Armstrong Whitworth F.K.8

Airplanes

Length

9.4488 m

Flat Wing Span

13.1064 m

Height

3.048 m

Flat Wing Area

50.1676 m²

Max Speed

152.8877 km/h

Max Ceiling

3962.4 m

Number of Engines

Aircraft Engine

First Flight

1916-05-01

Number Built

1650

Total Fuel Capacity

227.3045

Pictures

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Aircraft	Total Fuel Capacity
Armstrong Whitworth F.K.8	227.3045

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Abaris Golden Arrow	Walter M601	9.4488	12.8016	5	Compare
Boeing Model 95	Pratt & Whitney R-1690 Hornet	9.4488	13.4112		Compare
Bristol Boarhound	Bristol Jupiter	9.4488	13.4112		Compare
Airco DH.9C	Siddeley Puma	9.3	12.92	3	Compare
Airco DH.4		9.144	13.1064		Compare
Auster A.2/45		9.144	13.1064		Compare

All data (21 fields)

Name: Armstrong Whitworth F.K.8
Manufacturer: Armstrong Whitworth
Description: The Armstrong Whitworth F.K.8 was a British two-seat general-purpose biplane built by Armstrong Whitworth during the First World War.
First Flight: 1916-05-01
Designer: Frederick Koolhoven
Type: Bomber/Reconnaissance aircraft
Length (m): 9.4488
Height (m): 3.048
Cockpit Crew: 2
Max Speed (km/h): 152.8877
Max Ceiling (m): 3962.4
Armament: 1 × fixed, forward firing .303 in Vickers machine gun and 1 × flexibly mounted .303 in Lewis gun; up to 260 lb (118 kg) bombs
Endurance (h): 3
Number Built: 1650
Powerplant Description: 1 × Beardmore 160 hp water-cooled six-cylinder inline engine
Primary Users: Royal Flying Corps, Qantas
Wikipedia Article (URL): en.wikipedia.org/wiki/Armstrong_Whitworth_F.K.8
Flat Wing Span (m): 13.1064
Flat Wing Area (m²): 50.1676
Aircraft Engine: Beardmore 160 hp
Number of Engines: 1