Cessna 172P - Page 197

PII,OT'S OPERATING
HANDBOOK
SUPPLEMENT
* PROPEttER WINDIAITIING
*
ZERO WIND
8000
6000
4000
2000
2
{< SPEED
ó5
KIAS
*(
ttAPs
uP
18 20
I
F'LOAîPLANE
MODEL
172P
AIIIPL¡FIED
PROCEDUR
ES
MAXIMUM GLIDE
After
an engine
failure in flight, the
best
glide
speed
as shown
in
figure
3 sbould be
established
as
quickly
as
possible.
In the
likely event
the
propeller
should
stop, maintain the speed shown.
0.000
t--
l!
I
z
É.
É.
u.l
F
t¡J
o
ó
F
T
(9
t¡J
Í
0
0
46810121416
GROUND
DISTANCE -
NAUTICAL
MILES
Figure
3. Maximum
Glide
..,.t
,p
-
I
t
I
'tt
-,
-/
d_
J
,-
..,#
fl
d
i:fr
30
May
1980
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