By the way, ability to feather the prop is useful to single engined aircraft as well since it increases the glide distance. For example, in the T-34 which is a Navy trainer aircraft, with the prop feathered you have a 12:1 glide ratio, but with the condition lever set to full increase, you only have about a 2 or 3:1 glide ratio. In practical terms this means that if you lose your engine at say 10,000 feet you would be able to glide 20 miles with the prop feathered but only about 3 miles or so with the prop turning. Thus, one of the most important steps of the EP for engine failure is the 4th one: condition lever to feather.
I dont know if any of the single engined fighters in AH had the ability to feather their props although I think that the F-4U could at least. It has a prop pitch control in the throttle quadrant, and it seems logical to me that you would be able to set it to feather.