| CAA-2025-08-002(已更新) |
2025/08/11 |
EASA |
2025-0171 |
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-2025-08-004 |
2025/08/08 |
EASA |
2025-0173 |
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and
ATR 72-212 and ATR 72-212A aeroplanes, all MSN.
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| CAA-2025-08-001 |
2025/08/04 |
EASA |
2025-0169 |
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-2025-07-011(已更新) |
2025/08/04 |
EASA |
2025-0167 |
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, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-271NY, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN).
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| CAA-2025-07-010 |
2025/08/04 |
EASA |
2025-0166 |
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, except:
- A319 aeroplanes on which Airbus modification (mod) 28238, mod 28162 and mod 28342 have been embodied in production; and
- A318 aeroplanes on which mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service.
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| CAA-2025-07-009 |
2025/08/04 |
FAA |
2025-15-07 |
This AD applies to all The Boeing Company Model 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747- 400F, 747-8F, and 747-8 series airplanes, certificated in any category.
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| CAA-2025-02-018A修訂 |
2025/08/04 |
EASA |
2025-0043R1Correction |
A330-243, A330-243F, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers (MSN) having Airbus modification (mod) 207423 installed, except those having Airbus mod 211442 installed.
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| CAA-2025-02-018A(已更新) |
2025/08/04 |
EASA |
2025-0043R1 |
A330-243, A330-243F, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers (MSN) having Airbus modification (mod) 207423 installed.
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| CAA-2025-07-003A(已更新) |
2025/07/30 |
EASA |
2025-0151R1 |
Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, all manufacturer serial numbers.
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| CAA-2025-07-008 |
2025/07/28 |
FAA |
2025-15-01 |
(1) This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and-900ER series airplanes, certificated in any category.
(2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability toaccomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE isinstalled, a “change in product” alternative method of compliance (AMOC) approval request is notnecessary to comply with the requirements of
14 CFR 39.17
.
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