| CAA-2010-09-007 |
2010/09/30 |
FAA |
2010-20-07 |
(1) All International Aero Engines AG (IAE) V2500-A1 turbofan engines; and (2) All IAE V2525-D5 and V2528-D5 turbofan engines; and (3) IAE V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines with serial numbers (S/Ns) up to and including V13181, and with S/Ns from V15000 up to and including V15245. (4) These engines are installed on, but not limited to, Airbus A319, A320, and A321, and McDonnell Douglas MD-90 airplanes.
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| CAA-2010-09-006(已有後續修訂版) |
2010/09/29 |
EASA |
2010-0191 |
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 electrical rudder) has
been embodied in production, except those on which Airbus modification 58118 and Airbus modification 200667 have been embodied in production and
Airbus A340 aeroplanes, models -311, -312, and -313, all manufacturer serial numbers on which Airbus modification 49144 has been embodied in production, except those on which Airbus modification 58118 and Airbus
modification 200667 have been embodied in production and
Airbus A340 aeroplanes, models -541, -542, -642, -643, all manufacturer serial numbers, except those on which Airbus modification 200667 has
been embodied in production.
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| CAA-2010-09-005(已有後續修訂版) |
2010/09/27 |
EASA |
2010-0187 |
Airbus A330 aeroplanes, models -243, -243F, -341, -342 and -343 all
manufacturer serial numbers.
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| CAA-2010-05-002A |
2010/09/23 |
EASA |
2010-0083-CN |
Airbus A330 aeroplanes, models -201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342 and -343, all manufacturer serial numbers and
Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all manufacturer serial numbers.
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| CAA-2010-09-004 |
2010/09/16 |
FAA |
2010-18-13 |
Pratt & Whitney (PW) PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, and PW4462 turbofan engines. These engines are installed on, but not limited to, Boeing 747-400, 767-200, 767-300, 777-200, and 777-300 airplanes; McDonnell Douglas MD-11 airplanes; and Airbus A300-600, A310-300, and A330-200 airplanes.
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| CAA-2010-09-003 |
2010/09/16 |
FAA |
2010-17-16 |
Model S-76A, S-76B, and S-76C helicopters, with serial numbers 76005 through 760578, inclusive, and serial number 762976, with any of the following part-numbered vertical stabilizer aft spar assemblies having 1,000 or more hours time-in-service (TIS) installed, certificated in any category.
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| CAA-2010-09-002 |
2010/09/13 |
EASA |
2010-0186 |
FSG 2T VHF/AM Airband Transceivers, Part Number (P/N) F10350, serial numbers (s/n) 35(X)-05100 through 35(X)-06462 inclusive, except units marked with Mod-Index: SB 1.06, and s/n 353-05172, 353-05189, 355-05557,
355-05696 and 356-05828.
Note: (X) in the s/n prefix denotes any digit between 2 and 9, identifying the year of manufacture (e.g. 2 = 2002, 3 = 2003, etc.). These transceivers are known to be installed on, but not limited to, aircraft certificated (validated) by EASA under CS 22, CS 23, CS-31HB, CS-VLA, and aircraft certificated (validated) prior to 28 September 2003 under equivalent National Standards by EU Member States or associated countries.
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| CAA-2010-09-001(已有後續修訂版) |
2010/09/03 |
Japan CAB |
TCD-7698-2010 |
Kawasaki BK117, BK117 A-3, BK117 A-4, BK117 B-1, BK117 B-2 and BK117 C-1 helicopters
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| CAA-2010-08-014 |
2010/08/31 |
EASA |
2010-0177 |
Airbus 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 serial
numbers, if equipped with one or more Additional Centre Tank(s) (ACT(s)) with a Part Number (P/N) listed in Appendix 1 of this AD.
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| CAA-2010-08-013(已被CAA-2016-04-004取代) |
2010/08/31 |
ANAC |
2010-08-03(Brazil) |
This Airworthiness Directive (AD) applies to Embraer Model 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; all serial numbers.
NOTE 1: This AD requires revisions to certain operator maintenance documents to include new inspection tasks or modification of existing ones and its respective thresholds and
intervals. Compliance with these inspections is required by “Regulamento Brasileiro de
Homologação Aeronáutica” - RBHA 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the described inspections. In this situation, to comply with RBHA 91.403(c), the operator must request approval for an alternative method of compliance. The request should include a
description of changes to the required inspections that will ensure the continued operational safety of the airplane. An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Product Certification Branch (GGCP).
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