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MSFS 2024 · Airliner
Fokker F100 Startup Checklist
FLIGHT2.9.0Checklist
Fokker F100MSFS 2024 · Startup Checklist · 224 steps · 18 phases
PHS 1 — Pre-Flight Planning9 steps
| 01 | Weather Briefing (METAR / TAF / SIGMET)REVIEWEDNOTE: Check departure, destination, and alternate. Review wind shear advisories and icing conditions. | |
| 02 | NOTAMsREVIEWEDNOTE: Check runway closures, taxiway restrictions, approach procedure changes, and airspace NOTAMs. | |
| 03 | OFP / SimBrief Flight PlanREVIEWED & LOADEDNOTE: Verify route, cruising level, alternates, and fuel figures. | |
| 04 | Fuel Planning (Block Fuel Breakdown)CALCULATEDNOTE: Trip fuel + contingency + alternate + final reserve (30 min holding). Typical burn ~2,000-2,400 kg/hr at cruise. | |
| 05 | Weight & Balance / LoadsheetWITHIN LIMITSCAUTION: MTOW 45,810 kg. MLW 39,000 kg. Max ZFW 36,000 kg. Verify CG within envelope (17-35% MAC). | |
| 06 | SID / STAR / Approach ReviewREVIEWEDNOTE: Brief the departure procedure, cruise altitude, STAR into destination, and planned approach type. | |
| 07 | Takeoff Performance (V-Speeds)CALCULATEDNOTE: Calculate V1, Vr, V2 using OFP data and runway conditions. Typical values: V1 ~128 kts, Vr ~130 kts, V2 ~140 kts. | |
| 08 | MEL / CDL ReviewCHECKEDNOTE: Confirm all deferred items are within MEL limits and any required procedures are noted. | |
| 09 | ATIS / D-ATISOBTAINEDNOTE: Note active runway, QNH, wind, and temperature for performance calculations. |
PHS 2 — Electrical Power-Up10 steps
| 01 | Parking BrakeSET | |
| 02 | Battery SwitchONWARNING: Ensure battery is ON before connecting any other electrical systems. | |
| 03 | External Power (GPU)CONNECTED / ONNOTE: Connect GPU to preserve battery. Verify GPU AVAIL light illuminates. | |
| 04 | Cockpit LightingAS REQUIRED | |
| 05 | APU Battery SwitchON | |
| 06 | APU Master SwitchONNOTE: APU start takes approximately 60 seconds. Monitor APU EGT during start. | |
| 07 | APU StartINITIATED | |
| 08 | APU Running / AvailableCONFIRMEDNOTE: APU AVAIL light on. Switch AC busses to APU power. | |
| 09 | AC Bus 1 / AC Bus 2ON APU POWER | |
| 10 | GPU Disconnect (if APU available)DISCONNECTED |
PHS 3 — Cockpit Preparation20 steps
| 01 | Emergency Lights SwitchARMED | |
| 02 | Fuel QuantityCHECKEDNOTE: Verify fuel loaded matches OFP. Check both left and right wing tanks and center tank. | |
| 03 | Fuel Crossfeed ValveCLOSED | |
| 04 | Fuel Pump Switches (L/R)OFF (for now) | |
| 05 | Hydraulic System PressureCHECKEDNOTE: Both hydraulic systems (A and B) should indicate normal pressure when powered. | |
| 06 | Flight ControlsCHECKED - FREE AND CORRECTNOTE: Full deflection of ailerons, elevator, and rudder. Verify correct movement on primary flight display. | |
| 07 | Oxygen SystemCHECKEDNOTE: Both crew oxygen regulators set to NORMAL. Verify adequate pressure. | |
| 08 | Weather RadarSTANDBY | |
| 09 | Windshield Heat SwitchesONNOTE: Windshield heat is on continuously during flight. | |
| 10 | Pitot Heat SwitchesON | |
| 11 | Anti-Ice Engine (L/R)AS REQUIREDNOTE: ON when icing conditions exist or are anticipated. | |
| 12 | Spoiler LeverRETRACTED | |
| 13 | Flap LeverUP / 0 | |
| 14 | Trim (Elevator)SET FOR TAKEOFF | |
| 15 | Rudder TrimNEUTRAL | |
| 16 | Aileron TrimNEUTRAL | |
| 17 | Landing Gear LeverDOWN / CONFIRMED DOWN | |
| 18 | Autobrake SelectorRTO | |
| 19 | Speed Brake LeverRETRACTED | |
| 20 | Engine Master Switches (L/R)OFF |
PHS 4 — FMS / MCDU Setup20 steps
| 01 | FMS PowerONNOTE: FMS initializes automatically once AC power is available. | |
| 02 | IRS AlignmentALIGN INITIATEDNOTE: Select NAV on IRS mode selectors. Full alignment takes 8-12 minutes. Use FAST ALIGN if available in sim. | |
| 03 | FMS - Ident PageVERIFIEDNOTE: Check navdata cycle and database validity date. | |
| 04 | FMS - Position InitSETNOTE: Enter present position from GPS or manual ICAO reference. | |
| 05 | FMS - Route Entry (Origin/Destination)ENTERED | |
| 06 | FMS - SID EntrySELECTEDNOTE: Select departure runway and SID procedure. | |
| 07 | FMS - Route (Airways/Waypoints)ENTERED | |
| 08 | FMS - STAR / ApproachSELECTEDNOTE: Enter destination STAR and preferred approach. Verify transition altitude. | |
| 09 | FMS - Fuel / ZFW EntryENTEREDCAUTION: Verify ZFW within max limits before entry. Incorrect ZFW will corrupt fuel calculations. | |
| 10 | FMS - Cost Index / Cruise LevelSET | |
| 11 | FMS - V-Speeds (V1 / Vr / V2)ENTEREDNOTE: Enter calculated V1, Vr, V2 from performance data. | |
| 12 | FMS - Takeoff Flap SettingSETNOTE: Typically flap 8 for standard takeoff. | |
| 13 | FMS - Route ActivationACTIVATED | |
| 14 | Navigation Displays (PFD / ND)CHECKEDNOTE: Verify ND shows correct route. Set range as appropriate. | |
| 15 | Altimeters (Capt / FO)SET QNH | |
| 16 | Baro ReferenceSET | |
| 17 | Transponder CodeSETNOTE: Enter squawk code from ATC. Mode S / ADS-B if equipped. | |
| 18 | Transponder ModeSTANDBY | |
| 19 | Radio / Comms SetupSETNOTE: Active and standby frequencies for departure and ground. | |
| 20 | Autopilot - MCP (Mode Control Panel)PRESETNOTE: Set initial climb altitude, speed, and heading. Do not engage yet. |
PHS 5 — Before Start8 steps
| 01 | Doors CheckCLOSED AND LOCKEDNOTE: All cabin and cargo doors closed. Door warning lights extinguished. | |
| 02 | Fuel Pump Switches (L/R)ON | |
| 03 | Beacon LightONNOTE: Turn on beacon before engine start as a warning to ground crew. | |
| 04 | Pushback / ClearanceOBTAINEDNOTE: Request start and pushback clearance from ground. | |
| 05 | BrakesSETNOTE: Parking brake set during pushback. | |
| 06 | Anti-Collision LightON | |
| 07 | APU Bleed AirONNOTE: Required for engine start using pneumatic starter. | |
| 08 | Engine AreaCLEARNOTE: Verify no personnel or equipment near engine intakes. |
PHS 6 — Engine Start19 steps
| 01 | Engine Start SelectorSET TO START (ENG 2 first)NOTE: On the Fokker F100, start right engine (Eng 2) first to maintain electrical power balance. | |
| 02 | Engine 2 Master SwitchON | |
| 03 | Engine 2 - N2 RisingCONFIRMEDNOTE: Wait for N2 to reach approximately 20-25% before fuel on. | |
| 04 | Engine 2 Fuel Lever / MasterON (RICH / IDLE CUT-IN)CAUTION: Monitor EGT during light-off. Rapid EGT rise indicates good ignition. Hot start risk if EGT spikes above limits. | |
| 05 | Engine 2 - EGT RiseCONFIRMED LIGHT-OFFWARNING: Abort start if EGT exceeds 950 C or does not stabilize. Hot start can damage turbine blades. | |
| 06 | Engine 2 - N1 / N2 StabilizingIDLE (N2 approx 60-65%)NOTE: Engine settles to ground idle. Monitor oil pressure rising within 30 seconds. | |
| 07 | Engine 2 Oil PressureNORMALWARNING: If oil pressure does not rise within 30 seconds at idle, shut down immediately. | |
| 08 | Engine 2 GeneratorONLINENOTE: Eng 2 generator connects to AC Bus 2. APU may be offloaded. | |
| 09 | Engine 1 Start SelectorSET TO START | |
| 10 | Engine 1 Master SwitchON | |
| 11 | Engine 1 - N2 RisingCONFIRMED | |
| 12 | Engine 1 Fuel Lever / MasterONCAUTION: Monitor EGT during light-off. | |
| 13 | Engine 1 - EGT RiseCONFIRMED LIGHT-OFFWARNING: Abort start if EGT exceeds 950 C. | |
| 14 | Engine 1 - N1 / N2 StabilizingIDLE | |
| 15 | Engine 1 Oil PressureNORMAL | |
| 16 | Engine 1 GeneratorONLINE | |
| 17 | APU Bleed AirOFFNOTE: Once both engines are running and generators online, switch bleed air to engine sources. | |
| 18 | APU MasterOFF (if no longer required) | |
| 19 | Engine InstrumentsALL NORMALNOTE: Check N1, N2, EGT, FF, oil pressure, and oil temperature on both engines. |
PHS 7 — After Start / Before Taxi13 steps
| 01 | Engine Bleed Air Switches (L/R)ON | |
| 02 | Air Conditioning PacksONNOTE: Set to AUTO. Pressurization system will arm automatically. | |
| 03 | PressurizationAUTO / ARMED | |
| 04 | Hydraulic Systems A and BNORMAL PRESSURE | |
| 05 | Flight Controls - Final CheckFREE AND CORRECT | |
| 06 | Avionics / EFISNORMAL | |
| 07 | Autopilot / Flight DirectorCHECKEDNOTE: Verify FD bars present and correct. Set initial heading and altitude bugs. | |
| 08 | FlapsSET FOR TAKEOFF (FLAP 8 or 15)NOTE: Flap 8 for standard takeoff, Flap 15 for shorter field requirements. | |
| 09 | Elevator TrimSET FOR TAKEOFF | |
| 10 | Standby InstrumentsCHECKED | |
| 11 | Passenger Signs (Seat Belts / No Smoking)ON | |
| 12 | TransponderTA/RA (ON / ALTITUDE REPORTING) | |
| 13 | Pushback Complete / BrakesBRAKES SET |
PHS 8 — Taxi9 steps
| 01 | Taxi ClearanceOBTAINED | |
| 02 | Parking BrakeRELEASED | |
| 03 | Nose Wheel SteeringENGAGED | |
| 04 | Taxi SpeedMAX 20 KTSNOTE: Max 10 kts for sharp turns. | |
| 05 | Brake CheckCHECKEDNOTE: Light brake application after beginning to roll to verify brakes are functional. | |
| 06 | Navigation LightsON | |
| 07 | Weather RadarON / AS REQUIRED | |
| 08 | Altimeter (Capt / FO)SET / CROSSCHECK | |
| 09 | Heading IndicatorALIGNED WITH RUNWAY HDG |
PHS 9 — Before Takeoff15 steps
| 01 | Takeoff ClearanceOBTAINED | |
| 02 | Parking BrakeSET (HOLDING POSITION) | |
| 03 | Engine InstrumentsCHECKED - NORMAL | |
| 04 | FlapsCONFIRMED SET (FLAP 8 or 15) | |
| 05 | Flight ControlsFREE AND CORRECT | |
| 06 | Trim (Elevator)SET FOR TAKEOFF | |
| 07 | AutobrakeRTO | |
| 08 | Auto SpoilersARMED | |
| 09 | V-Speeds (V1 / Vr / V2)CONFIRMEDNOTE: Cross-check FMS-computed V-speeds against performance cards. | |
| 10 | Landing LightsON | |
| 11 | Strobe LightsON | |
| 12 | Pitot HeatON | |
| 13 | Anti-IceAS REQUIRED | |
| 14 | Transponder ModeTA/RA | |
| 15 | Crew Briefing (Takeoff / Rejected Takeoff)COMPLETENOTE: Brief V1, Vr, V2, initial climb altitude, and rejected takeoff procedure. |
PHS 10 — Takeoff11 steps
| 01 | Parking BrakeRELEASED | |
| 02 | Thrust - Initial Spool40% N1NOTE: Advance thrust levers to 40% N1. Allow engines to stabilize before applying full takeoff thrust. | |
| 03 | Takeoff Thrust90-95% N1 (TOGA) | |
| 04 | Engine Instruments at Full ThrustCHECKED - NORMALNOTE: Quick scan for symmetric thrust and no warning lights. | |
| 05 | V1 - Decision SpeedCONTINUE TAKEOFFCAUTION: After V1, takeoff MUST continue. Reject only if a critical emergency arises before V1. | |
| 06 | Vr - RotateROTATE 10 DEG NOSE UPNOTE: Smooth positive rotation. Target 10 degrees pitch attitude. | |
| 07 | V2 - Takeoff Safety SpeedMAINTAINNOTE: Maintain V2 + 10 kts for initial climb. | |
| 08 | Positive Rate of ClimbCONFIRMEDNOTE: Verify positive VSI and increasing altitude. | |
| 09 | Landing GearUPNOTE: Retract gear after positive rate confirmed. Gear limit speed 200 kts. | |
| 10 | Landing Gear LightsOUT (GEAR RETRACTED) | |
| 11 | AutobrakeCHECKED OFF (after gear up) |
PHS 11 — After Takeoff / Climb10 steps
| 01 | Flaps Retraction ScheduleINITIATEDNOTE: At flap retraction speed: Flap 8 - retract above V2 + 15 kts. Flap 0 - retract at acceleration altitude. | |
| 02 | FlapsUP (at or above Vfe)CAUTION: Do not exceed flap placard speeds during retraction. | |
| 03 | Climb ThrustSET (MCT / CLIMB DETENT)NOTE: Reduce from TOGA to climb thrust. Typically 85-88% N1. | |
| 04 | AutopilotENGAGED (above 400 ft AGL)NOTE: Minimum autopilot engagement altitude is 400 ft AGL. | |
| 05 | AutothrottleENGAGED | |
| 06 | Landing LightsOFF (above 10,000 ft) | |
| 07 | Seat Belt SignAS REQUIRED | |
| 08 | Climb Speed250 KIAS BELOW FL100 / 280 KIAS ABOVE | |
| 09 | Engine InstrumentsMONITORED | |
| 10 | PressurizationNORMAL (CABIN ALTITUDE CLIMBING) |
PHS 12 — Cruise8 steps
| 01 | Cruise Thrust / AutothrottleCRUISE POWER SETNOTE: Typical cruise at Mach 0.73-0.75 (approx 840-845 km/h). Autothrottle manages thrust. | |
| 02 | Cruise AltitudeREACHED AND LEVEL | |
| 03 | Altimeter SettingSTD (1013 hPa / 29.92 inHg) ABOVE TRANSITION ALTITUDE | |
| 04 | FMS Fuel PredictionsCHECKEDNOTE: Verify actual fuel burn vs. OFP plan. Plan diversion if fuel below minimums. | |
| 05 | Weather RadarMONITORING | |
| 06 | Position / ETACHECKEDNOTE: Cross-check FMS position with charts. | |
| 07 | Radios / ATCUPDATED AS REQUIRED | |
| 08 | Anti-IceAS REQUIRED |
PHS 13 — Descent Preparation7 steps
| 01 | ATIS (Destination)OBTAINED | |
| 02 | FMS - Arrival / STAR / ApproachUPDATED IF CHANGED | |
| 03 | Approach BriefCOMPLETENOTE: Brief approach type, minima, missed approach procedure, runway and lighting. | |
| 04 | Destination AltimeterNOTED (QNH) | |
| 05 | Landing Performance (Vapp / VREF)CALCULATEDNOTE: Calculate Vapp based on landing weight. Typical Vref ~122-130 kts depending on weight and flap. | |
| 06 | Autobrake SettingSELECTED | |
| 07 | Fuel StateCHECKED |
PHS 14 — Descent8 steps
| 01 | Descent ClearanceOBTAINED | |
| 02 | Descent Speed (Mach/IAS crossover)MACH 0.73 / 280 KIAS | |
| 03 | Altimeter SettingQNH SET BELOW TRANSITION LEVEL | |
| 04 | Seat Belt SignON | |
| 05 | Landing LightsON BELOW 10,000 FT | |
| 06 | Speed Below 10,000 ft250 KIAS MAX | |
| 07 | Flap / GearUP AND RETRACTED (during descent) | |
| 08 | Engine Anti-IceAS REQUIRED |
PHS 15 — Approach17 steps
| 01 | Approach ClearanceOBTAINED | |
| 02 | Speed - Initial Approach200 KIAS | |
| 03 | Flaps - 8 degreesSETNOTE: Establish 160 KIAS with Flap 8. | |
| 04 | Speed Established at 160 KIASCONFIRMED | |
| 05 | Flaps - 15 degreesSETNOTE: Establish 140 KIAS with Flap 15. | |
| 06 | Speed Established at 140 KIASCONFIRMED | |
| 07 | Flaps - 25 degreesSET | |
| 08 | Landing GearDOWNNOTE: Gear down with flaps 25. Verify 3 green lights. | |
| 09 | Landing Gear - 3 GreenCONFIRMED | |
| 10 | Flaps - Full (42 degrees)SET ON FINALNOTE: Set full flaps on final approach. Vapp typically 130 KIAS at normal landing weight. | |
| 11 | Auto SpoilersARMED | |
| 12 | AutobrakeSELECTED | |
| 13 | ILS / LOC CapturedCONFIRMED | |
| 14 | Glide SlopeESTABLISHED | |
| 15 | Approach Speed (Vapp)130 KIAS (TYPICAL) | |
| 16 | Parking BrakeVERIFY OFF | |
| 17 | Anti-IceAS REQUIRED |
PHS 16 — Landing10 steps
| 01 | Landing GearDOWN - 3 GREENWARNING: Never land without confirmed gear down and locked. 3 green lights required. | |
| 02 | Autopilot / AutothrottleOFF (at DH or manual override)NOTE: Disconnect AP below decision height for manual landing, or use autoland if CAT III. | |
| 03 | Final Approach SpeedVAPP (130 KIAS TYPICAL) | |
| 04 | FlareINITIATE AT ~30 FT AGL | |
| 05 | TouchdownMAIN WHEELS FIRSTNOTE: Land on main wheels, do not hold off - firm touchdown for spoiler deployment. | |
| 06 | Thrust ReversersDEPLOYED AFTER TOUCHDOWNCAUTION: Cancel reverse thrust above 60 kts. Do not use asymmetric reverse. | |
| 07 | Auto SpoilersDEPLOYED (VERIFY) | |
| 08 | Nose WheelLOWER GENTLY | |
| 09 | BrakesAS REQUIREDNOTE: Autobrake should be active. Manual braking as needed to achieve taxi speed. | |
| 10 | Thrust ReversersSTOW AT 60 KTS |
PHS 17 — After Landing10 steps
| 01 | Thrust ReversersSTOWED | |
| 02 | AutobrakeDISARMNOTE: Check autobrake is OFF after clearing runway. | |
| 03 | Strobe LightsOFF | |
| 04 | Landing LightsOFF | |
| 05 | FlapsRETRACT TO UPNOTE: Retract flaps after clearing active runway. | |
| 06 | Speed Brakes / SpoilersRETRACTED | |
| 07 | Weather RadarSTANDBY | |
| 08 | TransponderSTANDBY | |
| 09 | Anti-IceAS REQUIRED | |
| 10 | Taxi SpeedMAX 20 KTSNOTE: Obtain taxi-to-gate clearance from ATC. |
PHS 18 — Parking / Shutdown20 steps
| 01 | Parking BrakeSET | |
| 02 | ThrottlesIDLE | |
| 03 | GPU / External PowerCONNECT (if available)NOTE: Connect GPU before shutting down engines to maintain avionics power. | |
| 04 | APU MasterON (if no GPU)NOTE: Start APU before engine shutdown if GPU unavailable. | |
| 05 | Passenger SignsOFF | |
| 06 | Engine 1 Fuel LeverCUT OFF | |
| 07 | Engine 1 - N2 ReducingCONFIRMED SHUTDOWN | |
| 08 | Engine 2 Fuel LeverCUT OFF | |
| 09 | Engine 2 - N2 ReducingCONFIRMED SHUTDOWN | |
| 10 | Fuel Pumps (L/R)OFF | |
| 11 | Beacon LightOFF (after both engines spooled down) | |
| 12 | FMS / AvionicsDATA STORED / OFF | |
| 13 | Hydraulic SystemsDEPRESSURIZED | |
| 14 | Air Conditioning PacksOFF | |
| 15 | APU Bleed AirOFF | |
| 16 | APU MasterOFF | |
| 17 | Windshield Heat / Pitot HeatOFF | |
| 18 | Navigation LightsOFF | |
| 19 | Emergency LightsOFF | |
| 20 | Battery SwitchOFFNOTE: Last item. Verify all switches are OFF before disconnecting battery. |