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FAA AD on General Electric Company CF6-6 series turbofan engines
Washington, Usa - To prevent cracks in high pressure turbine rotor (HPTR) rear shafts, which could result in uncontained engine failure and damage to the airplane
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Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2002-NE-24-AD; Amendment 39-13144; AD 2003-10-01] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF6-6 Series Turbofan Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-10-01 General Electric...
AVIONEWS - World Aeronautical Press Agency - 45239
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency