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| SIMPLE, POWERFUL
& ELEGANT |
The wood liability & the composite material
surface finish joined into a performance aircraft
for everybody, the skilled pilot and the just
licensed one: cruise speed @75% power equal
to 265 km/h (S version with the shorter wing
span), stall speed equal to 65 km/h, retractable
landing gear and capability to operate in short
fields.
The aircraft could be operated in long range
trips or simple flights around the airfield,
actually is the best compromise between performances,
fuel consumption and flight quality.
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The aircraft
manoeuvrability and controllability, together
with its stability, make it easy to be flown by
the aerobatic pilot, with extraordinary satisfaction,
up to the flying school student, that will be
supported by the aircraft during their learning
activity.
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- Low wing.
- Rotax 914 Engine installation.
- Tricycle retractable landing gear
with oil-air shock absorbers.
- Electrical landing gear retraction
with manual emergency actuation.
- Stearable nose landing gear.
- 2 place, side by side arrangements
with double control stick.
- Tractive propeller.
- Mixed composite material and wood
structure.
- Three axis trim system.
- Well finished and comfortable interiors.
- Very good visibility.
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| DIMENSIONS |
| WING SPAN |
7.55
m |
| WING REFERENCE SURFACE |
10
mq |
| FUSELAGE LENGTH |
6.25
m |
| CABIN WIDTH |
1.05 m |
| CABIN HEIGHT |
1.05 m |
| WEIGHTS |
| EMPTY OPERATIVE WEIGHT |
290
Kg |
| MAXIMUM TAKE OFF WEIGHT (ULM) |
450 Kg |
| MAXIMUM DESIGNTAKE OFF WEIGHT |
530
Kg |
| LOADS |
| IN FLIGHT LOAD FACTORS |
+4
/ -2 g |
| TANK CAPACITY |
80
l |
| INSTALLABLE AUXILIARY TANK CAPACITY |
32
l |
| OVERALL PAY LOAD LIMIT (ULM) |
160
Kg |
| DESIGN PAY LOAD LIMIT |
240
Kg |
| BAGGAGE VOLUME |
226 l |
| MAXIMUM BAGGAGE AMOUNT |
20 Kg |
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PERFORMANCES
(ROTAX 914 DCDI, FIXED PITCH PROPELLER, SEA LEVEL) |
| MAXIMUM LEVELLED SPEED |
295
km/h |
| CRUISE SPEED (@ 75% POWER) |
265
km/h |
| STALL SPEED |
65
km/h |
| RAPID CIMB SPEED |
120
km/h |
| STEEP CLIMB SPEED |
100
km/h |
| BEST RATE OF CLIMB |
520
m/min (1700 ft/min) |
| ROLL SPEED |
120°/sec |
| AERODYNAMIC EFFICIENCY |
12.5:1 |
| RANGE @ 75% POWER |
990
km |
| RANGE @ 75% POWER WITH AUXILIARY TANK |
1430
km |
| FUEL CONSUMPTION @ 75% POWER |
20.4
l/h |
| OPERATIVE CEILING ALTITUDE |
7000
m |
| TAKE OFF & LANDING GROUND RUNNING
|
110
m |
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| Generals |
- Rotax Engine 914 UL DCDI.
- Electric Landing Gear.
- 2 Fuel Tanks 40 lt each.
- Electric Flap.
- Electric Elevator trim.
- Radio Predisposition.
- Central Tunnel with Objects Recovery.
- Cockpit Air Vents.
- Auxliliary Electric Socket.
- Tools.
- Flight Manual - Check list.
- Maintenance Manual.
- Standard Blue Upholstery.
- Pioneer Protective Cover.
- White Body with Two Stripes.
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| Instruments |
- Speedmeter.
- Altimeter.
- Vario.
- Turn Coordinator.
- Compass.
- RPM Counter with Hour Counter.
- 2 Fuel Level Indicators.
- Cooling Temperature Indicator.
- Oil Temperature Indicator.
- Oil Pressure Indicator.
- Voltmeter.
- Amperometer.
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