Engineering:SPCA 20
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 | This article relies largely or entirely on a single source. (November 2023) |
| SPCA 20 | |
|---|---|
| Role | Torpedo seaplane |
| National origin | France |
| Manufacturer | Société Provençale de Constructions Aéronautiques (SPCA) |
| Designer | Louis Paulhan and Pillard |
| First flight | 22 June 1928 |
| Number built | 2 |
The SPCA 20 was a French seaplane designed for torpedo bombing. It was a low-wing monoplane of all-metal construction.
Specifications
Data from Aviafrance:SPCA 20[1]
General characteristics
- Crew: Four
- Length: 18.62 m (61 ft 1 in)
- Wingspan: 26.22 m (86 ft 0 in)
- Height: 6.40 m (21 ft 0 in)
- Wing area: 123.00 m2 (1,324.0 sq ft)
- Empty weight: 4,300 kg (9,480 lb)
- Gross weight: 7,300 kg (16,094 lb)
- Powerplant: 2 × Gnome-Rhône 9Ae Jupiter 9-cylinder direct-drive air-cooled radial piston engines, 360 kW (480 hp) each
- Propellers: 2-bladed fixed pitch propellers
Performance
- Maximum speed: 180 km/h (110 mph, 97 kn)
- Range: 1,200 km (750 mi, 650 nmi)
- Service ceiling: 5,000 m (16,000 ft)
References
- ↑ Parmentier, Bruno. "SPCA 20" (in fr). Paris. https://www.aviafrance.com/s-p-c-a-20-aviation-france-4567.htm. Retrieved 26 February 2019.
Bibliography
- Espérou, Robert (July 1989). "Les SPCA: Le SPCA II type 20" (in Fr). Le Fana de l'Aviation (236): 40–43.
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