|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.
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- Crew: 2
- Capacity: 6 passengers
- Powerplant: 1 × Walter Bora radial engine, 175 kW (235 hp)
- Related development
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- 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.