The Jabiru J200 had a new style wing. The profile remains the same as the short wing but with a changed internal structure. Gone ares the foam core and two 50 litre fuel tanks occupy the space. The new wing is not a retrofit to existing Jabiru models as the attachment points are quite different. However an optional fuel in wing aerofoil is being considered for the ear-lier aircraft.
The four seat J400 model is basically the same as the J200 with two seats in the rear of the cabin and Jabiru 330 engine of 120 hp. J-200 Engine: Jabiru 3300, 120 hp Length: 21.5 ft / 6550mm Wing span: 26.5 ft / 8100mm Wing area: 87 sq.ft Height: 2200mm Empty weight: 627 lb / 310kg Gross weight: 1540 lb / 700 kg Useable load: 390 kg Fuel capacity: 36 USG Vne: 138 kts Cruise: 138 mph / 115 kts Stall: 55 mph / 48kt Vso: 60kts Range: 520nm Rate of climb: 1000 fpm Takeoff dist: 950 ft Landing dist: 650 ft Cockpit width: 44 in / 1120mm Cabin height: 1090mm Landing gear: nosewheel Endurance: 4.4 hrs. Fuel consumption @ cruise: 23 1t/hr. Seats: 2.
J-400 Engine: Jabiru 3300, 120 hp Prop: 60 in fixed pitch Length: 21 ft 6 in / 6.55m Height: 7 ft 3 in / 2.2 m Wing span: 26 ft 7 in / 8.1 m Wing area: 86 sq.ft Empty weight: 720 lb / 310 kg Gross weight: 1543 lb / 700 kg Useful load: 390 kg Fuel capacity: 36 USG Vne: 138 kt Max speed: 130 kt Cruise: 120 kt / 138 mph Stall: 55 mph / 48 kt Vso: 60 kt Rate of climb: 1000 fpm Takeoff dist: 950 ft Landing dist: 650 ft Service ceiling: 15,000 ft Seats: 4 Cockpit width: 44 in / 1.12 m Cockpit height: 43 in / 1.09m Landing gear: nose wheel Max wing loading: 17.9 lb/sq.ft Load factors: +3.8/-1.9G Range: 720 sm Range 45 min res: 520 nm Max endurance 45 min res: 4.4 hr