A pilot initiated ejection will always eject both crew members. The EJECT CMD lever controls what happens when the RIO ejects: In PILOT mode (lever forward), only the RIO will be ejected. In MCO mode, both pilot and RIO initiated ejection will eject both crew members

Switch controlling display of data and ADF on the HSD and ECMD. BOTH enables display of the ADF bug and navigation data block. DATA enables display of only the navigation data block. OFF disables display of either.

Thumbwheel controlling console lights and red floodlights. 0 turns off both console and red floodlights, 1-14 sets the console lights to an increasingly bright setting.

In air-to-ground mode up and down moves the designator and forward designates. In all other cases up and down selects VSL HI and VSL LO ACM-modes respectively and forward selects PAL.

Switch used to select which hemisphere aircraft is in for DG and SLAVED modes. Critical for correct earth-rate correction.

LAUNCH BAR – Selection switch – When held in ABORT lifts the launch bar for launch abortion. Spring-loaded to NORM (Normal) which is the standard position. Not currently used in DCS.

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Readout drum indicating the source of the data displayed on the TID readouts. Might be blank for sources not having its own text on the drum.

Warning light indicating flap retraction failure with greater than 225 knots indicated airspeed. Also indicates safe Mach number exceeded.

Advisory light indicating overheat or overpressure in the AWG-9 coolant flow or that the overtemperature switch has shut down the coolant pump.

Flap Position is displayed by an indicator moving between UP and DOWN. The first marked section of the indicator indicates maneuver flap-range. The landing gear is indicated as follows:

Image shows an F-14A with AN/ALR-45 having a third option on the HSD MODE and an ECM ORIDE which are not present in aircraft with the AN/ALR-67.

Sets if the ECM is allowed to override the current display on the HSD if a threat is detected. ORIDE allows override and OFF disables it. Only present in aircraft with AN/ALR-45.

Tape indicating angle of attack (AOA) on a scale of 0 to 30 units. (Equivalent to -10° to +40° rotation of the AoA probe.)

Three-position switch, springloaded to return from RESET. If power and altitude data from CADC is present, switch can be held in RESET for 3 seconds to allow normal (servoed) mode of operation. If set to STBY or power or CADC data is absent for more than 3 seconds system switches to backup (pressure) mode.

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Knob used to control the gain of the AWG-9 in pulse mode, normally left in detent unless needed because of clutter or jamming.

Switch selecting whether to jettison only WPNS (weapons) or MER/TER (weapon racks) in addition to weapons. Non-functional in modelled F-14 .

Button extending the amount of time before a track is dropped after last radar observation to two minutes. Normal time is 14 seconds.

The knob below and to the right of the indicator cages/uncages the indicator and allows trim to correct pitch. In pulled out position the indicator is caged. When pushed in uncages the indicator and allows pitch trim by turning the knob.

Switch used to control exterior lights. OFF disable all exterior lights and increases approach light intensity. ON enables all exterior lights and dims approach lights.

The hydraulic hand pump is located inboards of the throttle quadrant, near the pilot’s left leg. It is used to manually add hydraulic pressure for brake operation (with gear handle in the down position) or for refueling probe operation in case of a failure in the hydraulic system.

Has two engine stall warning lights (L STALL & R STALL) mounted on the left and right sides respectively. They indicate the presence of an engine stall condition in their respective engine.

Rotary drum indicator displaying currently selected radar range. Can also be blank if no range scale is used on the DDD.

SAM - SAM, steady illumination when detecting lock on from a SAM tracking radar. Flashes when missile launch is detected.

Indicator light showing status of the INS during alignment. STBY indicates power applied but not aligned. READY indicates minumum launch criteria for AIM-54. Both lights turn off when INS mode is selected. Can otherwise indicate faults.

The canopy air diffuser lever controls the flow of cabin air. The normal position, CABIN AIR, directs 70% of the conditioned air through the cockpit air diffusers and 30% through the canopy air diffusers. The CANOPY DEFOG position directs all air flow through the canopy air diffusers for canopy defog.

Pull to shut off fuel to the left engine in case of emergency. Push in to re-enable fuel-flow to the engine. Should not be used to secure the engine.

The knob on the lower left corner is used to wind up the clock by turning it clockwise and pulled out and turned to set the hour and minute hands.

Light indicating selection of STBY or XMT with the radar not yet timed out or selection of XMT with radar transmission remaining off.

Switch springloaded to center. Momentary selection of BIT indicates BIT in ALR-67. Selection of SPL (special) while BIT page 1 is displayed shows the special BIT status page while held and then for 3 seconds when released.

LIQ COOLING switch controlling the liquid cooling system for the AWG-9 and AIM-54. The AWG-9 circuit can be enabled independently of the AIM-54. This switch need to be enabled for the respective system before AWG-9 operation or AIM-54 missile preparation.

Used to select and trigger different functions in the WCS depending on current mode and hcu function. First detent is HALF ACTION, second detent is FULL ACTION. Examples of use are target acquisition and symbol hook.

Displays direct threats to own aircraft. Systems capable of engaging own aircraft and showing current intent of doing so.

The flap lever has a stepless range of motion between up and down and has two emergency positions, one emergency up and one emergency down. Both emergency positions have detents, the lever needs to be moved outboards to continue movement into these positions. Emergency up forces the flaps up, overriding the normal flap logic. Emergency down is non-functional.

Switch springloaded to center (OFF) position. Can be held to OFST (offset) and LMT (limit) position to enable respective function while held.

The manual/emergency wing-sweep handle is protected by a guard and is normally pushed in and stowed. The handle-top is extended for manual operation. For more information see Emergency Mode.

Sets local pressure in inches of mercury (in.Hg). Only used locally on the altimeter readout, all other digital indicators (via CADC) uses a set 29.92 in.Hg value.

The MASTER ARM bus is also interlocked with the landing gear control lever, disabling all releases except emergency jettison while the gear is down.

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Orange light indicating warmup when system is placed in STBY. Goes out after complete warmup. Indication during test or operation indicates a fault has occured.

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The HYD TRANSFER PUMP switch has two positions, SHUTOFF and NORMAL (guarded position). The NORMAL position (also the standard setting) will have the hydraulic transfer pump pressurize a failed hydraulic system from the other, functioning system, when it drops below 2,100 psi. The SHUTOFF position (which can be accessed by lifting the guard) is used to turn off the transfer pump in case it can’t supply enough pressure to the failed system as that would risk disabling the still operational system.

Sets local pressure in inches of mercury (in.Hg). Only used locally on the altimeter readout, all other digital indicators (via CADC) uses a set 29.92 in.Hg value.

Sets AOA lights to either FIELD or CARRIER mode, with the switch in CARRIER and wheels down the AOA lights flash if the hook isn’t down.

Instrument showing current aircraft g-load (acceleration along aircraft vertical axis). It’s graded in g from -5g to +10g. One pointer will show current g-load while the other two will indicate max reached negative and positive g-load. These can be reset by pushing the PUSH TO SET button on the lower left corner of the instrument.

At high speeds and below 10,000 feet, due to pressure changes, errors in readout up to as much as 1,200 feet when transonic and up to as much as 4,000 feet when supersonic can occur.

Caution light indicating disengagement of the automatic throttle control mode not resulting from the throttle mode switch.

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Meter with indicator needles indicating sensor elevation. Left indicator shows current actual radar antenna elevation. The right indicates commanded radar elevation while RDR is selected on HCU and TCS elevation while IR/TV is selected.

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The main throttle quadrant contains the two main-engine throttle controls, the flap lever and manual wing-sweep handle in addition to the HOTAS controls on the throttles themselves. The throttles have detents in the OFF, IDLE and MIL positions.

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Control knobs used to set pulse doppler video threshold in the CLEAR (upper half of DDD) region and in the CLUTTER (lower half of the DDD) region.

Button with green light used to indicate operation or test. When pressed with MODE in ACLS illumination indicates a successful test. The light also flashes when detecting an AN/SPN-42 radar sweeping past and illuminates when that radar has locked on for ACLS guidance.

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The CAP is used to enter data into the WCS. The MESSAGE indicator drum and buttons works similarly to the buttons on MFDs on newer aircraft.

Flashes to indicate status change on the pilot caution/advisory panel. Press to reset and turn off light until next event.

Toggle switch with light indication of selected option. Manual control of Sidewinder seeker cooling. Automatically set to ON when ACM mode is selected.

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If the HOOK BY-PASS switch is set to CARRIER the lights will flash if the arresting hook is up while the landing gear is down.

Warning light indicating that carrier motion is added to data link info and commands during landing. Indicates 10 seconds to arrival at the next point in approach pattern in other modes.

Switch used to select station 1 for jettison or weapons A/G delivery. B selects the lower pylon for release or jettison, the SW option is non-functional.

Three-position switch, springloaded to return from RESET. If power and altitude data from CADC is present, switch can be held in RESET for 3 seconds to allow normal (servoed) mode of operation. If set to STBY or power or CADC data is absent for more than 3 seconds system switches to backup (pressure) mode.

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At high speeds and below 10,000 feet, due to pressure changes, errors in readout up to as much as 1,200 feet when transonic and up to as much as 4,000 feet when supersonic can occur.

Selects cockpit and pressure suit air temperature. 0-14 is selectable with COOL and WARM placarded at each end stop. In auto 7 approximately corresponds to 21º C or 70º F. In manual the thumbwheel needs to be set for each variation in airspeed and altitude.

Projects flight and weapons data onto the forward section of the canopy/windscreen. Night mode can be selected using the control on the right side of the VDI.

Warning light indicating no data link command received for the last 2 seconds during ACL. When not in ACL it indicates no data link messages during last 10 seconds.

Shows hydraulic pressure of the combined and flight hydraulic systems. SPOIL (Spoiler) ON/OFF-flag indicates pressurization of outboard spoiler module. EMER FLT HI ON/OFF-flags indicates backup flight hydraulic system pressures when HI or LOW is selected respectively.

Displays altitude digitally on three drums showing 10 000, 1 000 and 100 of feet respectively. It also displays altitude on a pointer on a circular scale indicating 100’s of feet.

Indicates no data link message received in last 10 seconds. In ACL indicates no messages in last 2 seconds, will disengage AFCS.

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Moving the throttles to the IDLE position from OFF arms the ignition and disengages the fuel cutoff. The sideways movements of the throttles are not spring loaded, this is so the pilot can have the throttle resting at MIL power for catapult launches and prevents accidental spool down of the engines. A friction lever for selection of desired throttle movement friction is located on the left side of the throttle quadrant, beneath the flap lever.

Shows vertical velocity in thousands of feet. Can show erranous readings if sudden or abrupt changes of attitude occurs because of the changing airflow over the static probe.

The knob below and to the right of the indicator cages/uncages the indicator and allows trim to correct pitch. In pulled out position the indicator is caged. When pushed in uncages the indicator and allows pitch trim by turning the knob.

Selector switch controlling navigation reference systems. Controls which system is in use and also alignment of the INS.

Toggle switch with light indication of selected option. Commands WCS to prepare AIM-54 and AIM-7 missiles. Automatically set to ON when ACM mode is commanded.

All switches are springloaded to OFF position but held in position with solenoid to enable automatic disengagement when applicable.

The canopy control handle controls canopy operation and is located on the right cockpit wall. The handle is mounted downwards beneath the box containing the handle mechanism and the handle position texts. The canopy control handle is duplicated in the RIO cockpit.

Horizontal stabilizer position indicators, shows position of left and right stabilizer surfaces, marked L or R respectively.

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The knob on the lower left corner is used to wind up the clock by turning it clockwise and pulled out and turned to set the hour and minute hands.

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Displays direct threats to own aircraft. Systems capable of engaging own aircraft and showing current intent of doing so.

The horizontal situation display is used to display navigational information to the pilot. It can also be used to repeat the RIO’s TID to the pilot.

Advisory light indicating overtemperature or underpressure in missile coolant flow, either of which shuts down the missile coolant pump. Can also indicate that the LIQ COOLING switch is not in the AWG-9/AIM-54 position with the WCS in STBY or ON when the Phoenix fairings are installed.

Caution lights indicating fuel quantity below 1,000 pounds in aft and left or forward and right fuel feed group respectively.

Button under the ACM cover that enables jettison of stores selected on the RIO’s ARMAMENT panel. Will not jettison Sidewinders regardless if selected.

Switch controlling whether the wing or supplementary tail and position lights lights up steadily or flashes. With weight on wheels the supplementary lights are always steady.

Indicators illuminating with MCB Test switch activation to indicate left and right successful MCB circuit test respectively.

Shows fuel quantity in respective fuselage tanks. Left tape indicates left feed and aft fuselage tanks. Right tape indicates right feed and forward fuselage tanks.

Toggle switch with light indication of selected option. Selects NORM (normal) or BRSIT (boresight) operation for missile launch. Controlled by WCS when in ACM mode.

The canopy control handle controls canopy operation and is located on the right cockpit wall. The handle is mounted downwards beneath the box containing the handle mechanism and the handle position texts. The canopy control handle is duplicated in the pilot cockpit.

Leftmost indicator pointer shows wing-sweep program position which is also the max forward angle at present airspeed and altitude.

Display used for navigational information and AN/ALR-45 ECM (only in F-14A with AN/ALR-45). Has a brightness control knob, test button and a BIT indicator showing status of display (solid black when operational, showing white flags when indicating a fail condition).

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These lights are repeated on the approach lights on the nosewheel strut, allowing the LSO to see aircraft AOA during carrier landings.

Switch enabling white flood lights in the RIO cockpit. DIM and BRT (bright) settings available, switch locked to OFF unless pulled out.

AUX - Shows brake pressure in the auxilary brake pressure which can be used via the toe brakes on the pedals. Green segment indicates 2,150 to 3,000 psi (approximately 13 to 14 applications) while red indicates 1,900 to 2,150 psi (approximately 5 applications).

PARK - Shows brake pressure available for parking brakes. Green segment indicates 2,150 to 3,000 psi, red indicates 1,900 to 2,150 psi. When green there is pressure enough for approximately 3 applications.

Pull to shut off fuel to the right engine in case of emergency. Push in to re-enable fuel-flow to the engine. Should not be used to secure the engine.

Warning light, steady illumination when detecting lockon from a SAM tracking radar. Flashes when missile launch is detected.

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Control knob used to set the threshold at which a radar return is considered a jamming target. Currently non-functional in DCS.

Thumbwheel controlling console lights and red floodlights. 0 turns off both console and red floodlights, 1-14 sets the console lights to an increasingly bright setting.

Contains an indicator showing remaining quantity of liquid oxygen available. Graduated in 1 liter increments. Also has an OFF flag that is shown in case of power failure to the indicator. The indicator is tested through the INST mode on the MASTER TEST panel and should read 2 liters.

For more information see relevant chapters under Navigation and for the TID repeat Tactical Information Display (TID) and Associated Controls.

Selector switch used to modulate the amount of air from the ram air door after AIR SOURCE is set to RAM or OFF. Can be held to INCR (increase) or DECR (decrease), springloaded back to center.

Switch controlling WCS power (computer and radar). STBY turns on power to the WCS and begins radar warmup without transmission. XMT enables radar transmission if radar is ready. Display warmup time is 30 seconds, radar warmup is 3 minutes.

Two switch hats on the center RIO hand hold used to initiate release of countermeasures. The switches are mirrored in regards to functionality.

Selector switch used to jettison selected stations in normal (JETT) mode or AUX (backup) mode. The AUX position is guarded.

Lights when hook position does not correspond to handle position. Will not turn off until fully extended and may remain illuminated when lowered at high speeds due to hook blowback.

Warning light, steady illumination when detecting lockon from a AAA tracking radar. Flashes when AAA engagement is detected.

Switch enabling white flood lights in the pilot cockpit. DIM and BRT settings available, switch locked to OFF unless pulled out.

Two selector switches used to select A/G delivery mode. One switch controls whether to release in singles or pairs and the other sets whether to release once or multiple times according to settings.

Rounds remaining indicator for M-61A1 gun. Counts down from 676 but can be reset to desired readout with the knob on the right side.

Displays engine RPM (High-pressure compressor rotor speed (N2)), EGT (Exhaust Gas Temperature) and FF (Fuel Flow) for respective engine.

The indicator has markers on the right for climb (5), cruise (8.5), and stall (29), and a reference bar for on-speed approach (15).

Switch used to select station 8 for jettison or weapons A/G delivery. B selects the lower pylon for release or jettison, the SW option is non-functional.

Displays altitude digitally on three drums showing 10,000, 1,000 and 100 of feet respectively. It also displays altitude on a pointer on a circular scale indicating 100’s of feet.

Button allowing reset of inoperative secondary power supplies. If the condition triggering the inoperational state remains the affected supplies will remain inoperational.

Used to designate ground targets on the HUD and to control pilot ACM radar modes except PLM. Can be moved up/down and forward which is the designate position.

Light that illuminates to show that Sidewinder acquisition is in progress while in slaved and boresight SEAM modes. Lights up during the 4.5 second SEAM acquisition attempt, and remains lit thereafter if the seeker has locked onto a target.

Displays hydraulic pressure available from the emergency brake accumulators to the auxiliary and parking wheelbrake systems.

Analog counters used to indicate remaining quantities of loaded countermeasures. Are manually set by pushing in and rotating the knob below each counter.

Allows reset of the HSD to re-enable display if the overload protection is tripped. Also displays the HSD IR field test display on the HSD.

Shows fuel quantity in currently selected respective (L or R) tanks (feed, wing or ext) set by the QTY SEL switch on the fuel management panel.

Panel containing the control for the hydraulic transfer pump which equalizes pressure between the combined and flight hydraulic systems in case of a failure in one of them.

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The canopy air diffuser lever controls the flow of cabin air. The normal position, CABIN AIR, directs 70% of the conditioned air through the cockpit air diffusers and 30% through the canopy air diffusers. The CANOPY DEFOG position directs all air flow through the canopy air diffusers for canopy defog.

Control knob used to control radar sensitivity level at close ranges. Usually set automatically with the knob in the detent position.

Switch used to control the rate region covered by the doppler filters in pulse doppler modes and if to use edge or centroid tracking in pulse mode. These settings correspond to expected target aspect.