CESSNA
MODEL 172S NAV
III
PERFORMANCE
TABLE OF CONTENTS
SECTION 5
PERFORMANCE
Page
Introduction
......................................
5-3
Use of Performance Charts
..........................
5-3
Sample Problem
..................................
5-3
Takeoff
.......................................
5-4
Cruise
.......................................
5-5
Fuel Required
..................................
5-6
Landing
......................................
5-8
Demonstrated Operating Temperature
..................
5-8
Airspeed Calibration - Normal Static Source
..............
5-9
Airspeed
Calibration - Alternate Static Source . . .
..
. . . .
..
5-10
Temperature Conversion Chart
......................
5-11
Stall Speeds at 2550 Pounds
........................
5-12
Crosswind Components
............................
5-13
Short Field Takeoff Distance at 2550 Pounds . . . . . . . . . . . 5-14
Short Field Takeoff Distance at 2400 Pounds . . . . . . . . . . . 5-15
Short Field Takeoff Distance at 2200 Pounds . . . . . . . . . . . 5-16
Maximum Rate
Of Climb at 2550 Pounds . . . . . . . . . . . . . . 5-17
Time, Fuel, And Distance To Climb at 2550 Pounds
.......
5-18
Cruise Performance
...............................
5-19
Range Profile
...................................
5-21
Endurance Profile
................................
5-22
Short Field Landing Distance at 2550 Pounds
..
. . . . . 5-23/5-24
172SPHAUS-00
U.S.
5-1/5-2