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Based on the popular STOL CH 701 design from Chris Heintz that was first introduced more than 25 years ago, the STOL CH 750 design incorporates all of the 701's amazing short-field capabilities, while maximizing cabin size and load carrying capability allowed under the FAA's Sport Pilot / Light Sport Aircraftcategory. 

 

Like the original, the STOL CH 750 aircraft was developed as an "off-airport" short take-off and landing kit aircraft to fulfill the demanding requirements of both sport pilots and first-time builders.  Designer Chris Heintz has combined the features and advantages of a "real" airplane with the short-field capabilities of "ultralight" aircraft. The aircraft features fixed leading-edge slats for high lift, full-span flaperons (both ailerons and flaps), an all-flying rudder, and durable all-metal construction.

 

The modern STOL CH 750 design is available as an easy-to-build kit which revolutionizes ease and simplicity of construction, drawing upon Zenith's decades of experience in the kit industry.

 

Amazing short take-off and landing (STOL performance)

Surprisingly competitive cruise speed

Huge cabin, side-by-side seating, easy access  *** New raised skylight and increased cabin height ***

Spectacular "wrap-around" visibility

Many engine choices: Continental, Jabiru, Rotax, Corvair, and more...

Outstanding controls: full length flaperons and all-flying rudder

Great bushplane capabilities, simplicity of a tricycle gear.

 

 

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 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 CLIMB1,000 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