Cessna 172P - Performance

CESSNA
MODEL
172P
SECTION
5
PERFOF,MANCE
Page
SECTION
5
PERFORMANCE
TABLE
OF CONTENTS
Introduction
Use of Perforrnance
Charts
Sample Problem
Takeoff
Cruise
FueI
Required
.
Landing
Demonstrated
Operating lemperature
Figure
õ-1, Airspeed
Calibration
-
Normal Static Source
Airspeed
Calibration
-
Alternate
Static
Source
Figure
5-2, Tomperature
Conversion Chart
Figure
5-3,
Stall
Speeds
Figure
5-4,
Takooff
Distance -
2400 Lbs
Takeoff
Distance
- 22OO Lbs and
2000 Lbs
Figure 5-õ,
Maximum
Rate
Of Climb
Figure
5-6,
Time,
Fuel,
And Distance
To Ctimb
Figure
õ-7,
Cruise Performance
.
Figure
5-8,
Range Profile
-
40
Gallons Fuel
Range
Profile -
õ0
GaIIons Fuel
Range Profile
-
Q2
Gallons
Fuel
Figure
5-9,
Enduranoo
Profile -
40
Gallons
FueI
Endurance
Profile -
ã0
Gallons Fuet
Endurance
Profile
-
62 GaIIons
FueI
Figure
5-10,
Landing
Distance
. ã-3
. 5-3
. 5-3
. ó-4
. 5-5
. õ-õ
.
6-7
. 6-7
, ã-8
. ã-9
5-10
5-1 1
6-12
5-13
5-14
5-1õ
5-16
6-L7
õ-18
5-19
5-20
6-21
5-22
ã-23
30
May
1980
5-L/(6-2
blank)