Stall Speeds - Cessna 152 1979 Pilot Operating Handbook

CESSNA
MODEL 152
Conditions:
Power Off
Notes:
Altitude loss during a stall recovery may be as much as 160 feet
KIAS values are approximate and are base on airspeed calibration data with power off.
WEIGHT
LBS
DEFLECTION
1670
WEIGHT
LBS
DEFLECTION
1670
1 July 1978

STALL SPEEDS

MOST REARWARD CENETER OF GRAVITY
FLAP
0º
KIAS
UP 36
36
10°
31
30°
MOST FORWARD CENETER OF GRAVITY
FLAP
0º
KIAS
UP 40
40
10°
35
30°
Figure 5-3 Stall Speeds
ANGLE OF BANK
30º
KCAS KIAS KCAS
46 39 49
43 39 46
41 33 44
ANGLE OF BANK
30º
KCAS KIAS KCAS
48 43 52
46 43 49
43 38 46
PERFORMANCE
45º 60º
KIAS KCAS KIAS
43 55 51
43 51 51
37 49 44
45º 60º
KIAS KCAS KIAS
48 57 57
48 55 57
42 51 49
SECTION 5
KCAS
65
61
58
KCAS
68
65
61
5-10