2011 cockpit options - Download(PDF large MB)
SPECIFICATIONS
| Wing Span: | 28 Feet, 2 Inches |
| Length: | 21 Feet, 8 Inches |
| Height: | 7 Feet, 8 Inches |
| Cabin Width | 49 |
| Aspect Ratio | 7.29:1 |
| Empty Weight: | 790/ 810Pounds |
| Gross Weight: | 1,320 Pounds |
| Fuel Capacity | 34/35 Gallons |
| Fuel Economy: | 5.5/4.3 Gallons/Hour |
| Powerplant: | Rotax 912S or 912iS (100HP) 2000 TBO |
| Speed | 117 KTS |
| Economy Range @4300RPM | 830 NM /1055 NM |
PERFORMANCE
| Cruise Speed (@ 75% power) | 115 kts |
| Stall Speed (VS0) | 39 kts |
| VNE | 145 kts |
| Climb Rate | 805 fpm |
| Max. Range; 34 Gal. no reserve 4300 RPM | CTLS 830 miles, CTLSi 1005 Mi |
| Takeoff Roll (@ Wg) | 800 feet |
| Glide Ratio (engine off) | 8.5:1 |
3-view drawing
Rotax® 912S
4 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 | kW | HP | RPM | Nm | ft. lb. | RPM | Max RPM |
|---|---|---|---|---|---|---|---|
| Normal | 69.0 | 95 | 5500 | 128 | 94 | 5100 | 5800 |
| Max 5 minute (takeoff) | 73.5 | 100 | 5800 |
| Units | Bore | Stroke | Displacement | Compression Ratio |
|---|---|---|---|---|
| Metric | 84 mm | 61 mm | 1,352 cc | 10.5:1 |
| American | 3.31 in | 2.40 in | 82.6 cid |
