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FAA AD on Kaman Aerospace Corporation model K- 1200 helicopters
Washington, Usa - To prevent failure of the rotor shaft, teeter pin assembly, or flap clevis due to fatigue cracks, and subsequent loss of control of the helicopter
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Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000-SW-50-AD; Amendment 39-13123; AD 2001-13-03 R1] RIN 2120-AA64 Airworthiness Directives; Kaman Aerospace Corporation Model K- 1200 Helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2001-13-03 R1 Kaman...
AVIONEWS - World Aeronautical Press Agency - 44285
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency