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FAA AD on Eurocopter France helicopters Model AS-365N2, AS-365N3, EC-155B, EC-155B1, SA-365N and N1, and SA-366G1
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 Directives DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18850; Directorate Identifier 2004-SW-19-AD; Amendment 39-13771; AD 2004-16-15] RIN 2120-AA64 Preamble Information AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; request for comments. SUMMARY: This amendment adopts a new airworthiness...
AVIONEWS - World Aeronautical Press Agency - 101968
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency