CAA-2009-07-011 |
2009/07/21 |
EASA |
2009-0159-E |
Model ATR 42-200, 42-300, 42-320, 42-400 and 42-500 aeroplanes, and
Model ATR 72-101, 72-102, 72-201, 72-202, 72-211, 72-212 and 72-212A
aeroplanes that are equipped with PPG Aerospace cockpit forward side
glass windows part number (p/n) NP158862-1 and/or p/n NP158862-2.
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CAA-2009-07-009 |
2009/07/17 |
ANAC |
2007-02-02R2(BRAZIL) |
This Airworthiness Directive (AD) applies to all Embraer ERJ 190 airplane models equipped with firewall hydraulic shutoff valve (FWSOV) part number (P/N) 975287-3 or 975287-5.
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CAA-2009-07-008 |
2009/07/17 |
EASA |
2009-0153 |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, - 303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers on which Airbus modification 49144 (install rudder fly by wire)
has been embodied in production.
Airbus A340 aeroplanes, models -311, -312, and -313, all manufacturer serial numbers on which Airbus modification 49144 has been embodied in production.
Airbus A340 aeroplanes, models -541, -542, -642, -643, all manufacturer serial numbers.
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CAA-2009-07-007 |
2009/07/14 |
ANAC |
2009-07-02(BRAZIL) |
This Airworthiness Directive (AD) applies to Embraer model ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-200 IGW, ERJ 190-200 LR and ERJ 190-200 STD
airplanes, with serial number 19000002, 19000004, 19000006 thru 19000108, 19000110 thru 19000139,
19000141 thru 19000158, 19000160 thru 19000176, 19000178 thru 19000202, 19000204 thru 19000213,
and 19000215.
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CAA-2009-07-006 |
2009/07/14 |
EASA |
2009-0150 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243 aeroplanes, all manufacturer serial numbers (MSN), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and
A340-313 aeroplanes, all MSN, on which Airbus modification 49520 has been embodied in production or on which Airbus Service Bulletin (SB) A330-21- 3096 Revision 01 or SB A340-21-4107 Revision 01 has been embodied in service, except those on which Airbus modification 58551 has been embodied in production.
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CAA-2009-07-004 |
2009/07/14 |
FAA |
2009-14-05 |
Pratt & Whitney Models PW2037, PW2037(M), and PW2040
Turbofan Engines with the following high-pressure compressor (HPC) drum rotor disk assemblies installed:Drum Rotor Disk Assembly
Part Number 1B3702; 1B3702-
001; 1B3610; 1B3610-001; or
1B7377–Serial Number( ).12th Stage Disk Billet
and Heat Number( ).These engines are installed on, but not limited to, Boeing 757-200 and 757-300 airplanes.
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CAA-2009-07-005 |
2009/07/13 |
EASA |
2009-0148-E |
Agusta S.p.A model A109 series and AB139/AW139 helicopters ,
and
Eurocopter model AS332, AS350, AS355, SA330, SA365, AS365 and EC155
series, EC225 LP and SA360 C helicopters,
and
Eurocopter Deutschland GmbH model EC135, MBB-BK 117 and BO 105 series
helicopters,
and
Sikorsky Aircraft Corporation S-61N helicopters,
all serial numbers, if equipped with Lifesaving Systems D-Lok Hooks with part
numbers (P/N) 410-A or 410-F and identified as part of lot number 208 or 1108.
Note: the rescue hoist P/N provided in the service information of the rescue
hoist system manufacturers (Goodrich or Breeze-Eastern) is for information
only. Refer to Lifesaving Systems D-Lok Hooks P/N to determine AD
applicability.
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CAA-2009-07-003 |
2009/07/11 |
FAA |
2009-14-06 |
Boeing Model 777 airplanes.
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CAA-2009-07-001 |
2009/07/09 |
FAA |
2009-14-08 |
General Electric Company (GE) CF6-80C2B5F turbofan engines with a
high-pressure compressor rotor (HPCR) stages 11-14 spool/shaft, part number (P/N) 1703M74G03,
installed.But not limited to Boeing 747 series airplanes.
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CAA-2009-07-002 |
2009/07/06 |
EASA |
2009-0141 |
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 Carbon Fiber Reinforced
Plastic (CFRP) rudders having part numbers (P/N) and serial numbers
(S/N) as listed in Appendix A to this AD.
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