G3-8 MA FM 1205 - R06
5
Performance
Performance 5 - 5
5.3
Rate of Climb
Propeller
Woodcomp
or Tonini
Sensenich Neuform
best angle of climb
airspeed V
X
kIAS
mph IAS
51
59
51
59
51
59
best rate of climb
airspeed V
Y
kIAS
mph IAS
60
69
60
69
60
69
best rate of climb
at MSL
fpm
600
840
840
NOTE
Climb is flown with flaps retracted, see section 4
NOTE
Expect a performance loss of about 5% when flying
without wheel fairings.
NOTE
Expect a performance loss of about 10% when flying
without doors
5.4
Cruise Speed, RPM, Fuel Consumption, Range
Rotax 912 UL-S, 100 hp engine, Woodcomp or Tonini Fixed Pitch Prop
engine speed
fuel flow
true airspeed
endurance
range
[ rpm ]
[ gph ]
[ kTAS ]
[ mph true ]
[ h ]
[ nm ]
5.400
6,7
98
113
3,1
304
5.200
6,0
95
109
3,5
333
5.000
5,4
91
105
3,9
355
4.800
4,9
87
100
4,3
374
4.600
4,4
83
95
4,8
398
4.400
3,9
79
91
5,4
427
4.200
3,5
75
86
6,0
450
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