First produced in 1935, the Aiglon was built in two versions; the C.600 powered by a 100 hp Renault 4 Pgi, and the C.601 powered by a 140 hp Renault 4 Pei.

A tandem two-seat light monoplane of wooden construction with stressed plywood skin.

C.600
Engine: Renault 4 Pgi, 100 hp

C.601
Engine: Renault 4 Pei, 140 hp
Wingspan: 37 ft 4 in
Length: 24 ft 11 in
Height: 6 ft 7 in
Wing area: 156 sq.ft
Empty weight: 1276 lb
Loaded weight: 1936 lb
Max speed: 140 mph
Cruise: 124 mph
Landing speed: 34 mph
Service ceiling: 19,680 ft
Range: 335 mi

Single-seat

The Caudron C.530 Rafale (Gust of wind) was a French two-seat competition aircraft. The Rafale’s two seats were in tandem, one over the wing and the other just behind the trailing edge, under a long (about a third of the fuselage length), narrow multi-framed canopy with a blunt, vertical windscreen and sliding access.

The Rafale was intended as a competition aircraft and in 1934 it was very successful. On 8 July, Rafales took the first three places in the Angers 12-hour event and later that month filled the top six Esders Cup positions. Late in August, one won the Zénith Cup with a flight over the prescribed 1,578 km (981 mi) course at 240 km/h (149.1 mph).

Only seven were built.

The Caudron C.510 Pélican was a 1930s French air ambulance or touring monoplane. Designed and built by Caudron and based on the earlier Caudron C.282/8.

To create room for a stretcher and attendant the earlier Caudron C.282/8 design was modified with a lengthened fuselage, an improved wing and tailplane design. A single-engined high-wing monoplane, the Pélican had a conventional landing gear. As a touring aircraft the Pélican could carry three passengers. First flying in 1934, a total of 62 were built as both air ambulances and tourers.

The C.510 was operated in the Belgian Congo by Force Publique, and by the French Air Force.

Gallery

Specifications:

Ambulance
Engine: 1 × Renault 4Pei Bengali Junior, 100 kW (140 hp)
Wingspan: 11.82 m (38 ft 9 in)
Wing area: 23.75 m2 (255.6 sq ft)
Length: 8.52 m (27 ft 11 in)
Height: 2.25 m
Empty weight: 626 kg (1,380 lb)
Max takeoff weight: 1,140 kg (2,513 lb)
Maximum speed: 185 km/h (115 mph; 100 kn)
Cruising speed: 165 km/h (103 mph; 89 kn)
Stall: 43.47 mph
Range: 1,000 km (621 mi; 540 nmi)
Service ceiling: 4000 m
Crew: 1
Capacity: 2 (Stretcher and attendant)

The Caudron C.480 Frégate was a French three-seat touring monoplane designed by Maurice Devlieger and built by Société des avions Caudron.

Based on the earlier Caudron C.280 the Frégate was a high-wing braced monoplane with an enclosed cabin for the pilot with two side-by-seats behind for passengers. Powered by a front-mounted 140 hp (104 kW) Renault 4Pei inline piston engine it had a tailwheel landing gear. First flown in 1935, the company built 27 Frégates, in 1939, 20 were requisitioned into service with the French Air Force for liaison work.

Engine: 1 × Renault 4Pei, 100 kW (140 hp)
Length: 8.18 m (26 ft 10 in)
Wingspan: 11.90 m (39 ft 1 in)
Height: 2.12 m (6 ft 11 in)
Wing area: 20.00 m2 (215.3 sq ft)
Empty weight: 600 kg (1,323 lb) equipped
Max takeoff weight: 1,050 kg (2,315 lb)
Maximum speed: 210 km/h (130 mph; 113 kn)
Cruising speed: 185 km/h (115 mph; 100 kn)
Range: 850 km (528 mi; 459 nmi)
Service ceiling: 4,500 m (14,764 ft)
Crew: 1
Capacity: 2