- Joined
- Jun 13, 2008
- Messages
- 9,173
- Location
- Marietta, GA
- Display Name
- Drake the Outlaw
- Home Airfield
- Cartersville, GA
I've seen all sorts of debate about climb power, rpm, MP, cruise leaning, LOP, ROP, etc. But one subject I've never seen discussed at length is (are?) appropriate/optimal ways to descend from altitude flying a kinda fast airplane with a constant speed prop. Basically, I'm talking about my IO-540 powered RV-10 here. A couple of scenarios - assume I'm starting at 10K' headed towards a destination airport at 1,000 MSL.
1) Goal is to reduce power, but maintain speed by trading a 500 FPM descent for airspeed. Probably the most efficient approach.
2) Goal is to stay high until late (weather, traffic, whatever), then pull the plug - maybe a 1000 fpm descent to the destination while retaining airspeed.
What are your constraints (primarily engine constraints) for the two scenarios and why? Maintain MP at XX? Maintain RPM at YYYY? Gradual reduction in CHT? I'd think you'd want to lean pretty far at low(er) power, gradually enriching mixture during the descent.
1) Goal is to reduce power, but maintain speed by trading a 500 FPM descent for airspeed. Probably the most efficient approach.
2) Goal is to stay high until late (weather, traffic, whatever), then pull the plug - maybe a 1000 fpm descent to the destination while retaining airspeed.
What are your constraints (primarily engine constraints) for the two scenarios and why? Maintain MP at XX? Maintain RPM at YYYY? Gradual reduction in CHT? I'd think you'd want to lean pretty far at low(er) power, gradually enriching mixture during the descent.