Pioneer 300 Turbo

PIONEER 300 - 914 TURBO

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.

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.

DESCRIPTION

Low wing

Rotax 914 Engine installation

Tricycle retractable landing gear with oil-air shock absorbers

Retrazione elettrica carrello con sistema di emergenza manuale

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

SPECIFICATIONS

DIMENSIONS
Wing Span	7,55 m
Wing Reference Surface	10 mq
Fuselage Length	6,25 m
Cabin Width	1,05 m
Cabin Heigth	1,05 m

WEIGHTS
Empty Operative Weight	290 Kg
Maximum Takeoff Weight (ULM)	450 Kg
Maximum Design Takeoff Weight	530 Kg

LOADS
In Flight Load Factors	+4 / -2 g
Tank Capacity	80 lt
Installable Auxiliary Tank Capacity	32 lt
Overall Payload Limit (ULM)	160 Kg
Overall Design Payload Limit (VLA)	240 Kg
Baggage Volume	226 l
Maximum Baggage Amount	20 Kg

PERFORMANCES

ROTAX 914 DCDI - FIXED PITCH PROPELLER - SEA LEVEL
Maximum Levelled Speed	295 Km/h
Cruise Speed (@ 75% Of Power)	265 Km/h
Stall Speed	65 Km/h
Rapid Climb Speed	120 Km/h
Steep Climb Speed	100 Km/h
Best Rate Of Climb	520 m/min 1700 ft/min
Roll Rate	120° /sec


Aerodynamic Efficiency	12.5:1
Range @ 75% Of Power	990 Km
Range @ 75% Of Power With Aux. Tank	1430 Km
Fuel Consumption @ 75% of Power	20.4 lt/h
Operative Ceiling Altitude	7000 m
Takeoff Running	110 m
Landing Running	110 m

STANDARD EQUIPMENTS

Rotax Engine 914 UL DCDI	INSTRUMENTS
	Speedmeter
Electric Landing Gear	Altimeter
2 Fuel Tanks 40 lt each	Vario
Electric Flap	Turn Coordinator
Electric Elevator trim	Compass
Radio Predisposition	Fiber instrument panel and consolle
Central Tunnel with Objects Recovery	RPM Counter with Hour Counter
Cockpit Air Vents	2 Fuel Level Indicators
Auxliliary Electric Socket	Cooling Temperature Indicator
Tools	Oil Temperature Indicator
Flight Manual - Check list	Oil Pressure Indicator
Maintenance Manual	Voltmeter
Standard Blue Upholstery	Amperometer
Pioneer Protective Cover
White Body with Two Stripes