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FAA AD on Airbus Helicopters model AS-350B, BA, B1, B2, B3, and D, and model AS-355E, F, F1, F2, and N helicopters (2014-04-11)

Washington, Usa - To prevent loss of a T/R blade tab, which could result in excessive vibration and loss of control of the helicopter

[Federal Register Volume 79, Number 43 (Wednesday, March 5, 2014)] [Rules and Regulations] [Pages 12373-12375] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-04285] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0351; Directorate Identifier 2009-SW-049-AD; Amendment 39-17770; AD 2014-04-11] RIN...

fra/pec - 1158841

AVIONEWS - World Aeronautical Press Agency
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