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FAA AD on Airbus Helicopters, model AS-332C, AS-332L, AS-332L1, AS-332L2, and SA-330J helicopters (2014-03-02)

Washington, Usa - To prevent failure of a main servo-control upper end fitting, and subsequent failure of the flight controls and loss of control of the helicopter

[Federal Register Volume 79, Number 33 (Wednesday, February 19, 2014)] [Rules and Regulations] [Pages 9395-9397] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-02972] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0737; Directorate Identifier 2012-SW-111-AD; Amendment 39-17739; AD 2014-03-02] RIN...

fra/pec - 1158533

AVIONEWS - World Aeronautical Press Agency
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