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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

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
Rome, Italy, 12/28/2006 17:32
AVIONEWS - World Aeronautical Press Agency

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