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MSFS 2024 · General Aviation
Hawker 800XP (FlightFX) Startup Checklist
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Hawker 800XP (FlightFX)MSFS 2024 · Startup Checklist · 280 steps · 24 phases
PHS 1 - Pre-Flight Planning9 steps
| 01 | Weather Briefing (METAR / TAF / SIGMET)REVIEWEDNOTE: If icing is expected on the approach, add 10 KIAS to the approach and landing speeds and 15 percent to the landing distance. The APU is not approved for use in icing conditions. | |
| 02 | NOTAMsREVIEWED | |
| 03 | Flight Plan / OFPLOADEDNOTE: The EFB SimBrief icon imports the OFP. Service ceiling 41,000 ft. | |
| 04 | Fuel PlanningBLOCK FUEL CALCULATEDCAUTION: The ventral tank must be completely full or completely empty for flight.NOTE: Maximum fuel 10,000 lb (1,474 US gal usable), about 1,500 lb of it in the ventral tank. The ventral tank can only be filled once each wing holds at least 3,450 lb. | |
| 05 | Weight and BalanceZFW, TOW AND CG SETNOTE: MRW 28,120 lb, MTOW 28,000 lb, MLW 23,350 lb, MZFW 18,450 lb. Typical basic operating weight 16,010 lb. | |
| 06 | Takeoff V-Speeds (V1 / VR / V2)CALCULATEDNOTE: From the manual's Takeoff V-Speed Tables. Sea level, 28,000 lb, flaps 0°, 15 °C: V1 127, VR 136, V2 144 KIAS, TOFL 5,377 ft. With engine anti-ice ON, add 10 °C to the OAT before entering the table. | |
| 07 | Takeoff N1CALCULATEDNOTE: Take Off N1 Percent Reference Tables, APR armed (not operating), cabin air OFF. | |
| 08 | SID / STAR / Approach ReviewBRIEFED | |
| 09 | Destination Landing DistanceREVIEWEDNOTE: Flaps 45°, sea level, dry, 23,350 lb: 4,420 ft required at VREF 127 kt (factored 1.67 dry, 1.92 wet). |
PHS 2 - Exterior - Covers, Pins and Chocks6 steps
| 01 | Wheel ChocksREMOVEDNOTE: Click a chock in walkaround mode, or use the Ground tab on the EFB. | |
| 02 | Pitot Covers (Both Sides)REMOVED | |
| 03 | Engine Covers (Front and Rear)REMOVED | |
| 04 | Instrument Covers and Safety PinsREMOVEDNOTE: Once removed, these can only be reinstalled from the EFB Ground tab. | |
| 05 | External PanelsCLOSED | |
| 06 | Cabin DoorAS REQUIREDNOTE: Opened and closed from the EFB Ground tab or its walkaround clickspot. |
PHS 3 - Before Start Checks10 steps
| 01 | REFUEL SwitchesALL OFFNOTE: Inside the top left panel above the forward luggage compartment / vestibule, across from the entry door, next to the cabin light control panel. | |
| 02 | Circuit BreakersSETNOTE: Circuit breakers are not currently simulated. | |
| 03 | Pump HandleSTOWEDNOTE: Left side of the pedestal, forward of the trim wheel. | |
| 04 | Landing GearSELECTOR DOWNCAUTION: Make sure the GEAR OVRD button is not pushed. | |
| 05 | BrakesPARK | |
| 06 | All TrimsCHECK AND SET | |
| 07 | Thrust Reverse LeversSTOW - POWER OFF | |
| 08 | HP COCKSCLOSE | |
| 09 | LP COCKSLEVERS UPNOTE: The two round red knobs under the guard labelled L.P. COCKS. | |
| 10 | X-FEED and TRANSFERLEVERS UP |
PHS 4 - Power Up - Battery or GPU10 steps
| 01 | GPU (GPU Power Up Only)SELECTED - GREEN CHECKMARKNOTE: Ground tab on the EFB. Skip for a battery-only power up. | |
| 02 | BATTON - GEAR 3 GREENS | |
| 03 | BATT ISOLATENORM | |
| 04 | BUS TIE OPEN Annunciator (Battery Power Up Only)CHECK ILLUMINATED | |
| 05 | EXT PWR (GPU Power Up Only)ON | |
| 06 | Battery Volts (Selectors to B1 - B6)CHECK ALL OVER 23 VCAUTION: Any battery which does not indicate a minimum of 23 V must be recharged. | |
| 07 | Fire Extinguisher SwitchesOFF (2) - INDICATORS CLEAR (2) | |
| 08 | Nav Lights and LogoONNOTE: Logo only in low visibility. | |
| 09 | EXT PWRAS REQUIREDNOTE: Engines can be started on GPU, APU or battery power. For an APU or GPU start, complete this and the next item before starting the engine. | |
| 10 | EXT BATT CHGOFF |
PHS 5 - Engine 2 Battery Start (If No APU or GPU)10 steps
| 01 | EXT PWROFFNOTE: Only when neither the APU nor a GPU is available: battery power starts Engine 2 to provide aircraft power. Otherwise mark this phase complete and use APU Start. | |
| 02 | TEST Panel (Rear Overhead)TEST ENG FIRE 1 & 2 | |
| 03 | BEACONON | |
| 04 | R PUMP (Fuel)ON | |
| 05 | ENG CMPTR 2AUTO | |
| 06 | MAIN AIR VLV 2CLOSE | |
| 07 | START PWRON | |
| 08 | ENG 2PUSH OPERATING | |
| 09 | Right HP COCK (Pedestal)LEVER UP AT 15% N2 | |
| 10 | START PWROFFNOTE: Continue with Before Start Checks (Continued). |
PHS 6 - APU Start25 steps
| 01 | Left LP COCK (Pedestal)OPEN (UP)NOTE: The APU panel is on the left wall of the flight deck entryway. | |
| 02 | APU MASTER SwitchON (DO NOT START)CAUTION: The APU is not approved for use in icing conditions. Starting is limited to 20,000 ft and operation to 30,000 ft. | |
| 03 | L PUMP (Fuel, Overhead)EMERG | |
| 04 | FUEL 1 LO PRESS AnnunciatorOFF | |
| 05 | Over Voltage (OVV) SwitchNORM | |
| 06 | TEST (Lamp Test) SwitchNORM | |
| 07 | GEN SwitchCLOSE | |
| 08 | BLEED AIR SwitchOFF | |
| 09 | Fire Extinguishing SwitchGUARDED | |
| 10 | APU FIRE ButtonPUSH INNOTE: APU FIRE light ON and the fire bell sounds. | |
| 11 | APU LOW OIL PRESS LightON | |
| 12 | APU GEN LightON | |
| 13 | Remaining APU LightsALL OFF | |
| 14 | APU MASTER SwitchSTART (HOLD MOMENTARILY)CAUTION: Abort the start within 10 seconds if the APU fails to accelerate above 95% RPM, and shut down if READY TO LOAD does not illuminate within 60 seconds. | |
| 15 | APU LOW OIL PRESS LightOFF | |
| 16 | APU GEN LightOFF | |
| 17 | READY TO LOAD LightON | |
| 18 | AmmeterINDICATES LOADNOTE: The APU starter/generator is limited to 300 A. | |
| 19 | RPM GaugeCHECK 100%NOTE: Maximum 110%. | |
| 20 | EGT GaugeWITHIN LIMITSNOTE: 732 °C normal operating. Up to 974 °C is permitted during a start for no more than 10 seconds. | |
| 21 | BLEED AIR SwitchON (AFTER 2 MINUTES OF APU RUNNING)CAUTION: Never run APU and engine bleed air together, except for a brief 1-minute change-over. | |
| 22 | BLEED AIR ON LightON | |
| 23 | BLEED AIR VALVE FAIL LightOFF | |
| 24 | RPM Gauge, EGT Gauge and AmmeterRECHECK | |
| 25 | Cabin Air Condition Controls (Overhead)SET AS DESIRED |
PHS 7 - Before Start Checks (Continued)16 steps
| 01 | BUS TIE (If EXT PWR OFF)CLOSE | |
| 02 | InvertersON AND CHECK | |
| 03 | Air ConditioningAS REQUIRED | |
| 04 | ESIS (Standby Horizon)DISARM - OFF | |
| 05 | RADIO 1 & 2 MastersONNOTE: Pilot side below the MFD, near the LH TRANSFER buttons, labelled RADIO. | |
| 06 | TranspondersCHECKNOTE: CDU TUN button, ATC1 and TCAS Mode. | |
| 07 | PASSENGER SUPPLY OxygenON | |
| 08 | OxygenSUPPLY ON | |
| 09 | Left Hand Side PanelsCHECK | |
| 10 | CABIN HIGH DATUMAS REQUIREDNOTE: ON for departure airports above 9,000 ft. | |
| 11 | EGPWS SwitchesDESELECTED | |
| 12 | MWS (Below the Landing Gear Indicators)TEST - DIM OVRD TO NORM | |
| 13 | AHRS Mode (L & R)NORMNOTE: Next to LH TRANSFER and RH TRANSFER. Hide the pilot yoke to see them. | |
| 14 | LH and RH TRANSFER Switch LightsOFF | |
| 15 | AUX HYD SYSTEM HandleFULLY INNOTE: Next to the left CDU. | |
| 16 | DUMP VALVESHUTNOTE: Next to the right CDU, below the ELT. |
PHS 8 - Pressurization and System Tests17 steps
| 01 | PRESSURIZATION CONTROL LeverNORMAL POSITIONNOTE: Right hand side panel, inside the lid marked LIFT COVER FOR ACCESS TO. | |
| 02 | MANUAL CABIN ALTITUDE CONTROL KnobFULL DECREASE (CW) | |
| 03 | PRESSN (Overhead)AUTO | |
| 04 | F/DK VLV, CABIN FLOOD, MAIN AIR VALV 1 & 2ALL CLOSED | |
| 05 | Controller PresetSETNOTE: Forward panel right of the FO PFD. Cruising above 25,000 ft: cruise altitude + 2,000 ft. Below 25,000 ft: 2,000 ft above the departure airport. Always at least 1,000 ft above airport altitude. | |
| 06 | Right Hand Side PanelsCHECK | |
| 07 | GlareshieldCHECK | |
| 08 | OVERHEAD TEST PanelTEST ALL FUNCTIONSNOTE: On GPU or APU power, test every function. With No. 2 engine running, test all functions except ENG FIRE 1 & 2. | |
| 09 | Overhead PanelCHECK | |
| 10 | AP / YDCHECK | |
| 11 | Electric TrimTEST MOVEMENT | |
| 12 | FMS, Navaids and V BugsSET | |
| 13 | N1 REFSET | |
| 14 | AltimetersSET | |
| 15 | ESISCHECK NO FAILURE FLAGS | |
| 16 | Cabin Signs (Overhead)ON | |
| 17 | EMERG LightsARM |
PHS 9 - Start Checks10 steps
| 01 | BrakesPARK | |
| 02 | BEACONON | |
| 03 | ENG CMPTRsAUTO | |
| 04 | Fuel PumpsON | |
| 05 | START PWRPUSH PWR ON - LIGHT ILLUMINATESNOTE: During start there may be a slow or erratic indication of fuel flow. | |
| 06 | LP COCKsBOTH UP AND GUARDED | |
| 07 | ENG 2 (If Not Running)PUSH OPERATING - LIGHT ILLUMINATES | |
| 08 | Right HP COCKLEVER UP AT 15% N2 | |
| 09 | ENG 1PUSH OPERATING - LIGHT ILLUMINATES | |
| 10 | Left HP COCKLEVER UP AT 15% N2 |
PHS 10 - After Start Checks11 steps
| 01 | START PWROFF | |
| 02 | EXT PWR (If Used)DISCONNECT AND OFF | |
| 03 | Generators 1 & 2CHECK ON LINE | |
| 04 | APU GEN (If APU Installed)TRIP (READY TO LOAD LIGHT ON) | |
| 05 | Volts and AmpsCHECKNOTE: Each generator is limited to 300 A continuous. | |
| 06 | Air ConditioningAS REQUIREDNOTE: If the APU is supplying air conditioning, MAIN AIR VLVs 1 & 2 should be CLOSED. | |
| 07 | ALTERNATORSON | |
| 08 | Heaters (Windshield and Pitot)ON | |
| 09 | PITOT AMPSCHECK | |
| 10 | ENG ANTICEAS REQUIRED | |
| 11 | AIR BRAKESSHUT |
PHS 11 - APR and Engine Computer Checks13 steps
| 01 | APR ARM Switchlight (Forward Panel)PRESS AND ARMNOTE: White APR ARMED light ON. | |
| 02 | Right Thrust LeverSLOWLY INCREASENOTE: Until Engine 2 N2 is approximately 5% greater than Engine 1 N2. | |
| 03 | APR OVRIDE SwitchlightGREEN APR LIGHT ONNOTE: Between the N1 gauges on the MFD, the green APR box flashes and then stays on. | |
| 04 | Right Thrust LeverDECREASE TO IDLE | |
| 05 | APR ARM SwitchlightPRESS AND DISARMNOTE: APR ARMED light OFF. | |
| 06 | APR OVRIDE SwitchlightGREEN APR OFFNOTE: The green APR box on the MFD is no longer visible. | |
| 07 | THRUST REVERSER SwitchlightsPRESS AND ARMNOTE: Directly above the CDUs, the two inner buttons next to POWER. | |
| 08 | ENG CMPTRs (Overhead)SELECT OVRSPD PROT | |
| 09 | ENG 1 & ENG 2 CMPTR AnnunciatorsILLUMINATED | |
| 10 | Thrust LeversADVANCE SLOWLY - VERIFY RESPONSENOTE: With the DEEC off, engine acceleration and deceleration feel different. Just ensure the RPM does not run away and stays fully controllable with the throttle. | |
| 11 | Thrust LeversIDLE | |
| 12 | ENG CMPTRsSELECT AUTO | |
| 13 | ENG 1 & ENG 2 CMPTR AnnunciatorsEXTINGUISHED |
PHS 12 - Rudder Bias and Thrust Reverser Checks20 steps
| 01 | RUDDER BIAS Switches A & BOFFNOTE: Under the guards forward of the AIRBRAKE handle, below the OAT gauge. Set the sim view so the rudder pedals can be seen. | |
| 02 | RUDDER BIAS AnnunciatorILLUMINATED | |
| 03 | Left Thrust LeverADVANCE TO APPROX. 85% N2NOTE: Verify no rudder pedal movement from rudder bias. | |
| 04 | RUDDER BIAS Switch AON - PEDALS DEFLECT SLIGHTLY LEFT | |
| 05 | RUDDER BIAS Switch AOFF - PEDALS RETURN TO CENTER | |
| 06 | RUDDER BIAS Switch BON - PEDALS DEFLECT SLIGHTLY LEFT | |
| 07 | RUDDER BIAS Switch AON - PEDALS DEFLECT FURTHER LEFT | |
| 08 | Left Thrust LeverRETURN TO IDLE | |
| 09 | Rudder Bias Check - Right Thrust LeverREPEAT | |
| 10 | RUDDER BIAS Switches A & BONCAUTION: Both rudder bias switches must be ON and fully operational for every takeoff. | |
| 11 | RUDDER BIAS AnnunciatorEXTINGUISHED | |
| 12 | Left Thrust LeverADVANCE TO APPROX. 85.5% N2NOTE: Verify the rudder pedals deflect to the left. | |
| 13 | Left T/R ARM AnnunciatorEXTINGUISHED | |
| 14 | Right Engine T/RDEPLOYNOTE: Verify the rudder bias input is removed. | |
| 15 | REVERSER AnnunciatorREMAINS OFF | |
| 16 | Right T/R UNLCK & REVRS AnnunciatorsILLUMINATED | |
| 17 | Right Engine T/RRETURN TO IDLE | |
| 18 | Right T/R UNLCK & REVRS AnnunciatorsEXTINGUISHED | |
| 19 | Left Thrust LeverRETURN TO IDLE | |
| 20 | Thrust Reverser Check - Other Thrust LeverREPEATCAUTION: Idle reverse may be used to hold taxi speed and save the brakes. Powered reverse thrust is prohibited during taxi. |
PHS 13 - Before Take-Off Checks14 steps
| 01 | BrakesCHECK | |
| 02 | InstrumentsCHECK | |
| 03 | AltimetersREADING WITHIN 40 FT OF EACH OTHER | |
| 04 | THRUST REVERSERSENSURE STILL ARMED | |
| 05 | FLAPSSETNOTE: The takeoff V-speed tables are published for flaps 0° and 15°. | |
| 06 | Seats and HarnessesSECURE | |
| 07 | WindowsCLOSED | |
| 08 | BriefingCOMPLETE | |
| 09 | BATT AMPSBELOW 20CAUTION: The battery charge rate must be below 20 A before takeoff. | |
| 10 | FuelCHECK QUANTITY AND BALANCECAUTION: Maximum wing tank imbalance is 500 lb at any time, including takeoff and landing. | |
| 11 | FMSCHECK | |
| 12 | TCASTA / RA | |
| 13 | APUONNOTE: Left on for air conditioning and pressurization management. | |
| 14 | Flight ControlsFULL AND FREE MOVEMENT |
PHS 14 - Line Up Checks10 steps
| 01 | EXTERIOR LIGHTSAS REQUIRED | |
| 02 | TranspondersCHECK | |
| 03 | ANTICE and ENG IGNITIONAS REQUIRED | |
| 04 | MWSCHECK NO WARNING MESSAGENOTE: White messages, such as APU, are OK. | |
| 05 | F.A.T.S.CHECK - FLAPS, AIRBRAKES, TRIMS AND V-SPEEDS | |
| 06 | MAIN AIR VALV (1 & 2)CLOSEDCAUTION: Main air valves 1 and 2 and the flight deck heat valve must be closed for takeoff and landing. | |
| 07 | PRESSNAUTO | |
| 08 | F/DK VLVCLOSED | |
| 09 | Takeoff ThrustSET | |
| 10 | APRARM |
PHS 15 - After Take-Off Checks10 steps
| 01 | LANDING GEARUPCAUTION: VLO / VLE 220 KIAS. | |
| 02 | MAIN AIR VLVs 1 & 2OPEN | |
| 03 | APU (If Left On for Takeoff)APU BLEED OFF AND APU SHUTDOWN | |
| 04 | Yaw DamperENGAGE | |
| 05 | FLAPSUPCAUTION: VFE 220 KIAS at flaps 15°. | |
| 06 | THRUSTSET CLIMB POWERNOTE: Normal climb: 160 KIAS at 1,000 ft, 250 KIAS from 5,000 ft to 32,000 ft, then 0.70 IMN. Recommended speed in turbulence is 230 KIAS / 0.70 Mach. | |
| 07 | APRDISARM | |
| 08 | ENG SYNCN1 OR N2 | |
| 09 | ANTICE and ENG IGNITIONAS REQUIRED | |
| 10 | Duct Overheat AnnunciatorEXTINGUISHED |
PHS 16 - Cruise Checks4 steps
| 01 | PressurizationCHECKNOTE: Maximum differential 8.55 psi. | |
| 02 | OXYGENCHECK LEVELS | |
| 03 | ANTICE and ENG IGNITIONAS REQUIRED | |
| 04 | SystemsCHECK AND MONITORCAUTION: To extend engine life, ITT should not exceed 932 °C in cruise. |
PHS 17 - Ventral Tank Transfer (Ventral Tank Use Only)7 steps
| 01 | Aux Transfer Lever (Pedestal)OPEN (DOWN)CAUTION: VMO is limited to 280 KIAS until the ventral fuel is fully transferred and the tank is confirmed empty.NOTE: Only when the ventral tank was filled. Transfer the ventral fuel once the wing tanks drop to 3,300 lb. | |
| 02 | AUX FUEL TFR Annunciator (Overhead)LIT | |
| 03 | FUEL XFD TFR Annunciator (Forward MWS Panel)LIT | |
| 04 | Ventral Tank Fuel LevelMONITORNOTE: Upper left corner of the FO MFD. FULL at capacity, EMPT when empty (a small residual may remain), crosshatch between full and empty or with power off. Leave the lever open for 5 minutes after the climb-to-cruise transition even if it reads EMPT, and until the 280 KIAS limit leaves the PFD speed tape. | |
| 05 | Aux Transfer LeverCLOSE (UP) | |
| 06 | AUX FUEL TFR AnnunciatorEXTINGUISHED | |
| 07 | FUEL XFD TFR AnnunciatorEXTINGUISHEDWARNING: Landing with fuel in the ventral tank is prohibited except in an emergency. The tank must be empty before touchdown. |
PHS 18 - Descent Checks3 steps
| 01 | MAIN AIR VLVs 1 & 2OPEN | |
| 02 | PressurizationSET CONTROLLER TO DESTINATION ELEVATION + QNH CORRECTIONNOTE: Add the correction for destination QNH to the field elevation: 970 hPa +1,500 ft, 975 +1,350, 980 +1,250, 985 +1,100, 990 +950, 995 +800, 1000 +650, 1005 +550, 1010 +400, 1015 +250, 1020 +100, 1025 0, 1030 -150, 1035 -300. | |
| 03 | Descent BriefingCOMPLETENOTE: Descent tables assume 0.76 IMN / 285 / 250 KIAS. At low thrust lever settings the fuel flow indication may become erratic or read zero. This is normal. |
PHS 19 - Approach Checks8 steps
| 01 | AltimetersSET AND CHECKEDNOTE: The manual notes a real-world pilot suggestion to start the APU at this point. | |
| 02 | F/DK VLVCLOSE | |
| 03 | EXTERIOR LIGHTSAS REQUIRED | |
| 04 | Cabin SignsON | |
| 05 | Seats and HarnessesSECURE | |
| 06 | Nosewheel SteeringHANDWHEEL CLEAR | |
| 07 | FuelCHECK QUANTITY AND BALANCE | |
| 08 | VREF / VAPP / Landing DistanceSET AND COMPUTEDNOTE: VREF 108 KIAS at 17,000 lb to 127 KIAS at 23,350 lb (MLW); minimum single-engine VREF 111 KIAS. Add 10 for icing, 15 for no flap, 30 for icing with no flap. The FMS sets VAPP to VREF + 10, adjustable in the PFD REFS menu. |
PHS 20 - Landing Checks10 steps
| 01 | AIR BRAKESSHUTCAUTION: Airbrakes must not be extended in flight with the flaps in any position. | |
| 02 | APRARM | |
| 03 | LANDING GEARDOWNCAUTION: VLO / VLE 220 KIAS. | |
| 04 | Nosewheel SteeringCENTERED | |
| 05 | ENG SYNCOFF | |
| 06 | AltimetersSET AND CHECKED | |
| 07 | FLAPSSET (45° FOR LIFT DUMP)CAUTION: VFE 175 KIAS at flaps 25° and 165 KIAS at flaps 45°. In icing, add 10 KIAS to the approach and landing speeds; landing distance increases by 15 percent. | |
| 08 | MAIN AIR VLVs 1 & 2CLOSE | |
| 09 | AP & YDDISENGAGE | |
| 10 | Lift Dump (At Touchdown)AIR BRAKES HANDLE FULLY BACKCAUTION: Lift dump is restricted to ground operations.NOTE: Works only with weight on wheels and the flaps already at 45°. The flaps then run to 75° and the airbrakes open further. Keyboard users press the spoiler toggle (/ by default). |
PHS 21 - Missed Approach Checks5 steps
| 01 | ThrustAS REQUIRED | |
| 02 | FLAPSRETRACT TO 15° | |
| 03 | Pitch Attitude12° | |
| 04 | AirspeedVREF MINIMUM, OR VREF + 10 KIAS MINIMUM FLAPS RETRACTED | |
| 05 | LANDING GEARUP |
PHS 22 - After Landing Checks10 steps
| 01 | AIRBRAKES / LIFT DUMPSHUT | |
| 02 | FLAPSUP | |
| 03 | Exterior LightsAS REQUIRED | |
| 04 | PITOT / VANE HEAT L & ROFF | |
| 05 | ANTICEAS REQUIRED | |
| 06 | APRDISARM | |
| 07 | TransponderSTDBY | |
| 08 | RADAROFF | |
| 09 | APUAS REQUIRED | |
| 10 | Air ConditioningAS REQUIRED |
PHS 23 - Shutdown (Both Engines and APU Running)18 steps
| 01 | BrakesPARKNOTE: Use this phase when the APU is running, and mark Shutdown (No APU) complete. Without the APU, do the reverse. | |
| 02 | THRUST REVERSERSOFF | |
| 03 | EMERG LIGHTSOFF | |
| 04 | HP COCKSCLOSE | |
| 05 | Fuel PumpsOFF | |
| 06 | ENG CMPTRsOFF | |
| 07 | BEACONOFF | |
| 08 | Cabin NoticesOFF | |
| 09 | GEN FAIL 1 & 2 AnnunciatorsILLUMINATED | |
| 10 | SCREEN HEAT and ALTERNATORSOFF | |
| 11 | RADIO 1 & 2 MastersOFF | |
| 12 | ESISDISARM | |
| 13 | APUSHUT DOWN | |
| 14 | LP CocksDOWN | |
| 15 | Exterior & Interior LightsOFF | |
| 16 | OXYGEN SUPPLYOFF | |
| 17 | BATTOFF | |
| 18 | VESTIBULE / CABIN LIGHTSOFF |
PHS 24 - Shutdown (No APU)24 steps
| 01 | BrakesPARK | |
| 02 | THRUST REVERSERSOFF | |
| 03 | EMERG LIGHTSOFF | |
| 04 | MAIN AIR VLV 1CLOSE | |
| 05 | HP COCK 1CLOSE | |
| 06 | L Fuel PumpOFF | |
| 07 | ENG CMPTR 1OFF | |
| 08 | GEN FAIL 1 AnnunciatorILLUMINATED | |
| 09 | Cabin NoticesOFF | |
| 10 | SCREEN HEAT and ALTERNATORSOFF | |
| 11 | RADIO 1 & 2 MastersOFFNOTE: No. 2 engine still running, no APU. | |
| 12 | ESISDISARM | |
| 13 | MAIN AIR VLV 2CLOSE | |
| 14 | STBY INVOFF | |
| 15 | HP COCK 2CLOSE | |
| 16 | R Fuel PumpOFF | |
| 17 | ENG CMPTR 2OFF | |
| 18 | GEN FAIL 2 AnnunciatorILLUMINATED | |
| 19 | BEACONOFF | |
| 20 | LP CocksDOWN | |
| 21 | Exterior & Interior LightsOFF | |
| 22 | OXYGEN SUPPLYOFF | |
| 23 | BATTOFF | |
| 24 | VESTIBULE / CABIN LIGHTSOFF |