NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY AOA PROBE FLAT PLATE

航空

游客，如果您要查看本帖隐藏内容请回复

航空

@A340-500/600
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
This summary is for information only and is not approved for modification of the aircraft.
MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 34
TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY
AOA PROBE FLAT PLATE
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR 203295S32646
MINOR None
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the
mass, balance, structural strength, reliability, operational characteristics affecting the
airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES
Following a recent in-service event, as a precautionary measure, Airbus requires to suspend the
installation of the AOA (Angle Of Attack) conic plates as per Operator Information Transmission (OIT)
No. 999.0086/12, currently performed through an Airbus monitored campaign with Service Bulletin No.
A340-34-5081.
This modification requires the removal of the conic plates PN F3411060200000 and PN
F3411060900000, and the installation of flat plates PN F3411007920200 (LH) / PN F3411007920300
(RH).
Also, it requires to change the 3 AOA Sensor Protection Covers (FINs 7955ME, 7956ME and 7957ME)
stored in Flight Kit No 2 (FIN 7500NW or FIN 7503NW).
Refer to OIT No. 999.0086/12 and FOT No. 999.0089/12 for further explanations.
For aircraft already fitted with the AOA conic plates through retrofit or from production, Airbus released
associated operational recommendations in an FOT No. 999.0089/12, the Operations Engineering
Bulletin (OEB) 45 and Flight Manual (FM) Temporary Revision 294.
This Service Bulletin modifies the Ground System Equipment (the AOA Protection Covers) needed for
parking, mooring or storing the aircraft.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
Accomplishment of this Service Bulletin cancels OEB 45 and FM TR294. It is expected that an
Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued
to confirm this cancellation.
This Service Bulletin modifies the Ground System Equipment (the AOA Protection Covers) needed for
parking, mooring or storing the aircraft.
The operational consequence of this Service Bulletin is the modification of the Flight Manual (FM) and
Flight Crew Operating Manual (FCOM) by removing temporary operational measures introduced by
OEB 45, FOT No. 999.0089/12 and FM TR294.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO
POTENTIAL AD YES A/C OPERATION AFFECTED YES
RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO
COST SAVING NO LROPS AFFECTED NO
STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO
NOTE (1): Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION
**CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Component COMPA01 1 See SB Flat Plates, Covers
Component COMPA02 1 See SB Screws
**CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Component COMPA01 1 See SB Flat Plates, Covers
Component COMPA02 1 See SB Screws
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
06U 25R 36V 62X 70U 72W AHY CES CHH DLH ETD HFY IBE
QAF QTR SAA SIA TAM THA UAE VIR
CONCURRENT REQUIREMENTS
None
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
REFERENCES / REPERCUSSIONS
TFU None
OEB 45
AOT None
SIL None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None
OTHER OIT No. 999.0086/12
OTHER FOT No. 999.0089/12
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO
HARD NO
SOFT NO
OBRM NO
MANPOWER
**CONF 001
Task 345093-831-801-001: Modification of the AOA sensor plates.
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
**CONF 002
Task 345093-831-801-001: Modification of the AOA sensor plates.
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
APPENDICES
**CONF ALL
APPENDIX 01: Elapsed Time Assumption
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
**CONF ALL
NOTE:
TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS.
BEFORE
FR19
FR18
3FP1
3FP2
3FP3
A B
A B
A B
A
OR
THALES GOODRICH
F_SB_345093_5_SAAA_01_01
Figure A-FSAAA - Sheet 01
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
**CONF ALL
TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS.
AFTER
CAUTION:
NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND SHALL REMAIN AS DELIVERED.
C
NOTE:
DEPENDS ON AIRCRAFT CONFIGURATION.
ONLY ONE CONFIGURATION SHOWN, AOA SENSOR
F_SB_345093_5_SAAA_02_01
Figure A-FSAAA - Sheet 02
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
**CONF 001
B
FR69
FR73
A
A
Z160
B
7500NW
FLIGHT KIT No 2
NOTE:
ARE STORED IN FLIGHT KIT No 2 FIN (7500NW)
AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME)
F_SB_345093_5_SBAA_01_01
Figure A-FSBAA - Sheet 01
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
**CONF 002
A
A
Z130
FR20
FR25
FR26
B
FLIGHT KIT No 2
NOTE:
ARE STORED IN FLIGHT KIT No 2 FIN (7503NW)
AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME)
B
7503NW
F_SB_345093_5_SBAB_01_01
Figure A-FSBAB - Sheet 01
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
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
MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 34
TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY
AOA PROBE FLAT PLATE
MODIFICATION No.: 203295S32646
This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
NOTE: This modification is applicable by Service Bulletin only.
NOTE: This Service Bulletin is only applicable to aircraft listed below on which Mod.
No. 201609S31961 (INSTALL A NEW CONIC PLATE FOR NEW AOA
(ANGLE OF ATTACK SENSOR) THALES) or Mod. No. 201610S31887
(INSTALL A NEW CONIC PLATE FOR NEW AOA (ANGLE OF ATTACK
SENSOR) GOODRICH AND OLD THALES) are embodied or on which
Service Bulletin No. A340-34-5081 is accomplished.
(1) Models
340-541 340-542 340-642
(2) Effectivity by MSN
0371 0376 0383 0391 0394 0410 0416-0417 0426 0431 0436 0440 0445 0449 0453
0457 0460 0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499 0514 0517
0520 0523 0531 0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572 0575
0577 0580 0583 0586 0601 0604 0606 0608 0611 0615 0617 0619 0622 0624 0626
0628 0630 0639 0672 0677 0681 0685 0689 0694 0698 0702 0706 0710 0715 0719
0723 0727 0736 0740 0744 0748 0753 0757 0761-0768 0771 0775 0779 0783 0787
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
0790 0794 0798 0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902 0910
0912 0917 0924 0929 0933 0953 0960 0972 0981 0987 0993 1005 1017 1030 1040
1079 1091 1102 1122
(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
06U 1091 1102
25R 0924
36V 0391 0416
62X 0779
70U 0902
72W 0917
AHY 0886 0894
CES 0468 0488 0514 0577 0586
CHH 0436 0453 0475
DLH 0482 0517 0523 0537 0540 0543 0566 0569 0580 0583 0762 0763
0767 0771 0790 0794 0812 0846 0848 0897 0972 0981 0987 1005
ETD 0748 0757 0761 0783 0829 0837 0870 0929 0933 1030 1040
HFY 0910 0912
IBE 0431 0440 0460 0601 0604 0606 0617 0619 0672 0702 0727 0744
0960 0993 1017 1079 1122
QAF 0495
QTR 0715 0740 0766 0798
SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630
SIA 0478 0492 0499 0560 0563
TAM 0445 0464
THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953
UAE 0394 0457 0471 0485 0520 0572 0608 0611 0685 0694
VIR 0371 0376 0383 0449 0575 0615 0622 0639 0706 0723 0736 0753
0764 0765 0768 0787 0804
(4) Configuration by MSN
MSN CONFIGURATION
0371 0376 0383 0391 0416 0449 001
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
MSN CONFIGURATION
0394 0410 0417 0426 0431 0436 0440 0445 0453 0457 0460
0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499
0514 0517 0520 0523 0531 0534 0537 0540 0543 0547 0557
0560 0563 0566 0569 0572 0575 0577 0580 0583 0586 0601
0604 0606 0608 0611 0615 0617 0619 0622 0624 0626 0628
0630 0639 0672 0677 0681 0685 0689 0694 0698 0702 0706
0710 0715 0719 0723 0727 0736 0740 0744 0748 0753 0757
0761 0762 0763 0764 0765 0766 0767 0768 0771 0775 0779
0783 0787 0790 0794 0798 0804 0812 0829 0837 0846 0848
0870 0886 0894 0897 0902 0910 0912 0917 0924 0929 0933
0953 0960 0972 0981 0987 0993 1005 1017 1030 1040 1079
1091 1102 1122
002
(5) Configuration definition
**CONF 001
Config. 001 is valid for aircraft on which Mod. No. 50648D44169 is not embodied.
**CONF 002
Config. 002 is valid for aircraft on which Mod. No. 50648D44169 is embodied.
(6) Material Effectivity
MATERIAL QTY PER A/C SEE NOTES
Consumable CMLA01 1
Component COMPA01 1
Component COMPA02 1
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
Following a recent in-service event, as a precautionary measure, Airbus requires to
suspend the installation of the AOA (Angle Of Attack) conic plates as per Operator
Information Transmission (OIT) No. 999.0086/12, currently performed through an Airbus
monitored campaign with Service Bulletin No. A340-34-5081.
(2) Objective/Action
This modification requires the removal of the conic plates PN F3411060200000 and PN
F3411060900000, and the installation of flat plates PN F3411007920200 (LH) / PN
F3411007920300 (RH).
Also, it requires to change the 3 AOA Sensor Protection Covers (FINs 7955ME, 7956ME
and 7957ME) stored in Flight Kit No 2 (FIN 7500NW or FIN 7503NW).
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 3
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(3) Advantages
Refer to OIT No. 999.0086/12 and FOT No. 999.0089/12 for further explanations.
(4) Operational/Maintenance Consequences
For aircraft already fitted with the AOA conic plates through retrofit or from production,
Airbus released associated operational recommendations in an FOT No. 999.0089/12,
the Operations Engineering Bulletin (OEB) 45 and Flight Manual (FM) Temporary
Revision 294.
This Service Bulletin modifies the Ground System Equipment (the AOA Protection
Covers) needed for parking, mooring or storing the aircraft.
Accomplishment of this Service Bulletin cancels OEB 45 and FM TR294. It is expected
that an Airworthiness Directive (AD) published by the European Aviation Safety Agency
(EASA) will be issued to confirm this cancellation.
This Service Bulletin modifies the Ground System Equipment (the AOA Protection
Covers) needed for parking, mooring or storing the aircraft.
The operational consequence of this Service Bulletin is the modification of the Flight
Manual (FM) and Flight Crew Operating Manual (FCOM) by removing temporary
operational measures introduced by OEB 45, FOT No. 999.0089/12 and FM TR294.
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
**CONF 001
Task 345093-831-801-001: Modification of the AOA sensor plates.
(1) Replace the Conic Plate of the AOA Sensor FIN 3FP1, on the LH Side.
(2) Replace the Conic Plates of the AOA Sensors FINs 3FP2 and 3FP3, on the RH
Side.
(3) Replace the AOA Protection Covers in the Flight Kit No 2 (FIN 7500NW).
**CONF 002
Task 345093-831-801-001: Modification of the AOA sensor plates.
(1) Replace the Conic Plate of the AOA Sensor FIN 3FP1, on the LH Side.
(2) Replace the Conic Plates of the AOA Sensors FINs 3FP2 and 3FP3, on the RH
Side.
(3) Replace the AOA Protection Covers in the Flight Kit No 2 (FIN 7503NW).
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 4
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
**CONF ALL
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
Accomplishment of this Service Bulletin must be done at the earliest opportunity where
manpower and facilities are available but within 5 months from the initial Service Bulletin
date.
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness
Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued
to confirm this classification. It is anticipated that the AD will confirm the threshold
given above but reference should be made to the AD for confirmation of the mandated
accomplishment timescale.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
**CONF 001
Task 345093-831-801-001: Modification of the AOA sensor plates.
Get Access 0.50
On Aircraft
Replace the Conic Plate of the AOA Sensor FIN 3FP1,
on the LH Side.
1.50
Replace the Conic Plates of the AOA Sensors FINs
3FP2 and 3FP3, on the RH Side.
3.00
Replace the AOA Protection Covers in the Flight Kit No
2 (FIN 7500NW).
0.50
Tests 0.25
Close-Up 0.50
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 5
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Task 345093-831-801-001: Modification of the AOA sensor plates.
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
NOTE: For detail concerning the elapsed time assumption, refer to APPENDIX 01:
Elapsed Time Assumption .
**CONF 002
Task 345093-831-801-001: Modification of the AOA sensor plates.
Get Access 0.50
On Aircraft
Replace the Conic Plate of the AOA Sensor FIN 3FP1,
on the LH Side.
1.50
Replace the Conic Plates of the AOA Sensors FINs
3FP2 and 3FP3, on the RH Side.
3.00
Replace the AOA Protection Covers in the Flight Kit No
2 (FIN 7503NW).
0.50
Tests 0.25
Close-Up 0.50
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
NOTE: For detail concerning the elapsed time assumption, refer to APPENDIX 01:
Elapsed Time Assumption .
**CONF ALL
H. WEIGHT AND BALANCE
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 -0.549 KG (-1.2103 LB)
Effect on Balance -7.502 KGM (-54.262 LB.FT )
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53
12-34-24 20-21-11 20-28-00
52-30-00 52-41-00
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 6
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00
Flight Crew Operating Manual (FCOM)
Flight Manual (FM)
Standards Manual (SM)
Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00
Weight and Balance Manual (WBM) Chapter 1-00-07
**CONF 002
Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53
12-34-24 20-21-11 20-28-00
52-30-00 52-41-00
Consumable Material List (CML)
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00
Flight Crew Operating Manual (FCOM)
Flight Manual (FM)
Standards Manual (SM)
Structural Repair Manual (SRM) 51-24-00 51-42-00 51-43-00
Weight and Balance Manual (WBM) Chapter 1-00-07
**CONF ALL
K. PUBLICATION AFFECTED
Aircraft Maintenance Manual (AMM) 10-11-00 12-21-11 34-11-19
Aircraft Wiring List (AWL)
Flight Crew Operating Manual (FCOM)
Flight Manual (FM)
Illustrated Parts Catalog (IPC) 25-73-04 34-11-01
Tool Equipment Manual (TEM) 10-11-00
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 prior
to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online
through the SB Reporting service or alternatively by fax to:
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.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 7
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
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
Plate F3411060900000 F3411007920200 01 NO
Plate F3411060200000 F3411007920200 01 NO
AOA Sensor
Protection Cover
98D34203003000 98F10001000000 01 NO
Plate F3411060200000 F3411007920300 01 NO
Plate F3411060900000 F3411007920300 01 NO
NOTE: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE: Only the mixability configuration(s) and condition(s) stated in this Service
Bulletin are approved.
**CONF 002
DESCRIPTION OLD PART N˚ NEW PART N˚ INT MIXABILITY SEE
NOTES
Plate F3411060900000 F3411007920200 01 NO
Plate F3411060200000 F3411007920200 01 NO
AOA Sensor
Protection Cover
98D34203003000 98F10001000000 01 NO
Plate F3411060200000 F3411007920300 01 NO
Plate F3411060900000 F3411007920300 01 NO
NOTE: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE: Only the mixability configuration(s) and condition(s) stated in this Service
Bulletin are approved.
**CONF ALL
M. SPARES
AOA Sensor Protection Cover 98D34203003000
Plate F3411060200000
Plate F3411060900000
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 8
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
Component COMPA01 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
IFD - In Flight Desk
Weg beim Jaeger 150
D-22335 HAMBOURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by fax: +49 40 50 76 4012
For ordering by E-mail:
ifd.spares@airbus.com
Component COMPA02 Airbus Material, Logistics and Suppliers do
not stock standard hardware as competitive
multiple suppliers ensure access to minimum
prices Airbus recommends Customers with
aircraft shown in the effectivity of this Service
Bulletin to send a purchase order to B/E
Aerospace. The address is:
B/E AEROSPACE INC
CONSUMABLES MANAGEMENT
10000 NW 15TH Terrace Miami
FL 33172
USA
Tel EMEA: +49 (0) 40 822 285 31500
Tel US: +1 305 925 2600
Tel ASIA: +1 310 900 1300
Fax EMEA: +49 (0) 40 822 285 31010
Fax US: +1 305 507 7191
Fax ASIA: +1 310 819 1200
SITA: MIAMMCR
E-Mail: AOGdesk_CMG@beaerospace.com
internet: www.beconsumables.com
or, alternatively any other source on the open
market.
(2) Price and Availability
No AIRBUS kit will be provided.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 9
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be
purchased by a spares purchase order.
Operator supplied standard hardware parts required to accomplish this Service Bulletin
are to be supplied from the Operator’s stock.
B. INDUSTRY SUPPORT INFORMATION
AIRBUS will share the costs of accomplishment of this Service Bulletin by crediting the
operator supplied AIRBUS parts for orders placed before Jun 30/13. Claims for this allowance
should be received not later than 90 days after completion of the last affected aircraft of your
fleet.
For the accomplishment of this Service Bulletin before Jun 30/13, AIRBUS will credit the
manhours indicated in this Service Bulletin at the agreed in-house warranty labor rate for
claims received not later than 90 days after completion of the last affected aircraft of your
fleet.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit
management department.
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
France
Tel : (33) 5 67 19 06 22
E-mail : monitored.retrofit@airbus.com
Fax : (33) 5 61 93 27 45
C. LIST OF COMPONENTS
No Kit
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO CML
MAT. No.
QTY PER A/C SEE
NOTES
Release Agent (obsolete Use
05-013a)
05-013 As required
Corrosion Inhibitingfillet Consistency 09-016 As required
Fuel Tank Sealant Quick Repair
Permanent
09-058 As required
Solvent General Purpose 11-026 As required
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 10
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(2) Components
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE
NOTES
2 F3411007920200 1 PLATE (2) F3411060200000 01
(2) F3411060900000 01
2 F3411007920300 2 PLATE (2) F3411060200000 01
(2) F3411060900000 01
98F10001000000 3 AOAPRTCT 98D34203003000 01
NOTE: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE
NOTES
1 NAS1102-3-14 21 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.
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
(3) Equipment
None
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
None
F. TOOLING
None
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 11
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
This Page Intentionally Left Blank
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 12
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS
Task 345093-831-801-001 - Modification of the AOA sensor plates.
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP
ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS
NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND
OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION
AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.
Task Associated Data
**CONF 001
Zone
121 122 160
Modified FIN
7955ME 7956ME 7957ME 7500NW
Access
Door 823
Other access Access platform
Manpower
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
**CONF 002
Zone
121 122 130
Modified FIN
7955ME 7956ME 7957ME 7503NW
Access
Door 821
Other access Access platform
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 13
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Manpower
TOTAL MANHOURS 6.25
ELAPSED TIME (HOURS) 4.25
**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 345093-910-001-001 - Standard Practices
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001
06-31-53, Page Block 001
Task 20-21-11-911-801
Task 20-28-00-912-802
Task 20-28-00-912-805
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM) 20-51-20
Structural Repair Manual (SRM) 51-24-00
51-42-00
51-43-00
(a) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
Consumable Materials List (CML).
(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(d) To torque tighten the standard threaded fasteners, refer to AMM Task
20-21-11-911-801.
(e) Remove and install fasteners in accordance with SRM 51-42-00.
(f) Obtain alternative and substitute fasteners data, in accordance with SRM 51-43-00.
(g) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(h) For the electrical bonding, refer to ESPM 20-51-20 and AMM Task
20-28-00-912-802 and/or AMM Task 20-28-00-912-805.
(i) Apply sealant in accordance with SRM 51-24-00.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 14
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(2) Subtask 345093-839-001-001 - Administrative
Manpower Resources
Skills NON SPECIFIC
(a) Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
(1) Subtask 345093-910-001-001 - Standard Practices
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001
06-31-53, Page Block 001
Task 20-21-11-911-801
Task 20-28-00-912-802
Task 20-28-00-912-805
Consumable Material List (CML)
Elec. Std. Practices Manual (ESPM) 20-51-20
Structural Repair Manual (SRM) 51-24-00
51-42-00
51-43-00
(a) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
Consumable Materials List (CML).
(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.
(c) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(d) To torque tighten the standard threaded fasteners, refer to AMM Task
20-21-11-911-801.
(e) Remove and install fasteners in accordance with SRM 51-42-00.
(f) Obtain alternative and substitute fasteners data, in accordance with SRM 51-43-00.
(g) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(h) For the electrical bonding, refer to ESPM 20-51-20 and AMM Task
20-28-00-912-802 and/or AMM Task 20-28-00-912-805.
(i) Apply sealant in accordance with SRM 51-24-00.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 15
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(2) Subtask 345093-839-001-001 - Administrative
Manpower Resources
Skills NON SPECIFIC
(a) Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF ALL
B. PREPARATION
**CONF 001
(1) Subtask 345093-941-001-001 - Job Set-up
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001
Task 12-34-24-860-802
Task 52-30-00-010-803
52-41-00, Page Block 001
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Put the access platforms in position at the Bulk cargo-compartment door 823, at
avionics compartment door 811 and at zone 121 to get access to the AOA sensor
FIN 3FP1 and at zone 122 to get access to the AOA sensors FINs 3FP2 and 3FP3.
(c) Open the Bulk cargo-compartment door 823, refer to AMM Task 52-30-00-010-803.
(d) Open the avionics compartment door 811, refer to AMM 52-41-00, Page Block 001
and AMM 06-41-53, Page Block 001.
(e) Safety precaution
1 On the panel 225VU:
a Make sure that the PROBE/WINDOW HEAT pushbutton switch is
released (the ON legend is OFF).
**CONF 002
(1) Subtask 345093-941-001-002 - Job Set-up
Manpower Resources
Skills NON SPECIFIC
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 16
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
References
Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001
Task 12-34-24-860-802
Task 52-30-00-010-801
52-41-00, Page Block 001
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Put the access platform(s) in position at the FWD cargo-compartment door 821, at
avionics compartment door 811 and at zones 121 to get access to the AOA sensor
FIN 3FP1 and zone 122 to get access to the AOA sensors FINs 3FP2 and 3FP3.
(c) Open the FWD cargo-compartment door 821, refer to AMM Task
52-30-00-010-801.
(d) Open the avionics compartment door 811, refer to AMM 52-41-00, Page Block 001
and AMM 06-41-53, Page Block 001.
(e) Safety precaution
1 On the panel 225VU:
a Make sure that the PROBE/WINDOW HEAT pushbutton switch is
released (the ON legend is OFF).
**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 345093-831-001-001 - Replace the Conic Plate of the AOA Sensor FIN
3FP1, on the LH Side.
Work Zones and Access Panels
Zone Access/Work location
121 Access Other access Access platform
Manpower Resources
Manhours 1.50
Minimum number of person 1
Subtask elapsed time 1.50
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
2 F3411007920200 1 PLATE
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 17
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
1 NAS1102-3-14 7 SCREW
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO
CML MAT. No.
QTY PER A/C SEE
NOTES
Solvent General Purpose 11-026 As required
References
Structural Repair Manual (SRM) 51-42-00
51-43-00
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
NOTE: The screw item (3) must not be removed to keep the AOA sensor in
position and to avoid removing it.
(a) Replace the conic plate by the flat plate of the AOA Sensor FIN 3FP1:
NOTE: Make sure that the previous plate installed on the aircraft is a conic
plate. Refer to aircraft maintenance records.
In accordance with SRM 51-42-00 and SRM 51-43-00
1 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
2 Remove the conic plate:
Refer to Fig. A-FBAAA Sheet 01
1 Plate F3411060200000 Item (2) Discard
or
1 Plate F3411060900000 Item (2) Discard
attached with:
7 Screw Item (1) Discard
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 18
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
3 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
4 Install the flat plate:
CAUTION: NEW AOA FLAT PLATE SHALL NOT BE PAINTED AND
SHALL REMAIN AS DELIVERED.
NOTE: The attaching holes of the flat plates are delivered stripped
from protection at level of the surface of the bonding areas.
Refer to Fig. A-FBAAA Sheet 02
1 Plate F3411007920200 Item 2
attached with:
7 Screw NAS1102-3-14 Item 1
(2) Subtask 345093-831-002-001 - Replace the Conic Plates of the AOA Sensors FINs
3FP2 and 3FP3, on the RH Side.
Work Zones and Access Panels
Zone Access/Work location
122 Access Other access Access platform
Manpower Resources
Manhours 3.00
Minimum number of person 1
Subtask elapsed time 3.00
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
2 F3411007920300 2 PLATE
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
1 NAS1102-3-14 14 SCREW
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 19
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO
CML MAT. No.
QTY PER A/C SEE
NOTES
Solvent General Purpose 11-026 As required
References
Structural Repair Manual (SRM) 51-42-00
51-43-00
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
NOTE: The screw item (3) must not be removed to keep the AOA sensors in
position and to avoid removing them.
(a) Replace the conic plates by the flat plates of the AOA Sensors FINs 3FP2 and
3FP3:
NOTE: Make sure that the previous plate installed on the aircraft is a conic
plate. Refer to aircraft maintenance records.
In accordance with SRM 51-42-00 and SRM 51-43-00
1 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
2 Remove the conic plates:
Refer to Fig. A-FBAAA Sheet 01
2 Plate F3411060200000 Item (2) Discard
or
2 Plate F3411060900000 Item (2) Discard
attached with:
14 Srew Item (1) Discard
3 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
4 Install the flat plates:
CAUTION: NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND
SHALL REMAIN AS DELIVERED.
NOTE: The attaching holes of the flat plates are delivered stripped
from protection at level of the surface of the bonding areas.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 20
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
Refer to Fig. A-FBAAA Sheet 02
2 Plate F3411007920300 Item 2
attached with:
14 Screw NAS1102-3-14 Item 1
(3) Subtask 345093-831-003-001 - Replace the AOA Protection Covers in the Flight Kit
No 2 (FIN 7500NW).
Work Zones and Access Panels
Zone Access/Work location
160 Access Door 823
Manpower Resources
Manhours 0.50
Minimum number of person 1
Subtask elapsed time 0.50
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
98F10001000000 3 AOAPRTCT
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
References
Fig. A-FBBAA
Modification of AOA Protection Covers in
the Flight Kit No 2
Sheet 01
NOTE: Depending on airline internal policy the Flight Kit No 2 may not be
located in the place defined by Fig. A-FBBAA Sheet 01. Refer to airline
internal policy for exact location for Flight Kit No 2 and/or its contents.
(a) Remove in the Flight Kit No 2 (FIN 7500NW):
Refer to Fig. A-FBBAA Sheet 01:
FIN 7955ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
FIN 7956ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 21
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
FIN 7957ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
(b) Install in the Flight Kit No 2 (FIN 7500NW):
Fig. A-FBBAA Sheet 01:
FIN 7955ME
1 AOA Sensor Protection
Cover
98F10001000000
FIN 7956ME
1 AOA Sensor Protection
Cover
98F10001000000
FIN 7957ME
1 AOA Sensor Protection
Cover
98F10001000000
**CONF 002
(1) Subtask 345093-831-001-001 - Replace the Conic Plate of the AOA Sensor FIN
3FP1, on the LH Side.
Work Zones and Access Panels
Zone Access/Work location
121 Access Other access Access platform
Manpower Resources
Manhours 1.50
Minimum number of person 1
Subtask elapsed time 1.50
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
2 F3411007920200 1 PLATE
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
1 NAS1102-3-14 7 SCREW
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 22
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO
CML MAT. No.
QTY PER A/C SEE
NOTES
Solvent General Purpose 11-026 As required
References
Structural Repair Manual (SRM) 51-42-00
51-43-00
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
NOTE: The screw item (3) must not be removed to keep the AOA sensor in
position and to avoid removing it.
(a) Replace the conic plate by the flat plate of the AOA Sensor FIN 3FP1:
NOTE: Make sure that the previous plate installed on the aircraft is a conic
plate. Refer to aircraft maintenance records.
In accordance with SRM 51-42-00 and SRM 51-43-00
1 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
2 Remove the conic plate:
Refer to Fig. A-FBAAA Sheet 01
1 Plate F3411060200000 Item (2) Discard
or
1 Plate F3411060900000 Item (2) Discard
attached with:
7 Screw Item (1) Discard
3 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
4 Install the flat plate:
CAUTION: NEW AOA FLAT PLATE SHALL NOT BE PAINTED AND
SHALL REMAIN AS DELIVERED.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 23
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
NOTE: The attaching holes of the flat plates are delivered stripped
from protection at level of the surface of the bonding areas.
Refer to Fig. A-FBAAA Sheet 02
1 Plate F3411007920200 Item 2
attached with:
7 Screw NAS1102-3-14 Item 1
(2) Subtask 345093-831-002-001 - Replace the Conic Plates of the AOA Sensors FINs
3FP2 and 3FP3, on the RH Side.
Work Zones and Access Panels
Zone Access/Work location
122 Access Other access Access platform
Manpower Resources
Manhours 3.00
Minimum number of person 1
Subtask elapsed time 3.00
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
2 F3411007920300 2 PLATE
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
1 NAS1102-3-14 14 SCREW
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO
CML MAT. No.
QTY PER A/C SEE
NOTES
Solvent General Purpose 11-026 As required
References
Structural Repair Manual (SRM) 51-42-00
51-43-00
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 24
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
References
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
NOTE: The screw item (3) must not be removed to keep the AOA sensors in
position and to avoid removing them.
(a) Replace the conic plates by the flat plates of the AOA Sensors FINs 3FP2 and
3FP3:
NOTE: Make sure that the previous plate installed on the aircraft is a conic
plate. Refer to aircraft maintenance records.
In accordance with SRM 51-42-00 and SRM 51-43-00
1 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
2 Remove the conic plates:
Refer to Fig. A-FBAAA Sheet 01
2 Plate F3411060200000 Item (2) Discard
or
2 Plate F3411060900000 Item (2) Discard
attached with:
14 Srew Item (1) Discard
3 Use a non-metallic spatula to remove the sealant and clean the areas with:
Solvent General
Purpose
11-026 As required
4 Install the flat plates:
CAUTION: NEW AOA FLAT PLATES SHALL NOT BE PAINTED AND
SHALL REMAIN AS DELIVERED.
NOTE: The attaching holes of the flat plates are delivered stripped
from protection at level of the surface of the bonding areas.
Refer to Fig. A-FBAAA Sheet 02
2 Plate F3411007920300 Item 2
attached with:
14 Screw NAS1102-3-14 Item 1
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 25
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(3) Subtask 345093-831-003-002 - Replace the AOA Protection Covers in the Flight Kit
No 2 (FIN 7503NW).
Work Zones and Access Panels
Zone Access/Work location
130 Access Door 821
Manpower Resources
Manhours 0.50
Minimum number of person 1
Subtask elapsed time 0.50
Skills NON SPECIFIC
Material necessary to do the job
Component COMPA01
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
98F10001000000 3 AOAPRTCT
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
References
Fig. A-FBBAB
Modification of AOA Protection Covers in
the Flight Kit No 2
Sheet 01
NOTE: Depending on airline internal policy the Flight Kit No 2 may not be
located in the place defined by Fig. A-FBBAB Sheet 01. Refer to airline
internal policy for exact location for Flight Kit No 2 and/or its contents.
(a) Remove in the Flight Kit No 2 (FIN 7503NW):
Refer to Fig. A-FBBAB Sheet 01:
FIN 7955ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
FIN 7956ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
FIN 7957ME
1 AOA Sensor Protection
Cover
98D34203003000 Discard
(b) Install in the Flight Kit No 2 (FIN 7503NW):
Refer to Fig. A-FBBAB Sheet 01
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 26
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
FIN 7955ME
1 AOA Sensor Protection
Cover
98F10001000000
FIN 7956ME
1 AOA Sensor Protection
Cover
98F10001000000
FIN 7957ME
1 AOA Sensor Protection
Cover
98F10001000000
**CONF ALL
D. TEST
**CONF 001
(1) Subtask 345093-700-001-001 - Testing
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805
Task 20-28-00-869-801
(a) Test of electrical bonding at level of the 7 screws item 1:
1 Do a check of the electrical bonding, refer to AMM Task 20-28-00-720-805.
NOTE: For the Maximum Permitted Resistance Values, refer to AMM Task
20-28-00-869-801.
(b) Make sure that the bonding contact resistance between the sensor and
the fuselage structure is not higher than 5 milliohms as per AMM Task
20-28-00-720-805.
**CONF 002
(1) Subtask 345093-700-001-001 - Testing
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805
Task 20-28-00-869-801
(a) Test of electrical bonding at level of the 7 screws item 1:
1 Do a check of the electrical bonding, refer to AMM Task 20-28-00-720-805.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 27
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
NOTE: For the Maximum Permitted Resistance Values, refer to AMM Task
20-28-00-869-801.
(b) Make sure that the bonding contact resistance between the sensor and
the fuselage structure is not higher than 5 milliohms as per AMM Task
20-28-00-720-805.
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 345093-942-001-001 - Close-up
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
Release Agent 05-013 As required
Corrosion Inhibiting fillet
Consistency
09-016 As required
Fuel Tank Sealant Quick
Repair Permanent
09-058 As required
References
Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001
Task 20-28-00-912-802
Task 20-28-00-912-804
Task 52-30-00-410-803
52-41-00, Page Block 001
Elec. Std. Practices Manual (ESPM) 20-51-20
Structural Repair Manual (SRM) 51-24-00
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
(a) Protect the screws Item 1 in accordance with ESPM 20-51-20 and AMM Task
20-28-00-912-802 and/or AMM Task 20-28-00-912-804.
(b) Blank off the hole located in front of the screw item (3) in accordance with SRM
51-24-00 and as shown on Fig. A-FBAAA Sheet 02 with:
Release Agent 05-013 As required
Corrosion Inhibiting
fillet Consistency
09-016 As required
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 28
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
or
Fuel Tank Sealant
Quick Repair
Permanent
09-058 As required
(c) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(d) Close the Bulk cargo-compartment door 823, refer to AMM Task 52-30-00-410-803.
(e) Close the avionics compartment door 811, refer to AMM 06-41-53, Page Block 001
and AMM 52-41-00, Page Block 001.
(f) Remove the access platform(s).
(g) Restore the systems and the aircraft to normal operating condition.
**CONF 002
(1) Subtask 345093-942-001-002 - Close-up
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
Release Agent 05-013 As required
Corrosion Inhibiting fillet
Consistency
09-016 As required
Fuel Tank Sealant Quick
Repair Permanent
09-058 As required
References
Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001
Task 20-28-00-912-802
Task 20-28-00-912-804
Task 52-30-00-410-801
52-41-00, Page Block 001
Elec. Std. Practices Manual (ESPM) 20-51-20
Structural Repair Manual (SRM) 51-24-00
Fig. A-FBAAA
Modification of the Plates
Sheet 01
Sheet 02
(a) Protect the screws Item 1 in accordance with ESPM 20-51-20 and AMM Task
20-28-00-912-802 and/or AMM Task 20-28-00-912-804.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 29
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(b) Blank off the hole located in front of the screw item (3) in accordance with SRM
51-24-00 and as shown on Fig. A-FBAAA Sheet 02 with:
Release Agent 05-013 As required
Corrosion Inhibiting
fillet Consistency
09-016 As required
or
Fuel Tank Sealant
Quick Repair
Permanent
09-058 As required
(c) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(d) Close the FWD cargo-compartment door 821, refer to AMM Task
52-30-00-410-801.
(e) Close the avionics compartment door 811, refer to AMM 06-41-53, Page Block 001
and AMM 52-41-00, Page Block 001.
(f) Remove the access platform(s).
(g) Restore the systems and the aircraft to normal operating condition.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 30
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
**CONF ALL
BEFORE
FR19
FR18
3FP1
3FP2
3FP3
A B
A B
A B
A
(7 POS) (1) (7 POS) (1)
OR
(2) (2)
(3) (3)
NOTE:
TYPICAL ILLUSTRATION ASSOCIATED WITH THALES OR GOODRICH AOA SENSORS.
THALES GOODRICH
F_SB_345093_5_BAAA_01_01
Figure A-FBAAA - Sheet 01
Modification of the Plates
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 31
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
**CONF ALL
AFTER
1
2
(7 POS)
(3)
NOTE:
ONLY ONE CONFIGURATION SHOWN, AOA SENSOR
01 BLANK OFF THE HOLE LOCATED IN FRONT OF THE SCREW ITEM WITH:
MAT. No. 05−013 AND MAT. No. 09−058 OR 09−016.
(3)
DEPENDS ON AIRCRAFT CONFIGURATION.
01
B
ELECTRICAL BONDING
F_SB_345093_5_BAAA_02_03
Figure A-FBAAA - Sheet 02
Modification of the Plates
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 32
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
**CONF 001
B
FR69
FR73
A
A
Z160
B
7500NW
FLIGHT KIT No 2
NOTE:
ARE STORED IN FLIGHT KIT No 2 FIN (7500NW)
AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME)
F_SB_345093_5_BBAA_01_02
Figure A-FBBAA - Sheet 01
Modification of AOA Protection Covers in the Flight Kit No 2
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 33
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
**CONF 002
A
A
Z130
FR20
FR25
FR26
B
FLIGHT KIT No 2
NOTE:
ARE STORED IN FLIGHT KIT No 2 FIN (7503NW)
AOA PROTECTION COVERS FINs (7955ME, 7956ME AND 7957ME)
B
7503NW
F_SB_345093_5_BBAB_01_02
Figure A-FBBAB - Sheet 01
Modification of AOA Protection Covers in the Flight Kit No 2
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 34
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
APPENDIX 01: Elapsed Time Assumption
**CONF ALL
(1) The following Gantt chart is only a proposal operators may determine that another way to do the
work is more suitable for them.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
APPENDIX 01: Elapsed Time Assumption
**CONF ALL
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A340−34−5093
GET ACCESS
MH ET/S
TOTAL MANHOURS
SB ELAPSED TIME
6.25
4.25
STEPS
0.50 0.50
0 5
1.50 1.50
3.00 3.00
TEST 0.25 0.25
CLOSE−UP 0.50 0.50
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.
01
02
NOTE:
PER
1
1
1
1
1
REPLACEMENT OF AOA PROTECTION 0.50 1 0.50
: :
SB ELAPSED TIME
(HOURS)
1 2 3 4
IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ARE NOT REFLECTED IN THIS GANTT CHART.
COVERS IN THE FLIGHT KIT No 2
REPLACEMENT OF THE PLATE OF
THE AOA SENSOR FIN 3FP1, RH SIDE
REPLACEMENT OF THE PLATE OF
THE AOA SENSOR FINs 3FP2 AND
3FP3, LH SIDE
F_SB_345093_5_AAAA_01_01
Figure A-FAAAA - Sheet 01
Gantt Chart
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 2
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
REPORTING SHEET
TITLE: NAVIGATION - GENERAL - REPLACE AOA PROBE CONIC PLATE BY
AOA PROBE FLAT PLATE
MODIFICATION No.: 203295S32646
Please complete the appropriate item (A or B):
A - SB WILL BE embodied YES/NO (if NO please comment)
If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of
embodiment:
B - SB HAS BEEN embodied on aircraft:
Operator comments:
From Airline:
Name/Title:
Signature: Date:
If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to
next normal revision or prior to SB embodiment, please indicate required service(s):
Either: Modification Operational Impact (MOI), if available YES/NO
Or : Intermediate revision YES/NO
Important Information: This SB will only be incorporated in your maintenance and operational
documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With
the next feasible revision, this will result in
- Updating of maintenance documentation to show pre and post SB data.
- Updating of maintenance and operational documentation to show post SB data after embodiment.
If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically
include them in the manual revisions. Refer to SIL 00-037 for detailed information.
Please return this completed sheet to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn: SDC32 Technical Data and Documentation Services
FAX: (+33) 5 61 93 28 06
e-mail: sb.reporting@airbus.com
or via your Resident Customer Support Office.
Alternatively, SB lists via letters or fax are also accepted.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
QUALITY PERCEPTION FORM
Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data
that you provide us will be used to analyse areas of difficulties and to take corrective action to further
improve the quality of our Service Bulletins.
We thank you for the time you have taken in completing this form.
(Please rate on a scale of 1 to 4, with 4 being the highest score)
- Quality rating of this SB 4 3 2 1
- Quality rating of the Accomplishment Instructions 4 3 2 1
- Quality rating of the Illustrations 4 3 2 1
- Is this SB easy to understand ? Y / N
If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a
short description of the issue.
Planning Material Instructions
X Effectivity X Kit content X Preparation
X Reason X List of Materials Operator Supplied X Mod/Inspection
X Manpower X Industry support X Test
X References X Re-identification X Close-Up
X Publication X Tooling X Illustrations
Comments:
Operator: Date:
Name/Title:
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management
FAX : (33) 5 61 93 42 51
Or via your Resident Customer Support Office.
DATE: Jan 30/13 SERVICE BULLETIN No.: A340-34-5093
REVISION No.: 00 - Jan 30/13 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.