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FAA AD on Eurocopter France model AS-365N2, AS-365 N3, EC-155B, EC-155B1, SA-365N, N1, and SA-366G1 helicopters (2006-16-15R1)

Washington, Usa - To detect a crack in an 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: July 26, 2006 (Volume 71, Number 143)] [Page 42254-42258] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18850; Directorate Identifier 2004-SW-19-AD; Amendment 39-14694; AD 2004-16-15 R1] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 146065
Rome, Italy, 08/01/2006 12:13
AVIONEWS - World Aeronautical Press Agency

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