Fokker F100MSFS 2024 Startup Checklist · 224 steps
Fokker F100
MSFS 2024 - 0/224 STEPS
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Airliner1980s
AIRCRAFT BRIEF
The Fokker 100 is a twin-engine regional jet developed by Dutch manufacturer Fokker, announced in 1983 as a modernized successor to the F28 Fellowship. It made its maiden flight on 30 November 1986 and entered airline service with Swissair in February 1988, featuring Rolls-Royce Tay turbofan engines, a glass cockpit, and a fuselage stretched by 5.7 m over the F28 to seat up to 109 passengers. Despite commercial success in the competitive 100-seat market, Fokker's bankruptcy in 1996 ended production at 283 aircraft delivered, making the F100 the largest jet airliner ever built by Fokker.
RANGE VISUALIZER
SPECIFICATIONS
manufacturerFokker
first Flight1986
roleRegional narrow-body airliner
crew2 pilots + cabin crew
engines2x Rolls-Royce Tay 620-15 (61.6 kN / 13,850 lbf each)
max Speed845 km/h (Mach 0.77)
range3,170 km (1,710 nmi)
ceiling35,000 ft
weight45,810 kg (MTOW)
PHS 1 — Pre-Flight Planning9 steps
| 01 | Weather Briefing (METAR / TAF / SIGMET)NOTE: Check departure, destination, and alternate. Review wind shear advisories and icing conditions. | REVIEWED | |
| 02 | NOTAMsNOTE: Check runway closures, taxiway restrictions, approach procedure changes, and airspace NOTAMs. | REVIEWED | |
| 03 | OFP / SimBrief Flight PlanNOTE: Verify route, cruising level, alternates, and fuel figures. | REVIEWED & LOADED | |
| 04 | Fuel Planning (Block Fuel Breakdown)NOTE: Trip fuel + contingency + alternate + final reserve (30 min holding). Typical burn ~2,000-2,400 kg/hr at cruise. | CALCULATED | |
| 05 | Weight & Balance / LoadsheetCAUTION: MTOW 45,810 kg. MLW 39,000 kg. Max ZFW 36,000 kg. Verify CG within envelope (17-35% MAC). | WITHIN LIMITS | |
| 06 | SID / STAR / Approach ReviewNOTE: Brief the departure procedure, cruise altitude, STAR into destination, and planned approach type. | REVIEWED | |
| 07 | Takeoff Performance (V-Speeds)NOTE: Calculate V1, Vr, V2 using OFP data and runway conditions. Typical values: V1 ~128 kts, Vr ~130 kts, V2 ~140 kts. | CALCULATED | |
| 08 | MEL / CDL ReviewNOTE: Confirm all deferred items are within MEL limits and any required procedures are noted. | CHECKED | |
| 09 | ATIS / D-ATISNOTE: Note active runway, QNH, wind, and temperature for performance calculations. | OBTAINED |
PHS 2 — Electrical Power-Up10 steps
| 01 | Parking Brake | SET | |
| 02 | Battery SwitchWARNING: Ensure battery is ON before connecting any other electrical systems. | ON | |
| 03 | External Power (GPU)NOTE: Connect GPU to preserve battery. Verify GPU AVAIL light illuminates. | CONNECTED / ON | |
| 04 | Cockpit Lighting | AS REQUIRED | |
| 05 | APU Battery Switch | ON | |
| 06 | APU Master SwitchNOTE: APU start takes approximately 60 seconds. Monitor APU EGT during start. | ON | |
| 07 | APU Start | INITIATED | |
| 08 | APU Running / AvailableNOTE: APU AVAIL light on. Switch AC busses to APU power. | CONFIRMED | |
| 09 | AC Bus 1 / AC Bus 2 | ON APU POWER | |
| 10 | GPU Disconnect (if APU available) | DISCONNECTED |
PHS 3 — Cockpit Preparation20 steps
| 01 | Emergency Lights Switch | ARMED | |
| 02 | Fuel QuantityNOTE: Verify fuel loaded matches OFP. Check both left and right wing tanks and center tank. | CHECKED | |
| 03 | Fuel Crossfeed Valve | CLOSED | |
| 04 | Fuel Pump Switches (L/R) | OFF (for now) | |
| 05 | Hydraulic System PressureNOTE: Both hydraulic systems (A and B) should indicate normal pressure when powered. | CHECKED | |
| 06 | Flight ControlsNOTE: Full deflection of ailerons, elevator, and rudder. Verify correct movement on primary flight display. | CHECKED - FREE AND CORRECT | |
| 07 | Oxygen SystemNOTE: Both crew oxygen regulators set to NORMAL. Verify adequate pressure. | CHECKED | |
| 08 | Weather Radar | STANDBY | |
| 09 | Windshield Heat SwitchesNOTE: Windshield heat is on continuously during flight. | ON | |
| 10 | Pitot Heat Switches | ON | |
| 11 | Anti-Ice Engine (L/R)NOTE: ON when icing conditions exist or are anticipated. | AS REQUIRED | |
| 12 | Spoiler Lever | RETRACTED | |
| 13 | Flap Lever | UP / 0 | |
| 14 | Trim (Elevator) | SET FOR TAKEOFF | |
| 15 | Rudder Trim | NEUTRAL | |
| 16 | Aileron Trim | NEUTRAL | |
| 17 | Landing Gear Lever | DOWN / CONFIRMED DOWN | |
| 18 | Autobrake Selector | RTO | |
| 19 | Speed Brake Lever | RETRACTED | |
| 20 | Engine Master Switches (L/R) | OFF |
PHS 4 — FMS / MCDU Setup20 steps
| 01 | FMS PowerNOTE: FMS initializes automatically once AC power is available. | ON | |
| 02 | IRS AlignmentNOTE: Select NAV on IRS mode selectors. Full alignment takes 8-12 minutes. Use FAST ALIGN if available in sim. | ALIGN INITIATED | |
| 03 | FMS - Ident PageNOTE: Check navdata cycle and database validity date. | VERIFIED | |
| 04 | FMS - Position InitNOTE: Enter present position from GPS or manual ICAO reference. | SET | |
| 05 | FMS - Route Entry (Origin/Destination) | ENTERED | |
| 06 | FMS - SID EntryNOTE: Select departure runway and SID procedure. | SELECTED | |
| 07 | FMS - Route (Airways/Waypoints) | ENTERED | |
| 08 | FMS - STAR / ApproachNOTE: Enter destination STAR and preferred approach. Verify transition altitude. | SELECTED | |
| 09 | FMS - Fuel / ZFW EntryCAUTION: Verify ZFW within max limits before entry. Incorrect ZFW will corrupt fuel calculations. | ENTERED | |
| 10 | FMS - Cost Index / Cruise Level | SET | |
| 11 | FMS - V-Speeds (V1 / Vr / V2)NOTE: Enter calculated V1, Vr, V2 from performance data. | ENTERED | |
| 12 | FMS - Takeoff Flap SettingNOTE: Typically flap 8 for standard takeoff. | SET | |
| 13 | FMS - Route Activation | ACTIVATED | |
| 14 | Navigation Displays (PFD / ND)NOTE: Verify ND shows correct route. Set range as appropriate. | CHECKED | |
| 15 | Altimeters (Capt / FO) | SET QNH | |
| 16 | Baro Reference | SET | |
| 17 | Transponder CodeNOTE: Enter squawk code from ATC. Mode S / ADS-B if equipped. | SET | |
| 18 | Transponder Mode | STANDBY | |
| 19 | Radio / Comms SetupNOTE: Active and standby frequencies for departure and ground. | SET | |
| 20 | Autopilot - MCP (Mode Control Panel)NOTE: Set initial climb altitude, speed, and heading. Do not engage yet. | PRESET |
PHS 5 — Before Start8 steps
| 01 | Doors CheckNOTE: All cabin and cargo doors closed. Door warning lights extinguished. | CLOSED AND LOCKED | |
| 02 | Fuel Pump Switches (L/R) | ON | |
| 03 | Beacon LightNOTE: Turn on beacon before engine start as a warning to ground crew. | ON | |
| 04 | Pushback / ClearanceNOTE: Request start and pushback clearance from ground. | OBTAINED | |
| 05 | BrakesNOTE: Parking brake set during pushback. | SET | |
| 06 | Anti-Collision Light | ON | |
| 07 | APU Bleed AirNOTE: Required for engine start using pneumatic starter. | ON | |
| 08 | Engine AreaNOTE: Verify no personnel or equipment near engine intakes. | CLEAR |
PHS 6 — Engine Start19 steps
| 01 | Engine Start SelectorNOTE: On the Fokker F100, start right engine (Eng 2) first to maintain electrical power balance. | SET TO START (ENG 2 first) | |
| 02 | Engine 2 Master Switch | ON | |
| 03 | Engine 2 - N2 RisingNOTE: Wait for N2 to reach approximately 20-25% before fuel on. | CONFIRMED | |
| 04 | Engine 2 Fuel Lever / MasterCAUTION: Monitor EGT during light-off. Rapid EGT rise indicates good ignition. Hot start risk if EGT spikes above limits. | ON (RICH / IDLE CUT-IN) | |
| 05 | Engine 2 - EGT RiseWARNING: Abort start if EGT exceeds 950 C or does not stabilize. Hot start can damage turbine blades. | CONFIRMED LIGHT-OFF | |
| 06 | Engine 2 - N1 / N2 StabilizingNOTE: Engine settles to ground idle. Monitor oil pressure rising within 30 seconds. | IDLE (N2 approx 60-65%) | |
| 07 | Engine 2 Oil PressureWARNING: If oil pressure does not rise within 30 seconds at idle, shut down immediately. | NORMAL | |
| 08 | Engine 2 GeneratorNOTE: Eng 2 generator connects to AC Bus 2. APU may be offloaded. | ONLINE | |
| 09 | Engine 1 Start Selector | SET TO START | |
| 10 | Engine 1 Master Switch | ON | |
| 11 | Engine 1 - N2 Rising | CONFIRMED | |
| 12 | Engine 1 Fuel Lever / MasterCAUTION: Monitor EGT during light-off. | ON | |
| 13 | Engine 1 - EGT RiseWARNING: Abort start if EGT exceeds 950 C. | CONFIRMED LIGHT-OFF | |
| 14 | Engine 1 - N1 / N2 Stabilizing | IDLE | |
| 15 | Engine 1 Oil Pressure | NORMAL | |
| 16 | Engine 1 Generator | ONLINE | |
| 17 | APU Bleed AirNOTE: Once both engines are running and generators online, switch bleed air to engine sources. | OFF | |
| 18 | APU Master | OFF (if no longer required) | |
| 19 | Engine InstrumentsNOTE: Check N1, N2, EGT, FF, oil pressure, and oil temperature on both engines. | ALL NORMAL |
PHS 7 — After Start / Before Taxi13 steps
| 01 | Engine Bleed Air Switches (L/R) | ON | |
| 02 | Air Conditioning PacksNOTE: Set to AUTO. Pressurization system will arm automatically. | ON | |
| 03 | Pressurization | AUTO / ARMED | |
| 04 | Hydraulic Systems A and B | NORMAL PRESSURE | |
| 05 | Flight Controls - Final Check | FREE AND CORRECT | |
| 06 | Avionics / EFIS | NORMAL | |
| 07 | Autopilot / Flight DirectorNOTE: Verify FD bars present and correct. Set initial heading and altitude bugs. | CHECKED | |
| 08 | FlapsNOTE: Flap 8 for standard takeoff, Flap 15 for shorter field requirements. | SET FOR TAKEOFF (FLAP 8 or 15) | |
| 09 | Elevator Trim | SET FOR TAKEOFF | |
| 10 | Standby Instruments | CHECKED | |
| 11 | Passenger Signs (Seat Belts / No Smoking) | ON | |
| 12 | Transponder | TA/RA (ON / ALTITUDE REPORTING) | |
| 13 | Pushback Complete / Brakes | BRAKES SET |
PHS 8 — Taxi9 steps
| 01 | Taxi Clearance | OBTAINED | |
| 02 | Parking Brake | RELEASED | |
| 03 | Nose Wheel Steering | ENGAGED | |
| 04 | Taxi SpeedNOTE: Max 10 kts for sharp turns. | MAX 20 KTS | |
| 05 | Brake CheckNOTE: Light brake application after beginning to roll to verify brakes are functional. | CHECKED | |
| 06 | Navigation Lights | ON | |
| 07 | Weather Radar | ON / AS REQUIRED | |
| 08 | Altimeter (Capt / FO) | SET / CROSSCHECK | |
| 09 | Heading Indicator | ALIGNED WITH RUNWAY HDG |
PHS 9 — Before Takeoff15 steps
| 01 | Takeoff Clearance | OBTAINED | |
| 02 | Parking Brake | SET (HOLDING POSITION) | |
| 03 | Engine Instruments | CHECKED - NORMAL | |
| 04 | Flaps | CONFIRMED SET (FLAP 8 or 15) | |
| 05 | Flight Controls | FREE AND CORRECT | |
| 06 | Trim (Elevator) | SET FOR TAKEOFF | |
| 07 | Autobrake | RTO | |
| 08 | Auto Spoilers | ARMED | |
| 09 | V-Speeds (V1 / Vr / V2)NOTE: Cross-check FMS-computed V-speeds against performance cards. | CONFIRMED | |
| 10 | Landing Lights | ON | |
| 11 | Strobe Lights | ON | |
| 12 | Pitot Heat | ON | |
| 13 | Anti-Ice | AS REQUIRED | |
| 14 | Transponder Mode | TA/RA | |
| 15 | Crew Briefing (Takeoff / Rejected Takeoff)NOTE: Brief V1, Vr, V2, initial climb altitude, and rejected takeoff procedure. | COMPLETE |
PHS 10 — Takeoff11 steps
| 01 | Parking Brake | RELEASED | |
| 02 | Thrust - Initial SpoolNOTE: Advance thrust levers to 40% N1. Allow engines to stabilize before applying full takeoff thrust. | 40% N1 | |
| 03 | Takeoff Thrust | 90-95% N1 (TOGA) | |
| 04 | Engine Instruments at Full ThrustNOTE: Quick scan for symmetric thrust and no warning lights. | CHECKED - NORMAL | |
| 05 | V1 - Decision SpeedCAUTION: After V1, takeoff MUST continue. Reject only if a critical emergency arises before V1. | CONTINUE TAKEOFF | |
| 06 | Vr - RotateNOTE: Smooth positive rotation. Target 10 degrees pitch attitude. | ROTATE 10 DEG NOSE UP | |
| 07 | V2 - Takeoff Safety SpeedNOTE: Maintain V2 + 10 kts for initial climb. | MAINTAIN | |
| 08 | Positive Rate of ClimbNOTE: Verify positive VSI and increasing altitude. | CONFIRMED | |
| 09 | Landing GearNOTE: Retract gear after positive rate confirmed. Gear limit speed 200 kts. | UP | |
| 10 | Landing Gear Lights | OUT (GEAR RETRACTED) | |
| 11 | Autobrake | CHECKED OFF (after gear up) |
PHS 11 — After Takeoff / Climb10 steps
| 01 | Flaps Retraction ScheduleNOTE: At flap retraction speed: Flap 8 - retract above V2 + 15 kts. Flap 0 - retract at acceleration altitude. | INITIATED | |
| 02 | FlapsCAUTION: Do not exceed flap placard speeds during retraction. | UP (at or above Vfe) | |
| 03 | Climb ThrustNOTE: Reduce from TOGA to climb thrust. Typically 85-88% N1. | SET (MCT / CLIMB DETENT) | |
| 04 | AutopilotNOTE: Minimum autopilot engagement altitude is 400 ft AGL. | ENGAGED (above 400 ft AGL) | |
| 05 | Autothrottle | ENGAGED | |
| 06 | Landing Lights | OFF (above 10,000 ft) | |
| 07 | Seat Belt Sign | AS REQUIRED | |
| 08 | Climb Speed | 250 KIAS BELOW FL100 / 280 KIAS ABOVE | |
| 09 | Engine Instruments | MONITORED | |
| 10 | Pressurization | NORMAL (CABIN ALTITUDE CLIMBING) |
PHS 12 — Cruise8 steps
| 01 | Cruise Thrust / AutothrottleNOTE: Typical cruise at Mach 0.73-0.75 (approx 840-845 km/h). Autothrottle manages thrust. | CRUISE POWER SET | |
| 02 | Cruise Altitude | REACHED AND LEVEL | |
| 03 | Altimeter Setting | STD (1013 hPa / 29.92 inHg) ABOVE TRANSITION ALTITUDE | |
| 04 | FMS Fuel PredictionsNOTE: Verify actual fuel burn vs. OFP plan. Plan diversion if fuel below minimums. | CHECKED | |
| 05 | Weather Radar | MONITORING | |
| 06 | Position / ETANOTE: Cross-check FMS position with charts. | CHECKED | |
| 07 | Radios / ATC | UPDATED AS REQUIRED | |
| 08 | Anti-Ice | AS REQUIRED |
PHS 13 — Descent Preparation7 steps
| 01 | ATIS (Destination) | OBTAINED | |
| 02 | FMS - Arrival / STAR / Approach | UPDATED IF CHANGED | |
| 03 | Approach BriefNOTE: Brief approach type, minima, missed approach procedure, runway and lighting. | COMPLETE | |
| 04 | Destination Altimeter | NOTED (QNH) | |
| 05 | Landing Performance (Vapp / VREF)NOTE: Calculate Vapp based on landing weight. Typical Vref ~122-130 kts depending on weight and flap. | CALCULATED | |
| 06 | Autobrake Setting | SELECTED | |
| 07 | Fuel State | CHECKED |
PHS 14 — Descent8 steps
| 01 | Descent Clearance | OBTAINED | |
| 02 | Descent Speed (Mach/IAS crossover) | MACH 0.73 / 280 KIAS | |
| 03 | Altimeter Setting | QNH SET BELOW TRANSITION LEVEL | |
| 04 | Seat Belt Sign | ON | |
| 05 | Landing Lights | ON BELOW 10,000 FT | |
| 06 | Speed Below 10,000 ft | 250 KIAS MAX | |
| 07 | Flap / Gear | UP AND RETRACTED (during descent) | |
| 08 | Engine Anti-Ice | AS REQUIRED |
PHS 15 — Approach17 steps
| 01 | Approach Clearance | OBTAINED | |
| 02 | Speed - Initial Approach | 200 KIAS | |
| 03 | Flaps - 8 degreesNOTE: Establish 160 KIAS with Flap 8. | SET | |
| 04 | Speed Established at 160 KIAS | CONFIRMED | |
| 05 | Flaps - 15 degreesNOTE: Establish 140 KIAS with Flap 15. | SET | |
| 06 | Speed Established at 140 KIAS | CONFIRMED | |
| 07 | Flaps - 25 degrees | SET | |
| 08 | Landing GearNOTE: Gear down with flaps 25. Verify 3 green lights. | DOWN | |
| 09 | Landing Gear - 3 Green | CONFIRMED | |
| 10 | Flaps - Full (42 degrees)NOTE: Set full flaps on final approach. Vapp typically 130 KIAS at normal landing weight. | SET ON FINAL | |
| 11 | Auto Spoilers | ARMED | |
| 12 | Autobrake | SELECTED | |
| 13 | ILS / LOC Captured | CONFIRMED | |
| 14 | Glide Slope | ESTABLISHED | |
| 15 | Approach Speed (Vapp) | 130 KIAS (TYPICAL) | |
| 16 | Parking Brake | VERIFY OFF | |
| 17 | Anti-Ice | AS REQUIRED |
PHS 16 — Landing10 steps
| 01 | Landing GearWARNING: Never land without confirmed gear down and locked. 3 green lights required. | DOWN - 3 GREEN | |
| 02 | Autopilot / AutothrottleNOTE: Disconnect AP below decision height for manual landing, or use autoland if CAT III. | OFF (at DH or manual override) | |
| 03 | Final Approach Speed | VAPP (130 KIAS TYPICAL) | |
| 04 | Flare | INITIATE AT ~30 FT AGL | |
| 05 | TouchdownNOTE: Land on main wheels, do not hold off - firm touchdown for spoiler deployment. | MAIN WHEELS FIRST | |
| 06 | Thrust ReversersCAUTION: Cancel reverse thrust above 60 kts. Do not use asymmetric reverse. | DEPLOYED AFTER TOUCHDOWN | |
| 07 | Auto Spoilers | DEPLOYED (VERIFY) | |
| 08 | Nose Wheel | LOWER GENTLY | |
| 09 | BrakesNOTE: Autobrake should be active. Manual braking as needed to achieve taxi speed. | AS REQUIRED | |
| 10 | Thrust Reversers | STOW AT 60 KTS |
PHS 17 — After Landing10 steps
| 01 | Thrust Reversers | STOWED | |
| 02 | AutobrakeNOTE: Check autobrake is OFF after clearing runway. | DISARM | |
| 03 | Strobe Lights | OFF | |
| 04 | Landing Lights | OFF | |
| 05 | FlapsNOTE: Retract flaps after clearing active runway. | RETRACT TO UP | |
| 06 | Speed Brakes / Spoilers | RETRACTED | |
| 07 | Weather Radar | STANDBY | |
| 08 | Transponder | STANDBY | |
| 09 | Anti-Ice | AS REQUIRED | |
| 10 | Taxi SpeedNOTE: Obtain taxi-to-gate clearance from ATC. | MAX 20 KTS |
PHS 18 — Parking / Shutdown20 steps
| 01 | Parking Brake | SET | |
| 02 | Throttles | IDLE | |
| 03 | GPU / External PowerNOTE: Connect GPU before shutting down engines to maintain avionics power. | CONNECT (if available) | |
| 04 | APU MasterNOTE: Start APU before engine shutdown if GPU unavailable. | ON (if no GPU) | |
| 05 | Passenger Signs | OFF | |
| 06 | Engine 1 Fuel Lever | CUT OFF | |
| 07 | Engine 1 - N2 Reducing | CONFIRMED SHUTDOWN | |
| 08 | Engine 2 Fuel Lever | CUT OFF | |
| 09 | Engine 2 - N2 Reducing | CONFIRMED SHUTDOWN | |
| 10 | Fuel Pumps (L/R) | OFF | |
| 11 | Beacon Light | OFF (after both engines spooled down) | |
| 12 | FMS / Avionics | DATA STORED / OFF | |
| 13 | Hydraulic Systems | DEPRESSURIZED | |
| 14 | Air Conditioning Packs | OFF | |
| 15 | APU Bleed Air | OFF | |
| 16 | APU Master | OFF | |
| 17 | Windshield Heat / Pitot Heat | OFF | |
| 18 | Navigation Lights | OFF | |
| 19 | Emergency Lights | OFF | |
| 20 | Battery SwitchNOTE: Last item. Verify all switches are OFF before disconnecting battery. | OFF |