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The third prototype of the S.E.5 flew at Farnborough on
12 January 1917 powered by a 200hp geared Hispano-
Suiza 8B water-cooled eight-cylinder V-type engine,
but otherwise similar to the 150hp-engined earlier prototypes.
While production deliveries of the 200hp
engine were awaited, airframe modifications were introduced
in the light of early experience with the first
production batch of S.E.5s. In particular, the wing rear
spars were shortened at the tips to provide greater strength, this serving to blunt the previously raked tips
and reduce overall span by 39.4cm. At the
same time, lateral control was improved by shortening
the levers on the ailerons. With a small Avro-type windscreen
in place of the S.E.5's voluminous structure, a
small fabric-covered head fairing behind the cockpit,
the blunt wings and the standard Vickers + Lewis gun
armament, the version with 200hp engine became the
subject of large-scale production as the S.E.5a, starting
with part of the second batch S.E.5s already ordered
from the RAF. Two hundred more were built at Farnborough
itself and, in addition, by the time the war came
to an end in November 1918, some 5125 S.E.5a's had
been built by five companies in less than 18 months:
Austin (1,550), Bleriot & Spad (560), Martinsyde (400),
Vickers (2,215) and Wolseley (400). Production of the
200hp Hispano (in several sub-variants, and including
licence-production by Wolseley as the W.4B Adder I, II
and III) failed to keep pace with this prodigious output,
and numerous operational difficulties with the engine
enhanced the problem. Consequently, many S.E.5a's
were fitted (without change of designation) with the
200hp direct-drive Wolseley W.4A Viper, a derivative
of the French engine. At least six S.E.5a's were flown
with the 200hp Sunbeam Arab I (geared) or Arab II
(direct drive) water-cooled eight-cylinder engine in
trials at Farnborough, and some production aircraft received
high-compression versions of the French-built
Hispano-Suiza engine, increasing maximum" output to
220hp. Twenty-two squadrons of the RFC and the US Air Service were flying the S.E.5a by the time of the
Armistice, but this brought an end to planned largescale
production by Curtiss in the US when only one of
1,000 on order had been completed (in addition to 56
assembled from British components). Service use continued on a small scale for only a short time after the
end of the war, in Australia, Canada and South Africa as
well as with the RAF.
| ENGINE | 1 x Hispano-Suiza engine, 200 hp |
| WEIGHTS |
| Take-off weight | 929 kg | 2048 lb |
| Empty weight | 694 kg | 1530 lb |
| DIMENSIONS |
| Wingspan | 8.11 m | 26 ft 7 in |
| Length | 6.37 m | 20 ft 11 in |
| Height | 2.89 m | 9 ft 6 in |
| Wing area | 22.83 m2 | 245.74 sq ft |
| PERFORMANCE |
| Max. speed | 203 km/h | 126 mph |
| Ceiling | 5180 m | 17000 ft |
 | A three-view drawing (1278 x 942) |
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