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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
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