|
PERFORMANCE
AND
SPECIFICATIONS
|
SPECIFICATIONS |
STOL CH 750 |
|
WING SPAN |
29 FT. 9 In. |
9.1 m. |
|
HEIGHT (rudder tip) |
8 Ft. 8 In. |
2.6 m. |
|
WING AREA |
144 SQ.FT. |
13.4 m.sq. |
|
WING CHORD |
4 Ft. 10 In. |
1.5 m. |
|
LENGTH |
21 Ft. 10 In. |
6.7 m. |
|
HORIZONTAL TAIL SPAN |
8 Ft. 5 In. |
2.6 m. |
|
HORIZONTAL TAIL AREA |
22.2 Sq. Ft. |
2.0 m.sq. |
|
EMPTY WEIGHT |
775 LBS. |
350 kg. |
|
GROSS WEIGHT |
1,320 LBS. |
600 kg. |
|
USEFUL LOAD |
545 LBS. |
250 kg. |
|
WING LOADING |
9.15 LBS/FT² |
44.8 m² |
|
POWER LOADING |
13.2 LBS/BHP |
6.0 kg/BHP |
|
DESIGN LOAD FACTOR (ultimate) |
+6 G / -3G |
|
CABIN WIDTH (shoulders) |
42 INCHES |
100 cm. |
|
CABIN WIDTH (optional bubble doors) |
50 INCHES |
1.27 m. |
|
FUEL CAPACITY (std., dual wing tanks) |
24
US Gallons
(2 x 12 gal.) |
90
liters
(2 x 45 liters) |
|
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. Please
contact AMD for all the latest information. |
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