| CAA-2006-10-001(已有後續修訂版) |
2006/10/04 |
FAA |
2006-20-51 |
777-200LR series airplanes GE90-110B engines and 777-300ER series airplanes GE90-115B engines
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| CAA-2006-09-015 |
2006/10/04 |
FAA |
2006-20-07 |
This AD applies to Rolls-Royce Corporation (RRC) models 250- C30, -C30G, -C30G/2, -C30M, -C30P, -C30R, -C30R/1, -C30R/3, -C30R/ 3M, -C30S, -C30U, -C40B, -C47B, and -C47M turboshaft engines, with a third-stage turbine wheel, part number (P/N) 6898663 or P/N 23065843 installed, or a fourth-stage turbine wheel, P/N 6892764 or P/N 23066744, installed. These engines are installed on, but not limited to, Bell 206L-3, Bell 206L-4, Bell 230, Bell 407, Bell 430, MDHI 369F, MDHI 369FF, MDHI 600N, and Sikorsky S-76A helicopters.
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| CAA-2006-07-017A |
2006/10/04 |
CAA-NL |
NL-2006-009R1 |
Fokker Aircraft B.V. Model F27 Mark 050 aircraft, serial numbers 20103 through 20172
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| CAA-2006-09-014 |
2006/10/02 |
FAA |
2006-19-12 |
Boeing Model 777-200 and -300 series airplanes, certificated in any category; as identified in Boeing Special Attention Service Bulletin 777-54-0021, Revision 1
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| CAA-2006-09-013(已有後續修訂版) |
2006/09/26 |
EASA |
2006-0286-E |
Oxygen Reserve Cylinders having Part Number (P/N) GLF(XXX)-(X),
GLD(XXX)-(X), PC2300 and SLF300, which are known to be installed on,
but not limited to Airbus A300 series aircraft; Dassault Aviation (AMD-BA)
Mystère-Falcon 20, Mystère-Falcon 50, Falcon 200 and Falcon 900
aircraft; Pilatus aircraft; Eurocopter SA 315 B and AS 350 B3 helicopters;
and Hindustan Aeronautics Limited helicopters.
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| CAA-2006-09-012 |
2006/09/26 |
FAA |
2006-19-09 |
This AD affects Model B300 airplanes, serial numbers FL-1 through FL-289, that are certificated in any category.
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| CAA-2002-10-013A(已有後續修訂版) |
2006/09/25 |
EASA |
2006-0288 |
TAY 650-15 Engines, serial numbers 17251, 17255, 17256, 17273,
17275, 17280, 17281, 17282, 17300, 17301, 17327, 17332, 17365,
17393, 17437, 17443, 17470, 17520, 17521, 17523, 17539, 17542,
17556, 17561, 17562, 17563, 17580, 17581, 17612, 17618, 17635,
17637, 17645, 17661, 17686, 17699, 17701, 17702, 17736, 17737,
17738, 17739, 17741, 17742 and 17808 with Module M05300AA (LP
Turbine Module) installed.
These engines are known to be installed in Fokker F28 Mark 0100 aircraft.
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| CAA-2006-09-006 |
2006/09/20 |
FAA |
2006-18-15 |
Hartzell Propeller Inc. ( )HC-( )2Y( )-( ) series propellers with non-suffix serial number (SN) propeller hubs installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines.
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| CAA-2006-09-004 |
2006/09/19 |
FAA |
2006-19-03 |
(c) This AD applies to the McDonnell Douglas airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Model DC-10-10 and DC-10-10F airplanes; Model DC-10-15 airplanes; Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) airplanes; Model DC-10-40 and DC-10-40F airplanes; and Model MD-10- 10F and MD-10-30F airplanes; fuselage numbers (F/Ns) 1 through 446 inclusive.
(2) Model MD-11 and MD-11F airplanes; F/Ns 0447, 0448, 0449, 0451 through 0464 inclusive, 0466 through 0489 inclusive, 0491 through 0517 inclusive, 0519 through 0552 inclusive, and 0554 through 0646 inclusive.
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| CAA-2006-09-011(已有後續修訂版) |
2006/09/18 |
EASA |
2006-0285 |
AIRBUS 310 and A300-600 aircraft, all certified models and all serial numbers.
The applicability for each of the actions required by this directive is identified in each relevant "Action" paragraph of the Compliance-section of this Airworthiness Directive (AD)
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