Embraer EMB145 - Page 2078

AIRPLANE
OPERATIONS
MANUAL
PNEUMATICS
AIR CONDITIONING
AND PRESSURIZATION
REVISION 38
2-14-10
Page
3
Code
01
AOM-145/1114
FROM
LEFT BLEED
SYSTEM
PRESSURE REGULATING
AND SHUTOFF VALVE
SPRAY
NOZZLE
RAM
AIR
RAM AIR
VALVE
EMERGENCY
RAM AIR
SECONDARY
HEAT
EXCHANGER
LEFT
ECS
PACK
DUAL
TEMPERATURE
CONTROL
VALVE
HEAT
EXCHANGER
PRIMARY
FAN
TO
OUTSIDE
COMPRESSOR
TURBINE
CONDENSER
WATER
SEPARATOR
FROM
RIGHT
PACK
RECIRCULATION
FAN
PASSENGER
COMPARTMENT
RECIRCULATION
AIR INLET
TO
COCKPIT
TO
GASPER
TO
PASSENGER
CABIN
GROUND
CONNECTION
TEMPERATURE SENSOR
TEMPERATURE SWITCH
PRESSURE SWITCH
EICAS MESSAGE
LEGEND
EM145AOM142002A.DGN
AIR CONDITIONING SYSTEM SCHEMATIC