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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

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
Rome, Italy, 04/22/2003 13:49
AVIONEWS - World Aeronautical Press Agency

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