The Fairey Hendon was a British twin-engined heavy night bomber designed by the Fairey Aviation Company to Air Ministry Specification B.19/27, which sought a replacement for the Vickers Virginia. It was a low-wing cantilever monoplane with a fixed tailwheel undercarriage, a steel tube fuselage with fabric covering, a crew of five including gunners in open nose, dorsal and tail positions, and bombs carried in cells in the fuselage and centre section. It was the first all-metal low-wing monoplane to enter service with the Royal Air Force. The prototype first flew on 25 November 1930 with Bristol Jupiter radial engines, crashed in March 1931 and was rebuilt with Rolls-Royce Kestrel engines. Fourteen production Hendon Mk.II aircraft were built at Stockport in 1936 and 1937, orders for sixty more were cancelled, and the type served with a single RAF squadron between 1936 and 1939.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Fairey Hendon (Wikipedia)
Of Make
Source Fairey Hendon (Wikipedia)
Sources
1. Fairey Hendon (Wikipedia)
Development
The prototype K1695 (which was known as the Fairey Night Bomber until 1934) first flew on 25 November 1930
Lead
The Fairey Hendon was a British monoplane, heavy bomber of the Royal Air Force, designed by Fairey Aviation, and first flown in 1930.
Specifications (Hendon II)
2 × Rolls-Royce Kestrel VI V-12 water-cooled piston engines, 600 hp (450 kW)
Specifications (Hendon II), mass
Empty weight: 12,773 lb (5,794 kg)
Specifications (Hendon II), maximum mass
Gross weight: 20,000 lb (9,072 kg)
Specifications (Hendon II), top speed
Maximum speed: 152 mph (245 km/h, 132 kn) at 15,000 ft (4,600 m)
Lead, status
The aircraft served in small numbers with one squadron of the RAF between 1936 and 1939.
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