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FAA AD on Bombardier model CL-600-2B19 airplanes (2007-15-02)

Washington, Usa - To prevent exceeded backlashes in both aileron PCUs, which, if accompanied by the failure of the flutter damper, could result in aileron vibration/flutter and reduced controllability of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 24, 2007 (Volume 72, Number 141)] [Page 40224-40226] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25779; Directorate Identifier 2006-NM-088-AD; Amendment 39-15131; AD 2007-15-02] RIN 2120-AA64 Airworthiness Directives; Bombardier...

fra/pec - 1077448

AVIONEWS - World Aeronautical Press Agency
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