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FAA AD on Bombardier model CL-600-2B19 airplanes (2008-08-09)

Washington, Usa - To prevent undetected failure of the shear pins 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: April 14 ,2008 [Page 19979-19982] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0047; Directorate Identifier 2007-NM-295-AD; Amendment 39-15461; AD 2008-08-09] RIN 2120-AA64 Airworthiness Directives; Bombardier Model CL-600-2B19...

fra/pec - 1088399
Rome, Italy, 04/15/2008 15:07
AVIONEWS - World Aeronautical Press Agency

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