737 Operations Manual
PITOT STATIC HEAT switches .......................................................OFF WING and ENGINE ANTI–ICE switches .......................................OFF VALVE OPEN lights – Extinguished Hydraulics ....................................................................................Normal Note: Alert ground personnel before pressurizing hydraulic
system.
System A HYDRAULIC PUMPS switches – ON
System B HYDRAULIC PUMPS switches – ON
Electric pump LOW PRESSURE lights – Extinguished
Brake pressure – 2800 PSI minimum
System A and B pressure – 2800 PSI minimum
Quantity indicators – Above RFL
Pressurization indicators ................................................................Check Cabin differential pressure – Zero Cabin altitude – Field elevation Cabin rate of climb – Zero
Exterior light switches ............................................................ As desired
Ignition select switch .............................................................IGN L or R
Alternate ignition select switch on subsequent starts. ENGINE START switches ................................................................OFF NAV switch (as installed)...................................................... As required
Select FMC, ANS-L or ANS-R position, as appropriate for navigation system to be used for departure.
Mode control panel ............................................................................. Set When selecting a value on the MCP, ensure the corresponding display on the instrument panel changes, if applicable.
COURSE(S) – Set and crosscheck
Copyright . The Boeing Company. See title page for details.
NP.20.10 June 4, 2004
Normal Procedures -Amplified Procedures
FLIGHT DIRECTOR switches – ON
Position the switch for the pilot flying to ON first.
AUTOTHROTTLE switch – OFF
Heading – Runway heading
Bank angle limit – as desired
Altitude – as desired
Autopilots – DISENGAGE
Marker Beacon Switch (as installed) .......................................As desired Clock....................................................................................................Set Left flight instruments .........................................................................Set Note: IRS alignment must be complete.
EFIS – Correct
A/T, Pitch and ROLL FMA’s - Blank
A/P STATUS FMA - FD
Flight instrument indications are correct.
Verify no flags displayed.
Altimeter - Set
MAP – Correct
Verify no flags displayed.
Route - Displayed, correct.
Standby instruments ...................................................................... Check Standby horizon – Set Erect horizon and verify proper attitude. Standby altimeter/airspeed indicator – Set Set altimeter and verify airspeed is zero.
Normal Procedures -Amplified Procedures 737 Operations Manual
NOSE WHEEL STEERING switch (as installed) ................................................................................. NORM
Light controls .......................................................................... As desired
Fuel quantity indicators..................................................................Check Test IAW the supplementary procedure.
Fuel flow switch (Non-EIS) ............................................................ Reset N1 manual set knobs ........................................................................Press Permits FMC control of the N1 cursors. Engine Instruments ........................................................................Check Primary and secondary engine indications - Normal
.
engine indications display existing conditions
.
no exceedance values are displayed
.
engine oil quantity meets dispatch requirements
ENG OIL QTY TEST switch (Non-EIS airplanes) ......................................................................... Push
Verify both indicators move toward zero and return to the original setting when the switch is released.
Fuel used reset switch (EIS)............................................................Reset
ANTISKID switch ............................................................................. ON Verify ANTISKID INOP light extinguished.
AUTO BRAKE select switch........................................................... RTO AUTOBRAKE DISARM light – extinguished
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