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FAA AD on Bombardier model CL-600-2C10, CL-600-2D15, and CL-600-2D24 airplanes (2006-04-09)

Washington, Usa - To prevent 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: February 17, 2006 (Volume 71, Number 33)] [Page 8441-8443] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22872; Directorate Identifier 2005-NM-198-AD; Amendment 39-14490; AD 2006-04-09] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 136297

AVIONEWS - World Aeronautical Press Agency
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