The SPCA 10 was a parasol wingthree-engined flying boat of all-metal construction. Its one-piece wing had a rectangular central region and trapezoidal outer areas, the latter carrying narrow ailerons over the whole of their trailing edges. The primary wing structure had a pair of steel spars and duralumin ribs. Unlike the rest of the aircraft, the wing was fabric covered. It was braced to the upper hull by a pair of parallel, vertical struts to each spar but stabilized with N-struts out to the floats, which were themselves braced to the outer wing spars with pairs of outward-leaning struts as well as by horizontal struts to the mid-hull. All these struts were steel tubes enclosed in streamlined casings. The flying boat was powered by three Gnome-Rhône 9Ac Jupiter nine-cylinder radials mounted, uncowled, on the wingleading edge as closely as the propeller discs allowed. Their fuel and oil tanks were in the wing, away from the engines to reduce fire risks. The wing was thick enough to allow the engineer in-flight access to most of the engine accessories. The SPCA 10's hull was flat-sided and slender. Its single step planing bottom had a cross-section which altered from V in the nose to rounded at mid-hull. There was an open, circular position for a gunner or navigational observer in the extreme nose, with an enclosed navigator's cabin immediately aft. The pilots sat side by side in an open cockpit, equipped with dual control, midway between the nose and the leading edge. The central hull had internal compartments for the radio operator and the photographer and for rest. There were two, left-right staggered, open gunner's positions halfway between the trailing edge and the tail, which had openings in their floors above the waterline to allow downward fire or observation. The SPCA 10 had a steel-framed, fabric covered fin with a swept leading edge and flat top. Its servo-balancedrudder was almost rectangular apart from a rounded heel at the base of the fuselage. The tailplane was mounted on the fin at about one third height and supported on each side by a splayed pair of struts from the hull. Both it and the elevators were rectangular in plan, apart from a cut-out between the latter in which the rudder worked.
Operational history
The SCPA 10 first flew on 4 April 1928 at La Ciotat, piloted by Burri. After display at the July 1928Paris Salon it went to Saint-Raphaël, Var for official tests. These revealed a serious handling problem. When the engines speeds were reduced, the CAMS entered a dive, behaviour ascribed to the closeness of the propellers to the wing leading edge. As a result, alightings had to be made, counter-intuitively, under full power. The tests continued, though on 18 December 1928 an order was issued to stop them and modify the engine installation. Regrettably, this order was slow to reach Saint-Raphaël and on 8 Januarythe pilot of the CAMS 10 reduced power on approach. The aircraft dived into the sea, killing all aboard. No more were built.
