| Attribute | Kawasaki C-1 × | ATR 72-500 × |
|---|---|---|
| General | ||
| Manufacturer | Kawasaki | ATR Aircraft |
| Model | Kawasaki C-1 | ATR 72-500 |
| Country | Japan | France |
| Manufactured from (year) | 1970 | 1989 |
| Manufactured to (year) | 1981 | - |
| Type | Military Transport Planes | Passenger Turbo Props |
| Icao | C1 | - |
| Performance | ||
| Engine | 2x Pratt & Whitney JT8D-M-9 | 2 × Pratt & Whitney Canada PW127F - |
| Power, hp (hp) | - | 2,475 |
| Power, lbf (lbf) | 14,500 | - |
| Max cruise speed (km/h) | 806 | 319 |
| Approach speed (km/h) | 250 | - |
| Travel range (km) | 1,300 | 3,056 |
| Service ceiling (m) | 11,579 | 7,600 |
| Rate of climb (m/sec) | 17.75 | - |
| Take off distance (m) | 2,190 | 1,220 |
| Landing distance (m) | 1,180 | 1,067 |
| Weights | ||
| Max take off weight (kg) | 38,700 | 22,800 |
| Max landing weight (kg) | 23,320 | - |
| Max payload (kg) | 11,900 | 7,350 |
| Fuel tank capacity (l) | 52,996 | 24,227 |
| Baggage volume (m³) | - | 0.7 |
| Dimensions | ||
| Seats | 5 | 74 |
| Cabin width (m) | - | 2.57 |
| Exterior length (m) | 29 | 27.2 |
| Tail height (m) | 9.99 | - |
| Fuselage diameter (m) | - | 7.6 |
| Wing span (m) | 30.6 | 27 |
| Wing tips | No Winglets | No Winglets |