CH 750 CRUZER Sport Aircraft

  

CH 750 Cruzer 
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PERFORMANCE AND SPECIFICATIONS: CH 750 CRUZER
Zenith CH 750 Cruzer
 

SPECIFICATIONS STOL CH 750 CH 750 CRUZER

Based on factory prototype: 

100-hp Continental O-200 130-hp UL350iS
WING SPAN 29 FT. 9 In. 9.1 m. 29 FT. 9 In. 9.1 m.
HEIGHT (rudder tip) 8 Ft. 8 In. 2.6 m. 9 Ft. 2 In. 2.8 m.
WING AREA 144 SQ.FT. 13.4 m.sq. 144 SQ.FT. 13.4 m.sq.
WING CHORD 4 Ft. 10 In. 1.5 m. 4 Ft. 11 In. 1.51 m.
LENGTH 21 Ft. 10 In. 6.7 m. 23 Ft. 3 In. 6.7 m.
HORIZONTAL TAIL SPAN 8 Ft. 5 In. 2.6 m. 8 Ft. 0 In. 2.44 m.
EMPTY WEIGHT 775 LBS. 350 kg. 780 LBS. 354 kg.
DESIGN GROSS WEIGHT 1,440 LBS. 652 kg. 1,440 LBS. 652 kg.
GROSS WEIGHT (LSA Limit) 1,320 LBS. 600 kg. 1,320 LBS. 600 kg.
USEFUL LOAD @ 1,440 gross 665 LBS. 300 kg. 660 LBS. 300 kg.
USEFUL LOAD (LSA Limit) 545 LBS. 250 kg. 540 LBS. 245 kg.
WING LOADING (LSA) 9.15 LBS/FT.SQ 44.8 kg/m.sq. 9.0 LBS/FT.SQ. 43.7 kg/m.sq.
POWER LOADING (LSA) 13.2 LBS/BHP 6.0 kg/BHP 10.15 LBS/BHP 4.6 kg/BHP
DESIGN LOAD FACTOR (ultimate) +6 G / -3 G +6 G / -3 G
NEVER EXCEED SPEED (VNE) 125 MPH 200 km/h 145 MPH 233 km/h
CABIN WIDTH 42 INCHES 100 cm. 42 INCHES 100 cm.
CABIN WIDTH (bubble doors) 50 INCHES 1.27 m. 50 INCHES 1.27 m.
FUEL CAPACITY (std., dual wing tanks) 24 US Gallons
(2 x 12 gal.)
90 liters
(2 x 45 liters)
30 US Gallons
(2 x 15 gal.)
114 liters
(2 x 57 liters)
SUITABLE POWER / Max Engine Weight 80 - 160 hp.  /  350 lbs. (158 kg.) installed

Zenith CH 750 Cruzer

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PERFORMANCE STOL CH 750 CH 750 CRUZER

Based on factory prototype: 

Continental O-200 UL Power UL350iS
TAKE-OFF ROLL 100 Feet 30 m. 350 Feet 107 m.
LANDING ROLL 125 Feet 38 m. 350 Feet 107 m.
CRUISE (75%), Sea Level 100 MPH 162 km/h 118 MPH 190 km/h
STALL, flaps down 35 MPH 56 km/h 39 MPH 63 km/h
RATE OF CLIMB 1,000 fpm 5.1 m/s 1,200 fpm 6 m/s
SERVICE CEILING 14,000+ feet 4,200+ m. 14,000+ feet 4,200+ m.
RANGE (standard, no reserve) 440 miles 710 km. 520 miles 830 km.
ENDURANCE (standard, no reserve) 4.4 Hours 4.4 Hours 4.5 Hours 4.5 Hours

Zenith CH 750 Cruzer

Specification and performance figures quoted with the engine indicated above. Standard atmosphere, sea level, no wind.
Performance and specification figures based on prototype flight test results. All technical data, specification and performance figures subject to change without notice. 
Suitable powerplant range: 100 - 160 HP engines.
Different engines and installed options will affect performance and specification figures. Heavier engines will limit useful load (by increasing the empty weight).

Engine Limitations: 100 - 160 hp, up to 350 lbs. installed. Alternative engines will affect performance, specifications and flight characteristics of the aircraft. Also, the weight and balance of the aircraft may be adversely affected by alternative engines, and the original fuel system may not be adequate or suitable for some engines. Most alternative engines will require a custom engine mount and engine cowl. Zenith Aircraft Company does not manufacture or directly support engines.

While the CH 750 was developed to meet the definition of a light-sport aircraft, as defined in the FAA's Sport Pilot category, Zenith Aircraft Company cannot guarantee that the aircraft, as constructed by the builder, will meet the definition. Due to the gross weight 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 limit the useful load of the aircraft, and may disqualify the aircraft from meeting the defined category limits of the Sport Pilot category.


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 Zenith Aircraft Company

Zenith Aircraft Company
1881 Airport Road, Mexico Memorial Airport
Mexico, Missouri, 65265  USA.
Tel: 573-581-9000 (Mon - Fri, 8-5 Central),
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Zenith Aircraft Company: 2015-02-12