| CAA-2011-08-013(已有後續修訂版) |
2011/08/30 |
EASA |
2011-0155 |
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, A320-111,
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 aeroplane models, all manufacturer serial numbers
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| CAA-2011-08-012(已有後續修訂版) |
2011/08/29 |
EASA |
2011-0154 |
EC 155 B, EC 155 B1, SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3 and SA 366 G1 helicopters, all serial numbers except helicopters on which MOD 0767B65 has been embodied in-production or having embodied MOD 0767B65 in-service through accomplishment of Eurocopter AS365 Service Bulletin (SB) No. 67.00.12. or SA 366 SB No. 67.07 or EC 155 SB No. 67-009 Revision 1, as applicable to helicopter version.
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| CAA-2011-08-011 |
2011/08/26 |
FAA |
2011-17-11 |
This AD applies to The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes, certificated in any category; as identified in Boeing Alert Service Bulletin MD80-57A242, Revision 1, dated January 7, 2011.
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| CAA-2011-08-010 |
2011/08/26 |
FAA |
2011-18-02 |
This AD applies to General Electric Company (GE) CF34-10E2A1; CF34-10E5; CF34-10E5A1; CF34-10E6; CF34-10E6A1; CF34-10E7; and CF34-10E7-B turbofan engines, with a fan rotor spinner part number (P/N) 2050M34G03; 2050M34G04; 2050M34G05; 2050M34G06; 2437M60G01; or 2437M60G02, installed.
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| CAA-2011-08-009 |
2011/08/19 |
Transport Canada Civil Aviation |
CF-2011-32 |
Bombardier Inc. DHC-8 Aeroplanes:
Models 102, 103, 106, 201, 202, 301, 311, 314 and 315, Serial Numbers 003 through 672 Models 400, 401 and 402, Serial Numbers 4003 through 4372
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| CAA-2011-08-008 |
2011/08/19 |
Transport Canada Civil Aviation |
CF-2011-31 |
Bombardier Inc. DHC-8 Aeroplanes:
Models 102, 103, 106, 201, 202, 301, 311, 314 and 315, serial numbers 413, 443, 450 through 452, 456, 458, 462 through 465, 467 through 470 and 473 through 588.
Models 400, 401 and 402, serial numbers 4001, 4003 through 4006 and 4008 through 4197.
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| CAA-2011-08-007(已有後續修訂版) |
2011/08/19 |
FAA |
2011-18-51 |
Applies to all Honeywell international, Inc. TPE331 model turboprop engines with a Dixie Aerospace, LLC main shaft bearing, P/N 3108098-1WD, installed.
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| CAA-2011-08-006 |
2011/08/19 |
Japan CAB |
TCD-7916-2011 |
Kawasaki BK117, BK117 A-3, BK117 A-4, BK117 B-1, BK117 B-2 and BK117 C-1 helicopters
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| CAA-2010-08-004B |
2011/08/19 |
EASA |
2010-0165-CN |
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, A320-111,
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 aeroplane models, all manufacturer serial numbers.
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| CAA-2011-08-005 |
2011/08/09 |
FAA |
2011-16-06 |
This AD applies to The Boeing Company Model 747-400 and -400F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-25A3588, Revision 1, dated April 7, 2011.
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