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FAA AD on General Electric Company CF34-3A1, -3B, and -3B1 turbofan engines
Washington, Usa - To prevent B-sump scavenge screen blockage due to coking, which could result in ignition of B-sump oil in the secondary air system, fan drive shaft separation, and uncontained engine failure
Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-21-AD; Amendment 39-13086; AD 2003-05-10] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF34-3A1, -3B, and -3B1 Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-05-10...
AVIONEWS - World Aeronautical Press Agency - 42446
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency