| CAA-2024-02-006緊急(已被CAA-2024-02-006A取代) |
2024/02/06 |
EASA |
2024-0037-E |
E4 and E4P engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Diamond Aircraft Industries DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes.
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| CAA-2024-02-004 |
2024/02/06 |
FAA |
2024-01-07 |
Boeing Company Model 777–200, –200LR, –300, –300ER, and 777F series airplanes, certificated in any category.
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| CAA-2024-02-001修訂(已被CAA-2025-02-007取代) |
2024/02/06 |
EASA |
2024-0031Correction |
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-2024-02-002(已被CAA-2025-02-008取代) |
2024/02/02 |
EASA |
2024-0030 |
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-2024-02-001(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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