SPECIFICATIONS

Wing Span: 28 Feet, 2 Inches
Length:21 Feet, 8 Inches
Height: 7 Feet, 8 Inches
Wing Area: 107 Square Feet
Aspect Ratio7.29:1
Empty Weight:730 Pounds
Gross Weight:1,320 Pounds
Fuel Capacity34 Gallons
Fuel Economy: 4.5 Gallons/Hour
Powerplant:Rotax 912S (100HP)
Propellers: Two (2) blade composite
Airfoil Type:C 180, 13.8% Thick


CTLS

PERFORMANCE

Cruise Speed (@ 75% power)115 kts
Stall Speed (VS0)39 kts
VNE145 kts
Climb Rate805 fpm
Max. Range; 34 Gal. no reserve 4300 RPMCTLS 830 miles, CTLSi 1005 Mi
Takeoff Roll (@ Wg)800 feet
Glide Ratio (engine off)8.5:1


3-view drawing
3-view drawings

Rotax® 912S
Rotax® 912S4 cylinder, 4 stroke liquid/air cooled engine with opposed cylinders, dry sump forced lubrication with separate 3l (.8 gal US) oil tank, automatic adjustment by hydraulic valve tappet, 2 CD carburetors, mechanical fuel pump, electronic dual ignition, electric starter, integrated reduction gear i= 2.43.

912 ULS / S kWHPRPMNmft. lb.RPMMax RPM
Normal69.0/73.58* i95/100 i5500/5800 i * 5 min1289451005800
Max 5 minute (takeoff)73.51005800    
UnitsBoreStrokeDisplacementCompression Ratio
Metric84 mm61 mm1,352 cc10.5:1
American3.31 in2.40 in82.6 cid 

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