Zenair CH 100

· Zenair

Airplanes

Length

5.7912 m

Flat Wing Span

6.7056 m

Height

1.8288 m

Flat Wing Area

8.5006 m²

Flat Wing Aspect Ratio

5.28

Cruise Speed

177.0278 km/h

Max Speed

201.168 km/h

Max Ceiling

3657.6 m

Number of Engines

First Flight

1975-05-08

Maximum Take-Off Weight

0.4354 t (paragliders: kg)

Total Fuel Capacity

Maximum Range

643.7376 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Zenair CH 100	0.4354	55	643.7376

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All data (20 fields)

Name: Zenair CH 100
Manufacturer: Zenair
Description: The Zenair Mono-Z CH 100 is a single-seat, single-engined Canadian light aircraft of the 1970s, that was designed by Chris Heintz.
First Flight: 1975-05-08
Designer: Chris Heintz
Length (m): 5.7912
Height (m): 1.8288
Cockpit Crew: 1
Max Speed (km/h): 201.168
Cruise Speed (km/h): 177.0278
Min Speed (km/h): 77.2485
Max Ceiling (m): 3657.6
Rate of Climb (m/s): 4.1656
National Origin: Canada
Powerplant Description: 1 × Volkswagen, 48 kW (65 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Zenair_CH_100
Flat Wing Span (m): 6.7056
Flat Wing Area (m²): 8.5006
Flat Wing Aspect Ratio: 5.28
Number of Engines: 1