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changes are scheduled on a through flight. This cabin inspection may be
accomplished by the flight attendants and status reported to the Captain.
A complete EXTERIOR INSPECTION and FLIGHT DECK INSPECTION
will be accomplished on each originating flight or crew change. Subsequent
inspections are to be performed at each station in accordance with the
EXTERIOR INSPECTION - THROUGH FLIGHT procedure.
Upon arrival at the aircraft, the following procedures are normally accomplished
in the designated order:
· Safety Inspection - Exterior
· Safety Inspection - Flight Deck (if required)
· Establish Electrical Power And Air Conditioning (if required)
· Flight Deck Inspection
· Exterior Inspection
· Cabin Inspection
· Receiving Aircraft Procedure/Checklist
When operationally efficient during crew changes, the exterior inspection may
be accomplished while waiting for passengers and crew to deplane.
Sec. 3 Page 12
Rev. 11/15/02 #41 Continental
737
Flight Manual
SAFETY INSPECTION - EXTERIOR
Either the Captain, First Officer or IRO will conduct an Exterior Safety
Inspection on all originating flights and crew changes.
Surfaces and Chocks ...........................................................................CHECK
Visually check that all movable surfaces are clear and the chocks are in
place.
Maintenance Status.............................................................................CHECK
If maintenance is in progress, confer with maintenance personnel to
determine if the work will prevent activation of any aircraft systems.
737
Flight Manual Continental
Sec. 3 Page 13
Rev. 11/15/02 #41
SAFETY INSPECTION – FLIGHT DECK
Either the Captain, First Officer or IRO will conduct the Flight Deck Safety
Inspection from memory when there is neither APU nor External electrical
power on the busses.
Logbook (Aircraft & Cabin) ..............................................................CHECK
Verify maintenance status is acceptable for flight and ensure agreement
with authorized dispatch deviations, if required.
The remaining items from Flight Deck Safety Inspection may be omitted if both
AC and DC Electrical systems are already powered when the crew arrives at the
aircraft.
Battery Switch...............................................................................................ON
Verify guard down.
DC Meter Selector......................................................................................BAT
Check voltmeter at least 23V DC and ammeter zero.
Electric Hydraulic Pump Switches...........................................................OFF
Landing Gear Lever..............................................................................DOWN
Verify three green gear lights illuminated.
Radar Switch..................................................................................OFF / TEST
Sec. 3 Page 14
Rev. 11/15/02 #41 Continental
737
Flight Manual
ESTABLISH ELECTRICAL POWER AND AIR CONDITIONING
(IF REQUIRED)
APU ELECTRIC AND PNEUMATIC POWER
Starting
If first flight of the day, complete the “Fire / Ovht / Extinguisher Test” described
in the RECEIVING AIRCRAFT expanded checklist procedures in this section.
Battery Condition.......................................................................... CHECKED
A minimum of 23V is required for APU start.
APU Bleed Air Switch................................................................................OFF
APU Switch............................MOMENTARY START, RELEASE TO ON
Check the LOW OIL PRESSURE light illuminated and >>@ check a full
scale negative deflection on the DC ammeter.
Check the LOW OIL PRESSURE light extinguished. Monitor EGT.
APU Generator.............................................................................ON BUSSES
When the APU GEN OFF BUS light illuminates, move the APU Generator Bus
switches to ON. Verify >>@ BUS OFF BCD SOURCE OFF lights
extinguish.
Note: The APU must be operated one minute before using a pneumatic
source.
Note: Provide positive fuel pressure to the APU by selecting a left
(forward recommended) main tank boost pump ON or a right
(forward recommended) main tank boost pump ON with crossfeed
open.
Note: If extended APU operation is required on the ground and fuel is
loaded in the center tank, leave the left center tank fuel pump
switch ON. This will preclude a fuel imbalance before takeoff.
Caution: Center tank fuel pumps must be OFF unless personnel are
available on the flight deck to monitor LOW PRESSURE lights.
　
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