STEMME S6 User Manual

Flight Manual STEMME S6
Doc.-No.:P400-006.000 E Page: 1-6 Revision: 9
Date of Issue: 07. October 2008 Date of Rev.: 01.10.2012
Engine Design
4-Cylinder 4-Stroke Otto-engine in
opposed-cylinder design,
Turbocharger with electronic
Manifold-Air-Pressure (MAP) control,
integrated reduction gear
Model
Rotax 914 F2
Max. Take-off Power
113.3 HP / 84.5 kW at 5800 RPM
(Takeoff RPM limited to 5600 RPM)
Max. Continuous
Power
98.4 HP / 73.4 kW at 5500 RPM
Fuel Consumption at
Max. Continuous
Power (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 / 13.0 l/h
Transmission-Ratio
of Reduction-Gear
i=2.428
Propeller Design
Electrically-adjustable 3-Blade
Constant-Speed Propeller
Model
MTV-7-A/170-051 with Constant-
Speed Control-Unit
Diameter
5.58 ft / 1.70 m
Front-Drive Design
Gear in Magnesium-Casing, mounted
elastically on rubber elements
Model
STEMME 050.251
Transmission-Ratio
i=1.100
Fuel-Tanks Design
Integral-tanks located in the forward
section of the inner-wing
Capacity
17.2 US gal / 65 l in right-hand inner-
wing (optionally 17.2 US gal / 65 l in
left-hand inner-wing)
Non-useable Fuel
0.55 US gal / 2.1l in right-hand wing-
tank (optionally 0.3 US gal/ 1l in left-
hand wing-tank)

STEMME S6 Specifications

General

Brand	STEMME
Model	S6
Category	Aircrafts
Language	English