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FAA AD on Bombardier model DHC-8-400 series airplanes (2007-01-14)

Washington, Usa - To detect and correct fatigue cracking of certain PSEs, which could result in reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 30, 2007 (Volume 72, Number 19)] [Page 4197-4198] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-26217; Directorate Identifier 2006-NM-209-AD; Amendment 39-14886; AD 2007-01-14] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 73485

AVIONEWS - World Aeronautical Press Agency
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