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MSFS 2024 · Airliner
PMDG 747-400 Startup Checklist
PMDG 747-400 Startup Notes
Unlike the 777, the 747-400 has no autostart, so all four engines are on you. Get both APU generators connected, enter your position and give the IRS units the roughly ten minutes they need to align, and configure the fuel pumps for your load. For each start, pull the start switch, let N2 rise to maximum motoring, then move the fuel control switch to RUN while watching EGT. The airplane has enough duct pressure to spin two starters, so starting in pairs is normal.
Most botched starts come from rushing the fuel. Introducing fuel at low N2 gives a hot, slow start, and with four engines you get four chances to do it wrong. Leaving the packs running starves the starters of bleed air, so check duct pressure before pulling the switch. Electrical setup catches people too: the APU drives two generators and both need to be connected, and an IRS alignment skipped or entered with the wrong position will ruin the flight before taxi.
Common mistakes
- Introducing fuel before N2 reaches maximum motoring speed
- Connecting only one of the two APU generators
- Leaving packs on and starving the starters of duct pressure
Related Aircraft
Pilot Tools for This Flight
FLIGHT2.17.0Checklist
PMDG 747-400MSFS 2024 · Startup Checklist · 215 steps · 19 phases
PHS 1 - Pre-Flight Planning8 steps
| 01 | Weather Briefing (METAR / TAF / SIGMET)REVIEWEDNOTE: Check departure, destination, alternates and enroute weather. Long-range 747-400 routes normally require more than one alternate. | |
| 02 | NOTAMsREVIEWEDNOTE: Check runway closures, approach procedure changes and nav-aid outages at origin, destination and alternates. | |
| 03 | Fuel PlanCALCULATEDNOTE: Fuel is loaded symmetrically wing to wing. All main tanks carry approximately the same load until the outboard mains (1 and 4) are full, then the inboard mains (2 and 3) are filled. Reserve tanks 2 and 3 stay empty until the inboard mains hold about 40,000 lb each, and the centre wing tank is filled last. | |
| 04 | Weight and Balance / Load ManifestWITHIN LIMITSCAUTION: 747-400 certified weights: max taxi 397,800 kg (877,000 lb), max takeoff 396,893 kg (875,000 lb), max landing 285,762 kg (630,000 lb), max zero fuel 246,754 kg (544,000 lb). The 747-400F and the 910K increased gross weight versions are higher - always use the AFM figures for your model. | |
| 05 | Operating LimitsNOTEDNOTE: VMO/MMO 375 KCAS / Mach 0.92. Maximum operating altitude 45,100 ft pressure altitude. Minimum flight crew two pilots. | |
| 06 | Takeoff PerformanceCALCULATEDNOTE: Compute the takeoff flap setting, assumed temperature if a reduced thrust takeoff is planned, and V1, VR and V2. Four-engine acceleration height is normally 3,000 ft and thrust reduction height is normally 1,500 ft. | |
| 07 | OFP / RoutingREVIEWEDNOTE: Review each waypoint, crossing altitude and the planned step climb profile before loading the FMC. | |
| 08 | ATIS and ATC ClearanceOBTAINEDNOTE: Obtain ATIS and the ATC clearance before the Captain calls for the Before Start checklist. |
PHS 2 - Preliminary Cockpit Preparation16 steps
| 01 | FuelCHECKNOTE: Captain item. Verify fuel quantity and distribution are correct for the planned flight. If fuelling is still in progress, delay the check until it is complete. | |
| 02 | Hydraulic QuantityCHECKNOTE: Verify the hydraulic quantity indications on the Status page do not display RF. | |
| 03 | Oxygen PressureCHECKNOTE: Check crew and supernumerary oxygen pressure is sufficient for the planned flight. Refer to the Minimum Oxygen Dispatch Pressure tables if crew oxygen is low. | |
| 04 | Engine Oil QuantityCHECKNOTE: Verify the engine oil quantity indications on the secondary ENG display are shown in white. Magenta indications require maintenance. | |
| 05 | Battery SwitchONNOTE: First Officer item, accomplished when APU or external power is not already powering the aircraft. Verify the OFF light extinguishes. | |
| 06 | Standby Power SelectorAUTO | |
| 07 | Hydraulic Demand PumpsOFF | |
| 08 | Windshield WipersOFF | |
| 09 | Alternate Flaps SelectorOFF | |
| 10 | Landing Gear LeverDOWN | |
| 11 | Flap Lever and Position IndicationAGREENOTE: On standby power the left inboard and outboard trailing edge flap indications are displayed with an amber X. | |
| 12 | Electrical PowerESTABLISHNOTE: Bus Tie switches AUTO, then EXT PWR 1 switch ON and EXT PWR 2 switch ON, verifying the ON lights illuminate. Alternatively start the APU and select APU GEN 1 and APU GEN 2 ON after the AVAIL lights illuminate. | |
| 13 | APU Selector (if APU required)START, THEN ONCAUTION: Ensure the APU area is clear, rotate the selector to START and release to ON. Do not allow the APU selector to spring back to the ON position. | |
| 14 | IRS Mode SelectorsOFF, THEN NAVCAUTION: A full alignment is required for all originating flights and for flights requiring long-range navigation. Do not accept an IRS alignment made by maintenance or another crew - if the IRSs are not OFF on arrival at the aircraft, turn the mode selectors OFF then back to NAV. | |
| 15 | Smoke Evacuation HandleCLOSED | |
| 16 | Overhead Circuit BreakersCHECK |
PHS 3 - Cockpit Preparation - First Officer42 steps
| 01 | ELT SwitchARMEDNOTE: Verify the ON light is extinguished. If it is illuminated, verify the switch is in ARMED, press TEST/RESET and advise ATC of the unintentional activation. | |
| 02 | Elec Engine Control SwitchesNORMNOTE: Verify the ALTN lights are extinguished. | |
| 03 | Electrical PanelSETNOTE: Standby Power Selector AUTO, Utility Power switches ON (OFF lights out), Battery switch ON (OFF light out), Bus Tie switches AUTO (ISLN lights out), Generator Control switches ON (OFF and DRIVE lights illuminated). | |
| 04 | Hydraulic PanelSETNOTE: Demand Pump selectors OFF, verifying all SYS FAULT and demand pump PRESS lights illuminate. Engine Pump switches ON, verifying all engine pump PRESS lights illuminate. | |
| 05 | Emergency Light SwitchARMED | |
| 06 | Audio System SwitchesNORMNOTE: Captain and observer audio system switches NORM. Service interphone switch OFF. | |
| 07 | Fuel Xfer Main 1 and 4 SwitchOFF | |
| 08 | Fire PanelSETNOTE: Engine fire switches IN, BTL A DISCH and BTL B DISCH lights extinguished, APU BTL DISCH lights extinguished, APU fire switch IN, Cargo Fire ARM switches OFF with the FWD and AFT lights extinguished, and the Cargo Fire DEPRESS and DISCH lights extinguished. | |
| 09 | Engine Start PanelSETNOTE: Start switches IN with the lights extinguished, Standby Ignition selector NORM, Continuous Ignition switch OFF, Auto Ignition selector SINGLE, Autostart switch ON. | |
| 10 | Fuel Jettison PanelSETNOTE: Fuel Jettison selector OFF and Fuel Jettison Nozzle switches OFF, verifying the VALVE lights are extinguished. | |
| 11 | Fuel PanelSETNOTE: All crossfeed valve switches ON with the VALVE lights extinguished, and all fuel pump switches OFF. Verify the main tank pump PRESS lights illuminate, and that the OVRD 2 and 3 pump and CTR tank pump PRESS lights are extinguished. | |
| 12 | Fuel SynopticCHECKNOTE: Select the Fuel synoptic and check for proper fuel quantity and distribution to identify any gross fuelling error. Fuel temperature variations can make tank quantities read above or below tank capacity and should not be read as improper distribution. | |
| 13 | Anti-Ice PanelSETNOTE: Nacelle Anti-ice switches OFF and Wing Anti-ice switch OFF, with the VALVE lights extinguished. | |
| 14 | Windshield Protection PanelSETNOTE: Window heat switches ON with the INOP lights extinguished, windshield wiper switches OFF. | |
| 15 | Exterior LightingSETNOTE: Landing light switches OFF, runway turnoff light switches OFF, taxi light switch OFF. Beacon OFF, NAV ON, Strobe OFF, Wing OFF. | |
| 16 | Supernumerary Oxygen SwitchNORMNOTE: Guard closed. | |
| 17 | Yaw Damper SwitchesONNOTE: The INOP lights remain illuminated until the first IRU is aligned. | |
| 18 | Cabin Altitude PanelSETNOTE: Landing Altitude switch AUTO, Outflow Valve Manual switches OFF, Cabin Altitude AUTO selector NORM. When manual is selected, MAN is displayed in amber at the bottom of the primary EICAS. | |
| 19 | ECS PanelSETNOTE: Flight deck and lower lobe temperature selectors AUTO, Zone SYS FAULT light extinguished, Trim Air switch ON, Equipment Cooling selector NORM, Pack High Flow switch OFF, Pack Reset SYS FAULT light extinguished. | |
| 20 | Bleed Air PanelSETNOTE: Pack selectors NORM, left and right isolation switches ON with the VALVE lights extinguished, engine bleed SYS FAULT lights extinguished, APU bleed switch ON with the VALVE light extinguished, engine bleed switches ON. The engine bleed OFF lights stay illuminated until after engine start. | |
| 21 | F/D SwitchON | |
| 22 | EFIS Control PanelSETNOTE: Clear the minimums displays, set the barometric reference selector to inches or hectopascals as required and set QNH, ND mode selector MAP, ND traffic switch ON, WXR OFF. TCAS OFF will be displayed in amber on the ND until IRS alignment is complete. | |
| 23 | Alternate Flaps and GearSETNOTE: Alternate Flaps selector OFF, Alternate Flaps Arm switch OFF, Alternate Gear Extend switches OFF. | |
| 24 | Landing Gear LeverDOWN | |
| 25 | EICAS EIU SelectorAUTONOTE: Heading Reference switch NORM, Master FMC selector LEFT. | |
| 26 | Primary EICASCHECKNOTE: Press Recall and review the EICAS alert messages. Contact maintenance if messages are displayed which are not normal for the preflight condition. Verify the primary engine indications show existing conditions with no exceedance, then review the EICAS memo messages. | |
| 27 | Secondary EICASCHECKNOTE: Verify the secondary engine indications show no exceedance and the oil quantity is displayed in white. Check the Status display shows only expected messages - if others are displayed, contact maintenance and refer to the MEL. | |
| 28 | CDU IDENT PageCHECKWARNING: An RNAV or GPS procedure shall not be used if doubt exists as to the validity or accuracy of the database procedure.NOTE: Verify the aircraft model and engines are correct and the active navigation database is current. The database cycle begins at 0901 UTC on the published effective date. | |
| 29 | CDU POS INIT PageSETNOTE: Enter the departure airport on line 2L and the present position on the SET IRS POS line using the most accurate source available - GPS POS, the gate position from the Jeppesen 10-10 page, or manually entered ramp coordinates. Verify UTC time is correct on line 4L. | |
| 30 | Radio Tuning Panels (Left, Centre, Right)SETNOTE: Verify the OFF lights and the offside tuning lights are extinguished. Verify VHF C is selected with DATA displayed in the active frequency window. Do not operate HF radios during or near fuelling operations. | |
| 31 | Seat Belt Sign SelectorOFF | |
| 32 | Weather RadarSET/TESTNOTE: Select the R/T switch on the side corresponding to the Pilot Flying, tilt approximately +4 deg, gain full clockwise, TFR and GCS switches off, mode WX or WX+T. Run the test, observe the test pattern on the ND, then switch the EFIS WXR switch and the WX RDR TEST switch off. | |
| 33 | ACARSINITIALIZENOTE: Initialize ACARS using the centre CDU. | |
| 34 | Rudder TrimSETNOTE: Verify rudder trim is set to zero. | |
| 35 | TransponderSETNOTE: XPNDR selector Left, mode selector STBY. | |
| 36 | Smoke Goggles and Oxygen MaskCHECKNOTE: Mask stowed, oxygen ON flag out of view, Normal/100% switch at 100%, Emergency/Test selector at EMER. Test the mask and verify the crew oxygen indication on the Status display decreases no more than 30 PSI during the test. | |
| 37 | Source Select PanelSETNOTE: Flight Director source Right, Navigation source FMC Right, EIU source AUTO, IRS source Right, Air Data source Right. CRT select panel: lower CRT selector NORM, inboard CRT selector NORM. | |
| 38 | Navigation DisplayCHECKNOTE: IRS alignment must be complete before checking the PFD and ND. Compare the ND heading to the standby compass and the PFD heading. Verify TCAS OFF is the only flag displayed. | |
| 39 | Primary Flight DisplayCHECKNOTE: Verify NO VSPD is the only flag, TO/GA is the engaged pitch and roll mode, airspeed indicates 30 knots, QNH is set with STD not displayed, and the altitude display is within 75 feet of field elevation and within RVSM tolerance of the other pilot's display. | |
| 40 | ClockCHECKNOTE: SET selector in RUN, date and time correct. Correct time is essential to the accuracy of position reports. | |
| 41 | Gnd Proximity PanelCHECKNOTE: GND PROX light extinguished, FLAP OVRD switch off, GEAR OVRD switch off, TERR OVRD switch off. | |
| 42 | Seat and Rudder PedalsADJUSTWARNING: Do not place objects between the pilot's seat and the aisle stand. Injury can occur when the seat is adjusted. |
PHS 4 - FMC Initialization8 steps
| 01 | ROUTE PageSETNOTE: Enter the origin and destination airports and the flight number exactly as listed on the flight plan. Enter the route manually or select the company route, verify it is correct, then ACTIVATE and EXECUTE. | |
| 02 | DEP/ARR PageSETNOTE: Select the runway, SID and transition as appropriate and execute. Select the STAR and transition if applicable and execute. Return to the Route page and verify the runway and route are correct. | |
| 03 | LEGS PageSETNOTE: Verify the route and all altitude and speed constraints are correct. | |
| 04 | ROUTE DATA PageSETNOTE: Enter flight plan forecast winds for the enroute waypoints. Forecast wind entries are recommended for all flights that exceed 2 hours. | |
| 05 | PERF INIT PageSETWARNING: The FMC fuel reserve is a tool that can provide a reminder of fuel state but should not be used as the sole determinant for fuel-related decision making.NOTE: Verify the fuel displayed on line 2L agrees with the fuel on board shown on the primary EICAS. Enter 0.0 in the RESERVES line, then the cost index and cruise altitude from the OFP. Change STEP SIZE to 2,000 feet if FMC-based step climbs are planned, or to zero if no step climb is planned. | |
| 06 | VNAV CLB PageSETNOTE: Verify the proper transition altitude is displayed for the departure airport on line 3R and modify if necessary. | |
| 07 | NAV/RAD PageSETNOTE: Verify the VHF NAV radios are not manually tuned (M displayed) unless required for departure. Pre-select the VOR and course for departure and set the ADFs if required. | |
| 08 | PROGRESS PageCHECKNOTE: Compare the FMC flight plan distance to the OFP distance for reasonability. If the difference is excessive, use the Jeppesen charts to reconcile the discrepancy. |
PHS 5 - Cockpit Preparation - Captain25 steps
| 01 | EFIS Control PanelSETNOTE: Clear the minimums displays, set the barometric reference and QNH, ND mode selector MAP, ND traffic switch ON, WXR OFF. The PF map range is normally 5 or 10 NM. | |
| 02 | Mode Control PanelSETNOTE: F/D switch On, A/T Arm switch On, heading set to runway heading or the initial clearance heading, Bank Angle selector AUTO, altitude set to the initial clearance altitude, autopilot disengage bar Up, AFDS mode switches set as desired for departure. | |
| 03 | Primary EICASCHECKNOTE: Press Recall, review the alert messages, verify the primary engine indications show no exceedance, then review the memo messages. | |
| 04 | Secondary EICASCHECKNOTE: Select the Fuel synoptic and check fuel quantity and distribution. Check the Status display shows only expected messages and the hydraulic quantities do not display RF. | |
| 05 | Integrated Standby Flight DisplaySETNOTE: Verify a normal display with no flags, airspeed indicating 30 knots, HP/IN as required and BARO set to QNH, altitude agreeing with field elevation, and heading compared to the standby compass and ND. Do not press the ISFD ATT RST switch unless the ATT:RST message is displayed. | |
| 06 | CDU IDENT, POS INIT and ROUTE PagesCHECKNOTE: Verify the aircraft model and engines, current navigation database, departure airport on line 2L, GPS POS showing current position, UTC on line 4L, and that the route is correct, activated and executed. | |
| 07 | CDU DEP/ARR, LEGS and PERF INIT PagesCHECKNOTE: Verify the departure runway, SID, STAR and transitions, the route and its altitude and speed constraints, and the fuel, reserves, cost index and cruise altitude. | |
| 08 | SATCOM Link StatusTESTNOTE: If Satcom data capability is required for the flight, conduct the link status test. | |
| 09 | ADSARMNOTE: If ADS will be used during the flight, verify the ADS mode indicates ARM on the ATC LOGON/STATUS page. | |
| 10 | Parking BrakeSETWARNING: Do not assume the parking brake will prevent aircraft movement. Accumulator pressure may be insufficient to prevent aircraft movement.CAUTION: Verify the PARK BRAKE SET memo message on the primary EICAS. If the brake accumulator indicates less than approximately 800 PSI, maintenance action is required. | |
| 11 | Speedbrake LeverDOWNWARNING: Do not pressurize any hydraulic system until the area around the aircraft has been cleared. | |
| 12 | Reverse Thrust LeversDOWN | |
| 13 | Forward Thrust LeversCLOSED | |
| 14 | Flap LeverVERIFY AGREES WITH FLAP POSITIONWARNING: Do not operate flaps without ground clearance. Serious personal injury could result.NOTE: The flaps are retracted if no flap indication is displayed on the primary EICAS. | |
| 15 | Fuel Control SwitchesCUTOFFNOTE: Check the fuel control switch fire warning lights are extinguished. | |
| 16 | Stab Trim Cutout SwitchesGUARD CLOSEDNOTE: Alternate stab trim switches NEUTRAL. | |
| 17 | Captain's Audio PanelSET | |
| 18 | Weather RadarSET/TESTNOTE: Left tilt selector approximately +4 deg, left gain full clockwise, TFR and GCS switches off, mode WX or WX+T. Run the test, then switch the EFIS WXR switch and the WX RDR TEST switch off. | |
| 19 | Smoke Goggles and Oxygen MaskCHECKNOTE: Mask stowed, oxygen ON flag out of view, Normal/100% switch at 100%, Emergency/Test selector at EMER, and the mask tested with crew oxygen dropping no more than 30 PSI. | |
| 20 | Source Select PanelSETNOTE: Flight Director source Left, Navigation source FMC Left, EIU source AUTO, IRS source Left, Air Data source Left. CRT select panel lower and inboard selectors NORM. | |
| 21 | ClockCHECKNOTE: SET selector in RUN, date and time correct. | |
| 22 | Navigation Display and Primary Flight DisplayCHECKNOTE: Heading compared to standby compass, TCAS OFF the only flag on the ND, departure runway and active route displayed on the map. On the PFD verify NO VSPD is the only flag, TO/GA engaged, airspeed 30 knots, QNH set and altitude within 75 feet of field elevation. | |
| 23 | Brake Source LightILLUMINATEDNOTE: The BRAKE SOURCE light is illuminated when hydraulic systems 4, 1 and 2 are depressurized. | |
| 24 | AutobrakesRTONOTE: Verify the AUTOBRAKES RTO memo message is displayed on the primary EICAS. | |
| 25 | Seat and Rudder PedalsADJUSTWARNING: Do not place objects between the pilot's seat and the aisle stand. Injury can occur when the seat is adjusted. |
PHS 6 - Final Cockpit Preparation9 steps
| 01 | PERF INIT Page - ZFW and Takeoff CGCOMPLETEWARNING: Inadvertent entry of ZFW into the GR WT field on the PERF INIT page will result in takeoff speeds being calculated for a much lower weight than the actual takeoff weight.NOTE: This procedure is accomplished after weight and balance information has been received and the crew is ready for engine start or pushback. The load manifest is the official record for weight and balance data and must be verified against the FMC values. Both pilots verify the ZFW and GR WT displayed on the PERF INIT page. | |
| 02 | THRUST LIM PageSETNOTE: Select the takeoff thrust reference limit. Enter the assumed temperature into line 1L if an assumed temperature takeoff is planned. | |
| 03 | TAKEOFF REF PageSETNOTE: Enter the takeoff flap setting, the four-engine acceleration height (normally 3,000 feet), the engine-out acceleration height, and the thrust reduction height and flap setting (normally 1,500 feet). Enter the tailwind component and positive runway slope if applicable. Entry of headwind and negative slope is optional. | |
| 04 | Takeoff CGENTERED AND VERIFIEDNOTE: The Captain verbalizes the takeoff CG from the load manifest and the First Officer enters and verifies it. The FMC only accepts whole numbers - round 0.5 and above up and 0.4 and below down. | |
| 05 | V-SpeedsV1, VR AND V2 SELECTEDNOTE: The Captain enters or line-selects V1, VR and V2. If a V1 correction is required for clutter or an inoperative anti-skid, the Captain manually enters the corrected V1 speed. | |
| 06 | CDU DisplaysSETNOTE: The Pilot Flying normally displays the TAKEOFF REF page for takeoff while the Pilot Monitoring displays the LEGS page. | |
| 07 | MCPSETNOTE: The Captain sets V2 in the MCP speed window and verifies VNAV and/or LNAV are armed for takeoff as appropriate. | |
| 08 | Crew Entry DoorCLOSENOTE: The Captain closes the crew entry door after the load supervisor leaves the aircraft. | |
| 09 | Doors SynopticSELECT / DOORS CLOSEDNOTE: Select the Doors synoptic, verify all doors are closed and locked, and leave the Doors synoptic displayed. |
PHS 7 - Before Start Checklist12 steps
| 01 | Departure BriefingCOMPLETENOTE: Read by the First Officer, response by the Captain. The briefing covers the aircraft log and MEL limits, taxi routing, CRM, rejected takeoff considerations, the engine out procedure and acceleration height and turn procedure, GR WT, thrust setting and N1, flap setting, NADP, EOAH, thrust reduction and V speeds, departure runway and SID, initial heading and constraints, roll and pitch modes, initial altitude, navaids, minimum safe altitude and terrain, and WX or TERR selection. | |
| 02 | OxygenCHECKEDNOTE: Verify each oxygen system has been tested and the Normal/100% switch is set to 100%. | |
| 03 | Flight InstrumentsCHECKED AND SET FOR DEPARTURENOTE: Verify all IRSs are aligned, the PFD and ND headings agree with the standby compass, and the altimeters are set to QNH. Each pilot crosschecks the other pilot's altitude display and the ISFD. | |
| 04 | Altimeters___ IN (hPa), ___ FT, SETNOTE: Respond with the altimeter setting and confirmation that all instruments are properly set. | |
| 05 | MCPV2 ___, HDG ___, ALT ___ | |
| 06 | Takeoff SpeedsV1 ___, VR ___, V2 ___NOTE: Verbalize the takeoff speeds while verifying V1, VR and V2 on the TAKEOFF REF page. Verify V1 and V2 are displayed on the PFD and V2 is in the MCP speed window. | |
| 07 | Fuel Quantity___ PLANNED, ___ CHECKEDNOTE: Respond with the fuel on board shown on the primary EICAS and the takeoff fuel listed on the flight release, and verify the two agree. | |
| 08 | Fuel Control SwitchesCUTOFF | |
| 09 | Parking BrakeSETNOTE: Verify the PARK BRAKE SET memo message is displayed on the primary EICAS. | |
| 10 | AutobrakesRTONOTE: Verify the AUTOBRAKES RTO memo message is displayed on the primary EICAS. | |
| 11 | Passenger SignsON / AS DESIRED | |
| 12 | Upper Deck Emergency DoorsARMEDNOTE: First Officer response. Verify the door operating handles are down and the door mode select levers are set as required. |
PHS 8 - Before Pushback Checklist7 steps
| 01 | CabinREADY | |
| 02 | DoorsCLOSEDNOTE: Verify all doors indicate closed and locked on the Doors synoptic. | |
| 03 | Demand Pumps#4 AUX AND AUTO | |
| 04 | BeaconBOTH | |
| 05 | RecallCHECKEDNOTE: Verify only expected EICAS alert messages are displayed. | |
| 06 | Trim___ UNITS, 0, 0NOTE: Verify the stabilizer trim is set for takeoff and that rudder and aileron trim are zero. | |
| 07 | TransponderSET / TCAS OFF |
PHS 9 - Engine Start8 steps
| 01 | Engine Start ClearanceOBTAINEDNOTE: Confirm the area around the aircraft is clear before pressurizing any hydraulic system or starting engines. | |
| 02 | Autostart SwitchONNOTE: Verify the autostart switch is ON for engine start. | |
| 03 | Standby Ignition SelectorNORM | |
| 04 | Continuous Ignition SwitchOFF | |
| 05 | Auto Ignition SelectorSINGLE | |
| 06 | Start SwitchesIN, LIGHTS EXTINGUISHEDNOTE: Panel configuration before the start sequence begins. | |
| 07 | Fuel Control SwitchesCUTOFF UNTIL STARTNOTE: The fuel control switches are verified CUTOFF on the Before Start checklist and are moved to RUN as each engine is started. | |
| 08 | Engine IndicationsMONITOR ON EICASNOTE: Monitor the primary and secondary EICAS engine indications throughout each start. |
PHS 10 - After Start Checklist6 steps
| 01 | APUOFF | |
| 02 | Nacelle Anti-IceOFF / ONNOTE: Verify nacelle anti-ice is selected ON if icing conditions are present. | |
| 03 | Aft Cargo HeatONNOTE: First Officer response. | |
| 04 | RecallCHECKEDNOTE: Verify only expected EICAS alert messages are displayed. | |
| 05 | CDUsCHECKEDNOTE: Verify the route is properly entered, the CDU preflight is complete and the appropriate page is displayed for takeoff. | |
| 06 | Ground EquipmentCLEAR L, CLEAR RNOTE: Captain responds Clear L, First Officer responds Clear R. |
PHS 11 - Before Takeoff Checklist11 steps
| 01 | Flaps___ PLANNED, ___ CHECKEDNOTE: Verify the flap position agrees with the planned takeoff setting. | |
| 02 | Flight ControlsCHECKEDNOTE: Checked by both the Captain and the First Officer. | |
| 03 | T/O Departure ReviewCOMPLETENOTE: Called by the Pilot Flying. | |
| 04 | Runway and Runway Entry PointVERIFIED BY BOTH PILOTSNOTE: When cleared for lineup or takeoff, and before entering the departure runway, both pilots verify that the runway and the runway entry point are correct. | |
| 05 | Final ItemsCALLED BY CAPTAINCAUTION: The Final Items and the checklist must be completed before crossing the Hold Short line. | |
| 06 | CabinNOTIFIEDNOTE: Final Item. Notify the cabin to prepare for takeoff and verify the upper deck is secure. | |
| 07 | AutothrottlesARMEDNOTE: Final Item. | |
| 08 | WXR or TERRSELECTEDNOTE: Final Item. | |
| 09 | TransponderTA/RANOTE: Final Item. Position the transponder mode selector to TA/RA when entering the departure runway. | |
| 10 | RunwayRWY ___, VERIFIEDNOTE: Final Item. Verify the airplane heading agrees with the assigned runway heading. | |
| 11 | LightsSET FOR TAKEOFFNOTE: When cleared for takeoff the Captain sets the inboard LANDING light switches ON. When entering the departure runway the First Officer sets the STROBE light switch ON and uses other lights as needed. |
PHS 12 - Takeoff11 steps
| 01 | Thrust LeversADVANCE TO APPROXIMATELY 70% N1NOTE: Allow the engines to stabilize before pushing the TO/GA switch. | |
| 02 | TO/GA SwitchPUSH | |
| 03 | Takeoff ThrustVERIFY SETNOTE: The Pilot Monitoring monitors the engine instruments throughout the takeoff and calls out any abnormal indications, adjusting takeoff thrust prior to 80 knots as needed. During strong headwinds, if the thrust levers do not advance to the planned takeoff thrust, manually advance them before 80 knots. | |
| 04 | Thrust LeversCAPTAIN'S HAND ON UNTIL V1WARNING: After takeoff thrust is set, the Captain's hand must be on the thrust levers until V1. | |
| 05 | 80 Knots"80 KNOTS, THRUST SET" / "CHECK"NOTE: The Pilot Monitoring calls 80 knots with takeoff thrust set and HOLD indicated on the FMA. The Pilot Flying verifies 80 knots and calls CHECK, maintaining light forward pressure on the control column. | |
| 06 | V1"V1"NOTE: Called 5 knots prior to V1 - either the automatic callout or the Pilot Monitoring calls V1. | |
| 07 | VR"ROTATE" - ROTATE TOWARD 15 DEG PITCHNOTE: At VR the Pilot Monitoring calls ROTATE. The Pilot Flying rotates toward a 15 deg pitch attitude and follows the flight director commands after liftoff. | |
| 08 | Positive Rate of Climb"POSITIVE CLIMB"NOTE: The Pilot Monitoring verifies both the altimeter and vertical speed displays show a positive rate of climb with airspeed above V2. | |
| 09 | Landing GearUPNOTE: The Pilot Flying verifies a positive rate of climb on the altimeter and calls GEAR UP. The Pilot Monitoring sets the landing gear lever to UP. | |
| 10 | Roll ModeSELECT ABOVE 400 FT RADIO ALTITUDENOTE: Above 400 feet radio altitude the Pilot Flying calls for a roll mode as needed. The Pilot Monitoring selects or verifies the roll mode and verifies VNAV is engaged. | |
| 11 | Climb ThrustVERIFY SET |
PHS 13 - After Takeoff Checklist5 steps
| 01 | Acceleration HeightVERIFY ACCELERATIONNOTE: The Pilot Flying verifies acceleration at the acceleration height and calls FLAPS ___ according to the flap retraction schedule. The Pilot Monitoring positions the flap lever as directed and verifies the VNAV page is selected on the Pilot Flying's CDU. | |
| 02 | Flap Retraction ScheduleFOLLOWCAUTION: Above 309,000 kg limit bank angle to 15 deg with flaps up until reaching UP + 20 knots.NOTE: From takeoff flaps 20, select 10, 5, 1 then UP as the speed tape displays 10, 5, 1 and UP. From takeoff flaps 10, select 5, 1 then UP as the speed tape displays 5, 1 and UP. | |
| 03 | Landing Gear LeverOFF AFTER RETRACTION COMPLETENOTE: The Pilot Monitoring also verifies the air conditioning packs are operating. | |
| 04 | Landing GearUP AND OFFNOTE: Checked aloud by the Pilot Monitoring. The After Takeoff checklist is done at flaps up speed, after flap retraction is complete. | |
| 05 | FlapsUPNOTE: Checked aloud by the Pilot Monitoring. |
PHS 14 - Climb and Cruise9 steps
| 01 | Sterile CockpitCOMPLY BELOW 10,000 FTNOTE: Complete the After Takeoff checklist before starting the Climb and Cruise procedure. | |
| 02 | Inboard Landing and Turnoff LightsOFF ABOVE 10,000 FT | |
| 03 | Passenger SignsAS NEEDED | |
| 04 | AltimetersSET AND CROSSCHECKED TO STANDARDNOTE: At transition altitude, set and crosscheck the altimeters to standard. The Pilot Monitoring calls TRANSITION. | |
| 05 | 1,000 Feet Below Assigned Altitude"1,000 TO LEVEL OFF" | |
| 06 | Centre Tank Pumps - ClimbOFF AT FUEL LOW CTRNOTE: When the FUEL LOW CTR L or R message is shown and the tank quantity is approximately 3,200 kg in the climb (pitch 5 deg or greater), set both Centre L and R pump switches off. | |
| 07 | Centre Tank Pumps - CruiseON AT FUEL OVD CTRNOTE: When the FUEL OVD CTR L or R message is shown and the tank quantity is 1,800 kg or more in cruise (pitch less than 5 deg), set both Centre L and R pump switches ON. | |
| 08 | Centre Tank Pumps - Cruise DepletionOFF AT FUEL LOW CTRNOTE: When the FUEL LOW CTR L or R message is shown and the tank quantity is approximately 1,300 kg in cruise (pitch less than 5 deg), set both Centre L and R pump switches off. | |
| 09 | Cruise AltitudeMAINTAINCAUTION: Maximum operating altitude 45,100 ft pressure altitude. VMO/MMO 375 KCAS / Mach 0.92.NOTE: The Pilot Monitoring calls ALTITUDE for any deviation of plus or minus 100 feet from the assigned altitude. |
PHS 15 - Descent/Approach Checklist8 steps
| 01 | 1,000 Feet Above Assigned Altitude"1,000 TO LEVEL OFF" | |
| 02 | RecallCHECKEDNOTE: The Descent/Approach checklist is checked aloud by the Pilot Monitoring. | |
| 03 | Autobrakes___ SET (OFF) | |
| 04 | Landing DataVREF ___, MINIMUMS ___, SET | |
| 05 | Altimeters___ IN (hPa), PRESET (SET)NOTE: On reaching transition level the Pilot Monitoring calls TRANSITION, ___ (in/hPa) SET. | |
| 06 | WXR or TERRSELECTED | |
| 07 | Approach BriefingCOMPLETE | |
| 08 | Localizer / Course"LOCALIZER ALIVE" / "COURSE ALIVE"NOTE: Called when the localizer CDI starts its first positive movement from full deflection, or when the VOR or ADF bearing pointers are within 10 degrees of the inbound course. |
PHS 16 - Landing Checklist4 steps
| 01 | CabinNOTIFIEDNOTE: The Landing checklist is checked aloud by the Pilot Monitoring. | |
| 02 | SpeedbrakeARMED | |
| 03 | Landing GearDOWN | |
| 04 | FlapsSET, LANDING FLAP CONFIRMEDNOTE: The card prints 'Flaps ____' and the Pilot Monitoring responds with the actual landing flap setting, 25 or 30 on the 747-400. |
PHS 17 - After Landing Checklist11 steps
| 01 | Nacelle Anti-IceAS REQUIREDNOTE: The After Landing checklist is checked silently by the First Officer. | |
| 02 | Strobe LightsOFF | |
| 03 | WXR or TERROFF | |
| 04 | Flight DirectorsOFF | |
| 05 | AutothrottlesOFF | |
| 06 | SpeedbrakeDOWN | |
| 07 | FlapsUP | |
| 08 | Stab Trim6 UNITS | |
| 09 | TransponderSTBY / XPNDR | |
| 10 | AutobrakesOFF | |
| 11 | APUAS REQUIRED |
PHS 18 - Shutdown Checklist10 steps
| 01 | Fuel Control SwitchesCUTOFF | |
| 02 | Fuel PumpsOFF | |
| 03 | Nacelle Anti-IceOFF | |
| 04 | BeaconOFF | |
| 05 | Aft Cargo HeatOFF (ON)NOTE: First Officer response. | |
| 06 | TransponderSTBYNOTE: First Officer response. | |
| 07 | Parking BrakeRELEASED (SET) | |
| 08 | Demand PumpsOFF | |
| 09 | IRS SelectorsOFFNOTE: Left ON when Satcom is needed. | |
| 10 | Upper Deck Emergency DoorsDISARMEDNOTE: First Officer response. |
PHS 19 - Securing Checklist5 steps
| 01 | Emergency LightsOFF | |
| 02 | PacksOFF | |
| 03 | APU, EXT PowerOFF | |
| 04 | Standby PowerOFF | |
| 05 | BatteryOFF |