| Manufacturer |
Aircraft Designs Inc |
| Description |
The ADI Stallion is a US civil utility aircraft that first flew in July 1994. |
| First Flight |
1994-07-01 |
| Designer |
Martin Hollmann |
| Type |
Light utility aircraft |
| Length (m) |
7.62 |
| Height (m) |
2.9 |
| Max Seating |
5 |
| Max Speed (km/h) |
493 |
| Cruise Speed (km/h) |
474 |
| Min Speed (km/h) |
115 |
| Max Ceiling (m) |
9750 |
| Rate of Climb (m/s) |
13.2 |
| Capacity Description |
5 passengers |
| National Origin |
United States of America |
| Number Built |
7 |
| Powerplant Description |
1 × Continental TSIO-550-B air-cooled turbocharged flat-six engine, 224 kW (300 hp) each |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/ADI_Stallion |
| Flat Wing Span (m) |
10.67 |
| Flat Wing Area (m²) |
13 |
| Flat Wing Aspect Ratio |
8.8 |
| Number of Engines |
1 |