GENERAL ELECTRIC CT7 series turboprop engines
GENERAL ELECTRIC CT7 series turboprop engines (Docket No. 96-ANE-06) - proposes to require replacement of the gas generator turbine stage 2 forward cooling plates before the published cyclic life limits. The proposal also defines the new, reduced cyclic life limits for the affected forward cooling...
Subscription Required
This content requires a subscription to one of the Aviation Week Intelligence Network (AWIN) bundles.
Schedule a demo today to find out how you can access this content and similar content related to your area of the global aviation industry.
Already an AWIN subscriber? Login
Did you know? Aviation Week has won top honors multiple times in the Jesse H. Neal National Business Journalism Awards, the business-to-business media equivalent of the Pulitzer Prizes.
Related Content
