Armstrong Whitworth F.K.3

· Armstrong Whitworth · 1 × RAF 1

Airplanes

Length

8.8392 m

Flat Wing Span

12.192 m

Height

3.3528 m

Flat Wing Area

41.0631 m²

Max Speed

140.0129 km/h

Max Ceiling

3657.6 m

Number of Engines

Aircraft Engine

First Flight

1915-01-01

Number Built

500

Total Fuel Capacity

127.2905

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Aircraft	Total Fuel Capacity
Armstrong Whitworth F.K.3	127.2905

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Caproni Bergamaschi PL.3	Pratt & Whitney R-1690 Hornet	8.8392	11.8872		Compare
Aermacchi AL-60		8.79	11.84	8	Compare
AEA Silver Dart		9.144	12.192		Compare
Breese-Dallas Model 1		8.5344	12.192		Compare
CAMS 46		9.07	12		Compare
Blériot-SPAD S.40	Lorraine 12D	9.02	12.47		Compare

All data (22 fields)

Name: Armstrong Whitworth F.K.3
Manufacturer: Armstrong Whitworth
Description: The Armstrong Whitworth F.K.3 was a British two-seat general-purpose biplane built by Armstrong Whitworth Aircraft during the First World War.
First Flight: 1915-01-01
Production End: 1917-01-01
Designer: Frederick Koolhoven
Type: General purpose / Trainer aircraft
Length (m): 8.8392
Height (m): 3.3528
Cockpit Crew: 2
Max Speed (km/h): 140.0129
Max Ceiling (m): 3657.6
Armament: 1 × 0.303 in (7.7 mm) Lewis Gun in rear cockpit; up to 112 lb (51 kg) bombs (if flown as single seater)
Endurance (h): 3
Number Built: 500
Powerplant Description: 1 × RAF 1A air-cooled V-8 engine, 67 kW (90 hp) each
Primary Users: Royal Flying Corps
Wikipedia Article (URL): en.wikipedia.org/wiki/Armstrong_Whitworth_F.K.3
Flat Wing Span (m): 12.192
Flat Wing Area (m²): 41.0631
Aircraft Engine: RAF 1
Number of Engines: 1