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| Viper Mk. 521, Mk. 522 and Mk. 601-22 engines, all serial numbers. These engines are known to be installed on, but not limited to, Beechcraft Corporation (formerly Hawker Beechcraft, Raytheon Aircraft Company, Beech Aircraft Corporation, British Aerospace, Hawker Siddeley) BH.125 and HS.125 Series 1A and 1B, Series 3, 3A/B, 3A/R, 3B/R, 3A/RA, 3B/RA, 3B/RB and 3B/RC, Series 400, 400A, 400B, 401B, 403A(C) and 403B, and Series 600, 600A and 600B aeroplanes. |
 EASA AD 2012-0243 N/A Rolls-Royce Alert SB 72-A207, original issue dated January 2015. Rolls-Royce Alert SB 72-A408 (Circ. A), original issue dated January 2015. Rolls-Royce Alert SB 72-A408 (Circ. B), original issue dated January 2015. Rolls-Royce Alert SB 72-A412 (Circ. B), original issue dated January 2015. Rolls-Royce Alert SB 72-A413 (Circ. A), original issue dated January 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Windows - Rear Hatch / Jettisoning System - Inspection |
| SA330 J helicopters, all manufacturer serial numbers, if equipped with an extraction tape fitted with press-studs on the emergency exit rear hatch. |
| N/A N/A Airbus Helicopters ASB SA330-56.02 original issue, dated 10 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Windows - Cabin Windows / Jettisoning System - Inspection |
| EC 155 B and B1 helicopters, all manufacturer serial numbers, if equipped with an extraction tape fitted with press-studs on the emergency exit windows. |
| N/A N/A Airbus Helicopters ASB EC155-56A006 original issue, dated 10 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Doors - Sliding / Plugging Cabin Doors - Limitation / Modification / Inspection |
| AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 and EC 225 LP helicopters, all serial numbers, if equipped with one or two cabin lateral sliding and plugging doors incorporating a sliding lateral plug door fitting Part Number (P/N) 332A223314.00 or P/N 332A221366.06 or P/N 332A090856.02. |
| EASA AD 2012-0111 N/A Eurocopter AS332 ASB No. 01.00.79 Revision 1 dated 06 June 2012 and Airbus Helicopters AS332 ASB No. 01.00.79 Revision 2 dated 23 June 2015. Eurocopter EC225 ASB No. 04A007 Revision 1, dated 06 June 2012, and Airbus Helicopters EC225 ASB No. 04A007 Revision 2, dated 23 June 2015. Airbus Helicopters SB AS332-52.00.43 original issue, dated 23 June 2015. Airbus Helicopters SB EC225-52-008 original issue, dated 23 June 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Tail Rotor - Pitch Link Spherical Bearing Accelerated Wear |
| Bell Helicopter Textron Canada Limited (BHTC) model 429 helicopters, serial numbers 57001 and subsequent. |
| N/A N/A BHTC Alert Service Bulletin (ASB) 429-15-16 |
 Exhaust - Thrust Reverser Doors Attachment Lugs - Inspection / Replacement |
| Mystere-Falcon 50 aeroplanes, all manufacturer serial numbers. |
| N/A N/A Dassault Aviation SB F50-541 original issue dated 24 September 2014, or Revision 1 dated 12 May 2015. Dassault Aviation Master Minimum Equipment List, DTM 824 Revision 6 dated 2 November 2011 and M&O DGT85583 Revision 2 dated 02 September 2011 Dassault Aviation Master Minimum Equipment List, DTM 824EX Revision 2 dated 25 March 2010 and M&O DTM610 Revision 2 dated 25 March 2010. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. Dassault Aviation AMM task 78-31-00-250-802, as per Mystère-Falcon 50 AMM revision 26, dated October 2014. Dassault Aviation AMM task 78-30-00-910-809, as per Mystère-Falcon 50 AMM revision 26, dated October 2014. |
 Main Rotor - Swashplate Assembly - Replacement / Inspection |
| MBB-BK117 A-1, MBB-BK117 A-3, MBB-BK117 A-4, MBB-BK117 B-1, MBB-BK117 B-2, MBB-BK117 C-1, MBB-BK117 C-2 and MBB-BK117 C-2e helicopters, all serial numbers (s/n), and BO105 A, BO105 C, BO105 D, BO105 S and BO105 LS A-3 helicopters, all variants, all s/n. |
| EASA AD 2014-0180R1 N/A AHD ASB MBB-BK117-40A-115 original issue dated 31 March 2014, or Revision 1 dated 04 August 2014, and Revision 2 dated 30 July 2015. AHD ASB MBB-BK117C-2-62A-007 original issue dated 31 March 2014, revision 01 dated 04 August 2014, and Revision 2 dated 30 July 2015. AHD ASB BO105-40A-107 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015. AHD ASB BO105LS-40A-12 original issue dated 31 March 2014, or Revision 1 dated 08 September 2014, and Revision 2 dated 30 July 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
 Wing Structure and Fuselage Attachment - Revised Airworthiness Limitations |
| Model R 2100, R 2100 A, R 2112, R 2120 U and R 2160 D aircraft, S/N 001 through to 378. Model R 2160 aircraft, S/N 001 though to 378 and S/N 160A-06001 onwards. Model R 2160i aircraft, S/N 001 through to 378 and S/N 160Ai-07007 onwards |
| N/A N/A Section 3.2 - Airworthiness Limitations of Service Manuals AAA079 and AAA080 |
 Equipment / Furnishings - Overhead Stowage Compartment Attachments - Modification |
| Airbus A321-211 and A321-231 aeroplanes, manufacturer serial numbers 3191, 3217, 3241, 3251, 3267, 3334, 3459, 3493, 3507, 3552, 3566, 3587, 3645, 3681, 3764, 3784, 3847, 3867, 3920, 3934, 3938, 3951, 3981, 4058, 4074, 4099, 4103, 4116, 4148, 4184, 4189, 4194, 4217, 4224, 4230, 4266, 4271, 4274, 4292, 4299, 4338, 4341, 4369, 4387, 4416, 4430, 4461 and 4500. |
| N/A N/A Airbus SB A320-25-1852 original issue dated 24 September 2012. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Oxygen - Chemical Oxygen Generators - 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 aeroplane models, all manufacturer serial numbers, except those that have embodied Airbus modification 33125 (gaseous system for all oxygen containers) in production. |
| EASA AD 2014-0275R1 N/A Airbus AOT A35N006-14 dated 10 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. |
 Fin Forward Pickup - Inspection |
| Model PAL 750XL aircraft, S/N all through to 193, 195 and 197. |
| NZCAA AD DCA/750XL/16A N/A Pacific Aerospace Limited Mandatory Service Bulletin (MSB) PACSB/XL/068 |
 Engine - Accessory Gear Box Module M01 - Inspection / Replacement |
| ARRIEL 2B, 2B1, 2B1A, 2B1B, 2C, 2C1, 2C2, 2D, 2E, 2N, 2S1 and 2S2 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters AS350B3, EC130B4, EC130T2, AS365N3, EC155B and EC155B1, Airbus Helicopters Deutschland MBB-BK 117 D-2 (EC145T2 or H145), Avic international AC311 and Sikorsky S-76C helicopters. |
| N/A N/A Turboméca MSB 292 72 2861 version A dated 24 April 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD |
 Doors - Jettison System Adhesive Seal - Removal |
| MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2 and MBB-BK 117 C-1 helicopters, all serial numbers. |
| N/A N/A AHD ASB MBB-BK117-20A-114 Revision 1 dated 30 July 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Wings - Movable Flap Track Fairing (MFTF) #6 - Inspection / Replacement / Modification |
| Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers on which Airbus modification (mod) 68729 or mod 71589 has been embodied in production, or Airbus Service Bulletin (SB) A380-57-8017 or SB A380-57-8036 has been embodied in service, except aeroplanes on which Airbus mod 74424 has been embodied in production. |
| EASA AD 2011-0002R1 N/A Airbus SB A380-57A8032 original issue dated 26 November 2010. Airbus SB A380-57-8017 original issue dated 05 June 2009. Airbus SB A380-57-8036 original issue dated 13 July 2012. Airbus SB A380-57-8096 original issue dated 16 April 2014. Airbus SB A380-57-8093 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. |
 Stabilizers - Tailplane Lower Fitting - Inspection / Replacement |
| AW 189 helicopters, all serial numbers, if equipped with tailplane lower fitting Part Number (P/N) 8G5350A07051, which is part of tailplane lower fitting assembly P/N 8G5350A06731. |
| N/A N/A AgustaWestland BT 189-038 original issue, dated 05 August 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
 Power Plant - Engine Fan Cowl Panel Dislodgement During Flight |
| Bombardier Inc. model CL-600-2B19 aeroplanes. |
| N/A N/A Service Bulletin (SB) 601R-71-034 |
 Equipment / Furnishings - Hoist - Test / Replacement |
| 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, AB412 and AW189 (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, EC225 LP and EC175 B helicopters, all s/n; AHD MBB-BK117 C-2 and D-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 2015-0069 (including Correction)FAA AD 2013-06-51 AHD ASB No. MBB-BK117 C-2-85A-038, Revision 4, dated 10 June 2015. AHD ASB No. MBB-BK117 D-2-85A-004, original issue, dated 10 June 2015. AHD ASB No. EC135-85A-058, Revision 5, dated 10 June 2015. AH ASB No. AS365-25.01.25, Revision 5, dated 10 June 2015. AH ASB No. AS332-25.02.70, Revision 5, dated 10 June 2015. AH ASB No. EC225-25A133, Revision 5, dated 10 June 2015. AgustaWestland BT 139-430, original issue, dated 11 June 2015. AgustaWestland BT 109-095, original issue, dated 11 June 2015. AgustaWestland BT 189-028, original issue, dated 11 June 2015. Bell Helicopter Textron Canada Ltd.: None. Bell Helicopter Textron, Inc.: None. MD Helicopters, Inc.: None. Sikorsky Aircraft Corporation: None. |
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EASA biweekly AD report 2015-18
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