Cessna 152 1979 - Stall Speeds

CESSNA SECTION 5
MODEL 152 PERFORMANCE
1 July 1978 5-10
STALL SPEEDS
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.
MOST REARWARD CENETER OF GRAVITY
ANGLE OF BANK
0º 30º 45º 60º
WEIGHT
LBS FLAP
DEFLECTION
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 36 46 39 49 43 55 51 65
10°
36 43 39 46 43 51 51 61
1670
30°
31 41 33 44 37 49 44 58
MOST FORWARD CENETER OF GRAVITY
ANGLE OF BANK
0º 30º 45º 60º
WEIGHT
LBS FLAP
DEFLECTION
KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS
UP 40 48 43 52 48 57 57 68
10°
40 46 43 49 48 55 57 65
1670
30°
35 43 38 46 42 51 49 61
Figure 5-3 Stall Speeds