The DH.9A was planned as an improved version of the existing
Airco DH.9. The DH.9 was a disappointment owing to its under-performing and unreliable engines, and the DH.9A was to use a more powerful engine to resolve this. As the
Rolls-Royce Eagle engine used in the successful
DH.4 was unavailable in sufficient quantities, the new American
Liberty engine was chosen instead. As
Airco was busy developing the
Airco DH.10 Amiens twin-engined bomber, detailed design was carried out by
Westland Aircraft. The DH.9 was fitted with new, longer-span wings and a strengthened fuselage structure. The first prototype flew in March 1918, powered by a Rolls-Royce Eagle as no Liberty engines were yet available. The prototype proved successful, with the first Liberty-engined DH.9A flying on 19 April 1918, and deliveries to the
Royal Air Force starting in June. By the end of the war, a total of 2,250 DH.9As had been ordered, with 885 being built by the end of the year. As it was decided that the DH.9A would be a standard type in the postwar RAF, the majority of outstanding orders were fulfilled, with 1,730 being built under the wartime contracts before production ceased in 1919. While the existing aircraft were subject to a programme of refurbishment, a number of small contracts were placed for new production of DH.9As in 1925–26. These contracts resulted in a further 268 DH.9As being built. The new production and refurbished aircraft included batches of dual control
trainers, as well as six aircraft powered by
Napier Lion engines, which were capable of a maximum speed of .
Soviet versions The Soviet Union acquired a number of DH.9A’s during the
Allied intervention in the Russian Civil War; they built large numbers of an unlicensed copy of the aircraft, supervised by
N. N. Polikarpov and designated the
Polikarpov R-1. After the production of 20 DH.4 copies, followed by about 200 copies of the DH.9 powered by the
Mercedes D.IV engine (also designated R-1) and a further 130 powered by the
Siddeley Puma (designated
R-2), a copy of the DH.9A powered by the M-5 engine, a Soviet copy of the DH.9A's Liberty, entered production in 1924. Over 2,400 built from 1922 to 1932. The
R-4 was a modification of the R-1, with the engine lowered and moved forward by to improve both the forward visibility and the C.G position. The nose shape was improved by fairing and by installing a retractable ventral radiator. Overall length was increased by . Landing legs were changed from wood to steel. Testing showed insufficient improvement over the R-1 to justify production but late R-1s incorporated some of the modifications.
US version and pressurised flights The United States also planned to adopt the DH.9A as a replacement for the DH.4. Development work on the Americanization of the aircraft commenced at
McCook Field in
Dayton, Ohio. Plans called for
Curtiss to build 4,000 modified aircraft, designated
USD-9A. This order was cancelled with the end of the war and only nine were built by McCook Field and
Dayton-Wright. ==Operational history==