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FAA AD on Eurocopter France model SA-360C, SA- 365C, SA-365C1, and SA-365C2 helicopters

Washington, Usa - To detect a crack in a MGB base plate and prevent failure of one of the MGB attachment points to the frame, which could result in severe vibration and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: April 13, 2006 (Volume 71, Number 71)] [Page 19110-19114] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24446; Directorate Identifier 2005-SW-15-AD; Amendment 39-14561; AD 2006-08-06] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 139253
Rome, Italy, 04/14/2006 13:21
AVIONEWS - World Aeronautical Press Agency

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