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CH 701
First introduced in 1986, the STOL CH 701 aircraft
was developed as an "off-airport" short take-off and landing kit
aircraft to fulfil the demanding requirements of both sport pilots
and first-time builders.
With the STOL CH 701, designer Chris Heintz combined the features
and advantages of a "real" airplane with the short-field
capabilities of an "ultralight" aircraft. The aircraft features
fixed leading-edge slats for high lift, full-span flaperons (both
ailerons and flaps), an all-flying rudder, and durable all-metal
construction.
|
SPECIFICATIONS |
STOL CH 701 |
|
wing span |
27 ft |
|
wing area |
122 sq.ft. |
|
length |
20
ft. 11 In. |
|
height |
8
ft. 7 In. |
|
empty weight* |
580
lbs |
|
gross weight |
1,100
lbs |
|
useful load |
520
lbs |
|
wing loading |
9.0 LBS/ft˛ |
|
power loading |
13.75
lbs/bhp |
|
design load
factor |
+6 G / -3G |
|
cabin width
(shoulders) |
41
ins |
|
fuel capacity (std) |
20 US Gallons
(2 x 10 gal.) |
|
PERFORMANCE |
ROTAX 582 (65 HP) |
ROTAX 912 (80 HP) |
|
|
single |
dual |
single |
dual |
|
top speed mph |
85 |
85 |
95 |
95 |
|
Ccruise
mph |
75 |
75 |
80 |
80 |
|
Vne mph |
110 |
110 |
110 |
110 |
|
stall mph |
28 |
30 |
28 |
30 |
|
rate of climb
f/min |
1400 |
1200 |
1600 |
1400 |
|
take off roll ft |
60 |
115 |
45 |
90 |
|
landing roll ft |
80 |
140 |
80 |
140 |
|
service ceiling
ft |
15000+ |
12000+ |
15000+ |
12000+ |
|
std range miles |
300 |
300 |
400 |
400 |
|
endurance |
4 Hrs. |
4 Hrs. |
5 Hrs. |
5 Hrs. |
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