CAA-2024-03-002A |
2024/04/18 |
EASA |
2024-0058R1 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
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CAA-2022-06-001B |
2024/04/17 |
EASA |
2022-0096R2 |
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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-2024-04-002 |
2024/04/15 |
FAA |
2024-05-11 |
This AD applies to nternational Aero Engines, LLC (IAE LLC) Model PW1122G–JM, PW1124G1–JM, PW1124G–JM, PW1127G–JM, PW1127G1–JM, PW1127G1A–JM, PW1127G1B–JM, PW1127GA–JM, PW1129G–JM, PW1130G–JM, PW1133G–JM, PW1133GA–JM, PW1428G–JM, PW1428GA–JM,PW1428GH–JM, PW1431G–JM, PW1431GA–JM, and PW1431GH–JM engines with an installed: (i) High-pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR–7) having part number (P/N) 30G2307 or 30G4407; (ii) HPC 8th-stage integrally bladed rotor (IBR–8) having P/N 30G5608, 30G5908, or 30G8908; (iii) HPC rear hub having P/N 30G4008 or 30G8208; (iv) High-pressure turbine (HPT) 1st-stage hub having P/N 30G4201, 30G6201, or 30G7301; or (v) HPT 2nd-stage hub having P/N 30G3902, 30G5502, or 30G6602. (2) This AD does not apply to parts identified in paragraphs (c)(1)(i) through (v) of this AD if thoseparts were manufactured from powdered metal material produced prior to November 1, 2015, or afterSeptember 1, 2021, as identified by part serial number in Tables 1, 2, and 3 of PW Special Instruction(SI) No. 222F–23, Revision B, dated March 1, 2024 (PW SI No. 222F–23, Revision B) or in theoriginal manufacturing records for the part.
(3) If the original manufacturing records do not identify the production date of the powdered metalused to make the parts identified in paragraphs (c)(1)(i) through (v) of this AD, and the part serialnumber is not listed in Tables 1, 2, and 3 of PW SI No. 222F–23, Revision B, then the part is subjectto the requirements of this AD.
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CAA-2024-04-001(已被CAA-2024-05-005取代) |
2024/04/10 |
EASA |
2024-0081 |
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and
ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN.
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CAA-2024-03-014 |
2024/03/27 |
FAA |
2024-06-09 |
This AD applies to the following CFM International, S.A. Model engines: (1) CFM56–2, CFM56–2A, CFM56–2B, CFM56–3, CFM56–3B, and CFM56–3C engines;
(2) CFM56–5, CFM56–5–A1/F, CFM56–5A3, CFM56–5A4, CFM56–5A4/F, CFM56–5A5, and CFM56–5A5/Fengines;
(3) CFM56–5B1, CFM56–5B1/2P, CFM56–5B1/3, CFM56–5B1/P, CFM56–5B2, CFM56–5B2/2P, CFM56–5B2/3, CFM56–5B2/P, CFM56–5B3/2P, CFM56–5B3/2P1, CFM56–5B3/3, CFM56–5B3/3B1, CFM56–5B3/P,CFM56–5B3/P1, CFM56–5B4, CFM56–5B4/2P, CFM56–5B4/2P1, CFM56–5B4/3, CFM56–5B4/3B1,CFM56–5B4/P, CFM56–5B4/P1, CFM56–5B5, CFM56–5B5/3, CFM56–5B5/P, CFM56–5B6, CFM56–5B6/2P,CFM56–5B6/3, CFM56–5B6/P, CFM56–5B7, CFM56–5B7/3, CFM56–5B7/P, CFM56–5B8/3, CFM56–5B8/P,CFM56–5B9/2P, CFM56–5B9/3, and CFM56–5B9/P engines; (4) CFM56–5C2, CFM56–5C2/4, CFM56–5C2/F, CFM56–5C2/F4, CFM56–5C2/G, CFM56–5C2/G4, CFM56–5C2/P, CFM56–5C3/F, CFM56–5C3/F4, CFM56–5C3/G, CFM56–5C3/G4, CFM56–5C3/P, CFM56–
5C4,CFM56–5C4/1, CFM56–5C4/1P, and CFM56–5C4/P engines; and
(5) CFM56–7B20, CFM56–7B20/2, CFM56–7B20/3, CFM56–7B20E, CFM56–7B22, CFM56–7B22/2,CFM56–7B22/3, CFM56–7B22/3B1, CFM56–7B22/B1, CFM56–7B22E, CFM56–7B22E/B1, CFM56–7B24,CFM56–7B24/2, CFM56–7B24/3, CFM56–7B24/3B1, CFM56–7B24/B1, CFM56–7B24E, CFM56–7B24E/B1,CFM56–7B26, CFM56–7B26/2, CFM56–7B26/3, CFM56–7B26/3B1, CFM56–7B26/3B2, CFM56–7B26/3B2F,CFM56–7B26/3F, CFM56–7B26/B1, CFM56–7B26/B2, CFM56–7B26E, CFM56–7B26E/B1, CFM56–7B26E/B2, CFM56–7B26E/B2F, CFM56–7B26E/F, CFM56–7B27, CFM56–7B27/2, CFM56–7B27/3, CFM56–7B27/3B1, CFM56–7B27/3B1F, CFM56–7B27/3B3, CFM56–7B27/3F, CFM56–7B27/B1, CFM56–7B27/B3,CFM56–7B27A, CFM56–7B27A/3, CFM56–7B27AE, CFM56–7B27E, CFM56–7B27E/B1, CFM56–7B27E/B1F,and CFM56–7B27E/B3 engines.
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CAA-2024-03-013 |
2024/03/25 |
EASA |
2024-0073 |
Airbus A350-941 aeroplanes and A350-1041, all manufacturer serial numbers having a date of manufacture on 31 December 2023 or earlier.
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CAA-2024-03-012 |
2024/03/22 |
EASA |
2024-0078 |
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0044, 0049, 0050, 0052, 0055-0057 inclusive, 0060, 0066, 0067, 0073, 0074, 0080, 0082, 0086, 0087, 0091, 0092, 0094, 0095, 0098, 0105, 0111, 0112, 0115, 0117, 0121, 0123, 0124, 0127, 0129, 0130, 0132, 0135, 0136, 0138, 0142, 0143-0146 inclusive, 0149-0151 inclusive, 0153, 0157, 0159, 0160, 0162-0165 inclusive, 0167, 0168, 0172-0179 inclusive, 0181-0185 inclusive, 0187, 0189-0193 inclusive, 0195, 0197-0199 inclusive, 0201-0204 inclusive, 0207-0214 inclusive, 0217, 0218, 0221, 0224, 0228, 0231, 0234-0237 inclusive, 0239, 0240, 0243, 0246, 0247, 0249, 0251, 0255, 0256, 0257, 0260, 0267, 0268, 0270, 0277, 0279, 0280, 0281, 0283-0285 inclusive, 0287, 0292, 0295, 0297 and 0299; and A350-1041 aeroplanes MSN 0065, 0071, 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0258, 0262, 0266, 0274, 0286, 0290, 0296 and 0298.
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CAA-2024-03-011 |
2024/03/22 |
FAA |
2024-04-09 |
This AD applies to The Boeing Company Model 777–200, 777–200LR, 777–300, 777–300ER, and777F series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin777–31A0342 RB, dated July 19, 2021.
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CAA-2023-07-001A |
2024/03/22 |
EASA |
2023-0132R1 |
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0005 through 0046 inclusive, except MSN 0025 and MSN 0033.
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CAA-2024-03-010(已被CAA-2024-03-010修訂取代) |
2024/03/21 |
EASA |
2024-0077 |
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 (MSN), except those having Airbus modification (mod) 151574 embodied in production.
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