CESSNA
MODEL 172S
SECTION 7
AIRPLANE & SYSTEMS DESCRIPTION
CABIN HEATING, VENTILATING AND
DEFROSTING SYSTEM
The temperature
and volume
of airflow into the cabin can be
regulated
by manipulation
of the push-pull CABIN HT and CABIN
AIR controls
(Refer to Figure 7-8). Both controls are the double-
button locking type and permit intermediate settings.
For cabin ventilation, pull the CABIN AIR knob out. To raise the
air temperature,
pull the CABIN HT knob out approximately
1/4 to
1/2 inch for a. small
amount
of cabin
heat. Additional
heat
is
available by pulling the knob out farther; maximum heat is available
with the CABIN
HT knob pulled out and the CABIN
AIR knob
pushed full in. When no heat is desired in the cabin, the CABIN HT
knob is pushed full in.
Front cabin hear and ventilating
air is. supplied by outlet holes
spaced
across
a cabin
manifold
just forward
of the pilot's
and
copilot's feet. Rear cabin heat and air is supplied by two ducts from
the manifold,
cine extending
down each side of the cabin to an
outlet just aft of the rudder pedals at floor level. Windshield defrost!
air is also supplied .by two ducts leading from the cabin manifold to
defroster outlets near the .Iower edge of the windshield.
Two knobs
control sliding valves in either defroster outlet to permit regulation of
defroster airflow.
Separate
adjustable
ventilators
supply additional
air; one near
each upper corner of the windshield
supplies air for the pilot and
copilot, and two ventilators are available for the rear cabin area to
supply
air 10 the
r~ar
seat
passengers.
There .are additionall.
ventilators located in various positions in the cockpit.
,
; i
Revision 4
7-39
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