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FAA AD on Bombardier model DHC-8-401 and -402 airplanes

Washington, Usa - To prevent a short circuit on the aileron/rudder trim control panel that could cause a runaway condition of the rudder trim actuator, which could result in reduced controllability of the airplane

Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NM-120-AD; Amendment 39-13534; AD 2004-06-08] RIN 2120-AA64 Airworthiness Directives; Bombardier Model DHC-8-401 and -402 Airplanes PDF Copy (If Available): Preamble Information AGENCY: Federal Aviation...

fra/pec - 60779
Rome, Italy, 03/26/2004 14:07
AVIONEWS - World Aeronautical Press Agency

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