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FAA AD on CFM International, S.A. CFM56-7B series turbofan egines (2008-03-09)

Washington, Usa - To prevent failure of the TRF from low-cycle fatigue cracks. Failure of the TRF could result in engine separation from the airplane, which could lead to loss of control of the airplane

Airworthiness Directive Federal Register Information [Federal Register: February 4, 2008 (Volume 73, Number 23)] [Page 6419-6423] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27229; Directorate Identifier 2007-NE-03-AD; Amendment 39-15359; AD 2008-03-09] RIN 2120-AA64 Airworthiness Directives; CFM International,...

fra/pec - 1085448
Rome, Italy, 02/05/2008 11:50
AVIONEWS - World Aeronautical Press Agency

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