Zenair CH 50 Mini-Z

ยท Zenair
Flat Wing Span
5.7 m
Height
1.6 m
Flat Wing Area
6.2 m²
Cruise Speed
138 km/h
Max Speed
148 km/h
Number of Engines
1
First Flight
1979-01-01
Number Built
1
Maximum Take-Off Weight
0.252 t (paragliders: kg)
Maximum Range
354 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Zenair CH 50 Mini-Z 0.252 354
All data (19 fields)
Name
Zenair CH 50 Mini-Z
Manufacturer
Zenair
Description
The Zenair CH 50 Mini-Z is a single-seat light aircraft built by Chris Heintz in Canada in the late 1970s.
ICAO Code
CH50
First Flight
1979-01-01
Designer
Chris Heintz
Height (m)
1.6
Cockpit Crew
1
Max Speed (km/h)
148
Cruise Speed (km/h)
138
Rate of Climb (m/s)
2.75
National Origin
Canada
Number Built
1
Powerplant Description
1 × Cuyuna two-cylinder, two-stroke engine, 18 kW (24 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Zenair_CH_50_Mini-Z
Flat Wing Span (m)
5.7
Flat Wing Area (m²)
6.2
Wake Category
L
Number of Engines
1