GCA1 Pedro
| GCA1 Pedro | |
|---|---|
| Type: | Training aircraft / liaison aircraft |
| Manufacturer: | |
| First flight: |
1953 |
| Production time: |
1953 |
| Number of pieces: |
1 piece |
The GCA1 Pedro was a two-seat, single-engine light aircraft produced by the Italian Gruppo Costruzioni Aeronautiche . It was a wooden construction with plywood planking and designed as a braced high-decker with a rear wheel . The two seats next to each other had double controls .
Technical specifications
| Parameter | Data |
|---|---|
| crew | 2 |
| length | 6.29 m |
| span | 10.13 m |
| height | 2.46 m |
| Wing area | 13.01 m² |
| Wheelbase nose wheel-main landing gear | 2.00 m |
| Maximum take-off mass | 1820 kg |
| Ascent time to 1000 meters | 6:30 min |
| Summit height | 5350 m |
| Cruising altitude | 4300 m |
| Empty mass | 340 kg |
| Max. Takeoff mass | 578 kg |
| Engine type | CNA D |
| Propeller | Two-leaf |
| Engine power | 60 hp |
| Top speed | 170.6 km / h |
| Cruising speed | 150 km / h |
| Normal range | 550 km |