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| This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD: AW109SP, AB139, AW139 and AB412 (all Models) helicopters, all serial numbers (s/n); BHTI 212, 214 and 412 helicopters (all Models), all s/n; BHTC 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n. |
 EASA AD 2015-0160 FAA AD 2013-06-51 Airbus Helicopters Deutschland ASB MBB-BK117 C-2-85A-038, Revision 5, dated 18 November 2015. Airbus Helicopters Deutschland ASB MBB-BK117 C-2-85A-045, original issue, dated 18 November 2015. Airbus Helicopters Deutschland ASB EC135-85A-058, Revision 6, dated 19 November 2015. Airbus Helicopters Deutschland ASB EC135-85A-064, original issue, dated 19 November 2015. Airbus Helicopters ASB AS365-25.01.25, Revision 6, dated 19 November 2015. Airbus Helicopters ASB AS365-25.01.65, original issue, dated 19 November 2015. Airbus Helicopters ASB AS332-25.02.70, Revision 6, dated 19 November 2015. Airbus Helicopters ASB AS332-25.03.19, original issue, dated 19 November 2015. Airbus Helicopters ASB EC225-25A133, Revision 6, dated 19 November 2015. Airbus Helicopters ASB EC225-25A187, original issue, dated 19 November 2015. AgustaWestland Bolletino Tecnico (BT) 139-443 dated 19 November 2015. AgustaWestland BT 109SP-100 dated 19 September 2015. Bell Helicopter Textron Canada Ltd.: None. Bell Helicopter Textron, Inc.: None. MD Helicopters, Inc.: None. Sikorsky Aircraft Corporation: None. |
 Rotorcraft Flight Manual - Limitations Section - Amendment |
| A109S helicopters, all serial numbers. |
| N/A N/A AgustaWestland RFM 109G0040A013 Issue 2 Revision 3, dated 23 April 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 21 - Air Conditioning - Electronic Centralized Aircraft Monitoring / Flight Warning System - Software Update / Aircraft Flight Manual Changes |
| Airbus A380-841, A380-842, and A380-861 aeroplanes, all manufacturer serial numbers, except aeroplanes on which Airbus modification (mod) 76212, or mod 76214, or mod 76715 has been embodied in production. |
| N/A N/A Airbus SB A380-31-8082 original issue dated 31 July 2015. Airbus SB A380-31-8083 original issue dated 31 July 2015. AFM TR 173 Issue 1 dated 17 July 2015. AFM TR 174 Issue 1 dated 17 July 2015. AFM TR 179 Issue 1 dated 17 July 2015. AFM TR 180 Issue 1 dated 17 July 2015. |
 ATA 72 - Engine - Operating Restriction |
| Solo Model 2350 C engines, all manufacturer serial numbers, equipped with a non-foldable propeller, except engines modified in accordance with Solo Kleinmotoren GmbH drawing nb. 2031211-V2 and, for engines installed on DG-Flugzeugbau Model DG-1000T powered sailplanes, concurrently modified in accordance with DG-Flugzeugbau drawing nb. 10 M 067. These engines are known to be installed on, but not limited to, DG-Flugzeugbau Model DG-1000T powered sailplanes. |
| EASA AD 2013-0217R1 N/A Solo Kleinmotoren GmbH Inspection Instruction SB 4603-1, dated 26 March 2015. Solo Kleinmotoren GmbH SB 4603-17, dated 15 July 2015. DG Flugzeugbau TN 1000/26, dated 23 September 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 52 - Doors - Main Landing Gear Doors - Modification |
| CN-235, CN-235-200, and CN-235-300 aeroplanes, all manufacturer serial numbers. |
| N/A N/A EADS CASA SB-235-52-0068 original issue 15 July 2002 or Revision 1 dated 24 October 2014 or Revision 2 dated 09 January 2015. EADS CASA SB-235-52-0061 original issue 31 dated October 1996 or Revision 1 dated 24 October 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 05 - Fuel - Fuel Tanks Safety - Inspection / Modification |
| 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). 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 A330-21-3096 Revision 01 dated 10 October 2005. Airbus SB A330-21-3148 original issue dated 30 January 2009. Airbus SB A330-28-3092 Revision 01 dated 14 December 2005. Airbus SB A330-28-3044 Revision 01 dated 25 November 1997. Airbus SB A330-28-3053 original issue dated 25 November 1997. Airbus SB A330-28-3101 Revision 01 dated 11 October 2006. Airbus SB A330-28-3082 original issue dated 14 June 2004, Revision 01 dated 2 March 2005, Revision 02 dated 11 August 2006, Revision 03 dated 15 November 2006 and Revision 04 dated 3 August 2007. Airbus SB A330-28-3113 original issue dated 19 July 2011. Airbus SB A330-31-3146 original issue dated 2 February 2010. Airbus SB A330-55-3016 Revision 01 dated 12 February 1997. Airbus SB A340-21-4107 Revision 01 dated 10 October 2005. Airbus SB A340-21-4147 original issue dated 30 January 2009. Airbus SB A340-28-4107 Revision 01 dated 14 December 2005. Airbus SB A340-28-4054 Revision 01 dated 25 November 1997. Airbus SB A340-28-4118 Revision 02 dated 10 July 2007. Airbus SB A340-28-4097 original issue dated 14 June 2004, Revision 01 dated 3 March 2005, Revision 02 dated 16 August 2006, Revision 03 dated 03 July 2007, Revision 04 dated 15 September 2008 and Revision 05 dated 3 June 2010. Airbus SB A340-28-4129 original issue dated 19 July 2011. Airbus SB A340-28-4078 original issue dated 17 March 2000. Airbus SB A340-28-4073 original issue dated 14 May 1998. Airbus SB A340-31-4125 original issue dated 27 October 2008. Airbus SB A340-55-4017 Revision 01 dated 12 February 1997. Airbus SB A340-57-5007 original issue dated 20 July 2005. Airbus SB A340-92-5010 original issue dated 31 March 2004. Airbus SB A340-28-5051 original issue, dated 01 September 2011. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 ATA 72 - Engine - Third Stage Turbine Wheel - Inspection |
| ASTAZOU XIV B and XIV H engines, all serial numbers, if fitted with a third stage turbine wheel part number (P/N) 0 265 25 700 0 or 0 265 25 706 0, and incorporate Turbomeca modification (mod) AB 173 or mod AB 208. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Aerospatiale, Sud Aviation) SA 319 B (Alouette III) and SA 342 J (Gazelle) helicopters. |
| N/A N/A Turbomeca SB 283 72 0811 Version A dated 25 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 72 - Engine - Intermediate Pressure Turbine Blade Rear Seal Fins - Inspection |
| Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-AE and Trent 1000-CE engines, serial numbers 10062, 10081, 10146, 10154, 10166, 10172 and 10186. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes. |
| N/A N/A Rolls-Royce NMSB Trent 1000 72-J125, original issue, dated 06 November 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 64 - Tail Rotor - Rotor Blades - Inspection |
| AS 332 C, AS 332 L, and AS 332 L1 helicopters, equipped with tail rotor (TR) de-icing installation unit Part Number (P/N) 204ZP01Y01 and tail rotor blade P/N 332A12-0055-XX (where XX represents any dash number) (type A10). |
| N/A N/A Airbus Helicopters ASB AS332-05.01.02 original issue, dated 22 July 2015, or Revision 1 dated 05 November 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 ATA 90 - Electrical Power - Ground Reference Connection - Inspection / Modification |
| BO105 A, BO105 C, BO105 D and BO105 S helicopters (all variants, except CB-5 and CBS-5), all serial numbers (S/N), if equipped with voltage regulator part number (P/N) 51565-000, or P/N 51565-000R, or P/N 51509-002R, except helicopters modified in service in accordance with ECD Alert Service Bulletin (ASB) BO105-80-118, or Service Bulletin (SB) BO105-80-119, or SB BO105-90-104. |
| N/A N/A ECD ASB BO105-90-103 Revision 2, dated 06 May 2009, or Revision 3, dated 08 March 2010, or Revision 4, dated 21 June 2010. ECD SB BO105-90-104 original issue, dated 08 March 2010, or Revision 1, dated 21 June 2010. The use of later approved revisions (that may be published by Airbus Helicopters Deutschland GmbH, the current design approval holder) of these documents is acceptable for compliance with the requirements of this AD. |
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EASA biweekly AD report 2015-24
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