Alpi Aviation Pioneer 300

The Asso V Champion was built by Alpi Aviation with composite skin panels as the Pioneer 300.

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.

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.

Variation: Keli SkySpark

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