Spartan C4

Airplanes

Length

15.24 m

Flat Wing Span

9.7536 m

Height

2.7432 m

Flat Wing Area

27.778 m²

Max Seating

Cruise Speed

175.4185 km/h

Max Speed

208.7319 km/h

Max Ceiling

4572 m

Number of Engines

First Flight

1930-01-01

Number Built

Total Fuel Capacity

321.76

Pictures

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Aircraft	Total Fuel Capacity
Spartan C4	321.76

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Sukhoi Su-17 (1949)		15.253	9.6	Compare
General Dynamics F-16 Fighting Falcon	General Electric F110	14.9352	9.7536	Compare
General Dynamics X-62 VISTA	General Electric F110	14.8	9.8	Compare
Grumman F11F-1F Super Tiger	General Electric J79	14.85	9.65	Compare
Lockheed Martin X-35	Pratt & Whitney F135	15.3924	10.0584	Compare
Saab 35 Draken		15.35	9.42	Compare

All data (20 fields)

Name: Spartan C4
Manufacturer: Spartan Aircraft Ltd
Description: The Spartan C4 was an American four-seat cabin monoplane designed and built by the Spartan Aircraft Company.
First Flight: 1930-01-01
Designer: Spartan Aircraft Ltd
Length (m): 15.24
Height (m): 2.7432
Max Seating: 2
Max Speed (km/h): 208.7319
Cruise Speed (km/h): 175.4185
Max Ceiling (m): 4572
Rate of Climb (m/s): 4.5974
Capacity Description: 2 or 3 passengers, (four seats total)
National Origin: United States of America
Number Built: 7
Powerplant Description: 1 × Wright J-6 9-cylinder air-cooled radial piston engine, 179 kW (240 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Spartan_C4
Flat Wing Span (m): 9.7536
Flat Wing Area (m²): 27.778
Number of Engines: 1