Does anyone know of references made to the use of reduced climb thrust for the CF6-50E2? I know that such information is available for the JT9D, however I have not yet been able to come up with CF6 data.
Thought I would try here first with the hope of another company having implemented a procedure where I can reference the source document, if no luck, then off to GE I go...many thanks for your comments.
Heavy...
