Performance and Specifications
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Click here for additional detailed views of the STOL CH 701
Download schematic views of the STOL CH 701 assembly
Range and endurance figures are quoted with no fuel reserve. Figures are based on factory prototype results, and are given at standard atmosphere, no wind, unless otherwise indicated. All technical data, specifications, and performance figures are 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 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!”
