| CAA-2015-10-010 |
2015/11/04 |
FAA |
2015-22-03 |
This AD applies to:(1) All Pratt & Whitney Division PW4164, PW4168, PW4168A, PW4164C, PW4164C/B, PW4164-1D, PW4168-1D, PW4168A-1D, PW4170, PW4164C-1D, and PW4164C/B-1D turbofan engines with a low-pressure turbine (LPT) 4th stage inner air seal (IAS), part number (P/N) 51N038, installed. (2) All PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C, PW4062, PW4062A, PW4152, PW4156, PW4156A, PW4158, PW4160, PW4460, PW4462, and PW4650 turbofan engines including models with a ''-3'' suffix with an LPT 4th stage IAS, P/N 51N038, installed.
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| CAA-2015-10-004修訂 |
2015/11/04 |
FAA |
2015-18-03Correction |
This AD applies to Honeywell International Inc. TPE331-5, -5A, -5AB, -5B, -10, -10R, -10U, -10UF, -10UG, -10UGR, and -10UR model turboprop engines, with an engine propeller shaft coupling, part number (P/N) 3107065-1, 865888-3, 865888-6, or 865888-8, installed.
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| CAA-2015-10-008 |
2015/11/02 |
FAA |
2015-19-51 |
This AD applies to Model S-76A, S-76B, S-76C, and S-76D helicopters with main rotor (M/R) servo input control pushrod (pushrod) assembly part number (P/N) 76400-00034-059 or tail rotor (T/R) pushrod assembly P/N 76400-00014-071 installed, certificated in any category.
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| CAA-2015-10-009 |
2015/10/30 |
FAA |
2015-22-01 |
This AD applies to all The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes, certificated in any category.
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| CAA-2015-10-007 |
2015/10/30 |
FAA |
2015-21-10 |
This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category.
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| CAA-2015-10-001 |
2015/10/26 |
EASA |
2015-0199 |
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.
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| CAA-2015-10-006 |
2015/10/22 |
EASA |
2015-0213 |
ARRIEL 2E and 2N engines, all serial numbers. and These engines are known to be installed on, but not limited to, Airbus Helicopters AS 365 N3 and Airbus Helicopters Deutschland MBB-BK 117 D-2 helicopters.
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| CAA-2015-10-002 |
2015/10/20 |
EASA |
2015-0205 |
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.
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| CAA-2015-10-005 |
2015/10/16 |
EASA |
2015-0207 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial number (MSN), except those on which Airbus modification (mod) 49194 has been embodied in production. and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313, all MSN, except those on which Airbus mod 49194 has been embodied in production.
Airbus A340-541 and A340-642 all MSN, except those on which Airbus mod 51172 has been embodied in production.
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| CAA-2015-10-004(已有後續修訂版) |
2015/10/15 |
FAA |
2015-18-03 |
This AD applies to Honeywell International Inc. TPE331-5, -5A, -5AB, -5B, -10, -10R, -10U, -10UF, -10UG, -10UGR, and -10UR model turboprop engines, with an engine propeller shaft coupling, part number (P/N) 3107065-1, 865888-3, 865888-6, or 865888-8, installed.
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