Design and Development
The Flamingo was designed by de Havilland, led by their chief designer, as a twin-engined civil airliner. It was the first all-metal aircraft built by de Havilland. The metal framework was mostly metal-covered with fabric covered control surfaces. Two pilots were seated side-by-side with a radio operator behind them in the cockpit, with the cabin accommodating 12-17 passengers. It featured a retractable undercarriage, slotted flaps and variable pitch propellers, and was considered a highly promising sales prospect for the de Havilland company capable of competing with the American Douglas DC-3 and Lockheed Model 10 Electra.
The first prototype flew on 22 December 1938, powered by 890 hp (660 kW) Bristol Perseus engines. With these, performance was excellent with a takeoff at maximum weight in 750 ft (230 m) and the ability to maintain height or climb at 120 mph (190 km/h) on a single engine. Testing was successful, with the Flamingo being granted a certificate of airworthiness on 30 June 1939, with an initial production run of twenty aircraft being laid down.
A single military transport variant was built to Specification 19/39 as the DH.95 Hertfordshire. It had oval cabin windows instead of rectangular ones, and seating for 22 paratroopers. A proposed order for 40 was cancelled to leave de Havillands free to produce Tiger Moth trainers. The sole Hertfordshire crashed with the loss of 11 lives at Mill Hill, Hertfordshire on 23 October 1940, apparently due to jamming of the elevator.
Read more about this topic: De Havilland Flamingo
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