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FAA (Revision) 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
Airworthiness Directive Federal Register Information [Federal Register: March 28, 2006 (Volume 71, Number 59)] [Page 15323-15325] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24252; Directorate Identifier 2006-NM-062-AD; Amendment 39-14528; AD 2006-05-11 R1] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 138352
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency