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Pioneer 300 Standard


PIONEER 300 STANDARD

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.

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
 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
 

SPECIFICATIONS

DIMENSIONS
 Wing Span
 7,55 m
 Wing Reference Surface
 10 mq (11 mq)
 Fuselage Length
 6,25 m
 Cabin Width
 1,05 m
 Cabin Heigth
 1,05 m
   
WEIGHTS
 Empty Operative Weight
 285 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)
 168 Kg
 Overall Design Payload Limit (VLA)
 245 Kg
 Baggage Volume
 226 l
 Maximum Baggage Amount
 20 Kg
   
   
   
   

PERFORMANCES

ROTAX 912S 100 HP - FIXED PITCH PROPELLER - SEA LEVEL
P300S (P300N)
Maximum Levelled Speed
 285 Km/h (270 Km/h)
Cruise Speed (@ 75% Of Power)  255 Km/h (240 Km/h)
Stall Speed
 65 Km/h (62 Km/h)
Rapid Climb Speed
 120 Km/h
Steep Climb Speed
 100 Km/h
Best Rate Of Climb
 460 m/min
 1500 ft/min
Roll Rate
 120° /sec
   
 
Aerodynamic Efficiency
 13:1 (12.5:1)
Range @ 75% Of Power
 1000 Km
Range @ 75% Of Power With Aux. Tank  1450 Km
Fuel Consumption @ 75% of Power  18,5 lt/h
Operative Ceiling Altitude
 6000 m
Takeoff Running
 120 m
Landing Running
 120 m
   

STANDARD EQUIPMENTS

 Rotax 912 UL 80 hp ENGINE
INSTRUMENTS
   Speedmeter
 Electric Landing Gear  Altimeter
 2 Fuel Tanks 40 lt each  Vario
 Electric Flap  Turn Coordinator
 Electric Elevator trim  Compass
 Radio Predisposition  RPM Counter with Hour Counter
 Central Tunnel with Objects Recovery  2 Fuel Level Indicators
 Cockpit Air Vents  Cooling Temperature Indicator
 Auxliliary Electric Socket  Oil Temperature Indicator
 Tools  Oil Pressure Indicator
 Flight Manual - Check list  Voltmeter
 Maintenance Manual  Amperometer
 Standard Blue Upholstery
 Pioneer Protective Cover  
 White Body with Two Stripes  

BROCHURE

iso-9001-2008-2