| CAA-2014-07-010 |
2014/07/21 |
FAA |
2014-11-03 |
The Boeing Company Model 777-200, -200LR, -300, and -300ER series airplanes, certificated in any category, as identified in Boeing Service Bulletin 777-27A0078, Revision 1, dated April 1, 2013.
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| CAA-2014-07-009 |
2014/07/21 |
EASA |
2014-0125 |
HR Smith (Technical Developments) Crash Position Indicator (CPI) system 15-503-134-1 series, if equipped with
- Beacon Release Unit (BRU) Part Number (P/N) 503-21-1, and
- System Interface Unit (SIU) P/N 503-24 or P/N 503-24-2 or P/N 503-24-6.
This CPI system is known to be installed on, but not limited to the following aircraft:
- Airbus Helicopters (formerly Eurocopter) Model EC 225 LP
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| CAA-2014-07-005 |
2014/07/21 |
EASA |
2014-0161 |
Airbus A330-202, A330-203, A330-223 and A330-243 aeroplanes, all Manufacturer Serial Numbers (MSN) on which Airbus modification (Mod) 45775, 45790, 45795, 46165, 46779, 48099, 48454, 52131, 52802, 53730, 53819, 54310, 54410, 54530, 54420, 55231, 55630, 56080, 56260, 56620, 57186, 57430, 200774, 201071, 201298, 201888, 202558 or 203045 has been embodied in production, except those on which Airbus Mod 203395 has been embodied in production. and Airbus A340-211, A340-212, A340-311 and A340-313 aeroplanes, all MSN on which Airbus Mod 40413, 40550, 40901, 42021, 43590 or 46487 has been embodied in production, except those on which Airbus Mod 203395 has been embodied in production.
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| CAA-2014-07-007 |
2014/07/15 |
FAA |
2014-12-52. |
Honeywell International Inc. TFE731-4, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, -40BR, -50R, and -60 turbofan engines with 2nd stage low-pressure turbine (LPT2) blades, part number (P/N) 3075424-1, -2, or -3, installed.
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| CAA-2014-07-006A(已有後續修訂版) |
2014/07/15 |
EASA |
2014-0162R1 |
SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial
numbers, and SA 366 G1 helicopters, all serial numbers.
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| CAA-2014-07-006(已有後續修訂版) |
2014/07/15 |
EASA |
2014-0162 |
SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial
numbers, and SA 366 G1 helicopters, all serial numbers.
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| CAA-2014-07-004 |
2014/07/14 |
ANAC |
Brazil-2014-07-01 |
Embraer S.A. model ERJ 190-100STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200STD, ERJ 190-200 LR, and ERJ 190-200 IGW airplanes; as identified in Group 1, Group 2 and Group 3 of Embraer Service Bulletin 190-54-0015, original issue, dated July 3, 2014, and 190LIN-54-0006, original issue, dated July 3, 2014, as applicable.
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| CAA-2014-07-003(已有後續修訂版) |
2014/07/11 |
EASA |
2014-0159 |
SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial
numbers, and SA 366 G1 helicopters, all serial numbers.
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| CAA-2013-02-002D(已有後續修訂版) |
2014/07/11 |
EASA |
2013-0020R4 |
All part numbers of safety belts and torso restraint systems of manufacture by AmSafe, Anjou Aeronautique, Davis Aircraft Products Co., Schroth Safety Products GmbH, Pacific Scientific, installed on any aircraft where dynamically tested seats are required in accordance with
airworthiness requirements like the European Certification Specifications (CS),
or JAR/FAR, paragraphs 23.562, 25.562, 27.562 and 29.562, if safety belts and torso restraint systems have been maintained or repaired after 28 September 2003 by maintenance organizations not holding the applicable maintenance data of the relevant approval holders, unless they are marked
with European Parts Approval (EPA). Safety belts and torso restraints system repaired by an organization holding an EASA Design Organization Approval
(DOA) in accordance with Commission Regulation (EU) No 748/2012 Part 21, Subpart J are not affected by this AD. These articles are approved through
design changes or STC and are marked with the letters EPA accordingly. The affected safety belts and torso restraint systems may be installed on, but
not limited to, the aircraft listed in Appendix 1 of this AD.
Note 1: This AD is applicable to safety belts and torso restraint systems, whose Component Maintenance Manuals (CMM) explicitly prohibit webbing
replacement, unless this is accomplished by the design approval holder or by
a repair station/maintenance organization authorized by the design approval holder.
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| CAA-2014-07-002 |
2014/07/04 |
EASA |
2014-0154 |
Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212 and A321-213 aeroplane models, all manufacturer serial numbers on which Airbus modification (mod) 33844 (improvement of aerodynamic shape for CFM pylon) has been embodied in production.
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