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 |