Cessna T182 Series User Manual

MODEL
182 & T182 SERIES
SERVICE MANUAL
16-69.
OVERHEAD
CONSOLE.
the "EL"
panel lighting
is controlled
by a rheostat
located on the instrument
switch
panel.
16-70. DESCRIPTION.
The overhead
console con-
tains
the instrument
flood lights
which
also may be
16-77.
REMOVAL
AND INSTALLATION.
(See
used
as map
lights
by
moving
the
slide covers
below
figure
16-11.
)
the lamps.
The intensity
of the
lights
is controlled
a. Disconnect
positive
cable
from
battery.
by
a rheostat
mounted
on
the instrument
panel.
b. Disconnect
and tag
all electrical
leads
from
panel.
16-71.
REMOVAL
AND INSTALLATION.
(See
c.
Remove
knobs,
decorative
nuts,
and switches.
figure
16-9
for removal
and installation.
d.
Remove
screws
securing
panel
to
stationary
panel and remove panel.
16-72.
INSTRUMENT
LIGHTING.
e. For
installation
reverse
the
preceding
steps.
After installation, check
all switches for
operation,
16-73.
DESCRIPTION.
The
instrument
panel
light-
ing
consists
of two
seperate
sections.
The lower
16-78.
INSTRUMENT
POST
LIGHTING.
two-thirds
of the
panel
is illuminated
by two
lights
mounted
in the
overhead
console.
The
lighting
for
16-79.
DESCRIPTION.
Individual
post
lighting
may
the
upper one-third
of the panel
is provided
by four
be installed
to provide
nonglare
instrument
lighting.
lights
mounted
in the
instrument
panel
glare
shield.
The post
light
consists
of a
cap and
a clear
lamp
The intensity
of the lighting
is controled
by
the in-
assembly
with
a tinted
lens.
The intensity
of
the
strument
light
dimming
rheostat
located
on the
post
lights
is controlled
by
the instrument
light
swithc
panel.
dimming
rheostat
located
on the switch
panel.
16-74.
REMOVAL
AND
INSTALLATION.
See
figure
16-9 and
16-10.
NOTE
16-75.
ELECTROLUMINESCENT
PANEL
LIGHTING.
When
installing
postlight
assemblies
assemblies shall be coated with RTV-102,
16-76. DESCRIPTION.
The
electroluminscent
light-
General Electric,
Waterford,
New York.
on
ing
consists
of two "EL"
panels. The
switch panel
forward
side of
panel where
postlight
could
and
the comfort
control
panel.
The ac
voltage
re -
come
in contact
with
sheet metal
subpanel.
quired
to drive
the "EL"
panels
is supplied
by a
This
coating
shall insulate
postlight
assem-
small invertapak
(power
supply)
located
behind
the
bly
from
contact
with airplane
structure.
instrument
panel on
the glove box.
The intensity
of
Maximum coating
thickness
to be .03.
16-79A.
TROUBLE SHOOTING
- POSTLIGHTING.
TROUBLE
PROBABLE CAUSE
REMEDY
LAMP WILL NOT
LIGHT.
Defective
lamp.
1. Test lamp
with ohmmeter
or
replace
with
a new
lamp.
is
OK, roceed
to step
2.
Defective socket or open 2. With switch on, test socket. If
circuit. defective, replace socket or
wiring.
ONE SECTION
OF
LAMPS
Defective
connector.
1. Test
for voltage
on
lamp side
WILL NOT LIGHT.
of onnector.
If voltage is
not
present,
check
opposite
side
of
connector.
If
voltage
is present,
replace pins
and sockets
as
necessary.
If
voltage
is not
pres-
ent.
check
connections
at term-
inal
block.
Defective
circuit in
dimming
2. Refer to
paragrph 17-90B.
assembly.
16-48

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)