| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Piper Aircraft |
| Model | Piper PA-61 Aerostar |
| Country | United States |
| Manufactured from | 1967 year |
| Manufactured to | 1984 year |
| Type | Twin Turboprops |
| Icao | PA61 |
| Performance | |
| Engine | 2x Lycoming IO-540-K |
| Power, hp | 290 hp |
| Power, lbf | Add |
| Avionics | Dual Collins VHF-250 , Dual VIR-350 etc. |
| Max cruise speed | 444 km/h |
| Approach speed | 137 km/h |
| Travel range | 1,969 km |
| Fuel economy | Add |
| Service ceiling | 7,620 m |
| Rate of climb | 9.14 m/sec |
| Take off distance | 759 m |
| Landing distance | 619 m |
| Weights | |
| Max take off weight | 2,721 kg |
| Max landing weight | 2,721 kg |
| Max payload | 930 kg |
| Fuel tank capacity | 670 l |
| Baggage volume | 0.85 m³ |
| Dimensions | |
| Seats | 6 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.22 m |
| Cabin width | 1.25 m |
| Cabin length | 3.8 m |
| Exterior length | 10.61 m |
| Tail height | 3.7 m |
| Fuselage diameter | 1.35 m |
| Wing span | 11.18 m |
| Wing tips | No Winglets |