Cessna 152 - Page 72

SECTION
5
PERFORMANCE
CONDITIONS:
Power
Off
NOTES:
STALL SPEEDS
1.
Altitude
loss
during a stall recovery may
be
as
much
as
160 feet.
CESSNA
MODEL
152
2.
KIAS
values
are
approximate
and
are
based
on airspeed calibration data with power
off.
MOST
REARWARD
CENTER OF
GRAVITY
ANGLE OF
BANK
WEIGHT
FLAP
oo
300
45°
60°
LBS
DEFLECTION
KIAS KCAS KIAS KCAS KIAS KCAS
KIAS KCAS
UP
36
46
39
49
43
55
51
65
1670
10°
36
43 39
46
43
51
51
61
300
31
41
33
44
37
49
44
58
MOST
FORWARD
CENTER OF
GRAVITY
ANGLE
OF
BANK
WEIGHT
FLAP
oo
30°
45°
500
LBS
DEFLECTION
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
UP
40
48
43
52
48
57
57
68
1670
10°
40
46
43 49
48
55
57
65
300
35
43
38
46
42
51
49
61
Figure
5-3.
Stall
Speeds
5-10
1
July
1978