| CAA-2010-05-004A |
2010/06/18 |
EASA |
2010-0086R1 |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers, except those on which Airbus modifications 58773 and 45968
have been embodied in production and Airbus A340 aeroplanes, models -211, -212, -213, -311, -312, -313, all manufacturer serial numbers, except those on which Airbus modifications 58773 and 45968 have been embodied in production and Airbus A340 aeroplanes, models -541, -542, -642 and -643, all manufacturer serial numbers, except those on which Airbus modifications 58773 and 45968 have been embodied in production.
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| CAA-2010-06-004(已有後續修訂版) |
2010/06/14 |
EASA |
2010-0103 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers,
except those which have embodied in production: both Airbus modifications (mod.) 57349 and 57562, and mod. 55770 or 58924.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and
A340-313 aeroplanes, all manufacturer serial numbers, except those which have embodied in production : both Airbus mod. 57349 and 57562, and - mod. 55770 or 58924.
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| CAA-2010-06-003(已有後續修訂版) |
2010/06/07 |
EASA |
2010-0101-E |
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, and the following helicopters: Eurocopter AS350 series, AS365 and SA365 series, Sikorsky S-76A series
and C series.
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| CAA-2010-06-002 |
2010/06/07 |
FAA |
2010-11-05 |
This AD applies to oxygen cylinders with a capacity of 114/115 cubic feet, approved under United States Department of Transportation Regulations for Type 3HT cylinders, identified in Table 1 of this AD. These oxygen cylinders may be installed on various 14 CFR part 23 and CAR 3 airplanes, certificated in any category. The affected oxygen cylinders may be installed as a component of, but not limited to, the AVOX Systems Inc. and B/E Aerospace cylinder assemblies listed in Table 2 of this AD.
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| CAA-2010-06-001 |
2010/06/07 |
FAA |
2010-11-12 |
McDonnell Douglas Corporation Model MD-11 and MD-11F airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin MD11-28A140, dated November 6, 2008.
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| CAA-2010-04-007A(已被CAA-2013-07-008取代) |
2010/06/01 |
EASA |
2010-0071R1 |
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 aeroplanes, all manufacturer serial numbers.
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| CAA-2010-01-011A |
2010/05/28 |
ANAC |
2010-01-02R1(BRAZIL) |
This Airworthiness Directive (AD) is applicable to Embraer models ERJ 190-100 ECJ, ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-100 SR, ERJ 190-200 IGW, ERJ 190- 200 LR and ERJ 190-200 STD airplanes equipped with Air Management System (AMS) controller cards part number (P/N) 1001050-1-YYY or P/N 1001050-2-YYY containing software version Black Label 08 or lower installed.
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| CAA-2009-08-010A |
2010/05/28 |
ANAC |
2009-08-02R1(BRAZIL) |
This Airworthiness Directive (AD) is applicable to EMBRAER models ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 LR, ERJ 190- 200 STD and ERJ 190-200 IGW airplanes equipped with Goodrich Corporation door-mounted escape slide part number (P/N) 104003-1.
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| CAA-2006-11-004E(已有後續修訂版) |
2010/05/28 |
ANAC |
2006-11-01R5 |
This Airworthiness Directive is applicable to Embraer models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR e ERJ 190-200 IGW airplanes equipped with Hamilton Sundstrand Low Pressure Check Valve (LPCV) part numbers (P/N) 1001447-3 and/or 1001447-4.
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| CAA-2010-05-010(已有後續修訂版) |
2010/05/27 |
EASA |
2010-0100-E(BRAZIL) |
SA 365 N1, AS 365 N2, N3 helicopters 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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