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FAA AD on Bombardier model CL-600-2B19 airplanes
To prevent undetected failure of the shear pin of both pitch feel simulator (PFS) units simultaneously, which could result in loss of pitch feel forces and consequent loss of control of the airplane
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-262-AD; Amendment 39-13442; AD 2004-02-07] RIN 2120-AA64 Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) Airplanes PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 57593
AVIONEWS - World Aeronautical Press Agency
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AVIONEWS - World Aeronautical Press Agency