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Verify OFF and DRIVE lights illuminated.
HYDRAULIC panel ............................................................................Set
Hydraulic SYS FAULT and
demand pump PRESS lights - Illuminated
DEMAND pump selectors - OFF
ENGINE pump switches - ON
Verify engine pump PRESS lights illuminated.
EMERGENCY LIGHTS switch................................................ ARMED
OBSERVER’S AUDIO SYSTEM switch ....................................NORM
SERVICE INTERPHONE switch .................................................... OFF
FUEL TRANSFER MAIN 1 AND 4 switch .................................... OFF
Fire Panel .............................................................................................Set
December 19, 2000
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
NP.20.4 D6-30151-425
Normal Procedures -
Amplified Procedures
Engine fire switches - In
BTL A DISCH and BTL B DISCH
lights - Extinguished
APU BTL DISCH light - Extinguished
APU fire switch - In
CARGO FIRE DISCH light - Extinguished
CARGO FIRE ARM switches - OFF
Verify FWD and AFT lights extinguished.
Engine START panel ........................................................................... Set
START switches - In, extinguished
STANDBY IGNITION selector - NORM
CONTINUOUS IGNITION switch - Off
AUTO IGNITION selector - SINGLE
AUTOSTART switch - ON
FUEL JETTISON panel ...................................................................... Set
Fuel jettison selector - OFF
Fuel jettison NOZZLE valve switches - Off
Verify VALVE light extinguished.
Fuel panel ............................................................................................ Set
All X FEED valve switches - On
Verify VALVE lights extinguished.
All fuel pump switches - Off
Main pump PRESS lights illuminated.
Main 2 aft pump PRESS light
extinguished when APU running.
Override 2 and 3 pumps, center pumps,
and stabilizer pumps PRESS lights
extinguished.
December 19, 2000
747 Operations Manual
Normal Procedures -
Amplified Procedures
Copyright © The Boeing Company. See title page for details.
D6-30151-425 NP.20.5
Anti-ice panel ......................................................................................Set
NACELLE ANTI-ICE switches - AUTO
WING ANTI-ICE switch -AUTO
Windshield protection panel ................................................................Set
WINDOW HEAT switches - ON
Verify INOP lights extinguished.
Windshield WIPER selectors - OFF
PASSENGER OXYGEN switch...........................NORM (guard closed)
YAW DAMPER switches ...................................................................ON
INOP lights remain iluminated until first IRU aligns.
CABIN ALTITUDE panel ...................................................................Set
OUTFLOW VALVES - OPEN
Verify outflow valves OPEN.
LANDING ALTITUDE switch - AUTO
Outflow valve manual switches - Off
Cabin Altitude AUTO SELECTOR - NORM
ECS panel ............................................................................................Set
PASSENGER TEMPERATURE selector - AUTO
FLIGHT DECK TEMPERATURE selector - AUTO
ZONE SYS FAULT light - Extinguished
TRIM AIR switch - ON
UPPER and LOWER RECIRCULATION fan switches - ON
AFT CARGO HEAT switch - Off
EQUIPMENT COOLING selector - NORM
HIGH FLOW switch - Off
Bleed air panel .....................................................................................Set
April 01, 2001
747 Operations Manual
Copyright © The Boeing Company. See title page for details.
NP.20.6 D6-30151-425
Normal Procedures -
Amplified Procedures
Pack SYS FAULT light - Extinguished
Pack control selectors - NORM
LEFT and RIGHT ISOLATION valve switches - On
Verify VALVE lights extinguished.
Engine bleed air SYS FAULT lights - Extinguished
APU bleed air switch - ON
Verify VALVE light extinguished.
ENGINE BLEED air switches - ON
Lighting panel ..................................................................................... Set
First Officer’s FLIGHT DIRECTOR switch ...................................... ON
STATUS display switch.................................................................... Push
Verify status display appears.
EFIS control panel .............................................................................. Set
CDU ...................................................................................Check and set
IDENT page - Check
Verify airplane model number
　
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