SETCA Milan
# SETCA Milan

The SETCA Milan was a French-built two-seat light utility aircraft of the 1940s manufactured by SETCA (Société d'Études Techniques et de Constructions Aéronautiques).

## 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 hp (67 kW) Regnier 4E.0 inverted inline 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 The Aircraft of the World

General characteristics

* Length: 7.34 m (24 ft 1 in)
* Wingspan: 9.98 m (32 ft 9 in)
* Empty weight: 1,210 kg (2,668 lb)
* Gross weight: 1,742 kg (3,840 lb)
* Powerplant: 1 × Regnier 4E.0 4-cylinder inverted air-cooled in-line piston engine, 67 kW (90 hp)
* Propellers: 2-bladed fixed pitch propeller

Performance

* Maximum speed: 196 km/h (122 mph, 106 kn)
* Cruise speed: 180 km/h (110 mph, 97 kn)
