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1 2015 TAES TECHNICAL PUBLICATION Issued: January 2015 ATR THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION ATR 42/72 - 2015 THALES - CUSTOMER SUPPORT DEPARTMENT 41 boulevard de la République B. P. n° 53 78401 CHATOU CEDEX France Tel : 33 1 34.80.73.46 Fax : 33 1 34.80.75.95 E-Mail : [email protected]

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Page 1: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

1

2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

THALES AVIONICS ELECTRICAL SYSTEMS

TECHNICAL PUBLICATION

ATR 42/72

- 2015 –

THALES

- CUSTOMER SUPPORT DEPARTMENT – 41 boulevard de la République – B. P. n° 53 – 78401 CHATOU CEDEX – France

Tel : 33 1 34.80.73.46 Fax : 33 1 34.80.75.95 E-Mail : [email protected]

Page 2: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

APPLICABLE TECHNICAL PUBLICATION

1. General conditions

2. List of LRU’s

3. Details of evolutions

4. Statement of agreement

Page 3: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

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ATR

1. GENERAL CONDITIONS CMM : Component Maintenance Manual. TCMS : Technical Characteristics Maintenance Sheet. SB : Service Bulletin SIL : Service Information Letter E/R : Electronic/Rotable Technical Publications (CMM/SB/SIL) are available. To obtain the sale conditions, contact your Commercial Contact. Prior to the delivery of a CMM, the customer shall sign a Statement of Agreement.

2. LIST OF LRU’S

THALES vendor code

TAES P/N DESCRIPTION E/R Qty per plane

Applicability

F0296 156 Transformer E 2 All ATR

F0296 102-003-11 DC Generator Control Unit E 2 All ATR

F0296 103-003-2 (-11) Hall Effect Current Sensor (HECS) E 5 All ATR

F0296 105-003-2

105-003-1 DC Bus Power Control Unit E 1 All ATR

F0296 20032-2 Alternator R 2 All ATR

F0296 20732 Transformer (DPCT) E 3 All ATR

F0296 2432-11

2432-30 AC Generator Control Unit E 2 All ATR

F0296 559-012A 559-012B

559-012C 559-012D Static Inverter E 2 All ATR

F0296 680-0040-000 Emergency axe - 1 All ATR

F0296 8260-123

8260-121 DC Starter Generator R 2 All ATR

F0296 945-12

945-11 AC Bus Power Control Unit E 1 All ATR

F0296 F11NA3121 Transformer Rectifier Unit E 1 -500 and

ETOPS only

F0296 F46BC0101

F46BD0101 Control Box E 1 All ATR

F0296 F96GA0102

F96GA0101 Landing Gear Control Lever E 1 All ATR

F0296 B3893-000 DC-STAR GSE – Direct Current

System Tester Analyzer Recorder Ground Support Equipment

E / All ATR

Page 4: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

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3. DETAILS OF EVOLUTIONS

STARTER-GENERATOR P/N 8260-121

CMM reference : 24-32-61 Revision 10 : Date of update February, 09th 2012

Evolution Reason Application In

Production since

SB SIL

/ Brush and bearing

replacement

Mandatory during brush and bearing replacement

/ / SIL8260-120-005

Rev. 7 dated 03/09/2009

/ Best practice on Starter Generator

Operation, Maintenance,

storage, transportation,

handling.

/ / SIL8260-12X-24-007

Rev. 2 dated 27/03/2013

/ Recommended scheduled maintenance

/ / / SIL8260-12X-24-009

Rev. 3 dated 06/04/2006

/

Brush check procedure with S/G fitted on engine.

/ / / SIL8260-12X-24-010

Rev. 1 dated 09/09/2009

/ Brush replacement procedure

Mandatory during brush replacement

/ / SIL8260-12X-24-011

Rev. 2 dated 10/07/2009

/ Speed sensor tightening procedure.

During each speed sensor assembling operation

/ / SIL8260-12X-24-012

Rev. 1 dated 13/11/2009

/

Brush and bearing replacement without disassembly of the S/G.

Mandatory during brush and bearing replacement

/ / SIL8260-12X-24-013

dated 05/06/2009

/ Packaging for Starter Generator

Recommended for shipment

/ / SIL8260-12X-24-014

dated 09/07/2009

/ Armature information

Recommended / / SIL8260-12X-24-015

dated 09/11/2011

/ Checking of the torque shaft

Recommended / / SIL8260-12X-24-016

dated 10/12/2012

Page 5: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

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ATR

Evolution Reason Application In

Production since

SB SIL

/ Brushes replacement

Recommended / / SIL8260-12X-24-017

dated 10/09/2013

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/ Second source of Anti-flash varnish

Recommended / / SIL24-99-003

dated 05/09/2012

/ Second source of primer and paint

Recommended / / SIL24-99-004

Rev. 1 dated 19/06/2014

Amendment A, B & C

/ Do not exist for

this unit / / /

Amendment D Improvement of reliability

Recommended under repair

1989 SB8260-120-24-007

dated 03/08/1992 /

Amendment E Improvement of reliability

During repair if component has to be replaced & Recommended during overhaul.

1990 SB8260-120-24-006

dated 10/12/1990 /

Amendment F Improvement of reliability

During repair if component has to be replaced

1991 SB8260-120-24-005

Rev. 1 dated 12/04/1991

/

Amendment G Improvement of reliability

During repair if component has to be replaced

1994 / /

Amendment H Improvement of reliability

During repair if component has to be replaced

1998 SB8260-12X-24-008

Rev. 1 dated 21/12/1998

/

Amendment J Improvement of reliability

During repair if component has to be replaced

1998 SB8260-12X-24-009

Rev. 1 dated 21/12/1998

/

Amendment K Improvement of reliability

During overhaul 1998 SB8260-12X-24-010

dated 28/10/1997 /

8260-123 Improvement of scheduled maintenance

On customer request

2000 SB8260-12X-24-011

dated 21/12/1998 /

Amendment M Conformity Mandatory

during overhaul 2000

SB8260-12X-24-012 Rev. 1

dated 09/08/1999 /

Page 6: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

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ATR

Evolution Reason Application In

Production since

SB SIL

Amendment N Improvement of reliability

During repair if component has to be replaced

2003 SB8260-12X-24-013

dated 17/12/2002 /

/ Overhaul procedure

Mandatory during overhaul

/ SB8260-12X-24-014

Rev. 1 dated 07/04/2004

/

Amendment P Component obsolescence

During repair if component has to be replaced

Only under repair since 2006

SB8260-12X-24-016 dated 17/12/2004

/

Amendment R Improvement of reliability

During repair if component has to be replaced

2012 SB8260-12X-24-017

dated 12/11/2012

STARTER-GENERATOR P/N 8260-123

CMM reference : 24-32-61 Revision 10 : Date of update February, 09th 2012

Evolution Reason Application In

Production since

SB SIL

/ Brush and bearing replacement

Mandatory during brush and bearing replacement

/ / SIL8260-120-005

Rev. 7 dated 03/09/2009

/ Best practice on Starter Generator

Operation, Maintenance,

storage, transportation,

handling.

/ / SIL8260-12X-24-007

Rev. 2 dated 27/03/2013

/ Recommended scheduled maintenance

/ / / SIL8260-12X-24-009

Rev. 3 dated 06/04/2006

/

Brush check procedure with S/G fitted on engine.

/ / / SIL8260-12X-24-010

Rev.1 dated 09/09/2009

Page 7: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

Evolution Reason Application In

Production since

SB SIL

/ Brush replacement procedure

Mandatory during brush replacement

/ / SIL8260-12X-24-011

Rev. 2 dated 10/07/2009

/ Speed sensor tightening procedure.

During each speed sensor assembling operation

/ / SIL8260-12X-24-012

Rev. 1 dated 13/11/2009

/

Brush and bearing replacement without disassembly of the S/G.

Mandatory during brush and bearing replacement

/ / SIL8260-12X-24-013

dated 05/06/2009

/ Packaging for Starter Generator

Recommended for shipment

/ / SIL8260-12X-24-014

dated 09/07/2009

/ Armature information

Recommended / / SIL8260-12X-24-015

dated 09/11/2011

/ Checking of the torque shaft

Recommended / / SIL8260-12X-24-016

dated 10/12/2012

/ Brushes replacement

Recommended / / SIL8260-12X-24-017

dated 10/09/2013

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/ Second source of Anti-flash varnish

Recommended / / SIL24-99-003

dated 05/09/2012

/ Second source of primer and paint

Recommended / / SIL24-99-004

Rev. 1 dated 19/06/2014

Amendment A Improvement of reliability

During repair if component has to be replaced

2000 SB8260-12X-24-008

Rev. 1 dated 21/12/1998

/

Amendment B Improvement of reliability

During repair if component has to be replaced

2000 SB8260-12X-24-009

Rev. 1 dated 21/12/1998

/

Amendment D Conformity Mandatory

during overhaul 2000

SB8260-12X-24-012 Rev. 1

dated 09/08/1999 /

Page 8: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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ATR

Evolution Reason Application In

Production since

SB SIL

Amendment E Improvement of reliability

During repair if component has to be replaced

2003 SB8260-12X-24-013

dated 17/12/2002 /

/ Overhaul procedure

Mandatory during overhaul

/ SB8260-12X-24-014

Rev. 1 dated 07/04/2004

/

Amendment F Component obsolescence

During repair if component has to be replaced

2006 SB8260-12X-24-016

dated 17/12/2004 /

Amendment G Improvement of reliability

During repair if component has to be replaced

2012 SB8260-12X-24-017

dated 12/11/2012

AC GENERATOR P/N 20032-2

CMM reference : 24-22-61 Revision 4 : Date of update May, 30th 2008

Evolution Reason Application In

Production since

SB SIL

/ Verification of measurement

Under repair / / SIL20032-X-24-003

dated 06/1993

/ Verification of torque value

On aircraft Under repair

/ / SIL20032-2-24-007 dated 28/09/2004

/ Improvement of reliability

Under repair (overhaul or

bearing replacement)

/ / SIL20032-2-24-008 dated 24/03/2005

/ Best practice on AC Generator

Operation, Maintenance,

storage, transportation,

handling.

/ / SIL20032-2-24-010 dated 27/03/2013

Page 9: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

Amendment A Component obsolescence

During repair if component has to be replaced

1988 SB20032-2-24-002 dated 15/02/1992

/

Amendment B Improvement of reliability

During repair of rotating diodes

bridges. 1988 / /

Amendment C Improvement of repair procedure

Under repair only if rewinding

of stator is necessary

Only under repair since 1997

/ /

Amendment D Improvement of reliability

On customer request

or if component

has to be replaced

(P058137)

1998 / /

Amendment E Improvement of reliability

Recommended / On customer

request or if component

has to be replaced

(P058137 or P058137A)

1999 SB20032-2-24-009

Rev. 1 dated 03/04/2008

/

Amendment F Improvement of reliability

During repair if component has to be replaced

1999 SB20032-2-24-005 dated 21/12/1998

/

Amendment G Improvement of reliability

During repair if component has to be replaced

1999 SB20032-2-24-006 dated 21/12/1998

/

Amendment H

Improvement of reliability & assembly procedure.

During repair if component has to be replaced

2004 SB20032-2-24-007 dated 04/12/2002

/

Amendment J

Improvement of reliability & assembly procedure. Qualification of a new source.

During repair if component has to be replaced (Diode-holder plate assy.)

2007 SB20032-2-24-008

Rev. 1 dated 03/04/2008

SIL20032-2-24-009 Rev. 1

dated 31/03/2008

Amendment K Improvement of reliability

During repair if component has to be replaced

2012 SB20032-2-24-010

Rev. 1 dated 12/11/2014

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AC GCU P/N 2432-11

CMM reference : 24-22-14 Revision 4 : Date of update September, 30th 1999

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability

Mandatory during repair by

OEM only 1988

SB2432-11-24-002 dated 15/02/1992

/

Amendment B Improvement of reliability

Mandatory during repair by

OEM only 1988

SB2432-11-24-003 dated 15/02/1992

/

Amendment C Improvement of reliability

Mandatory during repair

1989 / /

Amendment D Component obsolescence

During repair if PCB or

component has to be replaced

Systematically during repair if

PCB Z500 must be replaced

Only under repair since 1998

SB2432-30-24-001 dated 25/04/2006

/

Amendment E Improvement of reliability

During repair if PCB or

component has to be replaced

Only under repair since 1998

SB2432-30-24-002 Dated 07/12/2009

SIL2432-11-24-001 dated 15/11/2006

2432-30

Modification for ATR72-210 version (new propeller).

On customer request

1994 SB2432-30-24-001

dated 10/1993 /

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AC GCU P/N 2432-30

CMM reference : 24-22-14 Revision 4 : Date of update September, 30th 1999

Evolution Reason Application In

Production since

SB SIL

/ Mechanical check of the rear guide bushing.

Under repair / / SIL2432-30-24-001 dated 21/06/2007

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Component obsolescence

During repair if PCB or

component has to be replaced

Systematically during repair if

PCB Z500 must be replaced

1999 SB2432-30-24-001 dated 25/04/2006

/

Amendment B Improvement of reliability

During repair if PCB or

component has to be replaced

1999 SB2432-30-24-002 dated 07/12/2009

/

DC GCU P/N 102-003-11

CMM reference : 24-32-11 Revision 2 : Date of update July, 5th 2006

Evolution Reason Application In

Production since

SB SIL

/ Mechanical check of the rear guide bushing.

Under repair / / SIL102-003-11-24-

002 dated 21/06/2007

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2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability

Mandatory during repair.

1988 SB102-003-11-24-

001 dated 15/02/1992

/

Amendment B Improvement of reliability

Recommended during repair.

1988 SB102-003-11-24-

002 dated 15/02/1992

/

Amendment C Improvement of reliability

Mandatory during repair.

1988 SB102-003-11-24-

004 dated 15/02/1992

/

Amendment D Improvement of reliability

Mandatory during repair.

2001 SB102-003-11-24-

005 dated 22/12/1999

/

Amendment E Improvement of reliability

Mandatory during repair.

2004

SB102-003-11-24-006

Rev. 2 dated 08/11/2012

/

Amendment F Improvement of reliability

On customer request or if

PCB has to be repaired.

2005 SB102-003-11-24-

007 dated 27/01/2005

/

Amendment G Component obsolescence

During repair if selector switch or PCB has to be replaced

2006 SB102-003-11-24-

008 dated 25/04/2006

/

Amendment H Improvement of reliability

Recommended 2013 SB102-003-11-24-

009 dated 05/07/2013

/

AC BPCU GCU P/N 945-11

CMM reference : 24-41-13 Revision 3 : Date of update June, 15th 1999

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

Page 13: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

Evolution Reason Application In

Production since

SB SIL

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability

Mandatory during repair.

1989 SB945-11-24-002

ated 02/1992 /

945-12 Improvement of reliability

On customer request.

1997 SB945-11-24-003 dated 30/06/1996

/

AC BPCU GCU P/N 945-12

CMM reference : 24-41-13 Revision 3 : Date of update June, 15th 1999

Evolution Reason Application In

Production since

SB SIL

/ Mechanical check of the rear guide bushing.

/ / / SIL945-12-24-001 dated 21/06/2007

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Page 14: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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DC BPCU P/N 105-003-1

CMM reference : 24-76-13 Revision 3 : Date of update August, 8th 2006

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability

Mandatory during repair.

1994 SB105-003-24-003

dated 02/1992 /

Amendment B Improvement of reliability

Mandatory during repair.

1994 SB105-003-24-004

dated 02/1992 /

Amendment C Improvement of manufacturing process

During repair if component has to be replaced

1994 SB105-003-24-005

dated 02/1992 /

Amendment D Improvement of reliability

Mandatory during repair.

1994 SB105-003-24-006

dated 02/1992 /

Amendment E Improvement of reliability

Mandatory during repair.

1994 SB105-003-24-007

dated 02/1992 /

Amendment F Improvement of reliability

Mandatory during repair.

1994 SB105-003-24-001

dated 09/1990 /

Amendment G Improvement of reliability

Mandatory during repair.

Only under repair since 1993

/ /

Amendment H Improvement of reliability

During repair if PCB or

component has to be replaced

Only under repair since 1998

SB105-003-24-008 dated 21/12/1998

/

Amendment J Improvement of reliability

During repair if PCB has to be

replaced.

Only under repair since 1998

/ /

Amendment K Improvement of reliability

During repair if PCB or

component has to be replaced

Only under repair since 1999

SB105-003-24-009 dated 21/12/1998

/

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Evolution Reason Application In

Production since

SB SIL

Amendment L Improvement of reliability

During repair if PCB or

component has to be replaced

Only under repair since 1999

/ /

Amendment M Component obsolescence

During repair if PCB or

component has to be replaced

Only under repair since 2001

/ /

Amendment N Improvement of reliability

Mandatory during repair.

Only under repair since 2003

SB105-003-24-011 dated 12/01/2004

/

Amendment P Component obsolescence

During repair if PCB or

component has to be replaced

Only under repair since 2004

SB105-003-24-012 dated 25/04/2006

/

105-003-2 Improvement of reliability

On customer request.

1990 SB105-003-24-002

dated 02/1992 /

DC BPCU P/N 105-003-2

CMM reference : 24-76-13 Revision 3 : Date of update August, 8th 2006

Evolution Reason Application In

Production since

SB SIL

/ Mechanical check of the rear guide

bushing. / / /

SIL105-003-2-24-001 dated 26/06/2007

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Page 16: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

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Evolution Reason Application In

Production since

SB SIL

Amendment G Improvement of reliability

On customer request.

1994 / /

Amendment H Improvement of reliability

Mandatory during repair.

1994 / /

Amendment J Improvement of reliability

During repair if PCB or

component has to be replaced

1999 SB105-003-24-008 dated 21/12/1998

/

Amendment K Improvement of reliability

During repair if PCB has to be

replaced. 1999 / /

Amendment L Improvement of reliability

During repair if PCB or

component has to be replaced

2000 SB105-003-24-009 dated 21/12/1998

/

Amendment M Improvement of reliability

During repair if PCB or

component has to be replaced

2000 / /

Amendment N Component obsolescence

During repair if PCB or

component has to be replaced

2002 / /

Amendment P Component obsolescence

During repair if PCB or

component has to be replaced

2003 SB105-003-24-010 dated 12/01/2004

/

Amendment R Improvement of reliability

Mandatory during repair.

2004 SB105-003-24-011 dated 12/01/2004

/

Amendment S Component obsolescence

During repair if PCB or

component has to be replaced

2005 SB105-003-24-012 dated 25/04/2006

/

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STATIC INVERTER P/N 559-012A

CMM reference : 24-21-11 Revision 3 : Date of update January, 15th 2015

Evolution Reason Application In

Production since

SB SIL

/ Checking of over-voltage threshold protection

Under repair / / SIL 559-012B-24-001

dated 15/06/2006

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability

Mandatory during repair

1995 / /

Amendment B

Improvement of the control of "Static Inverter fault" signal

Mandatory during repair

1995 / /

Amendment C

Improvement of reliability of auxiliary power card

Mandatory during repair

Only under repair since 1997

SB559-012A-80-001 dated 15/12/1997

/

Amendment D Component obsolescence

During repair if PCB or

component has to be replaced

Only under repair since 2004

/ /

559-012C

Improvement of reliability in order to avoid double loss of static inverter

Mandatory during repair

Only under repair since 2009

SB559-012AB-24-002

Rev. 1 dated 25/01/2011

/

STATIC INVERTER P/N 559-012B

CMM reference : 24-21-11 Revision 3 : Date of update January, 15th 2015

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

Page 18: THALES AVIONICS ELECTRICAL SYSTEMS TECHNICAL PUBLICATION · PDF file1 2015 taes – technical publication issued: january 2015 atr thales avionics electrical systems technical publication

18

2015 TAES – TECHNICAL PUBLICATION

Issued: January 2015

ATR

Evolution Reason Application In

Production since

SB SIL

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A

Improvement of reliability of auxiliary power card

Mandatory during repair

Only under repair since 1997

SB559-012A-80-001 dated 01/12/1997

Amendment B Component obsolescence

During repair if PCB or

component has to be replaced

2005 / /

559-012D

Improvement of reliability in order to avoid double loss of static inverter

Mandatory during repair

2008

SB559-012AB-24-002

Rev. 1 dated 25/01/2011

/

STATIC INVERTER P/N 559-012C

CMM reference : 24-21-11 Revision 3 : Date of update January, 15th 2015

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

STATIC INVERTER P/N 559-012D

CMM reference : 24-21-11 Revision 3 : Date of update January, 15th 2015

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

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Evolution Reason Application In

Production since

SB SIL

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

TRU P/N F11NA3121

CMM reference : 24-32-13 Revision / : Date of update October, 15th 1996

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

LIGHTING TRANSFORMER P/N 156

Technical Characteristics & Maintenance Sheet reference : 30-31-13 Revision 3 : Date of update April, 2010

Evolution Reason Application In

Production since

SB SIL

/ / / / / /

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CONTROL BOX P/N F46BC0101

CMM reference : 26-15-24 Revision 1 : Date of update December, 01st 1993

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability and functionning.

Mandatory under repair.

1987 / /

Amendment B Improvement of manufacturing & repair processes.

During repair if necessary.

2009 SBF46BC0101-24-

001 dated 29/08/2012

/

/ Inspection of the fan control box

Unit in operation

2012 SBF46BC0101-24-

002 dated 31/08/2012

Amendment C Improvement of reliability

During repair if necessary.

2012 SBF46BC0101-24-

004 dated 25/09/2014

/

Amendment D Improvement of reliability

During repair if necessary.

2012 SBF46BC0101-24-

003 dated 25/02/2014

/

CONTROL BOX P/N F46BD0101

CMM reference : 26-15-25 Revision / : Date of update June, 15th 2001

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/

Electrostatic Discharge Sensitive Components

Recommended / / SIL24-99-002

dated 09/12/2010

Amendment A Improvement of reliability.

Only under production.

1996 / /

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LANDING GEAR CONTROL LEVEL P/N F96GA0101

CMM reference : 32-31-11 Revision 2 : Date of update January, 26th 2009

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

LANDING GEAR CONTROL LEVEL P/N F96GA0102

CMM reference : 32-31-11 Revision 2 : Date of update January, 26th 2009

Evolution Reason Application In

Production since

SB SIL

/ Order consumables products

Recommended / / SIL24-99-001

dated 03/01/2011

/ Screw replacement

Recommended / / SILF96GA0102-32-

001 Rev. 1 dated 21/10/2014

Amendment A Improvement of

functionning Mandatory

during repair. 1987 / /

Amendment B Improvement of

reliability On customer

request. 1989 / /

Amendment C Improvement of

reliability On customer

request. 1998

SBF96GA0102-24-001

dated 21/12/1998 /

Amendment D Improvement of

functionning

During repair if component has to be replaced.

2001 / /

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TRANSFORMER (DPCT) P/N 20732

(DPCT : Differential Protection Current Transformer)

Technical Characteristics & Maintenance Sheet reference : 24-22-11 Revision 2 : Date of update June, 1993

Evolution Reason Application In

Production since

SB SIL

/ / / / / /

HALL EFFECT CAPTOR SENSOR P/N 103-003-2

Technical Characteristics & Maintenance Sheet reference : 24-32-12 Revision 4 : Date of update April, 2006

Evolution Reason Application In

Production since

SB SIL

Amendment A Improvement of reliability

Only under production

1998 / /

Amendment B Improvement of reliability

Only under production

2003 / /

Amendment C Improvement of reliability

Only under production

2005 / /

Amendment D Obsolescence of the potting resin

Only under production

2010 / /

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EMERGENCY AXE P/N 680-0040-000

Technical Characteristics & Maintenance Sheet reference : 25-65-01 Revision 1 : Date of update 1992

Evolution Reason Application In

Production since

SB SIL

/ Packaging for Emergency axe

Recommended for shipment

/ / SIL680-0040-000-25-

001 dated 26/10/2009

DC-STAR GSE P/N B3893-000

USER MANUAL : Y28-0617

Revision a : Date of update October, 17rd 2008

Evolution Reason Application In

Production since

SB SIL

/ / / / / /

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4. STATEMENT OF AGREEMENT

Statement of Agreement to Terms and Conditions of Sale of Thales Technical Publications Thales Component Maintenance Manual 24-XX-XX is intended solely for use by Company Name. Copying, reproducing or redistribution of this or any Thales Component Maintenance Manual (CMM) or Service Bulletin (SB), to any other party or location is strictly prohibited without Thales prior written consent. Thales retains all intellectual property rights, title and interest in the CMMs and/or SBs provided, including all rights under applicable patents, copyrights, trademarks and trade secrets, and all renewals and extensions thereto. Company Name shall not alter or remove any patent, copyright, trademark, or proprietary rights notice. Agreed to and Accepted by: ____________________________ __________________________ (Print Name) (Title) ____________________________ __________________________ (Signature) (Date)