Jabiru J200

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 kitplane models have been structurally tested to 8.5g.

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
Jabiru 3300cc
2 Blade Fixed Pitch Wooden/Composite 60" dia x 53" pitch
21' 5"
7' 2"
26 4"
86.1 sq.ft)
2
x
858 lbs
1197 lbs
36 USgals
558sm

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
640ft
x
130kts
120kts
640ft
15,000ft

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
90kts
138kts
45kts
x

All specifications are based on manufacturer's calculations