Vickers VC.1 Viking

· Vickers

Airplanes

Length

19.812 m

Flat Wing Span

27.1272 m

Height

5.7912 m

Flat Wing Area

81.9405 m²

Cruise Speed

337.9622 km/h

Max Speed

423.2575 km/h

Max Ceiling

7620 m

Number of Engines

First Flight

1945-06-22

Entry Into service

1946-01-01

Number Built

163

Maximum Take-Off Weight

15.4221 t (paragliders: kg)

Total Fuel Capacity

3364.107

Maximum Range

2735.885 km

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Vickers VC.1 Viking	15.4221	3364.107	2735.885

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Saab 90 Scandia	Pratt & Whitney R-2180-E Twin Wasp E	21.3	28	24	Compare
Saunders-Roe A.36 Lerwick		19.2024	24.384		Compare
Focke-Wulf Fw 206		19.6	27.3		Compare
Blackburn B-20	Rolls-Royce Vulture	21.0312	24.9936		Compare
CASA/IPTN CN-235	General Electric T700	21.4	25.81	51	Compare
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All data (23 fields)

Name: Vickers VC.1 Viking
Manufacturer: Vickers
Description: The Vickers VC.1 Viking is a British twin-engine short-range airliner derived from the Vickers Wellington bomber and built by Vickers-Armstrongs Limited at Brooklands near Weybridge in Surrey.
First Flight: 1945-06-22
Entry Into service: 1946-01-01
Production End: 1954-01-01
Designer: R.K. Pierson
Type: Airliner
Length (m): 19.812
Height (m): 5.7912
Max Speed (km/h): 423.2575
Cruise Speed (km/h): 337.9622
Max Ceiling (m): 7620
Rate of Climb (m/s): 7.62
National Origin: United Kingdom
Number Built: 163
Powerplant Description: 2 × Bristol Hercules 634 14-cylinder two-row radial engines, 1260 kW (1690 hp) each
Primary Users: British European Airways
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Vickers_VC.1_Viking
Flat Wing Span (m): 27.1272
Flat Wing Area (m²): 81.9405
Number of Engines: 2