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| SIMPLE, FORCEFUL
& 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 255 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.
- Tricycle retractable landing gear.
- 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.
- Detachable wing.
- Well finished and comfortable interiors.
- Very good visibility.
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| DIMENSIONS
P300 S & (P300 N) |
| WING SPAN |
7.55
m |
| WING REFERENCE SURFACE |
10
mq (11 mq) |
| FUSELAGE LENGTH |
6.25
m |
| CABIN WIDTH |
1.05 m |
| CABIN HEIGHT |
1.05 m |
| WEIGTHS |
| EMPTY OPERATIVE WEIGHT |
285
Kg |
| MAXIMUM TAKE OFF WEIGHT (ULM) |
450 Kg |
| MAXIMUM TAKE OFF WEIGHT (JAR-VLA) |
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) |
165
Kg |
| OVERALL PAY LOAD LIMIT (JAR-VLA) |
245
Kg |
| BAGGAGE VOLUME |
226 l |
| MAXIMUM BAGGAGE AMOUNT |
20 Kg |
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PERFORMANCES (ROTAX 912S, FIXED PITCH PROPELLER,
SEA LEVEL, P300S & P300N) |
| MAXIMUM LEVELLED SPEED |
285
km/h (270 km/h) |
| CRUISE SPEED (@ 75% POWER) |
255
km/h (240 km/h) |
| STALL SPEED |
65
km/h (62 km/h) |
| RAPID CIMB SPEED |
120
km/h |
| STEEP CLIMB SPEED |
100
km/h |
| BEST RATE OF CLIMB |
460
m/min (1500 ft/min) |
| ROLL SPEED |
120°/sec |
| AERODYNAMIC EFFICIENCY |
13:1
(12.5:1) |
| RANGE @ 75% POWER |
1000
km |
| RANGE @ 75% POWER WITH AUXILIARY TANK |
1450
km |
| FUEL CONSUMPTION @ 75% POWER |
18.5
l/h |
| OPERATIVE CEILING ALTITUDE |
6000
m |
| TAKE OFF & LANDING GROUND RUNNING
|
120
m |
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| Generals |
- Rotax Engine 912 UL 80 hp.
- 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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