Cessna R182 - Page 39

CESSNA
MODEL
R,182
SECTION
3
EMER,GENCY
PROCEDI'RES
in
the
line
to
the
gage
is
not
necessarily
cause
for
an immediato
prec&u:
ti-onary
landing
beceuse
an
orifice
in
thii line
will
pr"o"ht
r
"rrddenloss
of
9il
fr_om
tJrg
qngine
s'mp.
frowever,.a
randirg
at tue
nearest
airport
would
'
be
advisable
to
inspect
the.source
of
troublel
rf
a
total
loss
of
oil
pressure
is
accompanied,by-
a rise
in
oil
tempera_
ture.,
there
is
good
reaso'-to
suspect
an
engine
failuie
is
imminent.
Reduce
engine
powsr
immsdia,tely-andselect'a
srtitabli
fiirced
landing
ti"ra.
u""
only
tJre
minimum power
required
to
reach
tbe
desired
touchdown
spot.
LANDING
GEAR
MALFUNCTION
PROCEDURES
rn
the
event
of
possible
landing gear
retraction
or extension
marfunc_
tions,
there
are
several
generat-ciecks
that
snouta'te-maae;;il;;
initiating
the
steps
outtined
in
the following
p;;;F";h".
R
ETRACTION
MALFUNCTIONS
EXTENSION
MALFUNCTIONS
Normal
landing
gear
extension
time
is
appro:iimdteryb
seconds.
If the
landing_gedr
will
not
extend,norma[y;:p"^;io"*
n"
Jlierar
checks
of
circuit
breakers
and
md,ster
switch
a-nd repeat
the
n"ormar.extension
3-17