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FAA AD on Airbus Helicopters, model EC-225LP helicopters (2014-04-12)

Washington, Usa - To prevent oscillations in the main rotor that can transfer dynamic loads to the structure, the MGB, and the main servo-control inputs, which could result in subsequent loss of control of the helicopter

[Federal Register Volume 79, Number 41 (Monday, March 3, 2014)] [Rules and Regulations] [Pages 11701-11703] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: 2014-04314] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0770; Directorate Identifier 2011-SW-057-AD; Amendment 39-17771; AD 2014-04-12] RIN...

fra/pec - 1158803
Rome, Italy, 03/05/2014 17:47
AVIONEWS - World Aeronautical Press Agency

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