SETCA Milan
The SETCA Milan was a French-built two-seat light utility aircraft of the 1940s.
| SETCA Milan | |
|---|---|
 | |
| The SETCA Milan prototype at Moisselles airfield near Paris in May 1957 | |
| Role | two-seat light utility aircraft |
| National origin | France |
| Manufacturer | SETCA |
| First flight | 1947 |
| Status | withdrawn |
| Number built | 1 |
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| |
Design and development
The Milan was designed by Messrs. Laboureix and Lagrevol as a two-seat side-by-side light utility aircraft. It was of all-wood construction with a fixed spatted tricycle undercarriage and had dual controls. Powered by a 90 h.p. Regnier 4-EO engine, it first flew in 1947.[1]
Production and service
The Milan obtained its CNRA in August 1949. Its normal certificat de navigabilite was awarded in 1952. The prototype F-BCZZ was flown until at least 1957, but plans for further production did not reach fruition.[2]
Specifications
Data from Green, 1955, p. 166
General characteristics
- Crew: two
- Length: 24 ft 1 in (7.34 m)
- Wingspan: 32 ft 9 in (9.98 m)
- Height: not available ()
- Empty weight: 1,210 lb (549 kg)
- Loaded weight: 1,742 lb (790 kg)
- Powerplant: 1 × Regnier 4-EO inverted air-cooled inline, 90 hp (67 kW)
Performance
- Maximum speed: 122 mph (196 km/h)
- Cruise speed: 112 mph (180 km/h)
- Range: 434 miles (700 km)
References
- Notes
- Bibliography
- Green, William (1955). The Aircraft of the World. Macdonald & Co. (Publishers) Ltd.
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