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Hansa-Brandenburg CC / W.22



Intended primarily for use by the Austro-Hungarian Navy, the CC single-seat fighter flying boat (the designation was derived from the initials of Camillo Castiglioni, the financier of the Hansa- und Brandenburgische Flugzeug-Werke) was a single-bay biplane of wooden construction which appeared in prototype form in mid-1916. Retaining the "star" interplane bracing strut arrangement introduced by the KD (D.I), the CC was supplied to the Austro-Hungarian Navy with both the 160hp Austro-Daimler and 180hp Hiero six-cylinder water-cooled engines, armament consisting of a single 8mm Schwarzlose machine gun projecting through the windscreen. A total of 37 fighter flying boats of this type was delivered to the service. The CC was also adopted by the German Navy, which received a total of 36, with deliveries commencing in February 1917. These were powered by the 150hp Benz Bz III, the engines of some examples being semi-cowled. The CC initially carried an armament of one 7.92mm LMG 08/15 machine gun, but late production examples had two such weapons fixed to fire forward in the upper decking of the hull nose, and the hull was lengthened to improve flying characteristics. In July 1917, the German Navy grounded the CC until all aircraft were provided with extra (Vee-type) interplane bracing struts to dampen severe wing vibration. The CC was employed extensively and with considerable success over the Adriatic by the Austro-Hungarian Navy. One example was completed experimentally as a triplane, the extra wing being placed at the intersection of the "starstruts". It was delivered to the Austro-Hungarian Navy for evaluation on 11 May 1917, but was written-off in a landing accident on the following 19 September. One CC was modified and tested in the summer of 1918 as the W 22, with broad sponsons replacing the outrigger stabilising floats. This experimental model, which crashed during testing, was intended solely to evaluate the sponson concept as part of the Staaken Rs IV development programme.

Max take-off weight: 1080 kg / 2381 lb
Empty weight: 800 kg / 1764 lb
Wingspan: 9.30 m / 31 ft 6 in
Length: 7.69 m / 25 ft 3 in
Height: 3.57 m / 12 ft 9 in
Wing area: 26.52 sq.m / 285.46 sq ft
Max. speed: 175 km/h / 109 mph
Range: 500 km / 311 miles





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