| Manufacturer | CNA |
| Model | PM.1 |
| Modification | PM.1 |
| Country | Italy |
| Years | 1940 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.00 m |
| Length | 6.50 m |
| Height | 2.20 m |
| Wing area | 14.00 m2 |
| Zero fuel weight | - |
| Empty weight | 420 kg |
| Maximum takeoff weight | 630 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 CAN D.IX |
| Power | 1 x 60 HP |
| Thrust | - |
| Maximum speed | 172 km/h |
| Cruising speed | 150 km/h |
| Rate of climb | - |
| Practical range | 540 km |
| Service ceiling | 4500 m |
| Hovering ceiling | - |
| Crew | 2 |
