Délémontez-Cauchy DC.1
| DC.1 | |
|---|---|
| Role | Ultralight monoplane | 
| National origin | France | 
| Manufacturer | Délémontez-Cauchy | 
| Designer | Jean Délémontez | 
| First flight | July 6, 1980 | 
| Developed from | Jodel D.9 | 
The Délémontez-Cauchy DC.1 is a French ultralight monoplane designed by Jean Délémontez for amateur construction, derived from the Jodel D.9.
Specifications
Data from Les Avions Français de 1965 a 1990[1]
General characteristics
- Crew: 2
 - Length: 5.65 m (18 ft 6 in)
 - Wingspan: 7.4 m (24 ft 3 in)
 - Wing area: 9.56 m2 (102.9 sq ft)
 - Empty weight: 225 kg (496 lb)
 - Gross weight: 397 kg (875 lb)
 - Powerplant: 1 × Volkswagen 1,600 cm3 (98 cu in) conversion 4-cylinder air-cooled horizontally-opposed piston engine, 48 kW (65 hp)
 - Propellers: 2-bladed fixed-pitch propeller
 
Performance
- Maximum speed: 194 km/h (121 mph, 105 kn)
 - Cruise speed: 175 km/h (109 mph, 94 kn) 
 - Economical cruise speed: 140 km/h (87 mph; 76 kn)
 
References
External links
- Parmentier, Bruno (8 December 2017). "Délémontez-Cauchy DC.1". Aviafrance (in French). Paris. Retrieved 8 March 2019.