| CAA-2014-09-002 |
2014/09/11 |
EASA |
2014-0201 |
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: AgustaWestland 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; AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC 635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76 (all Models) and S-92A helicopters, all s/n.
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| CAA-2013-02-002D修訂 |
2014/09/11 |
EASA |
2013-0020R4Correction |
All part numbers of safety belts and torso restraint systems of manufacture by AmSafe, Anjou Aeronautique, Davis Aircraft Products Co., Schroth Safety Products GmbH, Pacific Scientific,installed on any aircraft where dynamically tested seats are required in accordance with airworthiness requirements like the European Certification Specifications (CS), or JAR/FAR, paragraphs 23.562, 25.562, 27.562 and 29.562, if safety belts and torso restraint systems have been maintained or repaired after 28 September 2003 by maintenance organizations not holding the applicable maintenance data of the relevant approval holders, unless they are marked with European Parts Approval (EPA). Safety belts and torso restraints system repaired using repair data developed by an organization holding an EASA Design Organization Approval (DOA) in accordance with Commission Regulation (EU) No 748/2012 Part 21, Subpart J are not affected by this AD. These articles are approved through design changes or STC and are marked with the letters EPA accordingly.
The affected safety belts and torso restraint systems may be installed on, but not limited to, the aircraft listed in Appendix 1 of this AD. Note 1: This AD is applicable to safety belts and torso restraint systems, whose Component Maintenance Manuals (CMM) explicitly prohibit webbing replacement, unless this is accomplished by the design approval holder or by a repair station/maintenance organization authorized by the design approval holder.
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| CAA-2014-07-018A |
2014/09/04 |
EASA |
2014-0173R1 |
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers.
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| CAA-2014-08-012 |
2014/09/01 |
EASA |
2014-0189 |
Sikorsky S-76A, S-76B, S-76C and S-92A helicopters, all serial numbers (s/n), BHTI 212, 214B, 214B-1, 214ST, 412 and 412EP helicopters, all s/n, BHTC 222, 222B, 222U, 230 and 430 helicopters, all s/n.
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| CAA-2014-08-011(已有後續修訂版) |
2014/09/01 |
EASA |
2014-0188 |
SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, AS 332 C, AS332 C1, AS332 L, AS 332 L1, AS 332 L2 and EC 225 LP helicopters, all serial numbers (s/n), 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 s/n, and AB 212, AB 412 and AB 412EP helicopters, all s/n.
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| CAA-2014-08-010 |
2014/08/27 |
FAA |
2014-17-02 |
This AD applies to Honeywell ASCa Inc. emergency locator transmitters (ELTs) Model RESCU 406AF and 406AFN with transmitter unit (TU) part numbers (P/Ns) 1152682-1, -2, and -3.
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| CAA-2014-08-009(已有後續修訂版) |
2014/08/26 |
EASA |
2011-0173R1 |
Airbus A330-243, A330-243F, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers, except those that have embodied Airbus modification (mod) 202395 in production.
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| CAA-2014-08-008 |
2014/08/26 |
EASA |
2014-0187 |
Type D1-02 and D1-03 seats, also known as “Lightweight Classic” and “Lightweight Prestige”, Part Numbers (P/N) as specified in Geven Service Bulletin (SB) No. D103-25-004 Revision 2. The affected seats are known to be installed on, but not limited to, ATR 42 and ATR 72 aeroplanes.
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| CAA-2014-08-007 |
2014/08/26 |
EASA |
2014-0186 |
Airbus 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 on which Airbus modification (mod) 160500 or mod 160023 has been embodied in production, and those which have been modified in service through Airbus Service Bulletin (SB) A320-57-1173 at any revision (Rev.) up to Rev.04, or Airbus SB A320-57-1186 at any revision up to Rev.02, or Airbus SB A320-57-1187 at original issue or at Rev.01, except those on which Airbus mod 156108 has been embodied in production.
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| CAA-2014-08-006 |
2014/08/21 |
FAA |
2014-16-14 |
This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-22A1215, dated November 22, 2013.
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