| Manufacturer | Globe |
| Model | GC-1 Swift |
| Modification | GC-1B |
| Country | USA |
| Years | 1941 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.94 m |
| Length | 6.38 m |
| Height | 1.88 m |
| Wing area | 12.23 m2 |
| Zero fuel weight | - |
| Empty weight | 503 kg |
| Maximum takeoff weight | 758 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Continental C-125-2 |
| Power | 1 x 125 HP |
| Thrust | - |
| Maximum speed | 233 km/h |
| Cruising speed | 212 km/h |
| Rate of climb | - |
| Practical range | 676 km |
| Service ceiling | 4330 m |
| Hovering ceiling | - |
| Crew | 2 |
