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* Equipment cooling panel, P5
* Cabin pressure control panel, P5-6
* Cabin altitude panel, P5-6.
Cabin Temperature Panel
These controls and indications are on the cabin temperature
panel:
* Control cabin temperature control
* Forward cabin temperature control
* Aft cabin temperature control
* Trim air switch
* Temperature indication and selection
* Duct overheat indication.
Air Conditioning/Bleed Air Controls Panel
These controls and indications are on the air conditioning/bleed
air controls panel:
* Ram air inlet door indication
* Recirculation fans switches
* Cooling pack switches
* Pack overheat and fault indication
* Pack reset.
Equipment Cooling Panel
These controls and indications are on the equipment cooling
panel:
* Supply and exhaust fans switches
* No cooling indication.
Cabin Pressure Control Panel
These controls and indication are on the cabin pressure control
panel:
* Landing altitude selector
* Flight altitude selector
* Mode selector
* Outflow valve position indicator
* Manual control toggle switch.
Cabin Altitude Panel
These controls and indications are on the cabin altitude panel:
* Cabin altitude
* Cabin differential pressure
* Rate of change of cabin altitude
* Altitude horn cutout switch.
AIR CONDITIONING - CONTROL PANELS
EFFECTIVITY
GUN 001-099, 201-999 21-00-00
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AIR CONDITIONING - CONTROL PANELS
EFFECTIVITY
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AIR CONDITIONING - CONTROL PANELS
AIR CONDITIONING - CONTROL PANELS
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Distribution
The distribution system has these components in the
distribution compartment (aft of the forward cargo
compartment):
* Main distribution manifold
* Recirculation fans
* Ground conditioned air connection.
The equipment cooling system has components in the EE
compartment, the forward equipment compartment, and the
flight compartment.
Cooling System
The two air conditioning packs are in the air conditioning
compartments. The air conditioning compartments are on the
left and right sides of the keel beam in the wing-to-body area.
Access is from the bottom of the airplane fuselage.
Temperature Control
The temperature control system has components in these areas
of the airplane:
* Passenger distribution ducting
* EE compartment
* Flight compartment.
GUN 201-999
Humidity/Air Contaminant Control
The ozone converters are in the pneumatic manifold forward air
conditioning bays.
GUN 001-099, 201-999
Pressurization
The pressurization system has components in these areas of
the airplane:
* Flight compartment
* EE compartment
* Aft cargo compartment.
AIR CONDITIONING - COMPONENT LOCATION
EFFECTIVITY
GUN 001-099, 201-999 21-00-00
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21-00-00-805
AIR CONDITIONING - COMPONENT LOCATION
AIR CONDITIONING - COMPONENT LOCATION
EFFECTIVITY
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21-00-00-805
General
These are the primary parts of the air conditioning (A/C) system
that have an effect on the supply of fresh air or the recirculation
of conditioned air:
* Pack flow control
* Pack cooling system
* Zone temperature control
* Recirculation
* Air distribution.
The primary parts of the A/C system have these functions:
　
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