| CAA-2010-12-007 |
2010/12/23 |
EASA |
2010-0264 |
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.
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| CAA-2010-12-006 |
2010/12/21 |
FAA |
2010-24-14 |
Pratt & Whitney turbofan engines with a ring case configuration rear high-pressure compressor (HPC) installed, that includes a 9th stage compressor stator segment assembly with 24 slots. These engines are installed on, but not limited to, Boeing 747-400/-400F, 767-200/-300, and MD-11 airplanes, and Airbus A300-600, A310-300, A330-300, and A330-200 airplanes.
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| CAA-2010-12-005 |
2010/12/18 |
FAA |
2010-26-03 |
Affected airplane models and serial numbers:B200
BB-1926, BB-1978, and BB-1988 through BB-2000;and BB-1988 through BB-2000
B200GT
BY-1 through BY-26;B300
FL-427, FL-493, and FL-500 through FL-573;B300C (C-12W)
FM-14 through FM-18.
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| CAA-2010-12-004 |
2010/12/18 |
FAA |
2010-24-12 |
For Model –
Boeing –
777-200, -300, and -300ER airplanes
Service Bulletin 777-57A0050, Revision 2.777-200 and -300 airplanes
Alert Service Bulletin 777-57A0051.777-200, -300, and -300ER airplanes
Alert Service Bulletin 777-57A0057, Revision 1.777-200, -300, and -300ER airplanes
Alert Service Bulletin 777-57A0059.
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| CAA-2010-12-003 |
2010/12/13 |
FAA |
2010-25-04 |
McDonnell Douglas Corporation Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C-9A, C-9B), DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes; certificated in any category; as identified in Boeing Service Bulletins DC9-28-212 and MD90-28-010, both Revision 1, both dated June 16, 2009.
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| CAA-2006-12-004A修訂 |
2010/12/13 |
EASA |
2006-0368R1Correction |
SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and
EC 155 B1 helicopters, all serial numbers, fitted with a mast nut Part Number (P/N) 360A31-1020-20 installed in main rotor mast assemblies.
Note:
This AD does not apply to helicopters that have modifications (MOD) 0762B88
and/or MOD 0762C42 embodied in-production or EUROCOPTER Service
Bulletin No. 62-007 embodied in service as applicable to helicopter type. Embodiment of these modifications consists in replacement of mast nut P/N
360A31-1020-20 by mast nut P/N 365A31-2060-20 or P/N 365A31-2060-21, as applicable to helicopter type.
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| CAA-2010-12-002 |
2010/12/08 |
EASA |
2010-0253 |
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, -313, -541, -542, -642 and -643, all manufacturer serial numbers.
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| CAA-2010-10-009A |
2010/12/08 |
EASA |
2010-0211R1 |
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all manufacturer serial numbers.
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| CAA-2010-12-001 |
2010/12/03 |
FAA |
2010-24-11 |
The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes, certificated in any category; as identified in Boeing Service Bulletin 737-57A1279, Revision 2, dated February 2, 2010.
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| CAA-2006-12-004A(已有後續修訂版) |
2010/12/03 |
EASA |
2006-0368R1 |
SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and
EC 155 B1 helicopters, all serial numbers, fitted with a mast nut Part Number (P/N) 360A31-1020-20 installed in main rotor mast assemblies.
Note:
This AD does not apply to helicopters that have modifications (MOD) 0762B88
and/or MOD 0762C42 embodied in-production or EUROCOPTER Service
Bulletin No. 62-007 embodied in service as applicable to helicopter type. Embodiment of these modifications consists in replacement of mast nut P/N
360A31-1020-20 by mast nut P/N 360A31-2060-20 or P/N 360A31-2060-21, as applicable to helicopter type.
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