BUS TIE switches -AUTO
Verify ISLN lights extinguished.
GENERATOR CONTROL switches -ON
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
Copyright . The Boeing Company. See title page for details.
December 19, 2000 D6-30151-425 NP.20.3
Normal Procedures -Amplified Procedures 747 Operations Manual
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.
Allfuelpump 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.
Copyright . The Boeing Company. See title page for details.
NP.20.4 D6-30151-425 December 19, 2000
Normal Procedures -Amplified Procedures
Anti-ice panel ......................................................................................Set
NACELLE ANTI-ICE switches -AUTO WING ANTI-ICE switch -AUTO Windshield protectionpanel................................................................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
Copyright . The Boeing Company. See title page for details.
April 01, 2001 D6-30151-425 NP.20.5
Normal Procedures -Amplified Procedures 747 Operations Manual
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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本文鏈接地址：747-441 Operations Manual 747操作手冊(38)
