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FAA AD on The Cessna Aircraft Company model 525 airplanes

Usa - To correct this single-point failure in the electric pitch trim system, which will result in a runaway pitch trim condition where the pilot could not disconnect using the control wheel autopilot/trim disconnect switc

Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: July 13, 2004 (Volume 69, Number 133)] [Page 41920-41923] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-CE-54-AD; Amendment 39-13729; AD 2004-14-20] RIN 2120-AA64 Airworthiness...

fra/pec - 100462
Rome, Italy, 07/22/2004 11:16
AVIONEWS - World Aeronautical Press Agency

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