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FAA AD on Cessna Aircraft Company models 402C and 414A airplanes (2005-12-13)

Washington, Usa -To prevent wing spar cap failure caused by undetected fatigue cracks

Airworthiness Directive Federal Register Information [Federal Register: June 14, 2005 (Volume 70, Number 113)] [Page 34325-34329] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-05-21177; Directorate Identifier 2005-CE-26-AD; Amendment 39-14129; AD 2005-12-13] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 122156
Rome, Italy, 06/15/2005 13:58
AVIONEWS - World Aeronautical Press Agency

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