Comparison of Beechcraft Premier 2 and Grumman C-1 Trader [S]ave
| Attribute |  Beechcraft Premier 2 × |  Grumman C-1 Trader × |
|---|---|---|
| General | ||
| Manufacturer | Hawker Beechcraft | Grumman |
| Model | Beechcraft Premier 2 | Grumman C-1 Trader |
| Country | United States | United States |
| Manufactured from (year) | 2010 | 1955 |
| Type | Light Business Jets | Military Propellor Planes |
| Icao | - | G96 |
| Performance | ||
| Engine | 2 X Williams FJ44-3AP | 2x Wright R-1820-82WA Cyclone |
| Power, hp (hp) | - | 1,525 |
| Power, lbf (lbf) | 3,000 | - |
| Max cruise speed (km/h) | 859 | 444 |
| Travel range (km) | 3,022 | 1,778 |
| Fuel economy (km/l) | 1.468 | - |
| Service ceiling (m) | 13,716 | 7,620 |
| Rate of climb (m/sec) | 0.06 | 9.91 |
| Take off distance (m) | 915 | - |
| Landing distance (m) | 747 | - |
| Weights | ||
| Max take off weight (kg) | 30,423 | 13,222 |
| Max payload (kg) | 862 | 3,000 |
| Fuel tank capacity (l) | 2,025 | - |
| Dimensions | ||
| Seats | 6 | 3 |
| Cabin height (m) | 1.65 | - |
| Cabin width (m) | 1.68 | - |
| Cabin length (m) | 5 | - |
| Exterior length (m) | 16.5 | 12.9 |
| Tail height (m) | - | 4.9 |
| Fuselage diameter (m) | - | 1.7 |
| Wing span (m) | - | 21.2 |
| Wing tips | - | No Winglets |
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