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FAA AD on General Electric Aircraft Engines CT7 series turboprop engines
Washington, Usa - To prevent separation of PGB left-hand and right-hand idler gears, which could result in uncontained PGB failure and internal bulkhead damage, possibly prohibiting the auxiliary feathering system from fully feathering the propeller on
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Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 99-NE-48-AD; Amendment 39-13090; AD 2003-06-03] RIN 2120-AA64 Airworthiness Directives; General Electric Aircraft Engines CT7 Series Turboprop Engines PDF Copy (If Available): Preamble Information Regulatory Information 2003-06-03 General...
AVIONEWS - World Aeronautical Press Agency - 42640
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency