| CAA-2010-05-004(已有後續修訂版) |
2010/05/06 |
EASA |
2010-0086 |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers, except those on which the three Airbus modifications 58773 and
55923S18878 and 45968 have been embodied in production and Airbus A340 aeroplanes, models -211, -212, -213, -311, -312, -313, all
manufacturer serial numbers, except those on which the three Airbus modifications 58773 and 55923S18878 and 45968 have been embodied in production and Airbus A340 aeroplanes, models -541, -542, -642 and -643, all manufacturer serial numbers, except those on which the three Airbus modifications 58773 and 55924S19452 and 45968 have been embodied in production.
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| CAA-2010-05-003 |
2010/05/06 |
FAA |
2010-09-12 |
McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, DC-10-
15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-
30F, MD-11, and MD-11F airplanes。
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| CAA-2010-05-002(已有後續修訂版) |
2010/05/05 |
EASA |
2010-0083 |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers and
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all manufacturer serial numbers.
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| CAA-2010-05-001 |
2010/05/05 |
Transport Canada Civil Aviation |
CF-2002-26R2 |
Bombardier DHC-8 aircraft, Models 102, 103, 106, 201, 202, 301, 311, 314 and 315, serial numbers 003 and subsequent.
Note: All installed flap drive actuators, Part Numbers 734181, 734374 and 755216, are subject to this revision, irrespective of serial number.
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| CAA-2010-04-014 |
2010/05/03 |
FAA |
2010-09-04 |
This AD applies to Honeywell International Inc., Primus EPIC and Primus APEX flight management systems (FMS), having the FMS part numbers (P/N) listed in Table 1 of this AD, installed on, but not limited to, Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 and ERJ 190 airplanes, and Pilatus Aircraft Ltd. Model PC-12/47E airplanes, certificated in any category.
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| CAA-2010-04-013(已有後續修訂版) |
2010/04/29 |
EASA |
2010-0081 |
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 and A330-343 aeroplanes, all manufacturer serial numbers.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-
313 aeroplanes, all manufacturer serial numbers. The requirements of paragraphs (1), (2) and (4) of the Required action and Compliance Time section of this AD are not applicable to Airbus A330-200 aeroplane on which Airbus modification 53969 or 54833 has
been embodied in production.
The requirements of paragraphs (3.1) and (8) of the Required action and Compliance Time section of this AD are not applicable to:
- Airbus A330-200/-300 aeroplanes on which both Airbus modifications
53468 and 55697 have been embodied in production, and Airbus A340-200/-300 aeroplanes on which both Airbus modifications 55879 and 55697 have been embodied in production.
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| CAA-2010-04-012 |
2010/04/29 |
EASA |
2010-0079 |
Saphir 20 Model 095 Auxiliary Power Units (APU), all serial numbers.
These APUs are known to be installed on, but are not limited to, Eurocopter EC225 and AS332 helicopters.
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| CAA-2010-04-011 |
2010/04/28 |
FAA |
2010-09-05 |
The Boeing Company Model 737-600, -700, -700C, -800, -900, and -
900ER series airplanes.
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| CAA-2010-04-10 |
2010/04/22 |
EASA |
2010-0077 |
All BR700-710A1-10 model engines.
All BR700-710A2-20 model engines.
All BR700-710C4-11 model engines which have hardware configuration
standard 710C4-11 engraved on the engine data plate (Service Bulletin
SB-BR700-72-101466 standard not incorporated). All BR700-710C4-11 model engines which have hardware configuration standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated).
These engines are known to be installed on, but not limited to Gulfstream GV, GV-SP (G500, G550) and Bombardier BD-700-1A10, BD-700-1A11 series aeroplanes.
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| CAA-2010-04-009 |
2010/04/22 |
EASA |
2010-0076 |
All BR700-710C4-11 model engines which have hardware configuration
standard 710C4-11/10 engraved on the engine data plate (Service Bulletin SB-BR700-72-101466 standard incorporated) and if equipped with HP Turbine Discs stage 1 or 2 listed in Table 1 or Table 2 of this AD. These engines are known to be installed on, but not limited to Gulfstream GV-SP (G500, G550) aeroplanes.
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