177 Or 3 Clamp NSA5516-23ND Item 178 And 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-10 Item 167 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 407 6

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# @A340 SERVICE BULLETIN
36 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, along the Frame 39.1 and between Stringers 38 and 37, remove for detail AE : 1 Screw Item (153) Discard 1 Washer Item (142) Discard 1 Clamp Item (135) Retain 37 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 38 and 37, install for detail AF : 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Screw NAS1801-3-9 Item 158 NOTE: Install this hardware on the support Item (88) installed previously. (b) Install the new route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : 1 Remove the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Remove : 2 Fitting-Seal NSA934710T11 Item (184) Discard And 3 Spring NSA934710E20 Item (183) Discard Attached with : 4 Screw NAS1801-3-12 Item (166) Discard 4 Washer ASNA2397-10L Item (14) Discard 4 Nut MS21042-3 Item (170) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 408 6

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# @A340 SERVICE BULLETIN
2 Put in position : FIN 301HF 1 Cable-Electrical Interconnecting 35301-74 Item 174
3 Install : 20 (M) Conduit E0432A04 4 Using supports installed at paragraph 3.C.(20).(a), route the wire No. 3622-0540 spliced at paragraph 3.C.(20).(b).2, from FIN 301HF located on the left hand side at stringer 36 and at Frame 40, through pressure seal 3520VP, to 3520VC located in avionics compartment as shown in Fig. A-FCCAA Sheet 01 and in Fig. A-FBMAA Sheet 01

. NOTE: The route 2SG rejoins route 2S on the right hand side at stringer 46 between Frame 39.1 and Frame 39.2 as shown in Fig. A-FBMAA Sheet 17

. 5 Connect the wire No. 3622-0540 as shown on the wiring diagram, Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines : - 1 and 2 (Refer to Fig. A-FCCAA Sheet 02). NOTE: Use the contacts supplied in : Bundle F9000095227895 6 Install the splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540 supplied in : Bundle F9000095227895 NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C32 item 27. 7 Install the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Install : 2 Fitting-Seal NSA934710T11 Item 184 And 3 Spring NSA934710E20 Item 183 Attach with : 4 Screw NAS1801-3-12 Item 166 4 Washer ASNA2397-10L Item 14 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 409 6

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# @A340 SERVICE BULLETIN
4 Nut MS21042-3 Item 170 8 Identify the splice FIN 3591VS with the identification sleeves and the identification label supplied in : Bundle F9000095227895 9 On the fuselage close to the plugs, identify the FIN 301HF with : 1 Placard F1131031522100

(23) Subtask 364033-831-201-001 - Install the electrical wiring in the FWD cargo compartment Work Zones and Access Panels Zone Access/Work location 130 Work location from Frame 19 to Frame 37.1 Manpower Resources Manhours 7.50 Minimum number of person 2 Subtask elapsed time 3.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 2 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBAAA Installation of the Electrical Wiring in the FWD Cargo Compartment Sheet 01 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 410 6

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# @A340 SERVICE BULLETIN (a) Install the electrical wiring in the FWD cargo compartment 1 Install the electrical wires: Refer to Fig. A-GBAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 2, END 1, Refer to Fig. A-GWAAA Sheet 01 supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBAAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 2 Placard Set F9237000207400 Item 402

(24) Subtask 364033-831-202-001 - Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment Work Zones and Access Panels Zone Access/Work location From 150 Work location Frame 55 To 170 Work location Frame 80 Manpower Resources Manhours 11.00 Minimum number of person 2 Subtask elapsed time 5.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 400 F9297000500000 1 EQUIPMNT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 411 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 402 F9237000207400 4 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBBAA Installation of the Electrical Wiring in the AFT Cargo Compartment Sheet 01 Sheet 02 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 Fig. A-GWAAA Wiring Diagram Sheet 01 (a) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 1 Install the electrical wires on 5866VB between Frame 55 thru Frame 80/82: Refer to Fig. A-GBBAA Sheet 01 Refer to Fig. A-GWAAA Sheet 01 Refer to Fig. A-GHAAA Sheet 01, Line 1 thru 3, END 1, supplied with:1 Equipment AssyElectrical F9297000500000 Item 400
2 Attach the electrical wires with: Refer to Fig. A-GBBAA Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 4 Placard Set F9237000207400 Item 402
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 412 6

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# @A340 SERVICE BULLETIN
3 Route the electrical wires through the thermal insulator at Frame 80/82: Refer to Fig. A-GBBAA Sheet 02 1 Insulator-Cable Protection ABS0596S006 Item (403) (25) Subtask 364033-831-203-001 - Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills ELECTRICAL References Fig. A-GBCAA Preparation for the Electrical Wiring Installation in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Fig. A-GHAAA Hook-up Chart Sheet 01 Fig. A-GHBAA Hook-up Chart Sheet 01 (a) Remove the pressure seal 5208VP from the pressure Frame at Frame 80/82 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 03 Remove: 1 Plate F9249011000200 Item (410) Retain 1 Plate F9249011000400 Item (411) Retain 2 Bulkhead Item (415) Discard 8 Screw Item (416) Discard 12 Washer Item (417) Discard 4 Washer Item (418) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 413 6

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# @A340 SERVICE BULLETIN 4 Nut Item (419) Discard or if alternate installed remove: 12 Washer Item (417) Discard 4 Washer Item (418) Discard 4 Nut Item (419) Discard 4 Screw Item (420) Discard 2 Screw Item (423) Discard (b) Remove the lightning protection of the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 01 thru Fig. A-GBCAA Sheet 08 1 At Frame 90 loosen the electrical receptacle 5215VC, Item (435). Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 4 Screw Item (430) Discard 4 Washer Item (431) Discard 4 Nut Item (432) Discard 2 Disconnect the electrical wires end from the electrical receptacle 5215VC. Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 thru 25 Fig. A-GHBAA Sheet 01 END 2, Line 1 and 2 Remove: 1 Receptacle Item (435) Retain 3 Remove from Frame 91 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 05 1 Screw Item (314) Discard 1 Washer Item (417) Discard 1 Clamp Item (437) Discard 1 Clip nut Item (353) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 414 6

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# @A340 SERVICE BULLETIN
4 Remove the lightning protection from the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAA Sheet 04thru Fig. A-GBCAA Sheet 08 8 Screw Item (314) Discard 12 Washer Item (417) Discard 3 Nut Item (419) Discard 21 Clamp Item (437) Retain 3 Spacer Item (442) Retain 1 Clamp Item (443) Retain 4 Screw Item (444) Discard 1 Clip nut Item (448) Discard or if alternate installed remove: 1 Washer Item (417) Discard 2 Spacer Item (442) Retain 3 Clamp Item (437) Retain 1 Clip nut Item (439) Discard 1 Screw Item (501) Discard (c) Disconnect the electrical wiring 5865VB from the APU overhead leak detection system at Frame 93 Refer to Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 09 thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 1 Remove between Frame 92 thru Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 1 Washer Item (417) Discard 1 Nut Item (419) Discard 2 Clamp Item (437) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 415 6

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# @A340 SERVICE BULLETIN 1 Screw Item (449) Discard 1 Spacer Item (464) Retain 1 Screw Item (465) Discard 1 Nut Item (470) Discard 1 Washer Item (471) Discard 2 Remove from Frame 93: Refer to Fig. A-GBCAA Sheet 09 2 Washer Item (417) Discard 4 Spacer Item (442) Retain 2 Clamp Item (437) Retain 2 Clip nut Item (448) Discard 2 Screw Item (501) Discard 3 Remove the electrical splice 5151VSA from Frame 93: Refer to Fig. A-GBCAA Sheet 09thru Fig. A-GBCAA Sheet 10 Refer to Fig. A-GHAAA Sheet 01 END 2, Line 4 and 5 1 Sleeve Item (479) Discard 1 Sleeve Item (480) Discard 1 Splice Item (481) Discard

(26) Subtask 364033-831-205-001 - Install an additional profile in the Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 90 to Frame 91 Stringer 6RH Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 416 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibitive interfay Sealant 09-005 Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018
References Fig. A-GBEAA Installation of the Bracket between FR90 and FR91 Sheet 01
(a) Install an additional profile in the Rear fuselage section 1 Between Frame 90 thru Frame 91, at RH STGR6, temporarily put into position Refer to Fig. A-GBEAA Sheet 01 1 Section Assy F5397083308600 Item 460 2 Transfer drill the holes and open holes to final dimension and install: 1 Nut MS21047L3 Item 461 with: 2 Rivet EN6101AD3-08 Item 462 NOTE: For dimensions refer to the table on Fig. A-GBEAA Sheet 01

. 3 Between Frame 90 thru Frame 91, at RH STGR6, install: 1 Section Assy F5397083308600 Item 460 with: 2 Screw NAS1801-3-8 Item 314 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 417 6

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# @A340 SERVICE BULLETIN
2 Washer NAS1149D0332J Item 463 and protect the surface with: Corrosion Inhibitive interfay Sealant 09-005 As required
and Corrosion Inhibiting, Fillet Consistency 09-016 As required , and seal the edges with: Corrosion Inhibiting low Adhesion Sealant 09-018 As required
(27) Subtask 364033-831-204-001 - Install the electrical wiring in the rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80/82 to Frame 93 Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 364033D01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 400 F9297000500000 1 EQUIPMNT 402 F9237000207400 10 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 50 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 24 WASHER DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 418 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 10 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.2 TUBING 489 F9249016510800 1 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 419 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBDAA Installation of the Electrical Wiring in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 (a) Install the electrical wire in the rear fuselage section 1 Install the electrical wire, Item 400, on 5866VB between Frame 80/82 thru Frame 90 Refer to Fig. A-GBDAA Sheet 011 Equipment AssyElectrical F9297000500000 Item 400 Attach the wire with: 2 Placard Set F9237000207400 Item 402 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 50 Tie-Cable NSA935401-05 Item 406 2 Install the electrical wire on 5866VB with the pressure seal 5208VP at Frame 80/82 Refer to Fig. A-GBDAA Sheet 01 thru Fig. A-GBDAA Sheet 03 Install: 1 Plate F9249011000200 Item (410) Retained at removal 1 Plate F9249011000400 Item (411) Retained at removal with: 2 Fitting-Seal NSA934710T14 Item 415 8 Screw NAS1801-3-9 Item 416 12 Washer NAS1149C0332R Item 417 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 420 6

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# @A340 SERVICE BULLETIN
4 Washer NAS1149D0363K Item 418 4 Nut NAS1291C3M Item 419 4 Screw NAS1102-3-10 Item 420 2 Screw NAS1801-3-10 Item 423 NOTE: Alternative to two of the, Item 416. 3 Spring NSA934710E20 Item 485 3 Install the lightning protection of the electrical bundle 5886VB at Frame 90. Attach to the wires on 5866VB leaving thru the 3 way transition at Frame 90 Refer to Fig. A-GBDAA Sheet 04 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 NOTE: Cut the sleeve to the necessary length. 4 Route the wires on 5866VB between Frame 90 thru Frame 91 Refer to Fig. A-GBDAA Sheet 04, Fig. A-GBDAA Sheet 08thru Fig. A-GBDAA Sheet 09 Install:1 Protection SystemLightning F9249016510800 Item 489
with: 1 Washer NAS1149C0332R Item 417 1 Screw NAS1801-3-18 Item 444 1 Clamp AS21919WCH13 Item 350 1 Clamp Item (437) Retained at removal 1 Spacer Item (442) Retained at removal 5 Route the electrical wires: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 08 1 Fitting-Conduit ABS0580A17P Item 492 and install, Item 492, at Frame 90 with: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 421 6

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# @A340 SERVICE BULLETIN
1 Clamp MS21919WCH14 Item 351 2 Nut NAS1291C3M Item 419 1 Strip ASNA0182-4ADL Item 469 2 Screw NAS1801-3-21 Item 493 2 Washer NSA935808C03 Item 494 2 Spacer NSA5527-03-08D Item 496 1 Clamp MS21919WCH12 Item 843 6 Route the electrical wires on 5866VB between Frame 90 thru Frame 91 to connector 5215VC Refer to Fig. A-GBDAA Sheet 04thru Fig. A-GBDAA Sheet 08 Reinstall the connector 5215VC 1 Receptacle Item (435) Retained at removal attached with: 4 Screw NAS1100-04-6 Item 430 4 Washer NAS1149CN416R Item 431 4 Nut MS21042-04 Item 432 and install: 1 Screw NAS1801-3-8 Item 314 1 Washer NAS1149C0332R Item 417 2 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-2 Item 448 or alternative install: 1 Washer NAS1149C0332R Item 417 3 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-1 Item 439
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 422 6

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# @A340 SERVICE BULLETIN 2 Spacer Item (442) Retained at removal 1 Screw NAS1801-3-27 Item 501 and install: 12 Clamp Item (437) Retained at removal 2 Spacer Item (442) Retained at removal 5 Clamp AS21919WCH13 Item 350 8 Washer NAS1149C0332R Item 417 7 Screw NAS1801-3-8 Item 314 1 Screw NAS1801-3-27 Item 501 2 Spacer NSA5527-03-02 Item 320 3 Nut NAS1291C3M Item 419 2 Screw NAS1801-3-18 Item 444 1 Nut NSA5067-3-1 Item 353 7 Route the wire, Item 400, from the 3 way transition, Item 492, to the splice 5410VS and route to the wire 5866VB with: Refer to Fig. A-GBDAA Sheet 04and Fig. A-GBDAA Sheet 081 Protection SystemLightning F9249016013200 Item 4511 Protection SystemLightning F9249016510800 Item 4891 Protection SystemLightning F9249016110900 Item 511 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 0.35 Tubing-Heat-Shrinkable E0126-01L Item 510 NOTE: Cut the sleeve to the necessary length. and install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 423 6

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# @A340 SERVICE BULLETIN
8 Placard Set F9237000207400 Item 402 8 Install the protection, Item 511, at Frame 93 with: 1 Nut ABS0520-07P Item 518 1 Support-Strain Relief ABS0513-09 Item 517 9 Install the electrical wire at Frame 93on 5865VB and 5866VB with: Refer to Fig. A-GBDAA Sheet 01 and Fig. A-GBDAA Sheet 10 thru Fig. AGBDAA Sheet 11 Install: 3 Spacer NSA5527-03-02 Item 320 1 Clamp MS21919WCH8 Item 352 1 Washer NAS1149C0332R Item 417 1 Nut NAS1291C3M Item 419 6 Clamp Item (437) Retained at removal 5 Spacer Item (442) Retained at removal 2 Screw NAS1801-08-8 Item 449 1 Screw NAS1801-3-15 Item 465 1 Strip ASNA0182-4ADL Item 469 3 Nut NAS1291C08M Item 470 5 Washer NAS1149CN816R Item 471 1 Strip-Bonding ASNA0182-3ADL Item 472 2 Screw NAS1801-08-36 Item 475 2 Nut-Clip NSA5066-08-1 Item 476 1 Clamp AS21919WCH07 Item 515 1 Clamp AS21919WCH14 Item 521 1 Screw NAS1801-08-12 Item 528 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 424 6

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# @A340 SERVICE BULLETIN 3 Clamp AS21919WCH02 Item 536 1 Clamp AS21919WCH09 Item 537 for the wire connection install: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481

(28) Subtask 364033-831-206-002 - Remove the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 5.25 Minimum number of person 1 Subtask elapsed time 5.25 Skills ELECTRICAL References Fig. A-GBFAB Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 (a) Remove the sensing elements in the AFT and Bulk cargo compartments 1 Remove the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBFAB Sheet 01 thru Fig. A-GBFAB Sheet 03 Remove: FIN 26HF 1 Sensing Element 35593-2-255 Item (358) FIN 27HF 1 Sensing Element 35609-2-255 Item (562) FIN 28HF 1 Sensing Element 35593-2-255 Item (564) FIN 29HF 1 Sensing Element 35593-2-255 Item (566) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 425 6

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# @A340 SERVICE BULLETIN
FIN 30HF 1 Sensing Element 35609-2-255 Item (563) FIN 31HF 1 Sensing Element 35609-2-255 Item (570) FIN 32HF 1 Sensing Element 35609-2-255 Item (572) attached with: 7 Nut Item (599) Retain 7 Flange Item (592) Discard 17 Sleeve Item (602) Discard 17 Clamp Item (357) Discard 10 Screw Item (620) Retain 10 Spacer Item (609) Discard 16 Clip Nut Item (399) Retain 16 Screw Item (601) Retain 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBFAB Sheet 01 and Fig. A-GBFAB Sheet 03 Remove: 1 Connector Item (355) Discard 2 Washer Item (596) Discard 1 Washer Item (597) Discard

(29) Subtask 364033-831-212-001 - Drill an additional hole for the dual loop overheat leak detection in the sheet metal pressure bulkhead Manpower Resources Manhours 0.75 Minimum number of person 1 Subtask elapsed time 0.75 Skills AIRFRAME
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 426 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBMAA Hole Location and Dimensions for the sensing element Installation in the Sheet Metal Pressure Bulkhead Sheet 01

(a) Drill the hole for the dual loop overheat leak detection in the pressure bulkhead For dimensions refer to Fig. A-GBMAA Sheet 01 1 Drill the additional sensing element hole into the pressure bulkhead Frame 80/82 with a diameter of 13.5mm (0.53in.) (30) Subtask 364033-831-207-002 - Install the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 11.25 Minimum number of person 1 Subtask elapsed time 11.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D11R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 22 CLAMP 358 35587-2-255 2 SNSGELEM 389 F3627011520000 1 PLACARD 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 7 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 427 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 176 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 14 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBGAB Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GBNAA Tolerances for the Waviness and Bend in the Electrical Wiring Sheet 01 Sheet 02 (a) Install the sensing elements in the AFT and Bulk cargo compartments Refer to AMM Task 36-22-17-400-801 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 08 Put the angles, Item 592, in position within the given tolerance area, transfer drill the rivet holes to the duct-brackets with the diameter between 3.28 mm and 3.35 mm (0.129 in and 0.132 in) and install: 7 Angle NSA5546-00 Item 592 with: 14 Rivet-Blind NAS1919C04S02U Item 607 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 428 6

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# @A340 SERVICE BULLETIN
2 Install the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 08 For the tolerances for waviness and bend in wires, refer to Fig. A-GBNAA Sheet 01 thru Fig. A-GBNAA Sheet 02

. NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: 2 Sensing Element 35587-2-255 Item 358 2 Sensing Element 35602-2-255 Item 562 2 Sensing Element 35600-2-255 Item 563 2 Sensing Element 35586-2-255 Item 564 2 Sensing Element 35594-2-255 Item 566 2 Sensing Element 35604-2-255 Item 570 1 Sensing Element 35597-2-255 Item 572 1 Sensing Element 35599-3-255 Item 574 with: 1 Connector NSA5549-00 Item 355 22 Clamp NSA5543-00 Item 357 16 Clip Nut Item (399) Retained at removal 6 Screw Item (408) Retained at removal 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0832R Item 597 16 Screw Item (601) Retained at removal 176 Sleeve-Protective NSA5539S Item 602 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 429 6

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# @A340 SERVICE BULLETIN
1 Washer NAS1149C0863R Item 604 1 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 6 Nut NSA5542-00 Item 612 6 Nut Item (599) Retained at removal 1 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(599), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAB Sheet 01 thru Fig. A-GBGAB Sheet 07 Install: 1 Placard F3627011520400 Item 356 1 Placard F3627011520000 Item 389 1 Placard F3627011520600 Item 591 2 Placard F3627011520800 Item 594 1 Placard F3627011522200 Item 593 1 Placard F3627011521000 Item 611 2 Placard F3627011520200 Item 606 1 Placard D3627006026600 Item 57

(31) Subtask 364033-410-003-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 430 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Install : Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (32) Subtask 364033-831-208-002 - Remove the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 2.75 Minimum number of person 1 Subtask elapsed time 2.75 Skills ELECTRICAL References Fig. A-GBHAC Removal of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the sensing elements in the rear fuselage 1 Remove the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBHAC Sheet 01 thru Fig. A-GBHAC Sheet 04 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 431 6

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# @A340 SERVICE BULLETIN
Remove: FIN 34HF 1 Sensing Element 35301-75 Item (361) Discard FIN 139HF 1 Sensing Element 35558-2-310 Item (362) Discard FIN 140HF 1 Sensing Element 35636-2-310 Item (365) Discard FIN 33HF 1 Sensing Element 35660-2-310 Item (370) Discard attached with: 3 Screw Item (601) Discard 33 Screw Item (601) Retain 47 Sleeve Item (602) Discard 1 Screw Item (603) Retain 4 Screw Item (620) Retain 5 Spacer Item (609) Retain 40 Clamp Item (357) Discard 37 Nut-Clip Item (399) Retain 3 Flange Item (59) Discard 3 Nut Item (612) Retain 2 Clamp Item (621) Discard 2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBHAC Sheet 01 thru Fig. A-GBHAC Sheet 04 Remove: 1 Connector Item (355) Discard 1 Washer Item (596) Discard 1 Washer Item (604) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 432 6

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# @A340 SERVICE BULLETIN (33) Subtask 364033-831-209-002 - Install the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 5.75 Minimum number of person 1 Subtask elapsed time 5.75 Skills ELECTRICAL Material necessary to do the job Kit 364033D14R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 314 NAS1801-3-8 2 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 37 CLAMP 360 35301-74 1 CABLE 361 35301-75 1 CABLE 362 35563-2-255 1 ELEMENT 363 35566-2-255 1 ELEMENT 365 35616-2-255 2 ELEMENT 369 35641-3-255 1 ELEMENT 370 35642-2-255 1 ELEMENT 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 397 NSA5527-03-04 2 SPACER 416 NAS1801-3-9 5 SCREW 496 NSA5527-03-08D 1 SPACER 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 94 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 3 SPACER 610 NSA5538-00 2 CLAMP 612 NSA5542-00 3 NUT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 433 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Fig. A-GBJAC Installation of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 (a) Install the sensing elements in the rear fuselage 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 Install: 3 Connection Flanges NSA5545-00 Item 59 with: 6 Rivet-Blind NAS1919C04S02U Item 607 2 Install the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: FIN 361HF 1 Cable-Electrical Interconnecting 35301-74 Item 360

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 434 6

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# @A340 SERVICE BULLETIN
FIN 34HF 1 Cable-Electrical Interconnecting 35301-75 Item 361
FIN 139HF 1 Sensing Element 35563-2-255 Item 362 FIN 359HF 1 Sensing Element 35566-2-255 Item 363 FIN 360HF 1 Sensing Element 35616-2-255 Item 365 FIN 140HF 1 Sensing Element 35616-2-255 Item 365 FIN 358HF 1 Sensing Element 35641-3-255 Item 369 FIN 33HF 1 Sensing Element 35642-2-255 Item 370 with: 1 Connector NSA5549-00 Item 355 1 Washer NAS1149C0832R Item 597 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0863R Item 604 attached with: 37 Nut-Clip Item (399) Retained at removal 33 Screw Item (601) Retained at removal 1 Screw Item (603) Retained at removal 5 Spacer Item (609) Retained at removal 3 Nut Item (612) Retained at removal

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 435 6

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# @A340 SERVICE BULLETIN 4 Screw Item (620) Retained at removal 2 Clamp Item (621) Retained at removal 2 Screw NAS1801-3-19 Item 313 2 Screw NAS1801-3-8 Item 314 37 Clamp NSA5543-00 Item 357 12 Clamp AS21919WCH04 Item 372 2 Clamp AS21919WCH10 Item 373 2 Spacer NSA5527-03-04 Item 397 5 Screw NAS1801-3-9 Item 416 1 Spacer NSA5527-03-08D Item 496 94 Sleeve-Protective NSA5539S Item 602 3 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 3 Nut NSA5542-00 Item 612 5 Nut MS21042-3 Item 640 7 Washer NAS1149D0332K Item 682 2 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAC Sheet 01 thru Fig. A-GBJAC Sheet 08 Install: 1 Placard F3617052620200 Item 374 1 Placard F3627011521400 Item 392 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 436 6

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# @A340 SERVICE BULLETIN
2 Placard F3627011521600 Item 393 2 Placard F3627011521800 Item 394 1 Placard F3617052620000 Item 591 1 Placard D3627006026800 Item 608

(34) Subtask 364033-831-210-002 - Install the sleeves at the APU Bleed Air Duct Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D17R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 377 F3617062400400 1 SLEEVE 380 F3617062401600 1 SLEEVE 382 F3617062402200 1 SLEEVE 383 F3617062403200 1 SLEEVE 384 F3617062403400 1 SLEEVE 385 F3617062403600 1 SLEEVE 386 F3617062403800 1 SLEEVE 387 F3617062404000 1 SLEEVE 602 NSA5539S 6 SLEEVE References Fig. A-GBKAC Installation of the Sleeves at the APU Bleed Air Duct Sheet 01
(a) Install the sleeves at the APU Bleed Air Duct between Frame 80/82 thru Frame 95 Refer to Fig. A-GBKAC Sheet 01 install the sleeves and close them with the adhesive strips: 1 Sleeve Assy F3617062400400 Item 377 1 Sleeve Assy F3617062401600 Item 380 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 437 6

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# @A340 SERVICE BULLETIN 1 Sleeve Assy F3617062402200 Item 382 1 Sleeve F3617062403200 Item 383 1 Sleeve F3617062403400 Item 384 1 Sleeve F3617062403600 Item 385 1 Sleeve F3617062403800 Item 386 1 Sleeve F3617062404000 Item 387 Close the sleeves with: 6 Sleeve-Protective NSA5539S Item 602 NOTE: Make sure that the blowout apertures of the blankets are close to (under) the sensing elements. **CONF 005 (1) Subtask 364033-831-016-001 - Modify the Wiring between the Avionics Compartment and the Cargo Compartment. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 300 TIE F9000095227895 BUNDLE NSA935401-08 300 TIE NSA935401-13 300 TIE

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 438 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCBAA Modification of the Wiring between the Cargo Compartment and the Avionics Compartment Sheet 01 Sheet 02
(a) As shown in Fig. A-FBMAA Sheet 01, install the wire, using spares conduits between Frame 37 and Frame 53.2, as shown on the wiring diagram, Fig. AFCBAA Sheet 01 and as given in the Hook-up Chart line : - 1 (Refer to Fig. A-FCBAA Sheet 02) supplied in : Bundle F9000095227895 NOTE: The spares conduits is divided in two parts. The first parts go away from Frame 40 to Frame 47 and the second parts go away from Frame 48 to Frame 53.2 (b) Attach the wires with : 300 Tie-Cable NSA935401-03 Item 169 300 Tie-Cable NSA935401-08 300 Tie-Cable NSA935401-13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 439 6

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# @A340 SERVICE BULLETIN (2) Subtask 364033-831-017-001 - Modify the Wiring in the Main rack 800VU. Work Zones and Access Panels Zone Access/Work location 120 Work location Electrical panel 800VU Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills ELECTRICAL Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 169 NSA935401-03 50 TIE F9000095227895 BUNDLE NSA935401-06 50 TIE NSA935401-13 50 TIE References Aircraft Maintenance Manual (AMM) Task 36-11-34-000-802 Task 36-11-34-400-802 Fig. A-FCAAA Modification of the Wiring in the Main Rack 800VU Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove and retain the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-000-802). (b) Remove the wires as shown on the wiring diagram Fig. A-FCAAA Sheet 01, and as given in the Hook-up Chart lines : - 1 thru 5 (Refer to Fig. A-FCAAA Sheet 04). (c) Install the wires as shown on the wiring diagrams, Fig. A-FCAAA Sheet 02and Fig. A-FCAAA Sheet 03and as given in the Hook-up Chart lines : - 9 thru 19 (Refer to Fig. A-FCAAA Sheet 04) supplied in : Bundle F9000095227895 (d) Attach the wires with : 50 Tie-Cable NSA935401-03 Item 169 50 Tie-Cable NSA935401-06 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 440 6

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# @A340 SERVICE BULLETIN
50 Tie-Cable NSA935401-13 (e) Install the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (3) Subtask 364033-831-001-001 - Remove the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 02 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 22 Screw Item (20) Discard 32 Washer Item (14) Discard 32 Clamp Item (86) Discard 32 Sleeve Item (13) Discard 5 Screw Item (91) Discard 10 Spacer Item (16) Discard 5 Screw Item (21) Discard 2 Nut Item (15) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 441 6

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# @A340 SERVICE BULLETIN
FIN 97HF 1 Sensing Element 35610-2-255 Item (1) Discard FIN 98HF 1 Sensing Element 35624-2-255 Item (2) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(4) Subtask 364033-831-002-001 - Remove the sensing elements and the supports between FR44 and FR51. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 51 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 03 (Refer to AMM Task 36-22-17-000-801) 18 Screw Item (21) Discard 30 Washer Item (14) Discard 30 Clamp Item (86) Discard 30 Sleeve Item (13) Discard 18 Spacer Item (16) Discard 12 Screw Item (20) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 442 6

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# @A340 SERVICE BULLETIN 2 Nut Item (15) Discard FIN 99HF 1 Sensing Element 35612-2-255 Item (3) Discard FIN 100HF 1 Sensing Element 35605-2-255 Item (6) Discard 4 Rivet Item (11) Discard 2 Support Item (10) Discard

(5) Subtask 364033-831-003-001 - Remove the sensing elements and the supports between FR51 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 51 to Frame 53.6 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Task 36-22-17-000-802 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 04 (Refer to AMM Task 36-22-17-000-801 and AMM Task 36-22-17-000-802) 18 Screw Item (21) Discard 37 Washer Item (14) Discard 37 Clamp Item (86) Discard 37 Sleeve Item (13) Discard 23 Spacer Item (16) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 443 6

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# @A340 SERVICE BULLETIN 16 Screw Item (20) Discard 1 Screw Item (93) Discard 1 Spacer Item (18) Discard 2 Screw Item (91) Discard 3 Nut Item (15) Discard FIN 101HF 1 Sensing Element 35603-2-255 Item (4) Discard FIN 102HF 1 Sensing Element 35600-2-255 Item (5) Discard FIN 23HF 1 Sensing Element 35571-2-255 Item (7) Discard 6 Rivet Item (11) Discard 3 Support Item (10) Discard

(6) Subtask 364033-831-004-001 - Remove the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 Manpower Resources Manhours 4.00 Minimum number of person 1 Subtask elapsed time 4.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-22-17-000-801 Fig. A-FBAAA Removal of the Sensing Elements between FR39 and FR55 on the LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Remove : Fig. A-FBAAA Sheet 01 Fig. A-FBAAA Sheet 05 (Refer to AMM Task 36-22-17-000-801) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 444 6

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# @A340 SERVICE BULLETIN 19 Screw Item (20) Discard 27 Washer Item (14) Discard 27 Clamp Item (86) Discard 27 Sleeve Item (13) Discard 4 Screw Item (91) Discard 12 Spacer Item (16) Discard 4 Screw Item (21) Discard 2 Nut Item (15) Discard FIN 24HF 1 Sensing Element 35580-2-255 Item (8) Discard FIN 25HF 1 Sensing Element 35611-3-255 Item (9) Discard 2 Rivet Item (11) Discard 1 Support Item (10) Discard

(7) Subtask 364033-010-002-001 - If necessary, remove the ducts between FR53.5 and FR53.6 for access. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 445 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBBAA (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (112) Retain 1 Duct assy Item (112) Retain 1 Duct assy Item (114) Retain

(8) Subtask 364033-831-005-001 - Drill a new hole in the structure between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Chemical Conversion Coating Yellow Aluminum 13-002 As required Anti-Corrosion Primer (polyurethane) 16-001 As required Polyurethane Finnish Paint 16-018 As required References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) Drill one hole on the structure between FR53.5 and FR53.6 to a diameter comprised between 13.5mm (0.531in.) Min. and 13.7mm (0.539 in.) Max. as shown on Fig. A-FBCAA

.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 446 6

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# @A340 SERVICE BULLETIN (b) Do a spotfacing on the structure between FR53.5 and 53.6 to a diameter of 24mm (0.944 in.) with a radius of 2mm (0.078in.) NOTE: Be careful at the depth : 2mm (0.078 in.) Min. and 3mm (0.118 in.) Max. (c) Protect the hole and the spotfacing with : Chemical Conversion Coating Yellow Aluminum 13-002 As required

Anti-Corrosion Primer (polyurethane) 16-001 As required
Polyurethane Finnish Paint 16-018 As required (9) Subtask 364033-831-006-001 - Install a new support for the routing of the sensing elements between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 96 F5392059300000 1 SUPPORT 97 ASNA2050DCJ3215 2 RIVET Reidentified part set REIDA01 ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE NOTES F0041196200000 BLANKET F2581571700000 F2582261900000 F0041196300000 BLANKET F2581566600000 F0041196400000 BLANKET F2581666600000 F0041196500000 BLANKET F2581677800000 F0041196600000 BLANKET F2581677900000 F0041196700000 BLANKET F2582242300000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 447 6

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# @A340 SERVICE BULLETIN
Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Adhesive Tape (insulation Blanket Repair) 08-073 As required Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBFAA Installation of a New Bracket between FR53.5 and FR53.6 Sheet 01 Sheet 02 (a) Move the insulation blanket to get access to the modification area. (b) Put the bracket Item 96 in position as shown on Fig. A-FBFAA

. (c) Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the bracket Item 96. Fig. A-FBFAA (d) Cut the insulation blanket to permit the installation of the bracket Item 96. NOTE: For the repair of the insulation blanket use : Adhesive Tape (insulation Blanket Repair) 08-073 As required
(e) Re-identify the insulation blanket : 1 Blanket-Insulation F2581571700000 or 1 Blanket-Insulation F2582261900000 becomes 1 Blanket-Insulation F0041196200000 or 1 Blanket-Insulation F2581566600000 becomes 1 Blanket-Insulation F0041196300000 or 1 Blanket-Insulation F2581666600000 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 448 6

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# @A340 SERVICE BULLETIN
becomes 1 Blanket-Insulation F0041196400000 or 1 Blanket-Insulation F2581677800000 becomes 1 Blanket-Insulation F0041196500000 or 1 Blanket-Insulation F2581677900000 becomes 1 Blanket-Insulation F0041196600000 or 1 Blanket-Insulation F2582242300000 becomes 1 Blanket-Insulation F0041196700000 (f) Install : Fig. A-FBFAA 1 Support F5392059300000 Item 96 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure, apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (g) Install the insulation blanket.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 449 6

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# @A340 SERVICE BULLETIN (10) Subtask 364033-410-001-001 - If removed, install the ducts between FR53.5 and FR53.6. Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53.5 to Frame 53.6 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBBAA Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (112) Retained at removal 1 Duct assy Item (114) Retained at removal (11) Subtask 364033-010-003-001 - If necessary, remove the ducts between FR43 and FR45 for access. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-000-801
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 450 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Remove : (Refer to AMM Task 36-12-41-000-801) 1 Duct assy Item (115) Retain 1 Duct assy Item (116) Retain

(12) Subtask 364033-831-007-001 - Replace the web assy and the half clamp assy at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 117 F5331591000200 1 WEB 118 F5331583500200 1 CLAMP Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Fillet Consistency 09-016B As required Low Adhesion Polysulfide Sealant 09-019B As required
References Fig. A-FBEAA Replacement of the Web Assy at FR44 on the LH side Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 451 6

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# @A340 SERVICE BULLETIN (a) Remove : Fig. A-FBEAA 17 Screw Item (119) Retain 17 Washer Item (124) Retain 1 Strip cover assy Item (122) Retain 2 Screw Item (120) Retain 1 Half clamp assy F5331583500000 Item (118) Discard 1 Half clamp assy Item (121) Retain 1 Bracket Item (123) Retain 1 Web Assy F5331591000000 Item (117) Discard NOTE: It is not necessary to remove completely the bracket Item (123). (b) Install : Fig. A-FBEAA 1 Web Assy F5331591000200 Item 117 1 Bracket Item (123) Retained at removal 1 Half clamp assy Item (121) Retained at removal 1 Half clamp assy F5331583500200 Item 118 2 Screw Item (120) Retained at removal 1 Strip cover assy Item (122) Retained at removal 17 Washer Item (124) Retained at removal 17 Screw Item (119) Retained at removal NOTE: Install the new web assy with :
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 452 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Fillet Consistency 09-016B As required

and Low Adhesion Polysulfide Sealant 09-019B As required (13) Subtask 364033-831-008-001 - Install the new brackets for the routing of the sensing elements at FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 44 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 97 ASNA2050DCJ3215 2 RIVET 98 F0041178800000 1 SUPPORT 99 F0041178800100 1 SUPPORT Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Corrosion Inhibiting Fillet Consistency 09-016B As required
References Fig. A-FBGAA Installation of Two New Brackets at FR44 Sheet 01 Sheet 02 (a) Put the brackets Item 98 and 99 in position as shown on Fig. A-FBGAA

. (b) Drill two holes to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) as shown on Fig. A-FBGAA

. (c) Install : 1 Support F0041178800000 Item 98 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 453 6

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# @A340 SERVICE BULLETIN 1 Support F0041178800100 Item 99 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: To the interface of the new bracket and the structure apply : Interfay Sealant 09-005A As required

NOTE: Do a sealant bead around new parts with : Corrosion Inhibiting Fillet Consistency 09-016B As required

NOTE: Wet install the fasteners with : Interfay Sealant 09-005A As required (14) Subtask 364033-410-002-001 - If removed, install the ducts between FR43 and FR45. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 43 to Frame 45 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 36-12-41-400-801 Fig. A-FBDAA Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) Sheet 01

(a) Install : (Refer to AMM Task 36-12-41-400-801) 1 Duct assy Item (115) Retained at removal 1 Duct assy Item (116) Retained at removal

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 454 6

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# @A340 SERVICE BULLETIN (15) Subtask 364033-831-009-001 - Install the sensing elements and the supports between FR39 and FR44. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 39 to Frame 44 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 30 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 62 SLEEVE 14 ASNA2397-10L 34 WASHER 15 NSA5542-00 4 NUT 16 NSA5527-03-01 8 SPACER 18 NSA5527-03-11 6 SPACER 20 NAS6603-1 19 BOLT 21 NAS6603-9 8 BOLT 24 NAS6603-15 6 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 2 ANGLE 32 F1131031621700 2 PLACARD 33 F1131031623700 2 PLACARD 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 70 F3611548300000 1 SUPPORT 71 F3611548800000 1 SUPPORT 78 F3611549700000 1 SUPPORT 79 F3611549100000 1 SUPPORT 100 35606-2-255 1 SNSGELEM 101 35621-2-255 1 SNSGELEM 102 35620-2-255 1 SNSGELEM 113 35610-2-255 1 SNSGELEM References Fig. A-FBHAA Installation of the New Sensing Elements between FR39 and FR44 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 455 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR39 and FR40.2. 1 Install the supports between FR39 and FR40 : 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 8 Clamp NSA5543-00 Item 10 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-11 Item 18 8 Washer ASNA2397-10L Item 14 6 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-15 Item 24 2 Install the supports between FR40 and FR40.2 : 1 Support F3611549100000 Item 79 1 Support F3611549700000 Item 78 5 Clamp NSA5543-00 Item 10 1 Spacer NSA5527-03-01 Item 16 8 Washer ASNA2397-10L Item 14 1 Bolt NAS6603-9 Item 21 6 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-2 Item 29 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 3 Install the placards between FR39 and FR40.2 : 2 Placard F1131031621700 Item 32 2 Placard F1131031623700 Item 33 1 Placard F1131031621800 Item 34
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 456 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031623800 Item 35 4 Install the sensing elements between FR39 and FR40.2 : FIN 97HF 1 Sensing Element 35606-2-255 Item 100 FIN 302HF 1 Sensing Element 35610-2-255 Item 113 28 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR40.2 and FR44. 1 Install the supports between FR40.2 and FR44 : 1 Support F3611548300000 Item 70 1 Support F3611548800000 Item 71 17 Clamp NSA5543-00 Item 10 4 Spacer NSA5527-03-11 Item 18 1 Spacer NSA5527-03-01 Item 16 18 Washer ASNA2397-10L Item 14 13 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 4 Bolt NAS6603-15 Item 24 2 Install the sensing elements between FR40.2 and FR44 : FIN 98HF 1 Sensing Element 35620-2-255 Item 102 FIN 303HF 1 Sensing Element 35621-2-255 Item 101 34 Sleeve-Protective NSA5539S Item 13

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 457 6

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# @A340 SERVICE BULLETIN (16) Subtask 364033-831-010-001 - Install the sensing elements and the supports between FR44 and FR50. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 44 to Frame 50 Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 29 CLAMP 11 ASNA0342T04-01 4 BOLT 13 NSA5539S 58 SLEEVE 14 ASNA2397-10L 35 WASHER 15 NSA5542-00 8 NUT 16 NSA5527-03-01 11 SPACER 17 NSA5527-03-10 1 SPACER 18 NSA5527-03-11 3 SPACER 19 NAS6603-24 2 BOLT 20 NAS6603-1 14 BOLT 21 NAS6603-9 9 BOLT 23 NAS6603-16 1 BOLT 26 NAS6603-32 1 BOLT 29 NAS6603-2 8 BOLT 30 NSA5546-00 2 ANGLE 34 F1131031621800 1 PLACARD 35 F1131031623800 1 PLACARD 36 F1131031623900 2 PLACARD 37 F1131031621900 2 PLACARD 38 F1131031624000 2 PLACARD 39 F1131031622000 2 PLACARD 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 79 F3611549100000 4 SUPPORT 80 F3611549500000 1 SUPPORT 81 F3611549600000 1 SUPPORT 103 35618-2-255 2 SNSGELEM 105 35598-2-255 1 SNSGELEM 114 35597-2-255 1 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 458 6

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# @A340 SERVICE BULLETIN
References Fig. A-FBJAA Installation of the New Sensing Elements between FR44 and FR50 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR44 and FR46. 1 Install the supports between FR44 and FR46 : 1 Support F3611549600000 Item 81 17 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 3 Spacer NSA5527-03-11 Item 18 21 Washer ASNA2397-10L Item 14 2 Bolt NAS6603-24 Item 19 5 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-16 Item 23 2 Bolt NAS6603-2 Item 29 2 Install the placards at FR44 : 1 Placard F1131031621800 Item 34 1 Placard F1131031623800 Item 35 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 3 Install the sensing elements between FR44 and FR46 : FIN 99HF 1 Sensing Element 35618-2-255 Item 103 FIN 304HF 1 Sensing Element 35618-2-255 Item 103 34 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 459 6

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# @A340 SERVICE BULLETIN (b) Install the sensing elements and the supports between FR46 and FR50. 1 Install the supports between FR46 and FR50 : 2 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 1 Support F3611549500000 Item 80 4 Support F3611549100000 Item 79 12 Clamp NSA5543-00 Item 10 2 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-10 Item 17 14 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 2 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-32 Item 26 6 Bolt NAS6603-2 Item 29 2 Install the placards between FR46 and FR50 : 1 Placard F1131031623900 Item 36 1 Placard F1131031621900 Item 37 2 Placard F1131031624000 Item 38 2 Placard F1131031622000 Item 39 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 3 Install the sensing elements between FR46 and FR50 : FIN 100HF 1 Sensing Element 35597-2-255 Item 114 FIN 305HF 1 Sensing Element 35598-2-255 Item 105
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 460 6

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# @A340 SERVICE BULLETIN
24 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (17) Subtask 364033-831-011-001 - Install the sensing elements and the supports between FR50 and FR53.6. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 50 to Frame 53.6 Manpower Resources Manhours 21.00 Minimum number of person 1 Subtask elapsed time 21.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 37 CLAMP 11 ASNA0342T04-01 6 BOLT 13 NSA5539S 74 SLEEVE 14 ASNA2397-10L 51 WASHER 15 NSA5542-00 6 NUT 16 NSA5527-03-01 16 SPACER 18 NSA5527-03-11 1 SPACER 20 NAS6603-1 23 BOLT 21 NAS6603-9 16 BOLT 22 NSA5527-03-15 1 SPACER 24 NAS6603-15 1 BOLT 25 NSA5545-00 1 ANGLE 28 NAS6603-12 1 BOLT 29 NAS6603-2 10 BOLT 30 NSA5546-00 2 ANGLE 40 F1131031622100 1 PLACARD 41 F1131031624100 1 PLACARD 42 F1131031622200 2 PLACARD 43 F1131031624200 2 PLACARD 44 F1131031620400 2 PLACARD 45 F1131031624300 2 PLACARD 70 F3611548300000 1 SUPPORT 72 F3611548700000 1 SUPPORT 73 F3611548500000 1 SUPPORT 74 F3611548900000 1 SUPPORT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 461 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 75 F3611548400000 1 SUPPORT 76 F3611548200000 1 SUPPORT 77 F3611548620000 1 SUPPORT 79 F3611549100000 3 SUPPORT 82 F3611549400000 1 SUPPORT 83 F3611549800000 1 SUPPORT 84 F3611549300000 1 SUPPORT 104 35567-3-255 1 SNSGELEM 106 35595-2-255 3 SNSGELEM 107 35596-2-255 1 SNSGELEM 108 35568-4-255 1 SNSGELEM References Fig. A-FBKAA Installation of the New Sensing Elements between FR50 and FR53.6 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Install the sensing elements and the supports between FR50 and FR53.2. 1 Install the supports between FR50 and FR53.2 : 1 Support F3611548700000 Item 72 1 Support F3611548400000 Item 75 1 Support F3611549400000 Item 82 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 13 Clamp NSA5543-00 Item 10 7 Spacer NSA5527-03-01 Item 16 16 Washer ASNA2397-10L Item 14 9 Bolt NAS6603-1 Item 20 7 Bolt NAS6603-9 Item 21 2 Install the placards between FR50 and FR53.2 : 1 Placard F1131031622100 Item 40 1 Placard F1131031624100 Item 41 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 462 6

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# @A340 SERVICE BULLETIN
1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 3 Install the sensing elements between FR50 and FR53.2 : FIN 101HF 1 Sensing Element 35595-2-255 Item 106 FIN 306HF 1 Sensing Element 35595-2-255 Item 106 26 Sleeve-Protective NSA5539S Item 13 2 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (b) Install the sensing elements and the supports between FR53.2 and FR53.6. 1 Install the supports between FR53.2 and FR53.6 : 1 Support F3611548300000 Item 70 1 Support F3611548500000 Item 73 1 Support F3611548900000 Item 74 1 Support F3611548200000 Item 76 1 Support F3611548620000 Item 77 3 Support F3611549100000 Item 79 1 Support F3611549800000 Item 83 1 Support F3611549300000 Item 84 1 Angle NSA5545-00 Item 25 1 Angle NSA5546-00 Item 30 4 Rivet-Blind ASNA0342T04-01 Item 11 24 Clamp NSA5543-00 Item 10 9 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 463 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-15 Item 22 35 Washer ASNA2397-10L Item 14 14 Bolt NAS6603-1 Item 20 9 Bolt NAS6603-9 Item 21 1 Bolt NAS6603-15 Item 24 1 Bolt NAS6603-12 Item 28 10 Bolt NAS6603-2 Item 29 2 Install the placards between FR53.2 and FR53.6 : 1 Placard F1131031622200 Item 42 1 Placard F1131031624200 Item 43 2 Placard F1131031620400 Item 44 2 Placard F1131031624300 Item 45 3 Install the sensing elements between FR53.2 and FR53.6 : FIN 102HF 1 Sensing Element 35595-2-255 Item 106 FIN 307HF 1 Sensing Element 35596-2-255 Item 107 FIN 23HF 1 Sensing Element 35568-4-255 Item 108 FIN 308HF 1 Sensing Element 35567-3-255 Item 104 48 Sleeve-Protective NSA5539S Item 13 4 Nut NSA5542-00 Item 15 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (18) Subtask 364033-831-012-001 - Install the sensing elements and the supports between FR53.6 and FR55. Work Zones and Access Panels Zone Access/Work location 190 Work location from Frame 53.6 to Frame 55 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 464 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 14.00 Minimum number of person 1 Subtask elapsed time 14.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 NSA5543-00 27 CLAMP 11 ASNA0342T04-01 2 BOLT 13 NSA5539S 55 SLEEVE 14 ASNA2397-10L 32 WASHER 15 NSA5542-00 2 NUT 16 NSA5527-03-01 6 SPACER 17 NSA5527-03-10 2 SPACER 18 NSA5527-03-11 5 SPACER 20 NAS6603-1 17 BOLT 21 NAS6603-9 1 BOLT 26 NAS6603-32 2 BOLT 29 NAS6603-2 2 BOLT 30 NSA5546-00 1 ANGLE 70 F3611548300000 1 SUPPORT 79 F3611549100000 1 SUPPORT 85 NSA5549-90 2 CONNECTR 86 NSA5538-00 3 CLAMP 87 NAS6603-17 5 BOLT 88 F1131031620500 1 PLACARD 89 F1131031624400 1 PLACARD 90 F1131031620600 1 PLACARD 91 F1131031624500 1 PLACARD 93 F3611549200095 1 SUPPORT 94 NAS6603-10 5 BOLT 95 F3611549000000 1 SUPPORT 109 35597-3-255 1 SNSGELEM 110 35587-2-255 1 SNSGELEM 111 35627-2-255 1 SNSGELEM 112 35625-2-255 1 SNSGELEM References Fig. A-FBLAA Installation of the New Sensing Elements between FR53.6 and FR55 on LH side Sheet 01 Sheet 02 Sheet 03 Sheet 04
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 465 6

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# @A340 SERVICE BULLETIN (a) Install the sensing elements and the supports between FR53.6 and FR55. 1 Install the supports between FR53.6 and FR55 : 1 Support F3611548300000 Item 70 1 Support F3611549100000 Item 79 1 Support F3611549200095 Item 93 1 Support F3611549000000 Item 95 1 Angle NSA5546-00 Item 30 2 Rivet-Blind ASNA0342T04-01 Item 11 27 Clamp NSA5543-00 Item 10 3 Clamp NSA5538-00 Item 86 6 Spacer NSA5527-03-01 Item 16 2 Spacer NSA5527-03-10 Item 17 5 Spacer NSA5527-03-11 Item 18 32 Washer ASNA2397-10L Item 14 17 Bolt NAS6603-1 Item 20 1 Bolt NAS6603-9 Item 21 2 Bolt NAS6603-32 Item 26 2 Bolt NAS6603-2 Item 29 5 Bolt NAS6603-17 Item 87 5 Bolt NAS6603-10 Item 94 2 Install the placards between FR53.6 and FR55 : 1 Placard F1131031620500 Item 88 1 Placard F1131031624400 Item 89 1 Placard F1131031620600 Item 90 1 Placard F1131031624500 Item 91 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 466 6

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# @A340 SERVICE BULLETIN
3 Install the sensing elements between FR53.6 and FR55 : FIN 24HF 1 Sensing Element 35597-3-255 Item 109 FIN 311HF 1 Sensing Element 35587-2-255 Item 110 FIN 25HF 1 Sensing Element 35627-2-255 Item 111 FIN 312HF 1 Sensing Element 35625-2-255 Item 112 2 Nut NSA5542-00 Item 15 2 Connector NSA5549-90 Item 85 55 Sleeve-Protective NSA5539S Item 13 NOTE: Secure the nuts Item 15 with wire-lock MS20995C32 Item 27. (19) Subtask 364033-010-004-001 - If necessary, remove the ducts between FR39 and FR40 for access. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Remove : Fig. A-FBPAA (Refer to AMM Task 21-20-00-010-801) 1 Duct assy Item (125) Retain 1 Duct assy Item (126) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 467 6

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# @A340 SERVICE BULLETIN 1 Duct assy Item (127) Retain

(20) Subtask 364033-831-013-001 - Install the new supports for the new harness between FR39.1 and FR39.2. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Kit 364033A01R02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 63 ASNA2327-3-8 2 SUPPORT 64 F5391094700095 1 PLATE 65 NSA5456-3-8 1 SUPPORT 97 ASNA2050DCJ3215 14 RIVET Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required
References Fig. A-FBNAA Installation of the Supports for the New Harness Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 (a) At FR39.1, remove a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (88) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 468 6

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# @A340 SERVICE BULLETIN
2 Install : 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (b) At FR39.1, install a support between STGR 37 and STGR 38. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 03 1 Put the support Item (88) in position as shown on Fig. A-FBNAA Sheet 03

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item (88). 3 Install : 1 Support Item (88) Retained at removal 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (c) At FR39.2, install a plate between STGR 46 and STGR 47. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Remove : 2 Rivet Item (97) Discard 1 Support Item (89) Retain 2 Put the plate Item 64 in position as shown on Fig. A-FBNAA Sheet 04

. 3 Drill one hole on the plate Item 64 to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the hole of the structure. 4 Drill three holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the plate Item (64). 5 Install : 1 Plate F5391094700095 Item 64 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 469 6

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# @A340 SERVICE BULLETIN Corrosion Inhibiting Brush Consistency 09-013B As required (d) At FR39.2, install two supports between STGR46 and STGR48. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 04 1 Put the supports Item 63 in position as shown on Fig. A-FBNAA Sheet 04

. 2 Drill four holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the supports Item 63. 3 Install : 2 Support ASNA2327-3-8 Item 63 4 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (e) At FR39.1, install a support between STGR 39 and STGR 40. Fig. A-FBNAA Sheet 02and Fig. A-FBNAA Sheet 05 1 Put the support Item 65 in position as shown on Fig. A-FBNAA Sheet 05

. 2 Drill two holes on the structure to a diameter comprised between 3.25mm (0.128in.) and 3.35mm (0.132in.) to match the holes of the support Item 65. 3 Install : 1 Support NSA5456-3-8 Item 65 2 Rivet ASNA2050DCJ3215 Item 97 NOTE: Wet install the fasteners with : Corrosion Inhibiting Brush Consistency 09-013B As required (21) Subtask 364033-831-014-001 - Install the Interconnecting Electrical Wire FIN 309HF and 310HF, between the sensing elements. Work Zones and Access Panels Zone Access/Work location 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 470 6

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# @A340 SERVICE BULLETIN Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 1 WASHER 18 NSA5527-03-11 1 SPACER 92 NSA57304-643ADL 1 PLATE 155 NSA5516-04ND 1 CLAMP 168 NAS1801-3-22 1 SCREW 169 NSA935401-03 8 TIE 174 35301-74 1 CABLE 175 35301-75 2 CABLE 182 NSA5050-4 1 NUT F1131031521900 1 PLACARD F1131031522000 1 PLACARD F9000095227895 BUNDLE F9100095005595 1 PLACARD References Fig. A-FBCAA Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02 (a) Put in position : FIN 309HF 1 Cable-Electrical Interconnecting 35301-74 Item 174 (b) Put in position : FIN 310HF 1 Cable-Electrical Interconnecting 35301-75 Item 175

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 471 6

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# @A340 SERVICE BULLETIN (c) Install the splice FIN 3593VS (PN E0360RK1816) between the FIN 309HF and the FIN 310HF, supplied in : Bundle F9000095227895 (d) Identify the splice FIN 3593VS with the identification sleeves and the identification label supplied in : 1 Placard F9100095005595 and Bundle F9000095227895 (e) On the fuselage close to the plugs, identify the FIN 309HF and the FIN 310HF with : 1 Placard F1131031521900 and 1 Placard F1131031522000 (f) Identify the wire No. 3622-0543 of the FIN 310HF and the wire No. 3622-0544 of the FIN 309HF with the identification sleeves supplied in : 1 Placard F9100095005595 (g) Modify the splice FIN 3503VS : 1 Before any disconnection, record the wires number associated to the FIN 137HF and the FIN 138HF. 2 Remove the splice FIN 3503VS between the FIN 137HF and the FIN 138HF : FIN 3503VS 1 Splice Discard NOTE: Retain the identification sleeves and the identification label of the 3503VS and of the wires associated to the FIN 137HF and the FIN 138HF. 3 Remove : FIN 137HF 1 Cable-Electrical Interconnecting 35301-74 Item (174) Discard
4 Maintain in position : FIN 138HF 1 Cable-Electrical Interconnecting 35301-75 Item (175)

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 472 6

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# @A340 SERVICE BULLETIN
5 Put in position : FIN 137HF 1 Cable-Electrical Interconnecting 35301-75 Item 175
6 Install the new splice FIN 3503VS (PN E0360RK1816) between the FIN 137HF and the FIN 138HF, supplied in : Bundle F9000095227895 NOTE: Identify the splice FIN 3503VS with the identification sleeves and the identification label retained at removal. NOTE: In accordance to the wires connections recorded at removal, identify the wires associated to the FINs 137HF and 138HF with the retained identification sleeves. (h) Between Frame 53.5 and Frame 53.6 and as shown in Fig. A-FBCAA Sheet 01 and Fig. A-FBCAA Sheet 03, install the FINs 137HF and 138HF and the FINs 309HF and 310HF (spliced previously) with : 1 Spacer NSA5527-03-11 Item 18 1 Clamp NSA5516-04ND Item (155) Retained at removal 1 Clamp NSA5516-04ND Item 155 1 Washer ASNA2397-10L Item 14 1 Screw NAS1801-3-22 Item 168 and attach it with : 8 Tie-Cable NSA935401-03 Item 169 NOTE: After connection, secure the FINs 137HF and 138HF and the FINs 309HF and 310HF with Wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (i) Secure the FIN 310HF : Refer to Fig. A-FBCAA Sheet 04 1 Remove : 1 Nut Discard 2 Install : 1 Plate-Attachment NSA57304-643ADL Item 92 With : DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 473 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-4 Item 182 3 Secure the new nut and the FIN 310HF with wire-lock MS20995C32 item 27, (Refer to Fig. A-FBCAA Sheet 05). (22) Subtask 364033-831-015-001 - Install the new Harness 2SG. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 26.00 Minimum number of person 2 Subtask elapsed time 13.00 Skills NON SPECIFIC Material necessary to do the job Kit 364033A02R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 14 ASNA2397-10L 4 WASHER 16 NSA5527-03-01 2 SPACER 18 NSA5527-03-11 1 SPACER 22 NSA5527-03-15 1 SPACER 131 NSA935808-03 24 WASHER 134 NSA935807-16 1 CLAMP 135 NSA935807-20 1 CLAMP 141 NSA5527-03-02 3 SPACER 150 NSA935807-04 30 CLAMP 151 NSA5159-17 19 STUD 152 NSA5527-03-08 19 SPACER 153 NSA935808-01 13 WASHER 154 NSA5050-3 28 NUT 157 NSA5159-10 1 STUD 158 NAS1801-3-9 4 SCREW 159 NAS1801-3-8 2 SCREW 163 NSA5159-27 5 STUD 165 NSA5527-03-05 1 SPACER 166 NAS1801-3-12 4 SCREW 167 NAS1801-3-10 3 SCREW 170 MS21042-3 4 NUT 171 NAS1801-3-17 2 SCREW 172 NAS1149F0332P 2 WASHER 173 NSA5527-03-12 6 SPACER 174 35301-74 1 CABLE 176 NSA5516-21ND 5 CLAMP DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 474 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 177 NSA5516-22ND 5 CLAMP 178 NSA5516-23ND 5 CLAMP 179 NSA5516-07ND 2 CLAMP 180 NSA5516-08ND 2 CLAMP 181 NSA5516-10ND 2 CLAMP 183 NSA934710E20 3 SPRING 184 NSA934710T11 2 FITTING E0432A04 20 (M) CONDUIT F1131031522100 1 PLACARD F9000095227895 BUNDLE References Elec. Std. Practices Manual (ESPM) 20-43-42 Fig. A-FBMAA Installation of the New Harness 2SG Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 Sheet 11 Sheet 12 Sheet 13 Sheet 14 Sheet 15 Sheet 16 Sheet 17 Sheet 18 Sheet 19 Sheet 20 Sheet 21 Sheet 22 Fig. A-FCCAA Installation of the Wiring of the New Sensing Elements Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 475 6

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# @A340 SERVICE BULLETIN (a) Install supports of new routing between 302HF located on the left hand side at stringer 36 and Frame 40 and the 3520VP located on the right hand side at Frame 39.1 : 1 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, remove : a For Section A-A : 7 Screw Item (130) Discard 7 Washer Item (131) Discard 7 Clamp Item (150) Retain 2 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 and Fig. AFBMAA Sheet 06, along the Frame 39.1 and between Frame 39.1 and Frame 39.2, install : a For Section B-B : 7 Stud NSA5159-17 Item 151 7 Clamp Item (150) Retained at removal 7 Spacer NSA5527-03-08 Item 152 7 Clamp NSA935807-04 Item 150 7 Washer NSA935808-03 Item 131 7 Nut NSA5050-3 Item 154 b For Section C-C : 1 Stud NSA5159-17 Item 151 1 Clamp NSA935807-04 Item 150 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 65 installed DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 476 6

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# @A340 SERVICE BULLETIN previously. 3 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, remove : a For Section F-F : 1 Screw Item (130) Discard 1 Washer Item (131) Discard 1 Clamp Item (150) Retain b For Section G-G : 1 Screw Item (132) Discard 1 Washer Item (133) Discard 1 Clamp Item (155) Retain 4 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 04, Fig. A-FBMAA Sheet 05 , Fig. A-FBMAA Sheet 07, Fig. A-FBMAA Sheet 08 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 39 and 40, install : a For Section H-H : 1 Stud NSA5159-17 Item 151 1 Clamp Item (150) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 b For Section J-J : 1 Stud NSA5159-17 Item 151 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 477 6

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# @A340 SERVICE BULLETIN 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 5 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, remove for detail F : 2 Screw Item (136) Discard 2 Washer Item (137) Discard 2 Clamp Item (135) Retain 2 Clamp Item (134) Retain 6 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 09, along the Frame 39.1 and between Stringer 40 and 43, install for detail G : 2 Stud NSA5159-17 Item 151 2 Clamp Item (134) Retained at removal 2 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 7 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section K-K : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 478 6

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# @A340 SERVICE BULLETIN 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard 8 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 11, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section M-M : 1 Stud Item (151) Retained at removal 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 479 6

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# @A340 SERVICE BULLETIN
1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 9 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, remove : a For Section L-L : 1 Screw Item (130) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 10 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 10 and Fig. A-FBMAA Sheet 12, along the Frame 39.1 and between Stringers 44 and 45, install : a For Section N-N : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 480 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 11 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section P-P : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (139) Retain 1 Spacer Item (152) Retain 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (139) Retain 1 Spacer Item (152) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 1 Stud Item (151) Discard
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 481 6

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# @A340 SERVICE BULLETIN
12 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 14, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section R-R : 1 Stud NSA5159-17 Item 151 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp Item (134) Retained at removal 1 Clamp Item (135) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 482 6

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# @A340 SERVICE BULLETIN
13 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, remove : a For Section Q-Q : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Spacer Item (152) Retain 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (151) Retain Or 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Clamp Item (135) Retain 1 Spacer Item (152) Discard 1 Clamp Item (134) Retain 1 Clamp Item (139) Retain 1 Stud Item (144) Discard 14 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03, Fig. A-FBMAA Sheet 13 and Fig. A-FBMAA Sheet 15, along the Frame 39.1 and between Stringers 46 and 48, install : a For Section S-S : 1 Stud Item (151) Retained at removal 1 Clamp NSA935807-04 Item 150

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 483 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (134) Retained at removal 1 Spacer Item (152) Retained at removal 1 Clamp Item (139) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 Or 1 Stud NSA5159-27 Item 163 1 Clamp NSA935807-04 Item 150 1 Clamp Item (134) Retained at removal 2 Spacer NSA5527-03-12 Item 173 1 Clamp Item (139) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 15 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, remove for detail K : 2 Screw Item (132) Discard 2 Washer Item (153) Discard 2 Clamp Item (138) Retain

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 484 6

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# @A340 SERVICE BULLETIN
16 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 16, along the Frame 39.1 and between Stringers 49 and 52, install for detail L : 2 Stud NSA5159-17 Item 151 2 Clamp Item (138) Retained at removal 2 Spacer NSA5527-03-08 Item 152 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Nut NSA5050-3 Item 154 17 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, remove for Section T-T : 1 Nut Item (154) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 1 Spacer Item (141) Retain 1 Clamp Item (138) Retain 1 Stud Item (140) Retain 18 On the left hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 17, along the Frame 39.1 and between Stringers 52 and 54, install for Section U-U : 1 Stud Item (140) Retained at removal 1 Clamp Item (138) Retained at removal 1 Spacer Item (141) Retained at removal 1 Clamp Item (138) Retained at removal 1 Clamp NSA935807-04 Item 150 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 485 6

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# @A340 SERVICE BULLETIN
1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 19 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, remove for detail N : 1 Screw Item (142) Discard 1 Washer Item (153) Discard 1 Clamp Item (138) Retain 20 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and near the Stringers 54, install for detail P : 1 Stud NSA5159-17 Item 151 1 Clamp Item (138) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 21 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, remove for detail Q : 3 Screw Item (142) Discard 3 Washer Item (153) Discard 3 Clamp Item (138) Retain 22 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, along the Frame 39.1 and between Stringers 54 and 48, install for detail R : 3 Clamp NSA935807-04 Item 150 3 Clamp Item (138) Retained at removal 3 Washer NSA935808-01 Item 153 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 486 6

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# @A340 SERVICE BULLETIN
3 Screw NAS1801-3-9 Item 158 23 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 18, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for detail S : 2 Clamp NSA935807-04 Item 150 2 Washer NSA935808-03 Item 131 2 Screw NAS1801-3-8 Item 159 NOTE: Install this hardware on the support Item 63 installed previously. 24 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section W-W : 2 Spacer NSA5527-03-02 Item 141 2 Clamp NSA5516-07ND Item 179 or 2 Clamp NSA5516-08ND Item 180 or 2 Clamp NSA5516-10ND Item 181 and 2 Washer NAS1149F0332P Item 172 2 Screw NAS1801-3-17 Item 171 NOTE: Depends on aircraft configuration, use the PN NSA5516-07ND or NSA5516-08ND or NSA5516-10ND for Item 170. NOTE: Install this hardware on the support Item 64 installed previously. 25 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 19, between the Frame 39.1 and Frame 39.2 and between Stringers 48 and 46, install for Section V-V : 1 Stud NSA5159-27 Item 163 1 Spacer NSA5527-03-01 Item 16 1 Clamp NSA935807-16 Item 134 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 487 6

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# @A340 SERVICE BULLETIN 1 Spacer NSA5527-03-08 Item 152 1 Clamp NSA935807-20 Item 135 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Install this hardware on the support Item 64 installed previously. 26 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail T : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Retain 27 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail U : 1 Stud NSA5159-17 Item 151 1 Spacer NSA5527-03-02 Item 141 1 Clamp Item (134) Retained at removal 1 Spacer NSA5527-03-05 Item 165 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 28 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, remove for detail Y : 1 Screw Item (143) Discard 1 Washer Item (133) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 488 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (155) Retain 1 Clamp Item (155) Retain 29 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 47 and 46, install for detail Z : 1 Stud NSA5159-27 Item 163 1 Clamp Item (155) Retained at removal 1 Clamp Item (155) Retained at removal 1 Spacer NSA5527-03-08 Item 152 1 Spacer NSA5527-03-15 Item 22 1 Clamp NSA935807-04 Item 150 1 Washer NSA935808-03 Item 131 1 Nut NSA5050-3 Item 154 30 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, remove for detail W : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 31 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 20, between the Frame 39.1 and Frame 39.2 and between Stringers 46 and 45, install for detail X : 1 Stud NSA5159-10 Item 157 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 489 6

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# @A340 SERVICE BULLETIN
Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-01 Item 16 1 Spacer NSA5527-03-08 Item 152 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 32 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, remove for detail AA : 1 Screw Item (136) Discard 1 Washer Item (153) Discard 1 Clamp Item (135) Retain 1 Clamp Item (134) Discard 33 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 44 and 43, install for detail AB : 1 Stud NSA5159-17 Item 151 And 1 Clamp NSA5516-21ND Item 176 Or 1 Clamp NSA5516-22ND Item 177 Or 1 Clamp NSA5516-23ND Item 178 And 1 Spacer NSA5527-03-11 Item 18 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 490 6

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# @A340 SERVICE BULLETIN 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Nut NSA5050-3 Item 154 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166. 34 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, remove for detail AC : 3 Screw Item (136) Discard 3 Washer Item (153) Discard 3 Clamp Item (135) Retain 3 Clamp Item (134) Discard 35 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 42 and 38, install for detail AD : 3 Clamp NSA5516-21ND Item 176 Or 3 Clamp NSA5516-22ND Item 177 Or 3 Clamp NSA5516-23ND Item 178 And 3 Clamp Item (135) Retained at removal 3 Washer NSA935808-01 Item 153 3 Screw NAS1801-3-10 Item 167 NOTE: Depends on aircraft configuration, use the PN NSA5516-21ND or NSA5516-22ND or NSA5516-23ND for Item 166.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 491 6

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# @A340 SERVICE BULLETIN
36 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, along the Frame 39.1 and between Stringers 38 and 37, remove for detail AE : 1 Screw Item (153) Discard 1 Washer Item (142) Discard 1 Clamp Item (135) Retain 37 On the right hand side, as shown in Fig. A-FBMAA Sheet 02, Fig. A-FBMAA Sheet 03 and Fig. A-FBMAA Sheet 21, between the Frame 39.1 and Frame 39.2 and between Stringers 38 and 37, install for detail AF : 1 Clamp Item (135) Retained at removal 1 Washer NSA935808-01 Item 153 1 Screw NAS1801-3-9 Item 158 NOTE: Install this hardware on the support Item (88) installed previously. (b) Install the new route 2SG between FIN 302HF located on the left hand side at stringer 36 and Frame 40 and the FIN 3520VC located in the avionics compartment : 1 Remove the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Remove : 2 Fitting-Seal NSA934710T11 Item (184) Discard And 3 Spring NSA934710E20 Item (183) Discard Attached with : 4 Screw NAS1801-3-12 Item (166) Discard 4 Washer ASNA2397-10L Item (14) Discard 4 Nut MS21042-3 Item (170) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 492 6

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# @A340 SERVICE BULLETIN
2 Put in position : FIN 301HF 1 Cable-Electrical Interconnecting 35301-74 Item 174
3 Install : 20 (M) Conduit E0432A04 4 Using supports installed at paragraph 3.C.(20).(a), route the wire No. 3622-0540 spliced at paragraph 3.C.(20).(b).2, from FIN 301HF located on the left hand side at stringer 36 and at Frame 40, through pressure seal 3520VP, to 3520VC located in avionics compartment as shown in Fig. A-FCCAA Sheet 01 and in Fig. A-FBMAA Sheet 01

. NOTE: The route 2SG rejoins route 2S on the right hand side at stringer 46 between Frame 39.1 and Frame 39.2 as shown in Fig. A-FBMAA Sheet 17

. 5 Connect the wire No. 3622-0540 as shown on the wiring diagram, Fig. AFCCAA Sheet 01 and as given in the Hook-up Chart lines : - 1 and 2 (Refer to Fig. A-FCCAA Sheet 02). NOTE: Use the contacts supplied in : Bundle F9000095227895 6 Install the splice FIN 3591VS (PN NSA936809RG0002) between the FIN 301HF and the wire No. 3622-0540 supplied in : Bundle F9000095227895 NOTE: After connection, Secure the FIN 301HF and FIN 302HF with Wire-lock MS20995C32 item 27. 7 Install the pressure seal 3520VP : Refer to ESPM 20-43-42 and to Fig. A-FBMAA Sheet 22 a Install : 2 Fitting-Seal NSA934710T11 Item 184 And 3 Spring NSA934710E20 Item 183 Attach with : 4 Screw NAS1801-3-12 Item 166 4 Washer ASNA2397-10L Item 14 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 493 6

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# @A340 SERVICE BULLETIN
4 Nut MS21042-3 Item 170 8 Identify the splice FIN 3591VS with the identification sleeves and the identification label supplied in : Bundle F9000095227895 9 On the fuselage close to the plugs, identify the FIN 301HF with : 1 Placard F1131031522100

(23) Subtask 364033-831-201-002 - Install the electrical wiring in the FWD cargo compartment Work Zones and Access Panels Zone Access/Work location 130 Work location from Frame 19 to Frame 37.1 Manpower Resources Manhours 7.50 Minimum number of person 2 Subtask elapsed time 3.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D02R04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 401 F9297000500200 1 EQUIPMNT 402 F9237000207400 1 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBAAE Installation of the Electrical Wiring in the FWD Cargo Compartment Sheet 01 Fig. A-GHAAB Hook-up Chart Sheet 01 Fig. A-GHBAB Hook-up Chart Sheet 01 Fig. A-GWAAE Wiring Diagram Sheet 01 Sheet 02

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 494 6

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# @A340 SERVICE BULLETIN (a) Install the electrical wiring in the FWD cargo compartment 1 Install the electrical wires: Refer to Fig. A-GBAAE Sheet 01 Refer to Fig. A-GHAAB Sheet 01, Line 1 thru 2, END 1, Refer to Fig. A-GWAAE Sheet 01 thru Fig. A-GWAAE Sheet 02 supplied with:1 Equipment AssyElectrical F9297000500200 Item 401
2 Attach the electrical wires with: Refer to Fig. A-GBAAE Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 1 Placard Set F9237000207400 Item 402

(24) Subtask 364033-831-202-002 - Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment Work Zones and Access Panels Zone Access/Work location From 150 Work location Frame 55 To 170 Work location Frame 80 Manpower Resources Manhours 11.00 Minimum number of person 2 Subtask elapsed time 5.50 Skills ELECTRICAL Material necessary to do the job Kit 364033D02R04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 401 F9297000500200 1 EQUIPMNT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 495 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 402 F9237000207400 1 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 100 TIE 407 NSA935401-10 100 TIE References Fig. A-GBBAE Installation of the Electrical Wiring in the AFT Cargo Compartment Sheet 01 Sheet 02 Fig. A-GWAAE Wiring Diagram Sheet 01 Sheet 02 Fig. A-GHAAB Hook-up Chart Sheet 01 Fig. A-GHBAB Hook-up Chart Sheet 01 (a) Install the electrical wiring in the AFT cargo compartment and Bulk cargo compartment 1 Install the electrical wires on 5866VB between Frame 55 thru Frame 80/82: Refer to Fig. A-GBBAE Sheet 01 Refer to Fig. A-GWAAE Sheet 01 thru Fig. A-GWAAE Sheet 02 Refer to Fig. A-GHAAB Sheet 01, Line 1 thru 3, END 1, supplied with:1 Equipment AssyElectrical F9297000500200 Item 401
2 Attach the electrical wires with: Refer to Fig. A-GBBAE Sheet 01 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 100 Tie-Cable NSA935401-05 Item 406 100 Tie-Cable NSA935401-10 Item 407 Install the identification placards 1 Placard Set F9237000207400 Item 402
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 496 6

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# @A340 SERVICE BULLETIN
3 Route the electrical wires through the thermal insulator at Frame 80/82: Refer to Fig. A-GBBAE Sheet 02 1 Insulator-Cable Protection ABS0596S006 Item (403) (25) Subtask 364033-831-203-002 - Modify the electrical wiring in the AFT cargo compartment, Bulk cargo compartment and Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80/82 to Frame 93 Manpower Resources Manhours 4.50 Minimum number of person 1 Subtask elapsed time 4.50 Skills ELECTRICAL References Fig. A-GBCAE Preparation for the Electrical Wiring Installation in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GHAAB Hook-up Chart Sheet 01 Fig. A-GHBAB Hook-up Chart Sheet 01 (a) Remove the pressure seal 5208VP from the pressure Frame at Frame 80/82 Refer to Fig. A-GBCAE Sheet 01 thru Fig. A-GBCAE Sheet 02 Remove: 2 Plate G9249050020000 Item (412) Retain 2 Bulkhead Item (415) Discard 12 Washer Item (417) Discard 4 Washer Item (418) Discard 12 Nut Item (419) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 497 6

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# @A340 SERVICE BULLETIN 4 Screw Item (420) Discard 6 Screw Item (426) Discard 2 Screw Item (427) Discard (b) Remove the lightning protection of the electrical bundle 5886VB at Frame 90 Refer to Fig. A-GBCAE Sheet 01 thru Fig. A-GBCAE Sheet 07 1 At Frame 90 loosen the electrical receptacle 5215VC, Item (433) Refer to Fig. A-GBCAE Sheet 03thru Fig. A-GBCAE Sheet 04 4 Screw Item (430) Discard 4 Washer Item (431) Discard 4 Nut Item (432) Discard 2 Disconnect the electrical wires end from the electrical receptacle 5215VC. Refer to Fig. A-GBCAE Sheet 03thru Fig. A-GBCAE Sheet 04 Refer to Fig. A-GHAAB Sheet 01 END 2, Line 9 thru 25,Fig. A-GHBAB Sheet 01 END 2, Line 1 and 7 1 Receptacle Item (433) Retain 3 Remove from Frame 91: Refer to Fig. A-GBCAE Sheet 03thru Fig. A-GBCAE Sheet 04 1 Screw Item (314) Discard 1 Washer Item (417) Discard 1 Clamp Item (437) Discard 1 Clip nut Item (353) Discard 4 Remove the lightning protection from the electrical bundle 5886VB at Frame 90. Fig. A-GBCAE Sheet 03thru Fig. A-GBCAE Sheet 07 8 Screw Item (314) Discard 12 Washer Item (417) Discard 3 Nut Item (419) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 498 6

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# @A340 SERVICE BULLETIN 21 Clamp Item (437) Retain 3 Spacer Item (442) Retain 1 Clamp Item (443) Retain 4 Screw Item (444) Discard 1 Clip nut Item (448) Discard or if alternate installed remove: 1 Washer Item (417) Discard 2 Spacer Item (442) Retain 3 Clamp Item (437) Retain 1 Clip nut Item (439) Discard 1 Screw Item (501) Discard (c) Disconnect the electrical wiring 5865VB from the APU overhead leak detection system at Frame 93 Refer to Fig. A-GBCAE Sheet 01, Fig. A-GBCAE Sheet 08 thru Fig. A-GBCAE Sheet 09 Refer to Fig. A-GHAAB Sheet 01 1 Remove between Frame 92 thru Frame 93: Refer to Fig. A-GBCAE Sheet 08thru Fig. A-GBCAE Sheet 09 1 Washer Item (417) Discard 1 Nut Item (470) Discard 2 Clamp Item (437) Retain 1 Spacer Item (436) Retain 1 Screw Item (465) Discard 2 Remove from Frame 93: Refer to Fig. A-GBCAE Sheet 08 2 Washer Item (417) Discard DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 499 6

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# @A340 SERVICE BULLETIN 4 Spacer Item (442) Retain 2 Clamp Item (437) Retain 2 Clip nut Item (439) Discard 2 Screw Item (501) Discard 3 Remove the electrical splice 5151VSA from Frame 93: Refer to Fig. A-GBCAE Sheet 08thru Fig. A-GBCAE Sheet 09 Refer to Fig. A-GHAAB Sheet 01 END 2, Line 8 and 9 1 Sleeve Item (479) Discard 1 Sleeve Item (480) Discard 1 Splice Item (481) Discard Refer to Fig. A-GBCAE Sheet 09 1 Washer Item (471) Discard 2 Clamp Item (437) Retain 1 Nut Item (470) Discard 1 Screw Item (464) Discard

(26) Subtask 364033-831-205-001 - Install an additional profile in the Rear fuselage section Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 90 to Frame 91 Stringer 6RH Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 500 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D03R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 2 SCREW 460 F5397083308600 1 SECTION 461 MS21047L3 1 NUT 462 EN6101AD3-08 2 RIVET 463 NAS1149D0332J 2 WASHER Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibitive interfay Sealant 09-005 Corrosion Inhibiting, Fillet Consistency 09-016 As required Corrosion Inhibiting low Adhesion Sealant 09-018
References Fig. A-GBEAA Installation of the Bracket between FR90 and FR91 Sheet 01
(a) Install an additional profile in the Rear fuselage section 1 Between Frame 90 thru Frame 91, at RH STGR6, temporarily put into position Refer to Fig. A-GBEAA Sheet 01 1 Section Assy F5397083308600 Item 460 2 Transfer drill the holes and open holes to final dimension and install: 1 Nut MS21047L3 Item 461 with: 2 Rivet EN6101AD3-08 Item 462 NOTE: For dimensions refer to the table on Fig. A-GBEAA Sheet 01

. 3 Between Frame 90 thru Frame 91, at RH STGR6, install: 1 Section Assy F5397083308600 Item 460 with: 2 Screw NAS1801-3-8 Item 314 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 501 6

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# @A340 SERVICE BULLETIN
2 Washer NAS1149D0332J Item 463 and protect the surface with: Corrosion Inhibitive interfay Sealant 09-005 As required
and Corrosion Inhibiting, Fillet Consistency 09-016 As required , and seal the edges with: Corrosion Inhibiting low Adhesion Sealant 09-018 As required
(27) Subtask 364033-831-204-002 - Install the electrical wiring in the rear fuselage section Manpower Resources Manhours 14.00 Minimum number of person 2 Subtask elapsed time 7.00 Skills ELECTRICAL Material necessary to do the job Kit 364033D02R04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 314 NAS1801-3-8 8 SCREW 320 NSA5527-03-02 5 SPACER 350 AS21919WCH13 6 CLAMP 351 MS21919WCH14 1 CLAMP 352 MS21919WCH8 1 CLAMP 353 NSA5067-3-1 1 NUT 401 F9297000500200 1 EQUIPMNT 402 F9237000207400 6 PLCRDSET 404 NSA935401-03 100 TIE 405 NSA935401-04 100 TIE 406 NSA935401-05 50 TIE 415 NSA934710T14 2 FITTING 416 NAS1801-3-9 8 SCREW 417 NAS1149C0332R 32 WASHER 418 NAS1149D0363K 4 WASHER 419 NAS1291C3M 18 NUT 420 NAS1102-3-10 4 SCREW 423 NAS1801-3-10 2 SCREW DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 502 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 426 NAS6703U4 6 BOLT 427 NAS6703U5 2 BOLT 430 NAS1100-04-6 4 SCREW 431 NAS1149CN416R 4 WASHER 432 MS21042-04 4 NUT 439 NSA5066-3-1 1 NUT 444 NAS1801-3-18 3 SCREW 448 NSA5066-3-2 1 NUT 449 NAS1801-08-8 2 SCREW 451 F9249016013200 1 PROTSYS 465 NAS1801-3-15 1 SCREW 469 ASNA0182-4ADL 2 STRIP 470 NAS1291C08M 3 NUT 471 NAS1149CN816R 5 WASHER 472 ASNA0182-3ADL 1 STRIP 475 NAS1801-08-36 2 SCREW 476 NSA5066-08-1 2 NUT 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE 485 NSA934710E20 3 SPRING 488 E0126-06L 0.2 TUBING 489 F9249016510800 2 PROTSYS 492 ABS0580A17P 1 FITTING 493 NAS1801-3-21 2 SCREW 494 NSA935808C03 2 WASHER 496 NSA5527-03-08D 2 SPACER 501 NAS1801-3-27 2 SCREW 510 E0126-01L 0.35 TUBING 511 F9249016110900 1 PROTSYS 515 AS21919WCH07 1 CLAMP 517 ABS0513-09 1 SUPPORT 518 ABS0520-07P 1 NUT 521 AS21919WCH14 1 CLAMP 528 NAS1801-08-12 1 SCREW 536 AS21919WCH02 3 CLAMP 537 AS21919WCH09 1 CLAMP 843 MS21919WCH12 1 CLAMP

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 503 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBDAE Installation of the Electrical Wiring in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Sheet 10 (a) Install the electrical wire in the rear fuselage section 1 Install the electrical wire, Item 401, on 5866VB between Frame 80/82 thru Frame 90 Refer to Fig. A-GBDAE Sheet 011 Equipment AssyElectrical F9297000500200 Item 401 Attach the wire with: 2 Placard Set F9237000207400 Item 402 100 Tie-Cable NSA935401-03 Item 404 100 Tie-Cable NSA935401-04 Item 405 50 Tie-Cable NSA935401-05 Item 406 2 Install the electrical wire on 5866VB with the pressure seal 5208VP at Frame 80/82 Refer to Fig. A-GBDAE Sheet 01 thru Fig. A-GBDAE Sheet 02 Install: 2 Plate G9249050020000 Item (412) Retained at removal attached with: 2 Fitting-Seal NSA934710T14 Item 415 20 Washer NAS1149C0332R Item 417 4 Washer NAS1149D0363K Item 418 12 Nut NAS1291C3M Item 419 4 Screw NAS1102-3-10 Item 420 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 504 6

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# @A340 SERVICE BULLETIN
6 Bolt NAS6703U4 Item 426 2 Bolt NAS6703U5 Item 427 3 Spring NSA934710E20 Item 485 or alternative install: 8 Screw NAS1801-3-9 Item 416 2 Screw NAS1801-3-10 Item 423 3 Install the lightning protection of the electrical bundle 5886VB at Frame 90 Attach to the wires on 5866VB leaving thru the 3 way transition at Frame 90 Refer to Fig. A-GBDAE Sheet 03 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 NOTE: Cut the sleeve to the necessary length. 4 Route the wires (on 5866VB) between Frame 90 thru Frame 91 Refer to Fig. A-GBDAE Sheet 03and Fig. A-GBDAE Sheet 08 Install:1 Protection SystemLightning F9249016510800 Item 489
with: 1 Washer NAS1149C0332R Item 417 1 Screw NAS1801-3-18 Item 444 1 Clamp AS21919WCH13 Item 350 1 Clamp Item (437) Retained at removal 1 Spacer Item (442) Retained at removal 5 Route the electrical wires: Refer to Fig. A-GBDAE Sheet 03and Fig. A-GBDAE Sheet 07 1 Fitting-Conduit ABS0580A17P Item 492 and install, Item 492, at Frame 90 with: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 505 6

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# @A340 SERVICE BULLETIN
1 Clamp MS21919WCH14 Item 351 2 Nut NAS1291C3M Item 419 1 Strip ASNA0182-4ADL Item 469 2 Screw NAS1801-3-21 Item 493 2 Washer NSA935808C03 Item 494 2 Spacer NSA5527-03-08D Item 496 1 Clamp MS21919WCH12 Item 843 6 Route the electrical wires on 5866VB between Frame 90 thru Frame 91 to connector 5215VC Refer to Fig. A-GBDAE Sheet 03thru Fig. A-GBDAE Sheet 07 Reinstall the connector 5215VC 1 Receptacle Item (433) Retained at removal attached with: 4 Screw NAS1100-04-6 Item 430 4 Washer NAS1149CN416R Item 431 4 Nut MS21042-04 Item 432 and install: 1 Screw NAS1801-3-8 Item 314 1 Washer NAS1149C0332R Item 417 2 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-2 Item 448 or alternative install: 1 Washer NAS1149C0332R Item 417 3 Clamp Item (437) Retained at removal 1 Nut-Clip NSA5066-3-1 Item 439
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 506 6

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# @A340 SERVICE BULLETIN 2 Spacer Item (442) Retained at removal 1 Screw NAS1801-3-27 Item 501 and install: 12 Clamp Item (437) Retained at removal 2 Spacer Item (442) Retained at removal 5 Clamp AS21919WCH13 Item 350 8 Washer NAS1149C0332R Item 417 7 Screw NAS1801-3-8 Item 314 1 Screw NAS1801-3-27 Item 501 2 Spacer NSA5527-03-02 Item 320 3 Nut NAS1291C3M Item 419 2 Screw NAS1801-3-18 Item 444 1 Nut NSA5067-3-1 Item 353 7 Route the wire, Item 401, from the 3 way transition, Item 492, to the splice 5410VS and route to the wire 5866VB with: Refer to Fig. A-GBDAE Sheet 03 and Fig. A-GBDAE Sheet 07 thru Fig. AGBDAE Sheet 081 Protection SystemLightning F9249016013200 Item 4511 Protection SystemLightning F9249016510800 Item 4891 Protection SystemLightning F9249016110900 Item 511 0.1 Tubing-Heat-Shrinkable E0126-06L Item 488 0.35 Tubing-Heat-Shrinkable E0126-01L Item 510 NOTE: Cut the sleeve to the necessary length. and install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 507 6

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# @A340 SERVICE BULLETIN
4 Placard Set F9237000207400 Item 402 8 Install the protection, Item 511, at Frame 93 with: 1 Nut ABS0520-07P Item 518 1 Support-Strain Relief ABS0513-09 Item 517 9 Install the electrical wire at Frame 93 on 5865VB and 5866VB with: Refer to Fig. A-GBDAE Sheet 01 and Fig. A-GBDAE Sheet 09 thru Fig. AGBDAE Sheet 10 3 Spacer NSA5527-03-02 Item 320 1 Clamp MS21919WCH8 Item 352 1 Washer NAS1149C0332R Item 417 1 Nut NAS1291C3M Item 419 6 Clamp Item (437) Retained at removal 5 Spacer Item (442) Retained at removal 2 Screw NAS1801-08-8 Item 449 1 Screw NAS1801-3-15 Item 465 1 Strip ASNA0182-4ADL Item 469 3 Nut NAS1291C08M Item 470 5 Washer NAS1149CN816R Item 471 1 Strip-Bonding ASNA0182-3ADL Item 472 2 Screw NAS1801-08-36 Item 475 2 Nut-Clip NSA5066-08-1 Item 476 1 Clamp AS21919WCH07 Item 515 1 Clamp AS21919WCH14 Item 521 1 Screw NAS1801-08-12 Item 528 3 Clamp AS21919WCH02 Item 536 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 508 6

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# @A340 SERVICE BULLETIN 1 Clamp AS21919WCH09 Item 537 for the wire connection install: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481

(28) Subtask 364033-831-206-003 - Remove the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 5.25 Minimum number of person 1 Subtask elapsed time 5.25 Skills ELECTRICAL References Fig. A-GBFAE Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 (a) Remove the sensing elements in the AFT and Bulk cargo compartments 1 Remove the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBFAE Sheet 01 thru Fig. A-GBFAE Sheet 03 Remove: FIN 26HF 1 Sensing Element 35593-2-255 Item (564) FIN 27HF 1 Sensing Element 35609-2-255 Item (566) FIN 28HF 1 Sensing Element 35593-2-255 Item (358) FIN 29HF 1 Sensing Element 35593-2-255 Item (563)
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 509 6

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# @A340 SERVICE BULLETIN
FIN 30HF 1 Sensing Element 35609-2-255 Item (562) FIN 31HF 1 Sensing Element 35609-2-255 Item (570) FIN 32HF 1 Sensing Element 35609-2-255 Item (572) attached with: 7 Nut Item (599) Retain 7 Flange Item (592) Discard 17 Sleeve Item (602) Discard 17 Clamp Item (357) Discard 10 Screw Item (408) Retain 10 Spacer Item (609) Discard 16 Clip Nut Item (399) Retain 16 Screw Item (601) Retain 2 Remove the sensing element at Frame 80/82 Refer to Fig. A-GBFAE Sheet 01 and Fig. A-GBFAE Sheet 03 Remove: FIN 32HF 1 Sensing Element 35609-2-255 Item (572) with: 1 Washer Item (602) Discard 1 Washer Item (604) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 510 6

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# @A340 SERVICE BULLETIN (29) Subtask 364033-831-212-002 - Drill an additional hole for the dual loop overheat leak detection in the CFK pressure bulkhead Manpower Resources Manhours 0.75 Minimum number of person 1 Subtask elapsed time 0.75 Skills AIRFRAME References Fig. A-GBMAE Hole Location and Dimensions for the Sensing Element Installation in the CFK Pressure Bulkhead Sheet 01

(a) Drill the hole for the dual loop overheat leak detection in the pressure bulkhead For dimensions refer to Fig. A-GBMAE Sheet 01 1 Drill the additional sensing element hole into the pressure bulkhead Frame 80/82 with a diameter of 13.5mm (0.53in.) (30) Subtask 364033-831-207-003 - Install the sensing elements in the AFT and Bulk cargo compartments Work Zones and Access Panels Zone Access/Work location From 160 Work location Frame 55 To 310 Work location Frame 83 Manpower Resources Manhours 11.25 Minimum number of person 1 Subtask elapsed time 11.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D12R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 57 D3627006026600 1 PLACARD 355 NSA5549-00 1 CONNECTR 356 F3627011520400 1 PLACARD 357 NSA5543-00 27 CLAMP 358 35587-2-255 2 SNSGELEM 389 F3627011520000 1 PLACARD 562 35602-2-255 2 ELEMENT 563 35600-2-255 2 SNSGELEM DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 511 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 564 35586-2-255 2 ELEMENT 566 35594-2-255 2 SNSGELEM 570 35604-2-255 2 SNSGELEM 572 35597-2-255 1 SNSGELEM 574 35599-3-255 1 ELEMENT 591 F3627011520600 1 PLACARD 592 NSA5546-00 7 ANGLE 593 F3627011522200 1 PLACARD 594 F3627011520800 2 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 176 SLEEVE 604 NAS1149C0863R 1 WASHER 606 F3627011520200 2 PLACARD 607 NAS1919C04S02U 14 RIVET 609 NSA5527-03-01 1 SPACER 610 NSA5538-00 2 CLAMP 611 F3627011521000 1 PLACARD 612 NSA5542-00 6 NUT 805 NAS1802-3-13 1 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Aircraft Maintenance Manual (AMM) Task 36-22-17-400-801 Fig. A-GBGAE Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 Sheet 09 Fig. A-GBNAA Tolerances for the Waviness and Bend in the Electrical Wiring Sheet 01 Sheet 02 (a) Install the sensing elements in the AFT and Bulk cargo compartments Refer to AMM Task 36-22-17-400-801 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBGAE Sheet 01 thru Fig. A-GBGAE Sheet 08 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 512 6

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# @A340 SERVICE BULLETIN Put the angles, Item 592, in position within the given tolerance area, transfer drill the rivet holes to the duct-brackets with the diameter between 3.28 mm and 3.35 mm (0.129 in and 0.132 in) and install: 7 Angle NSA5546-00 Item 592 with: 14 Rivet-Blind NAS1919C04S02U Item 607 2 Install the sensing elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAE Sheet 01 thru Fig. A-GBGAE Sheet 09 For the tolerances for waviness and bend in wires, refer to Fig. A-GBNAA Sheet 01 thru Fig. A-GBNAA Sheet 02

. NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: 2 Sensing Element 35587-2-255 Item 358 2 Sensing Element 35602-2-255 Item 562 2 Sensing Element 35600-2-255 Item 563 2 Sensing Element 35586-2-255 Item 564 2 Sensing Element 35594-2-255 Item 566 2 Sensing Element 35604-2-255 Item 570 1 Sensing Element 35597-2-255 Item 572 1 Sensing Element 35599-3-255 Item 574 with: 1 Connector NSA5549-00 Item 355 27 Clamp NSA5543-00 Item 357 16 Clip Nut Item (399) Retained at removal 6 Screw Item (408) Retained at removal DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 513 6

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# @A340 SERVICE BULLETIN 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0832R Item 597 16 Screw Item (601) Retained at removal 176 Sleeve-Protective NSA5539S Item 602 1 Washer NAS1149C0863R Item 604 1 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 6 Nut NSA5542-00 Item 612 6 Nut Item (599) Retained at removal 1 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(599), with lockwire: Lockwire 0.6 Mm 19-018 As required 3 Install the identification placards of the sensing-elements between Frame 55 thru Frame 83 Refer to Fig. A-GBGAE Sheet 01 thru Fig. A-GBGAE Sheet 09 Install: 1 Placard F3627011520400 Item 356 1 Placard F3627011520000 Item 389 1 Placard F3627011520600 Item 591 2 Placard F3627011520800 Item 594 1 Placard F3627011522200 Item 593 1 Placard F3627011521000 Item 611 2 Placard F3627011520200 Item 606 1 Placard D3627006026600 Item 57

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 514 6

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# @A340 SERVICE BULLETIN (31) Subtask 364033-410-003-001 - If removed, install the ducts between FR39 and FR40. Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Fig. A-FBPAA Removal/Installation of the Ducts Between FR39 and FR40 for Access Sheet 01
(a) Install : Fig. A-FBPAA (Refer to AMM Task 21-20-00-410-801) 1 Duct assy Item (125) Retained at removal 1 Duct assy Item (126) Retained at removal 1 Duct assy Item (127) Retained at removal (32) Subtask 364033-831-208-003 - Remove the sensing elements in the rear fuselage Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 2.75 Minimum number of person 1 Subtask elapsed time 2.75 Skills ELECTRICAL

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 515 6

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# @A340 SERVICE BULLETIN
References Fig. A-GBHAE Removal of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 (a) Remove the sensing elements in the rear fuselage 1 Remove the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBHAE Sheet 01 thru Fig. A-GBHAE Sheet 04 Remove: FIN 139HF 1 Sensing Element 35558-2-310 Item (362) Discard FIN 140HF 1 Sensing Element 35636-2-310 Item (365) Discard FIN 33HF 1 Sensing Element 35660-2-310 Item (368) Discard FIN 34HF 1 Sensing Element 35301-75 Item (361) Discard attached with: 3 Screw Item (601) Discard 35 Screw Item (601) Retain 45 Sleeve Item (602) Discard 2 Screw Item (620) Retain 2 Spacer Item (609) Retain 37 Clamp Item (610) Discard 3 Clamp Item (357) Retain 1 Clamp Item (621) Discard 37 Nut-Clip Item (399) Retain 3 Flange Item (592) Discard 3 Nut Item (599) Retain DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 516 6

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# @A340 SERVICE BULLETIN
2 Remove the connector of the sensing element at Frame 80/82 Refer to Fig. A-GBHAE Sheet 01 thru Fig. A-GBHAE Sheet 04 Remove: 1 Connector Item (355) Discard 1 Washer Item (596) Discard 1 Washer Item (604) Discard

(33) Subtask 364033-831-211-001 - Remove the sensing element, FIN 149HF, previously installed with Service Bulletin No. A340-36-4028 Manpower Resources Manhours 4.25 Minimum number of person 1 Subtask elapsed time 4.25 Skills ELECTRICAL Material necessary to do the job Kit 364033D02R04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 401 F9297000500200 1 EQUIPMNT 402 F9237000207400 1 PLCRDSET 479 E0718-01 0.06 TUBING 480 NSA937210MB0300 0.1 TUBING 481 NSA936809RG0001 2 SPLICE References Fig. A-GBLAE Removal of the Sensing Element, FIN 149HF, installed with Service Bulletin No. A340-36-4028 Sheet 01 Sheet 02 Fig. A-GWAAE Wiring Diagram Sheet 01 Sheet 02 Fig. A-GHAAB Hook-up Chart Sheet 01 (a) Remove the sensing element, FIN 149HF, previously installed with Service Bulletin No. A340-36-4028 1 Remove the electrical splice 5865VSA and 5865VSB at Frame 83 Refer to Fig. A-GBLAE Sheet 01 thru Fig. A-GBLAE Sheet 02 Refer to Fig. A-GWAAE Sheet 01 thru Fig. A-GWAAE Sheet 02 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 517 6

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# @A340 SERVICE BULLETIN
Refer to Fig. A-GHAAB Sheet 01, END 1, Lines 7 and 8 Remove: 2 Sleeve Item (479) Discard 2 Sleeve Item (480) Discard 2 Splice Item (481) Discard 2 Remove the sensing element, 149HF between Frame 80/82 thru Frame 83 Refer to Fig. A-GBLAE Sheet 01 thru Fig. A-GBLAE Sheet 02 Remove: FIN 149HF 1 Sensing 35610-2-255 Item (544) Discard and FIN 150HF 1 Sensing wire 35301-74 Item (542) Discard FIN 151HF 1 Sensing wire 35301-75 Item (543) Discard attached with: 6 Clamp Item (357) Discard 13 Sleeve Item (602) Discard 1 Clamp Item (610) Discard 7 Screw Item (601) Discard 1 Screw Item (493) Discard 8 Washer Item (494) Discard 2 Nut Item (612) Discard 1 Bonding strap Item (540) Discard 1 Nut Item (419) Discard 2 Plate Item (541) Discard

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 518 6

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# @A340 SERVICE BULLETIN
As required Lockwire Discard (b) Modify the electrical wiring of the removed overheat sensing element 149HF Between Frame 80/82 thru Frame 83 put the electrical wire in position on 5865VB Refer to Fig. A-GBLAE Sheet 01 thru Fig. A-GBLAE Sheet 02 Refer to Fig. A-GWAAE Sheet 01 thru Fig. A-GWAAE Sheet 02 Install:1 Equipment AssyElectrical F9297000500200 Item 401 with: 0.06 Tubing-Heat-Shrinkable E0718-01 Item 479 0.1 Tubing-Heat Shrink NSA937210MB0300 Item 480 2 Splice NSA936809RG0001 Item 481 Install the identification placard: 1 Placard Set F9237000207400 Item 402

(34) Subtask 364033-831-209-003 - Install the sensing elements in the rear fuselage Manpower Resources Manhours 5.75 Minimum number of person 1 Subtask elapsed time 5.75 Skills ELECTRICAL Material necessary to do the job Kit 364033D15R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 59 NSA5545-00 3 ANGLE 313 NAS1801-3-19 2 SCREW 314 NAS1801-3-8 5 SCREW 355 NSA5549-00 1 CONNECTR 357 NSA5543-00 38 CLAMP 359 F3627014700200 1 BRACKET 360 35301-74 1 CABLE 361 35301-75 1 CABLE 362 35563-2-255 1 ELEMENT 363 35566-2-255 1 ELEMENT DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 519 6

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# @A340 SERVICE BULLETIN
ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 365 35616-2-255 2 ELEMENT 367 35637-3-255 1 ELEMENT 368 35640-2-255 1 SNSGELEM 372 AS21919WCH04 12 CLAMP 373 AS21919WCH10 2 CLAMP 374 F3617052620200 1 PLACARD 392 F3627011521400 1 PLACARD 393 F3627011521600 2 PLACARD 394 F3627011521800 2 PLACARD 396 NAS1149F0332P 5 WASHER 397 NSA5527-03-04 2 SPACER 416 NAS1801-3-9 5 SCREW 591 F3617052620000 1 PLACARD 596 A2117050220000 1 RING 597 NAS1149C0832R 1 WASHER 602 NSA5539S 92 SLEEVE 604 NAS1149C0863R 1 WASHER 607 NAS1919C04S02U 6 RIVET 608 D3627006026800 1 PLACARD 609 NSA5527-03-01 3 SPACER 610 NSA5538-00 2 CLAMP 612 NSA5542-00 3 NUT 640 MS21042-3 5 NUT 682 NAS1149D0332K 7 WASHER 805 NAS1802-3-13 2 SCREW Consumable CMLD01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Lockwire 0.6 Mm 19-018 As required References Fig. A-GBJAE Installation of the Sensing Elements in the Rear Fuselage Section Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07 Sheet 08 (a) Install the sensing elements in the rear fuselage 1 For the installation of the sensing elements install the connection flanges Refer to Fig. A-GBJAE Sheet 01 thru Fig. A-GBJAE Sheet 08 Install: DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 520 6

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# @A340 SERVICE BULLETIN 3 Connection Flanges NSA5545-00 Item 59 with: 6 Rivet-Blind NAS1919C04S02U Item 607 2 Install a bracket for the correct attachment of the sensing elements at Frame 83 Refer to Fig. A-GBJAE Sheet 01 and Fig. A-GBJAE Sheet 03 1 Bracket Assy F3627014700200 Item 359 with: 2 Screw NAS1801-3-8 Item 314 4 Washer NAS1149F0332P Item 396 2 Nut MS21042-3 Item 640 3 Install the sensing elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAE Sheet 01thru Fig. A-GBJAE Sheet 08 NOTE: The length compensation of the sensing elements must be done at the couplings or retainer rings. NOTE: The sensing elements must be installed in front of the ventilation holes. Install: FIN 361HF 1 Cable-Electrical Interconnecting 35301-74 Item 360
FIN 34HF 1 Cable-Electrical Interconnecting 35301-75 Item 361
FIN 359HF 1 Sensing Element 35566-2-255 Item 363 FIN 360HF 1 Sensing Element 35616-2-255 Item 365 FIN 140HF 1 Sensing Element 35616-2-255 Item 365

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 521 6

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# @A340 SERVICE BULLETIN
FIN 139HF 1 Sensing Element 35563-2-255 Item 362 FIN 358HF 1 Sensing Element 35637-3-255 Item 367 FIN 33HF 1 Sensing-Element 35640-2-255 Item 368 with: 1 Connector NSA5549-00 Item 355 1 Washer NAS1149C0832R Item 597 1 Ring-Sealing A2117050220000 Item 596 1 Washer NAS1149C0863R Item 604 attached with: 37 Nut-Clip Item (399) Retained at removal 5 Spacer Item (609) Retained at removal 4 Screw Item (620) Retained at removal 3 Nut Item (599) Retained at removal 2 Clamp Item (436) Retained at removal 2 Screw NAS1801-3-19 Item 313 3 Screw NAS1801-3-8 Item 314 38 Clamp NSA5543-00 Item 357 12 Clamp AS21919WCH04 Item 372 2 Clamp AS21919WCH10 Item 373 1 Washer NAS1149F0332P Item 396 2 Spacer NSA5527-03-04 Item 397
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 522 6

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# @A340 SERVICE BULLETIN
5 Screw NAS1801-3-9 Item 416 92 Sleeve-Protective NSA5539S Item 602 3 Spacer NSA5527-03-01 Item 609 2 Clamp NSA5538-00 Item 610 3 Nut NSA5542-00 Item 612 3 Nut MS21042-3 Item 640 7 Washer NAS1149D0332K Item 682 2 Screw NAS1802-3-13 Item 805 NOTE: Secure the nuts, Item 612/(612), with lockwire: Lockwire 0.6 Mm 19-018 As required 4 Install the identification placards of the sensing-elements between Frame 80/82 thru Frame 95 Refer to Fig. A-GBJAE Sheet 01thru Fig. A-GBJAE Sheet 08 Install: 1 Placard F3617052620200 Item 374 1 Placard F3627011521400 Item 392 2 Placard F3627011521600 Item 393 2 Placard F3627011521800 Item 394 1 Placard F3617052620000 Item 591 1 Placard D3627006026800 Item 608

(35) Subtask 364033-831-210-002 - Install the sleeves at the APU Bleed Air Duct Work Zones and Access Panels Zone Access/Work location 310 Work location from Frame 80 to Frame 95 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills ELECTRICAL DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 523 6

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# @A340 SERVICE BULLETIN Material necessary to do the job Kit 364033D17R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 377 F3617062400400 1 SLEEVE 380 F3617062401600 1 SLEEVE 382 F3617062402200 1 SLEEVE 383 F3617062403200 1 SLEEVE 384 F3617062403400 1 SLEEVE 385 F3617062403600 1 SLEEVE 386 F3617062403800 1 SLEEVE 387 F3617062404000 1 SLEEVE 602 NSA5539S 6 SLEEVE References Fig. A-GBKAC Installation of the Sleeves at the APU Bleed Air Duct Sheet 01
(a) Install the sleeves at the APU Bleed Air Duct between Frame 80/82 thru Frame 95 Refer to Fig. A-GBKAC Sheet 01 install the sleeves and close them with the adhesive strips: 1 Sleeve Assy F3617062400400 Item 377 1 Sleeve Assy F3617062401600 Item 380 1 Sleeve Assy F3617062402200 Item 382 1 Sleeve F3617062403200 Item 383 1 Sleeve F3617062403400 Item 384 1 Sleeve F3617062403600 Item 385 1 Sleeve F3617062403800 Item 386 1 Sleeve F3617062404000 Item 387 Close the sleeves with: 6 Sleeve-Protective NSA5539S Item 602 NOTE: Make sure that the blowout apertures of the blankets are close to (under) the sensing elements.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 524 6

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# @A340 SERVICE BULLETIN
**CONF ALL D. TEST **CONF 001 (1) Subtask 364033-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801). (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 364033-700-201-001 - Test Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 36-22-17, Page Block 401 (a) Do the test after removal/installation of the Auxiliary Power Unit (APU) Bleed-air Duct Sensing Elements (Refer to AMM 36-22-17, Page Block 401). (3) Subtask 364033-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 525 6

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# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-21-41-400-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 526 6

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# @A340 SERVICE BULLETIN (b) Test of the equipments : 1 Do the test procedure as specified after the installation of the passenger seats (Refer to AMM Task 25-21-41-400-801). 2 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 4 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 2712VC, 3506VC, 3672VC and 3520VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the connector 2615VC and of the Terminal Block 2901VT : a Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801). **CONF 002 (1) Subtask 364033-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 527 6

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# @A340 SERVICE BULLETIN (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 364033-700-201-001 - Test Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 36-22-17, Page Block 401 (a) Do the test after removal/installation of the Auxiliary Power Unit (APU) Bleed-air Duct Sensing Elements (Refer to AMM 36-22-17, Page Block 401). (3) Subtask 364033-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-21-41-400-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 528 6

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# @A340 SERVICE BULLETIN
2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802). (b) Test of the equipments : 1 Do the test procedure as specified after the installation of the passenger seats (Refer to AMM Task 25-21-41-400-801). 2 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 4 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 2712VC, 3506VC, 3672VC and 3520VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the connector 2615VC and of the Terminal Block 2901VT : a Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 529 6

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# @A340 SERVICE BULLETIN
**CONF 003 (1) Subtask 364033-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801). (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 364033-700-201-001 - Test Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 36-22-17, Page Block 401 (a) Do the test after removal/installation of the Auxiliary Power Unit (APU) Bleed-air Duct Sensing Elements (Refer to AMM 36-22-17, Page Block 401). (3) Subtask 364033-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 530 6

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# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-21-41-400-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 531 6

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# @A340 SERVICE BULLETIN (b) Test of the equipments : 1 Do the test procedure as specified after the installation of the passenger seats (Refer to AMM Task 25-21-41-400-801). 2 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 4 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 2712VC, 3506VC, 3672VC and 3520VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the connector 2615VC and of the Terminal Block 2901VT : a Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801). **CONF 004 (1) Subtask 364033-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801).
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 532 6

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# @A340 SERVICE BULLETIN (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 364033-700-201-001 - Test Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 36-22-17, Page Block 401 (a) Do the test after removal/installation of the Auxiliary Power Unit (APU) Bleed-air Duct Sensing Elements (Refer to AMM 36-22-17, Page Block 401). (3) Subtask 364033-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-21-41-400-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 533 6

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# @A340 SERVICE BULLETIN
2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802). (b) Test of the equipments : 1 Do the test procedure as specified after the installation of the passenger seats (Refer to AMM Task 25-21-41-400-801). 2 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 4 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 2712VC, 3506VC, 3672VC and 3520VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the connector 2615VC and of the Terminal Block 2901VT : a Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 534 6

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# @A340 SERVICE BULLETIN
**CONF 005 (1) Subtask 364033-861-001-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 (a) In the cockpit, on the panel 235VU, push these pushbutton switches : - BAT 1, BAT 2, APU BAT, - GEN 1, (2, 3, 4), APU GEN, - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801). (d) Remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742VU 701PP 10PB1 72 S 742VU 702PP 10PB2 71 S

(2) Subtask 364033-700-201-001 - Test Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 36-22-17, Page Block 401 (a) Do the test after removal/installation of the Auxiliary Power Unit (APU) Bleed-air Duct Sensing Elements (Refer to AMM 36-22-17, Page Block 401). (3) Subtask 364033-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 535 6

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# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-801 Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 25-21-41-400-801 Task 25-75-41-400-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Task 36-11-34-400-802 Task 36-12-00-710-801 Task 36-12-41-400-801 Task 36-22-00-710-806 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Preliminary Tests : NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). 1 On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The Functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the Operational Test of the Instrument and Panel Integral Lighting (Refer to AMM Task 33-13-00-710-801). 3 Do the Operational Test of Lights (Refer to AMM Task 33-14-00-710-801). 4 Do the Operational Test of the Avionics-Equipment Ventilation System (Refer to AMM Task 21-26-00-710-803). 5 Do the Bite Test of the Auto Flight System (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). 6 Do the Operational Test of the Electronic Centralized Aircraft Monitoring (ECAM) Control Panel (Refer to AMM Task 31-50-00-710-803). 7 Do the test of the Flight Warning System (FWS) (Refer to AMM Task 31-50-00-740-801). 8 Do the Operational Test of the Electronic Instrument System (EIS) (Refer to AMM Task 31-60-00-710-802).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 536 6

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# @A340 SERVICE BULLETIN (b) Test of the equipments : 1 Do the test procedure as specified after the installation of the passenger seats (Refer to AMM Task 25-21-41-400-801). 2 If applicable, do the test procedure as specified after the installation of the Lower-Deck Mobile Crew-Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). 3 If ducts removed, do the test procedure as specified after the installation of the APU bleed air ducts (Refer to AMM Task 36-12-41-400-801). 4 If ducts removed, do the test procedure as specified after the installation of the air conditioning distribution ducts (Refer to AMM Task 21-20-00-410-801). 5 Do the test procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (c) Test of the connectors : 1 Test of the connectors 2712VC, 3506VC, 3672VC and 3520VC : a Do the Operational Test of the overheat detection system (Refer to AMM Task 36-22-00-710-806). 2 Test of the connector 2615VC and of the Terminal Block 2901VT : a Do the Operational Test of the APU bleed-air supply and crossbleed system (Refer to AMM Task 36-12-00-710-801). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 364033-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821, Door 831 Work location from Frame 20 to Frame 39.1 Panel 132TC Panel 132CC Panel 132GC Panel 132MC Panel 132RC Panel 132PC Panel 132KC 160 Access Door 313AL Work location Panel 161BC Panel 161EC 150 Access Door 822 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 537 6

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# @A340 SERVICE BULLETIN Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-30-00, Page Block 001 (a) In the FWD cargo compartment install the removed ceiling panels (Refer to AMM 25-52-00, Page Block 201). (b) In the BULK cargo compartment install the removed ceiling panels (Refer to AMM 25-54-00, Page Block 201). (c) Close the Bulk cargo compartment door (Refer to AMM 52-30-00, Page Block 001). (2) Subtask 364033-410-004-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-400-801 Task 25-28-41-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 538 6

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# @A340 SERVICE BULLETIN (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Seats (Refer to AMM Task 25-21-41-400-801). (g) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Textile Floor Covering (Refer to AMM Task 25-28-41-400-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the floor panel 252LG (Refer to AMM Task 53-00-00-400-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (k) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (l) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (m) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (3) Subtask 364033-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 539 6

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

# @A340 SERVICE BULLETIN (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions. **CONF 002 (1) Subtask 364033-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821, Door 831 Work location from Frame 20 to Frame 39.1 Panel 132TC Panel 132CC Panel 132GC Panel 132MC Panel 132RC Panel 132PC Panel 132KC 160 Access Door 313AL Work location Panel 161BC Panel 161EC 150 Access Door 822 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-30-00, Page Block 001 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 540 6

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

# @A340 SERVICE BULLETIN (a) In the FWD cargo compartment install the removed ceiling panels (Refer to AMM 25-52-00, Page Block 201). (b) In the BULK cargo compartment install the removed ceiling panels (Refer to AMM 25-54-00, Page Block 201). (c) Close the Bulk cargo compartment door (Refer to AMM 52-30-00, Page Block 001). (2) Subtask 364033-410-004-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-400-801 Task 25-28-41-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Seats (Refer to AMM Task 25-21-41-400-801). (g) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Textile Floor Covering (Refer to AMM Task 25-28-41-400-801).
DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 541 6

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

# @A340 SERVICE BULLETIN (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the floor panel 252LG (Refer to AMM Task 53-00-00-400-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (k) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (l) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (m) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (3) Subtask 364033-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 542 6

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

# @A340 SERVICE BULLETIN (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions. **CONF 003 (1) Subtask 364033-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821, Door 831 Work location from Frame 20 to Frame 39.1 Panel 132TC Panel 132CC Panel 132GC Panel 132MC Panel 132RC Panel 132PC Panel 132KC 160 Access Door 313AL Work location Panel 161BC Panel 161EC 150 Access Door 822 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-30-00, Page Block 001 (a) In the FWD cargo compartment install the removed ceiling panels (Refer to AMM 25-52-00, Page Block 201). (b) In the BULK cargo compartment install the removed ceiling panels (Refer to AMM 25-54-00, Page Block 201). (c) Close the Bulk cargo compartment door (Refer to AMM 52-30-00, Page Block 001). (2) Subtask 364033-410-004-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 543 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-400-801 Task 25-28-41-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Seats (Refer to AMM Task 25-21-41-400-801). (g) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Textile Floor Covering (Refer to AMM Task 25-28-41-400-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the floor panel 252LG (Refer to AMM Task 53-00-00-400-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (k) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 544 6

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

# @A340 SERVICE BULLETIN (l) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (m) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (3) Subtask 364033-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 545 6

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# @A340 SERVICE BULLETIN
**CONF 004 (1) Subtask 364033-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821, Door 831 Work location from Frame 20 to Frame 39.1 Panel 132TC Panel 132CC Panel 132GC Panel 132MC Panel 132RC Panel 132PC Panel 132KC 160 Access Door 313AL Work location Panel 161BC Panel 161EC 150 Access Door 822 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-30-00, Page Block 001 (a) In the FWD cargo compartment install the removed ceiling panels (Refer to AMM 25-52-00, Page Block 201). (b) In the BULK cargo compartment install the removed ceiling panels (Refer to AMM 25-54-00, Page Block 201). (c) Close the Bulk cargo compartment door (Refer to AMM 52-30-00, Page Block 001). (2) Subtask 364033-410-004-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 546 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-400-801 Task 25-28-41-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Seats (Refer to AMM Task 25-21-41-400-801). (g) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Textile Floor Covering (Refer to AMM Task 25-28-41-400-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the floor panel 252LG (Refer to AMM Task 53-00-00-400-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (k) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 547 6

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

# @A340 SERVICE BULLETIN (l) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (m) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (3) Subtask 364033-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 548 6

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

# @A340 SERVICE BULLETIN
**CONF 005 (1) Subtask 364033-942-201-001 - Close-up Work Zones and Access Panels Zone Access/Work location 130 Access Door 821, Door 831 Work location from Frame 20 to Frame 39.1 Panel 132TC Panel 132CC Panel 132GC Panel 132MC Panel 132RC Panel 132PC Panel 132KC 160 Access Door 313AL Work location Panel 161BC Panel 161EC 150 Access Door 822 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 25-52-00, Page Block 201 25-54-00, Page Block 201 52-30-00, Page Block 001 (a) In the FWD cargo compartment install the removed ceiling panels (Refer to AMM 25-52-00, Page Block 201). (b) In the BULK cargo compartment install the removed ceiling panels (Refer to AMM 25-54-00, Page Block 201). (c) Close the Bulk cargo compartment door (Refer to AMM 52-30-00, Page Block 001). (2) Subtask 364033-410-004-001 - Install/Close Items Removed/Opened for access Manpower Resources Skills NON SPECIFIC

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 549 6

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

# @A340 SERVICE BULLETIN
References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 25-21-41-400-801 Task 25-28-41-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-75-41-400-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-35-11-400-801 Task 53-35-13-400-801 Task 53-35-13-400-802 (a) Between Frame 37.4 and Frame 39.1 in the FWD cargo-compartment, install the floor panel 132DG (Refer to AMM 06-41-53, Page Block 001 and AMM Task 53-00-00-400-802).(b) On the RH side, between Frame 38 and Frame 39.1 in the FWD cargocompartment, install (if removed) the sidewall panels 132AX and 132ZW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801).(c) On the RH side, between Frame 37.1 and Frame 39.1 in the FWD cargocompartment, install (if removed) the ceiling panels 132TC and 132VC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (d) At Frame 39.2 in the FWD cargo-compartment, install (if removed) the partition panels 132DX and 132CX (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (e) At Frame 20 in the FWD cargo-compartment, install the partition panels 131AW and 132CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-52-00-400-801). (f) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Seats (Refer to AMM Task 25-21-41-400-801). (g) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the Textile Floor Covering (Refer to AMM Task 25-28-41-400-801). (h) On the RH side, between Frame 47 and Frame 53 in the PAX compartment, install (if removed) the floor panel 252LG (Refer to AMM Task 53-00-00-400-801). (i) On the LH side, between Frame 53.2 and Frame 57.1 in the AFT cargo compartment, install (if removed) the sidewall panels 151EW, 151GW and 151JW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801).(j) On the RH side, between Frame 53.2 and Frame 58 in the AFT cargocompartment, install (if removed) the ceiling panels 152BC, 152DC, 152FC and 152HC (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). (k) At Frame 53.2 in the AFT cargo-compartment, install the partition panel152CW (Refer to AMM 06-41-53, Page Block 001 and AMM Task 25-53-00-400-801). DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 550 6

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

# @A340 SERVICE BULLETIN (l) On the LH side of the belly fairing, install (if removed) the panels 191HB, 191FB, 191KB, 193AB, 195CB, 195DB, 197AT, 197BB and 197EB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802) (m) On the RH side of the belly fairing, install the panels 192BZ, 192CZ, 192HB and 192GB (Refer to AMM Task 53-35-11-400-801 and AMM Task 53-35-13-400-802). (n) If existing, remove the Lower Deck Mobile Crew Rest (LD-MCR) (Refer to AMM Task 25-75-41-400-801). (3) Subtask 364033-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 36-11-34-400-802 Task 36-22-17-400-801 Task 36-22-17-400-802 Task 52-10-00-410-801 52-30-00, Page Block 201 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the FWD cargo-compartment door 821 and AFT cargo-compartment door 822 (Refer to AMM 06-41-52, Page Block 001 and AMM 52-30-00, Page Block 201). (c) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM 52-52-00, Page Block 001). (d) Close the Main Landing Gear (MLG) doors (Refer to AMM Task 32-12-00-410-801). (e) Do the close-up procedure as specified in the installation of the sensing elements (Refer to AMM Task 36-22-17-400-801 and AMM Task 36-22-17-400-802). (f) Do the close-up procedure as specified in the installation of the BMC (FIN 1HA1, 1HA2, 1HA3 and 1HA4) (Refer to AMM Task 36-11-34-400-802). (g) Close the passenger/crew door(s) (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). (i) Restore the systems and the aircraft to normal operating conditions.

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 551 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### B **G H**  **K A** 

FR39 FR45 FR53.5 FR56

(2) 98HF (9) (8) 25HF 24HF (3) (6) 99HF 100HF (4) (5) 102HF
101HF

(7) 23HF Z190 

## BEFORE

**A** (1) 97HF F_SB_364033_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Removal of the Sensing Elements between FR39 and FR55 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 552 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

SCREW WASHER CLAMP SLEEVE SPACER FR44

FR40 FR40.1 FR40.2 FR40.3 FR41 FR42 FR43 FR43 FR42 FR41 FR40.3

FR40.2

FR40.1 (15)
(10)

(11)
(10) (15)

(11) 

## C

**K**

(21) (14) (86) (13) (16) (91) (14) (86) (13) (16) (20) (14) (86) (13) 

## F **E D**  **D D** 

**F D**  **F D** 
**E**
**E E**  (2) 98HF

(1) 

### C **K**

BELLY FAIRING TRACE FUSELAGE TRACE

97HF



## B
F_SB_364033_5_BAAA_02_00 Figure A-FBAAA - Sheet 02 Removal of the Sensing Elements between FR39 and FR55 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 553 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

SCREW WASHER CLAMP SLEEVE SPACER BELLY FAIRING TRACE FUSELAGE TRACE

FR51
FR50
FR49
FR48

FR47
FR46

FR45 FR45 FR46 FR47 FR48

(11) (10) (15)



## L

(21) (14) (86) (13) (16) (20) (14) (86) (13) 

## F **D F**  **D**

**D**

**F**

**F L** 

**F** (6) (4) 101HF

100HF

(3) 99HF 

### F

**D**

**F D** 

**F F**  **L**



## G F_SB_364033_5_BAAA_03_01 Figure A-FBAAA - Sheet 03 Removal of the Sensing Elements between FR39 and FR55 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 554 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

SCREW WASHER CLAMP SLEEVE SPACER FUSELAGE TRACE

(11) (10) (15)



## L

(91) (93) (21) (20) (14) (14) (14) (14) (86) (86) (86) (86) (13) (13) (13) (13) (16) (16) (16) (18) (16) 

## J **N F**  **D** FR51 FR52 FR53 FR53.1 FR53.2 FR53.3 FR53.4 FR53.5 FR53.6

(4) (7) 23HF



### D **F D**  **F F**  **D L** 

(5) 102HF FR53.2

FR52 FR53 FR53.1 FR53.5
FR53.4
FR53.3 

### L

**L**

BELLY FAIRING TRACE 

### J

**F D**  **F F** 

101HF 

### N



## H
F_SB_364033_5_BAAA_04_01 Figure A-FBAAA - Sheet 04 Removal of the Sensing Elements between FR39 and FR55 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 555 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

SCREW WASHER CLAMP SLEEVE SPACER FUSELAGE TRACE (11) (10) (15)



## L

(15)



## P

(91) (21) (20) (14) (14) (14) (86) (86) (86) (13) (13) (13) (16) (16) (16) 

## J **F D**  FR53.6 FR53.7 FR53.8 FR53.9 FR54 FR55 

### P **F D**  **F D**  **D**

**D**

**D J** 
**J D**  (8) (9) 25HF

24HF 

### D



## K F_SB_364033_5_BAAA_05_00 Figure A-FBAAA - Sheet 05 Removal of the Sensing Elements between FR39 and FR55 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 556 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A

(113)

(112)

(114) FR53.5 FR53.6

Z150

F_SB_364033_5_BBAA_01_00 

### B



## A

**B** Figure A-FBBAA - Sheet 01 Removal/Installation of the Ducts between FR53.6 and FR53.7 on the LH side (for Access) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 557 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Z150 FR53.3 FR54

FR53.5

FR53.6 

## AFTER **A**

**B**

**D**

**F** 

## A

**B C**  **E**

F_SB_364033_5_BCAA_01_02 Figure A-FBCAA - Sheet 01 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 558 6

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

# @A340 SERVICE BULLETIN

**CONF ALL SKIN PANEL NOT SHOWN

DIA. 24 mm (0.944 in) RADIUS 2 mm (0.078 in) 13.5 mm MIN. (0.531 in) 13.7 mm MAX. (0.539 in)
2 mm MIN. (0.078 in) 3 mm MAX. (0.118i n) **FWD** 

### A

**A**



## C

**A A**  207 mm (8.149 in)

NEW HOLE EXISTING HOLE

71 mm (2.795 in)

F_SB_364033_5_BCAA_02_02 Figure A-FBCAA - Sheet 02 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 559 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

169

169 155

2SG 1S NEW SENSING REPLACED SENSING

**FWD** 

## D 14 18 168 EXISTING SENSING

169 (155)

169 175 (175)

174 (174) 175 310HF 138HF

137HF 309HF 27

27

3503VS 3593VS

F_SB_364033_5_BCAA_03_02 Figure A-FBCAA - Sheet 03 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 560 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

NEW SENSING EXISTING SENSING

92 27 133

**FWD**



## E 182

F_SB_364033_5_BCAA_04_01 Figure A-FBCAA - Sheet 04 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 561 6

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

# @A340 SERVICE BULLETIN

**CONF ALL EXAMPLE OF INSTALLATION OF WIRE−LOCK PN MS20995C32 (ITEM ) 27



## F F_SB_364033_5_BCAA_05_00 Figure A-FBCAA - Sheet 05 Drilling of a New Hole in the Structure between FR53.5 and FR53.6 on the LH side and Installation of Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 562 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Z190 FR47 FR44 FR40.2

(116)

(115)

F_SB_364033_5_BDAA_01_00 

### A **B**



## A

**B**
Figure A-FBDAA - Sheet 01 Removal/Installation of the Ducts between FR44 and FR47 on the LH side (for Access) DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 563 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A **B** FR44

(119) (123) (124)

### B

**B**

(117) 117

(120) 120 (119) (124)

(121) (118) 118

(119) (122) 

## BEFORE/AFTER Z190



### C

**C A** 
**A** 

## B

F_SB_364033_5_BEAA_01_00 

## A

Figure A-FBEAA - Sheet 01 Replacement of the Web Assy at FR44 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 564 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

**FWD FWD** 

**FWD** 

## A **A B**  **B** (118) 118

(117) 117 (123)

(117) 117



## C **C**

MAT. NO. 09−016B MAT. NO. 09−019B F_SB_364033_5_BEAA_02_00 01 02 **NOTE:** 02 01

02

02

02

Figure A-FBEAA - Sheet 02 Replacement of the Web Assy at FR44 on the LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 565 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A Z150 FR53.3 FR54

FR53.5 FR53.6 96 

### C **B**

**FWD**



## B **A**

F_SB_364033_5_BFAA_01_00 STGR32

STGR33

STGR34

STGR35 STGR36

Figure A-FBFAA - Sheet 01 Installation of a New Bracket between FR53.5 and FR53.6 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 566 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

FR53.5

197 mm (7.75 in)

96

FR53.6 

### D

**F W**  **D**



## D **C**

19.8 mm (0.78 in)

ASNA2050DCJ3215 3.25 mm (0.128 in) 3.35 mm (0.132 in) HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX RIVET VIEW LOOKING DOWN STGR23

STGR33

STGR34 APPLY MAT. No. 09−005A TO THE INTERFACE 01 SEALANT BEAD WITH MAT No. 09−016B. 02 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A. 03 **NOTE:** OF THE NEW BRACKET AND THE STRUCTURE.

03 96 01 02

97 F_SB_364033_5_BFAA_02_01 Figure A-FBFAA - Sheet 02 Installation of a New Bracket between FR53.5 and FR53.6 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 567 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A

98 99



### C Z190 

### B FR44



## A

**A A** 

VIEW LOOKING FORWARD 

## C **B**

F_SB_364033_5_BGAA_01_00 184.5 mm (7.26 in)

Figure A-FBGAA - Sheet 01 Installation of Two New Brackets at FR44 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 568 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

99

98

**F W**  **D** 

## A **A**

ASNA2050DCJ3215 3.25 mm (0.128 in) 3.35 mm (0.132 in) HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX RIVET APPLY MAT. No. 09−005A TO THE INTERFACE 01 SEALANT BEAD WITH MAT No. 09−016B. 02 WET INSTALL THE FASTENERS WITH MAT. No. 09−005A. 03 **NOTE:** OF THE NEW BRACKET AND THE STRUCTURE.

03 01 02 01 02

109 mm (4.29 in)

97 F_SB_364033_5_BGAA_02_01 Figure A-FBGAA - Sheet 02 Installation of Two New Brackets at FR44 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 569 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A Z192 

### B FR39 FR40



## A
(125)

(126)
(127) 

## B F_SB_364033_5_BPAA_01_00 Figure A-FBPAA - Sheet 01 Removal/Installation of the Ducts Between FR39 and FR40 for Access DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 570 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A Z190

FR37 FR39.1 FR39.2 FR58



## A **B**

F_SB_364033_5_BNAA_01_01 Figure A-FBNAA - Sheet 01 Installation of the Supports for the New Harness DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 571 6

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

# @A340 SERVICE BULLETIN

**CONF ALL FR38 FR39 FR39.1 FR39.2 FR40 STGR36 STGR38 STGR40 STGR42 STGR44 STGR46 STGR48 STGR50 STGR52 STGR54 STGR54 STGR52 STGR50 STGR48 STGR46 STGR44 STGR42 STGR40 STGR38 STGR36 A/C C L

**FWD** 

## B 2HR 2M

1M 2MK/2M1K 2SK/2S1K 2MK/2M1K 2S 2M 2SK/2S1K
1HR

1M1M 2SG 1M−2M 1M 2M 1SK/1S2K 1MK/1M2K 1M 1S 1S 2SG

1SK/1S2K 1M 1S 1MK/1M2K 3501VS 3591VS 

### J

**H**

**F G** 

**C D**  **E**

F_SB_364033_5_BNAA_02_01

Figure A-FBNAA - Sheet 02 Installation of the Supports for the New Harness DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 572 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX 3.25 mm (0.128 in) 3.35 mm (0.132 in) RIVET ASNA2050DCJ3215 97 F 

## BEFORE **AFTER**

**AFTER**

HEAD ON HIDDEN SIDE FASTENER NOT AFFECTED F
APPLY MAT. No. 09−005A TO THE INTERFACE 01 WET INSTALL THE FASTENERS WITH MAT. No. 09−013B. 02 **NOTES:** OF THE PARTS AND THE STRUCTURE.

02 FR39.1

(88) (97) FR39.1

97

220 mm (8.66 in) 73 mm (2.87 in) FR39.1

(88) 97 STGR37

STGR38 01 

## C **D**

**E FWD**  **FWD**

**FWD**

F_SB_364033_5_BNAA_03_02 Figure A-FBNAA - Sheet 03 Installation of the Supports for the New Harness DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 573 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX 3.25 mm (0.128 in) 3.35 mm (0.132 in) RIVET ASNA2050DCJ3215 97 F 

## BEFORE **AFTER**

**AFTER**

HEAD ON HIDDEN SIDE FASTENER NOT AFFECTED F APPLY MAT. NO. 09−005A TO THE INTERFACE 01 WET INSTALL THE FASTENERS WITH MAT. NO. 09−013B. 02 **NOTES:** OF THE PARTS AND THE STRUCTURE.

02 FR39.2

(89) (97)

STGR46 POSITIONING FR39.2

97 97

64 STGR46 HOLE FR39.2

STGR46 STGR47 486 mm (19.13 in)

218 mm (8.58 in)

50 mm (1.97 in) 56.5 mm (2.22 in) 63

63

97 97 01 01


## F **G**

**H FWD**  **FWD**

**FWD** 01

F_SB_364033_5_BNAA_04_03 Figure A-FBNAA - Sheet 04 Installation of the Supports for the New Harness DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 574 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD BELLY−FAIRING AREA FUSELAGE CONTOURY2390

Z−2250

HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX 3.25 mm (0.128 in) 3.35 mm (0.132 in) RIVET ASNA2050DCJ3215 97 F 58.4 mm (2.30 in)

13.7 mm (0.54 in) FR39.1

65 97 STGR38

STGR39

STGR40

HEAD ON HIDDEN SIDE FASTENER NOT AFFECTED F
APPLY MAT. NO. 09−005A TO THE INTERFACE 01 WET INSTALL THE FASTENERS WITH MAT. NO. 09−013B. 02 **NOTES:** OF THE PARTS AND THE STRUCTURE. 01

02

**F W**  **D** 

### K



## J

**K**

F_SB_364033_5_BNAA_05_03 Figure A-FBNAA - Sheet 05 Installation of the Supports for the New Harness DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 575 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A FR56 FR53.5



## A FR45

FR39 101 102

113 100 303HF 98HF

302HF

97HF Z190



### B

F_SB_364033_5_BHAA_01_02 Figure A-FBHAA - Sheet 01 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 576 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

FR44

FR43
FR42
FR41
FR40.3
FR40.2
FR40.1 FR40 FR40.2 FR40.3 FR41 FR42 FR43

FR40.1

FR40

BELLY FAIRING TRACE FUSELAGE TRACE

114 97HF 101 303HF

113 302HF

102 98HF 

### L

**J**

**C G** 

**E**

30

11

TYPICAL 

## P OR

15 27

15 27 27 15 15 

## B

**Q** F_SB_364033_5_BHAA_02_01 Figure A-FBHAA - Sheet 02 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 577 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### R **C C**  **C C**  **C C**  **H D**  **B B** 

**P Q** 

**P Q**  **FWD**

**FWD** VIEW LOOKING AFT 

### C **C**
**C C** 

**C C**  **B**

**B** FR39.2

FR40



## C **D** 113

114 302HF

97HF 

### F 

## E

13

14 20 10 1013

14 20 14 20 13

14 16 21 10 14 20 13

14 20 10 78 

## F 33
32 35

34 30 33 32

30



## G **H** FR40.2 FR40.1 FR40

F_SB_364033_5_BHAA_03_01 Figure A-FBHAA - Sheet 03 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 578 6

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# @A340 SERVICE BULLETIN

**CONF ALL

13

10 14 20 18 10 13

14 24 16

13 10 14 21 FR41 FR40.3 FR40.2



### K 101 303HF

**FWD**


### D

**D A** 

**A A** 

**A A** 

**A B** 

**B** FR44 FR43 FR42



### N
**FWD** 10 13 14 20

13 14 20

10 13 14 20 14 20 14

13 10 14 16

13 10 70

10 13 14 18 24

18

13 14 24 18

13 10 10
14 24 79

14 29

1013 14 29

TYPICAL 

## R **S**

**N K**  **J**

**L**

**A A**  **B B**  **C C**  **D D**  10 

### S **A**

**A A** 

**A A** 

**A A** 

**A A** 

**A**
102 98HF 21 20

F_SB_364033_5_BHAA_04_00 Figure A-FBHAA - Sheet 04 Installation of the New Sensing Elements between FR39 and FR44 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 579 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A Z190

FR56 FR53.5

FR39 

## AFTER

114 105 103 103 100HF 305HF 99HF 304HFFR45



## A **B**

F_SB_364033_5_BJAA_01_02 Figure A-FBJAA - Sheet 01 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 580 6

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

# @A340 SERVICE BULLETIN

**CONF ALL FR48 FR47 FR46 FR45

FR51
FR50

FR49

FR48

FR47
FR46
FR45 

### N

**L**

**F**

**C H**  **K** FUSELAGE TRACE

BELLY FAIRING TRACE 114 100HF 105 305HF

99HF 103

30

11
TYPICAL INSTALLATION 

## B OR 27

15 27 15

27

15 15



## T 103 304HF


## S TYPICAL INSTALLATION F_SB_364033_5_BJAA_02_01 Figure A-FBJAA - Sheet 02 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 581 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

39 38 36

37 39

38 40

41 

### C

**C E**  **E**

**C C** 

**E E** 

**Q**

**C C** 

**C C** 

FR45 FR44

VIEW LOOKING FORWARD FR46 VIEW LOOKING FORWARD

VIEW LOOKING AFT

**FWD FWD** 

**FWD FWD**  **FWD** 2POS

36

37 103

103 99HF

304HF 

### E

**J**

13 13 13 10 13 14 20 14 16 21 14 18 23 14 20 14 20 

## G

2POS 10 13 14 20 34

35 

## D

**E**

**J H**  **D**



## C

**S T** 



## N **Q Q** 

30 30 

### C **C**

10 10 81

10 10 13 14 20



### T



## K **S T**  **G**

**C C** 



## F

F_SB_364033_5_BJAA_03_02 Figure A-FBJAA - Sheet 03 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 582 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### P **Q** 105 114



### G **G**

**A A**  **A**

**A C**  **C**
**C C** 

**FWD**



## L **P**

**R R**  

## Q TYPICAL INSTALLATION 

### A

**A A** 

**A A** 

**A** FR50 FR49 FR48 FR47

13 10

14 20 14 20 14 20 13 10 13 10

14 20

79 14 29 80

14 29 13

10

13

14 20 10 16 10

13 14 21 17 10

13 14 26 16

18 10

13 14 19 

## A **A C**  **C E**  **E G**  **G** 100HF

305HF

F_SB_364033_5_BJAA_04_01 Figure A-FBJAA - Sheet 04 Installation of the New Sensing Elements between FR44 and FR50 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 583 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### B **A** Z190

FR56 FR53.5

FR45

FR39 

## AFTER 106 107 102HF 307HF
106 106 101HF 306HF

108 104 23HF 308HF



## A
F_SB_364033_5_BKAA_01_01 Figure A-FBKAA - Sheet 01 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 584 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

FR52 FR53 FR53.1 FR53.2 FR53.4 FR53.5 307HF

306HF

101HF FUSELAGE TRACE

FR51 FR52 FR53 FR53.1 FR53.2 FR53.3 FR53.4 FR53.5 FR53.6

106 106 107 108 23HF 104 308HF 

### M

**C**


## OR **G H** 

11 15 27

15 27 27 15

30 25 OR

TYPICAL 

## B **X Y**  FR53.3

BELLY FAIRING TRACE 102HF 106

15

F_SB_364033_5_BKAA_02_01 Figure A-FBKAA - Sheet 02 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 585 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### J **K** FR53.2 FR53.3 FR53.4 

### A

**A A**  **A D**  **A**

**A F**  FR51 FR52 FR53 FR53.1 

### C

**C C** 

**C C** 

**C**

14 20 14 20 14 20 70 10 10 10 13 13



## K 72 13 10

14 16 21

13 13 10 10 10

14 20 75 14 16 21 14 16 21 13 13 10 10



## E 82 

## F 14 20 14 16 21 14 20

13 10 13 10

14 20 14 16 21 74 

## J 14 16 21 14 20 13 10 13 10 83

73 14 20 

## L 13 

### A

**A A** 

**A A** 

**A** FR53.2

**FWD** 

## C **X Y** 

42

43 30 40

41 106 101HF

106 306HF 

## G 14 20 14 20



## D

**L** 

## H 13

14 29 14 20 

### E

F_SB_364033_5_BKAA_03_00 Figure A-FBKAA - Sheet 03 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 586 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

10 13

14 20 77 14 29

14 29 13 84 10

14 20

14 20 14 22 28

10 13 10 13 14 20

76 STGR36 STGR37 STGR38 STGR39 STGR40 STGR41 STGR42 STGR43 STGR44 STGR45 STGR46 STGR47 STGR48 STGR49 STGR50 FR53.5 FR53.6



### C

**C C**  **C C** 

**C T** 

**FWD** 

## N 43

42 45

44 30 

### X **Y**



## R **S**
**T**

**C C** 

**C C** 

**C C** 

**B B** 
**N**
**P**

**Q R**  **C C** 

**T** 107

106 307HF

102HF104

108 308HF

23HF

VIEW LOOKING FORWARD 

## M 79 14 29

13

10 14 29


### U 

## T **U**

18

10 13

14 24 16

13 10 14 21 13

10 14 20 

## A **A B**  **B C**  **C P** 

**Q**

45 44 25 

### X



## S **Y**

F_SB_364033_5_BKAA_04_00 Figure A-FBKAA - Sheet 04 Installation of the New Sensing Elements between FR50 and FR53.6 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 587 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### B **A**

FR56 FR53.5

FR45

FR39 

## AFTER

112 111 109 110 312HF 25HF 24HF 311HF Z190



## A F_SB_364033_5_BLAA_01_01 Figure A-FBLAA - Sheet 01 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 588 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



## OR 27

15 27 15

27

15 30

11



## P **J**

**C** 109 24HF 312HF

TYPICAL 

## N FUSELAGE TRACE 112

FR53.6 FR53.7 FR53.8 FR53.9 FR54 FR55



## B 111 25HF

110 311HF 15

F_SB_364033_5_BLAA_02_00 Figure A-FBLAA - Sheet 02 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 589 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### N **F**

89
30 91

90 88 **FWD**



## H 27 

### J **J** 10 14 20

13

14 20 93 10 14 20

13


## F

14 29 79

13 10 14 29



## G **FWD** 

### D **D**

**A A** 
**H H**  13 14 20 86



## D

VIEW LOOKING FORWARD 

### G



## E **C C** 

**D D** 

**B B** 

**G G** 

**D D** 

**B B**  **B B**  **D**

**D D**  **D B**  **B D**  **D E**  112 312HF

111 25HF 108 24HF

110 311HF 

## C **FWD**

**FWD** 92 27 85



## J **J H**  **H** 55° 27 

### D

**D D**  **F**

F_SB_364033_5_BLAA_03_00 

### E

**E**

Figure A-FBLAA - Sheet 03 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 590 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

FR53.9 FR55



### L **K** FR54 

### D

**D D** 

**D**

14 16 94
14 20 14 20 10 10 13

14 16 94 13

95 13

10

14 16 94 10

14 16 94 14 16 94 13 13

10 

## J

**K L**  13 10 14 87 17
13

10 14 26 17
13 10 14 26

10

14 20 13 13

14 21 10 16

14 87

13 86 18 13 1014 20

13 10

14 20 13



## G **G E**  **E D**  **D C**  **C B**  **B A**  **A** 18

70

F_SB_364033_5_BLAA_04_00 Figure A-FBLAA - Sheet 04 Installation of the New Sensing Elements between FR53.6 and FR55 on LH side DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 591 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



### A

3520VP 3672VC

3506VC 3520VC NEW HARNESS 2SG SPARES CONDUITS
2S



## A 301HF FR37 FR39.1 FR39.2 FR56FR57 FR58 Z190



### B **C**

F_SB_364033_5_BMAA_01_01 Figure A-FBMAA - Sheet 01 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 592 6

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

# @A340 SERVICE BULLETIN

**CONF ALL FR38 FR39 FR39.1 FR39.2 FR40 STGR36 STGR38 STGR40 STGR42 STGR44 STGR46 STGR48 STGR50 STGR52 STGR54 STGR54 STGR52 STGR50 STGR48 STGR46 STGR44 STGR42 STGR40 STGR38 STGR36 A/C C L 

## BEFORE

2HR 2M 2S 1M 2MK/2M1K 2SK/2S1K 2MK/2M1K 2S 2M 2SK/2S1K
1HR

1M 1M−2M 1M 2M 1SK/1S2K 1MK/1M2K 1M 1S 1S

1SK/1S2K 1M 1S 1MK/1M2K

3501VS1M

**FWD** 

## B **F D** 

**H J** **K**

**M**

**N Q**  **Y**

**A E**  **A C A A**  **W T** 

F_SB_364033_5_BMAA_02_01 Figure A-FBMAA - Sheet 02 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 593 6

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

# @A340 SERVICE BULLETIN

**CONF ALL FR38 FR39 FR39.1 FR39.2 FR40 STGR36 STGR38 STGR40 STGR42 STGR44 STGR46 STGR48 STGR50 STGR52 STGR54 STGR54 STGR52 STGR50 STGR48 STGR46 STGR44 STGR42 STGR40 STGR38 STGR36 A/C C L 

## AFTER

2HR 2M 2S 1M 2MK/2M1K 2SK/2S1K 2MK/2M1K 2S 2M 2SK/2S1K 1HR

1M1M 2SG 1M−2M 1M 2M 1SK/1S2K 1MK/1M2K 1M 1S 1S 2SG

1SK/1S2K 1M 1S 1MK/1M2K NEW HARNESS

NEW HARNESS

NEW HARNESS 3501VS 3591VS

**FWD** 

## C **G**

**A L**  **A M**  **L**
**A N P**  **R Z**  **S U** 
**V X**  **A B A D** 

**A F**  **A G**  **E**

F_SB_364033_5_BMAA_03_02 Figure A-FBMAA - Sheet 03 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 594 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD 

## BEFORE

**D**

1SY2390

Z−2250

1S FUSELAGE CONTOUR

BELLY−FAIRING AREA

3501VS FR39.1 STGR38

STGR39

STGR40



### A

**A A** 

**A A**  **A**

**A**

**A A** 

**A A**  **A A** 

**A A**  **Q**
**A P** 



## A **P FWD**  F_SB_364033_5_BMAA_04_02 Figure A-FBMAA - Sheet 04 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 595 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD 

## AFTER

**E**

2SG

1SY2390

Z−2250

2SG 1S FUSELAGE CONTOUR

BELLY−FAIRING AREA

3591VS 3501VS FR39.1 STGR38

STGR39

STGR40



### C **C B** 

**B B** 

**B B**  **B**

**B B**  **B**

**B B** 

**B B** 

**B** 

## A **J A**  **J A K** 

**FWD** F_SB_364033_5_BMAA_05_02 Figure A-FBMAA - Sheet 05 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 596 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE

**AFTER** VIEW LOOKING FORWARD

VIEW LOOKING FORWARD 

## A **A**

**B B**  **C C**  1S (130) (131) (150)

2SG

1S 150 152 131 154 151

(150) 2SG 1S 151 131 154

65 152 150 150

**FWD** F_SB_364033_5_BMAA_06_02 Figure A-FBMAA - Sheet 06 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 597 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE

**FWD** 

## A H **G G**  **F**

**F**

F_SB_364033_5_BMAA_07_00 Figure A-FBMAA - Sheet 07 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 598 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## AFTER

**A K H** 

**H**

**FWD** 2SG



### J **J**

F_SB_364033_5_BMAA_08_02 Figure A-FBMAA - Sheet 08 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 599 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING FORWARD



## BEFORE **AFTER BEFORE** 

**AFTER**

**F G**  **F F**  **G G** 

**H H**  **J J**  1S

2SG

1M 1S 1S

(135) (134)

(136) (137) (150)
(130) (131)

(150)
152
131 154 151 150 1S

1S

2SG

1S 2SG 1M (135) (134)

152 150 131 154 151 (132) (133) (155)

151

(155)
150 152

131 154 **FWD**

**FWD FWD**  **FWD FWD** 

F_SB_364033_5_BMAA_09_02 Figure A-FBMAA - Sheet 09 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 600 6

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# @A340 SERVICE BULLETIN

**CONF ALL

STGR45

1M STGR45

1M FR39.1

FR39.1 

## BEFORE

**AFTER H** 

**A L**  **K K** 

**M M**  **L L** 

**N N**  **FWD**

**FWD** F_SB_364033_5_BMAA_10_00 Figure A-FBMAA - Sheet 10 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 601 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE

**AFTER K**  **K**

**M M** 



## OR

OR 1S 1M
1M 2SG 1S 1M
1M (135)

(138) (151) (134)

(152) (153) (154)

(151) (134) (152)
150 131 154 (135)

(138) 1S

1M1M

2SG 1S 1M

1M 1M

1M (135) (138) (151) (153) (154) (134) (152) (139)

131 (135) (139) (134)

173
(138) 150 163

154 **FWD**

**FWD** F_SB_364033_5_BMAA_11_02 Figure A-FBMAA - Sheet 11 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 602 6

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# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE

**AFTER L**  **L**

**N N**  1S 1M

2SG 1S 1M (135) (134)

(153) (130)

(134)

152

150 151 (135)

131 154 **FWD**

**FWD** F_SB_364033_5_BMAA_12_02 Figure A-FBMAA - Sheet 12 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 603 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



## OR

OR **BEFORE**

**AFTER J** 

**A M**  STGR49

STGR48

STGR47 

### Q **Q**

**P P**  FR39.1 FR39.2

STGR49

STGR48

STGR47 FR39.1 FR39.2 **FWD**

**FWD** 

### S **S**

**R R**  STGR49

STGR48

STGR47 

### P **P** FR39.1 FR39.2

STGR49

STGR48

STGR47 FR39.1 FR39.2



### R **R**

F_SB_364033_5_BMAA_13_02 Figure A-FBMAA - Sheet 13 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 604 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



## OR

OR **BEFORE**

**AFTER P**  **P**

**R R**  1S

1M 1M

2SG 1S 1M

1M (135) (139) (151) (153) (154) (152) (134)

(135) (139) 151 (134) (152)

150 131 154 1S

1M1M

1M (135)
(138) (151) (153) (154) (134) (152) (139)

2SG 1S 1M

1M 1M

131 (135) (139) (134)

173
(138) 150 163

154 **FWD**

**FWD** F_SB_364033_5_BMAA_14_02 Figure A-FBMAA - Sheet 14 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 605 6

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# @A340 SERVICE BULLETIN

**CONF ALL



## AFTER **BEFORE**

**Q Q** 

**S S**  

## OR

OR 1S 1M

1M

2SG

**FWD** 1M 1S

1M (134)

(139) (152) (135)

(151)

(151)
(139) (152) 150 (134) (135) (153) (154)

153 154 **FWD** 1S 1M

1M

2SG 1M 1S

1M (134)

(139) (152) (135)

(144)

163
(139) 173 150 (134) (135) (153) (154)

153 154 1M (138)

1M (138)

F_SB_364033_5_BMAA_15_02 Figure A-FBMAA - Sheet 15 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 606 6

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# @A340 SERVICE BULLETIN

**CONF ALL



## AFTER **K**

**L** 

## BEFORE

1M FUSELAGE CONTOUR

1M
2SG

**FWD** FUSELAGE CONTOUR (138) (132) (153)

(138)

150 151 152 131 154 **FWD**

F_SB_364033_5_BMAA_16_02 Figure A-FBMAA - Sheet 16 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 607 6

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# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE **AFTER**

**M**



## BEFORE **AFTER**

**T T**  **U U**  **A N** STGR54



### T **T**

**FWD**

1M

1M (140) (141) (138)

(153) (154)
**FWD** 1M

1M 2SGSTGR54



### U **U**

**FWD**

(140) (141)

150 (138)

131 154
**FWD** F_SB_364033_5_BMAA_17_02 Figure A-FBMAA - Sheet 17 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 608 6

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# @A340 SERVICE BULLETIN

**CONF ALL 

## BEFORE **AFTER**

**BEFORE AFTER** 

**AFTER N**  **P**

**R**

**S Q**  1M

1M

(138) (142) (153)

(138)

(142) (153) **FWD**

**FWD** 2SG 1M

1M 2SG (138) 152

150 151

131 154

(138) 150

153 158 **FWD**

**FWD**

131 159 150

**FWD** 2SG 63

F_SB_364033_5_BMAA_18_02 Figure A-FBMAA - Sheet 18 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 609 6

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

# @A340 SERVICE BULLETIN

**CONF ALL



## V 

## AFTER

2S

2M 2SG

2SG 

### V **V W**  **W**



## V **V** 1S

179 141 171 172 FUSELAGE CONTOUR

2S 179 171 172

14164 180 180 181 181 

## W **W** 2M FUSELAGE CONTOUR

2S 134
135 163 16 152 153 154 64 **FWD**

**NOTE:** ONLY ONE CONFIGURATION SHOWN. EQUIPMENT MAY DIFFER DEPENDING ON AIRCRAFT CONFIGURATION. F_SB_364033_5_BMAA_19_04 Figure A-FBMAA - Sheet 19 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 610 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## AFTER **BEFORE**

**T U** 

**W X** 

**Y Z**  2S 2M FUSELAGE CONTOUR

2MK/2M1K (135) (134) (136) (153)

2S 2M FUSELAGE CONTOUR

(135) (134) (136) (153)

FUSELAGE CONTOUR

(133) (143) 2SK/2S1K

(155) (155) 2S 2M

2SK/2S1K FUSELAGE CONTOUR

151 141 165 (135) (134)
153 154

2M FUSELAGE CONTOUR

2SG

2S

2SG FUSELAGE CONTOUR

2MK/2M1K

(155) (155) 152 22 163

150 131 154 157 16 152 (135)

176
153 154 177 178

F_SB_364033_5_BMAA_20_02 Figure A-FBMAA - Sheet 20 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 611 6

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

# @A340 SERVICE BULLETIN

**CONF ALL 

## AFTER **BEFORE**

(153) 

## A A **A B**

**A D A C** 

**A F**  **A E**  2S 2M FUSELAGE CONTOUR

(135) (134) (136) (153)

2S 2M FUSELAGE CONTOUR

(135) (134) (136) (153)

2M (135)
(142) (88) **FWD**

**FWD**

**FWD** 2M FUSELAGE CONTOUR

151

(135) 153 154

FUSELAGE CONTOUR 2SG

2S

176 18

2SG 2S

176 2M

(135) 153 167

2M (135)

153 158 **FWD**

(88) 177

177 178

178

**FWD**

**FWD** F_SB_364033_5_BMAA_21_05 Figure A-FBMAA - Sheet 21 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 612 6

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# @A340 SERVICE BULLETIN

**CONF ALL

(4 POS) (4 POS) (4 POS)

(3 POS) 14

170
(184) (183) 166

(184) (14) (170) (166)

184 183
184 **NOTE:** ONLY ONE CONFIGURATION SHOWN. EQUIPMENT MAY DIFFER DEPENDING ON AIRCRAFT CONFIGURATION. 

### A H

**FWD** 

## A **G**

**A H** F_SB_364033_5_BMAA_22_01 Figure A-FBMAA - Sheet 22 Installation of the New Harness 2SG DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 613 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 01 Modification of the Wiring in the Main Rack 800VU DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 614 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 02 Modification of the Wiring in the Main Rack 800VU DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 615 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 03 Modification of the Wiring in the Main Rack 800VU DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 616 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 851VU 1HA1−AB 12A 3612−0097 1M CF24 851VU 2901VT 65E D 2 851VU 2901VT 65F 3612−0072 1M CF24 801VU 2615VC 19 D 3 851VU 2901VT 65M 3612−0078 1M CF24 852VU 1HA2−AA 11D D 4 851VU 2901VT 65V 3612−0098 1M CF24 852VU 1HA3−AB 12A D 5 851VU 2901VT 65N 3612−0099 1M CF24 852VU 1HA4−AB 12A D 6 7 8 9 851VU 2901VT 54X EN3155−016M2222 3612−0078 1M CF24 2000 80 851VU 1HA2−AA 11D E0170FA2200 (a) A 10 851VU 2901VT 54S EN3155−016M2222 3612−0097 1M CF24 1500 60 851VU 1HA1−AB 12A E0170FA2200 (a) A 11 851VU 2901VT 54R EN3155−016M2222 3612−0111 1M CF24 1500 60 851VU 1HA1−AA 11D E0170FA2200 (a) A 12 851VU 2901VT 54T EN3155−016M2222 3612−0112 1M CF24 3000 120 851VU 1HA2−AB 12A E0170FA2200 (a) A 13 851VU 1HA1−AB 11A E0170FA2200 3612−0110 1M CF24 2500 100 851VU 2947VG GND EN3155−015F2018 (a) A 14 851VU 1HA2−AB 11A E0170FA2200 3612−0113 1M CF24 3000 120 851VU 2947VG GND EN3155−015F2018 (a) A 15 851VU 2901VT 54Y EN3155−016M2222 3612−0072 1M CF24 2500 100 801VU 2615VC 19 EN3155−014M2018 (a) A 16 851VU 2901VT 54U EN3155−016M2222 3612−0098 1M CF24 3000 120 852VU 1HA3−AB 12A E0170FA2200 (a) A 17 851VU 2901VT 54V EN3155−016M2222 3612−0099 1M CF24 3500 140 852VU 1HA4−AB 12A E0170FA2200 (a) A 18 851VU 1HA1−AA 7B E0170FA2200 3622−0538 2S CF24 6000 240 804VU 2712VC 55 EN3155−008M2222 (a) A 19 851VU 1HA1−AA 8B E0170FA2200 3622−0539 2S CF24 6000 240 804VU 2712VC 72 EN3155−008M2222 (a) A 20 21 22 23 24 25

(a) = BUNDLE F9000095227895 GND = GROUND A = ADDED WIRE D = DELETED WIRE Figure A-FCAAA - Sheet 04 Modification of the Wiring in the Main Rack 800VU DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 617 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Figure A-FCBAA - Sheet 01 Modification of the Wiring between the Cargo Compartment and the Avionics Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 618 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 132 3506VC−A 69 EN3155−003F2222 3622−0542 2S CF24 35000 1400 152 3672VC−A 37 EN3155−003F2222 (a) A 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

(a) = BUNDLE F9000095227895 A = ADDED WIRE Figure A-FCBAA - Sheet 02 Modification of the Wiring between the Cargo Compartment and the Avionics Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 619 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

Figure A-FCCAA - Sheet 01 Installation of the Wiring of the New Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 620 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 132 3520VC−A 66 EN3155−003F2222 3622−0540 2S DK22 25000 1000 137 3520VP / (a) A 2 137 3520VP / 193 3591VS A NSA936809RG0002 (a) A 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

(a) = BUNDLE F9000095227895 A = ADDED WIRE Figure A-FCCAA - Sheet 02 Installation of the Wiring of the New Sensing Elements DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 621 6

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

# @A340 SERVICE BULLETIN

**CONF ALL **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) GET ACCESS MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 184.00 90.00 STEPS 20.00 5.00

5 10 15 20 25 30 90 0 TESTS 4.00 4.00 CLOSE−UP 28.00 7.00

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MANHOURS GIVEN IN VENDOR SERVICE BULLETINS ARE NOT REFLECTED IN THIS GANTT CHART. 01 02 **NOTES:** PER

4

1 4

: : 85 REMOVAL OF SENSING ELEMENTS FR39−FR44 4.00 4.00 1

35 40 45 50 55 60 65 70 75 80 REMOVAL OF SENSING ELEMENTS FR44−FR51 4.00 4.00 1 REMOVAL OF SENSING ELEMENTS FR51−FR53.6 4.00 4.00 1 REMOVAL OF SENSING ELEMENTS FR53.6−FR55 4.00 4.00 1 REMOVAL OF DUCTS FR53.5−FR53.6 1.00 1.00 1 DRILLING OF NEW HOLE FR53.5−FR53.6 1.00 1.00 1 INSTALLATION OF SUPPORT FR53.5−FR53.6 1.00 1.00 1 INSTALLATION OF DUCTS FR53.5−FR53.6 2.00 2.00 1 REMOVAL OF DUCTS FR43−FR45 1.00 1.00 1 REPLACEMENT OF WEB ASSY FR44 3.00 3.00 1 INSTALLATION OF BRACKET FR44 1.00 1.00 1 INSTALLATION OF DUCTS FR43−FR45 2.00 2.00 1 INSTALLATION OF SENSING ELEMENTS FR39−FR44 14.00 14.00 1 INSTALLATION OF SENSING ELEMENTS FR44−FR50 14.00 14.00 1 INSTALLATION OF SENSING ELEMENTS FR50−FR53.6 21.00 21.00 1 INSTALLATION OF SENSING ELEMENTS FR53.6−FR55 14.00 14.00 1 REMOVAL OF DUCTS FR39−FR40 1.00 1.00 1 INSTALLATION OF SUPPORT FR39.1−FR39.2 3.00 3.00 1 INSTALLATION OF INTERCONNECTING ELECTRICAL WIRE 3.00 3.00 1 INSTALLATION OF NEW HARNESS 2SG 26.00 13.00 2 INSTALLATION OF THE WIRING 2.00 2.00 1 MODIFICATION OF THE WIRING IN 800VU 4.00 2.00 2 INSTALLATION OF DUCTS FR39−FR40 2.00 2.00 1

F_SB_364033_5_AAAA_01_01 Figure A-FAAAA - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 622 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003 thru 004

TYPICAL PLACARD INSTALLATION AD

TYPICAL 5704VB /2S

FR18 FR19 FR37.1 FR38



### B



## B**C** FR26 FR29



## C SB 36−4033 2712VCA /2S 3520VC /2S 3506VC /2S



## A **A**

Z130

**NOTE:** TIED TOGETHER WITH ITEMS, 404, 405 OR 406 01 01

TO EXISTING CABLE HARNESS F_SB_364033_6_BAAA_01_00 400

404 405 406

402 405 406 407

Figure A-GBAAA - Sheet 01 Installation of the Electrical Wiring in the FWD Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 623 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL PLACARD INSTALLATION TYPICAL 

## B **C** SB 36−4033 

### A

Z130

**NOTE:** TIED TOGETHER WITH ITEMS, 404, 405 OR 406 01 TO EXISTING CABLE HARNESS 5704VB /2S

FR18 FR19 FR37.1 FR38

FR26.1 FR26.2


### B

**C** AD 2712VCA /2S 3520VC /2S 3506VC /2S



## A

405 406 407 404 405 406

402

F_SB_364033_6_BAAE_01_00 401 01

Figure A-GBAAE - Sheet 01 Installation of the Electrical Wiring in the FWD Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 624 6

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

# @A340 SERVICE BULLETIN

**CONF 002

TYPICAL PLACARD INSTALLATION TYPICAL 

## B **C** SB 36−4033 

### A

Z130

**NOTE:** TIED TOGETHER WITH ITEMS, 404, 405 OR 406 01 TO EXISTING CABLE HARNESS 5704VB /2S

FR18 FR19 FR37.1 FR38

FR26.1 FR26.2


### B

**C** AD 2712VCA /2S 3520VC /2S 3506VC /2S



## A

F_SB_364033_6_BAAB_01_00 400

405 406 407 404 405 406

402 01

Figure A-GBAAB - Sheet 01 Installation of the Electrical Wiring in the FWD Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 625 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

**NOTE:** TIED TOGETHER WITH ITEMS, 404, 405 OR 406 01 TO EXISTING CABLE HARNESS TYPICAL PLACARD INSTALLATION TYPICAL 

## B FR80

FR55 FR54

AD 5866VB /2S 

### D **E**

**C B** 



## A 3672VC /2S 5208VP 5866VB /2S Z170 Z160 Z150 

### A

01

SB 36−4033

F_SB_364033_6_BBAA_01_00 

## C 400

404 405 406

402 405 406 407 /82

Figure A-GBBAA - Sheet 01 Installation of the Electrical Wiring in the AFT Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 626 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

5866VB /2S FR80



## E 5866VB /2SF FR80 5866VB /2S 5866VB /2SF

ALTERNATIVE 

## D

F_SB_364033_6_BBAA_02_00 (403)

(403) /82

/82

Figure A-GBBAA - Sheet 02 Installation of the Electrical Wiring in the AFT Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 627 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BBAE_01_00 **NOTE:** TIED TOGETHER WITH ITEMS, 404, 405 OR 406 01 TO EXISTING CABLE HARNESS TYPICAL PLACARD INSTALLATION TYPICAL 

## B FR80

FR55 FR54

AD 5866VB /2S 

### D **E**

**C B** 



## A 3672VC /2S 5208VP 5866VB /2S Z170 Z160 Z150 

### A

01

SB 36−4033 

## C 401

405 406 407 404 405 406

402 /82

Figure A-GBBAE - Sheet 01 Installation of the Electrical Wiring in the AFT Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 628 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BBAE_02_00 5866VB /2S FR80



## E 5866VB /2SF FR80 5866VB /2S 5866VB /2SF

ALTERNATIVE 

## D(403)

(403) /82

/82

Figure A-GBBAE - Sheet 02 Installation of the Electrical Wiring in the AFT Cargo Compartment DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 629 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

/82 FR80 FR83 FR84 FR90 FR91 FR93 5866VB /2S



### B **C F**  **X** Z310 

### A

F_SB_364033_6_BCAA_01_00 5208VP 5151VS

5215VC



## A

Figure A-GBCAA - Sheet 01 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 630 6

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# @A340 SERVICE BULLETIN

**CONF 001 thru 004

VIEW LOOKING AFT VIEW LOOKING AFT

ALTERNATIVE 5208VP

5208VP 5866VB /2S 5866VB /2S FR80

FR80/82 /82



## B

**C D** 

**E**

F_SB_364033_6_BCAA_02_00 Figure A-GBCAA - Sheet 02 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 631 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

(4 POS) (8 POS) (8 POS) (4 POS) (4 POS) (4 POS)



## D

(4 POS) (6 POS) (6 POS) (4 POS) (4 POS) (4 POS)



## E ALTERNATIVE (2 POS) (2 POS)

F_SB_364033_6_BCAA_03_00 (416) (417) (418) (417) (419)

(415) (420) (410)

(411)

(410)

(411) (416) (417) (418) (417) (419)

(415) (417) (423) (420)

Figure A-GBCAA - Sheet 03 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 632 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

VIEW LOOKING UP **FWD** FR91 FR90

STGR6LH STGR10LH

STGR6RH

STGR10RH AD 

### G **L M** 

**N P** 

**T**

**T**
**U**

**V W** 


## F F_SB_364033_6_BCAA_04_00 (450)

Figure A-GBCAA - Sheet 04 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 633 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## G VIEW LOOKING AFT 5866VB /2S 

### H **J**

**K**



## J

5215VC (4 POS) (4 POS) (4 POS) 

## H

**K**
F_SB_364033_6_BCAA_05_00 (353)

(417) (314)

(419) (417) (314) (432) (431) (430) (437)

(437) (437)

(435)

Figure A-GBCAA - Sheet 05 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 634 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## M

**N NOTE:**  IF INSTALLED 01 01

01

F_SB_364033_6_BCAA_06_00 

## L (442) (437) (437) (437) (437)

(437) (437) (417) (444) (417)
(444)
(419)

(417)

(314)

Figure A-GBCAA - Sheet 06 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 635 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## P FR91

FR90 5866VB /2S 

### Q **R**
**S**



## Q

**R**
**S** ALTERNATIVE

F_SB_364033_6_BCAA_07_00 (437)

(437)

(437) (437)

(437) (437)

(442) (437) (442) (417)(314) (448)

(417) (501) (439) (419)

(417) (444)

Figure A-GBCAA - Sheet 07 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 636 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

TYPICAL 

## T **U**

**W V** 
F_SB_364033_6_BCAA_08_00 (437)

(437) (437)

(437)

(437) (437) (437) (443)

(417) (314) (314) (417)
(417)
(314)

(442)

(417) (444) (417) (314)

Figure A-GBCAA - Sheet 08 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 637 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

FR93
STGR5RH
STGR6RH

STGR7RH

STGR9RH 5865VB /1S FR91 FR92 FR93

STGR5RH 5856VB /1S

STGR10RH

VIEW LOOKING FWD

TYPICAL 

## X **Y Y** 

**Z**



## Z **Z**

**A A A B** 

F_SB_364033_6_BCAA_09_00 (479) (480) (481)

(448)
(417) (501) (442) (437) 5151VS 5865VB /1S

Figure A-GBCAA - Sheet 09 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 638 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## A A

**A B**

F_SB_364033_6_BCAA_10_00 (437)

(437)

(437) (437) (464)

(417) (470)

(449)
(471)

(419)

(465)

Figure A-GBCAA - Sheet 10 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 639 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

F_SB_364033_6_BCAE_01_00 /82 FR80 FR83 FR84 FR90 FR91 FR93 5866VB /2S



### B **D V** 

5208VP 5151VS

5215VC



## A

Figure A-GBCAE - Sheet 01 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 640 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_02_00 VIEW LOOKING AFT 5208VP 5866VB /2S FR80/82



### C

(4 POS) (6 POS) (6 POS)

(4 POS) (4 POS) (4 POS)

(2 POS) (2 POS) (2 POS) (2 POS) (6 POS) (6 POS)



## C**B**

(417) (417) (426) (418) (417) (419)

(415)
(419) (417) (417) (427) (420)

(412) (412) (419)

Figure A-GBCAE - Sheet 02 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 641 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_03_00 VIEW LOOKING UP **FWD** FR91 FR90

STGR6LH STGR10LH

STGR6RH

STGR10RH AD 

### J **K**

**L M** 

**R**

**R**
**S**

**T U** 


## D (502) 

### E

Figure A-GBCAE - Sheet 03 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 642 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_04_00 VIEW LOOKING AFT 5866VB /2S

5215VC (4 POS) (4 POS) (4 POS) 

## E

**F F** 



## G **G**

**H**



## H (353)

(417) (314)
(417) (314) (419) (432) (431) (430) (437) (437)

(433) (437)

Figure A-GBCAE - Sheet 04 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 643 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_05_00

**NOTE:** IF INSTALLED 01 01

01 

## K

**L J**  (417) (444) (417)
(314)
(419)

(417)

(314) (437) (442) (437)

(437) (437)

(437) (437)

Figure A-GBCAE - Sheet 05 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 644 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_06_00 FR91

FR90 5866VB /2S

ALTERNATIVE 

## M **N**

**Q N**  **P**
**Q**



## P (448) (417)(314)

(417) (501) (439) (419)

(417) (444) (437) (437)

(437) (442) (437)

(437)

(437)
(442) (437)

Figure A-GBCAE - Sheet 06 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 645 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_07_00 TYPICAL 

## R **S**

**U T** (417)
(314) (417) (314) (443)

(417) (314)

(417) (314) (417) (444) (437) (437) (437)

(437)

(437) (442) (437) (437)

Figure A-GBCAE - Sheet 07 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 646 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_08_00 FR93
STGR5RH
STGR6RH

STGR7RH

STGR9RH 5865VB /1S FR91 FR92 FR93

STGR5RH 5856VB /1S

STGR10RH

VIEW LOOKING FWD

TYPICAL 

## V **W W**  **X**

**X**



## X **Y Z**  (479) (480) (481)

(439)
(417) (501) (442) (437) 5151VS 5865VB /1S

Figure A-GBCAE - Sheet 08 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 647 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BCAE_09_00 

## Y

**Z** (470)

(464)

(470)

(465)
(471) (437)

(437)

(437) (436) (437) (471)

Figure A-GBCAE - Sheet 09 Preparation for the Electrical Wiring Installation in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 648 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

Z310 

### A

/82 FR80 FR83 FR84 FR90 FR91 FR93 5866VB /2S



### B



## B TYPICAL PLACARD INSTALLATION 

### C **D G** 



## A**A A**

SB 36−4033

F_SB_364033_6_BDAA_01_00 404 405 406

402 400

5208VP 5151VS

5215VC 5410VS 5866VB /2S

Figure A-GBDAA - Sheet 01 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 649 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

VIEW LOOKING AFT VIEW LOOKING AFT

ALTERNATIVE 5208VP

5208VP 5866VB /2S 5866VB /2S FR80

FR80/82 /82



## C

**D E** 

**F**

F_SB_364033_6_BDAA_02_00 Figure A-GBDAA - Sheet 02 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 650 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

(4 POS) (8 POS) (8 POS) (4 POS) (4 POS) (4 POS)

(4 POS) (6 POS) (6 POS) (4 POS) (4 POS) (4 POS)

ALTERNATIVE (2 POS) (2 POS) 

## E

**F** (3 POS)

(3 POS)

F_SB_364033_6_BDAA_03_00 416

420 417
418

417 419

415

415 485

416 417
418

417 419

415 485

415 417 423 420 (411) (410)

(411) (410)

Figure A-GBDAA - Sheet 03 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 651 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

VIEW LOOKING UP **FWD** FR91 FR90

STGR6LH STGR10LH

STGR6RH

STGR10RH AD 

### H **M N** 

**P Q** 

**U**

**U**

**V W** 

**X Y**  **Z** FR93



## G F_SB_364033_6_BDAA_04_00 402

510 511 402

488 489 402 451

Figure A-GBDAA - Sheet 04 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 652 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

VIEW LOOKING AFT 5866VB /2S

5215VC (4 POS) (4 POS) (4 POS) 

## H **J**



## J

**K K** 

**L**



## L 5215VC

F_SB_364033_6_BDAA_05_00 353 (437)

417 314 (437)

419
(437) 417 314
432 431 430

(435)

Figure A-GBDAA - Sheet 05 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 653 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

**NOTE:** IF INSTALLED 01 01

01 

## M **N**

**P**

F_SB_364033_6_BDAA_06_00 (442) (437) (437)

(437) (437) 350

417
444 350
417

314

419

417

314

Figure A-GBDAA - Sheet 06 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 654 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

FR91

FR90 5866VB /2S

ALTERNATIVE 

## Q **R R**  **S**

**T**



## T
F_SB_364033_6_BDAA_07_00 

## S

437 (437)

417 314 448

(437) (437) (442) (437) 417 501 439

444 417 350 (437) 419

(442)

Figure A-GBDAA - Sheet 07 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 655 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

TYPICAL 

## U **V**

5215VC

5410VC
5866VB /2S TO

TO



## W (437) (437)

(437) 350
417

314 320

417

501

496
492 496 419

494 493 402 488
402 510 493 494 351 402 451

489

511 5866VB /2S

F_SB_364033_6_BDAA_08_01 843 469

Figure A-GBDAA - Sheet 08 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 656 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## X

**Z Y**  (442) (437) (437) 350

417

444 419

515

417 314

511 517 404

510

F_SB_364033_6_BDAA_09_01

518

Figure A-GBDAA - Sheet 09 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 657 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

STGR5RH STGR6RH

STGR7RH

STGR9RH 5865VB /1S FR91 FR92 FR93

STGR5RH

STGR10RH VIEW LOOKING FWD

TYPICAL
BONDING STRIP ATTACHED TO INSIDE OF CLAMP 

### A B 5866VB /2S



## A B

**A C A C** 

**A D**

**A D**

**A E**  5410VS 5151VS

**NOTE:** 02 5866VB /2S


### A **F**



## A D

F_SB_364033_6_BDAA_10_00 479 480 481 479 480 481

(442) (437) 528
471

320 352 472

515 469 470 476

536 471 320

475 FR93



## A A

02

02 5866VB /2S TO361HF 5865VB /1S 34HF TO

Figure A-GBDAA - Sheet 10 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 658 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004



## A **F**
F_SB_364033_6_BDAA_11_00 (437) (437)

(437)

(437) (442) 470 470

449 471

449 471 536 537

465 417 521 419 

## A **E**

Figure A-GBDAA - Sheet 11 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 659 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

/82 FR80 FR83 FR84 FR90 FR91 FR93 5866VB /2S



### B



## B TYPICAL PLACARD INSTALLATION 

### C **D G** 



## A**A A**

SB 36−4033

F_SB_364033_6_BDAE_01_00 404 405 406

402 401

5208VP 5151VS

5215VC 5410VS 5866VB /2S

Figure A-GBDAE - Sheet 01 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 660 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_02_00 VIEW LOOKING AFT 5208VP 5866VB /2S FR80/82

(4 POS) (6 POS) (6 POS)

(4 POS) (4 POS) (4 POS)

(2 POS) (2 POS) (2 POS) (2 POS) (6 POS) (6 POS)

(3 POS)



## D **D**



## C

417 417 426

420

427 417 417 419 415 485 415 419 417 418 419

(412)

(412)

Figure A-GBDAE - Sheet 02 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 661 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_03_00 VIEW LOOKING UP **FWD** FR91 FR90

STGR6LH STGR10LH

STGR6RH

STGR10RH AD

FR93 

### F **K L** 

**M N** 

**S**

**S**

**T U** 

**V W**  **X**



## E 451

511 5866VB /2S 402

488 489 402 510 402

Figure A-GBDAE - Sheet 03 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 662 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_04_00 VIEW LOOKING AFT 5866VB /2S

5215VC (4 POS) (4 POS) (4 POS) 5215VC



## F

**G G** 



## H **H**



## J **J**

353

417314

432 431 430

(433) 314 417 419 (437)

(437) (437)

Figure A-GBDAE - Sheet 04 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 663 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_05_00 **NOTE:** IF INSTALLED 01 01

01 

## K **L**

**M** 350

417
444 350
417

314

419

314 417 (442) (437) (437)

(437) (437)

Figure A-GBDAE - Sheet 05 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 664 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_06_00 FR91

FR90 5866VB /2S

ALTERNATIVE 

## N **P P**  **Q**



## R **R**



## Q 448 417 314

417 501 439 419

350 417 444 (437)

(437)

(437) (437)

(442) (437) (437) (442)

Figure A-GBDAE - Sheet 06 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 665 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL 

## S **T**

5215VC

5410VC
5866VB /2S TO

TO


## U 350
417

314 320

417

501

419 496 492 496

494 493 402 489 401 402 493 494 351 402 451

511 (437) (437)

(437)

5866VB /2S

488

F_SB_364033_6_BDAE_07_01 843 469

Figure A-GBDAE - Sheet 07 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 666 6

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

# @A340 SERVICE BULLETIN

**CONF 005



## V **W**

**X** 350

417

444 419

515

417 314

404

517 511 (442) (437) (437)

518

F_SB_364033_6_BDAE_08_01 510

Figure A-GBDAE - Sheet 08 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 667 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_09_00 STGR5RH

STGR7RH

STGR9RH 5865VB /1S FR91 FR92 FR93

STGR5RH

STGR10RH VIEW LOOKING FWD

TYPICAL
BONDING STRIP ATTACHED TO INSIDE OF CLAMP 5866VB /2S

**NOTE:** 02 5866VB /2S



## Z **Z A A** 



## A B **A B**

**A B**
**A C A D** 



## A A 479 480 481 479 480 481

528
471

352 472 320

469 515 470 476

320 536 471

475 (442) (437) FR93



## Y

02

02

STGR6RH

5410VS 5151VS

5866VB /2S TO361HF 5865VB /1S 34HF TO

Figure A-GBDAE - Sheet 09 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 668 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BDAE_10_00 

## A D (437) (437)

(437)

(442) (437) 470 470

471 449 536 471 449 537

419
521

417 465 

## A C

Figure A-GBDAE - Sheet 10 Installation of the Electrical Wiring in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 669 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

A B C

mm DIMENSIONS (in)

C B A DIA 5.1 22.0 25.0 DIA 0.20 0.87 0.98 FR89 FR90 FR91

FR91 STGR6RH

STGR6RH 

### B

01

**FWD** 

## B Z310 

### A

F_SB_364033_6_BEAA_01_00 

## A
460
462

314 463 461 460 STGR6RH 

### C



## C

INSTALL WITH CORROSION INHIBITIVE INTERFAY SEALANT (MAT. NO. 09−005) 01 **NOTE:** Figure A-GBEAA - Sheet 01 Installation of the Bracket between FR90 and FR91 DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 670 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR55 FR57 FR60 FR64 FR68 FR73 FR77 

### C **B**

**D D**  **E D**  **C** 32HF
31HF
30HF

29HF
28HF 27HF



## A **E B** 
**E E**  **E D**  **E E**  FR83 

### F

F_SB_364033_6_BFAA_01_00 (572) (570) (563)
(566) (564) (562) 

### A Z310 Z170 Z160 Z150

Figure A-GBFAA - Sheet 01 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 671 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

TYPICAL

01 **NOTE:** 01


## B

REMOVE RIVETS TYPICAL 

## C

F_SB_364033_6_BFAA_02_00 (602) (357) (408)

(408) (602) (357) (609)

(609) (592) (612)

Figure A-GBFAA - Sheet 02 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 672 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

TYPICAL

01 **NOTE:** REMOVE RIVETS TYPICAL 01



## E **D**

02

NUT, PART OF ITEM (355) 02 

## F

F_SB_364033_6_BFAA_03_00 (408)

(399)
(601) (357)

(602)

(357) (602)

(596)

(355) (596) (609)

(592) (612)

Figure A-GBFAA - Sheet 03 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 673 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR57 FR57.4 FR60 FR64 FR68 FR73 FR77 FR83

FR55 26HF 

### B

**D D**  **E D**  **C** 32HF
31HF
30HF

29HF
28HF 27HF



### E **E E**  **E D**  **E E**  **F**

**B**



## A **C**

**B**

**C**

F_SB_364033_6_BFAB_01_00 (572) (570) (563)
(566) (564) (562)

(358) 

### A Z310 Z170 Z160 Z150

Figure A-GBFAB - Sheet 01 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 674 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

TYPICAL

01 **NOTE:** 01


## B

REMOVE RIVETS TYPICAL 

## C

F_SB_364033_6_BFAB_02_00 (599) (592)

(602) (357)
(602) (357) (609)

(609)
(620) (620)

Figure A-GBFAB - Sheet 02 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 675 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

TYPICAL

01 **NOTE:** REMOVE RIVETS TYPICAL 01



## E **D**

02

NUT, PART OF ITEM (355) 02 

## F

F_SB_364033_6_BFAB_03_00 (609)

(620)

(399)
(601) (596) (599) (592) (357) (602)

(357) (602)

(597)

(355)

Figure A-GBFAB - Sheet 03 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 676 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BFAE_01_00 FR57 FR57.4 FR60 FR64 FR68 FR73 FR77 FR83

FR55 26HF 

### B

**D D**  **E D**  **C** 32HF
31HF
30HF

29HF
28HF 27HF



### E **E E**  **E D**  **E E**  **F**

**B**



## A **C**

**B**

**C A**  Z310 Z170 Z160 Z150

(564) (566) (358) (563) (562) (570) (572)

Figure A-GBFAE - Sheet 01 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 677 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BFAE_02_00 TYPICAL

01 **NOTE:** 01


## B

REMOVE RIVETS TYPICAL 

## C (592)

(602) (357)
(602) (357) (599)

(609)
(408)

(408) (609)

Figure A-GBFAE - Sheet 02 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 678 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BFAE_03_00 TYPICAL

TYPICAL 01



## E **D**

**F** 01 **NOTE:** REMOVE RIVETS

(602) (357)

(592)

(357) (602)

(604) (602) (609)

(408)

(599)
(399) (601)

Figure A-GBFAE - Sheet 03 Removal of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 679 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR57 FR57.4 FR60 FR64 FR68 FR73 FR77 FR83

FR55 

### B 27HF 352HF 351HF

26HF 32HF

31HF

30HF

29HF
28HF 353HF 354HF 355HF 356HF 357HF



### C **D E**  **F G**  **H J**  **K**



## A 574

572 570

570 563

563 566

566 564

564

562 562
358

358 

### A Z310 Z170 Z160 Z150

F_SB_364033_6_BGAA_01_01 

### P STANDARD CLAMP INSTALLATION 

### Q

**NOTE:** THE SENSING ELEMENTS MUST BE INSTALLED IN FRONT OF THE VENTILATION HOLES. THE LENGTH COMPENSATION OF THE SENSING ELEMENTS MUST BE DONE AT THE COUPLINGS OR RETAINER RINGS. Figure A-GBGAA - Sheet 01 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 680 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR56 FR55

FR57



## C **K** 352HF 312HF

**FWD** 

## B

**M M** 

**FWD** 593

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01 606

F_SB_364033_6_BGAA_02_02 Figure A-GBGAA - Sheet 02 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 681 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR60

FR64 **FWD**

**FWD** 

### M **K**

**M K**  352HF

353HF



## E **D**

356

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01 606

F_SB_364033_6_BGAA_03_02 Figure A-GBGAA - Sheet 03 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 682 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR68

FR73 

## F
**FWD**

**FWD** 

### M 355HF 354HF

355HF



### M **K**



## G 594 591

594

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01

01

F_SB_364033_6_BGAA_04_01 

### K

Figure A-GBGAA - Sheet 04 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 683 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

FR77

FR80 **FWD**

**FWD**

356HF



### K 

## H

**J**

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 611

F_SB_364033_6_BGAA_05_02 

### N

Figure A-GBGAA - Sheet 05 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 684 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003



## M TYPICAL 607

612 607

(408) 602 357

602 (612) 592

609

SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 **NOTE:** 03

03 03

F_SB_364033_6_BGAA_06_01 TORQUE VALUE 0.25m.daN (22lbf.in) 03 

## L 4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 04

04 592

04 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA TYPICAL 

## K 02

02 02


### L 02

Figure A-GBGAA - Sheet 06 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 685 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

(399)

609 602

805

610 610 602 03

F_SB_364033_6_BGAA_07_02 TORQUE VALUE 0.25m.daN (22lbf.in) 03 **NOTE:** TYPICAL 05 FR55 TO FR83

05 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 

## N

**P** 357

602 602 (601) 03 (399)

Figure A-GBGAA - Sheet 07 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 686 6

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

# @A340 SERVICE BULLETIN
**CONF 001, 003

375HF OVERHEAT SENSING ELEMENT 357HF
355 57

604 02 02

02 03 597

596 01

BOND WITH ADHESIVE (MAT. NO. 08−078) AND 01 SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 TORQUE VALUE 0.25m.daN (22lbf.in) 03 NUT, PART OF ITEM 355 **NOTE:** PROTECT WITH VARNISH (MAT. NO. 07−003C)

F_SB_364033_6_BGAA_08_01 

## Q

06 06

Figure A-GBGAA - Sheet 08 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 687 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR57 FR57.4 FR60 FR64 FR68 FR73 FR77 FR83

FR55 

### B 27HF 352HF 351HF

26HF 32HF
31HF
30HF

29HF
28HF 353HF 354HF 355HF 356HF 357HF



### C **D E**  **F G**  **H J**  **K**



## A 574

572 570

570 563

563 566

566 564

564

562 562
358

358 

### A Z310 Z170 Z160 Z150

F_SB_364033_6_BGAB_01_01 **NOTE:** THE LENGTH COMPENSATION OF SENSING ELEMENTS MUST BE DONE AT THE COUPLINGS OR RETAINER RINGS. THE SENSING ELEMENTS MUST BE INSTALLED IN FRONT OF THE VENTILATION HOLES. STANDARD CLAMP INSTALLATION 

### Q **R**

Figure A-GBGAB - Sheet 01 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 688 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR57

FR55 351HF 312HF



## B
**FWD** 593 389

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01

F_SB_364033_6_BGAB_02_01 

### L **N N** 

Figure A-GBGAB - Sheet 02 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 689 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

352HF

**FWD**

**FWD** 

## C

**D** FR57.3 FR57.2

FR57.4 606

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01

F_SB_364033_6_BGAB_03_01 

### L

**N N** 

Figure A-GBGAB - Sheet 03 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 690 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR60

FR64 **FWD**

**FWD** 352HF

353HF 

## E

**F** 606

356

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01

01

F_SB_364033_6_BGAB_04_01 

### L

**L N** 

**N**

Figure A-GBGAB - Sheet 04 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 691 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR68

FR73 **FWD**

**FWD** 355HF 354HF

355HF 

## G

**H** 594 591

594

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01

01

F_SB_364033_6_BGAB_05_01 

### N

**N L** 

**L**

Figure A-GBGAB - Sheet 05 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 692 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

FR77

FR80 **FWD**

**FWD** 356HF



## J

**K** 611

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01

/82

F_SB_364033_6_BGAB_06_01 

### L

**P**

Figure A-GBGAB - Sheet 06 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 693 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

TYPICAL (609)

(620) 602 357

602 03

F_SB_364033_6_BGAB_07_01 607

612 607 599 592

03 03 4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 04

04 592

TYPICAL 02

02 02 02

SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 **NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 03 04 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA 

## L **M M** 



## N

Figure A-GBGAB - Sheet 07 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 694 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

(399)

609 602

805

610 610 602

TORQUE VALUE 0.25m.daN (22lbf.in) 03 **NOTE:** 03

F_SB_364033_6_BGAB_08_01 

## P

TYPICAL 05 FR55 TO FR83

05 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 357 (601) 03 (399)



## Q 602 602

Figure A-GBGAB - Sheet 08 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 695 6

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

# @A340 SERVICE BULLETIN
**CONF 002, 004

375HF OVERHEAT SENSING ELEMENT 357HF
355 597 57

604 596 02 02

02

03 01

BOND WITH ADHESIVE (MAT. NO. 08−078) AND 01 SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 TORQUE VALUE 0.25m.daN (22lbf.in) 03 NUT, PART OF ITEM 355 06 **NOTE:** PROTECT WITH VARNISH (MAT. NO. 07−003C) 06

F_SB_364033_6_BGAB_09_01 

## R

Figure A-GBGAB - Sheet 09 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 696 6

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

# @A340 SERVICE BULLETIN

**CONF 005

FR57 FR57.4 FR60 FR64 FR68 FR73 FR77 FR83

FR55 

### B 27HF 352HF 351HF

26HF 32HF

31HF

30HF
29HF
28HF 353HF 354HF 355HF 356HF 357HF



### C **D E**  **F G**  **H J**  **K**



## A **A** Z310 Z170 Z160 Z150

566 563 562 570 564 574 358

572

570

562
563
358 566
564

F_SB_364033_6_BGAE_01_01 **NOTE:** THE LENGTH COMPENSATION OF SENSING ELEMENTS MUST BE DONE AT THE COUPLINGS OR RETAINER RINGS. THE SENSING ELEMENTS MUST BE INSTALLED IN FRONT OF THE VENTILATION HOLES. STANDARD CLAMP INSTALLATION 

### Q **R**

Figure A-GBGAE - Sheet 01 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 697 6

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

# @A340 SERVICE BULLETIN

**CONF 005

FR57

FR55 351HF 312HF



## B
**FWD**

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01 389 593

F_SB_364033_6_BGAE_02_01 

### L **N N** 

Figure A-GBGAE - Sheet 02 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 698 6

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

# @A340 SERVICE BULLETIN

**CONF 005

352HF

**FWD**

**FWD** 

## C

**D** FR57.3 FR57.2

FR57.4

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 606

F_SB_364033_6_BGAE_03_01 

### L

**N N** 

Figure A-GBGAE - Sheet 03 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 699 6

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

# @A340 SERVICE BULLETIN

**CONF 005

FR60

FR64 **FWD**

**FWD** 352HF

353HF 

## E

**F**

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01

356 606

F_SB_364033_6_BGAE_04_01 

### N

**N L** 

**L**

Figure A-GBGAE - Sheet 04 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 700 6

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

# @A340 SERVICE BULLETIN

**CONF 005

FR68

FR73 **FWD**

**FWD** 355HF 354HF

355HF 

## G

**H**

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 01

01 594 591

594

F_SB_364033_6_BGAE_05_01 

### L

**L N**  **N**

Figure A-GBGAE - Sheet 05 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 701 6

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

# @A340 SERVICE BULLETIN

**CONF 005

FR77

FR80 **FWD**

**FWD**

356HF



## J

**K**

01 **NOTE:** BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 01 611

/82

F_SB_364033_6_BGAE_06_01 

### L

**P**

Figure A-GBGAE - Sheet 06 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 702 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL 602 357

602 609

620 03

F_SB_364033_6_BGAE_07_01 607

612 607592

SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 **NOTE:** 03 03

TORQUE VALUE 0.25m.daN (22lbf.in) 03 4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 04

04 592

04 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA TYPICAL 02

02 02 02



## L **M**

**N M**  (599)

Figure A-GBGAE - Sheet 07 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 703 6

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

# @A340 SERVICE BULLETIN

**CONF 005

609 602

805

610 610 602 (399)

03

F_SB_364033_6_BGAE_08_01 357
601 03



## Q **P**

TORQUE VALUE 0.25m.daN (22lbf.in) 03 **NOTE:** TYPICAL 05 FR55 TO FR83

05 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 602 602 399

Figure A-GBGAE - Sheet 08 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 704 6

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

# @A340 SERVICE BULLETIN

**CONF 005

375HF

03 OVERHEAT SENSING ELEMENT 357HF 02

02

02 604 596 57

597 355 01

06

F_SB_364033_6_BGAE_09_01 

## R

BOND WITH ADHESIVE (MAT. NO. 08−078) AND 01 SECURE WITH LOCKWIRE (MAT. NO. 19−018) 02 TORQUE VALUE 0.25m.daN (22lbf.in) 03 NUT, PART OF ITEM 355 06 **NOTE:** PROTECT WITH VARNISH (MAT. NO. 07−003C)

Figure A-GBGAE - Sheet 09 Installation of the Sensing Elements in the Bulk and AFT Cargo Compartments DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 705 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

Z310 

### A



## A FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100



### C
**B** 34HF

33HF 139HF 140HF



### C
**C C** **C E**  **E** (364) (366)

(371) (361)

/82

F_SB_364033_6_BHAA_01_01 

### D

Figure A-GBHAA - Sheet 01 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 706 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002



## B 01

TYPICAL

NUT, PART OF ITEM (355) TYPICAL

01 **NOTE:** 

## C **D** (596)

(357) (357) (620) (601)

(399) (604)

(355)

(602) (602)

(609)

F_SB_364033_6_BHAA_02_01 FOR ALL CLAMPS

Figure A-GBHAA - Sheet 02 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 707 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

**NOTE:** TYPICAL 02

02 REMOVE RIVETS 

### K **K**

**G** 

## E (59)

(612)

**FWD** 

## F

F_SB_364033_6_BHAA_03_01 

### J

**H C** 

Figure A-GBHAA - Sheet 03 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 708 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL 02 **NOTE:** REMOVE RIVETS 02



## G **H**

**J** (399)
(621) (59)

(620)

(601) (399)

(601) (612) (609)

(602)

(602) (357)

(602)

F_SB_364033_6_BHAA_04_01 (621)



## K

Figure A-GBHAA - Sheet 04 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 709 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

Z310 

### A



## A FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100



### D **C**
**B F** 
**E D**  **F G**  34HF

33HF 139HF 140HF

F_SB_364033_6_BHAC_01_00 (361)

(362) (365)

(370) /82

Figure A-GBHAC - Sheet 01 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 710 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

F_SB_364033_6_BHAC_02_00 NUT, PART OF ITEM (355) TYPICAL 01 **NOTE:** 

## B

**C** 01 (604) (596)

(355)

(602)
(603)
(610) (609) (602) (620)

(610) (609)


## D

Figure A-GBHAC - Sheet 02 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 711 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

F_SB_364033_6_BHAC_03_00 TYPICAL 

## F 02



### L **K K** 

**J H**  **D** (601)

(399) (612) (610) (59) (602)

**NOTE:** REMOVE RIVETS 02 

## E

**FWD** 

## G

Figure A-GBHAC - Sheet 03 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 712 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

TYPICAL

02 **NOTE:** REMOVE RIVETS 02



## J

**K L**  (612) (609)

(399)

(621) (59) (357)

(620) (602)

(399)
(357)

(601) (602) (601) 

## H

F_SB_364033_6_BHAC_04_01 (602)

Figure A-GBHAC - Sheet 04 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 713 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

F_SB_364033_6_BHAE_01_00 FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100



### B **E** 34HF

33HF 139HF 140HF 

### D **F**

**D**
**C**



## A (361)

(368) (362) (365) /82

Figure A-GBHAE - Sheet 01 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 714 6

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

# @A340 SERVICE BULLETIN

**CONF 005

NUT, PART OF ITEM (355) 01 **NOTE:** 

## B 01

TYPICAL TYPICAL 02 

## C **D**

02 REMOVE RIVETS (596) (604)

(355)

(602)

(610) (592) (601)

(399) (599)

F_SB_364033_6_BHAE_02_01 FOR ALL CLAMPS

Figure A-GBHAE - Sheet 02 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 715 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BHAE_03_00 

## E

**G H**  **J J**  **K**

**E** (602)

(610) (620)

(609)

**FWD**



## F

Figure A-GBHAE - Sheet 03 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 716 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL

02 **NOTE:** REMOVE RIVETS 02



## G **H**

**J K**  (592)
(602)

(399)
(357)

(601) (602) (601) (602) (599) (609)

(399)

F_SB_364033_6_BHAE_04_01 (357) (620) (621)

Figure A-GBHAE - Sheet 04 Removal of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 717 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

Z310 

### A

MAKE SURE THAT THE SENSING ELEMENTS ARE INSTALLED IN FRONT OF THE APU DUCT VENTILATION HOLES 01 **NOTE:**

FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100



### B**C D**  **L**

33HF 358HF 139HF 359HF

140HF 360HF 34HF 361HF 361

360

366 366 364

364

371 398 /82

F_SB_364033_6_BJAA_01_01 

## A 01 STANDARD CLAMP INSTALLATION 

### R
**E F**  **F F** 

**G H**  **K**

Figure A-GBJAA - Sheet 01 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 718 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

**FWD** 

### D **D** OVERHEAT SENSING ELEMENT 358HF



## B 596

496 405 02 02

02

02 604

597 355

602 

## C 02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) 03 NUT, PART OF ITEM 355 03

TORQUE VALUE 0.25m.daN (22lbf.in) 04 04

05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 05 608

F_SB_364033_6_BJAA_02_02 Figure A-GBJAA - Sheet 02 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 719 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL 

## D (620)

(399)
805 (609)
357

602

602 609 602

610 610

**NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04 04

F_SB_364033_6_BJAA_03_01 

## E

Figure A-GBJAA - Sheet 03 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 720 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL

MAKE SURE THAT THE LENGHT COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 06 

### A

**A D** 

**D** 06 06

(399)
805 602 610

610

602 609 

### A

**A**

**NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04

F_SB_364033_6_BJAA_04_01 

## F

**G** MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in)

12.7 mm (0.49 in) 16.5 mm (0.65 in)



## A **A** TYPICAL

Figure A-GBJAA - Sheet 04 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 721 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

359HF 358HF

360HF 359HF 04 04

04

04 02
02

02

02 02

02 393 392

59

394 393

59 05 05

05 05 607 612

607
(612)

612 607

607
(612) 02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) F_SB_364033_6_BJAA_05_01 59

TYPICAL

07 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA 4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 07

07


## H

**K J**  **J**

**J**

Figure A-GBJAA - Sheet 05 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 722 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002



### B

**B** 361HF

34HF 360HF

140HF

**FWD**

04



## L **D**

360HF 361HF

34HF



## M **M N**  **N**

02 02

02 05

04 02

02 59 394 496

405

607

612

607 (612) 602 

### A

**A A** 

**A**

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 591 374

F_SB_364033_6_BJAA_06_02 

### J

Figure A-GBJAA - Sheet 06 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 723 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL STGR5RH

STGR6RH

STGR7RH

STGR9RH

34HF 361HF FR93 

## N

**P**

**P Q**  **P** 

## B **B** (399) (621)

372

313 682 372 609

602 602

602

08 TORQUE VALUE 0.40m.daN (35lbf.in) **NOTE:** 08

F_SB_364033_6_BJAA_07_01 Figure A-GBJAA - Sheet 07 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 724 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

TYPICAL 

## P 640
372

372 682 416 640 640

373 372
416

682

682 416 372
602 602 602 602



## Q 373

F_SB_364033_6_BJAA_08_02 TYPICAL **NOTE:** FR83 TO FR95

09 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 09 

## R

TORQUE VALUE 0.25m.daN (22lbf.in) 04 (399)

(601) 357

04 602

Figure A-GBJAA - Sheet 08 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 725 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

Z310 

### A

MAKE SURE THAT THE SENSING ELEMENTS ARE INSTALLED IN FRONT OF THE APU DUCT VENTILATION HOLES FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100 34HF 361HF

140HF 139HF 33HF 358HF 359HF 360HF



### B**C E** 

**G G** 

01 **NOTE:** 

### K **L F**  **M** 361 360

365

362 370 369 363 365
/82

F_SB_364033_6_BJAC_01_01 

## A 01 STANDARD CLAMP INSTALLATION 

### F**H**

**S**

Figure A-GBJAC - Sheet 01 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 726 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

**FWD** 

### D **E** 04 596 604

355 608

405 496 405

602 02 02

02

02 OVERHEAT SENSING

ELEMENT 358HF



## B 597

05



## C 02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) 03 NUT, PART OF ITEM 355 TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 03

F_SB_364033_6_BJAC_02_01 Figure A-GBJAC - Sheet 02 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 727 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

TYPICAL 

## E (609)

(603)

(609)

(620) 357

602

357

602

**NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04 04 

## D

F_SB_364033_6_BJAC_03_01 Figure A-GBJAC - Sheet 03 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 728 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

TYPICAL (399)
609 357

354 602

MAKE SURE THAT THE LENGHT COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 06 **NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04

F_SB_364033_6_BJAC_04_01 TYPICAL 

### A

**A** 06 06 

### A

**A**



## F MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in)

12.7 mm (0.49 in) 16.5 mm (0.65 in)



## A **A** TYPICAL 

### G

**G**



## G

Figure A-GBJAC - Sheet 04 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 729 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

360HF 359HF 393 394 607 612

607
(612) 04

04 02 02

02 59 05 05



## L 359HF 358HF



## K 602 610

610

805 602 (399) (609)

04 393 392

607 612

607 59 (612) 04 04

02 02 02 05 05

F_SB_364033_6_BJAC_05_01 

## H 59

TYPICAL 4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 07

07 

## J

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 07 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA 

### J

**J**

Figure A-GBJAC - Sheet 05 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 730 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004



### E **B**

**B** 361HF

34HF 360HF

140HF

361HF **FWD**



## M **N P**  **P**

04 04 361HF

34HF 374

59 607 591

607 612
612 02

02 02

02 

## N 394 

### A

**A A** 

**A**

05

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 

### J

F_SB_364033_6_BJAC_06_02 Figure A-GBJAC - Sheet 06 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 731 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

TYPICAL STGR5RH

STGR6RH

STGR7RH

STGR9RH

34HF 361HF 

## P

**R Q**  **Q**

**Q**

FR93



## B **B** 602 609 372 602

602 372 682 313 (399) (621)

08 TORQUE VALUE 0.40m.daN (35lbf.in) **NOTE:** 08

F_SB_364033_6_BJAC_07_01 Figure A-GBJAC - Sheet 07 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 732 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 004

TYPICAL 602
640
372 602

416 682 372
602 640
640 373

373 372
602 682 416 682 416372 

## Q

**R**

F_SB_364033_6_BJAC_08_01 (399)
397 357

314 04

TYPICAL **NOTE:** FR83 TO FR95

09 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 09

TORQUE VALUE 0.25m.daN (22lbf.in) 04 

## S 602

Figure A-GBJAC - Sheet 08 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 733 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

MAKE SURE THAT THE SENSING ELEMENTS ARE INSTALLED IN FRONT OF THE APU DUCT VENTILATION HOLES FR80 FR83 FR85FR86 FR88 FR91 FR93 FR95 FR98 FR100 34HF 361HF

140HF

139HF 33HF 358HF 359HF 360HF



### B

01 **NOTE:** 

### C**F F**  **F G**  **P J**  **K L** 

367 368 362 365 361 360

365 363 /82

F_SB_364033_6_BJAE_01_01 

## A 01 STANDARD CLAMP INSTALLATION 

### G

**S**

Figure A-GBJAE - Sheet 01 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 734 6

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

# @A340 SERVICE BULLETIN

**CONF 005

**FWD** 

### D 03 OVERHEAT SENSING ELEMENT 358HF



## B 02

02

02 608 596 604

597 355

405 496 405

602 

## C 05

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) 03 NUT, PART OF ITEM 355 TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 04

F_SB_364033_6_BJAE_02_01 Figure A-GBJAE - Sheet 02 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 735 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BJAE_03_00 

## D **E** FR83



## E 640

396

396 314 359 640 396

396 314

640 396

357

602

314 602

**NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04

Figure A-GBJAE - Sheet 03 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 736 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BJAE_04_01 MAKE SURE THAT THE LENGTH COMPENSATION IS DONE CLOSE TO THE APU DUCTS COUPLING OR TO THE APU DUCT RETAINER RINGS 06 59 

## H TYPICAL 

### H MIN 50.8 mm (2.00 in) MAX 80.0 mm (3.15 in)

12.7 mm (0.49 in) 16.5 mm (0.65 in)



## A **A** TYPICAL

4.8 mm TO 7.9 mm (0.19 in TO 0.31 in) 9.5 mm TO 12.7 mm (0.37 in TO 0.50 in) 07

07 

### A

**A** 06 06 

### A

**A**

TYPICAL 

## F **P**

**P**

07 INSTALL THE BRACKET WITHIN THE GIVEN TOLERANCE AREA 02 **NOTE:** SECURE WITH LOCKWIRE TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) (MAT. NO. 19−018) 359HF 358HF

04

04 02 02

02 393 392

607 612

607 59 (599) 05 05



## G

Figure A-GBJAE - Sheet 04 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 737 6

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

# @A340 SERVICE BULLETIN

**CONF 005

360HF 359HF

04 04



## K 02 02 02 610

805 602 610 602

394 393

607 612

607 59 (399) (609)

(599) 

## J

05 05

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 04

F_SB_364033_6_BJAE_05_01 

### H

Figure A-GBJAE - Sheet 05 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 738 6

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

# @A340 SERVICE BULLETIN

**CONF 005



### B

**B** 361HF

34HF 360HF

140HF

361HF **FWD**

04 04 

## L **M N**  **N**

**P**

361HF

34HF 607 59 374

591

607 612 394

(599) 02 02

02 02 02



## M **A**

**A A** 

**A**

05

02 **NOTE:** SECURE WITH LOCKWIRE (MAT. NO. 19−018) TORQUE VALUE 0.25m.daN (22lbf.in) 04 05 BOND WITH ADHESIVE (MAT. NO. 08−078) AND PROTECT WITH VARNISH (MAT. NO. 07−003C) 

### H

F_SB_364033_6_BJAE_06_02 Figure A-GBJAE - Sheet 06 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 739 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL STGR5RH

STGR6RH

STGR7RH

STGR9RH

34HF 361HF 

### R **Q Q** 

**Q**

FR93

TYPICAL 

## N

**P**

**B B**  (399) (436)

(609)

(620) 609 372 602

682 313 372 602 602

357

602

08 TORQUE VALUE 0.40m.daN (35lbf.in) **NOTE:** TORQUE VALUE 0.25m.daN (22lbf.in) 04 04 08

F_SB_364033_6_BJAE_07_01 Figure A-GBJAE - Sheet 07 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 740 6

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

# @A340 SERVICE BULLETIN

**CONF 005

TYPICAL 640 602

372 602

416 682 372

640 640

373 602

372
416

682 373 372
602 682 416 

## R **Q**

F_SB_364033_6_BJAE_08_01 TYPICAL **NOTE:** FR83 TO FR95

09 STANDARD CLAMP INSTALLATION FOR REMAINING AREAS. FOR ALL OTHER CLAMP INSTALLATIONS REFER TO THE RELATED DETAILS. 09

TORQUE VALUE 0.25m.daN (22lbf.in) 04 

## S 397 357

314 (399)

04 602

Figure A-GBJAE - Sheet 08 Installation of the Sensing Elements in the Rear Fuselage Section DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 741 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 002

Z310 

### A

FR80 FR83 FR86 FR88 FR91 FR93 FR95 FR98 FR100

01 **NOTE:** CLOSED BY ADHESIVE STRIP POSITION OF BLOWOUT APERTURE UNDER THE SENSING ELEMENT 02 01 02 01 02 01 02 01 02 01 02

01 01 01



## A 01

F_SB_364033_6_BKAA_01_00 379

376

375 377 378 380 384 381 382 /82

Figure A-GBKAA - Sheet 01 Installation of the Sleeves at the APU Bleed Air Duct DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 742 6

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

# @A340 SERVICE BULLETIN

**CONF 003 thru 005

Z310 

### A

F_SB_364033_6_BKAC_01_00 FR80 FR83 FR86 FR88 FR91 FR93 FR95 FR98 FR100

01 **NOTE:** CLOSED BY ADHESIVE STRIP POSITION OF BLOWOUT APERTURE UNDER THE SENSING ELEMENT 02 

## A 01 02 01 02 01 02 01 02 01 02 01 02 01

01 380

382 383
384
385

386

377
387 /82

Figure A-GBKAC - Sheet 01 Installation of the Sleeves at the APU Bleed Air Duct DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 743 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

F_SB_364033_6_BLAE_01_00 FR80 FR83 FR84
149HF



### D **B E** 



## C **B** FR83 

### C (6 POS)

TYPICAL



## D 149HF

150HF 151HF 

### F (541) (419)

(540) (612) (493) (494) (544)

(542)

(612) (543)

(610) (602) (494) (601) (357)

(602) (494) (601) /82

STGR11RH 

## A

Figure A-GBLAE - Sheet 01 Removal of the Sensing Element, FIN 149HF, installed with Service Bulletin No. A340-36-4028

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 744 6

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

# @A340 SERVICE BULLETIN

**CONF 005

F_SB_364033_6_BLAE_02_00 **FWD**

**FWD** 

## BEFORE

**AFTER** FR84 FR83

FR83

FR84 150HF 151HF 5865VSB

5865VSA

5865VSA 

## E

**F** (479) (480) (481)

401
402 479 480 481 5865VB /1S 5865VB /1S STGR11RH

STGR11RH (542) (543)

Figure A-GBLAE - Sheet 02 Removal of the Sensing Element, FIN 149HF, installed with Service Bulletin No. A340-36-4028

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 745 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

Z310 

### A

VIEW LOOKING FWD mm DIMENSIONS (in)
B A B C

D

C D 35.0 12.0 DIA 13.5 C

MIN 15.0 SENSING ELEMENT HOLE

SENSING ELEMENT HOLE

0.47 DIA 0.53 MIN 0.59

1.38 

### B

FR80

01 **NOTE:** DIMENSION FOR CONTROL ONLY 

## A

**B** 01 A /82

F_SB_364033_6_BMAA_01_01 Figure A-GBMAA - Sheet 01 Hole Location and Dimensions for the sensing element Installation in the Sheet Metal Pressure Bulkhead DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 746 6

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

# @A340 SERVICE BULLETIN

**CONF 005

Z310 

### A

mm DIMENSIONS (in)
B A
C A

DIA 13.5 B

MIN 24.0 62.0 C SENSING ELEMENT HOLE

SENSING ELEMENT HOLE

VIEW LOOKING AFT DIA 0.53 MIN 0.95

2.44 

### B



## A

**B** FR80/82

F_SB_364033_6_BMAE_01_01 Figure A-GBMAE - Sheet 01 Hole Location and Dimensions for the Sensing Element Installation in the CFK Pressure Bulkhead DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 747 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

F_SB_364033_6_BNAA_01_00 TOLERANCES FOR WAVINESS AND BEND IN WIRES

C

B A E
C

A E

E A C

D E

E

E E C

**NOTE:** FOR DIMENSIONS, REFER TO SHEET 2 C C

Figure A-GBNAA - Sheet 01 Tolerances for the Waviness and Bend in the Electrical Wiring DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 748 6

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

# @A340 SERVICE BULLETIN

**CONF ALL

F_SB_364033_6_BNAA_02_00 E

mm DIMENSIONS (in)

C D E B A 9.52 MAX 6.4
MIN 12.7 MIN 0.50 MIN 25.4 MIN 1.00 MIN R 25.4 MIN R 1.00 MAX 0.25

0.38 E

01 **NOTE:** USE OTHER HOLE OF BRACKET IF NECESSARY 02 01 02

ROTATE CLIP FOR SMOOTH ROUTING OF SENSING ELEMENT IF NECESSARY E F

E

F MAX 203.0 MAX 7.99

Figure A-GBNAA - Sheet 02 Tolerances for the Waviness and Bend in the Electrical Wiring DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 749 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

EXISTING WIRE ADDED WIRE
UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF24 GAUGE 

## AFTER

A ZONE 132 A

A ZONE 122

5401

5402−DM24 ZONE 313 ZONE 310 ZONE 270 ZONE 152 A

IDENTIFICATION WITH ATA−NO. 3622 UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2S 

## AFTER

5400

**NOTE:** FR20 FR38

2712VC 3520VC

3506VC 55

72 66

69

FR56 FR80 FR93

37

3672VC 5208VP /82 804VU

5410VS A

F_SB_364033_6_WAAA_01_00 Figure A-GWAAA - Sheet 01 Wiring Diagram DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 750 6

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

# @A340 SERVICE BULLETIN

**CONF 005

EXISTING WIRE

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF24 GAUGE IDENTIFICATION WITH ATA−NO. 3622 UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2S DELETED WIRE 

## BEFORE

5050−YY18−(150HF) 5051−YY18−(151HF) 5003 5052
ZONE 313

ZONE 311 ZONE 311 ZONE 310 ZONE 313 1S

5003 1S 9ZONE 151 FR56 3677VC A 5207VP

149HF FR80 FR83 FR93 /82

**NOTE:** 5865VS B
5865VS A ZONE 270

5151VSA

F_SB_364033_6_WAAE_01_00 Figure A-GWAAE - Sheet 01 Wiring Diagram DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 751 6

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

# @A340 SERVICE BULLETIN

**CONF 005

EXISTING WIRE REROUTED WIRE

UNLESS OTHERWISE SPECIFIED PREFIX ALL WIRE UNLESS OTHERWISE SPECIFIED ALL WIRES ARE CF24 GAUGE IDENTIFICATION WITH ATA−NO. 3622 UNLESS OTHERWISE SPECIFIED ALL ROUTES ARE 2S **NOTE:** 5003 5052

ZONE 313

ZONE 311 ZONE 310 ZONE 313 

## AFTER
FR83 FR93 FR80 5207VP /82 1S

5003 1S 9ZONE 151 FR56 3677VC A ZONE 270

5151VS A

5865VS A

F_SB_364033_6_WAAE_02_00 Figure A-GWAAE - Sheet 02 Wiring Diagram DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 752 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

A = ADDED WIRE 122 2712VC−A 55 EN3155−003F2222 3622− 5400 2S CF24 14300 3520VC 66 EN3155−008M2222 A 132 563.4 122 2712VC−A 72 EN3155−003F2222 3622− 5401 2S 132 3506VC 69 EN3155−008M2222 A CF24 14300 563.4 152 3672VC 37 EN3155−008M2222 3622−5402 2S DM24 28000 1103.2 313 5410VS A A NSA936809RG0001 152 3672VC 1

− 2842−5362 2S 311 5215VC −Q BEFORE/AFTER 310 5208VT 4K

− 2842−5370 2S 311 5215VC −P BEFORE/AFTER 310 5208VT 6K

− 2842−7857 2S 311 5215VC −N BEFORE/AFTER 311 2842−7857

− 2842−5388 2S 311 5215VC −M BEFORE/AFTER 152 3672VC 6

− 2842−5364 2S 311 5215VC −G BEFORE/AFTER 310 5208VT 1G

− 2842−5372 2S 311 5215VC −F BEFORE/AFTER 310 5208VT 3J

− 2842−7859 2S 311 5215VC −E BEFORE/AFTER 311 2842−7859

− − −

2842−5390 2S 311 5215VC −D BEFORE/AFTER 152 3672VC 7

− 2842−5365 2S 311 5215VC −C BEFORE/AFTER 310 5208VT 1E

− 2842−5373 2S 311 5215VC −B BEFORE/AFTER 310 5208VT 3H

− 2842−7860 2S 311 5215VC −A BEFORE/AFTER 311 2842−7860

− − 2842−5391 2S 311 5215VC Z BEFORE/AFTER

152 3672VC 9

− 2842−5367 2S 311 5215VC U BEFORE/AFTER 310 5208VT 1C

− 2842−5375 2S 311 5215VC T BEFORE/AFTER 310 5208VT 2H

− 2842−7862 2S 311 5215VC S BEFORE/AFTER 311 2842−7862

− − 2842−5393 2S 311 5215VC R BEFORE/AFTER 152 3672VC 8

− 2842−5366 2S 311 5215VC Y BEFORE/AFTER 310 5208VT 1D

− 2842−5374 2S 311 5215VC X BEFORE/AFTER 310 5208VT 3G

− 2842−7861 2S 311 5215VC W BEFORE/AFTER 311 2842−7861

− − 2842−5392 2S 311 5215VC V BEFORE/AFTER

152 3672VC 10

− 2842−5368 2S 311 5215VC P BEFORE/AFTER 310 5208VT 1B

− 2842−5376 2S 311 5215VC N BEFORE/AFTER

ELT. EQUIPMENT F9297000500000 "SHEET 1 ISSUE D" L I N E ZONE OR PANEL TERM. TERMINAL P/N WIRE IDENT C0L ROUTE GAUGE LENGTH MM INCH ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N INSTRUCTIONS 

## END 2 LEAD END 1

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.

Figure A-GHAAA - Sheet 01 Hook-up Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 753 6

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

# @A340 SERVICE BULLETIN

**CONF 005

A = ADDED WIRE D = DELETED WIRE 122 2712VC−A 55 EN3155−003F2222 3622− 5400 2S CF24 14300 3520VC 66 EN3155−008M2222 A 132 563.4 122 2712VC−A 72 EN3155−003F2222 3622− 5401 2S 132 3506VC 69 EN3155−008M2222 A CF24 14300 563.4 152 3672VC 37 EN3155−008M2222 3622−5402 2S DM24 28000 1103.2 313 5410VS A A NSA936809RG0001 151 3677VC 9

− 3622−5003 1S 311 NSA936809RG0001 BEFORE/AFTER
313 5151VS A

− 3622−5052 1S 311 NSA936809RG0001 5865VS
5865VS A A 2

2 AFTER 313 5151VS A

− 3622−5052 1S 311 5865VS B NSA936809RG0001 BEFORE

3672VC 1

− 2842−5362 2S 311 5215VC −Q BEFORE/AFTER 5208VT 4K

− 2842−5370 2S 311 5215VC −P BEFORE/AFTER 310 5208VT 6K

− 2842−7857 2S 311 5215VC −N BEFORE/AFTER 311 2842−7857

− 2842−5388 2S 311 5215VC −M BEFORE/AFTER 152 3672VC 6

− 2842−5364 2S 311 5215VC −G BEFORE/AFTER 310 5208VT 1G

− 2842−5372 2S 311 5215VC −F BEFORE/AFTER 310 5208VT 3J

− 2842−7859 2S 311 5215VC −E BEFORE/AFTER 311 2842−7859

− − −

2842−5390 2S 311 5215VC −D BEFORE/AFTER 152 3672VC 7

− 2842−5365 2S 311 5215VC −C BEFORE/AFTER 310 5208VT 1E

− 2842−5373 2S 311 5215VC −B BEFORE/AFTER 310 5208VT 3H

− 2842−7860 2S 311 5215VC −A BEFORE/AFTER 311 2842−7860

− − 2842−5391 2S 311 5215VC Z BEFORE/AFTER

152 3672VC 9

− 2842−5367 2S 311 5215VC U BEFORE/AFTER 152 3672VC 8

− 2842−5366 2S 311 5215VC Y BEFORE/AFTER 310 5208VT 1D

− 2842−5374 2S 311 5215VC X BEFORE/AFTER 310 5208VT 3G

− 2842−7861 2S 311 5215VC W BEFORE/AFTER 311 2842−7861

− − 2842−5392 2S 311 5215VC V BEFORE/AFTER 310 152 311 311 5865VS 5865VS A B −

− 3622−5051 3622−5050 1S 1S 311 311 149HF 149HF D D

ELT. EQUIPMENT F9297000500200 "SHEET 3 ISSUE D" L I N E ZONE OR PANEL TERM. TERMINAL P/N WIRE IDENT C0L ROUTE GAUGE LENGTH MM INCH ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N INSTRUCTIONS 

## END 2 LEAD END 1

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.

Figure A-GHAAB - Sheet 01 Hook-up Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 754 6

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

# @A340 SERVICE BULLETIN

**CONF 001 thru 004

310 5208VT 2G

− 2842−7863 2S 311 5215VC M BEFORE/AFTER 311 2842−7863

− − 2842−5394 2S 311 5215VC L BEFORE/AFTER

ELT. EQUIPMENT F9297000500000 "SHEET 2 ISSUE G" 151 3677VC 9

− 3622−5003 1S 313 5151VS A BEFORE/AFTER 313 5151VS A

− 3622−5004 1S 313 34HF BEFORE/AFTER 313 5410VS A 3622−5403 2S YY18 313 361HF A L I N E ZONE OR PANEL TERM. TERMINAL P/N WIRE IDENT C0L ROUTE GAUGE LENGTH MM INCH ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N INSTRUCTIONS END 2 LEAD END 1

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.

Figure A-GHBAA - Sheet 01 Hook-up Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 755 6

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

# @A340 SERVICE BULLETIN

**CONF 005

310 5208VT 2G

− 2842−7863 2S 311 5215VC M BEFORE/AFTER 311 2842−7863

− − 2842−5394 2S 311 5215VC L BEFORE/AFTER 311 2842−7862

− − 2842−5393 2S 311 5215VC R BEFORE/AFTER 152 3672VC 10

− 2842−5368 2S 311 5215VC P BEFORE/AFTER 310 5208VT 1B

− 2842−5376 2S 311 5215VC N BEFORE/AFTER 310 5208VT 1C

− 2842−5375 2S 311 5215VC T BEFORE/AFTER 310 5208VT 2H

− 2842−7862 2S 311 5215VC S BEFORE/AFTER

ELT. EQUIPMENT F9297000500200 "SHEET 4 ISSUE G" 313 5151VS A

− 3622−5004 1S 313 34HF BEFORE/AFTER 313 5410VS A 3622−5403 2S YY18 313 361HF A L I N E ZONE OR PANEL TERM. TERMINAL P/N WIRE IDENT C0L ROUTE GAUGE LENGTH MM INCH ZONE OR PANEL ELEC. IDENT TERM. TERMINAL P/N INSTRUCTIONS 

## END 2 LEAD END 1

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.

Figure A-GHBAB - Sheet 01 Hook-up Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 756 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions **CONF ALL For detail concerning the elapsed time assumptions, refer to the Gantt chart shown in the next page:

DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 001 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 27.75 7.00 4 GET ACCESS 2.00 1.00 2 MODIFICATION OF THE WIRING IN 800VU

REMOVAL OF THE DUCTS BETWEEN FR43 AND FR45

INSTALLATION OF THE NEW BRACKETS FOR THE ROUTING INSTALLATION OF THE DUCTS BETWEEN FR43 AND FR45 INSTALLATION OF THE SENSING ELEMENTS AND THE

REMOVAL OF THE DUCTS BETWEEN FR39 AND FR40 FOR 4.00 2.00 2 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 3.00 3.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 MODIFICATION OF THE WIRING BETWEEN AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR51 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR51 AND FR53.6 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 REMOVAL OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS DRILLING OF A NEW HOLE IN THE STRUCTURE BETWEEN FR53.5 AND FR53.6 INSTALLATION OF A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 INSTALLATION OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS REPLACEMENT OF THE WEB ASSY AND THE HALF CLAMP ASSY AT FR44 OF THE SENSING ELEMENTS AT FR44

SUPPORTS BETWEEN FR39 AND FR44 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 ACCESS

F_SB_364033_6_GAAA_01_00 Figure A-GGAAA - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 2 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 001 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 3.00 3.00 1 3.00 3.00 1 INSTALLATION OF THE NEW HARNESS 2SG

INSTALLATION OF THE DUCTS BETWEEN FR39 AND FR40

INSTALLATION OF THE SLEEVES AT THE APU BLEED AIR TEST 26.00 13.00 2 7.50 3.50 2 11.00 5.50 2 4.50 4.50 1 3.00 3.00 1 14.00 7.00 2 5.25 5.25 1 0.75 0.75 1 11.25 11.25 1 2.00 2.00 1 2.75 2.75 1 5.75 5.75 1 0.50 0.50 1 5.00 5.00 1 37.75 9.50 4

70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 INSTALLATION OF THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF INSTALLATION OF THE ELECTRICAL WIRING IN THE FWD CARGO COMPARTMENT INSTALLATION OF THE ELECTRICAL WIRING IN THE AFT CARGO COMPARTMENT AND BULK CARGO COMPARTMENT MODIFICATION OF THE ELECTRICAL WIRING IN THE AFT AND BULK CARGO COMPARTMENT AND REAR FUSELAGE INSTALLATION OF AN ADDITIONAL PROFILE IN THE REAR FUSELAGE SECTION INSTALLATION OF THE ELECTRICAL WIRING IN THE REAR FUSELAGE SECTION REMOVAL OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENT DRILLING OF AN ADDITIONAL HOLE FOR THE DUAL LOOP IN THE SHEET METAL PRESSURE BULKHEAD INSTALLATION OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENTS
REMOVAL OF THE SENSING ELEMENTS IN THE REAR FUSELAGE

CLOSE−UP

F_SB_364033_6_GAAA_02_00 INSTALLATION OF THE NEW SUPPORTS FOR THE NEW HARNESS BETWEEN FR39.1 AND FR39.2

INSTALLATION OF THE SENSING ELEMENTS IN THE REAR FUSELAGE DUCT

Figure A-GGAAA - Sheet 02 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 3 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 002 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 27.75 7.00 4 GET ACCESS 2.00 1.00 2 MODIFICATION OF THE WIRING IN 800VU

REMOVAL OF THE DUCTS BETWEEN FR43 AND FR45

INSTALLATION OF THE NEW BRACKETS FOR THE ROUTING INSTALLATION OF THE DUCTS BETWEEN FR43 AND FR45 INSTALLATION OF THE SENSING ELEMENTS AND THE

REMOVAL OF THE DUCTS BETWEEN FR39 AND FR40 FOR 4.00 2.00 2 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 3.00 3.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 MODIFICATION OF THE WIRING BETWEEN AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR51 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR51 AND FR53.6 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 REMOVAL OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS DRILLING OF A NEW HOLE IN THE STRUCTURE BETWEEN FR53.5 AND FR53.6 INSTALLATION OF A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 INSTALLATION OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS REPLACEMENT OF THE WEB ASSY AND THE HALF CLAMP ASSY AT FR44 OF THE SENSING ELEMENTS AT FR44

SUPPORTS BETWEEN FR39 AND FR44 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 ACCESS

F_SB_364033_6_GAAB_01_00 Figure A-GGAAB - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 4 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 002 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 3.00 3.00 1 3.00 3.00 1 INSTALLATION OF THE NEW HARNESS 2SG

INSTALLATION OF THE DUCTS BETWEEN FR39 AND FR40

INSTALLATION OF THE SLEEVES AT THE APU BLEED AIR TEST 26.00 13.00 2 7.50 3.50 2 11.00 5.50 2 4.50 4.50 1 3.00 3.00 1 14.00 7.00 2 5.25 5.25 1 0.75 0.75 1 11.25 11.25 1 2.00 2.00 1 2.75 2.75 1 5.75 5.75 1 0.50 0.50 1 5.00 5.00 1 37.75 9.50 4

70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 INSTALLATION OF THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF INSTALLATION OF THE ELECTRICAL WIRING IN THE FWD CARGO COMPARTMENT INSTALLATION OF THE ELECTRICAL WIRING IN THE AFT CARGO COMPARTMENT AND BULK CARGO COMPARTMENT MODIFICATION OF THE ELECTRICAL WIRING IN THE AFT AND BULK CARGO COMPARTMENT AND REAR FUSELAGE INSTALLATION OF AN ADDITIONAL PROFILE IN THE REAR FUSELAGE SECTION INSTALLATION OF THE ELECTRICAL WIRING IN THE REAR FUSELAGE SECTION REMOVAL OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENT DRILLING OF AN ADDITIONAL HOLE FOR THE DUAL LOOP IN THE SHEET METAL PRESSURE BULKHEAD INSTALLATION OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENTS
REMOVAL OF THE SENSING ELEMENTS IN THE REAR FUSELAGE

CLOSE−UP INSTALLATION OF THE NEW SUPPORTS FOR THE NEW HARNESS BETWEEN FR39.1 AND FR39.2

INSTALLATION OF THE SENSING ELEMENTS IN THE REAR FUSELAGE DUCT

F_SB_364033_6_GAAB_02_00 Figure A-GGAAB - Sheet 02 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 5 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 003 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 27.75 7.00 4 GET ACCESS 2.00 1.00 2 MODIFICATION OF THE WIRING IN 800VU

REMOVAL OF THE DUCTS BETWEEN FR43 AND FR45

INSTALLATION OF THE NEW BRACKETS FOR THE ROUTING INSTALLATION OF THE DUCTS BETWEEN FR43 AND FR45 INSTALLATION OF THE SENSING ELEMENTS AND THE

REMOVAL OF THE DUCTS BETWEEN FR39 AND FR40 FOR 4.00 2.00 2 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 3.00 3.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 MODIFICATION OF THE WIRING BETWEEN AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR51 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR51 AND FR53.6 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 REMOVAL OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS DRILLING OF A NEW HOLE IN THE STRUCTURE BETWEEN FR53.5 AND FR53.6 INSTALLATION OF A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 INSTALLATION OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS REPLACEMENT OF THE WEB ASSY AND THE HALF CLAMP ASSY AT FR44 OF THE SENSING ELEMENTS AT FR44

SUPPORTS BETWEEN FR39 AND FR44 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 ACCESS

F_SB_364033_6_GAAC_01_00 Figure A-GGAAC - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 6 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 003 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 3.00 3.00 1 3.00 3.00 1 INSTALLATION OF THE NEW HARNESS 2SG

INSTALLATION OF THE DUCTS BETWEEN FR39 AND FR40

INSTALLATION OF THE SLEEVES AT THE APU BLEED AIR TEST 26.00 13.00 2 7.50 3.50 2 11.00 5.50 2 4.50 4.50 1 3.00 3.00 1 14.00 7.00 2 5.25 5.25 1 0.75 0.75 1 11.25 11.25 1 2.00 2.00 1 2.75 2.75 1 5.75 5.75 1 0.50 0.50 1 5.00 5.00 1 37.75 9.50 4

70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 INSTALLATION OF THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF INSTALLATION OF THE ELECTRICAL WIRING IN THE FWD CARGO COMPARTMENT INSTALLATION OF THE ELECTRICAL WIRING IN THE AFT CARGO COMPARTMENT AND BULK CARGO COMPARTMENT MODIFICATION OF THE ELECTRICAL WIRING IN THE AFT AND BULK CARGO COMPARTMENT AND REAR FUSELAGE INSTALLATION OF AN ADDITIONAL PROFILE IN THE REAR FUSELAGE SECTION INSTALLATION OF THE ELECTRICAL WIRING IN THE REAR FUSELAGE SECTION REMOVAL OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENT DRILLING OF AN ADDITIONAL HOLE FOR THE DUAL LOOP IN THE SHEET METAL PRESSURE BULKHEAD INSTALLATION OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENTS
REMOVAL OF THE SENSING ELEMENTS IN THE REAR FUSELAGE

CLOSE−UP INSTALLATION OF THE NEW SUPPORTS FOR THE NEW HARNESS BETWEEN FR39.1 AND FR39.2

INSTALLATION OF THE SENSING ELEMENTS IN THE REAR FUSELAGE DUCT

F_SB_364033_6_GAAC_02_00 Figure A-GGAAC - Sheet 02 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 7 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 004 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 27.75 7.00 4 GET ACCESS 2.00 1.00 2 MODIFICATION OF THE WIRING IN 800VU

REMOVAL OF THE DUCTS BETWEEN FR43 AND FR45

INSTALLATION OF THE NEW BRACKETS FOR THE ROUTING INSTALLATION OF THE DUCTS BETWEEN FR43 AND FR45 INSTALLATION OF THE SENSING ELEMENTS AND THE

REMOVAL OF THE DUCTS BETWEEN FR39 AND FR40 FOR 4.00 2.00 2 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 3.00 3.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 MODIFICATION OF THE WIRING BETWEEN AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR51 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR51 AND FR53.6 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 REMOVAL OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS DRILLING OF A NEW HOLE IN THE STRUCTURE BETWEEN FR53.5 AND FR53.6 INSTALLATION OF A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 INSTALLATION OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS REPLACEMENT OF THE WEB ASSY AND THE HALF CLAMP ASSY AT FR44 OF THE SENSING ELEMENTS AT FR44

SUPPORTS BETWEEN FR39 AND FR44 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 ACCESS

F_SB_364033_6_GAAD_01_00 Figure A-GGAAD - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 8 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 004 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 268.75 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 3.00 3.00 1 3.00 3.00 1 INSTALLATION OF THE NEW HARNESS 2SG

INSTALLATION OF THE DUCTS BETWEEN FR39 AND FR40

INSTALLATION OF THE SLEEVES AT THE APU BLEED AIR TEST 26.00 13.00 2 7.50 3.50 2 11.00 5.50 2 4.50 4.50 1 3.00 3.00 1 14.00 7.00 2 5.25 5.25 1 0.75 0.75 1 11.25 11.25 1 2.00 2.00 1 2.75 2.75 1 5.75 5.75 1 0.50 0.50 1 5.00 5.00 1 37.75 9.50 4

70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 INSTALLATION OF THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF INSTALLATION OF THE ELECTRICAL WIRING IN THE FWD CARGO COMPARTMENT INSTALLATION OF THE ELECTRICAL WIRING IN THE AFT CARGO COMPARTMENT AND BULK CARGO COMPARTMENT MODIFICATION OF THE ELECTRICAL WIRING IN THE AFT AND BULK CARGO COMPARTMENT AND REAR FUSELAGE INSTALLATION OF AN ADDITIONAL PROFILE IN THE REAR FUSELAGE SECTION INSTALLATION OF THE ELECTRICAL WIRING IN THE REAR FUSELAGE SECTION REMOVAL OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENT DRILLING OF AN ADDITIONAL HOLE FOR THE DUAL LOOP IN THE SHEET METAL PRESSURE BULKHEAD INSTALLATION OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENTS
REMOVAL OF THE SENSING ELEMENTS IN THE REAR FUSELAGE

CLOSE−UP INSTALLATION OF THE NEW SUPPORTS FOR THE NEW HARNESS BETWEEN FR39.1 AND FR39.2

INSTALLATION OF THE SENSING ELEMENTS IN THE REAR FUSELAGE DUCT

F_SB_364033_6_GAAD_02_00 Figure A-GGAAD - Sheet 02 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 9 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 005 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 273.00 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 27.75 7.00 4 GET ACCESS 2.00 1.00 2 MODIFICATION OF THE WIRING IN 800VU

REMOVAL OF THE DUCTS BETWEEN FR43 AND FR45

INSTALLATION OF THE NEW BRACKETS FOR THE ROUTING INSTALLATION OF THE DUCTS BETWEEN FR43 AND FR45 INSTALLATION OF THE SENSING ELEMENTS AND THE

REMOVAL OF THE DUCTS BETWEEN FR39 AND FR40 FOR 4.00 2.00 2 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 4.00 4.00 1 1.00 1.00 1 1.00 1.00 1 1.00 1.00 1 2.00 2.00 1 1.00 1.00 1 3.00 3.00 1 1.00 1.00 1 2.00 2.00 1 14.00 14.00 1 14.00 14.00 1 21.00 21.00 1 14.00 14.00 1 1.00 1.00 1 70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 MODIFICATION OF THE WIRING BETWEEN AVIONICS COMPARTMENT AND THE CARGO COMPARTMENT REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR39 AND FR44 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR51 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR51 AND FR53.6 REMOVAL OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 REMOVAL OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS DRILLING OF A NEW HOLE IN THE STRUCTURE BETWEEN FR53.5 AND FR53.6 INSTALLATION OF A NEW SUPPORT FOR THE ROUTING OF THE SENSING ELEMENTS BETWEEN FR53.5 AND FR53.6 INSTALLATION OF THE DUCTS BETWEEN FR53.5 AND FR53.6 FOR ACCESS REPLACEMENT OF THE WEB ASSY AND THE HALF CLAMP ASSY AT FR44 OF THE SENSING ELEMENTS AT FR44

SUPPORTS BETWEEN FR39 AND FR44 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR44 AND FR50 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR50 AND FR53.6 INSTALLATION OF THE SENSING ELEMENTS AND THE SUPPORTS BETWEEN FR53.6 AND FR55 ACCESS

F_SB_364033_6_GAAE_01_00 Figure A-GGAAE - Sheet 01 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 10 6

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

# @A340 SERVICE BULLETIN Appendix 01: Elapsed Time Assumptions
**CONF 005 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−36−4033**

SB ELAPSED TIME (HOURS) MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 273.00 144.00 STEPS

75 0

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:** PER

: : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS 3.00 3.00 1 3.00 3.00 1 INSTALLATION OF THE NEW HARNESS 2SG

INSTALLATION OF THE DUCTS BETWEEN FR39 AND FR40

INSTALLATION OF THE SLEEVES AT THE APU BLEED AIR TEST 26.00 13.00 2 7.50 3.50 2 11.00 5.50 2 4.50 4.50 1 3.00 3.00 1 14.00 7.00 2 5.25 5.25 1 0.75 0.75 1 11.25 11.25 1 2.00 2.00 1 2.75 2.75 1

0.50 0.50 1 5.00 5.00 1 37.75 9.50 4

70 60 50 40 30 20 10 5 15 25 35 45 55 65 80 85 90 95 100 105 110 115 120 125 130 135 140 145 INSTALLATION OF THE INTERCONNECTING ELECTRICAL WIRE FIN 309HF AND 310HF INSTALLATION OF THE ELECTRICAL WIRING IN THE FWD CARGO COMPARTMENT INSTALLATION OF THE ELECTRICAL WIRING IN THE AFT CARGO COMPARTMENT AND BULK CARGO COMPARTMENT MODIFICATION OF THE ELECTRICAL WIRING IN THE AFT AND BULK CARGO COMPARTMENT AND REAR FUSELAGE INSTALLATION OF AN ADDITIONAL PROFILE IN THE REAR FUSELAGE SECTION INSTALLATION OF THE ELECTRICAL WIRING IN THE REAR FUSELAGE SECTION REMOVAL OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENT DRILLING OF AN ADDITIONAL HOLE FOR THE DUAL LOOP IN THE SHEET METAL PRESSURE BULKHEAD INSTALLATION OF THE SENSING ELEMENTS IN THE AFT AND BULK CARGO COMPARTMENTS
REMOVAL OF THE SENSING ELEMENTS IN THE REAR FUSELAGE

CLOSE−UP INSTALLATION OF THE NEW SUPPORTS FOR THE NEW HARNESS BETWEEN FR39.1 AND FR39.2

DUCT

F_SB_364033_6_GAAE_02_00 REMOVAL OF THE SENSING ELEMENT, FIN 149HF INSTALLATION OF THE SENSING ELEMENTS IN THE 4.25 4.25 1 5.75 5.75 1 REAR FUSELAGE

Figure A-GGAAE - Sheet 02 Gantt Chart DATE: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 11 6

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: PNEUMATIC - LEAK DETECTION - INTRODUCE ADAPTED DUAL LOOP OVERHEAT LEAK DETECTION APU BLEED AIR DUCT MODIFICATION No.: 55198D46290 55198D46286 55961D46493 55962D46494 58529D46961 58530D46962 Please complete the appropriate item (A or B): A - SB WILL BEembodied 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 BEENembodied 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: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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# @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: Sep 23/11 SERVICE BULLETIN No.: A340-36-4033 REVISION No.: 01 - Jan 28/13 Page: 1 6

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