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SECTION
7
AIRPLANE
&
SYSTEMS DESCRIPTION
CESSNA
MODEL 172R
|CLOCK
/ O.A.T. INDICATOR
An
integrated
clock
/
O.A.T.
/
voltmeter is installed in the
upper
left
side of the instrument
panel
as
standard
equipment.
For a
I
complete description and
operating
instructions, refer
to
the
Supplements,
Section
9.
STALL
WARNING
SYSTEM
The
airplane is
equipped with
a
pneumatic
type
stall
warning
system
consisting of an
inlet in
the
leading
edge of
the left wing,
an
|air-operated
horn
near
the
upper
left
corner
of
the windshield,
and
associated plumbing.
As
the
airplane approaches a
stall,
the
low
pressure on the
upper
surface
of
the
wings
moves
forward
around
the
leading edge of
the wings. This low pressure
creates
a
differential
pressure
in the stall
warning system
which
draws air
through
the
warning horn, resulting
in an
audible warning
at
5
to
10
knots above stall
in all
flight
conditions.
STANDARD
AVIONICS
Standard
avionics for
the
Model
172R
airplanes include
the
following equipment:
KX-155A
Nav/Com Radio with
Kl
208
or Kl 209A
Indicator Head
KT-76C
Transponder
KMA-26
Audio Panel
3000-1
1
Emergency
Locator Transmitter
(ELT)
For
complete operating instructions
on
the standard and optional
|avionics
systems,
refer
to
the Supplements,
Section
9.
7-46
Feb
28/00
Summary of Contents for 172R
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