SECTION 5
CESSNA
PERFORMANCE
MODEL 172S NAV III
KAP 140 AUTOPILOT
U.S.
AIRSPEED CALIBRATION
NORMAL STATIC SOURCE
CONDITIONS:
Power required for level flight or maximum power descent.
Flaps
UP
KIAS
50 60 70 80 90 100 110 120 130 140 150 160
KCAS
56 62 70 78 87 97 107 117 127 137 147 157
Flaps
10°
KIAS
40 50 60 70 80 90 100 110 --- --- --- ---
KCAS
51 57 63 71 80 89 99 109 --- --- --- ---
Flaps
FULL
KIAS
40 50 60 70 80 85 --- --- --- --- --- ---
KCAS
50 56 63 72 81 86 --- --- --- --- --- ---
Figure 5-1 (Sheet 1 of 2)*
172SPHAUS-05
5-10
For
Training
Purposes
Only
Summary of Contents for Cessna 172S NAV III Skyhawk SP
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