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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

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
Rome, Italy, 03/21/2003 13:59
AVIONEWS - World Aeronautical Press Agency

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