| CAA-2018-01-002 |
2018/01/15 |
EASA |
2018-0005 |
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, A330-343 aeroplanes, and A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes,
all manufacturer serial numbers (MSN) up to MSN 1779 inclusive, except those on which Airbus Service Bulletin (SB) A330-53-3275 or SB A340-53-4238 has been embodied.
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| CAA-2017-12-008A(已被CAA-2018-08-014取代) |
2018/01/15 |
EASA |
2017-0257R1 |
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, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers that have received Airbus modification (mod) 35871 in production or Airbus Service Bulletin (SB) A320-34-1397 in service (introducing Air Data Monitoring and BUSS function), except aeroplanes which have also received Airbus mod 159281 in production, or Airbus SB A320-34-1658 or A320-34-1659 in service (installing reversible BUSS function).
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| CAA-2015-07-005A(已有後續修訂版) |
2018/01/15 |
EASA |
2015-0135R1 |
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-2018-01-001 |
2018/01/12 |
EASA |
2018-0004 |
Airbus A350-941 aeroplanes, all serial numbers.
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| CAA-2017-12-009 |
2018/01/04 |
FAA |
2017-26-06 |
Rolls-Royce Corporation (RRC) AE 3007A, AE 3007A1, AE 3007A1/1, AE 3007A1/2, AE 3007A1/3, AE 3007A1P, AE 3007A1E, AE 3007A3, AE 3007C and 3007C1 turbofan engines with a fan wheel, part number (P/N) 23061670, installed.
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| CAA-2017-12-008(已有後續修訂版) |
2018/01/03 |
EASA |
2017-0257 |
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, A320-251N, A320-271N, 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-2017-12-007 |
2017/12/26 |
EASA |
2017-0254 |
DA 42 and DA 42 M (both Normal and Restricted category) aeroplanes, manufacturer serial numbers 42.004 to 42.427 inclusive, 42.AC001 to 42.AC151 inclusive, 42.M001 to 42.M027 inclusive, if equipped with TAE 125-02-99 engines (modification MÄM 42-198 or Optional Service Bulletin (OSB) 42-046) or TAE 125-02-114 engines (modification OÄM 42-252 or OSB 42-107).
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| CAA-2017-10-006修訂 |
2017/12/26 |
EASA |
2017-0208Correction |
Rotax 912 A1, 912 A2, 912 A3 and 912 A4 engines, Rotax 912 F2, 912 F3 and 912 F4 engines, Rotax 912 S2, 912 S3 and 912 S4 engines, Rotax 912 iSc2 Sport and 912 iSc3 Sport engines, and Rotax 914 F2, 914 F3 and 914 F4 engines, all serial numbers.
These engines are known to be installed on, but not limited to, the aeroplane types and models as listed in Appendix 1 of this AD. The installation of these engines was either done by the respective aeroplane manufacturer, or through modification of the aircraft by Supplemental Type Certificate (STC).
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| CAA-2017-12-005(已被CAA-2020-04-005取代) |
2017/12/22 |
EASA |
2017-0251 |
Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212, and A321-213 aeroplanes, all manufacturer serial numbers.
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| CAA-2017-12-004(已有後續修訂版) |
2017/12/22 |
EASA |
2017-0246 |
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), if equipped with Flight Control Primary Computer (FCPC) having software standard P13/M22 (hardware 2K2), P14/M23 (hardware 2K1) or M23 (hardware 2K0), or earlier standard.
Note 1: These software standards correspond, respectively, to Part Number (P/N) LA2K2B100DG0000, P/N LA2K1A100DF0000 and P/N LA2K01500AF0000. All affected aeroplanes should be equipped with this software, as required by EASA AD 2015-0124R3.
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