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FAA AD on MD Helicopters, Inc. model 369A, D, E, H, HE, HM, HS, F, and FF helicopters
Washington, Usa - To prevent a tail rotor blade pitch horn (pitch horn) from separating from the tail rotor blade, leading to an unbalanced condition, vibration, loss of tail rotor pitch control, and loss of directional control of the helicopter
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-17-AD; Amendment 39-13215; AD 2003-08-51] RIN 2120-AA64 Airworthiness Directives; MD Helicopters, Inc. Model 369A, D, E, H, HE, HM, HS, F, and FF Helicopters PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 47499
AVIONEWS - World Aeronautical Press Agency
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AVIONEWS - World Aeronautical Press Agency