Cessna 172P - Page 205

PILOT'S OPEN,ATINC}
HANDBOOK
SUPPLEMENT
1
FLOATPLANE
MODEL
172P
sEcTroN
5
PERFORMANCE
INTRODUCTION
The information
presented
in the Introduction,
Use
of Performance
Charts, and Sample
Problem
paragraphs
in
Section
õ of
the
basic
hand-
book
is
applicable
to
tho
floatplane. Using
this
information,
and
the
performance
cha,rts
in
this
supplement, complete
flight
planning may be
accomplished.
DEMONSTR,ATED
OPEN,ATING
TEMPER,ATURE
Satisfactory engine cooling has been demonstrated fo¡
this floatplane
with
an outside air temperature
23oC above
standard. This is
not to
be
considered a,s a,n
operating limitation. Reference should
be made
to
Section 2
for
engine operating
limitations.
AIRSPEED CATIBRATION
NORftlAt STATIC SOURCE
CONDITION:
Power
required
for level flight or maximum
rated RPM dive.
FLAPS UP
KIAS
KCAS
40 50 60
47 54
62
70
71
80 90
100
80 90 99
110
109
120
119
130
129
140
139
150
149
160
159
FLAPS lOO
KIAS
KCAS
40 50 60 70 80
90
46 53 62 72 82 91
100
101
110
111
FLAPS
3OO
KIAS
KCAS
40 50 60 70 80
45 52
62
72 82
85
---
---
87
30 May 1980
Figure 4.
Airspeed
Calibration
2l