Operating Limitations; Airspeeds; Weights - iKarus C 42 Series Pilot Operating Handbook

C42 SERIES Pilot Operating Handbook
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Operating limitations

1.1 Airspeeds

Never-exceed speed
C42 .......................................................................... V
C42B / C42E / C42C ............................................. V
C42CS ................................................................... V
Speed in turbulent air
C42 / C42B / C42E / C42C ....................................... V
C42CS .....................................................................V
Maximum manoeuver speed
C42 / C42B / C42E / C42C / C42CS ........................ V
Speed with landing flap set Vfe
until 2009 ................................................................ V
since 2009 ................................................................ V
Stall speed
Flap position I: ....................................................... V
Flap position II: ..................................................... V
Flap position III: .................................................... V
If V speed is exceeded, only little rudder movement are allowed.
A

1.2 Weights

Maximum take-off weight: ............................................... 992 lbs / 450,0 kg
Maximum take-off weight with
installed rescue system ................................................ 1041 lbs / 472,5 kg
Empty weight (see last Weight and Balance plan) .......................... lbs / kg
Minimum payload: (see last Weight and Balance plan) .......144 lbs / 65 kg
POH Issue 4 Rev. 5
= 97 kn / 180 km/h
NE
= 116 kn / 216 km/h
NE
= 121 kn / 225 km/h
NE
= 97 kn / 180 km/h
B
= 101 kn / 187 km/h
B
= 80 kn / 148 km/h
A
= 57 kn / 105 km/h
FE
= 63 kn / 117 km/h
FE
= 40 kn / 75 km/h
S
= 38 kn / 70 km/h
S1
= 35 kn / 65 km/h
S0
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