Armstrong Whitworth F.K.10
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Frederik Koolhoven's final designs for Armstrong Whitworth were several quad-ruplhnes in early 1916. A batch of 50 improved F.K.9 versions, later designated F. K. 10, was ordered from Angus Sanderson & Company of Newcastle-on-Tyne on December 30, 1916 on behalf of the RFC.
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Engine: Clerget 9B rotary, 130hp
Wingspan: 27 ft 10 in / 8.4 m
Length: 22 ft 3 in / 6.7 m
Height: 3.5 m (11 ft 6 in)
Empty weight: 1226 lb / 556 kg
Loaded weight: 2038 lb / 924 kg
Maximum speed: 169 km/h (105 mph) at ground level
Service ceiling: Approx 3660 m (12000 ft)
Armament: 1 Lewis .303‑in (7.7‑mm) mg
Engine: Le Rhone 9J, 110 hp
Wingspan: 8.48 m / 27 ft 10 in
Length: 6.78 m / 22 ft 3 in
Height: 3.50 m / 11 ft 6 in
Wing area: 36.27 sq.m / 390.41 sq ft
Take-off weight: 916 kg / 2019 lb
Empty weight: 560 kg / 1235 lb
Max. speed: 135 km/h / 84 mph
Armament: 1 x fixed .303 Vickers mg, 1 x Scarff-mounted .303 Vicker mg
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