Cessna skylance tc T182T, Information Manual

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SECTION 5 CESSNA
PERFORMANCE MODEL T182T NAV III
GFC 700 AFCS
U.S.
AIRSPEED CALIBRATION
NORMAL STATIC SOURCE
CONDITIONS:
Power required for level flight or maximum power descent.
Figure 5-1 (Sheet 1 of 2)
Flaps
UP
KIAS
55 60 70 80 90 100 110 120 130 140 150 160
KCAS
60 64 73 82 91 100 110 119 128 137 146 156
Flaps
20°
KIAS
45 50 60 70 80 90 100 110 120 --- --- ---
KCAS
51 55 63 72 81 90 100 110 120 --- --- ---
Flaps
FULL
KIAS
40 50 60 70 80 90 95 --- --- --- --- ---
KCAS
48 55 63 72 82 92 97 --- --- --- --- ---
T182TPHBUS-00
5-10