| CAA-2006-09-016 |
2006/10/12 |
FAA |
2006-20-02 |
This AD applies to 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, certificated in any category; as identified in Boeing Alert Service Bulletin 747- 53A2409, Revision 5, dated August 18, 2005.
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| CAA-2006-10-003(已有後續修訂版) |
2006/10/04 |
FAA |
2006-20-06 |
This AD applies to General Electric Company (GE) CF34- 10E2A1, -10E5, -10E5A1, -10E6, -10E6A1, and -10E7 turbofan engines. These engines are installed on, but not limited to, Embraer ERJ 190- 100-STD, ERJ 190-100-LR, and ERJ 190-100-IGW airplanes.
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| CAA-2006-10-002 |
2006/10/04 |
FAA |
2006-20-09 |
This AD applies to those Lycoming Engines (L)O-360, (L)IO- 360, AEIO-360, O-540, IO-540, AEIO-540, (L)TIO-540, IO-580, and IO- 720 series reciprocating engines listed by engine model number and serial number in Table 1, Table 2, Table 3, or Table 4 of Lycoming Mandatory Service Bulletin (MSB) 569A, dated April 11, 2006, and those engines with crankshafts listed by crankshaft serial number in Table 5 of Lycoming MSB 569A, dated April 11, 2006. These applicable engines are manufactured new or rebuilt, overhauled, or had a crankshaft installed after March 1, 1997.
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| 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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