| CAA-2022-02-008修訂 |
2022/03/04 |
FAA |
2022-02-03Correction |
CFM International, S.A. CFM56-3 and CFM56-7B model turbofan engines equipped with an accessory gearbox (AGB) assembly with the following part numbers (P/Ns):
(1) For CFM56-3, CFM56-3B, and CFM56-3C model turbofan engines, AGB P/N: 335-300-103-0, 335-300-105-0, 335-300-106-0, 335-300-107-0, 335-300-108-0, 335-300-109-0, or 335-300-110-0, installed.
(2) For CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/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, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1, and CFM56-7B27/B3 model turbofan engines, AGB P/N: 340-046-503-0, 340-046-504-0, or 340-046-505-0, installed.
(3) For CFM56-7B27A, CFM56-7B27A/3, or CFM56-7B27AE model turbofan engines, AGB P/N: 340-188-601-0, 340-188-603-0, or 340-188-605-0, installed.
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| CAA-2022-02-005A(已有後續修訂版) |
2022/03/04 |
EASA |
2022-0025R1 |
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 and A330-343 aeroplanes, all manufacturer serial numbers (MSN),
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-2020-10-018A |
2022/03/04 |
EASA |
2020-0227R1 |
ATR 72-212A aeroplanes, manufacturer serial numbers (MSN) 1165 to 1627 inclusive, except those on which ATR modification (mod) 10052 has been embodied in production, and except MSN 1589, 1591, 1592 and 1595.
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| CAA-2022-02-015 |
2022/03/01 |
Transport Canada Civil Aviation |
CF-2022-05 |
Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70006, 70007, 70009 through 70019, 70021 through 70029, and 70031.
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| CAA-2022-02-014(已被CAA-2023-06-008取代) |
2022/02/25 |
FAA |
2022-05-04 |
Boeing Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, except for Model 737-200 and -200C series airplanes equipped with an SP-77 flight control system.
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| CAA-2022-02-013 |
2022/02/25 |
FAA |
2022-02-14 |
Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin B787-81205-SB320045-00 RB, Issue 001, dated November 9, 2020.
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| CAA-2022-02-012 |
2022/02/25 |
EASA |
2022-0028 |
Airbus A319-151N, A319-153N, A319-171N, 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-2022-02-011 |
2022/02/23 |
Japan CAB |
TCD-9876-2022 |
Kawasaki BKll7, BKll7 A-3, BKll7 A-4, BKll7 B-1, BKll7 B-2, BKll7 C-1 and BKll7 C-2 helicopters.
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| CAA-2022-02-010(已被CAA-2023-02-001取代) |
2022/02/23 |
EASA |
2022-0026 |
Airbus 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, A320-251N, A320-271N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N and A321-253N aeroplanes, all manufacturer serial numbers (MSN), if equipped with an affected galley, as identified by Part Number (P/N) and serial number (s/n) in Table 1 and Table 2 of Appendix 1 of this AD, or as identified by P/N in Tables 3, 4 or 5 of Appendix 1 of this AD.
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| CAA-2022-02-009 |
2022/02/23 |
FAA |
2022-03-15 |
all serial numbers of the airplane models listed in table 1 to paragraph (c), certificated in any category, that are either:
(1) Modified with a Garmin G3X Touch Electronic Flight Instrument System under Supplemental Type Certificate No. SA01899WI, installed in accordance with Master Drawing List Document No. 005-01320-00, Revision 9 or earlier, interfaced with a Garmin Engine Adapter GEA 24 connected to resistive fuel probes; or
(2) Modified with a Garmin GI 275 Multi-Function Display under STC No. SA02658SE, installed in accordance with MDL Revision 9 or earlier, interfaced with a Garmin Engine Adapter GEA 24 connected to resistive fuel probes.
Note 1 to paragraph (c): Garmin Mandatory STC Service Bulletin No. 2134, Revision A, and Garmin Mandatory STC Service Bulletin No. 2135, Revision A, both dated April 23, 2021, contain information for how to determine if your airplane has a resistive probe interface.
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