Learjet 60 - Bleed Air Supply Schematic (Figure 6-1)

Learjet 60 Pilot’s Manual
PM-123 6-3
Change 6
Change 6
provides an additional means of ice detection and should not be used
as the only source of ice detection. The Rosemount Ice Detector System
receives 28 VDC through the 15-amp ICE DETECTOR circuit breaker
on the pilot’s circuit breaker panel.
BLEED AIR SUPPLY SCHEMATIC
Figure 6-1
COCKPIT AIR
DISTRIBUTION
CABIN AIR
DISTRIBUTION
EMER
BLEED AIR
OFF
O
N
L
R
CABIN AIR
DISTRIBUTION
HEAT EXCHANGER
RAM AIR
RAM AIR
PLENUM
CABIN AIR
ON
OFF
TEMPERATURE
CONTROL
VALVE
TEMPERATURE
CONTROL
VALVE
CREW
COLD HOT
C
OLD HOT
CABIN
ENGINE BLEED
WING ANTI-ICE
BYPASS CIRCUIT
NACELLE INLET
ANTI-ICE
EMERGENCY
PRESSURIZATION
VALVE
EMERGENCY
PRESSURIZATION
VALVE
BLEED-AIR
SHUT-OFF
VALVE
BLEED-AIR
SHUT-OFF
VALVE
BLEED
AIR
MIX
VALVE
BLEED
AIR
MIX
VALVE
TEMPERATURE
CONTROL
SYSTEM
(SERVO AIR)
PRESSURIZATION
JET PUMP &
ALCOHOL
ANTI-ICE
WING
ANTI-ICE
WINDSHIELD
ANTI-ICE
GROUND
SERVICE
HYDRAULIC
SYSTEM
LOW PRESS
HIGH PRESS
LOW PRESS
HIGH PRESS
ENGINE BLEED
WING ANTI-ICE
BYPASS CIRCUIT
NACELLE INLET
ANTI-ICE
FLOW
CONTROL
VALVE
RAM AIR
BLEED AIR
CONDITIONED AIR