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will ensure protection in the event of loss of AC power.
Cabin Temperature Selectors ............................................................... AUTO
Set for desired temperature.
Recirculation Fan Switch(es) ................................................................ AUTO
Isolation Valve Switch.............................................................................OPEN
APU Bleed Air Switch................................................................................OFF
Left and/or Right Air Conditioning Pack Switch(es)...............................ON
Position the pack switch(es) as desired to AUTO or HIGH.
Operation of two packs from one air source is permitted provided the
external air cart can maintain 20-25 PSI with both packs operating.
Pneumatic Duct Pressure Indicator............................................. 20 – 25 PSI
Sec. 3 Page 18
Rev. 11/15/02 #41 Continental
737
Flight Manual
IF External Air Cart Cannot Maintain 20 - 25 PSI:
Isolation Valve Switch .....................................................................AUTO
APU Bleed Air Switch ..........................................................................ON
APU bleed air will service the left pack and external air will service
the right pack.
737
Flight Manual Continental
Sec. 3 Page 19
Rev. 11/15/02 #41
FLIGHT DECK INSPECTION
The following flight deck items should be checked:
>@BCD ACARS .............................................. AUTO INITIALIZE
Position Lights...............................................................................................ON
Spare Bulbs ..........................................................................................CHECK
Escape Rope (Right)............................................................................CHECK
Smoke Goggles (Right) .......................................................................CHECK
Portable Oxygen and Mask (As Installed).......................................CHECK
Fire Extinguisher .................................................................................CHECK
>>@ Crew Oxygen Valve....................................................................ON
Circuit Breakers ..................................................................................CHECK
Crew / ACM Life Vests.......................................................................CHECK
Headsets and Microphones ................................................................CHECK
ACM Smoke Goggles..........................................................................CHECK
ACM Oxygen Mask (Test Not Required) ........................................CHECK
Crash Ax...............................................................................................CHECK
Emergency Medical Kit ......................................................................CHECK
Smoke Goggles (Left) ..........................................................................CHECK
Escape Rope (Left) ..............................................................................CHECK
Publications (Checklists, Manuals, etc.)...........................................CHECK
Crew Baggage (Under 2nd ACM Seat)........................................... STOWED
Protective Breathing Equipment (PBE) ...........................................CHECK
For operational convenience, tests and checks required by the RECEIVING
AIRCRAFT procedure applicable to modules located on the aft overhead
instrument panel (P5 aft) may be accomplished concurrently with the
FLIGHT DECK INSPECTION.
Sec. 3 Page 20
Rev. 11/15/02 #41 Continental
737
Flight Manual
EXTERIOR INSPECTION
Either the Captain, First Officer or IRO will conduct the Exterior Inspection.
The recommended sequence is to start at the left forward fuselage and proceed
in a clockwise direction. During the walk around, observe the general condition
of all surfaces, fuselage, empennage, wings, windows, antennas, flight controls,
engines, and cowlings. Check particularly for damage, fluid leakage, proper
position, and security of access panels. Also verify that crew, passengers, and
cargo doors, which are not in use, are closed and the door handles recessed.
Check all external lights are clean, with undamaged lenses. Check operation of
navigation / position lights.
Check potable water and lavatory fill and drain areas for leakage. If evidence of
leakage is found, notify maintenance.
737
Flight Manual Continental
Sec. 3 Page 21
Rev. 11/15/02 #41
Note: If evidence of fluid leakage or stains is noted at the forward and/or aft
lavatory service panel, ground personnel must verify if a leak exists
　
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