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FAA AD on Agusta SpA model A-109E helicopters (2005-09-07)

Washington, Usa - To detect a fracture, a crack, or looseness of a fitting bolt, and prevent fatigue failure of a fitting bolt and subsequent loss of control of the helicopter

Airworthiness Directive Federal Register Information [Federal Register: May 9, 2005 (Volume 70, Number 88)] [Page 24305-24307] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20292; Directorate Identifier 2004-SW-26-AD; Amendment 39-14075; AD 2005-09-07] RIN 2120-AA64 Airworthiness Directives; Agusta...

fra/pec - 120121
Rome, Italy, 05/10/2005 11:39
AVIONEWS - World Aeronautical Press Agency

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