Airspeed Oxford

Airplanes

Length

10.3632 m

Flat Wing Span

16.1544 m

Height

3.3528 m

Flat Wing Area

32.3303 m²

Max Speed

308.994 km/h

Max Ceiling

7178.04 m

Number of Engines

Aircraft Engine

First Flight

1937-06-19

Number Built

8751

Total Fuel Capacity

709.19

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity
Airspeed Oxford	709.19

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Airspeed Envoy	Armstrong Siddeley Cheetah	10.3632	15.8496	6	Compare
Curtiss Kingbird		10.3632	16.4592	7	Compare
Dewoitine D.750	Renault 12R	10.3632	15.8496		Compare
Airspeed Consul		10.668	16.1544		Compare
Tugan Gannet	De Havilland Gipsy Six	10.51	15.85		Compare
Airspeed Viceroy	Armstrong Siddeley Cheetah	10.3632	15.5448		Compare

All data (23 fields)

Name: Airspeed Oxford
Manufacturer: Airspeed Ltd
Description: The Airspeed AS.10 Oxford is a twin-engine monoplane aircraft developed and manufactured by Airspeed.
First Flight: 1937-06-19
Designer: Airspeed Ltd
Type: Training aircraft
Length (m): 10.3632
Height (m): 3.3528
Cockpit Crew: 3
Max Speed (km/h): 308.994
Max Ceiling (m): 7178.04
Rate of Climb (m/s): 6.8072
Armament: 1 × 0.303 in (7.7 mm) Vickers K machine gun in dorsal turret; 16 × 11.5 lb practice bombs carried externally
Endurance (h): 5.5
Number Built: 8751
Powerplant Description: 2 × Armstrong Siddeley Cheetah X radial engines, 261 kW (350 hp) each
Primary Users: Royal Air Force
Status: Out of production, out of service
Wikipedia Article (URL): en.wikipedia.org/wiki/Airspeed_Oxford
Flat Wing Span (m): 16.1544
Flat Wing Area (m²): 32.3303
Aircraft Engine: Armstrong Siddeley Cheetah
Number of Engines: 2