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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.
p-300-stddview 

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  
iso-9001-2008-2