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FAA AD on Bombardier model CL-600-2B19 airplanes
Washington, Usa - To prevent undetected failure of the shear pin of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: March 10, 2006 (Volume 71, Number 47)] [Page 12277-12280] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24110; Directorate Identifier 2006-NM-020-AD; Amendment 39-14508; AD 2006-05-11] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 137394
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency