Maintenance Manual STEMME S10-VT
Date of Issue: Jan. 01, 1998
Page 2-2
Amendment Nr. 8
Date: Nov. 11, 1999
A4011121_B23.doc
Doc. No. A40-11-121
Vertical Tail
height
1.60 m
5.2 ft.
total area
1.51 m²
16.25 sqft.
area of rudder
0.52 m²
5.60 sqft.
airfoil
FX 71-L-150/35
Horizontal Tail
span
3.10 m
10.2 ft.
total area
1.46 m²
15.72 sqft.
area of elevator
0.36 m²
3.88 sqft.
aspect ratio
6.58
airfoil
FX 71-L-150/25
Landing Gear
2 main wheels with brake discs, rim of wheel
127x127-30
tire size: (standard/wide tire)
5.00-5 / 6.00-5
wheel track: (standard/wide tire)
1.15 m / 1.16 m
3.77 ft / 3.8 ft.
tail wheel (steerable), tire size
210 x 65
wheel base
5.46 m
17.9 ft.
Power-Plant
engine
ROTAX 914 F2/S1
T/O-power (115%, max 5 minutes)
at 5800 RPM 84.5 kW
113.2 hp
max continuos power (100%)
at 5500 RPM 73.4 kW
98.4 hp
gear transmission ratio front gear
i = 1.109
gear transmission ratio engine-gear
i = 0.412
Variable-Pitch Propeller
Model
STEMME 11 AP
diameter extended
D
PA
= 1.63 m
63.4 in
mass of the propeller (incl. outer-casing of
needle bearing and rubber buffers)
m
P
= 9350 g
20.61 lbs
overall mass of propeller blade
m
B
= 650 g ± 10 g 1.433 lbs ± 0.022 lbs
max. propeller RPM
n
P
= 2.650 RPM
propeller pitch T/O position
P
= 17.65°
cruise position
P
= 24.05°
max. current consumption of the resistor element
I
max
= 10 A
Weights (see also figures 6.3a/ 6.3.b and form "Weight and Balance Report")
maximum allowable weight
850 kg
1874 lbs
empty weight, including minimum equipment
660 kg
1)
1455.1 lbs
1)
maximum weight of non-supporting parts
570 kg
1257 lbs
total useful load (occupants, fuel, baggage)
190 kg
1)
419 lbs
1)
1)
Load distribution according to Weight & Balance, refer to Flight Manual. Empty weight of 660 kg / 1455 lbs
is without optional equipment. Useful load is reduced by additional equipment.
Inflight Centre of Gravity range
In-flight Centre-of-Gravity range aft of datum
(central wing leading edge, see section 6.3)
254 - 420 mm
10 in. - 16.5 in.
For more technical data, please refer to the Flight Manual.
Following figure shows a 3-view plan of the S10-VT.
