|The prototype S.210M exhibited at the 1971 Paris Air Show at Le Bourget Airport in June 1971|
|Role||Twin-engined cabin monoplane|
|First flight||19 February 1970|
|Developed from||SIAI-Marchetti S.205|
The S.210 was developed from the single-engined S.205 and was an all-metal low-wing cantilever monoplane with a retractable tricycle landing gear. It was powered by two 200 hp (149 kW) Avco Lycoming TIO-360-A1B engines, one mounted on the leading edge of each wing. It had three pairs of side-by-side seats for one pilot and five passengers.
The prototype S.210M first flew on 18 February 1970 and was exhibited at the 1971 Paris Air Show wearing a military style colour scheme and markings. This aircraft was followed by an improved second prototype with increased baggage capacity and enlarged rear windows. A production batch of ten aircraft were built based on the second prototype.
- Crew: 1
- Capacity: 5
- Length: 8.83 m (29 ft 0 in)
- Wingspan: 11.63 m (38 ft 1¾ in)
- Height: 3.33 m (10 ft 11¼ in)
- Wing area: 17.23 m2 (185.5 ft2)
- Empty weight: 1,030 kg (2,271 lb)
- Gross weight: 1,850 kg (4,078 lb)
- Powerplant: 2 × Avco Lycoming TIO-360-A1B flat-four piston engine, 149 kW (200 hp) each
- Maximum speed: 357 km/h (222 mph)
- Cruising speed: 314 km/h (195 mph)
- Range: 1,900 km (1,180 miles)
- Service ceiling: 8,100 m (26,500 ft)
- Rate of climb: 10 m/s (1,980 ft/min)
|Wikimedia Commons has media related to SIAI-Marchetti.|
- Taylor 1971, p.131.
- Taylor, John W. R. (1971). Jane's All The World's Aircraft 1971-72. London: Jane's Yearbooks. ISBN 0-354-00094-2.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 206.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 2854.