My question is, if you were flying in a twin-engine aircraft such as a beechcraft baron, and when you increase/decrease manifold pressure with the throttle, do you always have to match it with the propeller rpm speed when changing altitude and in cruise altitude? And, do you set max propeller rpm when you are on final approach or sooner?
I'm just trying to figure out how important this ratio is with the propeller rpm when you are doing manifold pressure adjustments in climbs, decents and level flight. Thanks in advance!
Tags: