EASA Bi-weekly AD Report 11-2015

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EASA Flight Controls - Elevator Aileron Computers - Replacement / Software Update Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers (MSN). DGAC ADs 95-203-072, AD 2001-508 and F-2004-147
N/A

Airbus SB A320-27-1135 original issue dated 29 June 2001, or Revision 01 dated 31 August 2001, or Revision 02 dated 18 April 2002.
Airbus SB A320-27-1151 original issue dated 09 March 2004, or Revision 01 dated 19 October 2004.
Airbus SB A320-27-1152 original issue dated 04 June 2004, or Revision 01 dated 19 October 2004, or Revision 02 dated 04 April 2006.
Airbus SB A320-27-1243 original issue dated 17 March 2015.
Airbus SB A320-27-1244 original issue dated 05 March 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. EASA Flight Controls - Improperly Formulated Task in the Aircraft Maintenance Manual for the Flight Control Unit Back-up Module Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes, serial numbers 9002 and subsequent. N/A
N/A

Aircraft Maintenance Manual (AMM) Task 27-61-05-710-801
Certification Maintenance Requirement (CMR) task number 27-61-05-201 EASA Navigation - Angle of Attack Sensors - Replacement Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers EASA ADs 2012-0236R1, 2013-0022 and 2014-0266-E
N/A

Airbus SB A320-34-1415 Revision 03 dated 08 July 2010.
Airbus SB A320-34-1444 original issue dated 07 October 2009, or Revision 01 dated 17 March 2011.
Airbus SB A320-34-1452 original issue dated 29 January 2010.
Airbus SB A320-34-1564 original issue dated 25 January 2013.
Airbus SB A320-34-1610 original issue dated 31 March 2015.
Thales SB C16291A-34-007 Revision 01 dated 03 December 2009, or Revision 02 dated 16 December 2011, or Revision 03 dated 10 April 2012, or Revision 04 dated 11 October 2012.
Thales SB C16291A-34-009 original issue dated 10 September 2009, or Revision 01 dated 07 January 2010.
Airbus AFM A320 TR 502 issue 1, EASA approved 05 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. EASA Engine Controls - Electrical Wiring Harness - Modification RTM 322-01/9 and RTM 322-01/9A engines, all serial numbers.
These engines are known to be installed on, but not limited to, NH Industries NH90 (military) helicopters. N/A
N/A

Turbomeca MSBP-M3-A-76-10-10-02A-A-A Issue 1 dated 24 March 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. EASA Navigation - Angle of Attack Sensors - Replacement Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN. N/A
N/A

Airbus SB A330-34-3315 original issue dated 26 March 2015.
Airbus SB A330-34-3228 original issue dated 07 October 2009.
Airbus SB A330-34-3215 Revision 02 dated 29 March 2010.
Airbus SB A340-34-4294 original issue dated 26 March 2015.
Airbus SB A340-34-4234 original issue dated 07 October 2009.
Airbus SB A340-34-4215 Revision 02 dated 29 March 2010.
Airbus SB A340-34-5105 original issue dated 26 March 2015.
Airbus SB A340-34-5062 Revision 01 dated 29 March 2010.
Airbus SB A340-34-5070 original issue dated 09 October 2009.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. EASA Fuselage - Frame 5700 Middle Section - Inspection AB139 and AW139 helicopters, all serial numbers (S/N), if equipped with helicopter frames 5700 Middle Section:
Part Number (P/N) 3P5338A13352 (left hand) and P/N 3P5338A13452 (right hand), or
P/N 3P5338A13353 (left hand) and P/N 3P5338A13453 (right hand),
except helicopters S/N 31002, 31003, 31004 and 31007. N/A
N/A

Agusta BT 139-018 Revision B dated 18 October 2006.
Agusta BT 139-089 original issue dated 19 February 2010.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. EASA Fuselage - Rear Fuselage Frame 68 - Inspection / Repair   DGAC AD 96-298-093(B)R2
N/A

Airbus SB A320-53-1089 Revision 01 dated 04 June 1998, or Revision 02 dated 03 February 2003, or Revision 03 dated 18 March 2015.
Airbus SB A320-53-1090 original issue dated 22 November 1995, or Revision 01 dated 10 June 1998, or Revision 02 dated 22 December 1998.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. EASA Fuselage - Emergency Exit Cut-Out Area - Modification Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232 and A320-233 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 152637 has been embodied in production. EASA AD 2014-0176
N/A

Airbus SB A320-53-1265 original issue dated 02 January 2013, or Revision 01 dated 02 July 2013, or Revision 02 dated 10 July 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. EASA Time Limits / Maintenance Checks - ALS Part 2 - Damage Tolerant Airworthiness Limitation Items - Implementation Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers. EASA AD 2013-0147
N/A

Airbus A318/A319/A320/A321 ALS Part 2 Revision 03, dated 27 October 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. EASA Power Plant - Aft and Forward Engine Mount Bolts - Torque Check / Replacement Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, and
Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes,
from manufacturer serial number (MSN) 0715 to MSN 1507 inclusive, and MSN 1509, except aeroplanes on which all engines have been removed and/or replaced since Airbus date of manufacture. N/A
N/A

Airbus AOT A71L004-14 dated 01 April 2014, or Revision 01 dated 07 April 2014.
Airbus AOT A71L006-14 dated 22 July 2014.
Airbus AOT A71L005-14 dated 29 September 2014, or Revision 01 dated 11 December 2014.
Airbus AOT A71L008-14 dated 29 September 2014, or Revision 01 dated 18 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

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