C42 SERIES Pilot Operating Handbook
The deviation curve for the airspeed indicator can be interpolated from the
following table
IAS
33 38 43 49 54 60 65 70 76 81 86 92 97 103 108
kn
EAS
35 41 45 49 54 59 63 68 72 77 151 86 91 96 100
kn
IAS
60 70 80 90 100 110 120 130 140 150 160 170 180 190 200
km/h
EAS
65 74 83 91 100 109 117 125 134 142 151 160 168 177 185
km/h
1.6
Engine rpm limitations
Maximum engine rpm ...................................... n = 5800 1/min, 5 min. max
Maximum continuous rpm .................................................... n = 5500 1/min
1.7
Rpm indicator markings
Yellow arc ................................................................. n = 5500 - 5800 1/min
Red line ................................................................................ n = 5800 1/min
1.8
Flap settings
Position I: ......................................................................................... cruising
Position II: ......................................................................... take-off / landing
Position III: ....................................................................................... landing
POH Issue 4 Rev. 5
Page 15 of 91
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