Societe Francaise Deviation Nouvelle SFAN 5

The two-seat SFAN 5 was a one-off enclosed variant of the earlier SFAN 4, first flying in 1936.

Engine: 1 × Train 4T, 45 kW (60 hp)
Propeller: 2-bladed fixed-pitch pusher
Wingspan: 12.5 m (41 ft 0 in) (10.3 m (34 ft))
Wing area: 18 m2 (190 sq ft) (16.2 m2 (174 sq ft))
Length: 7.05 m (23 ft 2 in)
Empty weight: 285 kg (628 lb)
Gross weight: 500 kg (1,102 lb)
Maximum speed: 115 km/h (71 mph, 62 kn)
Cruise speed: 120 km/h (75 mph, 65 kn)
Landing speed: 45 km/h (28 mph; 24 kn)
Range: 450 km (280 mi, 240 nmi)
Time to altitude: 1,000 m (3,300 ft) in 6 minutes
Wing loading: 30.8 kg/m2 (6.3 lb/sq ft)
Power/mass: 11.17 kg/kW (18.37 lb/hp)
Crew: 2

Societe Francaise Deviation Nouvelle SFAN 2 / SFAN 4

Licensed for British BAC Drone 1935; modified to suit French requirements as the single seat SFAN 2, powered by a 25 hp Ava engine.

A larger, two-seat side-by-side model to same formula was SFAN 4, powered by a 35 hp Mengin engine. Only two SFAN 4 were built.

It was reported that the French Air Ministry ordered forty Drones from the French company.

The SFAN 5 was a one-off enclosed variant of the earlier SFAN 4.

Societe De Recherches Et De Constructions Mecaniques / SRCM

Originally a specialist in aircraft hydraulic systems, began small-scale construction of aircraft for other small manufacturers. After failing to obtain a license to build the CAB Supercab, designed a new lightplane known as the SRCM-153 Joigny, which first flew in March 1960. This was a three/four-seat monoplane with rectractable landing gear, powered by a Lycoming engine.