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FAA AD on Bombardier model CL-600-2B19 airplanes (2006-02-05)

Washington, Usa - To prevent these fasteners from disengaging and interfering with an inboard rudder pedal, which could reduce directional controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 20, 2006 (Volume 71, Number 13)] [Page 3210-3212] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22873; Directorate Identifier 2005-NM-197-AD; Amendment 39-14457; AD 2006-02-05] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 134782
Rome, Italy, 01/23/2006 15:03
AVIONEWS - World Aeronautical Press Agency

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