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Characterised by the pronounced negative stagger of
its mainplanes, which resulted from an attempt on the
part of Geoffrey de Havilland to combine the performance
of the tractor biplane with the cockpit visibility of
pusher aircraft, the D.H.5 was flown late in 1916, and
entered service in May 1917. Immensely strong and
possessing docile handling qualities, but easily outflown
by contemporary fighters at altitudes above
3050m, the D.H.5 was of wooden construction
with plywood and fabric skinning. Power was provided
by a 100hp Le Rhone 9J nine-cylinder rotary and
armament consisted of a single 7.7mm Vickers
gun. Some 550 were built by the parent company;
Darracq Motor Engineering; March, Jones and Cribb,
and British Caudron, but the D.H. 5 was deemed to be of limited success and had been withdrawn from operations
by the end of January 1918.
 | A three-view drawing (1280 x 996) |
| WEIGHTS |
| Take-off weight | 677 kg | 1493 lb |
| Empty weight | 458 kg | 1010 lb |
| DIMENSIONS |
| Wingspan | 7.82 m | 25 ft 8 in |
| Length | 6.71 m | 22 ft 0 in |
| Height | 2.78 m | 9 ft 1 in |
| Wing area | 19.70 m2 | 212.05 sq ft |
| PERFORMANCE |
| Max. speed | 164 km/h | 102 mph |
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