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FAA AD on Eurocopter France model EC-120B helicopters

Washington, Usa - To prevent separation of the cyclic pitch stick yokes from the cyclic pitch flight control torque tube (torque tube), loss of cyclic control, and subsequent loss of control of the helicopter

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-SW-52-AD; Amendment 39-13115; AD 2003-08-04] RIN 2120-AA64 Airworthiness Directives; Eurocopter France Model EC120B Helicopters PDF Copy (If Available): Preamble Information Regulatory Information 2003-08-04 Eurocopter France: Amendment...

AVIONEWS - World Aeronautical Press Agency - 44214
Rome, Italy, 04/18/2003 13:55
AVIONEWS - World Aeronautical Press Agency

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