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FAA AD on Airbus Helicopters, model AS-350B, BA, B1, B2, C, D, and D1; AS-355E, F, F1, F2, and N helicopters (2014-05-07)

Washington, Usa - To prevent failure of the TGB control lever, loss of tail rotor control, and subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 47 (Tuesday, March 11, 2014)] [Rules and Regulations] [Pages 13526-13528] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-04729] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0477; Directorate Identifier 2011-SW-015-AD; Amendment 39-17780; AD 2014-05-07] RIN...

fra/pec - 1158949

AVIONEWS - World Aeronautical Press Agency
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