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