SIAI-Marchetti p.210
The SIAI-Marchetti S.210 was a light, twin-engine travel and business aircraft produced by the Italian aircraft manufacturer SIAI-Marchetti in the 1970s.
History and construction
It was designed for one pilot and up to five passengers and equipped with two Lycoming four-cylinder boxer engines of the type TIO-360-A1B , each with a takeoff power of 200 hp.
The maximum speed was 375 km / h, the normal cruising speed 345 km / h at an altitude of 5,700 meters. The maximum range was 1,900 kilometers, the service ceiling was 8,500 meters. The curb weight was 1,080 kg, the maximum take-off weight 1,850 kg.
The first flight of the prototype took place on February 18, 1970. In 1971 the pre-series production of ten machines followed.
The S.210 is based in many parts and the basic construction of the cell on the single-engine machines from the same company as the SIAI-Marchetti S.205 and the SIAI-Marchetti S.208 . Around 35 machines of this type S.210 were produced.
Technical specifications
| Parameter | Data (p.210) |
|---|---|
| crew | 1 |
| Passengers | 5 |
| length | |
| span | |
| height | |
| Wing area | |
| Empty mass | 1,080 kg |
| Max. Takeoff mass | 1,850 kg |
| Cruising speed | 345 km / h |
| Top speed | 375 km / h |
| Service ceiling | 8,500 m |
| Range | 1,900 km |
| Engines | 2 × Lycoming TIO-360-A1B with 200 hp each |