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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

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
Rome, Italy, 09/02/2005 15:00
AVIONEWS - World Aeronautical Press Agency

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