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FAA AD on CFM International CFM56-5B and -7B series turbofan engines (2002-16-18)
Washington, Usa - To aid in containment of the LPT rotor in the event of LPT shaft failure
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-37-AD; Amendment 39-12857; AD 2002-16-18] RIN 2120-AA64 Airworthiness Directives; CFM International CFM56-5B and -7B Series Turbofan Engines Preamble Information Regulatory Information 2002-16-18 CFM International: Amendment 39-12857. Docket...
AVIONEWS - World Aeronautical Press Agency - 32199
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency