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FAA AD on Eurocopter France model EC-130 B4 helicopters
Washington, Usa - To detect and prevent jamming of the twist grip assembly, which, if present, could keep the engine from operating above idle speed and result in subsequent loss of control of the engine power of the helicopter
Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33598-33600] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24807; Directorate Identifier 2005-SW-41-AD; Amendment 39-14603; AD 2006-10-19] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 142664
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency