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FAA AD on Agusta SpA (Agusta) model A-109, A-109A, A-109AII, A-109C, A-109K2, A-109E, A-109S, and A-119 helicopters (2013-05-22)

Washington, Usa - To prevent failure of a tail rotor pitch control link and subsequent loss of control of the helicopter

[Federal Register Volume 78, Number 58] [Rules and Regulations] [Pages 18228-18230] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2013-06131] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2011-1453; Directorate Identifier 2009-SW-46-AD; Amendment 39-17394; AD 2013-05-22] RIN 2120-AA64 Airworthiness...

fra/pec - 1151024

AVIONEWS - World Aeronautical Press Agency
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