| Manufacturer | Curtiss |
| Model | T-32 Condor II |
| Modification | AT-32 |
| Country | USA |
| Years | 1933 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 24.99 m |
| Length | 14.80 m |
| Height | 4.97 m |
| Wing area | 112.22 m2 |
| Zero fuel weight | - |
| Empty weight | 5550 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 7938 kg |
| Flight duration | - |
| Engine | 2 Wright R-1820F Cyclone |
| Power | 2 x 720 HP |
| Thrust | - |
| Maximum speed | 306 km/h |
| Cruising speed | 269 km/h |
| Rate of climb | - |
| Practical range | 1152 km |
| Service ceiling | 7010 m |
| Hovering ceiling | - |
| Crew | 2 |
