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no customers near the door area. The door is normally opened by
rotating the door knob in either direction. It is the responsibility of the
individual who opens the door, to close the door immediately after
transit.
ENHANCED FLIGHT DECK DOOR (If Installed)
Note: THE DOOR WILL AUTOMATICALLY LOCK WHEN IT IS
CLOSED anytime the aircraft is operating on normal electrical power.
If the door does not electrically lock after closing or if there is an internal system
failure, the red UNLKD light will illuminate. The crew must investigate the
problem and take corrective action, including use of the mechanical lock if
necessary to secure the door.
The door will be left open / unlocked by the flight crew when departing the
aircraft after the flight. If the door is inadvertently closed (and therefore
automatically locked) either a pilot or maintenance technician may use the
FLIGHT DECK EMERGENCY ENTRANCE system to gain access.
737 Sec. 3 Page 87
Flight Manual Continental Rev. 11/15/02 #41
>>@ TAXI FLOW
Sec. 3 Page 88 737
Rev. 11/15/02 #41 Continental Flight Manual
BCD TAXI FLOW
737 Sec. 3 Page 89
Flight Manual Continental Rev. 11/15/02 #41
TAXI
Once the AFTER START checklist is complete, and the Captain is confident
that the area around the aircraft is clear, the Captain will call “FLAPS____,
TAXI CLEARANCE.” The First Officer will select the required flaps and
obtain a taxi clearance.
The Captain will call for the TAXI checklist when clear of congestion. The
TAXI flow will be initiated when the Captain calls for the checklist.
Caution: Outside vigilance during taxi is the responsibility of both pilots.
Prior to the aircraft movement or flap movement, both pilots
should verify that the aircraft is clear of all obstacles.
F/O CHALLENGE TAXI F/O RESPOND
Takeoff Briefing....................................................................COMPLETED
Flight Controls...........................................................................CHECKED
Speedbrake Lever..................................................DOWN DETENT (F,C)
Flaps .......................................................SET____, GREEN LIGHT (F, C)
Autobrake...............................................................................................RTO
CDU / Airspeed Bugs .................................................................. SET (F, C)
Trim.............................................................................................SET, ZERO
F/O Challenge F/O Respond
Takeoff Briefing........................................................................COMPLETED
Prior to the first leg of the trip series, the Captain will conduct a complete
departure briefing. This briefing should include, as applicable, a review of
the following areas:
· Weather and takeoff alternate
· Runway conditions and required lighting
· SID Departure routing and chart date
- Displays and automation modes
- Frequencies / courses
- Altitudes
· Rejected takeoff / evacuation procedures
· Engine out procedures
· Air return considerations
- Runway / Weight
· Non-normal and MEL inoperative equipment considerations
· Terrain considerations
737
Flight Manual Continental
Sec. 3 Page 90
TR 03-02 01/20/03
If EGPWS is installed, use the TERR feature on the EFIS control panel
for departure from any airport with significant terrain features. This
feature should be considered for use even in day VFR conditions. The
TERR function cannot be displayed with weather radar. Consider
using weather radar on one display and terrain on another when faced
with a weather / terrain situation.
If EGPWS is not installed, consider using radar to help identify
prominent terrain features.
· Transition Altitude
· 10-7 and 10-9 Pages
Whenever practical, it is recommended that the departure briefing be
completed at the gate or earlier.
For subsequent flights with the same crew the Captain may substantially
abbreviate the briefing. However, any changes or items peculiar to the
specific departure should be thoroughly reviewed.
Flight Controls ............................................................................... CHECKED
BC Per Airworthiness Directive 2002-08-20 / AMOC 120S-02-907:
“After any ground deicing / anti-icing of the horizontal stabilizer using Type II or
Type IV fluids, airspeed must be limited to 270 KIAS until the flight crew has
been informed that applicable maintenance procedures have been accomplished
that would allow exceedance of 270 KIAS. Once the applicable maintenance
　
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