"power" reduction a S/E performance
Sorry for asking, asking, asking, again and again!
Does the manual say the King will fly, after an engine failure at rotation, at standard day, with MTOW?
Is there a takeoff chart with the Performance-Limited MTOW for runway lenght, slope, temp & elevation?
What the FAR23 says about single engine performance on takeoff for King-like planes?
I though it would be interesting to reduce temps with a reduced power takeoff, to save the hot section of the engines. If there were takeoff charts like the ones on Boeing's manuals, with field limited and climb limited performances, we would be able to calculate engine power to meet at least FAR 23 requirements, when not fully loaded.
What do you think?