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French Civil Aircraft

Caudron Simoun
Specifications for C.630 from Wikipedia

General characteristics
Crew: 1-2: pilot and (optional) co-pilot
Capacity: 2 passengers
Length: 9.10 m (29 ft 10 in)
Wingspan: 10.4 m (34 ft 2 in)
Height: 2.3 m (7 ft 7 in)
Wing area: 16 m² (170 ft²)
Empty weight: 755 kg (1,660 lb)
Max takeoff weight: 1,380 kg (3,040 lb)
Powerplant: 1× Renault Bengali 6Q-09 six-cylinder inline engine, 220 hp (160 kW)

Performance
Maximum speed: 300 km/h (160 knots, 190 mph)
Range: 1,500 km (810 nm, 930 mi)
Service ceiling: 6,000 m (20,000 ft)

Variants
- C.500 Simoun I - experimental, one built.
- C.520 Simoun - experimental, one built.
- C.620 Simoun IV - experimental, one built.
- C.630 Simoun - initial production version with Renault Bengali 6Pri engine, 20 built.
- C.631 Simoun - modified version with a Renault Bengali 6Q-01 engine, three built.
- C.632 Simoun - similar to C.631, one built.
- C.633 Simoun - modified fuselage with a Renault Bengali 6Q-07 engine, 6 built.
- C.634 Simoun - modified wing and take-off weight with either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 3 built.
- C.635 Simoun - improved cabin layout and either a Renault Bengali 6Q-01 or Renault Bengali 6Q-09 engine, 46 built and conversions from earlier versions.
- C.635M Simoun - military version with either a Renault Bengali 6Q-09 or Renault Bengali 6Q-19 engine, 489 built.

Romano R.82
OTL aircraft, 160 produced by 1940.

General characteristics
Crew: 2
Length: 7.82 m (25 ft 7 in)
Wingspan: 9.88 m (32 ft 5 in)
Height: 3.34 m (10 ft 11½ in)
Wing area: 23.72 m² (255.33 ft²)
Empty weight: 918 kg (2024 lb)
Gross weight: 1328 kg (2928 lb)
Powerplant: 1 × Salmson 9Aba radial piston engine, 209 kW (280 hp)

Performance
Maximum speed: 240 km/h (149 mph)
Range: 660 km (410 miles)
Service ceiling: 6500 m (21325 ft)

Development Timeline
- First Flight: 1933

Salmson Phrygane
Historical Aircraft

General characteristics
Crew: One pilot
Capacity: 2 passengers
Length: 7.83 m (25 ft 8 in)
Wingspan: 11.70 m (38 ft 5 in)
Height: 2.35 m (7 ft 8 in)
Wing area: 22.5 m² (242 ft²)
Empty weight: 650 kg (1,433 lb)
Gross weight: 1,100 kg (2,425 lb)
Powerplant: 1 × Salmson 9Nc, 101 kW (135 hp)

Performance
Maximum speed: 195 km/h (122 mph)
Range: 1,000 km (620 miles)
Service ceiling: 5,800 m (19,024 ft)

Salmson Cricri
Historical Aircraft

General characteristics
Crew: One pilot
Capacity: 1 passenger
Length: 6.89 m (22 ft 7 in)
Wingspan: 9.66 m (31 ft 8 in)
Height: 2.18 m (7 ft 2 in)
Wing area: 16.0 m² (172 ft²)
Empty weight: 287 kg (633 lb)
Gross weight: 575 kg (1,268 lb)
Powerplant: 1 × Salmson 9Adr, 45 kW (60 hp)

Performance
Maximum speed: 150 km/h (94 mph)
Range: 500 km (310 miles)
Service ceiling: 2,450 m (8,040 ft)

Max Holste MH.52

Specifications
Crew: 2
Length: 7.25 m (23 ft 9 in)
Wingspan: 9.80 m (32 ft 1¾ in)
Height: 2.18 m (7 ft 1¾ in)
Wing area: 14 m2 (150.7 ft2)
Empty weight: 640 kg (1411 lb)
Gross weight: 870 kg (1918 lb)
Powerplant: 1 × Renault 4P inline piston engine, 112 kW (150 hp)

Performance
Maximum speed: 230 km/h (143 mph)
Range: 600 km (373 miles)