| 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 2014-0237R1 N/A Airbus SB A320-34-1127 original issue dated 24 April 1997, or Revision (Rev.) 01 dated 04 December 2001. Airbus SB A320-34-1456 original issue dated 02 December 2009, or Rev. 01 dated 15 May 2012. Airbus SB A320-34-1463 original issue dated 09 March 2010, or Rev. 01 dated 15 May 2012. Airbus SB A320-34-1170 original issue dated 18 December 1998, or Rev. 01 dated 14 May 1999, or Rev. 02 dated 07 December 1999, or Rev. 03 dated 17 February 2000, or Rev. 04 dated 24 May 2000, or Rev. 05 dated 11 September 2000, or Rev. 06 dated 18 October 2001, or Rev. 07 dated 04 December 2001, or Rev. 08 dated 15 January 2003, or Rev. 09 dated 17 February 2003, or Rev. 10 dated 21 November 2003, or Rev. 11 dated 18 August 2004, or Rev. 12 dated 02 December 2004, or Rev. 13 dated 18 January 2005, or Rev. 14 dated 21 April 2005, or Rev. 15 dated 19 July 2005, or Rev. 16 dated 23 November 2006, or Rev. 17 dated 14 February 2007, or Rev. 18 dated 09 October 2009, or Rev. 19 dated 09 November 2009, or Rev. 20 dated 01 December 2010, or Rev. 21 dated 24 March 2011, or Rev. 22 dated 19 July 2011, or Rev. 23 dated 03 February 2012, or Rev. 24 dated 12 April 2012, or Rev. 25 dated 04 September 2012, or Rev. 26 dated 16 September 2013, or Rev. 27 dated 18 March 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Fuselage - Lateral Engine Pylons - Stiffener Attachments to Pylon Spar 41 Assembly - Inspection / Repair |
| Falcon 7X aeroplanes serial numbers (S/N) 1 to 221 inclusive, except S/N 182 and S/N 220. |
| N/A N/A Dassault Aviation SB 7X-346 original issue dated 24 April 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Landing Gear - Nose Wheel Axle and Attachment Screws - Inspection / Replacement |
| Societe de Construction d'Avions de Tourisme et d'Affaires "S.O.C.A.T.A." - Groupe AEROSPATIALE, Société d'Exploitation des Etablissements MORANE-SAULNIER, Societe MORANE-SAULNIER) |
| DGAC France AD 91-163(A)R2 N/A SOCATA SB 150-32 Revision 2 dated January 1994, or Revision 3 dated September 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Navigation - Pitot / Static Pressure Head - Inspection / Test |
| BN2, BN2A, BN2B and BN2T (Islander) aeroplanes, all models, all serial numbers (s/n), and BN2A Mark III (Trislander) aeroplanes, all models, all s/n. |
| EASA AD 2006-0143R1 N/A Britten Norman Aircraft Ltd SB 310 issue 4 dated 25 September 2015. Britten Norman Aircraft Ltd Mod NB-M-1728 original issue (A) dated 20 May 2009, or issue 1 dated 04 August 2011, or issue 2 dated 14 August 2013. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Nacelles/Pylons - Pylon Side Panels at Rib 8 - Inspection |
| Airbus A300B4-203, A300B4-2C, A300C4-203 and A300F4-203 aeroplanes, manufacturer serial numbers (MSN) 210, 212, 218, 220, 227, 234, 235, 236, 239, 247, 255, 256, 259, 261, 274, 277, 292, 299, and 302. |
| N/A N/A Airbus SB A300-54-0075 original issue dated 11 August 1993, or Revision 01 dated 01 November 2007, or Revision 02 dated 26 June 2008, or Revision 03 dated 27 March 2013, or Revision 04 dated 26 May 2015. Airbus SB A300-54-0081 original issue dated 23 May 1995. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Fuel - FUELTRON Flowmeter - Removal |
| AS 355 E, AS 355 F, AS 355 F1 and AS 355 F2 helicopters, all serial numbers. |
| EASA AD 2013-0205 N/A Eurocopter ASB AS355-28.00.20 original issue dated 06 June 2013, or Airbus Helicopters ASB AS355-28.00.20 Revision 1 dated 24 June 2015. Airbus Helicopters SB AS355-28.00.21 original issue dated 24 June 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Exhaust - Exhaust Duct / End-pipe - Inspection / Modification |
| Scheibe SF 25 C powered sailplanes, all manufacturer serial numbers equipped with a Rotax 914 F3 engine. |
| N/A N/A Scheibe TM/SB 653-94 original issue, dated 24 September 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Power Plant - Engine Mount Bushings - Inspection |
| MBB-BK 117 D-2 helicopters, all serial numbers. |
| N/A N/A AHD ASB MBB-BK117 D-2-71A-002 original issue, dated 28 September 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Fuselage - Frame 74 to 90 / Shim Sheet on Section 18.1 - Inspection / Repair |
| Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0003, MSN from 0005 to 0017 inclusive, MSN from 0019 to 0023 inclusive, MSN from 0025 to 0031inclusive, MSN from 0033 to 0036 inclusive, MSN from 0038 to 0052 inclusive, MSN from 0054 to 0059 inclusive, MSN from 0061 to 0090 inclusive, MSN from 0092 to 0096 inclusive, MSN from 0098 to 0101 inclusive, MSN 0103, MSN from 0105 to 0112 inclusive, MSN 0114, MSN from 0120 to 0122 inclusive and MSN 0126. |
| N/A N/A Airbus SB A380-53-8095 original issue dated 22 July 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Flight Controls - Rudder Control System - Cracking of the Pilot-Side Rudder Pedal Tubes |
| Bombardier Inc.: Model CL-600-2C10 aeroplanes, serial numbers 10002 through 10340; Model CL-600-2D15 & CL-600-2D24 aeroplanes, serial numbers 15001 through 15318; Model CL-600-2E25 aeroplanes, serial numbers 19001 through 19039. |
| N/A N/A Bombardier Service Bulletin 670BA-27-065 |
 Equipment / Furnishings - Passenger / Crew and Emergency Exit Door Slide and Slide Raft Attachments - Inspection |
| 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 MSN 1543, 1592, 1607, 1608, 1619, 1624, 1628, 1634, 1635, 1641, 1642, 1645 through 1648 inclusive, 1650 and all higher 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, except those aeroplanes where all escape slides and slide rafts installations have passed an inspection in accordance with the instructions of the applicable Airbus Maintenance Planning Document (MPD) Task 256241-01-1, or Task 256241-02-1 or Task 256241-03-1, or Task 256241-04-1, as applicable, or Airbus Maintenance Review Board Report (MRBR) Maintenance Schedule Item (MSI) 25.62.00 section 01 or 02 or 03. |
| N/A N/A Airbus AOT A25L004-15 original issue, dated 24 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
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EASA biweekly AD report 2015-21
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