All performance figures and specifications are at a maximum takeoff weight of 544 kg as permitted by Australian RAA regulations, the aircraft however is approved for operations up to 560 kg in the LSA category.
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Technical Data
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TL 2000 Sting Carbon
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TL 96 Star
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Basic information and dimensions
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Engine options
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Rotax 912, 80, 100 or 115 hp
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Rotax 912, 80, 100 or 115 hp
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Propeller
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3 blade Woodcomp propeller available in fixed pitch, variable pitch or constant speed
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3 blade Woodcomp propeller available in fixed pitch, variable pitch or constant speed
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Length
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5.93 m
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Height
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2.3 m
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Cabin width - shoulder height
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1.25 m
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1.25 m
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Main wheel-spacing
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1.65 m
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1.65 m
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Wheelbase
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1.63 m
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1.63 m
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Tyre pressure
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25 PSI
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25 PSI
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Brakes
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Hydraulic disk brakes
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Hydraulic disk brakes
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Suspension main undercarriage
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Tyres, flexibility of undercarriage
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Tyres, flexibility of undercarriage
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Suspension front wheel
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Coil spring
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Coil spring
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Tyre sires all wheels
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14 x 4 (350 x 100)
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14 x 4 (350 x 100)
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Wing
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Centre of gravity limits
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22 - 34% MAC
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Wing profile
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MS (1)-0313
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Wingspan
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8.44 m
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Wing area
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9.85 m2
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12.1 m2
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Aspect ratio
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7.26
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Wing loading
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55.5 kg/m2 MTOW
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Design load limit
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+6 G and -4G
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Tested load limit
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+12 G and -9G
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Aileron span
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865 mm
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Flap area
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1.72 m2
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Flap span
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5.28 m
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4.94 m
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Aileron deflection down
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15°
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Aileron deflection up
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30°
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Flap deflection take off
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15°
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Flap deflection landing
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30°
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Elevator
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Elevator span
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2.68 m
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Elevator area
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0.75 m2
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Elevator deflection up
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30°
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Elevator deflection down
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30°
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Rudder
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Rudder span
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1.09 m
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Rudder area
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0.64 m2
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Rudder deflection left
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30°
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Rudder deflection right
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30°
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Weights
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Weight of empty aircraft
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290 kg
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305 kg
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Maximum takeoff weight
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544 kg (560 kg)
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544 kg (560 kg)
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Maximum payload – people, fuel luggage etc
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254 kg
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239 kg
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Maximum weight of baggage
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15 kg
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15 kg
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Fuel
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Fuel capacity standard
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69 L or 80 L
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69 L
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Fuel capacity long range
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120 L or 150 L
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Performance specifications
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TL 2000 Sting Carbon
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TL 96 Star
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Performance information figures are based on a standard model with Rotax 100 hp 912 engine, in-flight adjustable propeller and maximum takeoff weight of 544 kg
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Takeoff rotation speed
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41 kn
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42 kn
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Climb speed
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66 kn
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70 kn
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Cruise speed 65% at 5000 RPM
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127 kn TAS
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105 kn
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Cruise speed 75% at 5200 rpm
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135 kn TAS
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115 kn
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Fuel consumption 75% power
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19.5 L per hour
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19.5 L per hour
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Fuel consumption 65% power
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15.6 L per hour
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15.6 L per hour
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Fuel consumption 55% power
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12.4 L per hour
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12.4 L per hour
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Maximum speed horizontal flight
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142 kn
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125 kn
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Touchdown speed
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35 kn
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35 kn
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Final approach speed
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66 kn
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60 kn
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Velocity never exceed VNE
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165 kn
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149 kn
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Va
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132 kn
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Vx
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68 kn
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Vy
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75 kn
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Initial rate of climb at sea level
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1150 feet per minute
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1150 feet per minute
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Service ceiling
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18,000 feet
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18,000 feet
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Maximum speed in turbulence
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115 kn
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97 kn
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Stalling speed with no flaps Vs1
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44 kn CAS
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40 kn CAS
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Stalling speed with flaps 35° Vso
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35 kn CAS
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34 kn CAS
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Maximum speed first grade flaps Vfe
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15° @ 77 kn
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Maximum speed second grade flaps Vfe
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30° @ 66 kn
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Glide ratio engine at idle
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16.8:1
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Glide ratio propeller stopped
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15.2:1
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Takeoff ground roll - short dry grass
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75 m
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Take off over 15 meter screen -still air from rest
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220 m
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Maximum cross wind
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15 kn
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Landing ground roll - short dry grass
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100 m
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Landing distance to full stop - over 15 meter screen still air
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200 m
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