1. Single engine piston constant speed props. do not feather. Any reason why? 2. When oil pressure is lost some single engine constant speed props. default to high pitch and some default to low pitch. Why don't they all default to one or the other (low or high pitch prop. ) ? With a loss of oil pressure engine failure is usually not far behind. A single engine airplane with a constant speed prop. (as with any aircraft), you want to reduce drag to enhance the glide ratio/range. My understanding is placing the prop. in the high pitch position in this situation (engine failure) reduces drag yet in normal operations high pitch increases resistance (drag) of which reduces RPM. Thank you for the feedback.
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