| CAA-2024-02-001（已被CAA-2024-02-001修訂取代） |
2024/02/02 |
EASA |
2024-0031 |
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, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers.
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| CAA-2024-01-014 |
2024/02/02 |
EASA |
2024-0029 |
Trent 7000-72 and Trent 7000-72C engines, all serial numbers.
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| CAA-2024-01-012 |
2024/02/02 |
EASA |
2024-0024 |
AC32.（） digital air data computers defined as affected part in this AD.
These ADC are known to be installed on, but not limited to AW 189, Pilatus PC-21, Cessna 550, and aircraft having Supplemental Type Certificate embodied.
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| CAA-2024-01-013(已被CAA-2024-12-001取代) |
2024/01/29 |
EASA |
2024-0027 |
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers.
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| CAA-2024-01-010(已被CAA-2024-05-003取代) |
2024/01/29 |
EASA |
2024-0026 |
LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, LEAP-1A35A engines, all serial numbers （s/n）. These engines are known to be installed on, but not limited to, certain Airbus A319, A320 and A321
aeroplanes.
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| CAA-2024-01-009 |
2024/01/26 |
FAA |
2023-26-07 |
This AD applies to General Electric Company （GE） Model GE90–90B and GE90–94B engines with interstage
HPT seals listed in Table 1 to Paragraph （c） of this AD and GE90–110B1 and GE90–115B engines with an
installed high-pressure turbine （HPT） stage 1 disk, HPT stage 2 disk, forward HPT rotor seal, or stages 7–9
compressor rotor spool part number （P/N） and serial number （S/N） identified in Table 1 to Paragraph （c） of this AD, or identified in Paragraph 4. APPENDIX—A, Tables 1, 2, or 3, of GE GE90–100 Service Bulletin
72–0914, dated January 25, 2023 （GE90–100 SB 72–0914）.
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| CAA-2024-01-008 |
2024/01/26 |
EASA |
2024-0023 |
A330-243, A330-302, A330-343 and A330-941 aeroplanes, manufacturer serial numbers （MSN） 1627, 1628, 1637, 1679, 1691, 1692, 1701, 1716, 1720, 1721, 1745, 1754, 1757, 1769, 1779, 1783, 1792, 1872, 1878, 1915, 1920, 1931, 1935, 1949, 1953, 1957, 1962, 1983, 1990, 1991, 1994, 1999, 2000 and 2010.
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| CAA-2024-01-006 |
2024/01/17 |
EASA |
2024-0016 |
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, and A330-941 aeroplanes, all manufacturer serial numbers （MSN） up to MSN 1919 inclusive, except MSN 1915; and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
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| CAA-2024-01-005 |
2024/01/12 |
FAA |
2023-25-10 |
This AD applies to The Boeing Company Model 787–8, 787–9, and 787–10 airplanes, certificated in any category, as identified in Boeing Service Letter 787–SL–25–025, dated September 6, 2022.
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| CAA-2024-01-004 |
2024/01/12 |
EASA |
2024-0014 |
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, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers.
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