Airspeed Consul

· Airspeed Ltd

Airplanes

Length

10.668 m

Flat Wing Span

16.1544 m

Height

3.048 m

Flat Wing Area

32.3303 m²

Cruise Speed

262.3231 km/h

Max Speed

305.7754 km/h

Max Ceiling

5791.2 m

Number of Engines

First Flight

1946-01-01

Number Built

162

Maximum Take-Off Weight

3.7421 t (paragliders: kg)

Total Fuel Capacity

709.19

Maximum Range

1448.41 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Airspeed Consul	3.7421	709.19	1448.41

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beechcraft Queen Air	Lycoming O-540	10.668	15.24	9	Compare
Lockheed Model 12 Electra Junior		10.9728	14.9352	6	Compare
Towle WC		10.668	15.8496		Compare
Handley Page Hamlet	Armstrong Siddeley Lynx	10.62	15.85		Compare
Britten-Norman Defender		12.2	16.15	16	Compare
Cessna 425	Pratt & Whitney Canada PT6	10.668	13.4112		Compare

All data (23 fields)

Name: Airspeed Consul
Manufacturer: Airspeed Ltd
Description: The Airspeed Consul is a twin-engined light transport aircraft and affordable airliner designed and produced by the British aircraft manufacturer Airspeed Limited.
First Flight: 1946-01-01
Designer: Airspeed Ltd
Type: Utility transport
Length (m): 10.668
Height (m): 3.048
Cockpit Crew: 1
Max Speed (km/h): 305.7754
Cruise Speed (km/h): 262.3231
Min Speed (km/h): 102.998
Max Ceiling (m): 5791.2
Rate of Climb (m/s): 5.4356
Capacity Description: six passengers
Number Built: 162
Powerplant Description: 2 × Armstrong Siddeley Cheetah 10 seven cylinder air-cooled radial piston engines, 295 kW (395 hp) each
Primary Users: Israeli Defence Force Air Force, Argentine Air Force , Union of Burma Air Force , Royal New Zealand Air Force
Status: Out of production, out of service
Wikipedia Article (URL): en.wikipedia.org/wiki/Airspeed_Consul
Flat Wing Span (m): 16.1544
Flat Wing Area (m²): 32.3303
Number of Engines: 2