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TORNADO II (Titan aircraft)
The Tornado 11 introduced in 1992 is a
tandem seating two place, trigear, in a pusher configuration. The
fuselage is welded 4130 chromoly while the wing is all pop riveted
aluminium. Building times reported in the 250 to 350 hour range. The
kit includes all required material, components and fasteners. The
kit does not include the engine, propeller, and instruments. The
control system is standard stick and rudder. Entrance is through
doors located on one side of the plane, front entrance easy, rear
seat a little harder. Cabin width is 24 inches.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Rotax 618
x
19'-0"
6'-6"
23'-6"
108 sq
ft
x
440 lb
x
1000 lb
10 gal
275 mi |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
300 ft
1600 fpm
x
110 mph
250 ft
12,500 ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
150 mph
35 mph
x |
All specifications are based on manufacturer's
calculations
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