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Monitor rollout progress and proper autobrake operation. 
Verify Thrust levers closed and Speedbrake lever up. Without delay, raise Reverse Thrust levers to idle detent, hold light pressure until release, and then apply reverse thrust as required.  Verify Speedbrake lever UP and call “SPEEDBRAKES UP.” If Speedbrake lever not UP, call “SPEEDBRAKES NOT UP.” 
By 60 knots, initiate movement of Reverse Thrust levers to reach reverse idle detent prior to taxi speed. Position levers full down (forward thrust) when engines have decelerated to reverse idle.  Call “60 KNOTS.” 
Prior to taxi speed, disarm autobrakes and continue manual braking as required. 
Disengage autopilot prior to runway turnoff. 

WARNING: After reverse thrust is initiated, a full stop landing must be made.
After Landing Procedure
Accomplish this procedure when clear of the active runway.
STROBE lights switch ......................................................................OFF
INBOARD landing lights switches...................................................OFF
APU selector .........................................................START, release to ON
WEATHER radar switch ...................................................................OFF
Speedbrake lever ................................................................................ DN
Flap lever ............................................................................................. UP
AUTOBRAKES selector...................................................................OFF

Copyright . The Boeing Company. See title page for details.
NP.20.24 D6-30151-425 December 19, 2000

Normal Procedures -Amplified Procedures 747 Operations Manual
Transponder mode selector ............................................................ STBY

Shutdown Procedure
Parking brake.......................................................................................Set

Electrical power ......................................................................... Establish If external power desired: External power 1 and/or external power 2 AVAIL lights -Illuminated
EXTERNAL POWER 1 and/or EXTERNAL POWER 2 switches -Push
Verify ON light(s) illuminated.
If APU power desired:
APU generator 1 and APU generator 2
AVAIL lights -Illuminated
APU GENERATOR 1 switch -Push

Verify ON light illuminated.
APU GENERATOR 2 switch -Push
Verify ON light illuminated.

Hydraulic demand pump 1, 2, and 3 selectors.................................. OFF
Hydraulic demand pump 4 selector ................................................. AUX
FUEL CONTROL switches ...................................................... CUTOFF

SEATBELTS signs selector .............................................................. OFF When all passenger doors are in manual mode, place SEATBELT signs selector OFF.
Fuel pump switches .......................................................................... OFF
NACELLE and WING ANTI-ICE switches..................................... OFF
BEACON lights switch..................................................................... OFF
FLIGHT DIRECTOR switches ........................................................ OFF

Copyright . The Boeing Company. See title page for details.
December 19, 2000 D6-30151-425 NP.20.25
Normal Procedures -Amplified Procedures

Status messages..............................................................................Check
Parking brake ...............................................................................Release

When wheel chocks in place, release parking brake. Hydraulic demand pump 4 selector...................................................OFF Accomplish SHUTDOWN checklist down to “SECURE”.
Secure Procedure
IRS mode selectors............................................................................OFF

EMERGENCY LIGHTS switch .......................................................OFF

AFT CARGO HEAT switch..............................................................OFF

Pack control selectors........................................................................OFF

APU selector and/or EXTERNAL POWER switch(es)....................OFF

STANDBY POWER selector ............................................................OFF

When APU has completed shutdown cycle:
BATTERY switch.........................................................................OFF

Accomplish remaining items on SHUTDOWN checklist.
Copyright . The Boeing Company. See title page for details.
NP.20.26 D6-30151-425 December 19, 2000
Takeoff

. Accelerate to EconomyAcceleration Height
　
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本文鏈接地址：747-441 Operations Manual 747操作手冊(44)