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FAA emergency AD on Augusta model A109E helicopters (2002-17-51)
Washington, Usa - To prevent failure of the tail rotor blade and subsequent loss of control of the helicopter
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Docket No. 2002-SW-42-AD; AD 2002-17-51 E Augusta S.p.A. Model A109E helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2002-17-51 AGUSTA S.p.A.: Docket No. 2002-SW-42-AD. Supersedes Emergency AD 2002-14-51, Docket No. 2002-SW-35-AD. Applicability:...
AVIONEWS - World Aeronautical Press Agency - 32541
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency