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    F-16Block 50/52 (GE129)

    Checklists - Main Volume

    F-16 checklists main volume 0/16

    Not suited for Real OperationsMade for FALCON 4

    *Some switches and behaviours might not work depending on your version.

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    CONTENTS

    Check-lists

    1 Contents2 Verify Checks / Before Engine Start3 Starting Engine / Engine Check at Idle / After Engine Start4 After Engine Start (Continued) item 2 to 85 After Engine Start (Continued) item 9 to 136 After Engine Start (Continued) item 14 to 167 After Engine Start (Continued) item 17 to 198 Before Taxi / Taxi / If checks9 Before Take Off / Normal Take Off10 Airborne / Fence In11 Initial Point / Egress / Fence Out12 IF Checks Mnemonics / Descent / Approach13 Before Landing / Final Approach / Landing / After Landing14 Aerial Refuelling15 Prior to Engine Shut Down / Engine Shut Down16 Hotpit refuel / Supplemental procedures: ILS

    Annex1 : Cockpit layout with #PanelAnnex2: Blank page for notes

    NOTE:

    Refer to EP volume 0612 for Emergency procedures

    Refer to In Flight Quick References volume 0805 for charts

    and datacards. Refer to Cockpit Interior check Rev 0805 for placing all

    switches before entering the aircraft

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    BEFORE ENGINE START

    VERIFY CHECK

    ON Guard down PNL#3NORM PNL#3NORM Guard down PNL#2PRI Guard down PNL#4OFFConfirm Down and locked PNL#1UP PNL#1

    SAFE PNL#1NORM PNL#5

    1. MASTER FUEL Switch2. ENGINE FEED Knob3. EPU switch4. ENG CONT switch5. THROTTLE6. LD GEAR Handle7. HOOK switch

    8. MASTER ARM switch9. AIR SOURCE knob

    The following items are important switches that if not correctlypositioned, could cause a safety hazard and/or improperly operated

    systems during engine start.Please refer to cock it / interior checklist for a full cock it check.

    1. MAIN PWR switch

    2. FLCS PWR TEST switch

    3. FLCS PWR TEST switch4. MAIN PWR Switch

    5. EPU GEN & EPU PMG lights6. Communications7. Canopy

    BATT :Verify FLCS RLY light ON PNL#4TEST and holdVerify lights ON

    ACFT BATT TO FLCS PNL#4FLCS PMG PNL#4FLCS PWR (4) PNL#22

    Verify FLCS RLY light OFFReleaseMAIN PWR:Verify lights ON PNL#4

    ELEC SYS PNL#17HYD/OIL PRESSFLCS RLY PNL#4SEC PNL#17ENGINE

    Confirm OFF PNL#4EstablishedAs desired

    Note:To prevent possible depletion of battery power, do not allow MAIN PWR sw toremain in BATT or MAIN PWR for more than 5 minutes without engine running.

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    AFTER ENGINE START

    STARTING ENGINE GE129

    1. TEST switch panel check: PNL#22

    - PROBE HEAT switch: PROBE HEAT: check caution light OFFTEST: check caution light flashesOFF

    - Fire and Overheat Detect Button: TEST & HOLD- Check ENG FIRE Warning light ON- Check OVER HEAT caution light- Check MASTER CAUTION light ON

    - MAL&IND LTS button: DEPRESS and HOLD

    Proper VMS operation is verified by the presence of each word in priority sequence.

    ENGINE CHECK AT IDLE

    1. FUEL FLOW2. OIL pressure3. NOZ POS

    4. RPM5. FTIT6. HYD PRESS A&B7. Throttle cutoff release

    700 1700 PPHMIN 15 PSIGreater than 94%

    62 80%Below 650C2850 - 3250psi - around 12 Oclock positionCheck Attempt to retard the throttle to OFFwithout depressing the cutoff release.

    1. JFS

    2. THROTTLE3. Idle Detent4. SEC caution light5. ENGINE warning light6. JFS Switch7. HYD/OIL PRESS light

    START 2 PNL#7check JFS light ON

    Advance to IDLE at 20% RPM minimum.Toggle(Unless idle/cutoff code enabled in bmsconfig)Check OFF around 20% RPMOFF at 60% RPMConfirm OFF (snaps OFF at 55% RPM)OFF between 15 and 70% RPM

    Note :Engine light-off occurs within 10 seconds after throttle advance and is

    indicated by an airframe vibration and an increase in RPM followed by an

    increase of FTIT. Without external power connected, only the RPM and FTITindicators function until the standby generator is online.

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    AFTER ENGINE START Continued

    2. AVIONICS POWER Panela. MMC (FCC) switch: ON PNL#9

    b. ST STA (SMS) switch: ON PNL#9c. MFD switch: ON PNL#9d. UFC switch: ON PNL#9e. DL (MAP) switch: ON PNL#9f. GPS switch: ON PNL#9g. INS: Select ALIGN NORM PNL#9

    3. SNSR PWR panel:a.LEFT HDPT switch: OFF unless required PNL#10

    b. RIGHT HDPT switch: As required PNL#10c. FCR switch: FCR PNL#10d. RDR ALT switch STBY PNL#10

    4. HUD Panel: As desired PNL#11

    Set HUD SYM WHEEL ON PNL#145. CNI (C&I) knob : UFC PNL#256. MFL: Reset (MFD TEST page)

    7. SEC check :May be delayed until the BEFORE TAKEOFFa. THROTTLE: IDLEb. TOE BRAKE: ENGAGE, no PARKING BRAKESc. ENG CONT switch: SEC PNL#7d. SEC Caution Light: ON - Nozzle: Less than 5% PNL#17e. RPM: Stabilizedf. THROTTLE: Snap to MIL

    then snap to IDLE when RPM reaches 85%.

    Check for normal indication and smooth operation.g. NOZ POS: 10% or less within 30 sec after selecting SEC.h. ENG CONT switch: PRI PNL#7i. SEC Caution Light: OFF PNL#17 j. NOZ POS: Greater than 94%

    8. FLIGHT CONTROLS: CYCLE & CHECK

    Note :To assist in warming up the hydraulic fluid and removing air from thehydraulic system, maximum stick and rudder pedal input should be madeprior to running the FLCS BIT.

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    AFTER ENGINE START Continued

    9. FLCS BIT: Initiate and monitor.Position BIT switch to BIT. The RUN light ON FLCP illuminates.

    At successful completion of BIT (approximately 45seconds) the RUNlight goes OFF, the BIT switch returns to OFF and the FAIL light andFLCSwarning light remain OFF. A BIT pass message appears onthe FLCS MFD page

    10. SPD BRK switch: Cycle

    11. WHEELS down lights:Three green

    12. FUEL QTY SEL knob Check PNL#5

    The following Values are based on JP-4 or JP5/8

    a.Totalizer qty: Check according to flight planning.b. TEST: FWD/AFT fuel low lights ON PNL#17

    Tot: 6000 lbsA/L F/R: 2000 lbs

    c. NORM: A/L : 2675/2810 lbsF/R: 3100/3250 lbs

    d. RSVR: both 460/480 lbs

    e. INT WING: both 525/550 lbsf. EXT WING: both 2300/2420 lbs (if 370-gallon carried)both 3750/3925 lbs (if 600-gallon carried)

    g. EXT CTR: F/R: 1800/1890 lbsA/L: 0 lbs

    h. FUEL QTY SEL: NORM

    13. EPU FUEL QTY: 95 102%

    Note:If the FLCS BIT reports a failure through the FLCS warning light and the FAILlight on the FLCP, the failure cannot be reset. The BIT must be reinitiated. Inthis case, the RUN light and the FAIL light are simultaneously illuminated forthe first steps of the BIT, after which the FAIL light goes OFF unless BITdetects a subsequent failure.

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    AFTER ENGINE START Continued

    14. AVIONICS (Program as required and verify (manual or DTC)a.Threat Warning Aux: ON PNL#13

    b. CMDSRWR switch: ON PNL#13JMR switch: ON PNL#13CHAFF cmds switch: ON PNL#13FLARE cmds switch: ON PNL#13MODE knob: Set as required PNL#13

    c. ECM switch: Set as required (OPR)d. MFD

    DTE: LoadS-Jettison: Preset Jettison and exit S-J modeFlightplan: Check and SetMaster Mode: Set as required

    e. DED UFCCommunications: CheckALOW MSL BINGO: CheckCRUS TACAN: CheckVIP VRP Bullseye: SET as required

    f. AUDIOCOM1&2 Volume SET & check PNL#15MSL /Threat Volume SET & check PNL#15ILS Volume knob SET & check PNL#15

    15. DBU CHECK (AFTER FLCS BIT completed) PNL#18a. DIGITAL BACKUP switch: BACKUPb. DBU ON warning light: Verify ONc. Operate controls: All surfaces respond normallyd. DIGITAL BACKUP switch: OFFe. DBU ON warning light: Verify OFF

    16. TRIM CHECKSa. TRIM AP DISC switch: DISC PNL#12b. Stick TRIM buttons: Activate in ROLL and PITCH

    No control surface, no indicator motionc. TRIM AP DISC switch: NORMd:Stick TRIM buttons: Check and center

    Control surface & indicator motione. Rudder trim check: YAW TRIM knob:

    Check and center

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    AFTER ENGINE START Continued

    17. AIR REFUEL CHECKS

    a. AIR REFUEL switch: OPEN PNL#3CHECK RDY light ON, DSC light OFF

    b.A/R DISC button: DepressDSC light ON; RDY Light OFFthen 3sec later, RDY light ON, DSC light OFF

    c. AIR REFUEL switch: CLOSE

    18. EPU CHECK

    a. EPU GEN and EPU PMG lights: Confirm OFFb. O: 100% PNL#25c. Toebrakes: Engaged. EPU switch: OFF PNL#4e. EPU switch: NORM PNL#4f. THROTTLE: IDLE + 10%g. EPU/GEN TEST switch: EPU/GEN and hold. PNL#22

    Check lights: EPU AIR light ON PNL#4

    EPU GEN and EPU PMG light OFFFLCS PWR lights ON PNL#22EPU RUN light ON within 5 seconds

    h. EPU/GEN TEST switch: Release (OFF) PNL#22i. THROTTLE IDLEj. O: NORMAL PNL#25If no run light within 10 sec, reinitiate test with throttle at IDLE +15%

    19. OBOGS CHECK (At least 2 minutes after engine start)

    a. OBOGS BIT switch: BIT PNL#22b. VERIFY LIGHT: OXY LOW (right brow) ON for 10sec then OFFc. Pressure: CHECK 25-40 PSId. Mode Lever: PBG/ON (as required)e. Diluter lever: NORMf. EMERGENCY lever NORMg. FLOW indicator Check

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    BEFORE TAXI

    TAXI

    1. NoseWheel Steering2. Parking Brake

    3. Seat4. Wheelbrakes

    EngageRelease

    Armed Caution light OFFTest

    Note 1: Beware of spending excessive time checking the aircraft. Alwaysrefer to your next TOS.

    Note 2: Be sure the INS reaches stage 3 or higher before scrambling.Below stage 3 initial alignment, Gyros, Hud pitch ladder, compasses,

    HSI,will be inopNote 3: Excessive use of wheel brakes and/or differential braking is to be

    avoided Maximum safe taxi speed on ramps is 20Kts.Max 80% RPM - Think FOD!

    1. Landing Lights2. Drift Co Switch3. INS Check

    4. INS switch5. Canopy6. Aircraft Lights7. Radio Tower

    ON PNL#1Set Norm PNL#14Check Stage 8.3

    Check ALIGN flashes in HUDNAV position PNL#9 Closed locked - no lightSet Wing /Fus ON PNL#2Remove chocks - Request Taxi

    IF CHECKS Durin Taxi

    1. Pressure Instruments- AIRSPEED: Zero- ALTIMETER: Set (NI)- VVI: Zero Remember possible errors.

    2. Gyroscopic Instruments

    - TURNS: Needle/balls HSI Following3. Navigation Instruments- NAV: Check correct bearings for WAYPOINTS- TACAN: Set TCN channel and Course for Departure

    4. Miscellaneous:- HUD Compass tape Track heading change- HSD Compass tape Track heading change- HSI Compass tape Track heading change- STDBY Compass - Track heading change

    - Clock and Chrono : Check and Reset- Engine instruments: Check

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    BEFORE TAKE OFF

    1. PROBE HEAT switch2. ALT FLAPS switch3. MANUAL TF FLY UP switch

    4. Trims

    5. ENG CONT switch6. Speedbrake7. Departure Clearance8. Radar Altimeter9. Stores Config Switch10. GND JET ENABLE switch11. External Tanks

    12. Flight Controls13. OIL pressure14. All warning & caution lights15. Tacan16. Review Speeds

    Rotation , T/O, Climb speeds

    PROBE HEAT (NI) PNL#22NORM PNL#18ENABLE PNL#18

    Check PITCH and YAW centred,ROLL as requiredPRICheck closedReceivedSet ON PNL#10Cat1/Cat3 as required PNL#1As required PNL#1Check feeding then NORM PNL#5

    CycleCheck & OFFCheck PSIVerify reading if availableCommit to memory

    NORMAL TAKE OFF

    1. HSI

    2. Toe brakes3. RPM 90%

    4. Brakes5. Throttle6. NWS7. Rotation

    8. Positive Climb

    Check on Runway heading

    HOLDCheck gauges & lightsOil pressure increase nozzle closingEngine instruments in the greenNO CAUTION / NO WARNINGReleaseFull MIL, AB as requiredDisengage at 70 ktsAs computed

    (VSI + Alt) Brakes, Gear Up

    Normal engine operation during MIL takeoff is indicated by an exhaustnozzle position of 15% or less after 5 seconds at MIL.

    Apply Power smoothly, note computed speeds for 8-12 degrees pitchrotation as briefed.

    Do not exceed 14 degrees pitch in rotation.

    Insure LG is up and locked before exceeding 300 knots.

    Since TEF and LG retract at the same time, do not rush LG retraction

    after takeoff, a significant loss of lift may occur.

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    1. Master Mode2. Master ARM3. Radar4. Chaff/ Flares PGM mode5. ECM Jammer6. RWR

    7. RWR Mode7. PFD8. Master A/C Lights9. MFD10. A/G Weapons11. LASER Switch12. Volumes13. TGP pod14. AGM65 Missile power15. AIM-9 Cooling head16. CAT config17. Radio Flight

    As Required AG or AASet ARM PNL#16As RequiredAs Required PNL#13As Required PNL#13Check On PNL#13

    Diamond Float mode or as required PNL#26Check no FaultsCheck Off PNL#12Cycle/ Req dataSet release parametersON if required PNL#16Check threat, com, msl vol PNL#15Activate if required double checkCheck ON if required double checkCheck CoolCheck correct PNL#1Set Defensive Formation

    Note:Avoid Radio Chatter when entering enemy airspace unless in case of

    emergency. Use A/C or hands signals instead.

    1. Landing Light

    2. U/C3. Engine4. FUEL5. Radio6. DED7. MFD8. DRIFT CO Switch9. Wingman

    Off PNL#1

    Check Retracted - handle light OffGauges in the GreenVerify Tank feeding and set NORM PNL#5Call airborneSTP mode, Select NXTCycle As RequiredSet Drift PNL#14Set Formation and Route

    AIRBORNE / CLIMB

    FENCE IN

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    INITIAL POINT

    1. Radio Flight2. Master ARM3. Weapons

    4. Attitude5. DED A-LOW6. Threat7. Master Mode / Radar8. CounterMeasures9. Radio

    Split, Weapons Free, EngageCheck ARM PNL#16Check SET

    Check Speed and ALTSET on Weapon Min releaseAssume (A/A) - AWACSAs RequiredCheck As RequiredCall in HOT

    EGRESS

    Check to friendly airspaceCheck for DamageAs Required (A/A)Check Nearest threatCycle As RequiredSet Cat I (if possible) PNL#1As Required PNL#13At pilot discretion PNL#13Rejoin / Cover

    Set for EgressCheck Status & Fuel - Rejoin

    1. Heading2. Caution Panel3. Master Mode4. Awacs5. MFD6. Store config7. ECM Jammer8. EWMS mode+pgr9. Flight

    10. DED A-LOW11. Flight

    Note:When engaging an A/A threat, Jettison remaining A/G stores, and select CatI

    config. If threat is less than 10 Nm, Use Dogfight Mode

    FENCE OUT

    1. Threat2. Master ARM3. Laser switch3. Master Mode4. Radar5. ECM Jammer6. RWR Mode7. Chaff/ Flares Auto disp8. PFD9. Radio Flight

    Assume A/A Threat - AWACSSet Safe (According to Threat)Set Off PNL#16Set NavOff (According to Threat)Off (According to Threat) PNL#13As requiredSet Off PNL#13Check no FaultsFuel Check (Dest or Alt)

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    IF CHECKS MNEMONIC

    Holding/enroute

    W Weather

    H HoldingO Obtain app clearanceL Letdown plate reviewD Descent checksS Speeds

    Approach setup

    M Minimas

    A AltimeterI Initial descent rateL Letdown plateM Missed ApproachA Approach speedsN Navaids

    DESCENT

    Note:For Approach use the F4 Letdown plates

    1. Master Mode2. Master ARM3. Altimeter

    4. Approach plates5. Instr Mode Select switch

    6. TACAN channels7. HSI course and bearings8. GPS9. Speeds

    Set NAVSet Safe PNL#16Set & Check (transition ALT)Check altimeter readings vs HUD altitudeReviewedTCN/ILS or NAV/ILS PNL#21

    Set according to approach plateSet according to approach plateInput coordinates of IAFCompute final approach speeds

    APPROACH

    See Quick Reference charts volume to compute speeds

    1. Radio Tower2. Fuel3. At IAF

    Call InboundCheck Quantity/Transfer/BalanceFollow ATC procedures unless VisualApproach.

    Note:Unless previously cleared aerobatic manoeuvre is not permitted over the airfield.

    Pitch and bank should not exceed 70 IAS

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    BEFORE LANDING

    1. Radio Tower (5Nm out)2. A/C Weight3. A/C LDG/Taxi Lights

    4. Gear5. Speed brake6. Drift Co switch7. Traffic8. Radar/EW

    Request LandingVerify/Update VrefSet On/ On PNL#1

    Check 3green-handle light offFully DeployedSet Norm ICPAnnounce traffic in sight if requiredCheck all STBY PNL#13

    FINAL APPROACH

    1. Speed brake

    2. Gear3. Speed4. AoA5. Touchdown

    Extended

    Down 3 greensVref as computedGreen : 1111 to 13 AOA

    LANDING

    1. Speed2. AOA3. Speed 100 kts

    4. Wheel brakes

    Throttle IdleMaintain 13 for max aerobrakingRide the nosewheel on the groundMaintain Full AFT stickEngage NWS at taxi speed or when req.As required

    CLOSEOFF PNL#22OFF PNL#15As required PNL#1

    OFF PNL#10

    1. Speedbrake2. PROBEHEAT switch3. ILS4. Landing/ Taxi Lights

    5. Radar Alt

    AFTER LANDING

    Note:Final approach speed/13 AOA Cross Check:

    136 kts + 4 kts per 1000 Pound of FUEL/STORE weight

    Note:Smoothly apply moderate to heavy braking to decelerate to taxi speed. Using

    less than moderate braking increases the likelihood of a hot brake(s)

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    AERIAL REFUELLING

    Tanker rejoin :1. Radio2. TCN

    3. TCN Mode4. Heading5. AltitudeBefore Precontact:6. Master ARM7. Sensors8. EW Mode knob &ECM9. FCR10. RDR ALT

    11. EXT Lights12. ANTI COLLISION light13. AIR REFUEL switch14. AR status indicator15. SeatContact:16. Boom Operator17. AR status indicator18. Fuel Transfer

    Disconnect:19. A/R DISC button20. ThrottlePost Air refuelling:21. Seat22. Air Refuel switch23. Fuel quantity24. Master Arm / SMS25. Tacan

    26. EW Mode knob &ECM27. FCR28. RDR ALT29. EXT Lights

    Request RefuellingSelect TCN Channel (Texaco)

    SET A/A TRCourse to Intercept (HSI)Tanker ALT 1000 Ft

    Check Safe PNL#16Check Nose ColdSTBY and OFFSTBYSTBY

    DIM (night) STEADYOFF at NightOpen PNL#3Check RDY Light OnSAFE (As desired)

    Follow Instructions and LightsCheck AR/NWS Light OnMonitor

    DepressDecrease power

    ARMCLOSECheckAs requiredAs required

    As requiredAs requiredAs requiredAs required

    Note: Tanker overtake speedOver 1Nm : 100 Kts overtake

    6000 Ft : 60Kts5000 Ft : 50Kts

    Decrease overtake speed by 10 Kts for every 1000 Ft closure.When within 1000 Ft to Tanker: Do not exceed 10Kts overtake.

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    PRIOR TO ENGINE SHUT DOWN

    1. Radio (tower menu)2. Ejection Seat

    3. RWR PWR4. JMR&ECM PWR5. Chaff & Flares CMDs6. HUD7. L/R Hardpoints8. FCR9. MMC (FCC)10. ST STA (SMS)11. MFD

    12. UFC/DED13. D/Link14. GPS15. INS16. EPU

    17. CNI switch

    Request chocks in placeSafe

    OFF PNL#13OFF PNL#13OFF PNL#13ICP SYM knob OFF PNL#11Power OFF PNL#10Power OFF PNL#10Power OFF * PNL#9Power OFF PNL#9Power OFF PNL#9

    Power OFF PNL#9Power OFF PNL#9Power OFF PNL#9Power OFF PNL#9OFF(No crewchief able to insert the EPU pin)BACKUP

    ENGINE SHUT DOWN

    1. AIR Source2. Radios & Volume knobs3. Throttle

    4. Throttle (Idle Detent)5. JFS RUN light

    After MAIN GEN drops offline:

    6. EPU Light check7. Engine Feed switch8. Master LIGHT switch9. Canopy10. Main Power11. Oxygen Regulator

    Set OFF PNL#6All OFF PNL#15- Stabilize at 75-78% RPM for 5-10 sec- Idle to allow nozzle to open (1 to 2 sec)Cut OFF position PNL#20Check

    EPU GEN / EPU PMG lights OFF PNL#4Set OFF PNL#3OFF PNL#2OpenOFF -2 clicks when RPM

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    HOTPIT REFUEL

    Prior to HOTPIT Entry1. AFTER LANDING CHECKS

    2. Radio Frequency3. AIR REFUEL switch4. TACAN power knob5. GND JETT ENABLE switch

    Prior to Hot Refuelling1. EPU switch (safety pin in)2. Canopy3. Radio

    During Hot Refuelling2. Radio freq3. Flight controls

    Hot Refuelling complete1. AIR REFUEL switch2. EPU GEN & EPU PMG lights3. EPU switch (safety pin out)

    4. Taxi

    Complete

    Check proper tower frequency tunedOpen ; RDY light ON PNL#3Power OFF PNL#15OFF PNL#2

    OFF PNL#4As desiredrequest Hot Refuelling

    Monitor Tower freq & guardDo not touch - Ensure hands are visible

    CLOSE PNL#3Confirm OFFNORM PNL#4

    Taxi clear of the hotpit area and contactTower

    Note:Hotpit refuelling requires ground crew to establish intercom communication,inspect tires and install the EPU safety pin. This last action is simulated by

    switching the EPU OFF during hotpit refuel

    SUPPLEMENTAL PROCEDURE : ILS1. DED2. T-ILS button3. ILS frequency4. DCS5. HSI6. INSTR Mode knob

    Verify CNI displayDepress and ReleaseKey in and ENTRPosition asterisks about selectable items.Set Inbound localizer courseILS/TCN or ILS/NAV

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    COCKPIT LAYOUT

    PANEL #1: Gear panelPANEL #2: Ext lights

    PANEL #3: Fuel PanelPANEL #4: EPU PanelPANEL #5: Fuel QTYPANEL #6: Air sourcePANEL #7: Jet StartPANEL #8: Eng gaugesPANEL #9: Avionic pwrPANEL #10: SNSR pwrPANEL #18: Alt FlapsPANEL #19: Mpo

    PANEL #20: Idle detentPANEL #21: Instr. ModePANEL #22: Test Panel

    PANEL #11: HUD togglePANEL #12: Trim controlsPANEL #17: Caution lightsPANEL #24: HUD controls

    PANEL #14: ICPPANEL #15: AudioPANEL #23: UHFPANEL #25: O

    PANEL #13: EW ManagementPANEL #16: MISC (armement)

    PANEL #26: TWP (RWR)

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