Cessna 150G - Airspeed Correction Table; Stalling Speeds

Figure 5-1.
AIRSPEED CORRECTION TABLE
(Flaps Up)
IAS
40
50
60
70
80
90
100
110 120
130 140
CAS
51
57
65
73
82 91
100 109
118
127
136
(Flaps Down)
IAS
CAS
49
40
50
60
70
80 90 100
55
63
72
81
89
98
= Power Of f =
STALLING SPEEDS —
ANGLE OF BANK
Gross Weight
1600 lbs.
0°
20°
40°
60°
CONDITION
Flaps
UP
55 57
63
78
Flaps
20°
49
57
56
70
48
49 54
67
Flaps
40°
Figure 5-2.
5-2