Zenair CH 150

· Zenair

Airplanes

Length

6.17 m

Flat Wing Span

6.15 m

Height

1.52 m

Cruise Speed

257.4278 km/h

Max Speed

277.7998 km/h

Max Ceiling

4876.8 m

Number of Engines

First Flight

1980-01-01

Entry Into service

1980-01-01

Maximum Take-Off Weight

0.5216 t (paragliders: kg)

Maximum Range

1223.101 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Zenair CH 150	0.5216	1223.101

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Zenair CH 180		6.17	6.15	Compare
Van's Aircraft RV-3	Lycoming O-320	5.7912	5.7912	Compare
Godbille JG.1B	Potez 4E	6.1	6.2	Compare
Lacey M-10	Continental O-200	6.096	6.096	Compare
Miles M.35 Libellula	De Havilland Gipsy Major	6.096	6.096	Compare
PAR Special	Continental O-190	6.096	6.096	Compare

All data (19 fields)

Name: Zenair CH 150
Manufacturer: Zenair
Description: The Zenith CH 150 Acro Zenith is a Canadian single-engine, low wing, all-aluminum aircraft designed by Chris Heintz and produced by Zenair in kit form for amateur construction.
First Flight: 1980-01-01
Entry Into service: 1980-01-01
Designer: Chris Heintz
Length (m): 6.17
Height (m): 1.52
Cockpit Crew: 1
Max Speed (km/h): 277.7998
Cruise Speed (km/h): 257.4278
Min Speed (km/h): 88.8959
Max Ceiling (m): 4876.8
Rate of Climb (m/s): 11.176
National Origin: Canada
Powerplant Description: 1 × Lycoming 0-320, 112 kW (150 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Zenair_CH_150
Flat Wing Span (m): 6.15
Number of Engines: 1