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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).
Pilot Flying Pilot Not Flying
April 01, 2001
747 Operations Manual
Supplementary Procedures -
Automatic Flight
Copyright © The Boeing Company. See title page for details.
D6-30151-425 SP.4.11
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.
December 01, 1999
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
SP.4.12 D6-30151-425
Supplementary Procedures -
Automatic Flight
Intentionally
Blank
October 1, 2000
747 Operations Manual
Supplementary Procedures Chapter SP
Electrical Section 6
Copyright © The Boeing Company. See title page for details.
D6-30151-425 SP.6.1
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.
April 01, 2001
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
SP.6.2 D6-30151-425
Supplementary Procedures -
Electrical
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.
April 01, 2001
747 Operations Manual
Supplementary Procedures Chapter SP
Engines, APU Section 7
Copyright © The Boeing Company. See title page for details.
D6-30151-425 SP.7.1
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
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