Potez 43

Potez 43
The Potez 43 at Musée de l'Air et de l'Espace.
General information
Type	Sports and utility plane
Manufacturer	Potez
Primary user	France
Number built	161
History
Manufactured	1932-1934
Introduction date	1932
First flight	June 1932

The Potez 43 was a family of French light utility and sports aircraft, developed in early 1930s. They were three-seat single-engine high-wing monoplanes.

Design and development

The plane was a development of Potez 36. First of all it featured new, slimmer fuselage, with three seats, instead of two. A disadvantage were non-folding wings, with shorter slats. The original Potez 430 first flew in June 1932, powered by a 78 kW (105 hp) Potez 6Ас radial engine. 25 examples of this variant were completed, followed by other variants, differing with the last digit in designation. Other variants built in significant numbers were Potez 431 and Potez 438. 161 of Potez 43 family were built in total.

Operational service

Two Potez 430s (registrations: F-AMBM and F-AMBN) took part in the Challenge 1932 international tourist plane contest. Pierre Duroyon took the 22nd place (for 43 starting and 24 finishing crews), while Georges Detre was disqualified due to low cruise speed.

Variants

Potez 430: First version, 78 kW (105 hp) Potez 6Ас engine, 25 built.
Potez 431: Modified series version of 1933, Potez 6Ас engine, 60 built.
Potez 432: Version with 75 kW (100 hp) Renault 4Pei engine, 3 built (first flew 21 April 1933).
Potez 434: Version with 89 kW (120 hp) de Havilland Gipsy Major I straight engine, 9 built (first flew 2 November 1933).
Potez 435: Version with 89 kW (120 hp) Renault 4Pdi engine, 11 built (first flew 23 June 1933).
Potez 436
Potez 437: Modified version with 89 kW (120 hp) Renault 4Pdi engine, 9 built (first flew 17 July 1934).
Potez 438: Military trainer and liaison version with 89 kW (120 hp) Renault 4Pdi engine and a tail wheel, of 1934. 40 built (according to other sources, 33).
Potez 439

Operators

France

French Air Force

Specifications (Potez 430)

Mixed construction strutted high-wing monoplane. A steel framed fuselage covered with canvas. Rectangular two-spar wing, with rounded ends, of wooden construction, canvas covered. Wings were equipped with slats on 1/3 span and supported with main V-shaped struts. Closed cabin with three seats, well glazed. Engine in front, two-blade propeller. Conventional fixed landing gear, with a rear skid, wheels in teardrop covers.

Data from Aviafrance: Potez 430

General characteristics

Crew: 1
Capacity: 2 passengers / 330 kg (728 lb) payload
Length: 7.65 m (25 ft 1 in)
Wingspan: 11.3 m (37 ft 1 in)
Height: 2.36 m (7 ft 9 in)
Wing area: 18 m (190 sq ft)
Empty weight: 470 kg (1,036 lb)
Gross weight: 800 kg (1,764 lb)
Powerplant: 1 × Potez 6Ac 6-cylinder 2-row air-cooled radial piston engine, 78 kW (105 hp)
Propellers: 2-bladed fixed-pitch propeller

Performance

Maximum speed: 160 km/h (99 mph, 86 kn)
Cruise speed: 140 km/h (87 mph, 76 kn)
Stall speed: 60 km/h (37 mph, 32 kn) ~
Range: 800 km (500 mi, 430 nmi)
Service ceiling: 5,000 m (16,000 ft)
Wing loading: 44.4 kg/m (9.1 lb/sq ft)
Power/mass: 0.094 kW/kg (0.057 hp/lb)
Take-off distance to 8 m (26 ft): 156.5 m (513 ft)
Landing distance from 8 m (26 ft): 102.8 m (337 ft)

References

Parmentier, Bruno (30 September 1999). "Potez 430". Aviafrance (in French). Retrieved 13 December 2019.

Bibliography

Comas, Mathieu (September 1999). "La débacle des ambulanciers... ou l'histoire inconnu d'une section d'avions ambulanciers en mai-juin 1940" [Debacle of the Ambulances: Or the Unknown History of an Aerial Ambulance Section in May–June 1940]. Avions: Toute l'Aéronautique et Son Histoire (in French) (78): 18–21. ISSN 1243-8650.

External links

Photos and drawing at Ugolok Neba page

v t e Potez and Potez-CAMS aircraft
Potez	VII VIII IX X XI XII XV XVII XVIII XIX XXII 23 24 25 26 27 28 29 31 32 33 34 35 36 37 38 39 40 41 42 43 45 49 50 501 506 51 53 54 56 58 60 62 63 65 661 662 67 220 230 75 84 91 94
Potez-CAMS	141 160 161

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