Zenith STOL CH 750 Airplane Flight Manual page 8

Zenith STOL CH 750
1.4 DESCRIPTIVE DATA
Kind of Airplane:
Side by side 2 place, bubble doors, single engine, high wing with struts, sheet
aluminum with blind and solid rivets, airplane
The landing gear is of conventional three gear design. Leas spring main gear
with independent hydraulic brakes and a steerable nose wheel.
The airplane is equipped with a 100hp Rotax 912 ULS engine turning a
ground adjustable 3-blade Warp-Drive propeller.
Specifications:
Wing Span ....................................................................................... 9.1 m
Wing Area ..................................................................................... 13.4 m
Wing Chord ..................................................................................... 1.5 m
Horizontal Tail Span ........................................................................ 2.6 m
Horizontal Tail Area ........................................................................ 2.0 m
Maximum Height (Rudder Tip) ......................................................... 2.6 m
Length .............................................................................................. 6.7 m
Wheel Span (track) ......................................................................... 1.8 m
Maximum Take-Off Weight (MTOW): ............................................ 600 kg
Empty Weight. ................................................................................. 360 kg
Useful Load......................................................... ................ 240 kg
Baggage Capacity (maximum) ......................................................... 18 kg
Wing Loading, Gross ............................................................... 26.8 kg/m
Seats ........................................................................................................2
Tire Size
Main Gear ...................................... 8.00 – 6 in, 4 PLY, Max 20 psi
Nose Wheel .................................. 8.00 – 6 in, 4 PLY, Max 20 psi
Issued: 01.02.2020
Airplane Flight Manual
Revision 0, Dat. 01.02.2020
HB-YRC
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