Maintenance Manual STEMME S10
Date of Issue: Oct. 01, 1990 Page 10
Amendment No.: Date: --
A4010021_B19.doc
Doc.No.: A40-10-021
Fuselage
length 8.42 m
width 1.18 m
clear cockpit width 1.16 m
clear cockpit height 0.93 m
height at tail unit 1.75 m
Vertical Tail
height 1.60 m
total area 1.51 m²
area of rudder 0.52 m²
airfoil FX 71-L-150/35
Horizontal Tail
span 3.10 m
total area 1.46 m²
area of elevator 0.36 m²
aspect ratio 0.62
airfoil FX 71-L-150/25
Landing Gear
2 main wheels (disc brake) 348 x 122
wheel track 1.15 m
tail wheel (steerable) 210 x 65
wheel base 5.46 m
Power-Plant
engine Limbach L 2400 EB 1.D
take-off power (3400 rpm) 69 kW
propeller STEMME 10 AP-N
diameter 1.61 m
gear transmission ratio i=1.18
Masses (see also figure 14.3.a)
maximum allowable mass 850 kg
empty mass 640 kg
maximum mass of non-structural parts 570 kg
total useful load (occupants, fuel, baggage) 210 kg
mass of ballast: For pilot masses between 55 and 70 kg (including parachute), the defined ballast mass of 6
kg must be attached to the right-hand rudder pedal support.
For distribution of the useful load, please refer to the load and balance sheet in the Flight Manual.
The empty mass stated does not include any additional equipment. The total useful load will be reduced
depending on the equipment.
In-flight Centre-of-Gravity Range aft of datum
(formed by the central wing leading edge, see figure 6.3.a) 254 to 420 mm
For further technical data, please refer to the Flight Manual.
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