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FAA AD on CFM International, S.A. turbofan engines (2009-18-01)

Washington, Usa - To detect low-cycle-fatigue cracks in the LP turbine rear frame, which could result in an engine separating from the airplane, causing damage to, and possibly leading to loss of control of the airplane

Airworthiness Directive Federal Register Information Federal Register: [Page 43634-43636] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0174; Directorate Identifier 2008-NE-03-AD; Amendment 39-15997; AD 2009-18-01] RIN 2120-AA64 Airworthiness Directives; CFM International, S.A. CFM56-5B1/P; - 5B2/P;...

fra/pec - 1108774
Rome, Italy, 09/01/2009 17:17
AVIONEWS - World Aeronautical Press Agency

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