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FAA AD on Airbus Helicopters model AS-332C, AS-332L, AS-332L1, AS-332L2, EC-225LP, and SA-330J helicopters (2014-05-11)
Washington, Usa - To detect corrosion or a crack on a turnbuckle and prevent the failure of a turnbuckle, loss of control of the tail rotor and subsequent loss of control of the helicopter
[Federal Register Volume 79, Number 47 (Tuesday, March 11, 2014)] [Rules and Regulations] [Pages 13519-13521] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-04695] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0872; Directorate Identifier 2013-SW-012-AD; Amendment 39-17784; AD 2014-05-11] RIN...
fra/pec - 1158948
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency