|Role||Civil utility aircraft|
The Farman F.190 was a utility aircraft built in France in the 1920s and 1930s. It was a high-wing, strut-braced monoplane of conventional configuration with a fully enclosed cabin and fixed, tailskid undercarriage. Popular both as a private aircraft and in the air taxi role, some 30 examples were also operated by airlines in France and elsewhere in Europe. Fifteen of these joined Air France's fleet in 1933 from the fleets of the smaller airlines it had absorbed.
A dedicated air ambulance version was built as the F.197S (for "Sanitaire") with provision for two litters and an attendant.
In 1932, a version with a slightly enlarged cabin, revised tail fin, and four-blade propeller entered production as the Farman F.390.
Data from: Aviafrance
- main production version with a 170 kW (230 hp) Gnome et Rhône 5Ba engine, 57 built.
- Powered by a 180 kW (240 hp) Gnome et Rhône 5Bc for long distance flying, one built for a customer in Portugal.
- version with a 170 kW (230 hp) Salmson 9Ab engine, 22 built.
- version with a 210 kW (280 hp) Salmson 9Aba engine, 2 built.
- version with a 190 kW (250 hp) Farman 9Ea engine, 22 built.
- version with a 210 kW (280 hp) Farman 9Ebr engine, one built.
- version with a 190 kW (250 hp) Hispano-Suiza 6Mb engine, 4 built.
- version with a 170 kW (230 hp) Salmson 9Ab engine, 6 built for Venezuela.
- version with a 220 kW (300 hp) Gnome & Rhône 7Kb engine, one built.
- version with a 180 kW (240 hp) Lorraine 7Me Mizar engine, 9 built.
- F.197S air ambulance version of F.197
- version with a 190 kW (250 hp) Renault 9Pa engine, 2 built.
- version with a 220 kW (300 hp) Lorraine 9Na Algol engine, 6 built.
- version with a 110 kW (150 hp) Farman 7Ear engine, 6 built
- version with a 140 kW (190 hp) Farman 9Ecr engine, 4 built
- version with a 110 kW (150 hp) Farman 7Ear engine, 4 built
- version with a 140 kW (190 hp) Farman 9Ecr engine, 11 built
- Crew: One pilot
- Capacity: 4 passengers
- Length: 10.45 m (34 ft 4 in)
- Wingspan: 14.40 m (47 ft 3 in)
- Height: 3.00 m (9 ft 10 in)
- Wing area: 10.2 m2 (433 ft2)
- Empty weight: 926 kg (2.041 lb)
- Gross weight: 1,800 kg (3,968 lb)
- Powerplant: 1 × Gnome et Rhône 5Ba, 172 kW (230 hp)
- Maximum speed: 185 km/h (115 mph)
- Range: 850 km (528 miles)
- Service ceiling: 5,150 m (16,895 ft)
|Wikimedia Commons has media related to Farman.|
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 379.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 894 Sheet 16.
- Farman aircraft on aviafrance.com
- [Parmentier, Bruno. "Farman". Retrieved 11 November 2013. - Farman aircraft]