| CAA-2025-02-003 |
2025/02/12 |
FAA |
2025-01-03 |
This AD applies to the following CFM International, S.A. (CFM) engines:
(1) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1,LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35Aengines.
(2) Model LEAP-1C28, LEAP-1C30, and LEAP-1C30B1 engines.
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| CAA-2025-02-002 |
2025/02/10 |
FAA |
2025-01-09 |
This AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category.
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| CAA-2025-02-001 |
2025/02/05 |
FAA |
2024-26-02 |
(1) This AD applies to all airplanes and helicopters, certificated in any category, with a restraintsystem with a Pacific Scientific Company plastic rotary buckle assembly (buckle) part number (P/N)1111430 or P/N 1111475 (all dash numbers) installed having a date of manufacture on or before May31, 2007, or an unknown date of manufacture, except not those buckles repaired with the installationof an airworthy buckle handle after May 31, 2007, and marked with a BLUE logo on the centerbutton.
Note 1 to paragraph (c)(1):
Information about the location of the date of manufacture can befound in Meggitt Service Information Letter SIL Restraint-25-002-2023, dated September 25, 2023.
Note 2 to paragraph (c)(1):
This AD does not apply to buckles made of metal or to buckles with aBLUE logo on the center button.
(2) The buckles identified in paragraph (c)(1) of this AD may be installed on, but not limited to, TheBoeing Company, Bombardier Inc., Learjet Inc., Mitsubishi Heavy Industries, Ltd., Textron Aviation,Inc. (type certificate (TC) previously held by Cessna Aircraft Company), and Viking Air Limited (TCpreviously held by de Havilland, Inc.) model airplanes and Airbus Helicopters (TC previously held byEurocopter France) model helicopters, certificated in any category.
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| CAA-2025-01-020A |
2025/01/25 |
EASA |
2025-0021R1 |
Trent 7000-72 and Trent 7000-72C engines, all serial numbers, except those on which modification (mod) 72-K336 has been embodied in production.
These engines are known to be installed on, but not limited to, Airbus A330 (NEO) aeroplanes.
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| CAA-2025-01-020 |
2025/01/25 |
EASA |
2025-0021 |
Trent 7000-72 and Trent 7000-72C engines, all serial numbers, except those on which modification (mod) 72-K336 has been embodied in production.
These engines are known to be installed on, but not limited to, Airbus A330 (NEO) aeroplanes.
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| CAA-2025-01-018 |
2025/01/25 |
EASA |
2025-0024 |
ATR 42-300, ATR 42-320 and ATR 72-201 all MSN to which ATR modification (MOD) 00639 has been applied; and
ATR 42-400, ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN), except MSN 1617 and subsequent; and
ATR72-102, ATR 72-202, ATR 72-211, ATR 72-212 aeroplanes, all MSN; and
ATR 72-212A aeroplanes, to which ATR MOD 07900 has not been applied, except MSN 1627, 1677, 1678, 1703 to 1716 inclusive, 1718 to 1721 inclusive, 1723 to 1726 inclusive, 1728 and subsequent.
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| CAA-2025-01-019緊急 |
2025/01/23 |
EASA |
2025-0023-E |
Virus SW 121, SW 121A, SW 121C and Virus SW 128 aeroplanes, all serial numbers (s/n) as listed in the Pipistrel Vertical Solutions d.o.o. (PVS) Service Bulletin (SB) SB-121-00-80-028 Issue A02.
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| CAA-2025-01-017 |
2025/01/22 |
Transport Canada Civil Aviation |
CF-2025-06 |
Bombardier Inc. model CL-600-2A12 and CL-600-2B16 aeroplanes, all serial numbers.
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| CAA-2025-01-016 |
2025/01/21 |
Transport Canada Civil Aviation |
CF-2025-05 |
Bombardier Inc. model CL-600-1A11 aeroplanes, serial numbers 1004 through 1085
Bombardier Inc. model CL-600-2A12 aeroplanes, serial numbers 3001 through 3066
Bombardier Inc. model CL-600-2B16 aeroplanes, serial numbers 5001 through 5194, 5301 through 5665, 5701 through 6049, and 6050 and subsequent
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| CAA-2025-01-014修訂 |
2025/01/20 |
FAA |
2024-19-15Correction |
This AD applies to Safran Aerosystems (formerly AVOX Systems Inc.; Scott Aviation) oxygen cylinderand valve assemblies having part number (P/N) 89794050, 89794077, 89794015, 891511-14, 806835-01, 807982-01, 808433-01, or 891311-14; and oxygen valve assemblies (body and gage assemblies)having P/N 807206-01. These assemblies might be installed on, but not limited to, the aircraftidentified in paragraphs (c)(1) through (12) of this AD, certificated in any category.
(1) Airbus SAS Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes.
(2) Airbus SAS Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R,and C4-605R Variant F airplanes.
(3) Airbus SAS Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes.
(4) Airbus SAS Model A318-111, -112, -121, and -122 airplanes.
(5) Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, -133, and -151N airplanes.
(6) Airbus SAS Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N,and -273N airplanes.
(7) Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, -253N, -271N,-272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes.
(8) Airbus SAS Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342,-343, and -941 airplanes.
(9) Airbus Model A340-211, -212, -213, -311, -312, -313, -541, and -642 airplanes.
(10) ATR-GIE Avions de Transport Régional Model ATR42-200, -300, -320, and -500 airplanes.
(11) ATR-GIE Avions de Transport Régional Model ATR72-101, -102, -201, -202, -211, -212, and -212Aairplanes.
(12) The Boeing Company Model 747-8 series airplanes.
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