Caudron C.714

infobox Aircraft
name = Caudron C.714
type = Fighter
manufacturer = Caudron-Renault



caption = Finnish C.714
designer =Marcel Riffard
first flight =18 July 1936 (C.710)
introduced = 1940
retired = 1941 (Finland)
status =
primary user = Polish Air Force in France
more users = Armee de l'Air Finland
produced = 1939-1940
number built =approximately 90
unit cost =
variants with their known articles = The C.710 were a series of fighter aircraft developed by Caudron-Renault for the French Armée de l'Air just prior to the start of World War II. One version, the C.714, saw limited production, and were assigned to Polish pilots flying in France after the fall of Poland in 1939. A small number were also supplied to Finland.

Design and development

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 450 hp (336 kW) 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 Hispano-Suiza 20 mm HS-9 cannon under each wing in a small pod, with an option for a third firing through the propeller spinner.

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 in 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 [Green 1960, p. 39–40.]

Other projected versions were the C.720 trainer with a 100 or 220 hp (75 or 164 kW) engine, the C.760 fighter with a 750 hp Isotta-Fraschini Delta engine, and the C.770 fighter with an 800 hp (597 kW) Renault V-engine. None of these reached production.

Operational history

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 manoeuvrability 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 Finnish CR.714 aircraft were permanently grounded on September 10 1940, and taken out of service in 1941.

On 18 May, 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 front-line 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 C714s 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. Despite flying a fighter hopelessly outdated compared to the Messerschmitt Me 109E, the Polish pilots scored 12 confirmed and three unconfirmed victories in three battles between 8 June and 11 June, losing nine in the air and nine more on the ground. Interestingly, among the planes shot down were four Dornier Do 17 bombers, but also three Messerschmitt Bf 109 and five Messerschmitt Bf 110 fighters.

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 although they did not lose any machines. By the end of June when France fell, only 53 production machines had been delivered (although the number varies, 98 is another common figure). Despite a larger number being diverted to Finland, only six Caudron C.714s were received in a semi-assembled state. An additional ten were on the dockside at the time of France's Armistice with Germany, subsequently, further shipments were halted. After assembly, operations in Finland were limited to test flights and, in September 1941, combat flights with the fighters were prohibited. 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.

Operators

;FIN
*Finnish Air Force;FRA
*"Armée de l'Air";POL
*Polish Air Force in Exile

urvivors

One full CR.714 airframe as well as one additional fuselage were preserved in Finland. The fuselage was offered back to the Musée de l'Air et de l'Espace where it is currently undergoing restoration.

pecifications (Caudron C.714)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

ref=The Complete Book of FightersGreen, William and Swanborough, Gordon. "The Complete Book of Fighters". New York: Smithmark, 1994. ISBN 0-8317-3939-8.]

crew=One
capacity=
length main= 8.63 m
length alt= 28 ft 3⅞ in
span main= 8.97 m
span alt= 29 ft 5⅛ in
height main= 2.87 m
height alt= 9 ft 5 in
area main= 12.5 m²
area alt= 135 ft²
airfoil=
empty weight main= 1,395 kg
empty weight alt= 3,075 lb
loaded weight main= 1,880 kg
loaded weight alt= 4,145 lb
useful load main=
useful load alt=
max takeoff weight main=
max takeoff weight alt=
more general=

engine (prop)= Renault 12R 03
type of prop= inverted V-12 inline piston engine
number of props=1
power main= 373 kW
power alt= 500 hp
power original=

max speed main= 460 km/h
max speed alt= 249 knots, 286 mph
max speed more= at 5,000 m (16,400 ft)
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 900 km
range alt= 486 nm, 559 mi
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=*Climb to 4000 m: 9.66 min

armament=* 4x 7.5 mm MAC 1934 machine guns

avionics=

ee also

aircontent
related=

similar aircraft=
* Ambrosini SAI.207
* Ambrosini SAI.403 Dardo
* Bell XP-77
* Douglas XP-48
* Martin-Baker MB 2
* Miles M.20
* Tucker XP-57

sequence=
C.670 - C.680 - C.690 - C.710 - C.714 - C.720 - C.760 - C.770 - C.800 - C.870 - C.880

lists=
* List of aircraft of the Armée de l'Air
* List of fighter aircraft

see also=

References

Notes

Bibliography

* Belcarz, Bartłomiej. "GC 1/145 in France 1940". Sandomierz, Poland/Redbourn, UK: Mushroom Model Publications, 2002. ISBN 83-917178-1-X.
* Belcarz, Bartłomiej. "Morane MS 406C1, Caudron Cyclone CR 714C1, Bloch MB 151/152 (Polskie Skrzydła 2)" (in Polish). Sandomierz, Poland: Stratus, 2004. ISBN 83-89450-21-6. (This book recounts the use of the CR.714 by Polish Pilots of the Armée de l'Air.)
* Breffort, Dominique & Jouineau, André. "French Aircraft from 1939 to 1942, Volume 1: from Amiot to Curtiss". Paris, France: Histoire & Collections, 2004. ISBN 2-915239-23-1.
* Brindley, John F. "French Fighters of World War Two, Volume One". Windsor, UK; Hylton Lacy Publishers Ltd., 1971. ISBN 0-85064-015-6.
* Green, William. "War Planes of the Second World War, Fighters, Volume One". London: Macdonald & Co.(Publishers) Ltd., 1960. ISBN 0-356-01445-2.
* Gretzyngier, Robert & Matusiak, Wojtek. "Polish Aces of World War II". Oxford: Osprey Publishing., 1998. ISBN 1-85532726-0.
* Keskinen, Kalevi; Stenman, Kari and Niska, Klaus. "Suomen Ilmavoinen Historia 4: Morane-Saulnier M.S. 406/Caudron C.714". Helsinki, Finland: Tietoteos, 1975. ISBN 951-9035-19-2.
* Pelletier, Alain. "French Fighters of World War II in Action (Aircraft Number 180)". Carrollton, TX: Squadron/Signal Publications, Inc., 2002. ISBN 0-89747-440-6.

External links

* [http://www.plastikowe.pl/galerie/lotnictwo/caudron-c714 Photo gallery of Finnish Caudron C.714]
* [http://home.clara.net/acf/scale/scale-pics-3/low-wing/caudron-cyclone/caudron-cyclone.html replica of Caudron Cyclone]