Sadly, the link to Chris Young's apparently definitive webpage that RT posted no longer works (although almost every website mentioning the Flamingo includes it somewhere), so I thought I'd do my own.
The DH.95, a twin-engined 12/17-passenger commercial transport, was De Havilland's first all-metal areoplane. It was designed by a team headed by R E Bishop, and apparently including W J Jakimuk, a Pole who had been responsible for the design of the PZL 24 and PZL 50 Jastrab fighters, and who later emigrated to Canada to join the design team at deHavilland Canada. The prototype, powered by two 890hp Perseus XIIC engines, flew on 23rd December 1938, piloted by de Havilland's chief test pilot, Geoffrey de Havilland Jr.
Performance of the prototype was promising, with take off 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.
The prototype was delivered to Jersey Airways for evaulation and became the first revenue-earning Flamingo in 1939.
(picture from http://www.airliners...ats.main?id=177
De Havilland DH.95 Flamingo protoype G-AFUE in 1939
A further order from Jersey Airways was frustrated by the outbreak of war, and the prototype was transferred to RAF duties.
BOAC ordered eight Flamingos with 930 hp Perseus XVI engines, after being denied the credit necessary to buy Douglas DC-5s, and these were delivered in 1940/41, and were based in the Middle East throughout the war.
Two were ordered as VIP transports for the King's Flight (Specification 21/39), and were delivered in September 1940.
One was ordered as a communications aircraft for No 24 Sqn (Specification 20/39), and was delivered in May 1940.
A further three (or four â€“ the number produced varies between 16 and 17) aircraft were delivered to the RAF, with 2 going to the Fleet Air Arm.
All Flamingos were fitted with the Sperry Automatic Pilot
(Picture from http://www.jaapteeuw...RTFORDSHIRE.htm )
(picture from http://www.century-o...images/d/24.jpg )
The first FAA aircraft, BT312, was impressed and delivered to the RN at Hatfield in May 1940. It was named "Merlin VI", delivered to 782 squadron at RNAS Donibristle on 30 November 1940. R2766 was also delivered to 782 squadron at Donibristle, on 14 March 1945, but was quickly used as spares for BT312 in May 1945. The aircraft BT312 was the last of the type to see service with the FAA returned to the civil register as G-AFYH in 1946.
One DH.95 De Havilland Hertfordshire military transport version, designated R2510, was produced to Specification 19/39 with smaller, oval cabin windows and provision for 22 paratroopers sitting on bench seats along the main cabin walls. A proposed order for (30 or 40?) was cancelled to leave de Havilland free to produce Tiger Moth trainers, and the sole Hertfordshire crashed with the loss of 11 lives at Mill Hill, Hertfordshire on 23rd October 1940, apparently because of elevator jamming.
Flamingos were mostly withdrawn from service by 1950 - the last was scrapped in 1954
(picture from http://1000aircraftp...om/APS/2625.htm )
The photo shows AE444 (c/n 95005) carrying DH test marks E-16 undergoing single engine testing. It was an engine and propeller test bed.
Aircraft Type: de Havilland D.H.95 Flamingo Mk I
Primary Role: Transport
First Flight: 23 Dec 1938
Manufacturer: de Havilland
Engine: Two Bristol Perseus XVI nine cylinder sleeve valve air cooled radial engines with maximum power of 930 hp. Three blade full feathering airscrews of 12 ft 9 in diameter
Wingspan: 21.34m, 70 ft 0 in
Length: 15.72m, 51 ft 7 in
Height: 4.65m, 15 ft 3 in
Wing Area: 60.48 sq m, 651 sq ft
Wing load: 27.68 lbs/ft2, 135.00 kg/qm
Empty Weight 5137kg, 12,020 lbs
Max take-off weight: 8,172 kg, 18,000 Ib
Max Speed: 391 kmph; 243 mph, 211 kts
Cruise: 328 kmph, 177 kts
Service Ceiling: 6,370m, 20,899 ft
Rate of Climb: 1,470 ft/min at sea level
Range: 2,165 km, 1,169 nautical miles, 1,345 miles
Crew: 2-3 crew, 17 passengers (22 for Hertfordshire)
Wing: High wing cantilever monoplane. All metal structure with metal skins inboard and forward of spar, rest fabric covered. Ailerons and flaps have metal structure with fabric covering
Fuselage: Metal stressed skin structure
Tail Unit: Cantilever monoplane type with twin fins and rudders. Tailplane and fins all metal. Elevators and rudders have metal structure with fabric covering
Landing Gear: Retractable type. Each unit consists of a single leg which retracts backwards into tails of engine nacelles. Non retractable tailwheel
Accommodation: Enclosed cabin for two pilots in nose with radio operator immediately behind. Passenger cabin can be arranged for up to 17 passengers
(picture from http://www.fleetaira...ft/Flamingo.htm )
An interesting picture from a cigarette card from the 1930s, showing a Flamingo with 3 rear fins!
All text, performance data and pictures are from the following sites: