Specs and Performances - CH 750 Cruzer
Specs and Performances - CH 750 Cruzer
Specs and Performances - CH 750 Cruzer
Specs and Performances - CH 750 Cruzer
Specs and Performances - CH 750 Cruzer
Specs and Performances - CH 750 Cruzer
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Specifications - Zenith CH 750 Cruzer

SpecificationsZenith CH750 Cruzer
Wing Span29ft 9in
Wing Area144 sq.ft.
Length23ft 3in
Horizontal Tail Span8ft 0in
Rudder Tip Height9ft 2in
Empty Weight780lbs
Design Gross Weight1440lbs
Gross Weight (LSA)1320lbs
Useful Load (LSA)540lbs
Wing Loading (LSA)9.15psf
Power Loading13.2lbs/bhp
Never Exceed Speed (VNE)145mph
Fuel Capacity30 Gal.
Cabin Width42in
Cabin Width (bubble doors)50in
Load Factor (G) ultimate+6/-3 g
Suitable Power80-160hp
Max Engine Weight300lbs

Performances - Zenith CH 750 Cruzer

Figures based on a Zenith CH 750 Cruzer 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 Roll350ft
Landing Roll350ft
Cruise (75% Sea Level)118mph
Stall Speed39mph
Rate of Climb1200fpm
Range(standard miles)520 miles
Endurance4.5 hours

Light Sport Aircraft Regulations

The STANDARD Zenith CH 750 Cruzer 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.