|National origin||United Kingdom|
|First flight||11 April 1921|
|Primary user||Royal Air Force|
The Short N.3 Cromarty was a prototype British twin-engined biplane flying boat designed towards the end of the First World War. Only a single example was built, which first flew in 1921 and was wrecked in 1922.
In April 1917, the British Admiralty developed a requirement for a long-range patrol flying boat to work in support of the Fleet, and issued Specification N.3(b) (later re-issued as Air Ministry Specification XXX[a]) to meet this need. This resulted in designs from Vickers (for the Valentia) and Shorts of Rochester, who, although better known at the time for floatplanes, had gained experience of flying boats building Felixstowe F.3 and F.5s under licence from April 1917.
Short Brothers received an order for three prototypes just after the Armistice ended the First World War. Short's design, the N.3 Cromarty, was a large, twin engine biplane. It was powered by two 650 hp (480 kW) Rolls-Royce Condor engines, and had a similar, but larger hull to that of the Felixstowe flying boats, with a biplane tail. It featured a side-by-side cockpit for the two pilots, a large box cockpit for a gunner, who was armed with a COW automatic cannon, and a dorsal position for another gunner armed with a Lewis gun.
Production of the prototypes started in February 1919, but the second and third were cancelled before completion, with the first prototype eventually being launched on 21 March 1921, being first flown by John Lankester Parker on 11 April 1921.
After extensive testing, the Cromarty was handed over to the RAF's Seaplane Development Flight on 17 June 1922. In August, the Flight, comprising the Cromarty, two Felixstowe F.5s and a Phoenix Cork set out on trials of operating large flying boats away from support facilities for extended periods of time. Arriving at St Mary's, Isles of Scilly on 21 August, the Cromarty successfully weathered a storm, but was taxied onto a reef, holing the hull. The damage was declared uneconomic to repair and the Cromarty was scrapped in place.
While the Cromarty had performed well in its limited service, one problem (as with all wooden hulled flying boats) was soakage of water into the hull, with as much as 600 pounds (270 kg) of water absorbed after a few weeks of service. Tests with a metal-hulled Felixstowe F.5 resulted in an order for a prototype of an improved, metal-hulled flying boat based on the Cromarty. This became the prototype Short Singapore I.
Data from Short Aircraft since 1900 
- Length: 59 ft 0 in (17.98 m)
- Wingspan: 113 ft 6 in (34.60 m)
- Height: 23 ft 0 in (7 m)
- Wing area: 2243 ft2 (208.5 m2)
- Empty weight: 12,220 lb (5,555 kg)
- Gross weight: 18,000 lb (8,182 kg)
- Powerplant: 2 × Rolls-Royce Condor IA water-cooled V12 engine, 650 hp (485 kW) each
- Maximum speed: 95 mph (153 km/h)
- Range: 900 miles (1,450 km)
- Endurance: 11 hours
- Rate of climb: 300 ft/min (1.5 m/s)
- 1× 1½ lb (37 mm) COW gun in nose
- 1× .303 in (7.7 mm) Lewis gun in dorsal position
- 2,000 pounds (910 kg) bombs
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
- London 2003, p.62.
- Barnes 1967, p.155.
- London 2003, pp. 63—64.
- London 2003, p.64.
- Williams and Gustin 2003, p.101.
- Barnes 1967, p.157.
- London 2003, p.65.
- Short 1925, p.825.
- Barnes 1967, pp. 195—198.
- Barnes 1967, p.158.
- Flight 14 December 1922, p.737.
- Normal all-up weight - overload weight 19,800 pounds (9,000 kg)
- London 2003, pp. 262—263.
- Climb to 6,000 ft in 20 min.
- Following the formation of the Royal Air Force in April 1918 the specifications were re-numbered using roman numerals
- "Aircraft Production at a Glance". Flight, 14 December 1922, pp. 725–740.
- Barnes, C.H. Shorts Aircraft since 1900. London:Putnam, 1967.
- London, Peter. British Flying Boats. Stroud, UK:Sutton Publishing, 2003. ISBN 0-7509-2695-3.
- Short, Oswald "All-Metal Flying Boat Hulls". Flight, 17 December 1925. pp. 823–825.
- Williams, Anthony G. and Gustin, Emmanuel. Flying Guns: World War I and its Aftermath 1914-32. Ramsbury, UK:Airlife, 2003. ISBN 1-84037-396-2.
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