Dihedral
+3
0
Geometrical Torsion
0
Airfoil
Wortmann
mod.
Aileron
deflection
+12
o
-24
o
Dive brakes on the upper side
0.16 m
2
(1.77 ft
2
)
2.8.2 Horizontal Tail:
Span
2.4
m
(7.9
ft)
Area
1.07
m
2
(11.5 ft)
Root chord
0.55 m (1.8 ft)
Tip chord
0.35 m (1.1 ft)
Elevator area
0.355 m
2
(3.82 ft
2
)
Arm of the horizontal tail
4.18 m (13.7 ft)
Deflection
Up -20
o
Deflection
Down
+16
o
Airfoil
NACA
0011
Angle of attack
0
o
2.8.3 Vertical Tail:
Height
1.19
m
(3.9
ft)
Root chord
0.99 m (3.2 ft)
Tip chord
0.65 m (2.1 ft)
Area
0.949
m
2
(10.2 ft
2
)
Rudder
Area
0.294
m
2
(3.15 ft
2
)
Deflection
+/-
35
o
Airfoil
E
474
2.8.4 Fuselage:
Length
8.24 m (27.1 ft)
Width
0.64 m (2.1 ft)
Height
1.1
m
(3.6
ft)
Max. Cross Section
0.48 m
2
(4.9 ft
2
)
2.8.5 Engine:
Type
Rotax
503
UL
SCDI
two
cylinders,
two
stroke, with type B reducer 1:2
Cooling Air
cooled
Cylinder capacity
496.7 ccm (30.0 cu.in.)
Stroke
61
mm
(2.40
in.)
Bore
72
mm
(2.82
in.)
Performance
37 kW / 6500 rpm
TST-14 M – Aircraft Manual
rev.0 issued 2006-11-29 – page 9 of 40
