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FAA AD on Eurocopter France model AS-365 N3 helicopters (2004-05-28)
Washington, Usa - To prevent vibration in the tail rotor attachments and the pilot's anti-torque pedals, blade pitch control failure, 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. 2003-SW-11-AD; Amendment 39-13523; AD 2004-05-28] RIN 2120-AA64 Airworthiness Directives; Eurocopter France Model AS 365 N3 Helicopters PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation...
fra/pec - 60138
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency