GE AIRCRAFT
GE AIRCRAFT CT7 series turboprop engines (Docket No. 2000-NE-61-AD; Amendment 39-12594; AD 2002-01-03) - requires removal of Stage 2 turbine aft cooling plates of a certain part number (P/N) and installation of cooling plates of a new design. This amendment is prompted by a report of a Stage 2...
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