Airco DH.9

The Airco DH.9 (from de Havilland 9) - also known after 1920 as the de Havilland DH.9 - was a British bomber used in the First World War. A single-engined biplane, it was a development of Airco's earlier, highly successful DH.4 and was ordered in very large numbers for Britain's Royal Flying Corps and Royal Air Force.

Its engine was unreliable, and failed to provide the expected power, giving the DH.9 poorer performance than the aircraft it was meant to replace, and resulting in heavy losses, particularly over the Western Front. The subsequently-developed DH.9A had a more powerful and reliable American Liberty L-12 engine.


Airco DH.9
Class Aircraft
Type Bomber
Manufacturer Airco
Origin United Kingdom - UK (Great Britain)
Country Name Origin Year
United Kingdom - UK (Great Britain) 1917
Country Name Operational Year Retirement Year
Afghanistan 1924 View
Australia 1920 1929 View
Belgium View
Bolivia View
Canada View
Chile View
Estonia View
Greece View
India View
Ireland View
Latvia View
Netherlands View
Paraguay View
Peru View
Poland View
Romania View
Russia (USSR) View
South Africa View
Spain View
Switzerland View
Turkey (Ottoman Empire) View
United Kingdom - UK (Great Britain) 1917 1920 View
United States of America View
Uruguay View
New Zealand View
ManufacturerName Production From Production To Quantity
Airco 4091 View

The DH.9 was designed by de Havilland for the Aircraft Manufacturing Company in 1916 as a successor to the DH.4. It used the wings and tail unit of the DH.4 but had a new fuselage. This enabled the pilot to sit closer to the gunner/observer and away from the engine and fuel tank. The other major change from the DH.4 was the choice of the promising new BHP/Galloway Adriatic engine, which was predicted to produce 300 hp (224 kW) and so give the new aircraft an adequate performance to match enemy fighters.

By this time, as a result of attacks by German bombers on London, the decision was made to almost double the size of the Royal Flying Corps, with most of the new squadrons planned to be equipped with bombers. Based on the performance estimates for the DH.9 (which were expected to surpass those of the DH.4), and the similarity to the DH.4, which meant that it would be easy to convert production over to the new aircraft, massive orders (4,630 aircraft) were placed.

The prototype (a converted DH.4) first flew at Hendon in July 1917. Unfortunately, the BHP engine proved unable to reliably deliver its expected power, with the engine being de-rated to 230 hp (186 kW) in order to improve reliability. This had a drastic effect on the aircraft's performance, especially at high altitude, with it being inferior to that of the DH.4 it was supposed to replace. This meant that the DH.9 would have to fight its way through enemy fighters, which could easily catch the DH.9 where the DH.4 could avoid many of these attacks.

While attempts were made to provide the DH.9 with an adequate engine, with aircraft being fitted with the Siddeley Puma, a lightened and supposedly more powerful version of the BHP, with the Fiat A12 engine and with a 430 hp (321 kW) Napier Lion engine, these were generally unsuccessful (although the Lion engined aircraft did set a World Altitude Record of 30,500 ft (13,900 m) on 2 January 1919) and it required redesign into the DH.9A to transform the aircraft.

To boost the rate of production, quantity orders for the DH.9 were also placed with Alliance, G & J.Weir, Short Brothers, Vulcan, Waring & Gillow and National Aircraft Factories No. 1 and No. 2.

The first deliveries were made in November 1917 to 108 Squadron RFC and it first went into combat over France in March 1918 with 6 Squadron, and by July 1918 nine squadrons operational over the Western Front were using the type.

The DH.9's performance in action over the Western Front was a disaster, with heavy losses incurred, both due to its poor performance and to engine failures, despite the prior de-rating of its engine. Between May and November 1918, two squadrons on the Western Front (Nos. 99 and 104) lost 54 shot down, and another 94 written off in accidents. Nevertheless, on 23 August 1918 a DH9 flown by Lieutenant Arthur Rowe Spurling of 49 Squadron, with his observer, Sergeant Frank Bell, single-handedly attacked thirty Fokker D.VII fighters, downing five of them.[citation needed] Captain John Stevenson Stubbs managed 11 aerial victories in a DH9, including the highly unusual feat of balloon busting with one.

The DH.9 was also more successful against the Turkish forces in the Middle East, where they faced less opposition, and it was used extensively for coastal patrols, to try to deter the operations of U-boats.

Following the end of the First World War, DH.9s operated by 47 Squadron and 221 Squadron were sent to southern Russia in 1919 in support of the White Russian Army of General Denikin during the Russian Civil War. The last combat use by the RAF was in support of the final campaign against Mohammed Abdullah Hassan (known by the British as the "Mad Mullah") in Somalia during January—February 1920. Surprisingly, production was allowed to continue after the end of the war into 1919, with the DH.9 finally going out of service with the RAF in 1920.

Following the end of the First World War, large number of surplus DH.9s became available at low prices and the type was widely exported (including aircraft donated to Commonwealth nations as part of the Imperial Gift programme.

The South African Air Force received 48 DH.9s, and used them extensively, using them against the Rand Revolt in 1922. Several South African aircraft were re-engined with Bristol Jupiter radial engines as the M'pala, serving until 1937.

Role Bomber
Manufacturer Airco
Designer Geoffrey de Havilland
First flight July 1917
Introduction 1917
Retired 1920
Primary users Royal Air Force
RNAS, RFC.
Number built 4091
Variants Airco DH.9A
Airco DH.9C
Westland Walrus


General characteristics

  • Crew: 2
  • Length: 30 ft 5 in (9.27 m)
  • Wingspan: 42 ft 4? in (12.92 m)
  • Height: 11 ft 3½ in (3.44 m)
  • Wing area: 434 ft² (40.3 m²)
  • Empty weight: 2,360 lb (1,014 kg)
  • Max. takeoff weight: 3,790 lb (1,723 kg)
  • Powerplant: 1 × Armstrong Siddeley Puma piston engine, 230 hp (172 kW)

Performance

  • Maximum speed: 98 kn (113 mph, 182 km/h)
  • Endurance: 4½ hours
  • Service ceiling: 15,500 ft (4,730 m)
  • Climb to 10,000 ft: 18 min 30 sec

Armament

  • Guns: Forward firing Vickers machine gun and 1 or 2 × Rear Lewis guns on scarff ring
  • Bombs: Up to 460 lb (209 kg) bombs

End notes