STOL CH 750 Light Sport Utility Airplane

  

STOL CH 750
Performance
& Specifications
Cabin
  - Panel
Price
Photos
Kit Photos
Videos
Updates

  

Related designs:

NEW
CH 750 CRUZER

Original
STOL CH 701
Performance
& Specs
Photo Galleries 
Videos
Updates

Factory Workshop

Press Reviews

Four-Seat
STOL CH 801

High-Lift Design
 

Subscribe to Mail List
Your Email:

More Info...
STOL Info

Follow us for updates:

PERFORMANCE AND SPECIFICATIONS
STOL CH 750
 

SPECIFICATIONS STOL CH 750
(Based on factory prototype, equipped with 100-hp Continental O-200 powerplant)
WING SPAN 29 FT. 10 In. 9.1 m.
HEIGHT (rudder tip) 8 Ft. 8 In. 2.6 m.
WING AREA 144 SQ.FT. 13.4 m.sq.
WING CHORD 4 Ft. 10 In. 1.5 m.
LENGTH 21 Ft. 10 In. 6.7 m.
HORIZONTAL TAIL SPAN 8 Ft. 5 In. 2.6 m.
HORIZONTAL TAIL AREA 22.2 Sq. Ft. 2.0 m.sq.
EMPTY WEIGHT 775 LBS. 350 kg.
DESIGN GROSS WEIGHT (Edition 2) 1,440 LBS. 652 kg.
GROSS WEIGHT (LSA Limit) 1,320 LBS. 600 kg.
USEFUL LOAD (LSA) 545 LBS. 250 kg.
WING LOADING (LSA) 9.15 LBS/FT.SQ 44.8 m.sq.
POWER LOADING (LSA) 13.2 LBS/BHP 6.0 kg/BHP
DESIGN LOAD FACTOR (ultimate) +6 G / -3 G
NEVER EXCEED SPEED (VNE) 125 MPH 200 km/h
CABIN WIDTH 42 INCHES 100 cm.
CABIN WIDTH (bubble doors) 50 INCHES 1.27 m.
FUEL CAPACITY (std., dual wing tanks) 24 US Gallons
(2 x 12 gal.)
90 liters
(2 x 45 liters)
SUITABLE POWER / Max Engine Weight 80 - 140 hp.  /  300 lbs. installed

STOL CH 750

Click here for a full-size view

STOL CH 750 PERFORMANCE Continental O-200 - 100 hp
@ gross weight 1,320 lbs (LSA Limit)
TAKE-OFF ROLL 100 Feet 30 m.
LANDING ROLL 125 Feet 38 m.
MAX. CRUISE, Sea Level 100 MPH 162 km/h
STALL, flaps down 35 MPH 56 km/h
RATE OF CLIMB 1,000 fpm 5.1 m/s
SERVICE CEILING 14,000+ feet 4,200+ m.
RANGE (standard, no reserve) 440 miles 710 km.
ENDURANCE (standard, no reserve) 4.4 Hours 4.4 Hours

 

Specification and performance figures quoted with the Continental O-200-A engine (100 HP). Standard atmosphere, sea level, no wind.
Performance and specification figures based on prototype flight test results. All technical data, specification and performance figures subject to change without notice. 
Powerplant range: 80 - 125 HP engines.
Different engines and installed options will affect performance and specification figures. Heavier engines will limit useful load (by increasing the empty weight).

Engine Limitations: 80 - 140 hp, up to 300 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.

While the STOL CH 750 was developed to meet the definition of a light-sport aircraft, as defined in the FAA's Sport Pilot category, Zenith Aircraft Company cannot guarantee that the aircraft, as constructed by the builder, will meet the definition. Due to the gross weight limitations of the Sport Pilot / Light-Sport Aircraft category, it is recommended that the aircraft be kept as light as possible if planning to operate the aircraft in this category. Larger and heavier engines and other installed equipment limit the useful load of the aircraft, and may disqualify the aircraft from meeting the defined category limits of the Sport Pilot category.

STOL Performance STOL CH 750
True short take-off and landing
capability for the serious sport pilot.

 






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

New exclusive Zenith T-shirts from EAA!

 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

More Information

Zenith Aircraft Company: 2015-02-12