Top speed: 105 mph
Cruise: 85 mph
Stall: 35 mph
Range: 450 nm
Rate of climb: 800 fpm
Takeoff dist: 500 ft
Landing dist: 300 ft
Engine: Walter Mikron III, 65 hp
HP range: 50-90
Fuel capacity: 18 USG
Empty weight: 540 lb
Gross weight: 900 lb
Height: 5.5 ft
Length: 18.5 ft
Wing span: 29 ft
Wing area: 116 sq.ft
Seats: 1
Landing gear: tailwheel

A side by side two seater with standard undercarriage and high wing, the Aerocruiser has a fuselage and wing of fabric covered aluminium Conversion to floats takes one hour.

Engine: Rotax 912, 80 hp
Wing span: 9.75 m
Wing area: 16 sq.m
MAUW: 479 kg
Empty weight: 239 kg
Fuel capacity: 41 lt
Max speed: 169 kph
Cruise speed: 135 kph
Minimum speed: 48 kph
Climb rate: 4.5 m/s
Fuel consumption: 10 lt/hr
Seats: 2
Certification: Canada
Price (1998): Can$43,500
Kit price (1998): Can$37,000

The Magnum light aircraft has an all composite hydraulic fully retracting tricycle undercarriage, 30% Fowler flaps with low drag cruise setting, 160 kts continuous cruise on 100 hp, 1000 nautical miles range, 200 kg crew, 50 kg baggage, room for skiis, 21:1 L/D ratio, and a max 21 deg alpha

Stall: 45 kt / 52 mph / 83 kmh
Cruise: 137 kt / 158 mph / 254 kmh
VNE: 155 kt / 178 mph / 287 kmh
Climb Ratio: 800 ft/min / 4 m/s
Glide Ratio: 21:1