|
|
|
PERFORMANCE AND SPECIFICATIONS
| SPECIFICATIONS |
STOL
CH 701 |
| WING SPAN |
27 FEET |
8.2 m. |
| WING AREA |
122 SQ.FT. |
11.4 m.sq. |
| LENGTH |
20 Ft. 11 In. |
6.38 m. |
| HEIGHT (rudder tip) |
8 Ft. 7 In. |
2.6 m. |
| EMPTY WEIGHT |
580 LBS. |
263 kg. |
| GROSS WEIGHT |
1,100 LBS. |
500 kg. |
| USEFUL LOAD |
520 LBS. |
236 kg. |
| WING LOADING |
9.0 LBS/FT² |
43.8 m² |
| POWER LOADING |
13.75 LBS/BHP |
6.25 kg/BHP |
| DESIGN LOAD FACTOR (ultimate) |
+6 G / -3G |
| CABIN WIDTH (shoulders) |
40 INCHES |
100 cm. |
| CABIN WIDTH (optional bubble
doors) |
44 INCHES |
110 cm. |
| FUEL CAPACITY (std., dual wing tanks) |
20 US Gallons
(2 x 10 gal.) |
76 liters
(2 x 38 liters) |
Click here
for a full-size view | Click here for
additional detailed views of the STOL CH 701
| STOL
CH 701 PERFORMANCE |
ROTAX
912 (80 HP) |
ROTAX
912S (100 HP) |
| |
SINGLE |
DUAL |
SINGLE |
DUAL |
| TOP SPEED (MPH) |
85 |
85 |
95 |
95 |
| CRUISE, Sea Level (MPH) |
80 |
80 |
85 |
85 |
| 75% CRUISE @ 8,000 ft. (TAS*) |
92 |
92 |
98 |
98 |
| VNE (MPH) |
110 |
110 |
110 |
110 |
| STALL (MPH) |
28 |
30 |
28 |
30 |
| RATE OF CLIMB (FPM) |
1,100 |
1,000 |
1,200 |
1,100 |
| TAKE-OFF ROLL (FEET) |
60 |
115 |
50 |
90 |
| LANDING ROLL (FEET) |
80 |
140 |
80 |
140 |
| SERVICE CEILING (FEET) |
13,000+ |
12,000+ |
15,000+ |
12,000+ |
| STD. RANGE (MILES) |
372 |
372 |
350 |
350 |
| ENDURANCE |
4.6 Hrs. |
4.6 Hrs. |
4.1 Hrs. |
4.1 Hrs. |
Range and endurance figures are quoted with no fuel reserve. Figures are based on factory prototype results,
and are given at standard atmosphere, sea level, no
wind, unless otherwise indicated. All technical data,
specification and performance figures subject to change without notice.
* TAS is indicated airspeed corrected for temperature and altitude.
The corrections are approximate.
Engine Limitations: 50 - 100 hp, up to 185
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.
- Click here to
view flight demonstrations of the STOL CH 701's outstanding short
take-off and landing (STOL) performance.
 |
STOL CH 701
True short take-off and landing capability for
the serious sport pilot.Flying the STOL CH
701:
"You're already where you want to
be!" |
|
|
