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| MAKILA 2A and MAKILA 2A1 engines, all serial numbers. |
 N/A N/A Turbomeca MSB N° 298 72 2835 Version A dated 15 January 2016. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 53 - Fuselage - Door Stop Fitting Holes - Inspection / Repair |
| 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, except those on which Airbus modification (mod) 157039 has been embodied in production. |
| N/A N/A Airbus SB A320-53-1288, original issue dated 10 October 2014. Airbus SB A320-53-1290, original issue dated 10 October 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 28 - Fuel - Booster Pump - Inspection / Replacement |
| CN-235, CN-235-100, CN-235-200, CN-235-300 and C-295 aeroplanes, all manufacturer serial numbers (MSN). |
| EASA AD 2013-0186 N/A EADS CASA (Airbus Military) AOL 235-025, original issue dated 29 July 2013. EADS CASA (Airbus Military) AOL 295-025, Revision 01 dated 01 August 2013. Airbus D&S SB 235-28-0023 original issue, dated 14 March 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 27 - Flight Controls - Rudder Pedal Control System - Inspection |
| CN-235, CN-235-100, CN-235-200, CN-235-300 and C-295 aeroplanes, all manufacturer serial numbers. |
| N/A N/A Airbus D&S AOT-CN235-27-0002 original issue, dated 23 October 2014. Airbus D&S AOT-C295-27-0001 original issue, dated 23 October 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 38 - Water/Waste - Potable water system - Installation of Shrinkable Tubes as Spray Shields |
| Model 2000 aeroplanes, serial numbers (s/n) 017, s/n 019 through 021 inclusive, s/n 027 through 028 inclusive, s/n 030, 034, 040, 050 and 052. |
| N/A N/A SAAB SB 2000-38-012 original issue dated 20 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 72 - Engine - Gas Generator (Module 03) / Piston Shaft Small Diameter Labyrinth - Modification / Replacement |
| ARRIEL 1D and 1D1 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter) AS 350 BB, B1 and B2 helicopters. |
| N/A N/A Turbomeca SB 292 72 1357 version A dated 06 November 2014 or Mandatory SB 292 72 1357 version B dated 12 November 2015. Turbomeca SB 292 72 0357 version A dated 12 December 2007, or version B dated 21 February 2013. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 05 - Time Limits / Maintenance Checks - System Equipment Maintenance Requirements / ALS Part 4 - Amendment |
| Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, 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 A330 ALS Part 4 Revision 05, dated 19 October 2015. Airbus A340 ALS Part 4 Revision 04 issue 2, dated 26 November 2015. The use of later approved variations or revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 71 - Powerplant - Aft Engine Mount Retainers - Inspection / Replacement |
| Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212, and A321-213 aeroplanes, all manufacturer serial numbers |
| EASA AD 2015-0021 N/A Airbus AOT A71N001-12, Revision 01 dated 09 August 2012, or Revision 02 dated 27 February 2013. Airbus AOT A71N011-15 original issue, dated 16 September 2015. Airbus SB A320-71-1060 original issue, dated 09 October 2014. Airbus SB A320-71-1070 original issue, dated 23 November 2015. Goodrich Aerostructures SB RA32071-146, Revision 2 dated 26 July 2012. Goodrich Aerostructures SB RA32071-160, original issue dated 18 September 2014. Goodrich Aerostructures SB RA32071-165 dated 9 October 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 35 - Oxygen - Chemical Oxygen Generators - 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), except those that have a gaseous system installed for all oxygen containers 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, except those that have a gaseous system installed for all oxygen containers. |
| EASA AD 2014-0277 N/A Airbus AOT A35L007-14 original issue dated 18 December 2014, or Revision 01 dated 17 June 2015. B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. B/E Aerospace SIL D1019-01 Revision 1 dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator. |
 ATA 79 - Oil - Main Gearbox Oil Cooler Fan Hopper - Inspection |
| EC130 T2 helicopters, all serial numbers, except those that have embodied modification (MOD) 074547 in production. |
| N/A N/A Airbus Helicopters EC130 Emergency ASB 05A020 original issue, dated 20 October 2014, or Revision 1 dated 22 October 2015. Airbus Helicopters SB EC130-79-001 original issue dated 22 October 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 53 - Fuselage - Cabin and Cargo Compartment Structural Parts - Inspection / Replacement [Improper Heat Treatment] |
| Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0087 to 0089 inclusive, 0093 to 0096 inclusive, 0100, 0105 to 0116 inclusive, 0119 to 0128 inclusive, 0131 to 0136 inclusive, 0138 to 0140 inclusive, and MSN 0144. |
| N/A N/A Airbus SB A380-53-8082 original issue, dated 23 October 2015. Airbus SB A380-53-8083 original issue, dated 22 October 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Landing Gear - Main Landing Gear Door Fairing Seal Interference |
| Bombardier Inc. model CL-600-2E25 aeroplanes, serial numbers 19002 through 19041. |
| N/A N/A Bombardier SB 670BA-32-041 Bombardier SB 670BA-32-049 |
 ATA 76 - Engine Controls - Engine Control System Cables / Teleflex Cables - Replacement |
| CN-235, CN-235-100 and CN-235-200 aeroplanes, manufacturer serial numbers C-001 to C-074 inclusive |
| EASA AD 2014-0262 N/A CASA COM 235-140 revision 01, dated 21 March 2000. Airbus Military AOT-CN235-76-0001 original issue, dated 27 May 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 57 - Wing - Wing Top Skin Panels - Inspection / Repair |
| Airbus A310 aeroplanes, all certified models, all manufacturer serial numbers. |
| EASA AD 2014-0200R1 N/A Airbus SB A310-57-2096 original issue dated 06 May 2008, or Revision 01 dated 05 August 2010, or Revision 02 dated 05 March 2014, or Revision 03 dated 30 June 2015. The use of later approved revisions of this document or these is acceptable for compliance with the requirements of this AD. |
 Tail Rotor - Pitch Link Corrosion |
| Bell Helicopter Textron Canada Limited (BHTC) model 429 helicopters, serial numbers 57001 and subsequent |
| N/A N/A BHTC Alert Service Bulletin (ASB) 429-15-26 |
 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 73 - Engine Fuel & Control - Main Injector Half-Manifolds and Preference Injector - Replacement |
| ARRIUS 2B1 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters Deutschland (formerly Eurocopter Deutschland) EC135 twin-engine helicopters. |
| EASA AD 2012-0249 N/A Turbomeca ARRIUS 2B1 MM X 319 L5 301 2. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD |
 ATA 21 - Air Conditioning - Air Inlet Cover Ring - Inspection / Modification |
| MBB-BK117 C-2, MBB-BK117 C-2e, MBB-BK117 D-2 and MBB-BK117 D-2m helicopters, all serial numbers (S/N). |
| N/A N/A AHD ASB MBB-BK117 C-2-21A-011 original issue dated 16 November 2015. AHD ASB MBB-BK117 D-2-21A-004 original issue dated 16 November 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 62 - Main Rotor - Main Rotor Blade Vibration Absorber - Modification |
| MBB-BK117 C-2, MBB-BK117 C-2e, MBB-BK117 D-2 and MBB-BK117 D-2m helicopters, all serial numbers (s/n). |
| EASA AD 2015-0045 incl. corrections N/A AHD ASB MBB-BK117 C-2-62A-009 original issue dated 20 January 2015, or Revision 1 dated 28 October 2015. AHD ASB MBB-BK117 D-2-62A-001 original issue dated 20 January 2015, or Revision 1 dated 28 October 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
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EASA biweekly AD report 02-2016
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