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FAA AD on Schweizer Aircraft Corporation model 269C, C-1, and D helicopters

Washington, Usa - To prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of cont

Airworthiness Directive Federal Register Information [Federal Register: May 18, 2005 (Volume 70, Number 95)] [Page 28415-28417] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21217; Directorate Identifier 2005-SW-06-AD; Amendment 39-14089; AD 2005-10-12] RIN 2120-AA64 Airworthiness Directives; Schweizer...

fra/pec - 120742

AVIONEWS - World Aeronautical Press Agency
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