FlightSafety LEARJET 45 - Page 246

10-10
FOR TRAINING PURPOSES ONLY
LEARJET 45 PILOT TRAINING MANUAL
FlightSafety
international
ANTI-ICE
PRESSURE REGULATING
AND SHUTOFF VALVE (PRSOV)
PNEUMATIC
CROSS-OVER
(SERVO AIR)
ANTI-ICE
PRESSURE REGULATING
AND SHUTOFF VALVE (PRSOV)
HIGH PRESSURE
BLEED-AIR FROM
RIGHT ENGINE
HIGH PRESSURE
BLEED-AIR FROM
LEFT ENGINE
LEGEND
REGULATED FLOW
HP BLEED-AIR
SENSOR
HEAT DETECTION LOOP
CHECK
VALVES
HEAT SENSORS
UNDER OVER
TEMP
SENSOR
TEMP
SENSOR
WING/STAB LEAK
CAS
WING/
STAB
LEAK
CWP
WING/STAB
ON
L WING/
STAB HT
R WING/
STAB HT
R MAIN BUS
L MAIN BUS
INTEGRATED ECS
TEMP CONTROLLER
CAS
(SEE TABLE 10-1)
LEAK
DETECTION
UNIT (255° F)
140 ± 7°F
140 ± 7°F
> IDLE < 70°F
IDLE < 40°F
> 225°F
> 160°F
HEAT SENSORS
UNDER OVER
>IDLE < 85°F
IDLE < 49°F
> 233°F
> 175°F
HEAT SENSORS
UNDER OVER
>IDLE < 85°F
IDLE < 49°F
> 233°F
> 175°F
}
WING OVERHEATWING TEMP LOW
STAB TEMP LOW STAB OVERHEAT
{
{}
Figure 10-6. Wing/Stab Anti-Ice System Schematic