STEMME S6-RT, Руководство по эксплуатации самолета

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7 26 Revision:
Date of Issue: 18. November 2011 Date of Rev.: . .
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The installed engine is a model ROTAX 914 F2:
4 cylinder 4 stroke Otto engine in opposed cylinder design including
turbocharger with electronic manifold air pressure (MAP) control and
integrated reduction gear
Liquid cooled cylinder heads and ram air cooled cylinders
Electronic dual magneto capacitator ignition
Two CD carburetor, one on each engine side
Flanged reduction gear and overload clutch
The engine is mounted in the midsection of the fuselage with the engine
suspension connecting it to the steel tube framework. There, the engine causes
low noise emissions for the cabin and the aircraft’s surroundings.
Specifications of the ROTAX 914 F2:
Max. T/O Power (MTOP):
113 HP / 84.5 kW at 5800 RPM (max. 5 min)
Max. Continuous Power
(MCP):
98 HP / 73.4 kW at 5500 RPM
Engine Displacement:
73.9 in
3
/ 1211 cm
3
Transmission Ratio of
Engine Gear
i=2.428
Compression Ratio:
9.0 : 1
Fuel and fuel Consumption:
Fuel to be used:
MOGAS (unleaded gasoline according to EN
228, min. RON 95)
or AVGAS 100LL
Fuel Consumption at MCP
(100%)
7.0 US gal/h / 26.6 l/h
Fuel Consumption at 75%
Power
5.4 US gal/h / 20.4 l/h
Fuel Consumption at 55%
Power
3.4 US gal/h / 13 l/h