|Specifications||Zenith STOL CH750|
|Wing Span||29ft 10in|
|Wing Area||144 sq.ft.|
|Horizontal Tail Span||8ft 5in|
|Horizontal Tail Area||22.2 sq.ft|
|Rudder Tip Height||8ft 8in|
|Design Gross Weight||1440lbs|
|Gross Weight (LSA)||1320lbs|
|Useful Load (LSA)||545lbs|
|Wing Loading (LSA)||9.15psf|
|Never Exceed Speed (VNE)||125mph|
|Fuel Capacity||24 Gal.|
|Cabin Width (bubble doors)||50in|
|Load Factor (G) ultimate||+6/-3 g|
|Max Engine Weight||300lbs|
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)|
|Max Cruise (Sea Level)||100mph|
|Rate of Climb||1000fpm|
|Range(standard miles)||440 miles|
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.