CESSNA
MODEL 172N
SECTION 5
PERFORMANCE
STALL SPEEDS
CONDITIONS:
Power Off
NOTES:
1.
Maximum altitude loss during a stall recovery may be as much as 180 feet.
2.
KlAS values are approximate.
MOST REARWARD CENTER
OF
GRAVITY
MOST FORWARD CENTER
OF
GRAVITY
-
-
- . -
F i g u r e 5-3. Stall Speeds
1
July 1979
WEIGHT
LBS
2300
FLAP
DEFLECTION
UP
1 0°
40°
ANGLE OF BANK
o0
KlAS
39
38
31
KCAS
50
47
44
30°
KlAS
42
40
33
KCAS
54
51
47
45O
KlAS
47
45
37
60'
KCAS
59
56
52
KlAS
56
54
45
KCAS
71
66
62