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FAA AD on Bell Helicopter Textron Canada model 222, 222B, 222U, and 230 helicopters
Washington, Usa - To prevent the main rotor pendulum weights (pendulum weights) from separating from the pendulum weight support and striking the vertical fin or tail rotor, and subsequent loss of control of the helicopter
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-SW-01-AD; Amendment 39-13118; AD 2003-08-07] RIN 2120-AA64 Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2003-08-07...
AVIONEWS - World Aeronautical Press Agency - 44132
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency