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reaching 1,500 ft. or until obstacle clearance height has been attained.
When Cabin Rate of Climb Indicator Stabilizes:
No. 1 Engine Bleed Air Switch....................................................................ON
Isolation Valve Switch............................................................................ AUTO
Pressurization Mode Selector ...............................AUTO (AS REQUIRED)
Cabin Altitude Selector (If Installed)....................... SET (AS REQUIRED)
* * * *
AIR SYSTEMS
Sec. 2.2 Page 26
Rev. 11/15/02 #41
Continental
737
Flight Manual
WING-BODY OVERHEAT
The WING-BODY OVERHEAT light illuminated indicates a bleed air duct leak in the
fuselage, engine strut, or wing leading edge.
Isolation Valve Switch ...................................................................CLOSE
Prevents the isolation valve from opening in the following procedural
step.
Pack Switch (Affected Side) ...............................................................OFF
Engine Bleed Air Switch (Affected Side)..........................................OFF
IF WING-BODY OVERHEAT Light Extinguishes:
Avoid Icing Condition.
* * * *
IF The Left WING BODY OVERHEAT Light Remains Illuminated & APU Is
Operating:
APU Bleed Air Switch (If APU Running) ................................OFF
This stops the flow of air from the APU to the left side of the
pneumatic ducting.
Note: If APU is the source of bleed air, place the right engine
bleed air switch ON to maintain pressurization.
IF Light Extinguishes:
Avoid Icing Conditions.
* * * *
IF The Light Remains Illuminated:
APU Switch ...........................................................................OFF
The source of the bleed air leak is in the APU compartment
“before” the APU bleed air valve.
DO NOT OPERATE THE APU!
IF The Light Extinguishes:
Left Engine bleed air can be used as a source of pneumatics.
Isolation Valve Switch ...............................................AUTO
Engine Bleed Air Switch (Affected Side) .....................ON
Left Pack Switch ........................................................AUTO
* * * *
OR
OR
737
Flight Manual
Continental
AIR SYSTEMS
Sec. 2.2 Page 27
Rev. 11/15/02 #41
CD ZONE TEMP
A ZONE TEMP light illuminated indicates temperature in the related duct has
exceeded limits or flight deck temperature control has been lost.
If ZONE TEMP light does not extinguish when Master Caution system is reset:
Do Not Takeoff.
Temperature Selector.......................................COOLER TEMPERATURE
Prevents trim air modulating valve from returning to an overheat.
Trip Reset Button ...................................................................................PRESS
The ZONE TEMP light extinguishes if the duct temperature has cooled below
limits. Allow a 2 minute cooling period.
IF ZONE TEMP Light Extinguishes:
Proceed normally.
* * * *
IF Duct Temperature Increases Rapidly:
Trim Air Switch...................................................................................OFF
Shuts off trim air.
* * * *
OR
AIR SYSTEMS
Sec. 2.2 Page 28
Rev. 11/15/02 #41
Continental
737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
ANTI-ICE, RAIN
Sec. 2.3 TOC-1
Rev. 11/15/02 #41
2.3 – ANTI-ICE, RAIN
TABLE OF CONTENTS
ARCING / DELAMINATED / SHATTERED OR
CRACKED WINDOW....................................................................... 1
ENGINE COWL ANTI-ICE...................................................................... 3
ENGINE COWL VALVE OPEN .............................................................. 3
>>@ PITOT STATIC HEAT / BCD PROBE HEAT
MALFUNCTIONS............................................................................. 4
BCD TAI INDICATION ................................................................. 5
WINDOW OVERHEAT........................................................................... 5
WING ANTI-ICE VALVE FAILURE......................................................... 6
ANTI-ICE, RAIN
Sec. 2.3 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
ANTI-ICE, RAIN
Sec. 2.3 Page 1
Rev. 11/15/02 #41
ANTI-ICE, RAIN
ARCING / DELAMINATED / SHATTERED
OR CRACKED WINDOW
This condition is recognized by arcing, substantial delamination, shattering,
or cracking of any flight deck window. Window 4 is the only window
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