PERFORMANCE
AND
SPECIFICATIONS
- STOL CH750 S-LSA
| SPECIFICATIONS |
STOL CH 750 |
| WING
SPAN |
29 FT. 9 In. |
| HEIGHT
(rudder tip) |
8
Ft. 8 In. |
| WING
AREA |
144 SQ.FT. |
| WING
CHORD |
4
Ft. 10 In. |
| LENGTH |
21
Ft. 10 In. |
| HORIZONTAL
TAIL SPAN |
8
Ft. 5 In. |
| HORIZONTAL
TAIL AREA |
22.2
Sq. Ft. |
| EMPTY
WEIGHT |
820 LBS. |
| GROSS
WEIGHT |
1,320
LBS. |
| USEFUL
LOAD |
500 LBS. |
| WING
LOADING |
9.15
LBS/FT² |
| POWER
LOADING |
13.2
LBS/BHP |
| DESIGN
LOAD FACTOR (ultimate) |
+6
G / -3G |
| CABIN
WIDTH (shoulders) |
42
INCHES |
| CABIN WIDTH (optional bubble
doors) |
50 INCHES |
| FUEL
CAPACITY (std., dual wing tanks) |
30 US
Gallons
(2 x 15 gal.) |
| STOL
CH 750 PERFORMANCE |
Continental
O-200 - 100 hp |
| |
@ gross weight |
| TAKE-OFF
ROLL |
100
Feet |
30
m. |
| LANDING
ROLL |
125
Feet |
38
m. |
|
MAX. CRUISE, Sea Level |
100
MPH |
162
km/h |
|
VNE |
125
MPH |
200
km/h |
| STALL,
flaps down |
35
MPH |
56
km/h |
| RATE
OF CLIMB |
1,000
fpm |
5.1
m/s |
| SERVICE
CEILING |
14,000+
feet |
4,200+
m. |
| STD.
RANGE |
400
miles |
710
km. |
| ENDURANCE |
5
Hours |
5
Hours |
 |
STOL
CH 750
True short take-off
and landing
capability for the serious sport pilot. |
Specification and
performance figures quoted with the
Continental O-200-A engine (100 HP).
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.
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