Cessna 182 1978 - Encoding Altimeter Installation

MODEL 182
& T182 SERIES SERVICE
MANUAL
On aircraft
equipped
with alternate
static
Never
blow through
pitot or static
lines toward
source, use
the same procedure,
opening
the instruments.
alternate
static
source valve
momentarily
to clear
line,
then close
valve
and clear
Like the pitot
lines, static pressure lines must
be remainder of system.
kept clear
and connections
tight.
Static source
sumps
collect moisture
and keeps system clear.
However. Check
all static pressure line
connections for tight-
when necessary,
disconnect
static
line at first
instru-
ness.
If hose
or hose
connections
are
used, check
ment
to which
it is connected,
then blow
line to
clear
for general
condition and
clamps for
security.
Re-
with low
pressure air.
place
hose which
have cracked,
hardened
or show
other
signs of deterioration.
2
5
WITHOUT
ALTERNATE
STATIC SOURCE
INSTALLED
2
WITH ALTERNATE
STATIC SOURCE INSTALLED
1. Static Line
2. Standby
Altimeter
3.
Encoding
Altimeter
4. Airspeed
Indicator
NOTE
5.
Vertical
Speed
Indicator
STATIC
6. Alternate
Static Source
*
TO R/H STATIC
SOURCE
7. Line (To
Transponder) ** TO
L/H STATIC SOURCE
Figure
15-4. Encoding
Altimeter
Installation
15-8