Cessna SkyHawk SP 172S NAV III 2005 Pilot Operating Handbook page 169

CESSNA
MODEL 172S NAV III
SECTION 5
PERFORMANCE
AIRSPEED CALIBRATION
NORMAL STATIC SOURCE
CONDITION:
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 11 0 - - - - - - - - - - - -
KCAS 51 57 63 71 80 89 99 109 - - - - - - - - - - - -
FLAPS
FULL
KIAS
40 50 60 70 80 85
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KCAS 50 56 63 72 81 86
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Figure 5-1. Airspeed Calibration (Sheet 1 of 2)
172SPHAUS-00
u.S. 5-9