Samiksha Jaiswal (Editor)

Fairey Hendon

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Top speed
  
244 km/h

Length
  
19 m

Retired
  
January 1939

Manufacturer
  
Avions Fairey

Wingspan
  
31 m

Introduced
  
1936

First flight
  
November 25, 1930

Fairey Hendon Forgotten Aircraft Fairey Hendon Defence of the Realm

The Fairey Hendon was a British monoplane heavy bomber of the Royal Air Force designed by Fairey Aviation in the late 1920s, which served in small numbers with one Squadron of the RAF between 1936 and 1939. It was the first all-metal low-wing monoplane to enter service with the RAF.

Contents

Fairey Hendon Fairey Hendon

Development

Fairey Hendon Forgotten Aircraft Fairey Hendon Defence of the Realm

The Hendon was built to meet the Air Ministry Specification B.19/27 for a twin-engine night bomber to replace the Vickers Virginia, competing against the Handley Page Heyford and Vickers Type 150. The specification required a range of 920 mi (1,480 km) at a speed of 115 mph (185 km/h), with a bombload of 1,500 lb (680 kg). To meet this requirement, Fairey designed a low-winged cantilever monoplane with a fixed tailwheel undercarriage. The fuselage had a steel tube structure with fabric covering with a pilot, a radio operator/navigator and three gunners, in open nose, dorsal and tail positions. Bombs were carried in a bomb bay in the fuselage centre. Variants powered by either radial engines or liquid-cooled V12 engines were proposed.

Fairey Hendon Fairey Hendon night bomber

The prototype K1695 (which was known as the Fairey Night Bomber until 1934) first flew on 25 November 1930, from Fairey's Great West Aerodrome in Heathrow and was powered by two 460 hp (340 kW) Bristol Jupiter VIII radial engines. The prototype crashed and was heavily damaged in March 1931 and was rebuilt with two Rolls-Royce Kestrel VI engines. After trials, 14 production examples named the Hendon Mk.II were ordered. These were built by Fairey's Stockport factory in late 1936 and early 1937 and flown from Manchester's Barton Aerodrome. Orders for a further 60 Hendons were cancelled in 1936, as the prototype of the first of the next generation of British heavy bombers—the Armstrong Whitworth Whitley—had flown and showed much higher performance. The Hendon Mk.II was powered by two Rolls-Royce Kestrel VI engines. The production Hendon Mk.II included an enclosed cockpit for the pilot and navigator.

Operational history

Fairey Hendon httpsuploadwikimediaorgwikipediacommonsthu

The type was delayed by the crash and a rebuild of the prototype and the Heyford received the majority of the orders needed to replace RAF heavy bombers, the Hendon coming into service three years later. The only Hendon-equipped unit, 38 Squadron, began operational service at RAF Mildenhall in November 1936, replacing Heyfords, later moving to RAF Marham, Norfolk. Later, the Hendons went to No. 115 Squadron RAF, which was formed from 38 Squadron. The type was soon obsolete and replaced from late 1938 by the Vickers Wellington. By January 1939, the Hendons had been retired and were then used for ground instruction work, including the radio school at RAF Cranwell.

Variants

Hendon Mk.I
Prototype, one built
Hendon Mk.II
Production variant with two Rolls-Royce Kestrel VI engines, 14 built

Operators

  • Royal Air Force
  • No. 38 Squadron RAF
  • No. 115 Squadron RAF
  • No. 1 Electrical & Wireless School RAF
  • Accidents and incidents

    Of the 14 Hendon IIs only two were lost in accidents:

    Fairey Hendon 1 Fairey Hendon HD Wallpapers Backgrounds Wallpaper Abyss

  • 26 May 1937 - K5091 crashed on landing at RAF Marham
  • 25 February 1938 - K5095 crashed on landing at RAF Marham
  • Specifications (Hendon II)

    Data from The British Bomber since 1914; Fairey Aircraft since 1915

    General characteristics

  • Crew: five
  • Length: 60 ft 9 in (18.52 m)
  • Wingspan: 101 ft 9 in (31.02 m)
  • Height: 18 ft 8 in (5.69 m)
  • Wing area: 1,146 ft² (106.5 m²)
  • Empty weight: 12,773 lb (5,806 kg)
  • Loaded weight: 20,000 lb (9,091 kg)
  • Powerplant: 2 × Rolls-Royce Kestrel VI inline piston V12 engine, 600 hp (447 kW) each
  • Performance

  • Maximum speed: 132 kn (152 mph, 245 km/h) at 15,000 ft
  • Cruise speed: 116 kn (133 mph, 214 km/h) at 15,000 ft
  • Range: 1,183 nmi (1,360 mi, 2,190 km)
  • Service ceiling: 21,400 ft (6,524 m)
  • Rate of climb: 940 ft/min (4.8 m/s)
  • Wing loading: 17.5 lb/ft² (85.4 kg/m²)
  • Power/mass: 0.06 hp/lb (0.099 kW/kg)
  • Climb to 6,500 ft: 9 minutes 12 seconds
  • Armament

  • Guns: 3× .303 in (7.7 mm) Lewis guns in nose, dorsal and tail positions
  • Bombs: 1,660 lb (753 kg) bombs
  • References

    Fairey Hendon Wikipedia