

Download XT-912 SST Tundra Specifications
| PERFORMANCE | Australian | European | USA | |||
| Never Exceed Speed (Vne) indicated | 85 | kts | 157 | km/hr | 98 | mph |
| Manoeuvring Speed (Va) indicated | 80 | kts | 148 | km/hr | 92 | mph |
| Cruise Speed @ MTOW | 75 | kts | 139 | km/hr | 86 | mph |
| Stall Speed @ MTOW | 35 | kts | 65 | km/hr | 40 | mph |
| Climb Rate(49 kts) @ MTOW 450kg | 925 | ft/min | 4.7 | m/sec | 925 | ft/min |
| Best Climb Speed | 49 | kts | 91 | km/hr | 56 | mph |
| Take off Distance to 15 mts or 50 feet- Note 1 | 235 | m | 235 | m | 771 | ft |
| Land Distance @ MTOW from 15 mts- Note 1 | 320 | m | 320 | m | 1050 | ft |
| Descent Rate 54 kts @ MTOW | 770 | ft/min | 3.9 | m/sec | 770 | ft/min |
| Glide Angle at 54 kts @ MTOW | 6.5 | :1 | 6.5 | :1 | 6.5 | :1 |
| Fuel Tank Capacity - Note 3 | 70 | lt | 70 | lt | 18.5 | gal |
| Typical Fuel Burn @ Cruise (MTOW) | 11 | lt/hr | 11 | lt/hr | 2.9 | gal/hr |
| Range @ Cruise | 786 | km | 786 | km | 488 | miles |
| NOTE 1: Take off and landing distances were measured from a short grass runway. | ||||||
| NOTE 2: Fuel consumption figures are included as a guide only. The consumption figures should not be used for planning purposes. | ||||||
| NOTE 3: Maximum usable fuel 67 Liters or 17.7 US Gal | ||||||
| DESIGN LOADS | Australian | European | USA | |||
| Max take off weight (MTOW / W Max) | 450 | kg | 450 | kg | 992 | lbs |
| Max Base Weight (W susp) | 392 | kg | 392 | kg | 864 | lbs |
| Ultimate load @ MTOW | +6g / -3g | |||||
| Flight limits @ MTOW | +4g / -0g | |||||
| Total maximum crew weight | 200 | kg | 200 | kg | 441 | lbs |
| Permitted range of pilot weight (Front Seat) | 55-100 | kg | 55-100 | kg | 121-220 | lbs |
| Permitted range of pilot weight (Rear Seat) | 0-100 | kg | 0-100 | kg | 0-220 | lbs |
| Maximum empty weight - Note 4 | 265 | kg | 265 | kg | 584 | lbs |
| NOTE 4: Includes minimum fuel 1 hr full power and 2 x 86kg pilot | ||||||
| DIMENSIONS | Australian | European | USA | |||
| Wing Span | 9.46 | m | 9.46 | m | 31.0 | ft |
| Wing Area | 12.9 | sq mts | 12.9 | sq mts | 139 | sq ft |
| Aspect Ratio | 6.9 | |||||
| Wing Weight | 57 | kg | 57 | kg | 126 | lbs |
| Overall Height (Control Bar Fwd) | 3.07 | m | 3.07 | m | 10.1 | ft |
| Trike Width (to outside of wheels) | 1.91 | m | 1.91 | m | 6.3 | ft |
| Trike Length | 2.75 | m | 2.75 | m | 9.0 | ft |
| Wheel Track | 1.16 | m | 1.16 | m | 3.8 | ft |
| Trike Height | 1.70 | m | 1.70 | m | 5.6 | ft |
| Cockpit Width | 0.70 | m | 0.70 | m | 2.3 | ft |
| Wing (Packed) Length | 5.30 | m | 5.30 | m | 17.4 | ft |
| Wing Length (Short Packed) | 4.20 | m | 4.20 | m | 13.8 | ft |
| POWER PLANT | PROPELLOR | |||||
| Make | Rotax Bombardier | Propellor | Bolly | |||
| Model | 912 UL2 | Type | Bos# 68x58_SL ground adjustable | |||
| Power | 80 | Hp | Diameter | 68" | ||
| Type | 4 Stroke-1198cc | Pitch | 20 +/- 0.5 deg @ radius of 24" | |||
| Ignition System | Dual Electronic | |||||
| No Cylinders | 4 | |||||
| Electric Start | Standard | |||||
| Reduction Ratio | 2.43:1 | |||||