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FAA Emergency AD on Eurocopter Deutschland GmbH MBB-BK 117 C-2 helicopters (2006-26-51)
Washington, Usa - To prevent a separation of the tail rotor control lever dynamic weights in flight, severe vibration, and subsequent loss of control of the helicopter
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Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. FAA-2006-26721; AD 2006-26-51 Eurocopter Deutschland GmbH MBB-BK 117 C-2 PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation Administration, DOT FOR FURTHER INFORMATION CONTACT: Charles Harrison,...
fra/pec - 71844
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency