Table of Contents
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CESSNA
MODEL
182S
sEcTroN
5
PERFORMANCE
5-8
5-9
5-10
5-11
SECTION
5
PERFORMANCE
TABLE
OF CONTENTS
lntroduction
Use of
PeÍormance
Charts
Sample Problem
Takeoff
Cruise
Fuel Required
Landing
Demonstrated Operating Temperature
Figure 5-1, Airspeed Calibration - Normal Static
Source
.
.
.
.
.
Page
Airspeed Calibration
-
Allernate Static Source
Figure 5-2, Altimeter Correction
Figure 5-3, Temperature Conversion
Chafi
5-12
Figure 5-4, Stall Speeds
Figure 5-5, Crosswind Components
Figure 5-6, Short
Field
Takeoff Distance
-
3100
Lbs
Short Field Takeoff Distance
-
2700 Lbs
Short Field Takeoff Distance
-
2300 Lbs
Figure 5-7, Maximum Rate Of Climb
Figure 5-8, Time, Fuel, And Distance
To
Climb
Figure 5-9, Cruise
Performance
5-21
Figure
5-10,
Range
Profile
5-31
Figure
5-1
1,
Endurance
Profile
Figure 5-12, Short Field Landing Distance
5-3
5-3
5-3
5-4
5-5
5-6
5-8
5-13
5-14
5-15
5-16
5-17
5-18
5-19
5-33
5-35
Dec
1/97
5-11(5-2
blank)
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