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The Specifications of the Zenith STOL CH750

Specifications Zenith STOL CH750
Wing Span 29ft 10in
Wing Area 144 sq.ft.
Length 21ft 10in
Horizontal Tail Span 8ft 5in
Horizontal Tail Area 22.2 sq.ft
Rudder Tip Height 8ft 8in
Empty Weight 775lbs
Design Gross Weight 1440lbs
Gross Weight (LSA) 1320lbs
Useful Load (LSA) 545lbs
Wing Loading (LSA) 9.15psf
Power Loading 13.2lbs/bhp
Never Exceed Speed (VNE) 125mph
Fuel Capacity 24 Gal.
Cabin Width 42in
Cabin Width (bubble doors) 50in
Load Factor (G) ultimate +6/-3 g
Suitable Power 80-140hp
Max Engine Weight 300lbs

750-3v-sm

The Performance of the Zenith STOL CH750

Figures based on a Zenith CH750 with a gross weight of 1320lbs, standard atmosphere, sea level, no wind.  Range and endurance figures are quoted with no fuel reserves.  All technical data, specifications and performance figures are subject to change without notice.

Performance Continental O-200 (100hp)
Take-off Roll 100ft
Landing Roll 125ft
Max Cruise (Sea Level) 100mph
Stall Speed 35mph
Rate of Climb 1000fpm
Range(standard miles) 440 miles
Endurance 4.4 hours

Light Sport Aircraft Regulations

The STANDARD Zenith CH750 STOL kit aircraft meets the definition of a Light-Sport Aircraft as defined by “Certification of Aircraft and Airmen for the Operation of Light-Sport Aircraft” (7/20/04). A Sport Pilot may fly any aircraft that meets the definition of a Light-Sport Aircraft, and such aircraft does not need to change its certification category to be operated by a Sport Pilot.

Zenith Aircraft Company cannot guarantee that the aircraft, as constructed by the builder, will meet the definition of a Light-Sport Aircraft. Due to the gross weight and stall speed 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 will limit the useful load of the aircraft, and may disqualify the aircraft from meeting the defined category limits.