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https://en.wikipedia.org/wiki/Koolhoven_F.K.58
The Koolhoven F.K.58 was a single engine, interceptor-fighter aircraft designed and mainly manufactured by N V Koolhoven in the Netherlands under contract by France. Intended for Armée de l'Air use, the F.K.58 saw limited service in the Battle of France. In 1937, the French Conseil Supérieur de l'Air decided that domestic aircraft manufacturing capacity could not, in the event of war, equip the Armée de l'Air with fighters quickly enough. The Dutch manufacturer Koolhoven was contracted to design a cheap, easily built, high-performance fighter, that could be built and serviced with French-supplied engines and other components. According to some sources, the Koolhoven fighter was intended primarily for fighter units based in French colonies. On 17 July 1938, the prototype Koolhoven Model 1166 (later renamed the F.K.58) flew for the first time. Designed by Erich Schatzki – a Jewish refugee from Germany – the F.K.58 may be seen as a development of his preceding fighter design: the Fokker D.21. The F.K.58 used the same composite materials as the D.21: the structure of the fuselage consisted of welded steel tubing covered with sheet metal (front part) and fabric (aft); the wings had wooden members with a plywood and fabric skin. In January 1939, the Armée de l'Air placed an order for 50 aircraft, to be powered by Gnome-Rhône 14N engines. Due to the unavailability of Gnome-Rhône engines and French instruments, just 17 aircraft – six F.K.58s and 11 F.K.58As – were completed at the Koolhoven works, with Dutch supplied engines and instruments – and delivered to the Armée de l'Air. Production was transferred to Nevers, where the aircraft were re-built with French components and the extraneous parts were returned to the Netherlands. However, only one more F.K.58 was produced from scratch at Nevèrs. In July 1939, the Dutch government placed an order on behalf of the Luchtvaart Afdeling (Netherlands Army Aviation Corps) for 36 F.K.58 variants, powered by Bristol Taurus engines. As the British government restricted exports of Tauruses, they were to be replaced by Dutch stocks of the Bristol Mercury VIII (as used by the Dutch Fokker D.21 and Fokker G.1A). The lower output of the Mercury, relative to the Taurus, would have allowed a top speed to some 480 km/h. The F.K.58s comprising the Dutch order were in various stages of construction when they were destroyed by a German air raid on the Koolhoven factory in May 1940. Role Fighter Manufacturer Koolhoven Designer Erich Schatzki First flight 17 July 1938 Introduction 1940 Retired 1940 Primary users French Air Force Polish Air Force Produced 1939-1940 Number built 20 The F.K.58 was originally ordered to serve with AdA units based in French overseas territories. Following the outbreak of war with Germany, however, the type was assigned to an ad hoc, Free Polish air force unit commanded by Captain Walerian Jasionowski. Roughly equivalent to a French escadrille, or Polish eskadra, it was often known by the unofficial name "Eskadra Koolhoven". The unit's official role was patrouille ("patrol") – as the AdA designated units that defended rear areas against long-range bombers and other enemy aircraft, as part of the Défense Aérienne du Territoire ("Territorial Air Defense"; DAT). The unit operated from the Salon and Clermont-Aulnat air bases. By May 1940, 13 aircraft were operational with Eskadra Koolhoven. As delivered, however, the fighters were unarmed and the Poles had to acquire machine guns and fit them. From 30 May 1940, they were in service, patrolling firstly in the Avignon-Marseille area, and then over Clermont-Ferrand. At least 47 operational sorties were recorded, but the Escadron did not encounter enemy aircraft. The type's service life was short-lived, with ; the unit had no confirmed victories, but at least one F.K.58 was lost. After the fall of France, all surviving airframes were scrapped. Specifications (F.K.58) General characteristics Crew: One Length: 8.7 m (28 ft 6.75 in) Wingspan: 11 m (36 ft 1.25 in) Height: 3 m (9 ft 10 in) Wing area: 17.3 m2 (186.2 ft2) Empty weight: 1,930 kg (4,255 lb) Loaded weight: 2,750 kg (6,063 lb) Powerplant: 1 × Gnome-Rhône 14N-16 radial engine, 768 kW (1,030 hp) Performance Maximum speed: 505 km/h (314 mph) Cruise speed: 450 km/h (280 mph) Range: 750 km (466 mi) Service ceiling: 10,000 m (32,810 ft) Rate of climb: 11.6 m/s (1,130 ft/min) Wing loading: 159 kg/m2 (32.6 lb/ft2) Power/mass: 0.28kW/kg (0.17 hp/lb) Armament 4 x 7.5 mm FN-Browning machine guns in underwing fairings * |
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