| CAA-2014-10-008修訂(已有後續修訂版) |
2014/11/05 |
EASA |
2014-0234Correction |
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 (MSN).
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| CAA-2013-04-004A(已有後續修訂版) |
2014/11/05 |
Japan CAB |
8201A-2014 |
Kawasaki BK117 series helicopters equipped with a Goodrich rescue hoist assembly having a Part Number (P/N) as listed in Kawasaki Service Bulletin No. KSB-117-361C, or later JCAB-approved revision.
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| CAA-2014-10-008(已有後續修訂版) |
2014/10/30 |
EASA |
2014-0234 |
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 (MSN).
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| CAA-2014-10-007 |
2014/10/30 |
FAA |
2014-21-06 |
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes identified in paragraphs (c)(1)(i), (c)(1)(ii), and (c)(1)(iii) of this AD. (i) Model 400 Beechjet airplanes having serial numbers RJ-1 through RJ-65, inclusive.
(ii) Model 400A Beechjet airplanes having serial numbers RK-1 through RK-604, inclusive. (iii) Model 400T Beechjet airplanes having serial numbers TT-1 through TT-180, inclusive; and TX-1 through TX-13, inclusive. (2) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Mitsubishi Heavy Industries, Inc. Ltd.) Model MU-300 airplanes, having serial numbers A003SA through A093SA, inclusive.
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| CAA-2014-10-006 |
2014/10/30 |
EASA |
2014-21-01 |
This AD applies to all General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines with fuel manifold, part number (P/N) 1303M31G04, 1303M32G04, 1303M31G06, 1303M32G06, 1303M31G07, 1303M32G07, 1303M31G08, 1303M32G08, 1303M31G12, 1303M32G12, 2420M70G01, or 2420M71G01, installed.
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| CAA-2014-10-005 |
2014/10/24 |
EASA |
2014-0228 |
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 on which Airbus modification 202702 has been embodied in production, 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.
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| CAA-2014-07-025A |
2014/10/24 |
EASA |
2014-0180R1 |
MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK 117 C-1 and MBB-BK 117 C-2 helicopters, all serial numbers (s/n), and
BO 105 A, BO 105 C, BO 105 D, BO 105 S and BO 105 LS A-3 helicopters, all variants, all s/n.
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| CAA-2012-09-017A |
2014/10/14 |
EASA |
2012-0198R1 |
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 and A320-233 aeroplanes, all manufacturer serial numbers, except those which have embodied Airbus modification (mod) 154327 in production.
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| CAA-2006-05-003D(已被CAA-2023-05-008取代) |
2014/10/14 |
EASA |
2007-0218R2 |
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, if equipped with Eaton Aerospace Limited (formerly FR-HITEMP Limited) fuel pumps identified by Part Number (P/N) 568-1-27202-001, P/N 568-1-27202-002, or P/N 568-1-27202-005.
Note: Aeroplanes on which fuel pumps have not been modified or replaced since embodiment of Airbus modification (mod) 37508 in production are not affected by the requirements of this AD.
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| CAA-2014-10-004 |
2014/10/13 |
FAA |
2014-20-10 |
This AD applies to The Boeing Company Model 777-200 and -300 series airplanes, certificated in any category, equipped with Pratt & Whitney PW4000 series engines.
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