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FALCON BMS · Fighter
F-4E Phantom II (BMS) Startup Checklist
FLIGHT2.9.0Checklist
F-4E Phantom II (BMS)FALCON BMS · Startup Checklist · 191 steps · 18 phases
PHS 1 — Pre-Flight Planning8 steps
| 01 | Mission BriefREVIEWEDNOTE: Review mission type, objectives, ROE, threat environment, timeline, and ingress/egress routes. | |
| 02 | Weather BriefingREVIEWEDNOTE: Check departure, target area, and recovery weather. Note icing levels and visibility. | |
| 03 | NOTAMs / AirspaceREVIEWEDNOTE: Check restricted areas, active MOAs, and NOTAM restrictions along route. | |
| 04 | Fuel Planning - Bingo / JokerSETNOTE: Calculate bingo fuel (min fuel to RTB) and joker fuel (leave target area). Two J79 engines burn approximately 12,000 lbs/hr in afterburner - plan carefully. | |
| 05 | Stores / LoadoutVERIFIEDNOTE: Confirm weapons, pylons, fuel tanks, and ECM pod match mission requirements. Check asymmetric load limits. | |
| 06 | Waypoints / SteerpointsPLANNEDNOTE: Plan steerpoints for departure, IP, target, egress, and divert in BMS mission editor or kneeboard. | |
| 07 | Radio Frequencies / IFF CodesSETNOTE: Set UHF/VHF presets. Confirm IFF Mode 1/2/3/4 codes. Brief EMCON restrictions. | |
| 08 | Divert BasesIDENTIFIEDNOTE: Know nearest divert fields, runway lengths, approach frequencies, and fuel availability. |
PHS 2 — Electrical Power10 steps
| 01 | Seat Safety PinsREMOVED AND STOWEDWARNING: Confirm ejection seat pins are removed before flight - stow in designated pocket. | |
| 02 | CanopyOPENNOTE: Leave canopy open during startup for ventilation. Close and lock before engine start. | |
| 03 | ThrottlesOFF (CUTOFF)WARNING: Both throttles must be in the fully aft CUTOFF position before any power is applied. | |
| 04 | Battery SwitchONNOTE: Applies battery power to essential buses. Instrument lighting partially illuminates. | |
| 05 | External PowerCONNECT / CHECK (If Available)NOTE: Connect ground power unit if available. Reduces battery drain during long startups. | |
| 06 | Generator Switches (Both)ONNOTE: Set both generator switches to ON - they will supply power once engines are running. | |
| 07 | Bus Tie SwitchAUTONOTE: Allows automatic transfer of electrical loads between buses. | |
| 08 | Cockpit LightingSET AS REQUIREDNOTE: Set instrument, console, and flood lighting appropriate for time of day. | |
| 09 | Oxygen SwitchONNOTE: Open oxygen supply valve. Check O2 quantity gauge. | |
| 10 | Intercom SystemCHECK (Pilot / WSO)NOTE: Verify ICS communication between front and rear cockpits. |
PHS 3 — Avionics Power-Up8 steps
| 01 | UHF Radio (AN/ARC-164)ON / PRESET SETNOTE: Set departure frequency preset. Confirm guard monitoring on 243.0 MHz. | |
| 02 | TACANT/R, CHANNEL SETNOTE: Set TACAN channel for departure airfield. Verify azimuth/distance display. | |
| 03 | IFF MasterSTBYNOTE: Set to STBY during startup. Switch to NORM when cleared to taxi. | |
| 04 | IFF Modes 1/2/3SET AS BRIEFEDNOTE: Enter briefed mode codes. Mode 4 requires crypto key loaded. | |
| 05 | Radar Power SwitchSTBYNOTE: Place APQ-120 radar in STBY to begin warm-up. Allow 3-5 minutes before selecting ON. | |
| 06 | Weapons SelectorSAFENOTE: Confirm master arm and weapons selector are in safe positions. | |
| 07 | ECM Pod (ALQ-131, If Equipped)ON / WARM UPNOTE: Power ECM pod if equipped. Allow warm-up time before operational. | |
| 08 | Caution / Warning PanelCHECKNOTE: Note any illuminated caution lights at this stage - some may clear after engine start. |
PHS 4 — Before Engine Start10 steps
| 01 | Parking BrakeSETNOTE: Apply parking brake firmly. Verify brake pressure is adequate. | |
| 02 | Wheel ChocksIN PLACE (Confirm with Crew Chief) | |
| 03 | Fire GuardPOSTED | |
| 04 | Fore and Aft AreaCLEARNOTE: Confirm area around aircraft is clear of personnel and equipment. | |
| 05 | Fuel QuantityCHECK / VERIFYNOTE: Confirm fuel quantity matches planned load. Check all tanks individually. | |
| 06 | Fuel Boost PumpsOFF (Pre-Start)NOTE: Boost pumps will be activated after engine master switches are ON. | |
| 07 | Engine Master Switches (Both)OFF (Pre-Start)NOTE: Verify both engine master switches are OFF before connecting external air. | |
| 08 | Anti-Ice SwitchAS REQUIREDNOTE: Set based on ambient temperature and conditions. | |
| 09 | Flight ControlsCHECK FREENOTE: Verify controls are free and correct with full deflection check before engine start. | |
| 10 | Ejection Seat ArmedARMEDCAUTION: Ensure area around aircraft is clear of personnel before arming seats. Both pilot and WSO arm simultaneously. |
PHS 5 — Engine Start18 steps
| 01 | Right Engine Master SwitchONNOTE: Activates fuel boost pump and ignition system for right engine. | |
| 02 | External Air SourceCONNECT RIGHTNOTE: Connect external pneumatic air cart to right engine. Verify flow established. | |
| 03 | External AirflowONNOTE: Open air valve on ground cart to begin spinning right engine. | |
| 04 | Right Engine RPM - IncreasingCHECK INCREASINGNOTE: Monitor RPM rising toward 10%. Do not advance throttle yet. | |
| 05 | Right Throttle (at ~10% RPM)IDLECAUTION: Advance right throttle to IDLE when RPM reaches approximately 10%. Listen for light-off. | |
| 06 | Right EGT - Light-OffEGT RISING (220-420 deg C at idle)WARNING: If EGT exceeds 420 deg C at idle or rises rapidly above 700 deg C during start, retard throttle to CUTOFF immediately - HOT START. | |
| 07 | External AirflowOFF (at 45% RPM)NOTE: Stop external air when right engine reaches approximately 45% RPM. Engine self-sustains. | |
| 08 | Right Engine - IDLE ParametersVERIFYNOTE: Idle RPM 65+/-1%, EGT 220-420 deg C, Fuel Flow 800-1400 pph, Oil Pressure 12-50 PSI. | |
| 09 | Right GeneratorON / CHECKNOTE: Right generator should come online automatically. Verify generator bus light extinguishes. | |
| 10 | External Air SourceCONNECT LEFTNOTE: Move air cart connection to left engine for second engine start. | |
| 11 | Left Engine Master SwitchON | |
| 12 | External AirflowON (Left)NOTE: Open air valve to begin spinning left engine. | |
| 13 | Left Throttle (at ~10% RPM)IDLECAUTION: Advance left throttle to IDLE at approximately 10% RPM. | |
| 14 | Left EGT - Light-OffEGT RISING (220-420 deg C)WARNING: Monitor for hot start - EGT above 420 deg C at idle requires immediate cutoff. | |
| 15 | External AirflowOFF (at 45% RPM Left)NOTE: Stop external air when left engine reaches approximately 45% RPM. | |
| 16 | Left Engine - IDLE ParametersVERIFYNOTE: Idle RPM 65+/-1%, EGT 220-420 deg C, Fuel Flow 800-1400 pph, Oil Pressure 12-50 PSI. | |
| 17 | Left GeneratorON / CHECKNOTE: Left generator online. Verify bus tie light extinguishes confirming both generators online. | |
| 18 | External Power / AirDISCONNECTNOTE: Signal crew chief to disconnect external power and air after both generators are online. |
PHS 6 — Post-Start Checks12 steps
| 01 | Both Engine InstrumentsIN LIMITSNOTE: Confirm RPM, EGT, fuel flow, and oil pressure stable and within limits on both engines. | |
| 02 | Hydraulic Pressure (PC-1 / PC-2)3,000 PSI (NORMAL)NOTE: Both hydraulic systems should show approximately 3,000 PSI. PC-1 powers flight controls; PC-2 powers utility systems. | |
| 03 | Fuel QuantityCHECK ALL TANKSNOTE: Verify fuel quantity in internal and external tanks matches load plan. | |
| 04 | Fuel Boost PumpsONNOTE: Activate fuel boost pumps for both engines. | |
| 05 | Right Boost Pump Pressure30+/-5 PSI | |
| 06 | Left Boost Pump Pressure30+/-5 PSI | |
| 07 | Air Refueling SwitchNORM (Retracted)NOTE: Verify air refueling door is retracted and switch is in NORM position. | |
| 08 | Caution / Warning LightsALL CLEARNOTE: Address any remaining caution lights. Minor items may clear as systems warm up. | |
| 09 | Cockpit PressurizationCHECKNOTE: Verify pressurization system is functioning and no CABIN PRESS warning. | |
| 10 | Oxygen FlowCHECK (Blinker Moving)NOTE: Verify oxygen flow indicator blinker is cycling with each breath. | |
| 11 | Spoiler ActuatorCHECKNOTE: Visually confirm spoiler actuator movement. Left spoiler check after right engine start. | |
| 12 | Radar AltimeterON, LOW ALT SET 200 FTNOTE: Set radar altimeter low altitude warning as appropriate for departure phase. |
PHS 7 — INS / Navigation Setup10 steps
| 01 | INS Mode SelectorSTBY (WARM-UP)NOTE: Place INS in STBY for initial warm-up. Allow gyros to reach operating temperature. | |
| 02 | INS Alignment (GYRO COMP)INITIATENOTE: Select GYRO COMP on INS mode knob. Full alignment takes 8-10 minutes for accurate navigation. | |
| 03 | Present PositionENTER (Lat/Long)NOTE: Enter current airfield coordinates into INS. Accuracy of alignment depends on correct position entry. | |
| 04 | TACAN - Airfield ChannelSET / VERIFIEDNOTE: Confirm TACAN bearing and distance to airfield TACAN station. Cross-check with known position. | |
| 05 | Altimeter Setting (QNH)SETNOTE: Set QNH on barometric altimeter. Verify field elevation within +/- 75 ft. | |
| 06 | Compass SystemSET / SLAVEDNOTE: Verify compass heading agrees with INS and known runway heading. | |
| 07 | Steerpoints / WaypointsENTERED AND VERIFIEDNOTE: Confirm steerpoints match mission briefing coordinates. Check each steerpoint bearing and distance. | |
| 08 | INS Alignment StatusALIGNED (READY)NOTE: Wait for INS READY light before proceeding. Do not taxi until alignment is complete. | |
| 09 | INS ModeNAVNOTE: Switch INS to NAV mode after alignment completes. Verify navigation display is active. | |
| 10 | IFF MasterNORMNOTE: Switch IFF from STBY to NORM. Verify correct modes and codes set per briefing. |
PHS 8 — Weapons and Sensors8 steps
| 01 | Weapons Control PanelVERIFY SAFENOTE: Confirm all weapons switches are safe before proceeding. | |
| 02 | Optical Sight (LEAD COMP)SET AS REQUIREDNOTE: Set sight mode and reticle appropriate for mission weapons and profile. | |
| 03 | Radar (APQ-120)ON / RANGE SETNOTE: Switch radar from STBY to ON after warm-up. Set initial range scale for departure phase. | |
| 04 | Radar BITPASSNOTE: Run radar built-in test if time permits. Verify no fault indications. | |
| 05 | Weapons Delivery ModeSET AS BRIEFEDNOTE: Set DSCG weapons mode, fuzing, and release setting per mission weapons load. | |
| 06 | AIM-7 Sparrow (If Loaded)TUNED / STATUS CHECKNOTE: Allow AIM-7 seeker to tune. Check status lights on weapons control panel. | |
| 07 | AIM-9 Sidewinder (If Loaded)COOL / STATUS CHECKNOTE: Verify AIM-9 cooling tone. Check uncage capability if equipped. | |
| 08 | Centerline / Wing Tank Fuel TransferSET AS REQUIREDNOTE: Verify external tank transfer switches are set correctly per tank configuration. |
PHS 9 — Before Taxi12 steps
| 01 | CanopyCLOSE AND LOCKCAUTION: Ensure canopy is fully latched and locked. Verify canopy unlock light is extinguished. | |
| 02 | Slats / FlapsOUT AND DOWN (TO)NOTE: Select SLATS/FLAPS OUT for takeoff. Verify slat/flap position indicators. | |
| 03 | Stabilizer Augmentation SwitchesON (Pitch and Yaw SAS)NOTE: Ensure pitch and yaw SAS switches are ON for enhanced stability. | |
| 04 | Flight ControlsCHECK FREE AND CORRECTNOTE: Full deflection check - stick fore/aft, left/right, rudder full left/right. Verify control surface response. | |
| 05 | TrimSET FOR TAKEOFFNOTE: Set pitch trim 0-2 units nose up. Set rudder and aileron trim to neutral. | |
| 06 | BrakesCHECKCAUTION: Pump brakes to verify pressure. Test differential braking before releasing parking brake. | |
| 07 | Anti-Skid SwitchONNOTE: Activate anti-skid system. Will be verified on runway prior to takeoff. | |
| 08 | Internal Wing TransferVERIFYNOTE: Check wing fuel transfer is operating correctly. | |
| 09 | Warning Lights PanelCHECK ALL CLEARNOTE: Address any illuminated warning lights before taxi. | |
| 10 | RadarSTBY (Taxi)NOTE: Place radar in STBY during ground operations. Switch ON when airborne. | |
| 11 | Parking BrakeRELEASENOTE: Release parking brake when cleared to taxi. | |
| 12 | Nose Wheel SteeringENGAGEDNOTE: Verify nosewheel steering is active. Taxi with small power additions to test braking. |
PHS 10 — Taxi6 steps
| 01 | ATC Taxi ClearanceRECEIVEDNOTE: Obtain taxi clearance and confirm runway in use, QNH, and any taxi restrictions. | |
| 02 | Taxi SpeedAPPROPRIATE (< 20 KTS)NOTE: Maintain safe taxi speed. F-4 has high inertia - plan stopping distances carefully. | |
| 03 | InstrumentsCHECK DURING TAXINOTE: Verify attitude indicator, compass, and turn indicator respond correctly during taxi turns. | |
| 04 | Pitot HeatONNOTE: Activate pitot heat during taxi to ensure airspeed system is fully functional before takeoff. | |
| 05 | Defog / Temperature ControlSET AS REQUIREDNOTE: Set cockpit temperature and defog as needed. | |
| 06 | Engine InstrumentsMONITOR CONTINUOUSLYNOTE: Monitor EGT, RPM, and oil pressure throughout taxi. |
PHS 11 — Before Takeoff14 steps
| 01 | Lineup ChecksCOMPLETENOTE: Run through all lineup items before entering runway. | |
| 02 | Optical SightSET FOR MISSIONNOTE: Verify sight mode selected for departure air-to-air or air-to-ground as required. | |
| 03 | Internal Wing TransferVERIFYNOTE: Confirm wing fuel is transferring to feed the engines. | |
| 04 | Stabilizer Augmentation (SAS)BOTH ONNOTE: Re-verify pitch and yaw SAS are ON. | |
| 05 | Flight ControlsFREE AND CORRECTNOTE: Final flight control check at runway hold short. | |
| 06 | Slats / FlapsOUT AND DOWN - CONFIRMEDNOTE: Visually verify flap and slat position indicators show OUT and DOWN. | |
| 07 | Anti-IceAS REQUIREDNOTE: Set engine and pitot anti-ice as required for conditions. | |
| 08 | Fuel QuantityCHECK TOTALNOTE: Note total fuel and confirm bingo fuel setting on fuel low warning. | |
| 09 | CanopyCLOSED AND LOCKEDCAUTION: Confirm canopy locked before entering active runway. | |
| 10 | Warning LightsALL CLEARNOTE: No red or amber lights on caution/warning panel. | |
| 11 | Defog / TempSETNOTE: Ensure windscreen is clear. Set defog as needed. | |
| 12 | Command Selector ValveNORMNOTE: Set command selector to normal position for flight. | |
| 13 | Ejection SeatsARMED (Both Crew Confirm)CAUTION: Both pilot and WSO confirm ejection seat mode selector is set correctly per crew coordination. | |
| 14 | IFFNORM / CODES SETNOTE: Confirm IFF in NORM with correct codes for departure. |
PHS 12 — Takeoff13 steps
| 01 | Runway LineupALIGNEDNOTE: Align on runway centerline. Set heading reference on HSI to runway heading. | |
| 02 | Anti-SkidVERIFIED ON (Before Roll)NOTE: Check anti-skid light status before brake release. | |
| 03 | Compass CheckRUNWAY HEADING CONFIRMEDNOTE: Verify compass and INS heading agree with runway heading. | |
| 04 | Circuit BreakersCHECK INNOTE: Quick scan of circuit breaker panel - all in. | |
| 05 | BrakesHOLDNOTE: Apply toe brakes firmly. Advance throttles to 85% RPM before release for engine stabilization check. | |
| 06 | Engine Parameters at 85% RPMVERIFY (EGT ~450 C, FF ~4000 PPH, Nozzles 1/4, Oil 30-40 PSI)CAUTION: Do not advance beyond 85% until engine parameters are confirmed stable. | |
| 07 | Throttles to Military PowerMILITARY POWERNOTE: Advance both throttles to full military (non-afterburner) power. Or select afterburner for heavy loads or short runways. | |
| 08 | Brakes ReleaseRELEASENOTE: Release brakes when engines are stable at military or afterburner power. Confirm equal thrust from both engines. | |
| 09 | Nose Gear SteeringENGAGED TO 70 KTSNOTE: Use nose gear steering for directional control during initial roll. Rudder becomes effective at approximately 70 knots. | |
| 10 | Nose Gear SteeringDISENGAGE AT ~70 KTSNOTE: Disengage NWS when rudder steering becomes effective. Switch to rudder for directional control. | |
| 11 | RotationAPPLY AFT STICK (V1~180 KTS)NOTE: Apply aft stick pressure prior to nose wheel liftoff. Maintain 10-12 deg nose-high attitude for fly-off. | |
| 12 | Landing GearRETRACT (< 250 KTS)WARNING: Retract gear before reaching 250 knots maximum gear limit airspeed. Verify gear handle UP and warning light out. | |
| 13 | Slats / FlapsNORM (RETRACT > 180 KTS)NOTE: Retract slats and flaps above 180 knots. Verify slat/flap indicators show IN and UP. |
PHS 13 — After Takeoff / Climb9 steps
| 01 | Gear IndicatorsALL UP (3 Green Out)NOTE: Confirm all three gear indicators show UP. Verify gear warning light is extinguished. | |
| 02 | Slats / Flaps IndicatorsIN AND UPNOTE: Confirm slats and flaps fully retracted on position indicator. | |
| 03 | Climb Attitude10-12 DEG NOSE HIGH TO 350 KIASNOTE: Maintain 10-12 deg nose-high until reaching 350 KIAS, then adjust pitch to maintain airspeed. | |
| 04 | AfterburnerCANCEL (If Used)NOTE: Cancel afterburner after gear and flaps are up and climb established. Monitor EGT and fuel flow. | |
| 05 | Engine InstrumentsCHECK IN LIMITSNOTE: Verify RPM, EGT, oil pressure, and hydraulic pressure in limits during climb. | |
| 06 | RadarSWITCH TO ON (Airborne)NOTE: Switch radar from STBY to ON now that aircraft is airborne. Set appropriate search range. | |
| 07 | Fuel QuantityCHECK AND MONITORNOTE: Note fuel at wheels-up. Calculate fuel flow to confirm within expected parameters. | |
| 08 | Anti-IceAS REQUIREDNOTE: Monitor for icing conditions en route. Activate engine anti-ice as needed. | |
| 09 | ATC / Radar ContactCHECK INNOTE: Contact departure control or mission freq. Report airborne and climbing. |
PHS 14 — Cruise / Transit10 steps
| 01 | Altimeter / BARO SettingSET AND COMPARE (Pilot/WSO)NOTE: Set altimeter to FL transition altitude. Compare pilot and WSO altimeter readings. | |
| 02 | Radar AltimeterON / LOW WARN SETNOTE: Set radar altimeter low altitude warning appropriate for route altitude. | |
| 03 | Command Selector ValveNORMNOTE: Verify command selector in NORM position for cruise. | |
| 04 | TACANCHECK NAVIGATIONNOTE: Verify TACAN bearing and distance to next steerpoint or waypoint navaid. | |
| 05 | Fuel QuantityCHECK / MONITOR TRANSFERNOTE: Verify fuel is transferring from external tanks. Monitor total fuel against time plan. Note joker and bingo fuel targets. | |
| 06 | Operations Check (Oxygen)FLOW NORMALNOTE: Verify O2 blinker cycling normally. Check PSI. | |
| 07 | Cockpit PressurizationCHECK NORMALNOTE: Verify cabin altitude and differential pressure are within normal range. | |
| 08 | Engine InstrumentsIN LIMITSNOTE: Periodic check of RPM, EGT, oil, and hydraulic pressure throughout cruise. | |
| 09 | Standby CompassCHECK / VERIFY HEADINGNOTE: Periodically cross-check standby compass with primary heading reference. | |
| 10 | Anti-IceADJUST AS REQUIREDNOTE: Monitor for airframe icing. Activate engine anti-ice if required. |
PHS 15 — Descent / Approach9 steps
| 01 | Altimeter (QNH)SET (Destination)NOTE: Set destination airfield QNH. Compare with WSO altimeter. Note transition altitude. | |
| 02 | TACAN (Destination)SETNOTE: Set destination airfield TACAN channel. Verify bearing and distance to field. | |
| 03 | RadarSTBY (Prior to Approach)NOTE: Place radar in STBY when no longer needed. Reduces emissions during approach. | |
| 04 | IFFNORM / CODES CONFIRMNOTE: Confirm correct IFF codes for recovery. Squawk assigned code if applicable. | |
| 05 | Fuel QuantityCHECK TOTAL vs BINGONOTE: Verify fuel is above bingo. If below joker, notify wingman/flight lead. | |
| 06 | WeaponsSAFE / VERIFYNOTE: Confirm all weapons are safed and not live before approach to pattern. | |
| 07 | Anti-IceAS REQUIREDNOTE: Maintain engine and pitot anti-ice if icing conditions exist during descent. | |
| 08 | Air Refueling SwitchEXTEND (Prior to Landing)NOTE: Extend air refueling door to depressurize fuel tanks before landing. Reduces fuel tank overpressure risk. | |
| 09 | Landing Pattern Entry230 KIAS MINIMUMNOTE: Enter visual pattern at 230 KIAS minimum maneuvering speed. 250 KIAS single engine. |
PHS 16 — Landing12 steps
| 01 | Pattern Entry Speed230 KIAS (NORMAL) / 250 KIAS (SINGLE ENGINE)NOTE: Maintain minimum 230 knots in the pattern with flaps up. | |
| 02 | Landing GearDOWN (DOWNWIND)NOTE: Select landing gear down on downwind leg in level flight. Verify 3 green indicators. | |
| 03 | Slats / FlapsOUT AND DOWN (BELOW 210 KTS)NOTE: Select slats/flaps OUT when slowing below 210 knots. Actual flap extension may not occur until 210 KIAS. | |
| 04 | Angle of Attack19.2 UNITS (ON-SPEED)NOTE: Fly on-speed AOA (19.2 units / middle aural tone) for optimum approach. Do not fly by airspeed alone. | |
| 05 | Glidepath2.5 - 3 DEG (700 FPM DESCENT)NOTE: Maintain 2.5 to 3 degree glideslope producing approximately 700 fpm rate of descent. | |
| 06 | Power ManagementADJUST FOR AOA / GLIDEPATHNOTE: Use power to control glidepath. Use pitch to control AOA. Maintain coordinated approach. | |
| 07 | Base Leg / Final AOAON-SPEED ESTABLISHEDNOTE: Establish and maintain on-speed AOA on base leg or final approach. | |
| 08 | TouchdownPOWER TO IDLE / DEPLOY DRAG CHUTENOTE: At touchdown reduce power to idle immediately. Deploy drag chute to assist deceleration. | |
| 09 | Drag ChuteDEPLOY AT TOUCHDOWNNOTE: Deploy drag chute at touchdown. Effective between 180 and 70 knots for maximum deceleration. | |
| 10 | Directional ControlRUDDER/AILERONS TO 70 KTS, THEN BRAKESNOTE: Use rudder and ailerons for directional control above 70 knots. Transition to differential braking below 70 knots. | |
| 11 | Full Aft StickMAINTAIN THROUGHOUT ROLLOUTNOTE: Hold full aft stick throughout rollout to keep nose gear loaded for aerodynamic braking. | |
| 12 | BrakingAPPLY AS REQUIREDNOTE: Apply wheel brakes as needed. Maximum braking after nose gear contacts runway. |
PHS 17 — After Landing9 steps
| 01 | Drag ChuteJETTISON (Taxi Speed)NOTE: Jettison drag chute when clear of runway and at safe taxi speed. Crew chief will retrieve. | |
| 02 | Slats / FlapsNORM (RETRACT)NOTE: Retract slats and flaps after clearing runway. | |
| 03 | Anti-SkidOFFNOTE: Switch anti-skid off after clearing active runway. | |
| 04 | Air Refueling DoorRETRACT (NORM)NOTE: Return air refueling switch to NORM to retract door. | |
| 05 | RadarSTBY or OFFNOTE: Place radar in STBY or OFF during taxi. Reduces risk to ground personnel. | |
| 06 | IFFSTBYNOTE: Return IFF to STBY after clearing runway. | |
| 07 | LightsAS REQUIRED FOR TAXINOTE: Set taxi light and nav lights appropriately for post-landing taxi. | |
| 08 | Pitot HeatOFF (After Parking)NOTE: Turn off pitot heat once parked to prevent ground crew hazard. | |
| 09 | WeaponsSAFE / CONFIRMNOTE: Confirm all weapons in safe condition before reaching parking area. |
PHS 18 — Shutdown13 steps
| 01 | Parking BrakeSETNOTE: Apply parking brake firmly before shutdown. | |
| 02 | Wheel ChocksIN PLACE (Signal Crew Chief) | |
| 03 | AvionicsOFF / STANDBYNOTE: Switch avionics, radar, ECM, and navigation systems off or to minimum power. | |
| 04 | Ejection SeatsSAFE (Both Crew)NOTE: Both pilot and WSO safe ejection seats before exiting aircraft. | |
| 05 | IFFOFF / ZEROIZENOTE: Zeroize IFF codes if required by mission security requirements. | |
| 06 | Right ThrottleCUTOFFNOTE: Retard right throttle to CUTOFF. Engine will begin winding down. | |
| 07 | Left ThrottleCUTOFFNOTE: Retard left throttle to CUTOFF simultaneously or sequentially. | |
| 08 | Engine Spool-DownMONITOR (RPM Decreasing)NOTE: Both engines should spool down smoothly. Monitor EGT until cool. | |
| 09 | Engine Master Switches (Both)OFF (After Full Spool-Down)WARNING: Do not switch engine master OFF until engines have fully spooled down. Premature cutoff can cause fire. | |
| 10 | Generators (Both)OFFNOTE: Switch off both generators after engines have stopped. | |
| 11 | Battery SwitchOFFNOTE: Switch off battery after all systems have been properly shut down. | |
| 12 | CanopyOPENNOTE: Open canopy for crew egress and aircraft cooling. | |
| 13 | Post-Flight InspectionCOMPLETENOTE: Conduct post-flight walkaround. Note any discrepancies for maintenance debrief. |