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PERFORMANCE
AND
SPECIFICATIONS:
CH 750 CRUZER
| SPECIFICATIONS |
STOL
CH 750 |
CH 750 CRUZER |
|
Based on factory prototype:
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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 |
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for a brochure
| PERFORMANCE |
STOL
CH 750 |
CH 750 CRUZER |
|
Based on factory prototype:
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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 |
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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