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Learjet 24D - Page 203

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the leading edge (Figure 10A-10). The air is
then exhausted overboard through a scupper
drain on the bottom of the leading edge near
the tip tanks.
The control switch is usually located on the
pilot’s subpanel. The ON–OFF switch con-
trols electrical power to the wing regulator
valve located in the tail compartment.
The wing regulator valve is electrically con-
trolled and pneumatically operated. These air-
planes have one of two kinds of regulator
valves installed. The earlier kind is a Janitrol
valve which is electrically closed and fails to
the open position. The later kind is a Whittaker
valve which is electrically energized open and
fails to the closed position. Either valve reg-
ulates pressure to the wing ducts at 8 to 20 psi.
A green WING HEAT light illuminates when
the duct temperature reaches 215ºF. A red
WING OVERHEAT light illuminates when
the leading-edge structure temperature reaches
215ºF. Do not operate the system with the red
light illuminated.
10A-10
FOR TRAINING PURPOSES ONLY
LEARJET 20 SERIES PILOT TRAINING MANUAL
FlightSafety
international
WING
WING
OVERHEAT
HEAT
WING
ANTI-ICE
SWITCH
WING
ON
OFF
ANTI-ICE
SCUPPER
SENSE LINE
REGULATOR VALVE
(WING LE ANTI-ICE)
DEFOG SHUTOFF VALVE
TO DEFOG SYSTEM
RH ENGINE
LH ENGINE
TO
AIR-CONDITIONING
SYSTEM
BLEED-AIR
MANIFOLD
Figure 10A-10. Wing Anti-icing System

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