Cessna skylance tc T182T, Информационное руководство

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SECTION 7 CESSNA
AIRPLANE AND SYSTEM DESCRIPTION MODEL T182T NAV III
GFC 700 AFCS
U.S.
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 7-9). 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 heat and ventilating air is supplied by outlet holes spaced
across a cabin manifold just forward of the pilot's and front passenger's
feet. Rear cabin heat and air is supplied by two ducts from the manifold,
one 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 from the cabin manifold outlet on top of the glareshield;
therefore, the temperature of the defrosting air is the same as heated
cabin air. A rotating control knob, labeled DEFROST, regulates the
volume of air to the windshield. Turn the knob clockwise to ON and
counterclockwise to OFF.
Separate adjustable ventilators supply additional air; one near each
upper corner of the windshield supplies air for the pilot and front
passenger, and two ventilators are available for the rear cabin area to
supply air to the rear seat passengers. There are additional ventilators
located in various positions in the cockpit.
T182TPHBUS-00
7-72