Technical characteristics

Technical characteristics
General characteristics
Capacity: 6 passengers (4 VIP)
Length: 10.7 m (35 ft,1 in)
Wingspan: 14.9 m (48 ft, 10 in)
Height: 3 m (9ft, 10in)
Wing area: 19 m2 (204 sq ft)
Empty Weight: 1250 kg (2755 lb)
Max takeoff weight: 2,300 kg (5,071 lb)
Fuel capacity: 480 L / 127 Gal / 373 kg / 822 lb
Powerplant: 2 x Lycomming O-360 B 180 hp each (Optional Superior XP-360 Engine, 180 hp)
or 2 x Higgs Diesel E 330J/G (NA) (JET A / AUTO / 100LL / HYDROGEN GAS) 300HP
or 2 x Higgs Diesel E 330J/G-T (FI) (JET A / AUTO / 100LL / HYDROGEN GAS) 500HP
Propellers: MT PROPELLER MTV-12-B-C-F-R(M) CFR180-53, HOFFMANG V-123K3-RS (Pushing, 3-bladed, Reversible, with Full Feathering)

Performance:
Useful Load 1400 lbs (635 kg)
Usable Fuel Volume 110 gal (416 l)
Service Ceiling 9800 ft (2987 m)
Maximum Limit Speed 190 kias (352 kmph)
Maximum Cruise Speed 165 kias (305 kmph)
Economy Cruise Speed 145 kias (270 kmph)
Maximum Range at 50% Load 1200 nm (2000 km)
Maximum Range at Full Load 600 nm (1000 km)
Maximum Climb Rate 1180 fpm (360 mpm)
Takeoff Distance (land) 820 ft (250 m)
Takeoff Distance (water) 1000 ft (305 m)
Takeoff Speed at Full Load 50 kias (93 kmph)
Landing Speed at Full Load 50 kias (93 kmph)
Maximum Load Factors +3,8G / -1,9G