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I'm fairly new to GA after a 19 year break flying jets. I routinely
fly a single engine experimental with a constant speed prop mounted on a Lycoming IO-360. 2 QUESTIONS: 1. What's the proper setup to simulate the way the plane would glide in case of an engine failure? I'm looking for pitch and possibly a manifold pressure number here. 2. It that motor quits, will it still rotate through the flying airspeed envelope or can I expect it to stop rotation (assuming it's not frozen due to a mechanical failure)? In idle, with the prop at flat pitch, it feels too draggy and comes down like a rock. With it at high pitch, it seems to have too optimistic a glide ratio. What's the happy medium? I don't live near a dry lake bed or I'd just shut it down and find out. I have the proper airspeeds for max range and min sink out of the POH but it does not quote any type of glide ratio. Ed |
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