| 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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| CAA-2006-10-009(已有後續修訂版) |
2006/10/18 |
EASA |
2006-0309 |
AIRBUS A340 aircraft, models -211, -212, -311 and -312, all serial
numbers, except for those on which AIRBUS modification 42445 has
been embodied in production or AIRBUS Service Bulletin (SB) A340-78-
4031 in service.
This applicability is established considering that the aircraft have not
been subject to any replacement of the thrust reverser since delivery or
AIRBUS SB A340-78-4031 embodiment. It is the responsibility of the
operator to check that its aircraft is in compliance with the present
Airworthiness Directive (AD)
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| CAA-2006-10-008 |
2006/10/18 |
EASA |
2006-0303 |
ATR42-500 and ATR72-212A aircraft, fitted with modification n°4440
(composite vertical fin) and on which the modification n°5426 (Service
Bulletin ATR42-55-0012 or ATR72-55-1004) has not been embodied,
except the following serial numbers :
- 618 to 623 inclusive for ATR42-500 model.
- 682, 683, 684, 687 and from 694 to 708 inclusive for ATR72-212A
model.
This Airworthiness Directive (AD) does not affect aircraft modified by SB
ATR42-55-0012 original issue or by SB ATR72-55-1004 original issue.
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| CAA-2006-10-007(已有後續修訂版) |
2006/10/18 |
EASA |
2006-0298 |
AIRBUS A340 aircraft, models -211, -212, -213, -311, -312 and -313, all serial numbers, except those on which AIRBUS modification 54159 has been embodied in production or AIRBUS Service Bulletin (SB) A340-78-4032 Revision 01 has been embodied in service.
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