Samiksha Jaiswal (Editor)

SETCA Milan

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
196 km/h

Length
  
7.34 m

Wingspan
  
9.98 m

First flight
  
1947

SETCA Milan httpsuploadwikimediaorgwikipediacommonsthu

The SETCA Milan was a French-built two-seat light utility aircraft of the 1940s.

Contents

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.

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.

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

    SETCA Milan Wikipedia
    (Text) CC BY-SA


    Similar Topics