The Jabiru J200 (2 seater)

The Jabiru J200 (2 seater) has evolved from combining the best features of the LSA, SP & UL models. It comes with the standard LSA wings with the fuel in the wings. The longer tail boom results in more elevator and empennage authority, reducing the stall speed to 45 kts and increasing directional stability. The J200 was developed as a replacement to the GA alternatives i.e. Cessna 172. The aircraft had its maiden flight in Bundaberg on the 16th of March.
Jabiru have increased the Maximum Take Off Weight (MTOW) is now 544Kg All of the Jabiru kit plane models have been structurally tested to 8.5g.

specifications

Powerplant Jabiru 3300cc
Propeller 2 Blade Fixed Pitch Wooden/Composite 60" dia x 53" pitch
Length 21' 5"
Height 7' 2"
Wing span 26’ 4"
Wing area 86.1 sq.ft)
Seats 2 Seats
Useful load 858 lbs
Gross weight [GVW] 1197 lbs
Fuel capacity Fuel capacity
Range 558sm
Takeoff distance, ground roll 640ft
Max speed 130kts
Cruise speed 120kts
Landing distance, ground roll 640ft
Service ceiling 15,000ft
Design maneuvering speed (Va) 90kts
Never exceed speed (Vne) 138kts
Stall, power off (Vsl) 45kts