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FAA (Correction) AD on Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 411, and 411A airplanes

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

Airworthiness Directive Federal Register Information [Federal Register: June 28, 2005 (Volume 70, Number 123)] [Page 37152] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-05-21176; Directorate Identifier 2005-CE-25-AD; Amendment 39-14128; AD 2005-12-12] RIN 2120-AA64 Airworthiness Directives; Cessna...

fra/pec - 123010
Rome, Italy, 06/28/2005 21:27
AVIONEWS - World Aeronautical Press Agency

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