| CAA-2010-08-001 |
2010/08/16 |
FAA |
2010-16-05 |
The Boeing Company 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; line numbers 1 through 1229 inclusive.
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| CAA-2010-05-010A修訂 |
2010/08/16 |
EASA |
2010-0100R1Correction |
SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers except 6698, 6701, 6723, 6737 and 6741, delivered before 01 May 2010, flying in IMC (Instrumental Meteorological Conditions), IFR (Instrument Flight Rules) or Night
VFR (Visual Flight Rules) conditions, if equipped with the vertical gyro units GV76-1 installed on the rear left hand (LH) or rear right hand (RH) rack, on which modification 365P081895 (reinforcement of rack for vertical gyro unit GV76-1 in the rear compartment) has not been incorporated.
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| CAA-2010-08-005 |
2010/08/09 |
FAA |
2010-16-03 |
McDonnell Douglas Corporation Model MD-11 and MD-11F airplanes, certified in any category, equipped with General Electric CF6-80C2 series engines.
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| CAA-2010-08-004(已有後續修訂版) |
2010/08/09 |
EASA |
2010-0165 |
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112,
A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-
111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231,
A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-
212, A321-213, A321-231 and A321-232 aeroplane models, all manufacturer serial numbers and The affected oxygen masks P/N are known to be installed on, but not limited to A320 family aeroplanes.
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| CAA-2010-08-003 |
2010/08/09 |
EASA |
2010-0164 |
AIRBUS A318-111, A318-112, A318-121, A318-122, A319-111, A319-112,
A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111,
A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232,
A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213,
A321-231 and A321-232 aeroplane models, all manufacturer serial numbers, if equipped with rudders having part numbers (P/N) and serial numbers (S/N) as listed in Appendix A, B, C, D, or E to this AD.
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| CAA-2010-07-001A |
2010/08/09 |
FAA |
2009-15-16R1 |
McDonnell Douglas Corporation Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F airplanes, Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, and DC-9-32F (C-9A, C-9B) airplanes, Model DC-9-81 (MD-81) airplanes, Model DC-9-82 (MD-82) airplanes, Model DC-9-83 (MD-83) airplanes, Model DC-9-87 (MD-87) airplanes, Model MD-88 airplanes,airplanes; and Model MD-90-30 airplanes, airplanes; certificated in any category; equipped with flight deck doors installed in accordance with Supplemental Type Certificate ST02463AT.
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| CAA-2010-06-006A |
2010/08/09 |
ANAC |
2010-06-02R1(BRAZIL) |
This Airworthiness Directive is applicable to Embraer Models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR and ERJ 190-200 IGW airplanes with serial numbers 19000002, 19000004, 19000006 thru 19000108, 19000110 thru 19000139, 19000141 thru 19000157, 19000160, 19000165, 19000167 thru 19000176, 19000178 thru 19000199, 19000273 thru 19000276, 19000279 thru 19000286, 19000288 thru 19000295,19000297 thru 19000304, and 19000309.
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| CAA-2010-06-003A(已有後續修訂版) |
2010/08/09 |
EASA |
2010-0101R1 |
Arriel 1A, 1A1, 1B, 1C, 1C1, 1C2, 1D, 1D1 and 1S1 turbo-shaft engines, all serial numbers if modified by TU347 and These engines are known to be installed on, but not limited to, the following helicopters: Eurocopter AS350 series, AS365 and SA365 series, Sikorsky S-76A series
and C series.
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| CAA-2010-05-010A(已有後續修訂版) |
2010/08/09 |
EASA |
2010-0100R1 |
SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers except 6698, 6701, 6723, 6737 and 6741, delivered before 01 May 2010, flying in IMC (Instrumental Meteorological Conditions), IFR (Instrument Flight Rules) or Night
VFR (Visual Flight Rules) conditions, if equipped with the vertical gyro units GV76-1 installed on the rear left hand (LH) or rear right hand (RH) rack, on which modification 365P081895 (reinforcement of rack for ertical gyro unit GV76-1 in the rear compartment) has not been incorporated.
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| CAA-2010-07-020 |
2010/07/28 |
EASA |
2010-0152 |
Crew Oxygen Mask Regulator part number (P/N) MC10-02-60; Oxygen Mask Regulator with detachable Goggles P/N MLD20-507, MLD20-
518, MLD20-543 and MLD20-548;
Full Face Quick Donning Mask Regulator P/N MF10-06-05, MF10-06-12, MF20-548 and MF20-554 and
These devices are known to be installed on, but not limited to, the following aeroplane types:
‧ Bombardier BD-700-1A10- (Global Express) and Gulfstream GIV-X (G450) and GV-SP (G550)
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