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The SIAI-Marchetti S.210 was a 1970s Italian twin-engined cabin-monoplane designed and built by SIAI-Marchetti as a development of the single-engined SIAI-Marchetti S.205.

S.210
The prototype S.210M exhibited at the 1971 Paris Air Show at Le Bourget Airport in June 1971
Role	Twin-engined cabin monoplane Type of aircraft
Manufacturer	SIAI-Marchetti
First flight	19 February 1970
Number built	12
Developed from	SIAI-Marchetti S.205

Development

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.

Specifications (S.210)

Data from Jane's All The World's Aircraft 1971-72 [1]

General characteristics

• Crew: 1
• Capacity: 5 passengers
• Length: 8.83 m (29 ft 0 in)
• Wingspan: 11.63 m (38 ft 2 in)
• Height: 3.33 m (10 ft 11 in)
• Wing area: 17.23 m² (185.5 sq ft)
• Empty weight: 1,030 kg (2,271 lb)
• Gross weight: 1,850 kg (4,079 lb)
• Fuel capacity: 360 L (95 US gal; 79 imp gal)
• Powerplant: 2 × Avco Lycoming TIO-360-A1B flat-four piston engine , 150 kW (200 hp) each
• Propellers: 2-bladed Hartzell HC-C2YK-1B/8468-10R constant-speed propellers, 1.88 m (6 ft 2 in) diameter

Performance

• Maximum speed: 357 km/h (222 mph, 193 kn) at sea level
• Cruise speed: 314 km/h (195 mph, 170 kn) at 2,400 m (8,000 ft) (econ cruise)
• Range: 1,900 km (1,200 mi, 1,000 nmi) with maximum payload
• Service ceiling: 8,100 m (26,600 ft)
• Rate of climb: 10.1 m/s (1,980 ft/min)
• Take-off distance to 15 m (50 ft): 400 m (1,310 ft)
• Landing distance from 15 m (50 ft): 550 m (1,800 ft)

See also

Related development

• SIAI-Marchetti S.205
• SIAI-Marchetti S.208

References

Wikimedia Commons has media related to SIAI-Marchetti S.210.

• 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.

На других языках

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[de] SIAI-Marchetti S.210

Die SIAI-Marchetti S.210 war ein leichtes, zweimotoriges Reise- und Geschäftsflugzeug des italienischen Flugzeugbauers SIAI-Marchetti aus den 1970er-Jahren.

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- [en] SIAI-Marchetti S.210

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[it] SIAI-Marchetti S-210

Il SIAI-Marchetti S.210 è stato un aereo executive bimotore monoplano .mw-parser-output .chiarimento{background:#ffeaea;color:#444444}.mw-parser-output .chiarimento-apice{color:red}costruito[quale, quanti, tutti nel 1970?] nel 1970 dalla SIAI-Marchetti, derivato dal monomotore SIAI-Marchetti S-205.[2] Destinato al mercato dell'aviazione generale, volò per la prima volta nel 1970; ne vennero prodotti in totale 12 esemplari.

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