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Flightstar IISL
The Flightstar 11 which was introduced
in 1992, traces its roots back to the early days of ultralight
aviation. It was one of the first mass produced craft offered
by a financially secure company. The design utilizes aluminium tube
bolt together construction covered in Dacron sail cloth. Seating is
side by side in a 42 inch wide cabin.
Building times are in the 150 to 200 hour range. The latest
production models have folding wings for easy storage. The craft can
be purchased in two configurations completely enclosed or with a
fibreglass nose cone and windshield.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Rotax
503FA (496 C.C. 54HP @ 6800 RPM) 2.58 /1
reduction ratio
Ivo-prop.
3-BLADE 68”
19
ft.7in
7
ft 10in
32
ft
157
sq ft
2
385
lbs
x
950
lbs
10
gal
200 miles |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
205
ft
600
fpm
x
65
mph
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
96
mph
36
mph
x |
All specifications are based on manufacturer's
calculations |
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