On this page
ADs that cite it · 2
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
Also cited in 1 proposed AD.
Text · 28
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2015-4810; AD 2016-07-30 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '423b057aa8857f0088767459a5c7f934e17dbf844b8b13a2cafc1027606e2c2e' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '423b057aa8857f0088767459a5c7f934e17dbf844b8b13a2cafc1027606e2c2e' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
@A340-500/600
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft.
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 34 TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED
CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND
UTAS ON STANDBY **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR 204937S33428 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 aim of this modification is to allow the airlines to fly in a mixed Angle of Attack (AOA) configuration.
This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1 and 3FP2) PN 0861ED (installed by Mod. No. 46921S14694) or PN 0861ED2 (installed by Mod. No. 204294S33100 or Service Bulletin No. A340-34-5102) by two THALES AoA probes PN C16291AB.
The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA configurations.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY (1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
LROPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED NO NOTE
(1) : Service Bulletin must be accomplished.
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY
MATERIAL PRICE INFORMATION **CONF 001
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Equipment BFEA01 1 See SB AOA Probes **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Equipment BFEA02 1 See SB AOA Probes
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
16R 25R 31V 32P 81Q AIB CES HFM I2L MHK THA VIR
CONCURRENT REQUIREMENTS **CONF 001 None **CONF 002 None
REFERENCES / REPERCUSSIONS **CONF ALL TFU None OEB None AOT None SIL None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER Operator Information Transmission (OIT) No. 999.0017/15
NATURE OF THE WORK
AIRCRAFT NO
EQUIPMENT YES HARD NO DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY SOFT NO OBRM NO
MANPOWER **CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft
TOTAL MANHOURS
4.50
ELAPSED TIME (HOURS)
3.50 **CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft
TOTAL MANHOURS
4.50
ELAPSED TIME (HOURS)
3.50
APPENDICES **CONF ALL Appendix 01 - Elapsed Time Assumptions DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
SUMMARY **CONF ALL FR1 FR20 Z120 A FR19 FR18 A 3FP2 3FP1 A
TYPICAL INSTALLATION F_SB_345105_5_SAAA_01_00 Figure A-FSAAA - Sheet 01 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 4 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 T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
MANDATORY
MANDATORY
MANDATORY ATA SYSTEM: 34 TITLE: NAVIGATION - AOA - INSTALL AOA PROBES IN MIXED
CONFIGURATION - THALES FOR CAPT AND FIRST OFFICER AND
UTAS ON STANDBY MODIFICATION No.: 204937S33428 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 equipped with UTAS AOA PN 0861ED or PN 0861ED2.
NOTE : This Service Bulletin is only applicable to aircraft on which Mod. No.
46921S14694 (INSTALL ANGLE OF ATTACK SENSORS ROSEMOUNT) is embodied.
(1) Models 340-541 340-642
(2) Effectivity by MSN 0371 0376 0383 0391 0416 0436 0449 0453 0468 0475 0478 0488 0492 0499 0514 0560 0563 0575 0577 0586 0615 0622 0624 0628 0639 0677 0681 0689 0698 0706 0710 0719 0723 0736 0753 0764-0765 0768 0775 0787 0804 0924 0953 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN
(3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason.
OPERATOR MSN 16R 0615 0622 25R 0924 31V 0436 32P 0560 81Q 0563 AIB 0478 0492 0499 CES 0468 0488 0514 0577 0586 HFM 0391 I2L 0453 0475 MHK 0371 0376 0383 0416 0449 THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953 VIR 0575 0639 0706 0723 0736 0753 0764 0765 0768 0787 0804
(4) Configuration by MSN MSN
CONFIGURATION 0371 0376 0383 0391 0416 0436 0449 0453 0468 0475 0478 0488 0492 0499 0514 0560 0563 0575 0577 0586 0615 0622 0624 0628 0639 0677 0681 0689 0698 0706 0710 0719 0723 0736 0753 0764 0765 0768 0775 0787 0804 0924 0953 001 002
(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No.
A340-34-5102) is not embodied.
**CONF 002 Config. 002 is valid for aircraft on which Mod. No. 204294S33100 (Service Bulletin No.
A340-34-5102) is embodied.
(6) Material Effectivity **CONF 001
MATERIAL
QTY PER A/C
SEE NOTES Equipment BFEA01 1 **CONF 002
MATERIAL
QTY PER A/C
SEE NOTES Equipment BFEA02 1 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN **CONF ALL B. CONCURRENT REQUIREMENTS **CONF 001 None **CONF 002 None **CONF ALL C. REASON
(1) History The aim of this modification is to allow the airlines to fly in a mixed Angle of Attack (AOA) configuration.
(2) Objective/Action This Service Bulletin requires the replacement of two UTAS AoA probes (FINs 3FP1 and 3FP2) PN 0861ED (installed by Mod. No. 46921S14694) or PN 0861ED2 (installed by Mod. No. 204294S33100 or Service Bulletin No. A340-34-5102) by two THALES AoA probes PN C16291AB.
(3) Advantages The accomplishment of this Service Bulletin will allow the airlines to fly in mixed AoA configurations.
(4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to :
**CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft
(1) Replace the AOA Probe 1 (FIN 3FP1)
(2) Replace the AOA Probe 2 (FIN 3FP2) **CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN and 3FP2) on Aircraft
(1) Replace the AOA Probe 1 (FIN 3FP1)
(2) Replace the AOA Probe 2 (FIN 3FP2) **CONF ALL E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. It is anticipated that this Service Bulletin must be done before Mar 31/17, the AD will confirm it 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 Organization Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.
G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included.
**CONF 001 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft Get Access
1.00 On Aircraft Replace the AOA Probe 1 (FIN 3FP1)
1.00 Replace the AOA Probe 2 (FIN 3FP2)
1.00 Tests
0.50 Close-Up
1.00
TOTAL MANHOURS
4.50 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft
ELAPSED TIME (HOURS)
3.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions .
**CONF 002 Task 345105-831-801-001: Modification by Replacement of the two AOA Probes (FINs 3FP1 and 3FP2) on Aircraft Get Access
1.00 On Aircraft Replace the AOA Probe 1 (FIN 3FP1)
1.00 Replace the AOA Probe 2 (FIN 3FP2)
1.00 Tests
0.50 Close-Up
1.00
TOTAL MANHOURS
4.50
ELAPSED TIME (HOURS)
3.50 NOTE : For an explanation of the manhours and elapsed time, refer to the Gantt Chart, Fig. A-FAAAA given in Appendix 01 - Elapsed Time Assumptions .
**CONF ALL H. WEIGHT AND BALANCE Not Changed 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 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 **CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53 12-34-24 34-11-19 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN **CONF ALL K. PUBLICATION AFFECTED Aircraft Wiring List (AWL) Illustrated Parts Catalog (IPC) 34-11-01 34-11-19 L. INTERCHANGEABILITY/MIXABILITY The interchangeability/mixability possibilities are for new or modified parts introduced by the accomplishment of this Service Bulletin.
**CONF 001
DESCRIPTION OLD PART N˚ NEW PART N˚ INT
MIXABILITY SEE NOTES AOA Probe 0861ED C16291AB 03 NO
(1) 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.
NOTE
(1) : When AOA PN 0861ED is removed, it may be replaced:
- with the AOA PN 0861ED,
- with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and 3FP2) are replaced simultaneously.
When the new PN is removed, it must be replaced by the new PN.
**CONF 002
DESCRIPTION OLD PART N˚ NEW PART N˚ INT
MIXABILITY SEE NOTES AOA Probe 0861ED2 C16291AB 03 NO
(1) 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.
NOTE
(1) : When AOA PN 0861ED2 is removed, it may be replaced:
- with the AOA PN 0861ED2,
- with the AOA PN C16291AB only if both AOA probes (FINs 3FP1 and 3FP2) are replaced simultaneously.
When the new PN is removed, it must be replaced by the new PN.
DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN **CONF ALL M. SPARES AOA Probe 0861ED AOA Probe 0861ED2 DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600
SERVICE BULLETIN This Page Intentionally Left Blank DATE: Mar 26/15 SERVICE BULLETIN No.: A340-34-5105 REVISION No.: 00 - Mar 26/15 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.