Cessna R182 - Page 67

CESSNA
MODEL
R,182
SECTION
5
PERFOR,MANCE
SECTION
5
PERFORMANCE
TABLE
OF CONTENTS
Introductiol
Use of Performance
Charts
Sample Problem
Takeoff
Cruise
Fuel Required
Landing
Figure
5-1, Airspeed Calibration
-
Normal
Static Source
Airspeed Calibration
-
Alternate Static Source
Figure
5-2, Temperature Conversion Chart
Figure 5-3,
Stall
Speeds
Figure 5-4, Takeoff Distance
-
3100
Lbs
Cruise
Performance
-
4000 Feet
Cruise
Perfomance
-
6000 Feet
Cruise
Perfomance
-
8000
Feet
Cruise
Perforrnance
-
10d)0 Feet
Cruise
Perfornance
-
12,U)0
Feet
Figure
5-8, Range
Frofile
-
56
Gallons
Fuel
Range
Profile
-
75
Gallons
Fuel
Figure 5-9, Endurance Profile
-
56 Gallons
Fuel
Endurance
Profile
-
75 Gallons
Fuel
Takeoff
Distance
-
2800
Lbs And 2500 Lbs 5-13
Figure
5-5, Rate Of Ctimb
-
Maximum
5-t4
Figure
5-6, Time,
Fuel,
And Distance
To
Climb
-
Maximum Rate
Of Climb
5-15
Time,
Fuel,
And Distance
To
Climb
-
Normal Climb
5-16
Figure 5-7,
Cruise
Performance
-
2000
Feet
5-t7
Page
5-3
5-3
5-3
5-4
D-O
a-D
5-7
5-8
5-9
5-10
5-11
5-12
5-18
5-19
5-20
5-2L
5-22
5-23
5-24
5-25
5-26
5-27
Figure 5-10, Landing Distance
5-Ll(5-Z
blank)