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FAA AD on Bombardier model CL-215-1A10, CL-215-6B11, and CL-215-6B11 airplanes (2005-18-05)
Washington, Usa - To detect and correct cracking of the lower caps of the wing front spar and rear spar, which could result in reduced structural integrity of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: September 1, 2005 (Volume 70, Number 169)] [Page 52009-52011] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21595; Directorate Identifier 2002-NM-321-AD; Amendment 39-14245; AD 2005-18-05] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 126056
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency