STOL CH 701 Sport Utility Kit Aircraft

 

Updates

STOL CH 750
CH 750 Cruzer

Design Info
   Wings
  
Tail
   Fuselage
  
Gear

Performance & Specifications

Sport Utility

Building Info

Kit Info

Cabin Details

Drawing & Manuals

 Photo Galleries 

Videos

Engine Info

Press Reviews

Pricing Information

Building & Flying

Builders on the Net

Factory Workshops

  Starter Kit  

Folding Wings

Subscribe to Mail List
Your Email:

For More Information...

High-Lift Design

Four Seat
STOL CH 801

Zenith.Aero

Follow us for updates:

PERFORMANCE AND SPECIFICATIONS
STOL CH 701 take-off...

SPECIFICATIONS STOL CH 701
WING SPAN 27 FEET 8.2 m.
WING AREA 122 SQ.FT. 11.4 m.sq.
LENGTH 20 Ft. 11 In. 6.38 m.
HEIGHT (rudder tip) 8 Ft. 7 In. 2.6 m.
EMPTY WEIGHT 580 LBS. 263 kg.
GROSS WEIGHT 1,100 LBS. 500 kg.
USEFUL LOAD 520 LBS. 236 kg.
WING LOADING 9.0 LBS/FT 43.8 m
POWER LOADING 13.75 LBS/BHP 6.25 kg/BHP
DESIGN LOAD FACTOR (ultimate) +6 G / -3G
CABIN WIDTH (shoulders) 40 INCHES 100 cm.
CABIN WIDTH (optional bubble doors) 44 INCHES 110 cm.
FUEL CAPACITY (std., dual wing tanks) 20 US Gallons
(2 x 10 gal.)
76 liters
(2 x 38 liters)

STOL CH 701

Click here for a full-size view | Click here for additional detailed views of the STOL CH 701
Download schematic views of the STOL CH 701 assembly

STOL CH 701 PERFORMANCE ROTAX 912 (80 HP) ROTAX 912S (100 HP)
  SINGLE DUAL SINGLE DUAL
TOP SPEED (MPH) 85 85 95 95
CRUISE, Sea Level (MPH) 80 80 85 85
75% CRUISE @ 8,000 ft. (TAS*) 92 92 98 98
VNE (MPH) 110 110 110 110
STALL (MPH) 28 30 28 30
RATE OF CLIMB (FPM) 1,100 1,000 1,200 1,100
TAKE-OFF ROLL (FEET) 60 115 50 90
LANDING ROLL (FEET) 80 140 80 140
SERVICE CEILING (FEET) 13,000+ 12,000+ 15,000+ 12,000+
STD. RANGE (MILES) 372 372 350 350
ENDURANCE  4.6 Hrs. 4.6 Hrs. 4.1 Hrs. 4.1 Hrs.

Range and endurance figures are quoted with no fuel reserve. Figures are based on factory prototype results, and are given at standard atmosphere, sea level, no wind, unless otherwise indicated. All technical data, specification and performance figures subject to change without notice. 
* TAS is indicated airspeed corrected for temperature and altitude.  The corrections are approximate.

Engine Limitations: 50 - 100 hp, up to 185 lbs. installed. Alternative engines will affect performance, specifications and flight characteristics of the aircraft. Also, the weight and balance of the aircraft may be adversely affected by alternative engines, and the original fuel system may not be adequate or suitable for some engines. Most alternative engines will require a custom engine mount and engine cowl. Zenith Aircraft Company does not manufacture or directly support engines.

  • Click here to view flight demonstrations of the STOL CH 701's outstanding short take-off and landing (STOL) performance (video clips).
STOL Performance STOL CH 701
True short take-off and landing capability for the serious sport pilot.

Flying the STOL CH 701:
"You're already where you want to be!"

...short landings too!


Zenith.Aero: Online community for active Zenith builders, owners and pilots

The One Week Wonder project at AirVenture 2014

 Zenith Aircraft Company

Zenith Aircraft Company
1881 Airport Road, Mexico Memorial Airport
Mexico, Missouri, 65265  USA.
Tel: 573-581-9000 (Mon - Fri, 8-5 Central),
Comments or questions? Click Here

STOL CH 701

STOL CH 701
STOL CH 750
CH 750 Cruzer
STOL CH 801

STOL Updates

Search zenithair.com

Recommended Reading

Zenith Aircraft Company: 2013-05-06