Zenair CH 300

· Zenair · 1 × Lycoming O-320

Airplanes

Length

6.85 m

Flat Wing Span

8.1 m

Height

2.08 m

Flat Wing Area

12 m²

Flat Wing Aspect Ratio

5.48

Max Seating

Cruise Speed

230.1362 km/h

Max Speed

257.495 km/h

Number of Engines

Aircraft Engine

First Flight

1977-07-09

Maximum Take-Off Weight

0.8391 t (paragliders: kg)

Maximum Range

852.9523 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Zenair CH 300	0.8391	852.9523

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Aerotec A-122 Uirapuru	Lycoming O-320	6.6	8.5	Compare
Alpi Pioneer 400	Rotax 916 iS	7	8.8	Compare
Aerocar IMP		6.7056	8.8392	Compare
AMD Alarus	Lycoming O-235	7.0104	8.5344	Compare
Aviatik (Berg) D.I	Austro-Daimler 6	6.86	8	Compare
Aerotec A-132 Tangará		7.085	9	Compare

All data (22 fields)

Name: Zenair CH 300
Manufacturer: Zenair
Description: The Zenair Tri-Z CH 300 is a three-seat Canadian homebuilt light aircraft.
First Flight: 1977-07-09
Designer: Chris Heintz
Length (m): 6.85
Height (m): 2.08
Cockpit Crew: 1
Max Seating: 2
Max Speed (km/h): 257.495
Cruise Speed (km/h): 230.1362
Min Speed (km/h): 85.2952
Rate of Climb (m/s): 5.08
Capacity Description: 2 passengers
National Origin: Canada
Powerplant Description: 1 × Lycoming O-320 air-cooled flat-four, 112 kW (150 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Zenair_CH_300
Flat Wing Span (m): 8.1
Flat Wing Area (m²): 12
Flat Wing Aspect Ratio: 5.48
Aircraft Engine: Lycoming O-320
Number of Engines: 1