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FAA AD on Bombardier model CL-215-6B11 (CL215T Variant), and CL-215-6B11 (CL415 Variant) series airplanes (2004-10-04)
Usa - To prevent failure of the rear engine mount struts, which could subsequently result in reduced structural integrity of the nacelle and engine support structure
Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 17, 2004 (Volume 69, Number 95)] [Page 27831-27833] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-199-AD; Amendment 39-13634; AD 2004-10-04] RIN 2120-AA64 Airworthiness...
fra/pec - 63429
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency