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Alpi Aviation Pioneer 300

 

pioneer300


The Pioneer 300 STD has an S version with a shorter wing span, retractable landing gear and is produced in Italy. Both the 200 and 300 are fitted with the AVTEK in flight adjustable prop. The Pioneer 300 has a 300 kph VNE, while remaining within the ultralight aircraft rules, and the first engines installed were Mid-West, obtaining the BFU (German Certification). The aircraft is a compromise between performances, fuel consumption and flight quality.


The tricycle retractable landing gear has electrical landing gear retraction with manual emergency actuation and a stearable nose landing gear. The 2 place, side by side arrangements has double control stick and detachable wing.

 

Alpi-Pio-300-2

 

Engine options include the Rotax 912 80 hp, Rotax 912S 100 hp, Jabiru 3300 120 hp, Jabiru 2200 80 hp, and Midwest wankel 110 hp.


The Pioneer 300 Turbo is a turbocharged version.


The Pioneer 300 Hawk is derived from the Pioneer 300 standard, maintains the P300 flight qualities and is equipped with a good quality & luxury interiors.
The detachable wing has a skin fully made of plywood and the retractable landing gear is equipped with a gas-oil damper system. The aircraft is equipped with the higher and more aerodynamic canopy. The instrument panel is made of composite materials and has a three dimensional shape.
The electrical landing gear retraction has a manual emergency actuation and stearable nose gear.

 

Engine: Rotax 912 UL, 80 hp
Wing Span: 7.55 m
Wing Area: 10 sq.m
Fuselage Length: 6.25 m
Cabin Width: 1.05 m
Cabin Height: 1.05 m
Empty Operative Weight: 290 Kg
Maximum Take Off Weight (Ulm): 450 Kg
Maximum Design take Off Weight: 530 Kg
Load Factors: +4 / -2 G
Tank Capacity: 80 lt (2 x 40 lt)
Auxiliary Tank Capacity: 32 lt
Pay Load Limit (Ulm): 160 Kg
Design Pay Load Limit: 240 Kg
Baggage Volume: 226 lt
Maximum Baggage Amount: 20 Kg
Aspect ratio: 13-1

Pioneer 300 STD
Engine: Rotax 912, 100 hp.
Prop: AVTEK.
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 135 kt / 155 mph / 250 kmh
VNE: 154 kt / 177 mph / 285 kmh
Empty Weight: 285 kg / 628 lbs
MTOW Weight: 472 kg / 1041 lbs
Climb Ratio: 1400 ft/min / 7,5 m/s
Glide Ratio: 1:14
Take-off distance (50ft obstacle): 490 ft / 150 m
Landing distance (50ft obstacle): 490 ft / 150 m

Pioneer 300 S
Engine: Rotax 912S, 100 hp       
Propeller: Fixed Pitch
Wing Span: 7.55 m
Wing Area: 10 sq.m
Fuselage Length: 6.25 m
Cabin Width: 1.05 m
Cabin Height: 1.05 m
Empty Operative Weight: 285 Kg
Maximum Takeoff Weight (Ulm): 450 Kg
Maximum Takeoff Weight (Jar-Vla): 530 Kg
Load Factors: +4 / -2 G
Tank Capacity: 80 lt
Auxiliary Tank Capacity: 32 lt
Overall Payload Limit (Ulm): 165 Kg
Overall Payload Limit (Jar-Vla): 245 Kg
Baggage Volume: 226 lt
Maximum Baggage Amount: 20 Kg
Maximum Levelled Speed: 285 Km/H)
Cruise Speed (@ 75% Power): 255 Km/H
Stall Speed: 65 Km/H
Best ROC Speed: 120 Km/H
Best Climb Angle Speed: 100 Km/H
Best Rate Of Climb: 460 M/Min (1500 Ft/Min)
Roll Speed: 120°/Sec
Range @ 75% Power: 1000 Km
Range @ 75% Power With Auxiliary Tank: 1450 Km
Operative Ceiling Altitude: 6000 m
Takeoff & Landing Ground Run: 120m

Pioneer 300 N

Engine: Rotax 912S, 100 hp
Propeller: Fixed Pitch
Wing Span: 7.55 m
Wing Area: 11 sq.m
Fuselage Length: 6.25 m
Cabin Width: 1.05 m
Cabin Height: 1.05 m
Empty Operative Weight: 285 Kg
Maximum Takeoff Weight (Ulm): 450 Kg
Maximum Takeoff Weight (Jar-Vla): 530 Kg
Load Factors: +4 / -2 G
Tank Capacity: 80 lt
Auxiliary Tank Capacity: 32 lt
Overall Payload Limit (Ulm): 165 Kg
Overall Payload Limit (Jar-Vla): 245 Kg
Baggage Volume: 226 lt
Maximum Baggage Amount: 20 Kg
Maximum Levelled Speed: 270 Km/H
Cruise Speed (@ 75% Power): 240 Km/H
Stall Speed: 62 Km/H
Best ROC Speed: 120 Km/H
Best Climb Angle Speed: 100 Km/H
Best Rate Of Climb: 460 M/Min (1500 Ft/Min)
Roll Speed: 120°/Sec
Range @ 75% Power: 1000 Km
Range @ 75% Power With Auxiliary Tank: 1450 Km
Operative Ceiling Altitude: 6000 m
Takeoff & Landing Ground Run: 120m

Pioneer 300 Hawk

Engine: Rotax 912S
Propeller: Variable Pitch
Wing Span: 7.55 m
Wing Area: 10 sq.m
Fuselage Length: 6.25 m
Cabin Width: 1.05 m
Cabin Height: 1.05 m
Empty Operative Weight: 290 Kg
Maximum Takeoff Weight (Ulm): 450 Kg
Maximum Takeoff Weight ((Jar-Vla): 530 Kg
Load Factors: +4 / -2 G
Tank Capacity: 80 lt (2 x 40 lt)
Auxiliary Tank Capacity: 32 lt
Overall Payload Limit (Ulm): 160 Kg
Overall Payload Limit (Jar-Vla): 240 Kg
Baggage Volume: 226 lt
Maximum Baggage Amount: 20 Kg
Maximum Levelled Speed: 285 Km/H
Cruise Speed (@ 75% Power): 255 Km/H
Stall Speed: 65 Km/H
Best ROC Cimb Speed: 120 Km/H
Best Climb Angle Speed: 100 Km/H
Best Rate Of Climb: 460 M/Min (1500 Ft/Min)
Roll Speed: 120°/Sec
Range @ 75% Power: 1000 Km
Range @ 75% Power With Auxiliary Tank: 1450 Km
Operative Ceiling Altitude: 6000 m
Takeoff & Landing Ground Run: 120 m

 

 


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