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CH 801
The STOL CH 801 is a four-seat sport utility kit
aircraft based on the successful two-seat STOL CH 701 design
developed by aeronautical engineer Chris Heintz in the mid eighties.
Since its introduction in 1986, more than 400 short take-off and
landing STOL CH 701 aircraft have been successfully built and flown
around the world, many being used for light utility purposes.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
150 - 240
hp
x
24
ft 6 In.
10
ft 0 In.
31
ft . 4 In.
167
sq.ft .
2
1,150
lbs
1,050
lbs
2,200
lbs
30
gal. (2 x 15)
x |
performance
takeoff
distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
x
120
mph
x
x
x |
limiting and recommended speeds
design
manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
150
mph
x
x |
All specifications are based on
manufacturer's calculations |
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