SECTION 3
CESSNA
OPERATING LIMITATIONS
MODEL 162
GARMIN G300
U.S.
AIRSPEED LIMITATIONS
Airspeed limitations and their operational significance are shown in
Figure 3-1.
AIRSPEED LIMITATIONS
SYMBOL
SPEED
KCAS
KIAS
REMARKS
V
S
Stall Speed - Clean
44
41
Stall speed flap up.
V
SO
Stall Speed - Landing
Configuration
40
37
Stall speed flaps full
V
FE
Maximum Flap
Extended Speed:
FLAPS 10°
FLAPS 25°
FLAPS FULL
98
84
71
100
85
70
Do not exceed this speed
with flaps down.
V
O
Maximum Operating
Maneuvering Speed
1320 Pounds
1200 Pounds
1100 Pounds
88
84
81
89
85
80
Maximum speed at which
the airplane may be
stalled without exceeding
structural limitations.
V
A
Design Maneuvering
Speed:
100
102
Do not make full or abrupt
control movements above
this speed.
Does not provide
protection from possible
overstressing the airplane.
V
NE
Never Exceed Speed
143
148
Do not exceed this speed
in any operation.
V
NO
Maximum Structural
Cruising Speed
120
124
Do not exceed this speed
except in smooth air, and
then only with caution.
Figure 3-1
162PHUS-02
3-4
Summary of Contents for 162 SKYLANE
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