The De Havilland D.H.89 Dragon Rapide six/eight-passenger airliner was a scaled-down, twin engined version of the D.H.86 Dragon four-engined biplane airliner. The D.H.89 had a squarish section fuselage with large side windows, tapered biplane wings, and a trousered fixed undercarriage. Initially, it was powered by a pair of 200 hp De Havilland Gipsy Six six-cylinder air-cooled engines. The first prototype flew on April 17, 1934. The D.H.89 remained in production for ten years, a total of 728 being built. In its day, it was one of the most widely-used air transports in the world. Although officially known as the Dragon Rapide, it usually known simply as the Rapide.
The D.H.89 had a maximum speed of 157 mph, and a cruising speed of 132 mph. Initial climb rate was 1000 feet per minute, ceiling was 19,500 feet, and range was 578 miles. Weights were 3346 pounds tare, 5500 lbs. all-up. Dimensions were wingspan 48 feet 0 inches, length 34 feet 6 inches, height 10 feet 3 inches, and wing area 336 square feet. The first British operator of the Dragon Rapide was Hillmans Airways Ltd., making its debut with that airline on July 13, 1934. Railway Air Services Ltd. operated D.H.89s on trunk route between Croydon, Speke, Renfrew, and Belfast, and for summer services between Speke, Whitchurch, Eastleigh, and Shoreham. Two Dragon Rapides were acquired by Jersey Airways Ltd. The 1936 Dragon Rapide had a nose landing light, thickened wingtips, and cabin heating.