Kone on insinööri M. Riffardin suunnitteleman urheilukoneen Caudron C. 710-01 sotilasversio. C 710 lensi ensi kertaa 18. heinäkuuta 1936. Hävittäjä puolestaan heinäkuussa 1939 ja oli auttamattomasti vanhentunut.
Konetta kuitenkin rakennettiin 83 kappaletta.
Valtion lentokonetehdas vastaanotti koneet 24.–28. toukokuuta 1940. Ne saivat tunnukset CA-551 – CA-556. Koelennoilla tehtaalla koneet havaittiin heikoiksi hävittäjälentokoneiksi. Koneen vaatiman pitkän kiitotien vuoksi lentoonlähtö ja lasku suomalaisille kentille oli vaikeaa. Heikkotehoisen moottorin vuoksi kone menetti kaarroissa nopeuttaan niin, että aloitteen pitäminen taistelutilanteissa olisi ollut mahdotonta. Myös koneen nousunopeus oli taistelukoneelle riittämätön ja sen käyttö pommituskoneiden torjuntaan olisi ollut mahdotonta.
Vertailuna Caudronin nousunopeus 4000 metriin oli tehtaan ilmoittamana 7 minuuttia 2 sekuntia kun Fokker D.XXI kykeni nousemaan 1000 metriä korkeammalle 51 sekuntia lyhyemmässä ajassa. Urheilukoneeseen perustuvassa koneessa oli paljon rakenteellisia heikkouksia ja koneiden aseistus oli heikko.
Yksi kone palveli mekaanikkokoulussa Utissa - tähän se sopi, koska koneessa oli laipat ja jarrut ym. tuolloin modernia tekniikkaa.
Yksi kone, CA-556, on entisöimättömänä Vesivehmaalla varastoituna. Yksi on myyty Ranskaan Musée de l'Air et de l'Espace-ilmailumuseoon vuonna 1980-luvulla ja tätä yksilöä entisöidään.
Caudronissa oli puurakenteinen vapaastikantava alataso. Runko oli vanerisaloista ja kaarista rakennettu, etuosastaan alumiinilevyillä, takaosastaan vanerilla verhottu. Puurakenteisessa siivessä oli kaksi vanerista salkoa vaneriverhous. Vakaimet ja siivekkeet olivat alumiiniputkirunkoiset ja kangasverhoillut, laskusiivekkeet hydrauliset. Laskutelineet olivat sisäänvedettävät.
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Caudron 714
1-paikkainen
puurakenteinen
kärkiväli 8,97 m
pituus 8,63 m
tyhjäpaino 1 400 kg
450 hv Renault 12R.03 moottori
Suoritusarvot valmistajan ilmoittamat:
huippunopeus 400 km/h, merenpinnassa
huippunopeus 488 km/h, 5 000 m korkeudessa
käytännön matkanopeus 345 km/h
nousunopeus 2 000 m korkeuteen 3 (28) minuuttia
nousunopeus 4 000 m korkeuteen 7 (02) minuuttia
lakikorkeus 9 100 m
lentomatka 900 km
Aseistus: 4 x 7,5 mm konekivääriä.
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The original specification that led to the C.710 series was offered in 1936 in order to quickly raise the number of modern aircraft in French service, by supplying a "light fighter" of wooden construction that could be built rapidly in large numbers without upsetting the production of existing types. The contract resulted in three designs, the Arsenal VG-30, the Bloch MB-700, and the C.710. Prototypes of all three were ordered.
The original C.710 model was an angular design developed from an earlier series of air racers. One common feature of the Caudron line was an extremely long nose that set the cockpit far back on the fuselage. The profile was the result of using the 336 kW (450 hp) Renault 12R-01 12-cylinder inline engine, which had a small cross-section and was fairly easy to streamline, but very long.
The landing gear was fixed and spatted, and the vertical stabilizer was a seemingly World War I-era semicircle instead of a more common trapezoidal or triangular design. Armament consisted of a 20 mm Hispano-Suiza HS.9 cannon under each wing in a small pod.
The C.710 prototype first flew on 18 July 1936. Despite its small size, it showed good potential and was able to reach a level speed of 470 km/h (292 mph) during flight testing. Further development continued with the C.711 and C.712 with more powerful engines, while the C.713 which flew on 15 December 1937 introduced retractable landing gear and a more conventional triangular vertical stabilizer.
The final evolution of the 710 series was the C.714 Cyclone, a variation on the C.713 which first flew in April 1938 as the C.714.01 prototype. The primary changes were a new wing airfoil profile, a strengthened fuselage, and instead of two cannons, the fighter had four 7.5 mm MAC 1934 machine guns in the wing gondolas. It was powered by the newer 12R-03 version of the engine, which introduced a new carburettor that could operate in negative g.
The Armée de l'Air ordered 20 C.714s on 5 November 1938, with options for a further 180. Production started at a Renault factory in the Paris suburbs in summer 1939.
Other projected versions were the C.720 trainer with a 75 or 164 kW (100 or 220 hp) engine, the C.760 fighter with a 559 kW (750 hp) Isotta-Fraschini Delta engine, and the C.770 fighter with an 597 kW (800 hp) Renault V-engine. None of these reached production.
Deliveries did not start until January 1940. After a series of tests with the first production examples, it became apparent that the design was seriously flawed. Although light and fast, its wooden construction did not permit a more powerful engine to be fitted. The original engine seriously limited its climb rate and maneuverability with the result that the Caudron was withdrawn from active service in February 1940. In March, the initial production order was reduced to 90, as the performance was not considered good enough to warrant further production contracts. Eighty were diverted to Finland to fight in the Winter War. These were meant to be flown by French pilots.
However, events in France resulted in only six aircraft being delivered, and an additional ten were waiting in the harbour when deliveries were stopped. The six aircraft that arrived were assembled, tested and given registrations CA-551 to CA-556. The aircraft were found to be too unreliable and dangerous to use in Finnish conditions, and were not committed to combat.
Two of the aircraft were damaged during a transport flight to Pori. Further, the Finnish pilots found that it was difficult to start and land the aircraft from the air bases at the front. The aircraft were maintained on the roster until they were retired and scrapped on 30 December 1949. One example, CA-556 was transferred to the maintenance personnel school as an instructional airframe.
On 18 May 1940, 35 Caudrons were delivered to the Polish Warsaw Squadron, the Groupe de Chasse polonais I/145, stationed at the Mions airfield. After just 23 sorties, adverse opinion of the fighter was confirmed by frontline pilots who expressed concerns that it was seriously underpowered and was no match for contemporary German fighters.
On 25 May, only a week after it was introduced, French Minister of War Guy La Chambre ordered all C.714s to be withdrawn from active service. However, since the French authorities had no other aircraft to offer, the Polish pilots ignored the order and continued to fly the Caudrons.
The Caudron fighter was also used by the Polish training squadron based in Bron near Lyon. Although the pilots managed to disperse several bombing raids, they did not score any kills; but they did not lose any aircraft either. By the end of June when France fell, only 53 production machines had been delivered (although the number varies, 98 is another common figure).
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