| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Curtiss |
| Model | Curtiss O-52 Owl |
| Country | United States |
| Manufactured from | 1940 year |
| Manufactured to | 1942 year |
| Type | Military Propellor Planes |
| Icao | O52 |
| Performance | |
| Engine | 1x Pratt & Whitney R-1340-51 Wasp |
| Power, hp | 600 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 352 km/h |
| Approach speed | Add |
| Travel range | 1,128 km |
| Fuel economy | Add |
| Service ceiling | 6,401 m |
| Rate of climb | 6.35 m/sec |
| Take off distance | Add |
| Landing distance | Add |
| Weights | |
| Max take off weight | 2,433 kg |
| Max landing weight | Add |
| Max payload | Add |
| Fuel tank capacity | Add |
| Baggage volume | Add |
| Dimensions | |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 8 m |
| Tail height | 3.03 m |
| Fuselage diameter | 1.4 m |
| Wing span | 12.42 m |
| Wing tips | No Winglets |