Javelin Wichawk

Airplanes

Length

5.87 m

Flat Wing Span

7.32 m

Height

2.18 m

Flat Wing Area

17.2 m²

Max Speed

225 km/h

Number of Engines

Aircraft Engine

First Flight

1971-05-24

Number Built

Pictures

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Aircraft
Javelin Wichawk

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Andrews A1	Continental O-170	5.8	7.3	Compare
Caudron C.67		5.8	7.3	Compare
Alcock Scout	Clerget aircraft engines	5.82	7.39	Compare
Grumman American AA-1	Lycoming O-235	5.87	7.46	Compare
Extra EA-230		5.82	7.4	Compare
Arrow Active		5.74	7.32	Compare

All data (20 fields)

Name: Javelin Wichawk
Manufacturer: Javelin Aircraft Co
Description: The Javelin Wichawk is a sporting biplane designed in the United States in the early 1970s and marketed in plan form for amateur construction.
ICAO Code: WICH
First Flight: 1971-05-24
Designer: Dave Blanton
Length (m): 5.87
Height (m): 2.18
Max Speed (km/h): 225
Rate of Climb (m/s): 8.6
Capacity Description: one passenger
National Origin: United States of America
Number Built: 18
Powerplant Description: 1 × Lycoming O-360, 134 kW (180 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Javelin_Wichawk
Flat Wing Span (m): 7.32
Flat Wing Area (m²): 17.2
Wake Category: L
Aircraft Engine: Lycoming O-360
Number of Engines: 1