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FAA AD on Boeing Vertol model 107-II helicopters (2005-24-05)
Washington, Usa - To detect a fatigue crack in a quill shaft and prevent separation of the quill shaft between the aft transmission and the mix box assembly, loss of rotor synchronization, and subsequent loss of control of the helicopter
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Airworthiness Directive Federal Register Information [Federal Register: November 23, 2005 (Volume 70, Number 225)] [Page 70718-70720] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-23085; Directorate Identifier 2005-SW-25-AD; Amendment 39-14385; AD 2005-24-05] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 131670
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency