| CAA-2009-11-004 |
2009/11/11 |
EASA |
2009-0245-E |
Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K, 1K1, 1S and 1S1
turbo-shaft engines, all serial numbers if modified by TU332 and fitted with
Modules M05 (Reduction Gear Box) as identified in figure 1 of Turbomca
Mandatory Service Bulletin (MSB) A292 72 0825 version B.
These engines are known to be installed on, but not limited to, the
following helicopters:
Eurocopter AS350B/BA/BB/B1/B2, EC145/MBB-BK117-C1 and AS365N,
Agusta A109K2, Sikorsky S-76A+ and S-76A++.
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| CAA-2009-11-003 |
2009/11/11 |
EASA |
2009-0240 |
Airbus A330 aeroplanes, models -223, -321, -322 and -323, all
manufacturer serial numbers.
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| CAA-2009-11-002(已有後續修訂版) |
2009/11/06 |
EASA |
2009-0241-E |
AS365 N1, N2 and N3 helicopters, all serial numbers flying in IMC (Instrumental
Meteorological Conditions), IFR (Instrument Flight Rules) or Night VFR (Visual
Flight Rules) conditions, if equipped with the vertical gyro units GV 76-1 installed
on the rear left-hand (LH) or the rear right-hand (RH) rack.
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| CAA-2009-10-013 |
2009/11/06 |
EASA |
2009-0235 |
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 aeroplanes, all manufacturer
serial numbers, except aeroplanes that have received Airbus modification (MOD) 37317 in production.
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| CAA-2009-11-001(已有後續修訂版) |
2009/11/02 |
EASA |
2009-0237-E |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, -
303, -321, -322, -323, -341, -342 and -343 aeroplanes, all manufacturer
serial numbers on which Airbus modification 48809 has been embodied in
production, if delivered before 26 October 2009.
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313
aeroplanes, all manufacturer serial numbers on which Airbus modification
48809 has been embodied in production, if delivered before 26 October
2009.
Airbus A340 aeroplanes, models -541, -542, -642 and -643, all
manufacturer serial numbers, if delivered before 26 October 2009.
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| CAA-2009-10-012 |
2009/11/02 |
FAA |
2009-22-08 |
Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes.Boeing Model 757-200, -200PF, and -300 series airplanes,
certificated in any category.
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| CAA-2009-10-011 |
2009/10/30 |
FAA |
2009-22-03 |
This AD applies to Hartzell Propeller Inc. ()HC-()2Y(K,R)-() series propellers with nonsuffix
serial number (SN) propeller hubs and propeller hubs suffix SN letter ''E'', installed on
Lycoming O-, IO-, LO-, LIO-, TO-, LTO-, AIO-, AEIO-, and TIO-360 series reciprocating engines
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| CAA-2009-10-010 |
2009/10/30 |
FAA |
2009-22-06 |
International Aero Engines AG (IAE) V2500-A1, V2527E-A5, V2530-
A5, and V2528-D5 turbofan engines. These engines are installed on, but not limited to, Airbus A320
and A321 series, and McDonnell Douglas Corporation MD-90 airplanes.
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| CAA-2009-10-009(已有後續修訂版) |
2009/10/30 |
FAA |
2009-21-07 |
General Electric Company (GE) CF6-80C2 series turbofan engines with
thrust reverser ballscrew gearbox assembly adjustable-length end actuators having 3/8-inch rod-ends
installed. These engines are installed on, but not limited to, Airbus A300-600/R/F and A310-200/300,
and Boeing 747-200B/300/400/400D/400F, 767-200/300/300F/400ER, and MD-11 airplanes.
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| CAA-2009-10-008 |
2009/10/22 |
FAA |
2009-21-03 |
Hamilton Sundstrand Power Systems T-62T-46C12 auxiliary power units
(APUs). These APUs are installed on, but not limited to, Bombardier Inc. DHC-8-400 series
airplanes.
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