|Role||Single-engined transport cabin monoplane|
The SM.101 was a single-engined low-wing cantilever monoplane with a tailwheel landing gear with retractable main gear. It had an enclosed cabin for two crew and six passengers and was powered by a nose-mounted 235 hp (175 kW) Walter Bora radial engine. The prototype and only SM.101 first flew on 20 December 1947 but the company soon decided that a single-engined passenger transport was not likely to sell and the company developed the design with two engines as the SM.102.
Data from Jane's all the World's Aircraft 1947
- Crew: 2
- Capacity: 6 passengers
- Length: 10.2 m (33 ft 6 in)
- Wingspan: 16.5 m (54 ft 2 in)
- Height: 3 m (9 ft 10 in)
- Wing area: 29.91 m2 (321.9 sq ft)
- Aspect ratio: 9
- Empty weight: 1,320 kg (2,910 lb)
- Gross weight: 2,190 kg (4,828 lb)
- Powerplant: 1 × Walter Bora 9-cylinder air-cooled radial engine, 175 kW (235 hp)
- Maximum speed: 240 km/h (149 mph; 130 kn) at sea level
- Cruise speed: 225 km/h (140 mph; 121 kn) 70% power at 2,750 m (9,020 ft)
- Landing speed: 75 km/h (47 mph; 40 kn)
- Range: 1,250 km (777 mi; 675 nmi)
- Service ceiling: 4,800 m (15,700 ft)
- Wing loading: 73.2 kg/m2 (15.0 lb/sq ft)
- Power/mass: 12.71 kg/kW (20.9 lb/hp)
- Related development
|Wikimedia Commons has media related to SIAI-Marchetti.|
- Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. p. 150c.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. pp. 2853–4.