Jabiru Aircraft J-200 / J-400

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