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Start Switches .........................................................................CONTINUOUS
Takeoff Config. Switch (If Installed) ...............................CHECKED (F, C)
Transponder ..........................................................................................TA/RA
F/O Challenge F/O Respond
Recall............................................................................................... CHECKED
Press the recall panel. Observe all MASTER CAUTION annunciator lights
illuminated. Release the recall panel and observe all lights extinguish.
Takeoff Announcement............................................................COMPLETED
The FO will make the takeoff announcement by stating, “FLIGHT
ATTENDANTS PLEASE BE SEATED FOR DEPARTURE.”
Sec. 3 Page 106 737
Rev. 11/15/02 #41 Continental Flight Manual
Air Conditioning & Pressurization ...........................................................SET
An engine bleeds ON takeoff is preferred because it reduces flight deck
workload and provides improved cabin pressurization. However, weight
penalties are incurred for takeoffs with engine bleeds ON. Load planning
will calculate whether or not the actual gross takeoff weight permits the use
of engine bleed air, and will include the bleed configuration in the pilot
weight manifest given to the crew. For bleed configuration adjustments,
refer to Section 5.
Bleeds On Takeoff: Configure the air conditioning panel as follows:
Right Air Conditioning Pack.......................................................AUTO
Isolation Valve ............................................................................AUTO
Left Air Conditioning Pack .........................................................AUTO
No. 1 Engine Bleed Air Switch ....................................................... ON
APU Bleed Air Switch....................................................................OFF
No. 2 Engine Bleed Air Switch… ................................................... ON
Bleeds Off Takeoff: (APU bleed used for air conditioning) configure the
air conditioning panel as follows:
Right Air Conditioning Pack Switch ..........................................AUTO
Isolation Valve Switch...............................................................CLOSE
Left Air Conditioning Pack Switch.............................................AUTO
No. 1 Engine Bleed Air Switch ......................................................OFF
APU Bleed Switch........................................................................... ON
No. 2 Engine Bleed Air Switch ......................................................OFF
Caution: If engine failure occurs, do not position engine bleed air
switches ON until reaching 1,500 feet or until obstacle
clearance height has been attained.
Start Switches.......................................................................... CONTINUOUS
Verify that the ignition selector switch is set at L or R.
If moderate to severe precipitation is a factor, select start switches to FLT.
Takeoff Config. Switch (If Installed)................................ CHECKED (F, C)
The Captain will press and hold the TAKEOFF WARNING TEST switch on the
center instrument panel. Verify that the takeoff configuration warning horn
does not activate.
737 Sec. 3 Page 107
Flight Manual Continental Rev. 11/15/02 #41
Autothrottle (Flow).......................................................................................ON
Ensure that N1 limit is TO or REDUCED TO. When clear of congested
areas, arm the autothrottle. Observe the A/T mode annunciates ARM.
Verify power setting from FMC.
Transponder............................................................................................TA/RA
Rotate selector to TA/RA mode.
WARNING: On aircraft with operational predictive windshear, failure
to place the transponder to TA or TA/RA prior to taking the
runway will prevent operation of the radar in the
windshear mode unless the radar is selected to an active
mode.
Shoulder Harnesses (Flow) ..........................................................................ON
Each flight crewmember shall, during takeoff and landing keep their
shoulder harness fastened.
Note: > Update FMC to runway threshold on the TAKEOFF REF page of
the FMC/CDU. Depressing the (5R) key and then executing the update
is the only way to drive the FMC position to the departure end of the
runway.
Note: > Depressing TOGA will not automatically update the aircraft
position.
Sec. 3 Page 108 737
Rev. 11/15/02 #41 Continental Flight Manual
INTENTIONALLY LEFT BLANK
737 Sec. 3 Page 109
Flight Manual Continental Rev. 11/15/02 #41
　
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