Armstrong Whitworth Siskin

Airplanes

Length

7.62 m

Flat Wing Span

10.0584 m

Height

3.048 m

Flat Wing Area

27.2206 m²

Max Speed

251.0577 km/h

Max Ceiling

8229.6 m

Number of Engines

First Flight

1919-05-01

Entry Into service

1923-01-01

Number Built

485

Maximum Take-Off Weight

1.3662 t (paragliders: kg)

Maximum Range

450.6163 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Armstrong Whitworth Siskin	1.3662	450.6163

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Bernard 20	Hispano-Suiza 12Jb	7.45	10.8		Compare
Aubert Cigale	Lycoming O-320	7.5	10	3	Compare
Arado Ar 66		8.3	10		Compare
Aero Boero 260AG		7.3	10.9		Compare
Bellanca Aries	Lycoming O-540	7.9248	9.4488		Compare
Berliner-Joyce OJ		7.62	10.0584		Compare

All data (23 fields)

Name: Armstrong Whitworth Siskin
Manufacturer: Armstrong Whitworth
Description: The Armstrong Whitworth Siskin was a sesquiplane single-seat fighter aircraft developed and produced by the British aircraft manufacturer Armstrong Whitworth Aircraft.
First Flight: 1919-05-01
Entry Into service: 1923-01-01
Service End: 1932-01-01
Designer: F.M. Green
Type: Fighter
Length (m): 7.62
Height (m): 3.048
Cockpit Crew: 1
Max Speed (km/h): 251.0577
Max Ceiling (m): 8229.6
Rate of Climb (m/s): 15.0012
Armament: Two × 0.303 in Vickers machine guns; Four × 20 lb bombs under-wing
Endurance (h): 72
Number Built: 485
Powerplant Description: 1 × Armstrong Siddeley Jaguar IV 14-cylinder air-cooled radial piston engine, 287 kW (385 hp) each
Primary Users: Royal Air Force, Royal Canadian Air Force , Royal Swedish Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Armstrong_Whitworth_Siskin
Flat Wing Span (m): 10.0584
Flat Wing Area (m²): 27.2206
Number of Engines: 1