TM 1-1510-224-10
NOTE
Under conditions where one bleed air
source is inoperative, sufficient bleed
air pressure for deice boot inflation
may not be available. Prior to deice
boot inflation, check the regulated
bleed
air
pressure
gage
for a
minimum of 16 PSI. If insufficient
pressure exists, increasing engine N1
and/or decreasing aircraft altitude -
will increase bleed air pressure.
b.
Operation.
WARNING
To
ensure
adequate
bleed
air
pressure to the deice boots, do not
simultaneously actuate surface and
antenna deice systems in the manual
mode.
(1)
Deice boots are intended to remove ice
after it has formed rather than prevent ice formation. For
the mdst effective deicing operation, allow at least 1/2
inch of ice to form on the boots before attempting ice
removal. Very thin ice may crack and cling to the boots
instead of shedding.
WARNING
Never cycle the system rapidly. This
may cause the ice to accumulate
outside the contour of the inflated
boots and prevent ice removal.
(2)
A two position deice switch on the
overhead control panel, placarded SURFACE, controls
the deicing operation. The switch is spring loaded to
return to the off position from SINGLE CYCLE AUTO or
MANUAL. When the SINGLE CYCLE AUTO position is
selected, the distributor valve opens to inflate the wing
boots. After an inflation period of approximately 6
seconds, an electronic timer switches the distributor to
deflate the wing boots and a 4 second inflation begins in
the horizontal stabilizer, stabilon, and taillet boots.
When these boots have inflated and deflated, the cycle
is complete.
(3)
If the switch is held in the MANUAL
position, the boots will inflate simultaneously and remain
inflated until the switch is released. The switch will
return to the off position when released. After the cycle,
the boots will remain in the vacuum hold down condition
until again actuated by the switch.
(4)
Either engine is capable of providing
sufficient bleed
air for all requirements of the surface deice system.
Check valves in the bleed air and vacuum lines prevent
backflow through the system during single engine
operation. Regulated pressure is indicated on a gage,
placarded PNEUMATIC PRESSURE, located on the
center subpanel.
2-51. ANTENNA DEICING SYSTEM.
a.
Description. The antenna deicing system
removes or prevents ice accumulation on the mission
antennas. Pressure regulated bleed air is used to
supply pressure to inflate the boots. To assure
operation of the system in the event of failure of one
engine, a check valve is incorporated in the bleed air line
from each engine to prevent loss of pressure through the
compressor of the inoperative engine. Inflation and
deflation phases are controlled by distributor valves.
WARNING
To
ensure
adequate
bleed
air
pressure to the deice boots, do not
simultaneously actuate surface and
antenna deice systems in the manual
mode.
NOTE
Under conditions where one bleed air
source is inoperative, sufficient bleed
air pressure for deice boot inflation
may not be available. Prior to deice
boot inflation, check PNEUMATIC
PRESSURE gage for a minimum of 16
PSI. If insufficient pressure exists,
increasing
engine
N1
and/or
decreasing
aircraft
altitude
will
increase bleed air pressure.
b.
Antenna Deice System Switch. The antenna
deice system is controlled by a switch, placarded
ANTENNA, MANUAL SINGLE CYCLE AUTO, located
on the overhead control panel (fig. 2-15). The switch is
spring loaded to return to the off position from the
SINGLE CYCLE AUTO or MANUAL position. When the
switch is set to the SINGLE CYCLE AUTO position, the
system will run through one timed inflationdeflation
cycle. When the switch is held in the MANUAL position
the boots will inflate and remain inflated until the switch
is released.
c.
Operation. Deice boots are intended to remove
ice after it has formed rather than prevent ice formation.
For the most effective deicing operation, allow at least
1/8 to 1/4 inch of ice to form on the boots before
attempting removal. Very thin ice may crack and cling to
the boots instead of shedding.
2-57