Caudron C.690M
1936
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Caudron C.690M

With the same basic design characteristics as Marcel Riffard's lightweight all-wood low-wing cantilever monoplane racers, the Caudron C.690 was designed as a trainer for pilots of single-seat fighters. It was similar to the earlier C.720, with a large rounded fin and rudder assembly and independent fixed cantilever main landing gear units with wheel spats, but had a 164kW Renault 6Q-03 engine in place of a 104kW Bengali Sport and was also heavier than the C.720. The first prototype flew in early 1936 and was followed by the second on 18 February 1936. This latter aircraft was demonstrated by the Caudron company's flight director Christian Sarton du Jonchay in several foreign countries, including Austria, Hungary, Romania and Yugoslavia. Soon afterwards the first C.690 was demonstrated to Japanese, Soviet and US air missions, resulting in one example of a Caudron single-seater being bought by the Soviet Union and one by Japan, although the exact types are unknown. It is thought they were basically C.690s, but may have had tail-planes of a more angular type as fitted to the earlier experimental C.580.

While undergoing official tests at Villacoublay on 10 May 1937, the first prototype crashed, killing Caudron's chief test pilot Rene Paulhan. Despite this disaster official interest continued to grow and a production series was ordered for the Armee de I'Air. These aircraft differed from the prototype in having a triangular shaped fin and rudder, longer landing gear legs and fixed leading-edge slots. Production was slow to get under way and the first C.690M did not begin flight tests until the beginning of April 1939. These military aircraft were unarmed but equipped with an OPL camera gun. Fifteen aircraft had been delivered by the end of May that year, being allocated to CICs (Centres d'lnstruction a la Chasse, or Fighter Training Centres) at Salon, Dijon and Etampes, but none remained in flying condition after the French collapse in June 1940. One example (C.690 no. 9) was concealed from the occupying forces and restored to flying condition after the War, taking to the air on 12 April 1945. Repaired later after an accident, all trace of it was subsequently lost.


Specification 
 MODELCaudron C.690M
 ENGINE1 x 164kW Renault 6Q-05 inline piston engine
 WEIGHTS
    Take-off weight1050 kg2315 lb
    Loaded weight672 kg1482 lb
 DIMENSIONS
    Wingspan7.7 m25 ft 3 in
    Length7.82 m26 ft 8 in
    Height2.6 m9 ft 6 in
    Wing area90 m2968.75 sq ft
 PERFORMANCE
    Max. speed370 km/h230 mph
    Cruise speed320 km/h199 mph
    Ceiling9700 m31800 ft
    Range1100 km684 miles

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