

| XT-912 SPECIFICATIONS | ||||
| PERFORMANCE | XR-S | |||
| Never Exceed Speed (Vne) indicated | kts | 85 | ||
| mph | 98 | |||
| km/h | 157 | |||
| Manoeuvring Speed (Va) indicated | kts | 80 | ||
| Never exceed in turbulent air | mph | 92 | ||
| km/h | 148 | |||
| Cruise Speed @ MTOW | kts | 70 | ||
| mph | 81 | |||
| km/h | 130 | |||
| Trim Speed | kts | 60-65 | ||
| mph | 69-75 | |||
| km/h | 111-120 | |||
| Stall Speed @ 450kg (MTOW) | kts | 35 | ||
| mph | 40 | |||
| km/h | 65 | |||
| Stall Speed @ 320kg | kts | 31 | ||
| mph | 36 | |||
| km/h | 57 | |||
| Climb Rate @ MTOW 450kg | ft/m | 925 | ||
| at recommended climb speed | m/s | 4.7 | ||
| Recommended Climb Speed | kts | 49 | ||
| Take Off Safety Speed | mph | 56 | ||
| km/h | 91 | |||
| Take off Run | ft | 344 | ||
| Measure from short grass run way | m | 105 | ||
| Take off Distance to 15 mts or 50 feet- Note 1 | ft | 771 | ||
| Measure from short grass run way | m | 235 | ||
| Maximum Cross Wind | kts | 15 | ||
| Max gust factor of 5-10 kts. | mph | 17 | ||
| km/h | 28 | |||
| Land Distance @ MTOW from 15 mts- Note 1 | ft | 1050 | ||
| Measure from short grass run way | m | 320 | ||
| Descent Rate 49 kts @ MTOW | ft/m | 650 | ||
| m/s | 3.3 | |||
| Glide Angle at 49 kts @ MTOW | angle | 7.18 | ||
| Glide Distance from 1000 ft | miles | 1.4 | ||
| km | 2.2 | |||
| Typical Fuel Burn @ Cruise (MTOW) | L/hr | 10.5 | ||
| US Gal/hr | 2.8 | |||
| Range @ Cruise | miles | 459 | ||
| Max useable fuel 56 litres (17.7US Gallon) | km | 739 | ||
| DESIGN LOADS | XR-S | |||
| Max take off weight (MTOW / W Max) | kg | 450 | ||
| pound | 992 | |||
| Wing Weight | kg | 57 | ||
| pound | 126 | |||
| Max Base Weight (W susp) | kg | 393 | ||
| pound | 866 | |||
| Typical Empty Weight | kg | 241 | ||
| Standard XT3 Base (no options) 184kg | pound | 531 | ||
| Useable Load | kg | 209 | ||
| Optional Equipment Excluded | pound | 461 | ||
| Pilot weight range (Front Seat) | kg | 55-115 | ||
| (Max total load 215kg - 482lb) | pound | 224-258 | ||
| Pilot weight range (Rear Seat) | kg | 0-115 | ||
| (Max total load 215kg - 482lb) | pound | 0-258 | ||
| DIMENSIONS (Tundra base) | XR-S | |||
| Wing Span | m | 9.5 | ||
| ft | 31.0 | |||
| Wing Area | sq m | 12.9 | ||
| sq ft | 139 | |||
| Aspect Ratio | 6.9 | |||
| Wing Weight | kg | 57.0 | ||
| pound | 126 | |||
| Overall Height (Control bar forward) | m | 3.1 | ||
| ft | 10.1 | |||
| Trike Width (To outside of wheels) | m | 1.9 | ||
| ft | 6.3 | |||
| Trike Length | m | 2.8 | ||
| ft | 9.0 | |||
| Wheel Track | m | 1.7 | ||
| ft | 5.6 | |||
| Wheel Base | m | 1.9 | ||
| ft | 6.2 | |||
| Trike Height (Mast Folded Down) | m | 1.7 | ||
| ft | 5.6 | |||
| Cockpit Width | m | 0.76 | ||
| ft | 2.5 | |||
| Wing (Packed) Length | m | 5.3 | ||
| ft | 17.4 | |||
| Wing Length (Short Packed) | m | 4.0 | ||
| ft | 13.1 | |||
| POWER PLANT | ||||
| Make | Rotax | |||
| Model | 912 UL | |||
| Power | 80 | Hp | ||
| Type | 4 Stroke-1211cc | |||
| Ignition System | Dual Electronic | |||
| No Cylinders | 4 | |||
| Electric Start | Standard | |||
| Reduction Ratio | 2.43:1 | |||
| Fuel Limitations | ||||
| Maximum Usable Fuel | Litre | 56 | ||
| UK Gal | 12.3 | |||
| US Gal | 14.8 | |||