CESSNA
MODEL 172N
SECTION 5
PERFORMANCE
SECTION 5
PERFORMANCE
TABLE OF CONTENTS
Introduction . . . . . . .
Use of Performance Charts
Sample Problem .
Takeoff
Cruise . . . .
Fuel Required
Landing . . .
Demonstrated Operating Temperature
Figure �-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 - 2300 Lbs
. . . . . .
Takeoff Distance - 2100 Lbs and 1900 Lbs
Figure 5-5, Maximum Rate Of Climb
. . . .
Figure 5-6, Time, Fuel, And Distance To Climb
Figure 5-7, Cruise Performance . . . . . . .
Figure 5-8, Range Profile - 40 Gallons Fuel
Range Profile - 50 Gallons Fuel
Figure 5-9, Endurance Profile - 40 Gallons Fuel
Endurance Profile - 50 Gallons Fuel
Figure 5-10, Landing Distance
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1 July 1979
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