Zenair CH 200

· Zenair · 1 × Continental O-200

Airplanes

Length

6.25 m

Flat Wing Span

7 m

Height

2.11 m

Flat Wing Area

9.8 m²

Flat Wing Aspect Ratio

Cruise Speed

209.2147 km/h

Max Speed

236.5736 km/h

Max Ceiling

4602.48 m

Number of Engines

Aircraft Engine

First Flight

1970-03-22

Maximum Take-Off Weight

0.6577 t (paragliders: kg)

Total Fuel Capacity

72.5

Maximum Range

836.8589 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Zenair CH 200	0.6577	72.5	836.8589

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All data (21 fields)

Name: Zenair CH 200
Manufacturer: Zenair
Description: The Zenair Zenith CH 200 and CH 250 are a family of Canadian single-engined homebuilt light aircraft.
First Flight: 1970-03-22
Designer: Chris Heintz
Length (m): 6.25
Height (m): 2.11
Cockpit Crew: 2
Max Speed (km/h): 236.5736
Cruise Speed (km/h): 209.2147
Min Speed (km/h): 85.2952
Max Ceiling (m): 4602.48
Rate of Climb (m/s): 4.064
National Origin: France
Powerplant Description: 1 × Continental O-200 air-cooled flat-four, 75 kW (100 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Zenair_CH_200
Flat Wing Span (m): 7
Flat Wing Area (m²): 9.8
Flat Wing Aspect Ratio: 5
Aircraft Engine: Continental O-200
Number of Engines: 1