| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Rockwell International |
| Model | Rockwell Commander 112 / 114 |
| Country | United States |
| Manufactured from | 1972 year |
| Manufactured to | 2005 year |
| Type | Private Single Engine |
| Icao | AC11 |
| Performance | |
| Engine | 1x 1 × Lycoming IO-540-T4B5D |
| Power, hp | 260 hp |
| Power, lbf | Add |
| Avionics | Garmin GNC-300XL |
| Max cruise speed | 307 km/h |
| Approach speed | 104 km/h |
| Travel range | 1,356 km |
| Fuel economy | 5.083 km/l |
| Service ceiling | 5,304 m |
| Rate of climb | 5.44 m/sec |
| Take off distance | 655 m |
| Landing distance | 366 m |
| Weights | |
| Max take off weight | 1,479 kg |
| Max landing weight | 1,424 kg |
| Max payload | 446 kg |
| Fuel tank capacity | 265 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 4 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.24 m |
| Cabin width | 1.19 m |
| Cabin length | 1.9 m |
| Exterior length | 7.63 m |
| Tail height | 2.57 m |
| Fuselage diameter | 1.3 m |
| Wing span | 9.98 m |
| Wing tips | No Winglets |