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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

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
Rome, Italy, 11/24/2005 12:11
AVIONEWS - World Aeronautical Press Agency

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