Serial Number: 1203
14
Flaps deflections
15° / 30° / 45°
Horizontal tail plane span
2.8m
Horizontal tail plane surface
2.24m
2
Vertical tail plane surface
1.04m
2
Control surface deflections:
Ailerons
up
......... 23°
down ......... 12°
Elevator
up
......... 21°
down ......... 10°
Rudder
left
......... 23°
right ......... 25°
(b) Weights
Empty weight, per UL–2
320,5kg
Take-off weight, maximum
472.5kg
(c) Engine
Type (brief description): Rotax 912S 100HP – four-stroke, four-cylinder engine, air-cooled
cylinders with water-cooled heads, integrated reduction gearbox, dual electronic ignition.
Swept volume
1400ccm
Take-off power, max.
73.5kW@5800rpm
Cruising power, max.
69.0kW@5500rpm
Dry weight
56kg
including accessories
72kg
Fuel (fuel grade, octane index)
Natural 95
Oil (type)
SHELL HELIX H x 7AV 10W-40
Oil capacity
3L
Reduction gear (gear ratio)
2.43:1
Fuel tank volume – main tank
100L
(d) Propeller
Diameter / pitch at 75%
In-flight adjustable propeller SR-3000/3N
Weight
5kg
Material
Composite
The propeller shall be sent to the manufacturer for inspection in case of even the slightest
damage or if crack is found. Flying with damaged propeller may endanger life and limb and is
prohibited.
2.8
Aircraft equipment
(a) Instruments
Type
Serial No.
Speed indicator
LUN 1106
673
Altimeter
BG-3E
1316
Compass
CM-13
016
Climb & descent indicator
BC10-1B
1605
Tachometer
VDO COCKPIT
333025015 x
Cylinder temperature gauge
CHT/100 ROAD
0542
Oil-temperature gauge
R 2011
0561
Oil-pressure gauge
ROAD
0531
