OVERRIDE pumps 2 and 3 switches -Off
CROSSFEED valve 1 and 4 switches -Off
Cancel when review completed. Status Display ................................................................................ Select Trim ..................................................................................................... Set
Stabilizer trim – ___ UNITS
Set for takeoff.
Check in illuminated greenband.
Aileron trim – ZERO Rudder trim – ZERO Flight controls ................................................................................Check
Copyright . The Boeing Company. See title page for details.
NP.20.16 D6-30151-425 December 19, 2000
Normal Procedures -Amplified Procedures 747 Operations Manual
Displace rudder, control wheel, and control column
full travel in both directions. Verify freedom of
movement, controls return to center, and proper
flight control movement on secondary EICAS display.
Note: Hold nose wheel steering tiller stationary during rudder check to prevent nose wheel movement. Secondary ENGINE display switch .................................................Push Verify secondary engine display appears.
EICAS displays ............................................................................. Check Engine indications -Normal Accomplish remaining items on BEFORE START checklist.
Copyright . The Boeing Company. See title page for details.
December 19, 2000 D6-30151-425 NP.20.17
Normal Procedures -Amplified Procedures
Engine Start Procedure
Normal start sequence is 4, 3, 2, 1.
Two engines may be started simultaneously.
Captain First Officer
Call “START ____ .” Pull engine start switch(es).
Position engine ____ fuel control switch(es) to run.
Observe oil pressure increase. *
Monitor engine displays for start parameters listed below until engine(s) are stabilized at idle: . N1 rotation and *oil pressure must be indicated by idle N2. After engine(s) stabilized at idle, repeat procedure to start remaining engines. Autostart takes corrective action for the following non-normal conditions: .No EGT rise .Hot start . Hung start. (*During cold weather starts, initial oil pressure rise may be higher than normal.)
Copyright . The Boeing Company. See title page for details.
NP.20.18 D6-30151-425 December 19, 2000
Normal Procedures -Amplified Procedures 747 Operations Manual
After Start Procedure
APU selector ..................................................................................... OFF
Hydraulic demand pump selectors ................................................AUTO
NACELLE ANTI–ICE switches............................................As required
AFT CARGO HEAT switch .................................................. As required
Pack control selectors ...................................................................NORM
RECALL switch ...............................................................................Push
Verify only appropriate alert messages displayed.
Cancel when review completed. CDU ............................................................................................... Check
Verify takeoff speeds selected.
Ground equipment ........................................................................... Clear
Accomplish AFTER START checklist.
Before Takeoff Procedure
Pilot Flying Pilot Not Flying
Obtain taxi clearance
Brief taxi clearance
Release parking brake.
Call for “FLAPS _____” as required for takeoff. Position Flap lever to takeoff setting.
Accomplish takeoff briefing.
Notify flight attendants.
Call for “BEFORE TAKEOFF CHECKLIST”. Accomplish BEFORE TAKEOFF checklist.
Copyright . The Boeing Company. See title page for details.
December 19, 2000 D6-30151-425 NP.20.19
Normal Procedures -Amplified Procedures 747 Operations Manual
Takeoff Procedure
Pilot Flying Pilot Not Flying
Align airplane with runway. Position Inboard Landing Lights and Strobe Light switches ON. Position Transponder Mode selector to TA/RA.
Advance Thrust levers to approximately 70% N1 and allow engines to stabilize. Push TO/GAswitchtoadvance Thrust levers to takeoff thrust, or manually advance Thrust levers to takeoff thrust.
Verify correct takeoff thrust set. Monitor engine instruments throughout takeoff. Adjust takeoff thrust prior to 80 knots if required.
Note: After takeoff thrust is set, Captain’s hand must be on Thrust levers until V1.
Verify 80 knots. Call “80 KNOTS.”
Monitor airspeed noting V1. Rotate at VR. Establish positive rate of climb. Call “V1.” At VR, call “ROTATE.” Monitor airspeed and vertical speed.
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