Description
• Crew: 1 pilot
• Capacity: 1 passenger
• Payload: 210 kg
• Length: 6.02 m
• Wingspan: 8.08 m
• Height: 1.98 m
• Empty weight: 440 kg
• Useful load: 210 kg
• Max. takeoff weight: 650 kg
• Powerplant: 75 kW,max.5 minutes, 71 kW
• Propellers:
Proof of Concept - Prince Aircraft Company, four-bladed "P-Tip"
Production Prototype - Sensenich 3 Blade Rotax Ground Adjustable Propeller propeller
• Propeller diameter: 1.7 m
• Cockpit width: 1.2 m at the shoulder
• Fuel capacity: 87 L; 19 imp gal, 64 kg
• Length on road: 5.72 m with elevator up
• Width on road: 2.29 m with wings folded
• Height on road: 2.03 m
• Rear wheel drive on road
Avionics
Glass panel; the proof-of-concept airplane included
- Dynon Avionics EFIS-D100 Electronic Flight Information System with HS34 Nav and GPS Connectivity
- Dynon Avionics EMS-D120 Engine Monitoring System
The production prototype uses a glass cockpit including:
- Dynon Avionics SkyView SV-D1000
- XCOM Avionics VHF Transceiver
- Transition custom touch screen dashboard computer