Specs And Performances - Zenith STOL CH 750
Specs And Performances - Zenith STOL CH 750
Specs And Performances - Zenith STOL CH 750
Specs And Performances - Zenith STOL CH 750
Specs And Performances - Zenith STOL CH 750
Specs And Performances - Zenith STOL CH 750
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Specifications

SpecificationsZenith STOL CH750
Wing Span29ft 10in
Wing Area144 sq.ft.
Length21ft 10in
Horizontal Tail Span8ft 5in
Horizontal Tail Area22.2 sq.ft
Rudder Tip Height8ft 8in
Empty Weight775lbs
Design Gross Weight1440lbs
Gross Weight (LSA)1320lbs
Useful Load (LSA)545lbs
Wing Loading (LSA)9.15psf
Power Loading13.2lbs/bhp
Never Exceed Speed (VNE)125mph
Fuel Capacity24 Gal.
Cabin Width42in
Cabin Width (bubble doors)50in
Load Factor (G) ultimate+6/-3 g
Suitable Power80-160hp
Max Engine Weight300lbs

Performances

Figures based on a Zenith STOL CH 750 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.

 

PerformanceContinental O-200 (100hp)
Take-off Roll100ft
Landing Roll125ft
Max Cruise (Sea Level)100mph
Stall Speed35mph
Rate of Climb1000fpm
Range(standard miles)440 miles
Endurance4.4 hours

Light Sport Aircraft Regulations

The STANDARD Zenith STOL CH 750 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.