05 Normal Procedures 747 400 v10

NORMAL PROCEDURES 5 - 1

PMDG 747-400 AOM DO NOT DUPLICATE Revision – 26JUL05

NORMAL PROCEDURES

TABLE OF CONTENTS

SUBJECT PAGE

NORMAL PROCEDURES ....................................................................................3FIRST OFFICER’S FLIGHT DECK PREFLIGHT .....................................................................3CAPTAIN’S FLIGHT DECK PREFLIGHT.................................................................................8CAPTAIN’S FLIGHT DECK PREFLIGHT.................................................................................9FINAL COCKPIT PREPARATION ......................................................................................... 10PUSHBACK AND START...................................................................................................... 11ENGINE START.................................................................................................................... 12AFTER START...................................................................................................................... 13TAXI OUT.............................................................................................................................. 13TAKEOFF.............................................................................................................................. 14AFTER TAKEOFF ................................................................................................................. 15CLIMB ................................................................................................................................... 15CRUISE................................................................................................................................. 15INITIAL APPROACH ............................................................................................................. 16FINAL APPROACH ............................................................................................................... 16TAXI IN.................................................................................................................................. 16PARKING AND SHUTDOWN................................................................................................ 17LEAVING AIRCRAFT ............................................................................................................ 17

5 - 2 NORMAL PROCEDURES

Revision – 26JUL05 DO NOT DUPLICATE PMDG 747-400AOM

THIS PAGE INTENTIONALLY BLANK



NORMAL PROCEDURES

OVERVIEW: The following sets of procedures follow step by step through the processesrequired to fly the PMDG 747-400. These normal procedures are divided by major flight phaseand should provide a basic guideline for accomplishing the major procedures required duringflight. Although these checklists do not need to be removed from the manual and followed on astep by step basis, crews are encouraged to develop a pattern of behavior which ensures that allof the following steps are accomplished in the correct order and format. Use of the in flightchecklist procedures (bolded checklist steps) is required of crewmembers.

In the interest of containing operating costs, external ground power should be used during theinitial cockpit preparation. This will allow the crew to delay APU start until immediately beforedeparture. In circumstances where the quality of an external power connection is an issue, orwhen ground based aircraft cooling is not available, crews may elect to start the APU at theirdiscretion in the interest of preserving an on-time departure and passenger climate comfort.

In Cold Weather Operations crews should ensure that the cockpit has not been set up foraircraft deicing operations by ground crew. If this is determined to be the case, crews areadvised not to begin cockpit preparation until clearing their actions with the ground crew in orderto prevent damage to the aircraft or injuries to ground personnel.

FIRST OFFICER’S FLIGHT DECK PREFLIGHT(If aircraft is already powered, start below dashed line.)BATTERY SWITCH ................................................................................................................ONSTANDBY POWER SELECTOR ........................................................................................AUTOHYDRAULIC DEMAND PUMP SELECTORS ........................................................................OFFEXT PWR SWITCHES 1 & 2 (If Available).................................................................................ON If no EXT Power Available: INBD CRT SELECTOR ………………………………………………………………EICASALTERNATE FLAP SELECTOR ..........................................................................................OFFLANDING GEAR LEVER ...................................................................................................DOWNFLAP POSITION INDICATOR AND FLAP LEVER ..........................................................AGREEAPU BLEED SWITCH ...........................................................................................................OFFAPU (IF NEEDED) ...........................................................................................................START

Rotate APU selector to START, then release to ON. After APU has spooled up and is running,APU GENERATOR 1 and or 2 AVAIL lights will illuminate. Push APU GENERATOR 1 and or 2switches. Do not select or de-select both simultaneously. Verify ON light illuminates and AVAILlight extinguishes.

APU GEN SWITCHES ..............................................................................................VERIFY ONELECTRONIC ENGINE CONTROL SWITCHES NORM Verify ALTN lights extinguished and guards are closed.IRS SELECTORS ………………………………………………………OFF, then NAV, then ALIGN Set switches to NAV when IRS Align time counters reach 0 on Nav Display.



ELECTRICAL PANEL EICAS ELEC PAGE ………………………………………………………………………….DISPLAY L, R UTILITY BUS SWITCHES..............................................................................................ON Verify OFF light extinguished. BUS TIE SWITCHES ......................................................................................................AUTO Verify ISLN lights extinguished. GEN CONT SWITCHES......................................................................................................ON Verify OFF and DRIVE lights illuminated.NAV LIGHTS ..........................................................................................................................ON

For safety, Nav lights should remain illuminated whenever aircraft has functioning electrical powerprovided by APU, ground power, or engine generators. If operating only on battery power, NavLights should be selected OFF.

BATTERY .........................................................................................................................CHECKRotate the Standby Power selector to BAT and verify the BAT DISCH or BAT DISCH APUmessage appears on the EICAS and the OFF light does not illuminate. Rotate the selector toAUTO and verify the EICAS message is cleared and the OFF light does not illuminate.

HYDRAULIC PANEL: EICAS HYD PAGE ………………………………………………………………………….DISPLAY Hydraulic SYS FAULT and demand pump PRESS lights ILLUMINATED

HYD DEMAND PUMP SELECTORS 1-4 ………………………………………………………..OFF HYD ENG PUMP SWITCHES 1 - 4.......................................................................................ON

EMERGENCY LIGHTS SWITCH ………………………………………………ARMED (guard closed)

FIRE CONTROL PANEL: 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: ENGINE START SELECTORS 1 - 4 ...........................................IN, LIGHTS EXTINGUISHED STANDBY IGNITION SELECTOR ...............................................................................NORM CONTINUOUS IGNITION SWITCH ..................................................................................OFF AUTO IGNITION SWITCH ..........................................................................................SINGLE AUTOSTART SWITCH ......................................................................................................ON

FUEL JETTISON PANEL EICAS FUEL PAGE ………………………………………………………………………….DISPLAY FUEL JETTISON SELECTOR ..........................................................................................OFF



L, R, JETTISON NOZZLE SWITCHES ...........................................OFF, NOT ILLUMINATED



FUEL PANEL:FUEL DISTRIBUTION AND TOTAL FUEL QUANTITY ................................................CHECK All XFEED Switches ………………………………………………………………………………..ON Verify VALVE lights extinguish FUEL PUMP SWITCHES .........................................................................................ALL OFF Verify PRESS lights illuminate on all eight MAIN pump switches. If APU is running, MAIN 2 AFT pump PRESS light will extinguish Verify PRESS lights are extinguished on:

MAIN2/3 OVRD PumpsCENTER L/R PumpsHORIZONTAL STAB L/R Pumps

ANTI ICE PANEL: EICAS ECS PAGE ………………………………………………………………………….DISPLAY NACELLE ANTI-ICE SWITCHES ……………………………………………………………OFF Verify VALVE lights extinguish. WING ANTI-ICE SWITCH ………………………………………………………………….OFF Verify VALVE lights extinguish. WINDOW HEAT SWITCHES ………………………………………………………………ON Verify INOP lights extinguished. WINDSHIELD WIPER SELECTORS ……………………………………………………..OFF

PAX OXYGEN SWITCH ………………………………………………………….NORM (guard closed)YAW DAMPER SWITCHES……………………………………………………………………………ON

CABIN ALTITUDE PANEL: OUTFLOW VALVES …………………………………………………………..VERIFY OPEN LANDING ALTITUDE SWITCH …………………………………………………………..AUTO OUTFLOW VALVE MANUAL SWITCHES …………………………………………………OFF CABIN ALTITUDE AUTO SELECTOR …………………………………………………..NORM

ECS Panel: PASSENGER TEMPERATURE SELECTOR ……………………………………………….AUTO FLIGHT DECK TEMPERATURE SELECTOR ………………………………………………..AUTO ZONE SYS FAULT light ……………………………………………………………EXTINGUISHED TRIM AIR SWITCH ………………………………………………………………………………..ON UPR, LWR RECIRC FAN SWITCHES ..............................................................................ON

If ground based cooling is being used during temperatures exceeding 85°F, LWR RECIRC FANshould be switched on at least 20 minutes prior to passenger boarding in order to evacuatewarmer air from lower deck E&E spaces.

AFT CARGO HEAT SWITCH …………………………………………………………………….OFF EQUIPMENT COOLING SELECTOR ………………………………………………………..NORM

If OAT is less than 70°F, set to NORM. If above 70°F, set to OVRD. HIGH FLOW SWITCH …………………………………………………………………………….OFF GASPER SWITCH ………………………………………………………………………………….ON



PNEUMATICS PANEL Pack SYS FAULT Light …………………………………………………………….EXTINGUISHED PACK SELECTORS 1, 2, AND 3 ..................................................................................NORM L, R ISLN SWITCHES ...................................................................................................OPEN Verify VALVE lights extinguished. Engine Bleed air SYS FAULT lights ……………………………………………….EXTINGUISHED APU BLEED SWITCH .......................................................................................................ON

Allow the APU to operate for at least one full minute before activating APU bleed switch. ENG BLEED SWITCHES ...................................................................................VERIFY ON

LIGHTING PANEL: COCKPIT LIGHTING …………………………………………………………………..AS DESIRED EXTERIOR LIGHTING LANDING LIGHTS INBD/OUTBD ……………………………………………………OFF RUNWAY TURN-OFF LIGHTS ……………………………………………………….OFF TAXI LIGHTS……………………………………………………………………………..OFF BEACON ………………………………………………………………………………..OFF NAV LIGHTS …………………………………………………………………..VERIFY ON STROBE …………………………………………………………………………………OFF WING LIGHTS …………………………………………………………………………..OFF LOGO LIGHTS ……………………………………………………………………………ON

SECONDARY EICAS STAT PAGE......................................................................................DISPLAYEICAS ADIVISORY/CAUTION/WARNING MESSAGES.......................................CHECK/ERASE

FMC-CDU:See FMC Guide (Chapter 12) for detailed FMC instructions.

IDENT PAGE.................................................................................................................SELECT Verify airplane model number and engine model number. Verify NAVDATA is current. (Download updates from www.navdata.at) POS INIT PAGE..............................................................................................................SELECT REFerence AIRPORT ENTER ICAO Set IRS Position ENTER UTC VERIFY ROUTE PAGE SELECT ORIGIN/DESTINATION ENTER ROUTE ENTER ACTIVATE PUSH EXEC key PUSH DEP/ARR PAGE DISPLAY Runway and SID for departure SELECT ROUTE PAGE DISPLAY SID and route VERIFY EXEC key PUSH NAV/RAD PAGE DISPLAY

http://www.navdata.at)



Navigation Radios VERIFY INIT REF PAGE DISPLAY

CENTER CONSOLE RADIOS:WEATHER RADAR AS DESIRED Note: Wx Radar Functionality not modeled.RADIO TUNING PANEL AS DESIREDAUDIO PANEL AS DESIREDAILERON AND RUDDER TRIM ..................................................................................SET ZERO

TRANSPONDER: TRANSPONDER MODE SELECTOR STANDBY ATC SWITCH TEST Verify TCAS System Test Passes. ATC SWITCH AS DESIRED

AUTOBRAKES SELECTOR RTOCLOCK VERIFY/SET AS DESIRED

CRT SELECTORS: LOWER CRT SELECTOR NORM INBOARD CRT SELECTOR NORM

GROUND PROXIMITY: Ground PROX light EXTINGUISHED Ground proximity FLAP OVERRIDE SWITCH OFF Ground proximity CONFIG/GEAR OVERRIDE SWITCH OFF Ground Proximity TERRAIN OVERRIDE SWITCH OFF

ALTERNATE FLAPS/GEAR: LANDING GEAR LEVER DOWN ALTERNATE FLAPS SELECTOR OFF ALTERNATE FLAPS ARM SWITCH OFF ALTERNATE GEAR EXTEND SWITCHES OFF

HEADING REFERENCE SELECTOR NORMSECONDARY EICAS ‘STAT’ PAGE DISPLAY Hydraulic Quantity Verify RF Not Displayed Oxygen Pressure Sufficient for Flight

EICAS CONTROL PANEL:CAUTION MESSAGES CANCEL



CAPTAIN’S FLIGHT DECK PREFLIGHTCAPTAIN’S EFIS CONTROL PANEL SET AS DESIRED

AUTOPILOT MODE CONTROL PANEL: FLIGHT DIRECTOR SWITCHES …………..…………………………………………………ON AUTOTHROTTLE ARM SWITCH .................................................................................... OFF BANK LIMIT SELECTOR........................................................................................AS DESIRED AUTOPILOT DISENGAGE BAR……………………………………………………………………UP HDG INDICATOR ............................................................................SET RUNWAY HEADING ALT INDICATOR ...............................................................SET INITIAL CLEARED ALTITUDE

FMC-CDU: ACTIVE NAVIGATION DATA CHECK POS INIT Key PUSH Present Position CHECK UTC CHECK ROUTE Line Select Key PUSH Route of Flight VERIFY INIT REF Key PUSH INDEX Line Select Key PUSH APPROACH Line Select Key PUSH FLAP/SPEED Line VERIFY BLANK INIT REF Key PUSH

CENTER CONSOLE: PARKING BRAKE SET SPEEDBRAKE LEVER DOWN REVERSE THRUST LEVERS DOWN FLAP LEVER SET Position Lever to Agree with Flap Position. FUEL CONTROL SWITCHES CUTOFF STABILIZER TRIM CUTOUT SWITCHES AUTO(Guards Closed) Stab Trim Cutout Function not modeled in this version. RADIO TUNING PANEL AS DESIRED AUDIO PANEL AS DESIRED

PASSENGER SIGNS: NO SMOKING SELECTOR AUTO or ON SEATBELTS SELECTOR AUTO or ON

CLOCK VERIFY/SET AS DESIRED

CRT SELECTORS: LOWER CRT SELECTOR NORM INBOARD CRT SELECTOR NORM



PRIMARY FLIGHT DISPLAY (Both Capt and FO): FLIGHT MODE ANNUNCIATION VERIFY Autothrottle Mode BLANK Roll Mode TO/GA Pitch Mode TO/GA Autopilot Flight Director Status FD

DISPLAYS NORMAL Verify no flags displayed. Verify no V SPD flag displayed until V-Speeds selected. HEADING BUG CHECK Verify matches AFDS MCP Window ALTIMETER SET

NAVIGATION DISPLAY (Both Captain and FO): HEADING/TRACK CHECK ROUTE DISPLAYED DISPLAY CHECK Verify no flags displayed.

FINAL COCKPIT PREPARATION

FUEL CHECK Verify Fuel Quantity in FMC-CDU, EICAS and your flight plan match.FMC ROUTE OF FLIGHT.....................................................................................................VERIFY RUNWAY, SID..............................................................................................................ENTER

On DEPARTURES pages select the runway and SID if applicable.FMC PERF INIT PAGE ZFW .............................................................................................................................ENTER RESERVES ..................................................................................................................ENTER COST INDEX ...............................................................................................................ENTER CRZ ALT.......................................................................................................................ENTERFMC THRUST LIM PAGE OAT ..............................................................................................................................ENTER THRUST RATING ........................................................................................SELECT, CHECK

Verify thrust rating N1% performance numbers are reflected on upper EICAS display.FMC TAKEOFF PAGE TAKEOFF FLAP SETTING ..........................................................................SELECT, VERIFY RUNWAY CONDITION .............................................................................ENTER WET/DRY TAKEOFF SPEEDS ................................................................................CONFIRM, VERIFYFMC VNAV CLB PAGE SPEED/TRANSITION ALT ..........................................................................................ENTER SPD/RESTR ...............................................................................................................ENTER

Enter clean maneuvering speed in the SPD/RESTR line for VNAV use below 3000 feet AGL.



MCP IAS/MACH INDICATOR ...............................................................................SET TOV2+10APU (IF NOT RUNNING) ................................................................................................START

Rotate APU selector to START, then release to ON. After APU has spooled up and is running,APU GENERATOR 1 and or 2 AVAIL lights will illuminate. Push APU GENERATOR 1 and or 2switches. Do not select or de-select both simultaneously. Verify ON light illuminates and AVAILlight extinguishes.

FUEL PUMPS AND OVERRIDE FUEL PUMPS..........................................................................ON Select Pumps ON only for tanks containing fuel.FUEL CROSSFEEDS................................................................................................................SET

If tank quantity 2 is more than 1 and tank 3 is more than 4: All crossfeeds ON.If tank quantity 2 is less\equal to 1 and tank 3 is less\equal to 4: Crossfeeds 1 & 4 OFF, Overridepumps 2 & 3 OFF

STAB TRIM ............................................................................................CHECK SET IN GREEN

SECONDARY EICAS DOORS PAGE DISPLAY Verify all doors secured.BEFORE START CHECKLIST ...................................................................................PERFORM

PUSHBACK AND START

DOORS CLOSED ............................................................................................................VERIFYPUSHBACK/START CLEARANCE ..................................................................................OBTAINBEFORE PUSHBACK CHECKLIST.............................................................................PERFORMPUSHBACK COMMUNICATIONS/GND SVC INTERCOM .............................................COMPLYHYDRAULIC DEMAND PUMP SELECTOR 4 ........................................................................AUXHYDRAULIC DEMAND PUMP SELECTORS 1-3 ................................................................AUTORED ANTI-COLLISION BEACON .....................................................................................BOTHPACK SELECTORS........................................................................................ONE ON or ALL OFFRECALL SWITCH PUSH Verify only appropriate alert messages displayed.SECONDARY EICAS ‘ENG’ DISPLAY.............................................................................DISPLAYEICAS CANCEL .................................................................................................................PUSH



ENGINE START

DUCT PRESSURE ......................................................................................................MONITORVerify that sufficient duct pressure exists for a normal engine start. Duct pressure should exceed 30 psiimmediately after ENGINE START SELECTOR is pulled. Duct pressures below this level increases theprobability of an abnormal or hot start. If duct pressure is low, close opposite side cross bleed valveSTART ENGINE NUMBER ____ .............................................................................ANNOUNCE Engines 1 & 4 and engines 2 & 3 may be started simultaneously.

AUTOSTART IN USE:FUEL CONTROL SWITCH ____ .........................................................................................RUNENGINE START SELECTOR .......................................................PULL, VERIFY ILLUMINATIONENGINE INDICATIONS ..............................................................................................MONITOR

Monitor N2 indication for engine rotation and observe oil pressure indication. Maximum motoring isreached when N2 stops increasing for five seconds. At 25% N2 or maximum motoring, whichever isless, but not less than the N2 start bar:

EICAS ENGINE INDICATIONS ..................................................................................MONITORAt approximately 50% N2:

ENG START SELECTOR ...........................................VERIFY ILLUMINATION EXTINGUISHEDAfter starter cutout and RPM stabilization of engine:START ENGINE NUMBER ____ ..................................................REPEAT FOR ALL ENGINES Engines 1 & 4 and engines 2& 3 may be started simultaneously.

MANUAL START:ENGINE START SELECTOR .......................................................PULL, VERIFY ILLUMINATIONFUEL CONTROL SWITCH ____ .........................................................................................RUN Verify N2% RPM has reached magenta start line before introducing fuel.ENGINE INDICATIONS ..............................................................................................MONITOR

Monitor N2 indication for engine rotation and observe oil pressure indication. Maximum motoring isreached when N2 stops increasing for five seconds. At 25% N2 or maximum motoring, whichever isless, but not less than the N2 start bar:

EICAS ENGINE INDICATIONS ..................................................................................MONITORAt approximately 50% N2:

ENG START SELECTOR ...........................................VERIFY ILLUMINATION EXTINGUISHEDAfter starter cutout and RPM stabilization of engine:START ENGINE NUMBER ____ ..................................................REPEAT FOR ALL ENGINES Engines 1 & 4 and engines 2& 3 may be started simultaneously.



AFTER START

APU SELECTOR ...................................................................................................................OFFIf extended delays are anticipated which may require engine shutdown, leave APU running.

HYDRAULIC DEMAND PUMP SELECTOR 4 ......................................................................AUTOENG ANTI-ICE SWITCHES ..................................................................................AS REQUIRED If <10C with visible moisture, turn Engine Anti-Ice ON.AFT CARGO HEAT AS REQUIRED

PNEUMATICS L/R ISOLATION SWITCHES .......................................................................................OPEN PACK SELECTORS 1, 2, AND 3 ..................................................................................AUTO

Ensure engines have stabilized at idle for at least 2Min prior to engaging packs.EICAS RCL SWITCH .......................................................................................................CHECKRELEASE FROM PUSHBACK/GND SVC ........................................................................VERIFYFLAPS ...................................................................................................................................SETAFTER START/TAXI CHECKLIST..............................................................................PERFORM

TAXI OUT

SECONDARY EICAS STAT DISPLAY ...........................................................................DISPLAYFLIGHT CONTROLS .......................................................................................................CHECK

Move rudder and control column through full range of motion, verify flight control range of motion bywatching the flight control indicators on the display.

SECONDARY EICAS ENG MODE .................................................................................SELECTTAKEOFF PERFORMANCE ........................................................................................CONFIRM

Verify takeoff performance speeds to determine if still acceptable. If aircraft weight changed duringboarding/departure period, ensure that PERF INIT page has been updated and is accurate.

VNAV CLB PAGE ..........................................................................................................DISPLAYCABIN CREW TAKEOFF NOTIFICATION ....................................................................PROVIDEWhen cleared onto active runwayEICAS CAUTION/ADVISORY AND STATUS MESSAGES ...............RECALL/CANCEL/CHECK

Ensure all cautionary messages have been addressed prior to takeoff.PACKS …………………………………………………………………………………..AS DESIRED/REQUIREDBEFORE TAKEOFF CHECKLIST ...............................................................................PERFORM



TAKEOFF

LANDING LIGHTS ...................................................................ON FOR INCREASED VISIBILITYSTROBE LIGHTS ...................................................................................................................ONHDG INDICATOR ..................................................................................................................SET

Set assigned departure heading or runway heading.CONTINUOUS IGNITION .......................................................................................................ONPARKING BRAKE ........................................................................................VERIFY RELEASEDTAKEOFF THRUST ..............................................................................................................SET

Takeoff thrust can be set manually, or by advancing throttles beyond 70% N1 and pressing the TO/GAbutton. If the EICAS warning CONFIG is received early in the takeoff roll, discontinue the takeoff andcorrect the problem, which will be displayed on the upper EICAS.

ENGINE INDICATIONS ...............................................................................................MONITORAIRSPEED 80 KNOTS .............................................................................................ANNOUNCEAIRSPEED V1 ...........................................................................................................ANNOUNCEAIRSPEED Vr ..........................................................................................................ANNOUNCEINITIAL CLIMB .........................................................................................................ESTABLISHPOSITIVE RATE OF CLIMB ...........................................................................................VERIFYVertical speed indicator and radio altimeter will register a positive rate of climb prior to the main gearleaving the runway. As such, crews are advised to refrain from retracting the landing gear until at least a500 feet per minute rate of climb is registered on the vertical speed indicator.GEAR ......................................................................................................................................UP



AFTER TAKEOFF

HDG MODE/L NAV MODE ..............................................................................................SELECTTurn the HDG select knob to the desired heading or reset the heading and press to activate.Alternately, push the L NAV switch and verify that L NAV is annunciated on the PFD.

AUTOPILOT....................................................ENGAGE AS DESIRED ONCE ABOVE 250 FEETFLAPS ..............................................................................................RETRACT ON SCHEDULEV NAV MODE .................................................................................................................SELECT

Verify CLB is displayed as the thrust limit on the upper EICAS display and the throttles adjust to aclimb setting. Set the IAS/MACH indicator on the MCP to at least the clean maneuvering speed.

When above 1200 feet AGL:ENG START SELECTOR ...................................................................................................AUTOANTI-ICE SWITCHES .........................................................................................................AUTOCONTINUOUS IGNITION ....................................................................................AS REQUIREDLANDING GEAR LEVER ......................................................................................................OFFPACK CONTROL SELECTORS 1, 2, AND 3 ....................................................................NORMAFTER TAKEOFF CHECKLIST .................................................................................PERFORM

CLIMB

CLEARED ALTITUDE ................................................................VERIFY SET IN MCP WINDOWWING/ENGINE ANTI-ICE .....................................................SELECT AS REQUIRED OR AUTOL NAV (IF NOT ALREADY SELECTED) .......................................................................SELECT

When cleared to resume own navigation, select L NAV and ensure that L NAV is displayed on the PFD.ECON CLB .........................................................................................................VERIFY ACTIVE

Observe ACT ECON CLB page displayed on VNAV CLB page or selected MCP speed if applicablewhen passing through 10,000 ft. Commanded speed should agree with displayed flight performance.

CABIN SIGNS .....................................................................................................AS REQUIREDWhen passing transition altitudeALTIMETERS ..........................................SET AND ANNOUNCE QNE (29.92 In Hg or 1013hPa)After passing FL180LANDING LIGHTS .................................................................................................................OFF

CRUISE

LEVEL OFF .................................................................................................................PERFORMFLIGHT PROGRESS, PERFORMANCE AND NAVIGATION .......................................MONITORFUEL SYSTEM ............................................................................................................MONITORARRIVALS PROCEDURE ......................................................................ENTER AS REQUIRED

On ARRIVALS page, enter as much of the expected arrival procedure as possible. Verify routing usingthe MAP mode on the ND.



INITIAL APPROACH

ATIS ...............................................................................................................................OBTAINAPPROACH BRIEFING ........................................................................................ACCOMPLISHDH AND MDA BUGS ........................................................................................CHECK AND SETLANDING DATA ..............................................................................................CHECK AND SET

Determine correct REF speed for the planned landing weight and flap setting. Verify values againstFMC computed values, the adjust or accept FMC computed figures.

SEATBELT SELECTOR ..........................................................................................................ONEICAS RECALL ................................................................................................................CHECKAUTOBRAKES SELECTOR ................................................................................AS REQUIRED

See landing techniques section for detailed information regarding the use of the autobrakes.At FL180:WING LIGHTS .....................................................................................................AS REQUIREDWhen passing through transition level:ALTIMETERS ..................................................................................SET AND ANNOUNCE QNHFLAPS ..................................................................................................................AS REQUIRED

Expect varying speed vectors during the approach phase of the flight. When a flap level is selected, setMCP speed to the flap maneuver speed +10 knots. Do not use the flaps as air brakes to slow theaircraft; rather, slow the aircraft using appropriate throttle input and extend the flaps according to theflap deployment schedule displayed on the PFD.

APPROACH CHECKLIST ...........................................................................................PERFORM

FINAL APPROACH

AUTOFLIGHT SYSTEMS .....................................................................................AS REQUIREDLOCALIZER CAPTURE ...................................................................ANNOUNCE AS REQUIREDLANDING GEAR ........................................................................................DOWN AND VERIFYSPEED BRAKE ....................................................................................................................ARMFINAL APPROACH CHECLIST .................................................................................PERFORMGLIDE SLOPE CAPTURE ................................................................ANNOUNCE AS REQUIREDMCP MISSED APPROACH ALTITUDE .................................................................................SETAUTOFLIGHT SYSTEM (AS REQUIRED) ....................................................................MOINTORAUTOLAND OPERATION (IF USED) ...........................................................................MONITOR

TAXI IN

SPOILERS ................................................................................................VERIFY RETRACTEDAUTO BRAKES SELECTOR .................................................................................................OFFWhen clear of the active runway:LANDING LIGHTS .................................................................................................................OFFWHITE ANTI-COLLISION LIGHTS .......................................................................................OFFAUTOTHROTTLE ARM SWITCH .........................................................................................OFFFLIGHT DIRECTOR SWITCH ..............................................................................................OFF



FLAPS .........................................................................................................................RETRACTSTABILIZER TRIM ..........................................................................................................4 UNITSWEATHER RADAR ................................................................................................................OFFAPU ......................................................................................................................AS REQUIREDENGINE AND WING ANTI-ICE SWITCHES .........................................................................OFF

PARKING AND SHUTDOWN

PARKING BRAKE .................................................................................................................SETSEATBELT SELECTOR ........................................................................................................OFFENGINE BLEED SWITCHES ................................................................................................OFFObserve VALVE lights illuminateIf APU OFF Perform Next Line:GROUND/EXTERNAL POWER GEN ................................................WHEN AVAIL, SELECT ONIf APU ON Perform Next Line:APU GEN CTRL SWITCHES 1 AND 2 ......................................................................SELECT ONAfter completing APU ON/APU OFF sections from above:FUEL CONTROL SWITCHES 1, 2, 3, 4 (IN ORDER) ....................................................CUTOFFHYDRAULIC PUMPS ...........................................................................................................OFFFUEL PUMP SWITCHES .....................................................................................................OFFRED ANTI-COLLISION LIGHT SWITCH ...............................................................................OFFEXTERIOR LIGHTS ...........................................................................................AS REQUIREDSECONDARY EICAS STATUS DISPLAY ........................................................................SELECTEQUIPMENT COOLING SELECTOR ....................................................................................SET

If OAT is less than 70°F, set to NORM. If above 70°F, set to OVRD.PNEUMATICS PANEL APU BLEED SWITCH .......................................................................................................ON L AND R ISLN SWITCHES ............................................................................................OPENPARKING CHECKLIST ..............................................................................................PERFORM

LEAVING AIRCRAFT

PNEUMATIC PANEL PACK SELECTORS ........................................................................................................OFF UPR AND LWR RECIRC FANS ........................................................................................OFF APU BLEED SWITCH ......................................................................................................OFFAPU SELECTOR ..................................................................................................................OFF Allow APU to run without bleed or generator load for at least 1 minute before shutting down.STBY POWER SELECTOR ...................................................................................................OFFBAT SWITCH .......................................................................................................................OFF

05 Normal Procedures 747 400 v10

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Transcript of 05 Normal Procedures 747 400 v10