| CAA-2010-06-013(已有後續修訂版) |
2010/07/05 |
EASA |
2010-0132 |
Airbus A330 aeroplanes, models -243, -243F, -341, -342 and -343, all manufacturer serial numbers on which Airbus modification 56966H16199 has been embodied in production or Airbus Service Bulletin A330-28-3105 has been embodied in service.
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| CAA-2010-06-012 |
2010/07/05 |
EASA |
2010-0131 |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301,
-302, -303, -321, -322, -323, -341, -342 and -343, all anufacturer
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-2010-06-011 |
2010/06/30 |
FAA |
2010-13-09 |
This AD applies to: (1) CFM International CFM56-5, -5B, and -7B series turbofan engines with stage 3 low-pressure turbine (LPT) disks part number (P/N) 336-002-006-0, installed with the following serial numbers (S/Ns), DE255844, DE256388, DE256622, DE256623, DE256625, DE256627, DE256628, DE256631, and DE256637.
(2) CFM International, S.A. has stated that none of these affected disk S/Ns were originally installed on any CFM56-5 turbofan engine, however, that disk P/N is certified for use on CFM56-5 engines. (3) The -5 and -5B series engines are installed on, but not limited to, Airbus A318, A319, A320, and A321 airplanes, and the -7B series engines are installed on, but not limited to, Boeing 737 series airplanes.
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| CAA-2010-06-010 |
2010/06/30 |
FAA |
2010-12-09 |
This AD applies to Honeywell International Inc. Auxiliary Power Unit (APU) models GTCP36-150(R) and GTCP36-150(RR). These APUs are installed on, but not limited to, Fokker Services B.V. Model F.28 Mark 0100, and F.28 Mark 0070 airplanes.
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| CAA-2010-06-009 |
2010/06/29 |
FAA |
2010-13-03 |
The Boeing Company Model 777-200LR and -300ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-57A0069, dated November 5, 2009.
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| CAA-2010-06-008 |
2010/06/29 |
EASA |
2010-0127 |
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, if equipped with rudders having part numbers (P/N) and serial numbers (S/N) as listed in the Appendix A, B or C to this AD.
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| CAA-2010-06-007 |
2010/06/29 |
EASA |
2010-0120 |
Airbus Model A318-111, A318-112, A318-121, and A318-122 aeroplanes;
Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319- 132, and A319-133 aeroplanes; Model A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, and A320-233 aeroplanes, and Model A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, that are equipped with a Hamilton Sundstrand Ram Air Turbine (RAT) model ERPS08M as identified by Part-Number (P/N) in
Hamilton Sundstrand Service Bulletin (SB) ERPS08M-29-8 original issue dated 17 June 2009
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| CAA-2008-11-002A |
2010/06/29 |
EASA |
2008-0199R1 |
Airbus Model A320-111, A320-211, A320-212, A320-214, A320-215, A320-
216, A320-231, A320-232 and A320-233 aeroplanes, all serial numbers
equipped with Hamilton Sundstrand (formerly Dowty) Ram Air Turbine (RAT) Ejection Jack, Model ERPS13EJ, Part Number (P/N) 114160004A or P/N 114160005, except those aeroplanes which have received Airbus modification
27189 in production or Airbus Service Bulletin (SB) A320-29-1100 in service, and without having received Airbus modification 28413 in production.
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| CAA-2010-06-006(已有後續修訂版) |
2010/06/18 |
ANAC |
2010-06-02(BRAZIL) |
This Airworthiness Directive is applicable to Embraer Models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR and ERJ 190-200 IGW airplanes with serial numbers 19000002, 19000004, 19000006 thru 19000108, 19000110 thru 19000139, 19000141 thru 19000157, 19000160, 19000165, 19000167 thru 19000176, 19000178 thru 19000199, 19000273 thru 19000276, 19000279 thru 19000286, 19000288 thru 19000295,19000297 thru 19000304, and 19000309.
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| CAA-2010-06-005 |
2010/06/18 |
EASA |
2010-0116-E |
AS 365 N3, EC 155B and B1 and SA 366 G1 helicopters, all serial
numbers, if equipped with Main Gearbox (MGB) fitted with dual pump
lubrication system that has been subject to removal/installation since 04 November 2004.
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