Zenith STOL CH 701

Airplanes

Length

6.096 m

Flat Wing Span

8.2296 m

Height

2.4384 m

Flat Wing Area

11.3342 m²

Flat Wing Aspect Ratio

5.98

Cruise Speed

128.7475 km/h

Max Speed

136.7942 km/h

Max Ceiling

3657.6 m

Number of Engines

Aircraft Engine

First Flight

1986-01-01

Entry Into service

1986-01-01

Number Built

870

Maximum Take-Off Weight

0.499 t (paragliders: kg)

Total Fuel Capacity

Maximum Range

598.676 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Zenith STOL CH 701	0.499	76	598.676

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aerosport Woody Pusher	Continental O-170	6.096	8.8392	1	Compare
Armstrong Whitworth Ara	ABC Dragonfly	6.096	8.2296		Compare
Albatros L 69	Siemens-Halske Sh 12	6.1	8.06		Compare
AeroMobil s.r.o. AeroMobil	Rotax 912	6	8.32		Compare
Braunschweig LF-1 Zaunkönig		6.08	8.02		Compare
Airdrome Nieuport 24	Hirth F-30	5.9436	8.1991		Compare

All data (27 fields)

Name: Zenith STOL CH 701
Manufacturer: Zenith Aircraft Company
Description: The Zenith STOL CH 701 and CH 750 are a family of light, two-place kit-built STOL aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario, based company, Zenair.
ICAO Code: CH70
First Flight: 1986-01-01
Entry Into service: 1986-01-01
Designer: Chris Heintz
Type: Kit aircraft
Length (m): 6.096
Height (m): 2.4384
Max Speed (km/h): 136.7942
Cruise Speed (km/h): 128.7475
Min Speed (km/h): 48.2803
Max Ceiling (m): 3657.6
Rate of Climb (m/s): 5.08
Endurance (h): 4.6
National Origin: United States of America
Number Built: 870
Powerplant Description: 1 × Rotax 912 four-cylinder liquid-cooled piston engine, 60 kW (80 hp) each
Status: In production
Wikipedia Article (URL): en.wikipedia.org/wiki/Zenith_STOL_CH_701
Flat Wing Span (m): 8.2296
Flat Wing Area (m²): 11.3342
Flat Wing Aspect Ratio: 5.98
Wake Category: L
Aircraft Engine: Rotax 912
Number of Engines: 1