| Manufacturer | Cranfield |
| Model | A1 |
| Modification | A1 |
| Country | United Kingdom |
| Years | 1976 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.00 m |
| Length | 8.05 m |
| Height | - |
| Wing area | 15.00 m2 |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | 850 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Avco Lycoming IO-540-D |
| Power | 1 x 250 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 240 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 8858 m |
| Hovering ceiling | - |
| Crew | 1 |
