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FAA AD on CFM International (CFMI) CFM56-5C series turbofan engines
Washington, Usa - To prevent low cycle fatigue (LCF) failure of the high pressure turbine rotor (HPTR) front shaft, HPTR front air seal, and booster spool, which could result in an uncontained failure and damage to the airplane
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 95-ANE-64-AD; Amendment 39-13094; AD 97-09-02R2] RIN 2120-AA64 Airworthiness Directives; CFM International (CFMI) CFM56-5C Series Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 97-09-02R2 CFM International:...
AVIONEWS - World Aeronautical Press Agency - 42980
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency