General Electric Ct64 820 4

The faa is adopting a new airworthiness directive ad for general electric company ge ct64 820 4 turboprop engines with stage 1 turbine disk and shaft part number p n 6004t47p03 or 4921t10p02 installed. This ad requires removing from service these stage 1 turbine disk and shafts at reduced compliance times. The t408 provides 58 71 more power than the t64 engines that power the ch 53e mh 53e with 18 lower fuel consumption and 63 fewer parts.

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