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FAA AD on CFM International, S.A. CFM56-7B series turbofan engines (2010-01-05)
Washington, Usa - To prevent failure of the LP turbine rear frame could result in engine separation from the airplane, possibly leading to loss of control of the airplane
Airworthiness Directive Federal Register Information Federal Register: [Page 2064-2067] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0236; Directorate Identifier 2009-NE-06-AD; Amendment 39-16162; AD 2010-01-05] RIN 2120-AA64 Airworthiness Directives; CFM International, S.A. CFM56-7B Series Turbofan...
fra/pec - 1113967
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency