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FAA AD on Schweizer Aircraft Corporation model 269A, 269A-1, 269B, 269C, and TH-55A helicopters
Washington, Usa - To prevent failure of a tailboom support strut or lug on a cluster fitting, which could cause rotation of a tailboom into the main rotor blades, and subsequent loss of control of the helicopter
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-SW-25-AD; Amendment 39-13217; AD 2003-13-15] RIN 2120-AA64 Airworthiness Directives; Schweizer Aircraft Corporation Model 269A, 269A-1, 269B, 269C, and TH-55A Helicopters PDF Copy (If Available): Preamble...
fra/pec - 47688
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency