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History Brief, by Johan Visschedijk

June 15, 2005

Potez 75


Since 1937 Henry Potez had been concentrating on aircraft engines. In 1952 it was decided to re-enter the aircraft manufacturing industry and the Société des Moteurs Potez was renamed Société des Avions et Moteurs Henry Potez. The first design was the Potez 75, a private venture originally intended as an anti-tank aircraft. The prototype F-ZWSA was constructed in less than six months at the Argenteuil plant and Georges Détré made the first flight on June 10, 1953.

Constructed by Ing. Delaruelle the Potez 75 was a rugged simple light design with a central nacelle, twin booms with a high-set tail plane and a fixed, spatted landing gear. The two-seat aircraft had an enclosed gunner/observer's position in the nose and a high-mounted, open cockpit. Intended to operate from unprepared strips it had short take off and landing characteristics. The aircraft was powered by a single Potez 8-D reciprocating engine driving a pusher propeller.

The French Armée de l'Air and Aviation Legere de L'Armee de Terre (Air Force and Army) evaluated the design and rejected it as insufficient equipped for its task. The design was transformed into an army-co-operation and light ground attack aircraft and it was tested in Algeria as a counter-insurgency aircraft. Eventually in May 1956 15 pre-production aircraft and 100 production aircraft were ordered by the French National Defense Department.

The prototype had several improvements made to both cockpits including a sliding hood over the pilot's position. Despite this the contract for both the 15 pre- and 100 production aircraft were cancelled in June 1957 due to budget restrains. From late 1957 the prototype was being used by the French general Redon as a liaison aircraft until it crashed in September 1958.

Next to the initial F-ZWSA the aircraft, with construction number 01, carried subsequently the registrations F-WGVK and F-MAFY.

The aircraft carried four fixed 0.3 in (7.5 mm) machine guns and a maximum of eight Nord SS-10 or SS-11 wire-guided missiles or alternative ordnance.

Potez 75 Jacques Trempe Collection

Specifications

Type:

Two-seat ground support aircraft

Engine:

One 480 hp Potez 8D 32 eight-cylinder inverted V-engine

Span:

42 ft 11 in (13.08 m)

Length:

29 ft 1 in (8.87 m)

Height:

8 ft 10 in (2.69 m)

Wing area:

247 sq.ft (22.95 sq.m)

Empty Wt:

3,891 lb (1,765 kg)

Max T/O Wt:

5,578 lb (2,530 kg)

Max speed:

171 mph (275 km/h)

Max climb:

1,082 ft (330 m)/min

Range:

435 mile (700 km)

Models

Potez 75:

Two-seat prototype, 1 built