747-441 Operations Manual 747操作手册(50)

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Adjust speed as desired. 
Call for “FLAPS ____” according to flap extension schedule.  Position Flap lever as directed. 
Use VNAV, V/S, or FLCH mode for altitude changes. 
Use LNAV or heading select mode to track the approach or to establish intercept course for localizer or localizer back course approach. 
Select LOC when on intercept course for localizer approach. 
Approaching final approach fix, call for “GEAR DOWN” and “FLAPS 20”.  Position Landing Gear lever DN and Flap lever to 20. 
Position Speedbrake lever to ARM. 
Set intermediate altitude constraint or MDA (or closest 100 foot increment below). 

Copyright . The Boeing Company. See title page for details.
SP.4.10 D6-30151-425 April 01, 2001

Supplementary Procedures -Automatic Flight 747 Operations Manual
Pilot Flying (Cont)  Pilot Not Flying (Cont) 
Prior to final approach fix, call “FLAPS ____” as required for landing.* (*If circling, selection of landing flaps may be delayed until turning final.)  Position Flap lever as directed. 
Call for “LANDING CHECKLIST”.  Accomplish LANDING CHECKLIST. 
Use VNAV or select V/S mode and appropriate vertical speed to descend to MDA. 
In descent, set intermediate altitude constraints and MDA (or closest 100 foot increments below). 
If using VNAV: Prior to MDA, set or call for missed approach altitude in ALT window. At or above MDA and landing, disengage autopilot and disconnect autothrottle.  Set missed approach altitude in ALT window if requested by pilot flying. 
If using V/S: At or slightly above MDA, select ALT HOLD. Set or call for missed approach altitude in ALT window. If landing, disengage autopilot and disconnect autothrottle before descending below MDA.  Set missed approach altitude in ALT window if requested by pilot flying. 

Copyright . The Boeing Company. See title page for details.
December 01, 1999 D6-30151-425 SP.4.11
Supplementary Procedures -Automatic Flight 747 Operations Manual

Intentionally
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Copyright . The Boeing Company. See title page for details.
SP.4.12 D6-30151-425 October 1, 2000

747 Operations Manual

Electrical Power Up
Accomplish the following procedure to permit safe application of electrical power.
BATTERY switch ...............................................................................ON Verify OFF light extinguished. STANDBY POWER selector.........................................................AUTO
Hydraulic DEMAND pump selectors............................................... OFF
ALTERNATE FLAPS selector ......................................................... OFF
Landing gear lever ..............................................................................DN

Flap position indication and flap lever ...........................................Agree Electrical power .........................................................................Establish BUS TIE switches – AUTO
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 Start Source switch -TR

APU selector – START, RELEASE TO ON
APU generator 1 and
APU generator 2 AVAIL lights -Illuminated
APU GENERATOR 1 switch -Push

Verify ON light illuminated.
Copyright . The Boeing Company. See title page for details.
April 01, 2001 D6-30151-425 SP.6.1
Supplementary Procedures -Electrical 747 Operations Manual

APU GENERATOR 2 switch -Push
Verify ON light illuminated.

Standby Power Test
Airplane must be on ground with all busses powered.
STANDBY POWER selector ............................................................BAT Verify EICAS advisory messages BAT DISCH MAIN and BAT DISCH APU display. Messages may take up to 3 minutes to display.
STANDBY POWER selector ........................................................ AUTO Verify BAT DISCH MAIN and BAT DISCH APU messages no longer display.
Copyright . The Boeing Company. See title page for details.
SP.6.2 D6-30151-425 April 01, 2001

747 Operations Manual

Engine Continuous Ignition
Continuous ignition must be on when operating in:
.
moderate to heavy rain

.
hail or sleet

.
moderate to severe turbulence

.
volcanic ash

.
upon entering icing conditions Use standby ignition if continuous ignition is not available. To manually select continuous ignition:

CONTINUOUS IGNITION switch ................................................... ON Confirm CON IGNITION ON memo message is displayed.
　
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