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FAA AD on Bombardier model CL-600-2B19 airplanes
Washington, Usa - To detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG
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Airworthiness Directive Federal Register Information [Federal Register: January 12, 2007 (Volume 72, Number 8)] [Page 1430-1436] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22559; Directorate Identifier 2005-NM-076-AD; Amendment 39-14879; AD 2007-01-07] RIN 2120-AA64 Airworthiness Directives; Bombardier...
fra/pec - 72515
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency