CESSNA
MODEL TR182
SECTION 5
PERFORMANCE
SECTION 5
PERFORMANCE
TABLE OF CONTENTS
Page
Introduction . . . . . . .
Use Of Performance Charts
Sample Problem .
Takeoff
Cruise ....
Fuel Required
Landing ...
Demonstrated Operating Temperature .
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 - 3100Lbs .
Takeoff Distance - 2800Lbs And 2500Lbs
Figure
5-5,
Rate OfClimb - Maximum . . . . .
Figure
5-6,
Time, Fuel, And Distance To Clim.b-
Maximum Rate
Of
Climb ....
Time, Fuel, And Distance To Climb -
N
orrnal Climb . . . . . .
Figure 5-7, Cruise Performance - 2000Feet
Cruise Performance - 4000Feet
Cruise Performance - 6000Feet
Cruise Performance - 8000Feet
Cruise Perform.ance - 10,000Feet
Cruise Performance - 12,000Feet
Cruise Performance - 14,000Feet
Cruise Performance - 16,000Feet
Cruise Performance - 18,000Feet
Cruise Performance - 20,000Feet
Figure
5-8,
Range Profile . .
Figure
5-9,
Endurance Profile
Figure
5-10,
Landing Distance
5-3
5-3
5-3
5-4
5-5
5-5
5e7
5-7
5-8
5-9
5-10
5-11
5-12
5-13
5-14
5-15
5-16
5-17
5-18
5-19
5-20
5-21
5-22
5-23
5-24
5-25
5-26
5-27
5-28
5-29
1 October 1978
5-1/(5-2
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