Farman F.430

F.430

Farman F.430 of the Spanish Republican Air Force
Role	Light transport monoplane
Manufacturer	Farman Aviation Works
First flight	1934
Number built	3

The Farman F.430 was a 1930s French light transport designed and built by the Farman Aviation Works. Two variants with different engines were known as the F.431 and F.432.

Design and development

The F.430 was a low-wing cantilever monoplane with a tail-wheel landing gear. It was powered by two wing-mounted de Havilland Gipsy Major piston engines. The enclosed cockpit and cabin had room for a pilot and five passengers. The prototype F-ANBY appeared in 1934 and the F.431 variant with 185 hp (138 kW) Renault Bengali-Six inverted piston engines was exhibited at the 1934 Paris Salon de l'Aeronautique. A further variant with 180 hp (134 kW) Farman radial engines was designated the F.432.

After the company had been nationalised and became part of SNCAC a variant with a retractable landing gear (designated the Centre 433) was completed. The F.430 and two F.431s were used by Air Service between Paris and Biarritz.

Variants

F.430: Prototype with 130hp (97kW) de Havilland Gipsy Major I inline piston engines, one built.
F.431: Variant with 185hp (138kW) Renault 6Pdi inverted piston engines, two built.
F.432: Variant with 180hp (134kW) Farman radial engines or Renault 6Q-06 engines, two built and two converted from the F.431s.
Centre 433: Retractable landing gear version of the F.431, powered by 220 hp (160 kW) Renault 6Q-06 / Renault 6Q-O7 engines (left and right hand rotation), one built / converted, flying for the first time in December 1938.

Operators

France

Air Service

Spain

Spanish Republican Air Force^[1]

Specifications (F.430)

Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759

General characteristics

Crew: 1
Capacity: 5 passengers
Length: 11.70 m (38 ft 4½ in)
Wingspan: 15.40 m (50 ft 6¼ in)
Height: 2.82 m (9 ft 3 in)
Wing area: 36 m² (387.51 ft²)
Empty weight: 1306 kg (2879 lb)
Gross weight: 2200 kg (4850 lb)
Powerplant: 2 × de Havilland Gipsy Major 4-cylinder inverted inline piston, 97 kW (130 hp) each

Performance

Maximum speed: 210 km/h (130 mph)
Range: 1000 km (621 miles)
Service ceiling: 4500 m (14,765 ft)

References

↑ Spain - Air Force Farman F.430

The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1759

External links

Media related to Farman at Wikimedia Commons

Aircraft produced by Henri Farman, Maurice Farman, and Farman Aviation Works

Henri Farman	HF.6 HF.7 HF.10 HF.14 HF.16 HF.19 HF.20 HF.21 HF.22 HF.23 HF.24 HF.26 HF.27 HF.30 HF.206

Maurice Farman	MF.6 MF.7 MF.8 MF.9 MF.11 MF.16

Freres Farman/ Farman Aviation Works	I II III A.2 B.2 BN.4 F.3X F.4X F.21 F.30 F.31 F.40 F.41 F.50 (Landplane) F.50 (Flying Boat) F.51 F.56 F.60 F.60 Goliath F.63 Goliath FF.65 Sport Moustique F.70 F.73 F.80 F.110 F.120 F.130 F.140 F.150 F.160 F.162 F.166 F.167 F.168 F.169 F.170 F.180 F.190 F.200 F.209 F.211 F.220 F.230 F.250 F.270 F.280 F.290 F.300 F.310 F.350 F.360 F.370 F.380 F.390 F.400 F.410 F.420 F.430 F.450 F.455 F.460 F.470 F.480 F.500 F.510 F.520 F.1000 F.1010 F.1020

Aircraft produced by the Société Nationale de Constructions Aéronautiques du Centre (SNCAC)

NC.130 NC.150 NC.223 NC.4-10 NC.420 NC.433 NC.47-0 NC.47-1 NC.47-2 NC.510 NC.530 NC.600 NC.700 NC.701 NC.702 NC.832 NC.840 NC.841 NC.850 NC.851 NC.853 NC.854 NC.855 NC.856 NC.860 NC.900 NC.1070 NC.1071 NC.1080 NC.2001 NC.211 NC.271 NC.3021

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