| CAA-2003-02-017A |
2006/10/31 |
FAA |
2006-22-05 |
This AD applies to aircraft, certificated in any category, equipped with a Honeywell Primus II RNZ-850( )/-851( ) integrated navigation unit (INU) having a part number identified in Table 1 of this AD; including, but not limited to, BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes; Bombardier Model BD-700- 1A10 series airplanes; Model Bombardier CL-215-6B11 (CL-415 variant) series airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault Model Mystere-Falcon 50 series airplanes; AvCraft Dornier Model 328-100 and -300 series airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 airplanes and Model EMB- 145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; Learjet Model 45 airplanes; Raytheon Model Hawker 800XP and Hawker 1000 airplanes; and Sikorsky Model S-76A, S-76B, and S-76C aircraft.
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| CAA-2006-10-014(已有後續修訂版) |
2006/10/30 |
EASA |
2006-0322 |
AIRBUS A330, A340-200 and A340-300 aircraft, all certified models, all serial
numbers.
Note : Applicability for each of the actions rendered mandatory is defined in
Compliance section of this Airworthiness Directive (AD)
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| CAA-2006-10-015 |
2006/10/25 |
EASA |
2006-0324-E |
AIRBUS aircraft A330, A340-200 and A340-300 series, all certified
models, all serial numbers fitted with MLG retraction link Part Number
(PN) 201489311 (LH side) or PN 201489312 (RH side).
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| CAA-2006-10-013 |
2006/10/25 |
FAA |
2006-21-09 |
This AD applies to Boeing Model 777-200 series airplanes equipped with General Electric GE90-94B engines; certificated in any category; as identified in Boeing Alert Service Bulletin 777- 78A0056, dated April 20, 2006.
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| CAA-2006-10-012 |
2006/10/25 |
FAA |
2006-21-05 |
Model 747-400, 777-200, and 777-300 series airplanes, certificated in any category; as identified in Boeing Service Bulletin 747-21A2414, Revision 3, dated May 12, 2006; and Boeing Service Bulletin 777-21A0048, Revision 3, dated May 12, 2006.
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| CAA-2002-11-017B |
2006/10/25 |
FAA |
2006-17-07R1 |
This AD applies to the following Pratt & Whitney (PW) JT8D- 1, -1A, -1B, -7, -7A, -7B, -9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR, -209, -217, -217A, -217C, and -219 turbofan engines, with 8th stage high pressure compressor (HPC) front hubs
These engines are installed on, but not limited to, Boeing DC-9, MD-80 series, 727 series, and 737 series airplanes.
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| CAA-2005-09-016B(已有後續修訂版) |
2006/10/23 |
EASA |
2006-0321-E |
All Model SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, SA 365 C,
SA 365 C1, SA 365 C2 and SA 365 C3 helicopters, all serial numbers, equipped
with main rotor hub (MRH) Starflex stars (all part numbers).
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| CAA-2006-10-011(已有後續修訂版) |
2006/10/19 |
EASA |
2006-0315 |
AIRBUS A330 aircraft, models -201, -202, - 203, - 223, -243, -301, -321, -
322, -323, -341, -342 and -343, all serial numbers, except those on which
AIRBUS modification 49202 has been embodied in production or AIRBUS
Service Bulletin (SB) A330-57-3090 has been embodied in service.
AIRBUS aircraft A340-200 and A340-300 series, all certified models, all
serial numbers, except those on which AIRBUS modification 49202 has
been embodied in production or AIRBUS Service Bulletin (SB) A340-57-
4098 has been embodied in service.
This Airworthiness Directive (AD) is not applicable to A340-200/-300
aircraft repaired in accordance with Repair Drawing R57115053 or
R57115051 or R57115047 (installation of Titanium Doubler) which are
covered by EASA AD 2006 - 0314.
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| CAA-2004-12-014A |
2006/10/19 |
EASA |
2006-0314 |
AIRBUS A340 aircraft, models -211, -212, -311 and -312, serial numbers
0006, 0007 (RH side only), 0008 (LH side only), 0013, 0020, 0024 (LH
side only), 0027 through 0029, 0031, 0033, 0035, 0038 through 0040,
0043, 0047, 0049 and 0052.
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| CAA-2006-10-010 |
2006/10/18 |
EASA |
2006-0313 |
AIRBUS A330 aircraft, all certified models, all serial numbers, on which
AIRBUS modification 49144 (install rudder fly by wire) has been embodied in
production except those on which AIRBUS modification 55185 has been
embodied in production or AIRBUS Service Bulletin (SB) A330-27-3142 has
been embodied in service.
AIRBUS aircraft A340-200 and A340-300 series, all certified models, all
serial numbers, on which AIRBUS modification 49144 has been embodied in
production except those on which AIRBUS modification 55185 has been
embodied in production or AIRBUS SB A340-27-4142 has been embodied in
service.
AIRBUS aircraft A340-500 and A340-600 series, all certified models, all
serial numbers, except those on which AIRBUS modification 55186 has
been embodied in production or AIRBUS SB A340-27-5036 has been
embodied in service.
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