Climb performance chart:
rate of climb (FPM, full throttle):
sea level (ISA)
850
fpm
at IAS
4 2
kt
3000 ft density alt.
720
fpm
at IAS
39
kt
6000 ft density alt.
415
fpm
at IAS
3 5
kt
9000 ft density alt.
200
fpm
at IAS
3 3
kt
Service ceiling
with standard original carburetor jet setting: 14 000 feet density altitude at gross weight.
Best rate of climb and best angle of climb - see section 4
Fuel consumption:
(Rotax 912)
take-off power . . . . . . . . . . . . . . . . . . . . . . . . 22 litres/hour
75 % . . . . . . . . . . . . . . . . . . . . . . . . . .16.2 litres/hour
Range and endurance:
engine settings
cruise speed (kt)
max. continuous
80
75 %
70
range (NM)
150
180
Above values are valid for aircraft in good condition and are without reserve. Ensure that you
are not exceeding MTOW limit 450 kg while loading your aircraft.
Before attempting cross-country flights, proper knowledge of the fuel consumption and
capacity is required.
Best angle of glide
- (gross weight) 40 kt, with flaps up
Содержание STOL CH 701
Страница 4: ...Three view drawing 30 7 780 mm I 87 5 2220mm I 27FI 18220mm...
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