| CAA-2021-06-002(已被CAA-2022-08-019取代) |
2021/06/07 |
EASA |
2021-0136 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, 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 (MSN); and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542,
A340-642 and A340-643 aeroplanes, all MSN.
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| CAA-2021-06-001 |
2021/06/07 |
EASA |
2021-0135 |
Model 737-700, 737-800, 747-400, 747-8, 767-400ER and 777-200 aeroplanes, manufacturer serial numbers (MSN) 28551, 28961, 29953, 30791, 30884, 32445, 32575, 32915, 32970, 32971, 33010, 33102, 33361, 33684, 34205, 37500 and 37544, if modified by a Lufthansa Technik AG (LHT) STC as identified in Appendix 1 of this AD.
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| CAA-2019-03-007A |
2021/05/28 |
CAA |
CAA-2019-03-007 |
Model 737-8 and 737-9 airplanes (Boeing 737 MAX), certificated in any category.
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| CAA-2021-05-008緊急 |
2021/05/24 |
FAA |
2021-11-51 |
V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 model turbofan engines with: (1) A high-pressure turbine (HPT) 1st-stage disk, part number (P/N) 2A5001, with serial number, PKLBR34908, PKLBR59989, PKLBR83471, PKLBSC9996, PKLBSG0105, PKLBSG9043 or PKLBSH1829, installed; or
(2) An HPT 2nd-stage disk, P/N 2A4802, with S/N PKLBR87800, PKLBR88708 PKLBR89452, PKLBSA9907, PKLBSH9246, PKLBSC8066, PKLBSC8077, or PKLBSG2213, installed.
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| CAA-2021-05-007(已被CAA-2023-04-004取代) |
2021/05/24 |
FAA |
2021-10-09 |
CFM56-5B1, -5B1/2P, -5B1/3, -5B1/P, -5B2, -5B2/2P, -5B2/3, -5B2/P, -5B3/2P, -5B3/2P1, -5B3/3, -5B3/3B1, -5B3/P, -5B3/P1, -5B4, -5B4/2P, -5B4/2P1, -5B4/3, -5B4/3B1, -5B4/P, -5B4/P1, -5B5, -5B5/3, -5B5/P, -5B6, -5B6/2P, -5B6/3, -5B6/P, -5B7, -5B7/3, -5B7/P, -5B8/3, -5B8/P, -5B9/2P, -5B9/3, -5B9/P, CFM56-7B20, -7B20/2, -7B20/3, -7B20E, -7B22, -7B22/2, -7B22/3, -7B22/3B1, -7B22/B1, -7B22E, -7B22E/B1, -7B24, -7B24/2, -7B24/3, -7B24/3B1, -7B24/B1, -7B24E, -7B24E/B1, -7B26, -7B26/2, -7B26/3, -7B26/3B1, -7B26/3B2, -7B26/3B2F, -7B26/3F, -7B26/B1, -7B26/B2, -7B26E, -7B26E/B1, -7B26E/B2, -7B26E/B2F, -7B26E/F, -7B27, -7B27/2, -7B27/3, -7B27/3B1, -7B27/3B1F, -7B27/3B3, -7B27/3F, -7B27/B1, -7B27/B3, -7B27A, -7B27A/3, -7B27AE, -7B27E, -7B27E/B1, -7B27E/B1F, -7B27E/B3, and -7B27E/F model turbofan engines with a high-pressure turbine (HPT) inner stationary seal, part number (P/N) 1808M56G01 installed that has a serial number (S/N) listed in Planning Information, Paragraph 1.A., Table 1, of CFM Service Bulletin (SB) CFM56-5B S/B 72-0952, Revision 01, dated January 15, 2020, or in Planning Information, Paragraph 1.A., Table 1, CFM SB CFM56-7B S/B 72-1054, Revision 01, dated January 15, 2020, installed.
and This AD does not apply to affected CFM CFM56-5B and CFM56-7B model turbofan engines with the affected HPT inner stationary seal installed if the seal has been repaired as specified in CFM56-5B Engine Shop Manual (ESM), 72-41-03, REPAIR 003, or CFM56-7B ESM, 72-41-03, REPAIR 003, after the year listed in Paragraph 1.A., Table 1, of CFM SB CFM56-5B S/B 72-0952, Revision 01, dated January 15, 2020, or Paragraph 1.A., Table 1, CFM SB CFM56-7B S/B 72-1054, Revision 01, dated January 15, 2020.
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| CAA-2021-05-006(已有後續修訂版) |
2021/05/24 |
EASA |
2021-0130 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
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| CAA-2020-11-008A |
2021/05/24 |
Transport Canada Civil Aviation |
CF-2020-49R1 |
model BD-700-1A10 and BD-700-1A11 aeroplanes, serial numbers 9001 through 9879, 9998 and 60001 through 60033.
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| CAA-2021-05-005 |
2021/05/18 |
EASA |
2021-0128 |
Airbus A330-243, A330-243F, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial
numbers.
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| CAA-2007-10-002取消 |
2021/05/17 |
EASA |
2007-0256-CN |
Pacific Scientific rotary buckles, having Part Number (P/N) 1111430-XX or P/N 1111475-XX,
manufactured between November 2004 through May 2007 inclusive.
These rotary buckles are used on TSO-C114 approved Pacific Scientific restraint systems, having P/N 2000029-01, P/N 2000029-03, P/N 2000029-101, P/N 2000029-121, P/N 2000067-01, P/N 2000115-101 and P/N 2000115-121.
These P/N restraint systems are known to be installed on, but not limited to, Airbus Helicopters
type AS 350, AS 355, EC120, EC130 and EC155 helicopters.
EASA AD 2007-0256 applied only to these buckles when installed on rotorcraft, and was not
intended for aeroplanes.
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| CAA-2021-05-004 |
2021/05/14 |
EASA |
2021-0127 |
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, except those that
have embodied Airbus modification (mod) 114420 in production.
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