TM 55-1510-221-10
3. Cabin temperature control rheo-
stat - As required.
4. Cabin, cockpit and defrost air
knobs - As required.
(2.) Manual cooling mode.
1.
Bleed air valve switches - OPEN,
LEFT and RIGHT.
NOTE
For maximum cooling on the ground, set
the bleed air valve switches to the
ENVIRO OFF position.
2.
(3.) Air conditioning cold operation mode.
(Used if ambient
-25º C).
Cabin temperature mode selector
switch - MAN COOL.
temperature is between 10°C and
NOTE
Setting the cabin temperature mode selec-
tor switch to the A/C COLD OPN posi-
tion at ambient temperatures below -25°C
may cause the air conditioning system to
exceed the compressor low pressure limit
switch setting,
terminating compressor
operation, and thereby rendering the sys-
tem inoperative for the remainder of the
flight.
1.
Bleed air valve switches - OPEN,
LEFT and RIGHT.
2. Cabin temperature mode selector
switch - A/C COLD OPN.
3. Cabin temperature control rheo-
stat - As required.
4. Cabin, cockpit and defrost air
knobs - As required.
2-71. UNPRESSURIZED VENTILATION.
Ventilation is provided by two sources. One
source is through the bleed air heating system in
both the pressurized and unpressurized mode. The
second source of ventilation is obtained from ram
air through the condenser section in the nose
through a check valve in the vent blower plenum.
Ventilation from this source is in the unpressurized
mode only with the CABIN PRESS DUMP switch
in the DUMP position. The check valve closes dur-
ing pressurized operation. Ram air ventilation is dis-
tributed through the main ducting system to all out-
lets. Ventilation air, ducted to each individual eye-
ball cold air outlet, can be directionally controlled
by moving the ball in the socket. Volume is regu-
lated by twisting the outlet to open or close the
valve.
2-72. ENVIRONMENTAL CONTROLS.
An environmental control section on the over-
head control panel (fig. 2-12) provides for automatic
or manual control of the system. This section con-
tains all the major controls of the environmental
function including bleed air valve switches, a vent
blower control switch, an aft vent blower switch, a
manual temperature switch for control of the heat
exchanger valves, a cabin temperature level control,
and the cabin temp mode selector switch for select-
ing automatic heating or cooling or manual heating
or cooling. Four additional manual controls on the
main instrument subpanels may be utilized for par-
tial regulation of cockpit comfort when the cockpit
partition door is closed and the cabin comfort level
is satisfactory.
a. Heating Mode.
(1.)
If the cockpit is too cold:
1.
Pilot and copilot air knobs - As
required.
2.
Defrost air knob - As required.
3.
Cabin air knob - Pull out in small
increments. Allow 3 -5 minutes
after each adjustment for system
to stabilize.
(2.)
If the cockpit is too hot:
1.
Cabin air knob - As required.
2.
Pilot and copilot air knobs - In as
required.
3.
Defrost air knob - In as required.
b. Cooling Mode:
(1.)
If the cockpit is too cold:
1.
Pilot and copilot air knob - In as
required.
2.
Defrost air knob - In as required.
3. Overhead cockpit outlets - As
required.
(2.)
If the cockpit is too hot:
1.
Pilot and copilot air knobs - Out
as required.
2-56