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FAA AD on CFM International CFM56 Series Turbofan Engines (97-09-02R1 Amendment)
Washington, Usa - To prevent a low-cycle-fatigue (LCF) failure of the high pressure turbine rotor (HPTR) front shaft, HPTR front air seal, HPTR disk, booster spool
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 95-ANE-64-AD; Amendment 39-12876; AD 97-09-02 R1] RIN 2120-AA64 Airworthiness Directives; CFM International CFM56 Series Turbofan Engines Preamble Information Regulatory Information REVISION 97-09-02R1 CFM International: Amendment 39-12876....
AVIONEWS - World Aeronautical Press Agency