DE HAVILLAND DH.86

The De Havilland DH.86 was designed in 1933 and first flew on January 14, 1934, as a ten-passenger four-engined airliner initially to meet Australian requirements. Production totalled 62 in De Havilland DH.86, De Havilland DH.86A and De Havilland DH.86B ver-sions, with 200 hp Gipsy Six Srs I engines, of which four went to RAF - two as VIP transports for No 24 Squadron and two as wireless-operator trainers to Specification 28/37 for Radio School at Cranwell. Twenty-two DH.86A/Bs assigned to National Air Communications September 1939 operating in civil guise; four remained civil for UK domestic services throughout war, eight others impressed for RAF and FAA use in UK, plus ten impressed in Middle East and India. Seven Australian civil De Havilland DH.86s impressed by RAAF 1939/41, including three in Middle East equipped as ambulances. Three De Havilland DH.86s in New Zealand impressed by RNZAF September 1939 and served to 1945 as radio/navigation trainers.

Max speed, 166 mph (267 km/h). Gross weight, 10,250 Ib (4,654 kg). Span, 64ft 6 in (19.66 m). Length, 46ft 1 in (14.05 m).