| CAA-2002-04-012A |
2007/03/15 |
FAA |
2007-05-17 |
Pratt & Whitney (PW) JT9D-3A, -7, -7A, -7H, -7AH, -7F, -7J, -20J, -
59A, -70A, -7Q, -7Q3, -7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, -7R4G2, and -7R4H1 series.
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| CAA-2007-03-004 |
2007/03/12 |
EASA |
2007-0059 |
All Honeywell CAS67A ACASII System installed on Dornier 228 series aircraft in
accordance with Luftfahrtbundesamt (LBA) Supplemental Type Certificate
No.SA1310 before 31 January 2005.
This design change is approved for Dornier Model 228-100, 228-101, 228-200,
228-201 and 228-212 aircraft, all serial numbers.
Note: Dornier 228 series aircraft, serial numbers (S/N’s) 8191, 8232, 8233, 8244
and 8245 have already been modified and are therefore not affected by this
airworthiness directive.
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| CAA-2007-03-002 |
2007/03/12 |
FAA |
2007-05-14 |
GE CF6-80C2 series turbofan engines.
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| CAA-2007-03-001(已有後續修訂版) |
2007/03/07 |
Transport Canada Civil Aviation |
CF-2007-02 |
Bell Helicopter Textron Canada (BHTC) Model 206 series helicopters that have the following Transmission Pylon Support Spindle Part Number (P/N) 206-031-554 (Spindle) serial numbers installed:
B12-11568, B12-12244, B12-12260, B12-12647, B12-12676, B12-12847, B12-13292, B12-14395, B12-15750, B12-17149, B12-17266, B12-1828, B12-18649, B12-19330, B12-19381, B12-20668, B12-2224, B12-2286, B12-3595, B12-3774, B12-3808, B12-5171, B12-757, B12-8053, B12-8605, B12-932, B-21223, B-21297, B22005, B22515, B-22558, CAI3852, CAI3853, EA287, EA318, EA322, EA393, EA751,EA-761, MW546, RE1044, RE113, RE743.
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| CAA-2005-05-005A |
2007/03/02 |
CAA-NL |
NL-2005-005R1 |
Fokker Aircraft B.V. Model Fokker F28 Mark 0100 aircraft serial numbers 11244 thru 11486, 11488 thru 11491, 11496, 11498 thru 11502, 11504 thru 11507, 11511 thru 11520, 11522, 11523 and 11527, except those modified per Fokker SB F100-25-070 (Jet Line Interior configuration) or Fokker SBF100-25-109 (Future Interior). If aircraft serial numbers 11359, 11361, 11367, 11396, 11397, 11404, 11446, 11456, 11468, 11483, 11490, 11499, 11502, 11515 and 11520 are post- report FS-N545 or FS-N571, this AD is not applicable.
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| CAA-2007-02-009 |
2007/03/01 |
CAA-NL |
NL-2007-001 |
Fokker Aircraft B.V. Model F28 Mark 0070 and F28 Mark 0100, serial numbers 11244 thru 11585 if equipped with Messier-Dowty main landing gears (MLG), (effectively in a pre-SBF100-32-090 or post-SBF100-32-129 configuration), including units held as spares.
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| CAA-2007-02-007(已有後續修訂版) |
2007/03/01 |
FAA |
2007-04-19 |
The FAA is adopting a new airworthiness directive (AD) for certain SAP cast cylinder assemblies installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines, Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines, Avco Lycoming (AL) 540 series reciprocating engines, and Superior Air Parts, Inc. (SAP) 360 series reciprocating engines.
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| CAA-2004-11-008修訂 |
2007/03/01 |
FAA |
2004-23-02 Correction |
Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes
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| CAA-2002-06-019A |
2007/03/01 |
CAA-NL |
NL-2002-062R1 |
Fokker Aircraft B.V. Model Fokker F28 Mark 0070 and Fokker F28 Mark 0100, all serial numbers.
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| CAA-2002-06-018A |
2007/03/01 |
CAA-NL |
NL-2002-061R1 |
Fokker Aircraft B.V. Model F27 Mark 050, Mark 0502 and Mark 0604, all serial numbers.
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