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Cessna T182 Series User Manual

Cessna T182 Series
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MODEL
182
&
T182
SERIES
SERVICE
MANUAL
16-102.
EMERGENCY LOCATOR
TRANSMITTER.
16-105.
CHECKOUT
INTERVAL.
THRU
18265360.
100
HOURS
OR
THREE
MONTHS,
WHICHEVER
16-103.
DESCRIPTION.
The
ELT
is
a
Self-contained,
COMES
FIRST.
solid
state
unit,
having
its
own
power
supply,
with
an
a.
Turn
aircraft
master
switch
ON.
externally
mounted
antenna.
The
C589510-0209
trans-
b.
Turn
aircraft
transceiver
ON
and
set
frequency
mitter
is
designed
to
transmit
simultaneously
on
dual
on
receiver
to
121.
5
MHZ.
emergency
frequencies
of
121.
5
and
243.0
Megahertz.
c.
Remove
the
ELT's
antenna
cable
from
the
ELT
The
589510-0211
transmitter
thru
18265175
and
the
unit.
C589510-0212 beginning
with
18265176
used
for
Canad-
d.
Place
the
ELT's
function
selector
switch
in
the
ian
registry,
operates
on
121.
5
only.
The unit
is
mount-
ON
position
for
1
second
(3
sweeps
of
the
warble
ed
in
the
tailcone,
aft
of
the
baggage
curtain
on
the
tone).
Immediatly
replace
the ELT
function
sel-
right
hand
side.
The
transmitters
are
designed to
ector
switch
in
the
ARM
position
after
testing
ELT.
provide
a
broadcast
tone
that
is
audio
modulated
in
a
e.
Test
should
be
conducted
only
within
the
time
swept
manner
over
the
range
of
1600
to
300
Hz
in
a
period
made
up
of
the
first
five
minutes
after
any
distinct,
easily
recognizable
distress
signal for
re-
hour.
ception
by
search
and
rescue
personnel
and
others
monitoring
the
emergency
frequencies.
Power
is
supplied
to
the
transmitter
by
a
battery-pack
which
has
the
service
life
of
the
batteries
placarded
on
the
Tests
with
the
antenna
connected should
be
batteries
and
also
on
the
outside
end
of
the
transmit-
approved
and
confirmed
by
the
nearest
con-
ter.
ELT's
are
equipped with
a
battery-pack
contain-
trol
tower.
The
F.A.A./D.
O.T.
allows
ing
four
lithium
"D"
size
batteries
which
are
stacked
free
space
transmission
tests
from
the
air-
in
two's
(See
figure
16-15).
The
ELT
exhibits
line
of
craft
anytime
within five
minutes
after
each
sight
transmission
characteristics
which
correspond
hour. The
test
time
allowed
is
generally
approximately
to
100
miles at
a
search
altitude
of
three
sweeps
of
the
warble
tone,
or
approx-
10,
000
feet.
When
battery
inspection
and
replacement
imately
one
second.
The
control
tower
should
schedules
are
adhered
to,
the
transmitter
will
broad-
be
notified
that
a
test
is
about
to
be
performed.
cast
an
emergency
signal
at
rated
power
(75
MW-
minimum),
for
a
continuous
period
of
time
as listed
NOTE
in the
following
table.
Without
its
antenna
connected,
the
ELT
will
TRANSMITTER
LIFE
produce
sufficient
signal
to
reach
your
re-
TO
75
MILLIWATTS
OUTPUT
ceiver,
yet
it
will
not
disturb
other
commu-
Temperature
Lithium
NOTE
Battery
Pack
+130°F
115
hrs
After
accumulated
test
or
operation
time
+
70°F
115
hrs
equals
1
hour,
battery-pack
replacement
-
4°F
95
hrs
is
required.
-
40°F
23
hrs
f.
Check
calendar
date
for
replacement
of
battery-
pack.
This
date
is
supplied
on
a
sticker
attached
to
Battery-packs
have
a
normal
shelf
life
of
five
to
ten
the
outside
of
the
ELT
case
and
to
each
battery.
(5-10)
years
and
must
be
replaced
at
1/2
of
normal
shelf
life
in
accordance
with
TSO-C91.
Cessna speci-
16-106.
REMOVAL
AND
INSTALLATION OF
TRANS-
fies
5
years
replacement
of
lithium
(4-cell)
battery
MITTER.
(See
figure
16-16.)
packs.
a.
Remove
baggage
curtain
to
gain
access
to
the
transmitter
and
antenna.
16-104.
OPERATION.
A
three
position
switch
on
the
b.
Disconnect
co-axial
cable
from
end
of
transmit-
forward
end
of
the
unit
controls
operation.
Placing
ter.
the switch
in
the
ON
position
will
energize
the
unit to
c.
Cut
sta-strap
securing
antenna
cable
and
unlatch
start
transmitting
emergency
signals.
In
the
OFF
metal
strap
to
remove
transmitter.
position,
the unit
is
inoperative. Placing
the
switch
in
the
ARM
position
will
set
the
unit
to
start
trans-
NOTE
mitting
emergency
signals
only
after
the
unit
has
re-
ceived
a
5g
(tolerances
are
+2g
and
-0g)
impact
force,
Transmitter
is
also
attached
to the
mounting
for
a
duration
of
11-16
milliseconds.
bracket
by
velcro
strips;
pull
transmitter
to
free
from
mounting
bracket
and
velcro.
NOTE
Do
not
leave
the
emergency
locator
trans-
mitter
in
the
ON
position
longer
than
1
To
replace
velcro
strips,
clean
surface
thor-
second
(3
sweeps
of
the
warble
tone)
or
oughly
with
clean
cloth
saturated
in
one
of
you
may
activate
downed
aircraft
pro-
the
following
solvents:
Trichloric
thylene,
cedures
by
C.
A.
P.
,
D.O.T.
or
F.A.A.
Aliphatic
Napthas,
Methyl
Ethyl
Ketone
or
personnel.
Enmar
6094
Lacquer
Thinner.
Cloth
should
16-60

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Cessna T182 Series Specifications

General IconGeneral
Engine TypeLycoming IO-540-AB1A5
Horsepower230 hp
Seating Capacity4
Service Ceiling18, 100 feet
Takeoff Distance1, 600 feet
Landing Distance1, 350 ft
TypeSingle-engine
Max Takeoff Weight3, 100 lb
Wingspan36 ft
Length29 ft
Height9 feet 3 inches
Fuel Capacity92 US gal (348 L)

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