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FAA AD on Bombardier model CL-600-2B19 airplanes (2008-06-10)

Washington, Usa - To detect and correct cracking of the frame, which could lead to failure of the fuselage structure and possible loss of the airplane

Airworthiness Directive Federal Register Information Federal Register: March 12, 2008 [Page 13120-13122] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-29257; Directorate Identifier 2007-NM-144-AD; Amendment 39-15422; AD 2008-06-10] RIN 2120-AA64 Airworthiness Directives; Bombardier Model CL-600-2B19 (Regional...

fra/pec - 1087052
Rome, Italy, 03/14/2008 13:02
AVIONEWS - World Aeronautical Press Agency

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