EASA Airworthiness Directives 04-2016

The latest EASA airworthiness directives from myairlease.

ATA 32 - Landing Gear - Main Landing Gear Door Actuator - Monitoring / Inspection / Replacement / Modification

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 2013-0288
N/A

Airbus AFM TR 437 dated 06 June 2014.
Airbus AOT A320-32A1390 original issue dated 10 February 2011.
Airbus SB A320-32-1390 Revision 01 dated 21 September 2011, or Revision 02 dated 23 October 2013, or Revision 03 dated 13 July 2014.
Airbus AOT A32N001-13 original issue dated 24 June 2013.
Airbus SB A320-32-1409 original issue dated 19 March 2013.
Airbus SB A320-32-1407 original issue dated 14 May 2013, or Revision 01 dated 03 July 2014.
Airbus SB A320-31-1414 original issue dated 19 December 2012, or Revision 01 dated 21 March 2013, or Revision 02 dated 30 July 2013.
GE SB 114122-32-105 original issue dated 17 January 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Airbrake Panels - Inspection

Discus-2a, Discus-2b, Discus-2c sailplanes, Ventus-2a, Ventus-2b and Ventus-2c sailplanes, and Discus-2T, Discus-2cT, Ventus-2cT and Ventus-2cM powered sailplanes, serial numbers as listed in Schempp-Hirth Flugzeugbau GmbH issued Technische Mitteilung / Technical Note (TN) 349-39, 360-29, 825-55 and 863-22 (published as a single document).

N/A
N/A

Schempp-Hirth Flugzeugbau GmbH TN 349-39, 360-29, 825-55, 863-22 (single document) and the associated Arbeitsanweisung (Working Instructions) to the TN, both dated 22 January 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 62 - Main Rotor System - Main Rotor Hub - Inspection / Replacement

EC 135 P1(CDS), EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+, EC 135 T1(CDS), EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+, EC 635 T1(CPDS), EC 635 P2+ and EC 635 T2+ helicopters, all serial numbers.

EASA AD 2012-0041R1
N/A

ECD/AHD ASB No. EC135-62A-029 Rev. 1, dated 16 May 2012, or Rev. 2 dated 17 May 2012, or Rev.
3 dated 09 August 2012, or Rev. 4 dated 23 August 2012, or Rev. 5 dated 10 September 2012, or Rev. 6 dated 02 October 2012, or Rev. 7 dated 22 October 2012, or Rev. 8 dated 22 April 2015.
ECD SB No. EC135-62-030 original issue dated 16 August 2012, or Rev. 1 dated 31 August 2012, or Rev. 2 dated 15 October 2012.
ECD SB No. EC135-62-032 original issue dated 04 September 2012, or Rev. 1 dated 15 October 2012.
AHD SB No. EC 135-62-036 original issue dated 29 July 2015.
The use of later approved revisions of these documents (that may be published by AHD, the current design approval holder) is acceptable for compliance with the requirements of this AD.

ATA 73 - Engine Fuel & Control - Hydro-Mechanical Metering Unit - Inspection

ARRIEL 2D engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter) AS 350 B3 and EC 130 T2 helicopters.

EASA AD 2013-0079R1
N/A

Turbomeca MSB A292 73 2847 version A dated 29 May 2012, or version B dated 06 March 2013, or version C dated 03 December 2013.
Turbomeca MSB A292 73 2851 version A dated 03 December 2013, or version B dated 22 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 57 - Wings - Leading Edge Shear Cleats - Inspection / Replacement

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes on which Airbus modification (mod) 73979, mod 73981 and mod 73983 have been embodied in production.

EASA AD 2012-0052R1
N/A

Airbus SB A380-57-8035 original issue dated 16 September 2011, or Revision 01 dated 30 August 2013, or Revision 02 dated 09 June 2015.
Airbus SB A380-57-8089 original issue dated 01 October 2014.
Airbus SB A380-57-8108 original issue dated 05 October 2015.
Airbus SB A380-57-8110 original issue dated 01 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 57 - Wings - Wing Inboard Leading Edge Droop Nose Gooseneck - Inspection / Repair / Replacement

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes that have embodied Airbus modification (mod) 73979, mod 73981 and mod 73983 in production.

EASA AD 2012-0153
N/A

Airbus AOT A57R001-12 original issue dated 14 May 2012.
Airbus SB A380-57-8071 original issue dated 18 June 2013.
Airbus SB A380-57-8087 original issue dated 28 November 2013.
Airbus SB A380-57-8089 original issue dated 01 October 2014.
Airbus SB A380-57-8108 original issue dated 05 October 2015.
Airbus SB A380-57-8110 original issue dated 01 October 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 25 - Equipment / Furnishings - Emergency Parachute Rubber Bands - Replacement

Type 10-30/24, 12-61/24 and 12-82/23 Emergency Parachutes, all variants, serial number (s/n) 13-227154 to s/n 14-227292 inclusive.

N/A
N/A

Heinrich Mertens TM 002-03-16, dated 02 February 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Flight Control Primary Computer - Modification / 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 A330-27-3205 original issue dated 09 March 2015.
Airbus SB A330-27-3207 original issue dated 30 June 2015.
Airbus SB A330-27-3208 [expected to be issued in April 2017].
Airbus SB A340-27-4195 original issue dated 24 November 2015.
Airbus SB A340-27-4196 original issue dated 24 November 2015.
Airbus SB A340-27-5064 [expected to be issued in July 2016].
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

ATA 27 - Flight Controls - Trimmable Horizontal Stabilizer Actuator Ballscrew Lower Splines - Inspection / 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.

N/A
N/A

Airbus SB A320-27-1214 original issue dated 23 February 2012.
Airbus SB A320-27-1222 original issue dated 17 July 2015.
Goodrich SB 47145-27-16 original issue dated 07 November 2011.
UTAS SB 47145-27-18 original issue dated 31 March 2015.
UTAS SB 47145-27-20 original issue dated 16 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Time Limits and Maintenance Checks - Changes to Component Retirement Lives

Bell Helicopter Textron Canada Ltd. (BHTC) model 407 helicopters, serial numbers 53000 and subsequent.

TC AD CF-99-04
N/A

Bell 407 Maintenance Manual, BHT-407-MM, ALS, Chapter 4

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