| CAA-2014-05-007 |
2014/06/03 |
FAA |
2014-09-07 |
This AD applies to The Boeing Company Model 757-200, -200PF, -200CB, and -300 series airplanes, certificated in any category, equipped with Rolls-Royce RB211-535E4, -535E4-B, and -535E4-C engines; or with Rolls-Royce RB211-535E4, -535E4-B, and -535E4-C engines that have air intake cowls that were modified by Bombardier Aerospace Supplemental Type Certificate (STC) ST02102NY
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| CAA-2014-05-009 |
2014/05/31 |
EASA |
2014-0133 |
P.68 “Victor” and P.68B “Victor” aeroplanes, all serial numbers.
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| CAA-2014-05-006 |
2014/05/31 |
EASA |
2014-0131 |
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers.
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| CAA-2014-01-011A |
2014/05/31 |
EASA |
2014-0025R1 |
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, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232 and A320-233 aeroplanes, all manufacturer serial numbers.
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| CAA-2008-06-006B |
2014/05/31 |
EASA |
2008-0204R1 |
SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial
numbers, except those that have embodied Airbus Helicopter modification (mod) 07 55B28.
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| CAA-2014-05-010(已有後續修訂版) |
2014/05/30 |
EASA |
2014-0137 |
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, A320-211, 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-2014-05-005 |
2014/05/23 |
EASA |
2014-0130 |
CFM56-5B engines, all models, all serial numbers. CFM56-7B engines, all models, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A318, A319, A320 and A321 aeroplanes; and Boeing 737-600, -700, -800, -900 and -900ER aeroplanes.
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| CAA-2014-05-004 |
2014/05/22 |
EASA |
2014-0127 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all Manufacturer Serial Numbers (MSN) except those on which Airbus Modification 203287 has been embodied in production, and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
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| CAA-2014-05-003(已有後續修訂版) |
2014/05/19 |
EASA |
2014-0120 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, and A330-343 aeroplanes, all manufacturer serial numbers (MSN).
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642, and A340-643 aeroplanes, all MSN.
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| CAA-2014-04-006A |
2014/05/19 |
EASA |
2014-0095R1 |
HR Smith (Technical Developments) Crash Position Indicator (CPI) System 15-503-134 and 15-503-134-1 series, when equipped with Control Panel part number (P/N) 503-22-() and Beacon release unit P/N 503-21 and System
Interface Unit P/N 503-24-() (including 503-24) or P/N 503-42-() (including 503-
42), except System Interface Units having P/N 503-24-A, P/N 503-24-()-A, P/N 503-24-G, P/N 503-24-()-G, P/N 503-42-A, P/N 503-42-()-A, P/N 503-42-G or P/N 503-42-()-G.
This CPI System is known to be installed on, but not limited to the following aircraft:
- Airbus Helicopters (formerly Eurocopter) Models EC 155B, EC 155 B1, SA 365 N, AS 365 N3, AS 332 L1, AS 332 L2 and EC 225 LP, - Airbus Helicopters Deutschland (formerly Eurocopter Deutschland) EC 135 series and MBB-BK117-C2,
- Agusta Westland A109 series, AB139 and AW139, - Sikorsky S-61N, S-76 series and S-92A, and - MD Helicopters Inc. MD900.
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