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FAA AD on General Electric Company CT7-5, -7, and -9 series turboprop engines (2007-08-01)

Washington, Usa - To prevent separation of the stage 2 turbine aft cooling plate, resulting in uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information [Page 17379-17381] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20944; Directorate Identifier 2003-NE-64-AD; Amendment 39-15018; AD 2007-08-01] RIN 2120-AA64 Airworthiness Directives; General Electric Company CT7-5, -7, and -9 Series Turboprop Engines...

fra/pec - 1073086
Rome, Italy, 05/03/2007 12:36
AVIONEWS - World Aeronautical Press Agency

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