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Pitot Heat / Anti-Ice ...............................................................................OFF
Hydraulic System ...................................................................................SET
Beacon..................................................................................................... OFF
Log Book / ACARS .............................................................COMPLETED
IRS Selectors ...........................................................................................OFF
F/O Challenge Capt. Respond
Parking Brake......................................................................(AS REQUIRED)
Initially set parking brake when at a full stop. After all engines are shut
down and the appropriate signal has been received from ground service
personnel that the wheels are chocked, release the parking brake.
Start Levers........................................................................................ CUTOFF
The Captain will shut down the engine(s) upon arrival in the final park
position and monitor engine instruments to ensure that a complete
shutdown has occurred.
Caution: Prior to shutdown, the engine should be operated below 35% N1
(preferably at idle) for a period of 3 minutes (absolute minimum
of 1 minute) following touchdown or until arriving at the gate,
whichever occurs first.
Pitot Heat / Anti-Ice ...................................................................................OFF
The First Officer will insure that the pitot heat, engine anti-ice, and wing
anti-ice are turned off.
Seat Belt Sign (Flow) ..................................................................................OFF
The First Officer will turn the seat belt sign OFF when he observes the
parking brake set, and the engines being shut down unless the Captain
requests otherwise.
Sec. 3 Page 284
Rev. 11/15/02 #41 Continental
737
Flight Manual
Hydraulic System ........................................................................................SET
Both electric hydraulic pump switches are normally turned OFF; however, if
conditions dictate, one may be left ON to function as a gust lock.
Air Conditioning (Flow)..............................................................................SET
Evaluate air conditioning requirements and configure pneumatics
appropriately.
Caution: Possible supply duct manifold damage may occur when APU
air and ground preconditioned air are being supplied to the
aircraft simultaneously.
To avert possible damage to the ducting system(s) the
following procedures will be followed:
· If preconditioned air is supplied after gate arrival, the
APU bleed air switch and air conditioning pack
switch(es) must be turned OFF.
· If preconditioned air is not supplied after gate arrival, the
APU bleed air switch and air conditioning pack
switch(es) must be turned OFF prior to the last pilot
leaving the flight deck. Passenger comfort should always
be a consideration before this is accomplished.
Sterile Cockpit Light (Flow)......................................................................OFF
Beacon..........................................................................................................OFF
Log Book / ACARS ..................................................................COMPLETED
Actual FOB will be recorded in the logbook after each leg.
For ETOPS / LRN flights, record IRS data in the logbook as described in
Section 3-1.
Complete ACARS Post-Flight Report:
The POST FLIGHT REPORT is not available until after the In event.
After all the required information has been entered, touch SEND to
queue the In Report message and return the display to the screen from
which the POST FLIGHT REPORT was called.
SEND has no effect if any required information is missing.
737
Flight Manual Continental
Sec. 3 Page 285
Rev. 11/15/02 #41
If the POST FLIGHT REPORT is not sent, the FIELD LOCKED message
will appear when an attempt is made to initialize the system for the
next flight.
IRS Selectors ...............................................................................................OFF
Caution: Center tank fuel pumps must be OFF unless personnel are
available on the flight deck to monitor low-pressure lights.
Sec. 3 Page 286
Rev. 11/15/02 #41 Continental
737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual Continental
Sec. 3 Page 287
Rev. 11/15/02 #41
>>@ TERMINATION FLOW
Sec. 3 Page 288
Rev. 11/15/02 #41 Continental
737
Flight Manual
BCD TERMINATION FLOW
737
Flight Manual Continental
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