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