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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

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
Rome, Italy, 01/16/2007 13:26
AVIONEWS - World Aeronautical Press Agency

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