This section of the documentation lists the various sections and parameters that have been made obsolete in Microsoft Flight Simulator 2024. These parameters no longer exist in the simulation code and as such should never need to be used in any of the various CFG files used by your SimObjects (contrary to legacy / deprecated parameters which may still have a use).

ai.cfg

[TAKEOFF]

ParameterDescriptionTypeRequired
takeoffVerticalSpeedGroundNot currently used by the simulation.FloatNo
takeoffVerticalSpeedAirNot currently used by the simulation.FloatNo
takeoffAirspeedAirMultiplierNot currently used by the simulation.FloatNo

[LANDING]

ParameterDescriptionTypeRequired
horizontalSpeedErrorMultiplierNot currently used by the simulation.FloatNo
maxThrottleRateNot currently used by the simulation.FloatNo
maxThrottleSlopeNot currently used by the simulation.FloatNo
correctPitchDeltaMultiplierNot currently used by the simulation.FloatNo

[SIMPLIFIEDSIM]

ParameterDescriptionTypeRequired
brakesMultiplierNot currently used by the simulation.FloatNo
throttleFactorNot currently used by the simulation.FloatNo
portanceFactorNot currently used by the simulation.FloatNo
spoilersPortanceNot currently used by the simulation.FloatNo
flapsPortanceNot currently used by the simulation.FloatNo
airResistanceFactorXYZNot currently used by the simulation.List of 3 FloatsNo
spoilersXYZFactorNot currently used by the simulation.List of 3 FloatsNo
flapsXYZFactorNot currently used by the simulation.List of 3 FloatsNo

[TOWPLANE]

ParameterDescriptionTypeRequired
turnFrequencyNot currently used in the simulation.FloatNo
turnDeltaHeaderNot currently used in the simulation.FloatNo
climbPitchDegreesNot currently used in the simulation.FloatNo
takeoffThrottleNot currently used in the simulation.FloatNo

[STICKANDRUDDER]

ParameterDescriptionTypeRequired
brakeDifferentialPIDPID to adjust the differential braking controls on ground to stay on the centerline when taking off or taxiing using copilot and/or autopilot controls.Input is the heading rotational speed error, output is the target delta between brakes.Default is: 0.001, 0.001, 0.8, 1.0, 5.0List of FloatsNo
throttleDifferentialPIDPID to adjust the differential throttle controls on ground to stay on the centerline when taking off or taxiing using copilot and/or autopilot controls.Input is the heading rotational speed error, output is the increase in throttle.Default is: 10.0, 0.001, 20.0, 10.0, 40.0List of FloatsNo

aircraft.cfg

[GENERAL]

ParameterDescriptionTypeRequired
DistanceToNotAnimateThis is the distance (in meters) to turn off animation and model behavior systems, which lowers the processing overheads for the aircraft. The approximate values by category would be: - AircraftPilot = 100 meters - FlyingAnimals = 250 meters - All others = 1000 metersDefault is 1000.FloatNo
AvailabilityIf TRUE the aircraft is available for user selection within the sim, if FALSE it can only be used as AI aircraft.Default is 1 (TRUE).BoolNo
performanceThis is a legacy entry that was used to provide an alternative description for an aircraft.StringNo
wip_indicatorThis one is for developers and can be used to indicate whether an aircraft is a work in progress or not and what state it is in. Should be omitted if the aircraft is not a work in progress.Default is 0.Integer:0 (Bad)1 (WIP)2 (Good)No

[FLTSIM.N]

ParameterDescriptionType
atc_id_enableNot currently used in the simulation.BoolYes
atc_id_colorNot currently used in the simulation.StringYes
atc_id_fontNot currently used in the simulation.StringYes

[LOADING]

Set an image to be used when starting a flight with the aircraft, along with one or more accompanying “tips” texts. The available parameters are:

ParameterDescriptionTypeRequired
ImageNameThe relative path and filename of the loading image to use for the aircraft when starting a free flight. Images should be PNG or JPEG format and 3840*2160px in size. Note that you can use LOADING_FREEFLIGHT instead of a path to get generic freeflight images instead.StringYes
Tips*N*This is a “tip” text that will be shown along with the loading image. You can have multiple tips for any image, counted from 0, and these tips can be localisable. For example:Tips0=TT:LOADING.TIPS.AIRCRAFTNAME_000Tips1=TT:LOADING.TIPS.AIRCRAFTNAME_001Tips2=TT:LOADING.TIPS.AIRCRAFTNAME_002Tips (whether localised or not) are comprised of a comma separated list, which can be formatted in the following ways: - “[PackageName],[text]” - The package name the text comes from comes first and is prefixed by @. - “[text],[category]” - The text is assigned a category (categories are listed below) and will only be shown ¡f the flight is of that category. - “[PackageName],[text],[category]” - Text comes from the specified package and will only be shown if the flight is one of the given categories.The available categories are as follows: - “TipsCategory_Default” - “TipsCategory_Flight” - “TipsCategory_Aircraft” - “TipsCategory_Activity” - “TipsCategory_Weather” - “TipsCategory_Location”StringNo

sim.cfg

[Pilot.N]

ParameterUsed ByDescriptionTypeRequired
name- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”This is a localisable string that gives the pilot a name.StringYes
image- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”This defines the path (relative to the sim.cfg file) used to illustrate the pilot character in the simulation menu.StringYes
biography- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”Here you can give a short (localisable) text to describe the pilot.StringYes
pilot- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”When set to 1, this pilot character can also be selected as a pilot.BooleanYes
copilot- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”When set to 1, this pilot character can also be selected as a copilot.BooleanYes
instructor- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”When set to 1, this pilot character can also be selected as an instructor.BooleanYes
female- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”When set to 1, the pilot character is flagged as female.BooleanNo
military- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”When set to 1, the pilot character is flagged as military.BooleanNo
TTSNeuralVoice- “GroundVehicle” - “AircraftPilot” - “GroundVehiclePilot”This is a TTS voice that will be used for the character. Can be either “Boyd” or “Jenny”.StringNo

cameras.cfg

[CAMERADEFINITION.N]

ParameterDescriptionTypeRequired
MomentumEffectNot currently used in the simulation.BoolNo
SnapPbhAdjustNot currently used in the simulation.String: - None- Commands are ignored (position remains fixed). - Ordinal- Camera moves to the next ordinal compass position in the direction of the command. - Swivel- Camera moves incrementally in the direction of the command. - Orthogonal- Camera rotates in the direction of the command (used in top-down view).No
SnapPbhReturnNot currently used in the simulation.BoolNo
PanPbhAdjustNot currently used in the simulation.String: - None - Ordinal - Swivel - OrthogonalNo
PanPbhReturnNot currently used in the simulation.BoolNo
TrackNot currently used in the simulation.- String: - None - No tracking behavior. User has manual control over the camera. - FlyBy - Fly-by mode; the camera is positioned away from the user aircraft (at a location given by ChaseDistance, ChaseAltitude and ChaseHeading values) and tracks the aircraft for ChaseTime seconds before computing a new position. - Track - Camera tracks the object while maintaining its position. - TrackBank - Camera tracks the object while maintaining its position. - FlatChase - Camera moves with the object, maintaining a fixed distance from it. Camera movements are dampened. - FlatChaseLocked - Camera moves with the object, maintaining a fixed distance from it. Camera movements are rigid.No
ClipModeThis setting is used to control how the clip planes are computed. Clip planes are used to set the minimum and maximum distances for rendering in a 3D graphics program. The relative location of these planes determines how precise the graphics engine can maintain the Z-order of objects. A discussion of clip plane management is beyond the scope of this document, however the concept is relevant to the camera system because it determines whether the camera favors near or far objects in the view.Default value is “Normal”.String: - “Normal” – The near clip plane is scaled along with the zoom level. Useful for most views. - “Minimum” – Clamps the near clip plane at its absolute minimum value (1 meter). Useful for cameras where the camera is placed close to object geometry (e.g., aircraft cameras). - “Spot” – Favors distant objects by scaling the near clip plane with altitude and distance. Useful when the camera is positioned a reasonable distance away from the target object (e.g., spot view). - “Tower” – Favors near objects by scaling the near clip plane by one-half the zoom level and clamping the far plane based on visibility settings with an absolute limit of 20km. Useful when objects at the limits of visibility aren’t important.No
ShowAxisNot currently used in the simulation.Enum: - - NO / OFF - - FrontOnly - - YES / ON / TRUE / AlwaysNo
AllowZoomNot currently used in the simulation.BoolNo
ZoomPanScalarNot currently used in the simulation.BoolNo
ShowWeatherNot currently used in the simulation.BoolNo
XyzAdjustNot currently used in the simulation.BoolNo
ShowLensFlareNot currently used in the simulation.BoolNo
PitchPanRateNot currently used in the simulation.Float 0.0 - 100.0No
HeadingPanRateNot currently used in the simulation.Float 0.0 - 100.0No

engines.cfg

[PROPELLER]

ParameterDescriptionTypeRequired
defeathering_accumulators_availableValue to indicate if de-feathering oil accumulators are available (TRUE, 1) or not (FALSE, 0).Default value is 0 (FALSE).BoolNo
advance_ratio_on_effective_betaThis is the factor of the advance ratio on the effective beta.Default value is 0.2.No longer used by Microsoft Flight Simulator 2024. For legacy aircraft this has been replaced by the table prop_power_cf, or is internally calculated when using the modern flight model.FloatNo

[TURBOPROP_ENGINE]

ParameterDescriptionTypeRequired
engine_friction_tableDefines the friction/torque applied to the engine - especially when shutting down - using a 1D Curve of up to 8 paired values. Values are ftlbs for torques, and RPM for engine rotation speeds.Default values are:engine_friction_table = -1000:0.3, 0:0.3, 1000:0.3, 2000:0.3, 3000:0.3, 4000:0.3, 6000:0.31D Curve of FloatsNo

flight_model.cfg

[AIRPLANE_GEOMETRY]

ParameterDescriptionTypeRequired
wing_pos_apex_lonLongitudinal (z) distance of the wing apex - as measured at the centerline of the aircraft - from the Datum Reference Point point in ft. This distance is measured positive in the forward (aircraft nose) direction. Note that this value will have no effect if the compute_aero_center value is 0 - which is generally how it should be.Currently not used in Microsoft Flight Simulator 2024. Instead you should be using the aero_center_lift parameter.FloatNo

[CONTACT_POINTS]

ParameterDescriptionTypeRequired
max_number_of_pointsThe number of contact points for the aircraft. Note that if this parameter is omitted, then the maximum will be set to 25 and any defined points above this value will be ignored. It should also be noted that the simulation will expect the exact number of point.N definitions as the maximum given here. So, if you have this set to 10, you will need to have defined 10 points (0 - 9).Default value is 25.IntegerNo

[HELICOPTER]

ParameterDescriptionTypeRequired
reference_lengthThe overall length of the helicopter fuselage (excluding rotors), in ft.FloatYes
reference_frontal_areaThe front facing area of the helicopter fuselage (excluding rotors), in sqft.FloatYes
reference_side_areaThe lateral facing area of the helicopter fuselage (excluding rotors), in sqft.FloatYes
lift_aero_centerThe longitudinal position, in feet, from the Datum Reference Point of the helicopter that represents the vertical aerodynamic center.Default value is the Z component of the Datum Reference Point.FloatNo
side_aero_centerThe longitudinal position, in feet, from the Datum Reference Point of the helicopter that represents the lateral aerodynamic center.Default value is the Z component of the Datum Reference Point.FloatNo
correlator_availableThis defines whether the helicopter has a correlator that maps the throttle onto the collective (1, TRUE), or not (0, FALSE).NOTE: This parameter will no longer work and should not be used. It has been deprecated in favour of collective_to_throttle_correlator parameters.Default value is 1 (TRUE).Bool

systems.cfg

[RADIOS]

ParameterDescriptionTypeRequired
CollisionAvoidanceThis parameter can be used to indicate the presence of TCAS and / or FLARM systems. If supplying this parameter you give two values separated with a comma (val1, val2) where the first corresponds to the TCAS and the second to the FLARM. For the TCAS you can give one of the following values: - 0 - No TCAS capability (no transponder) - 1 - Only transponder responses - 2 - Standard TCAS - 3 - External TCASThis parameter can be used to indicate the presence of a FLARM system. It can have the following values: - 0 - No Flarm - 1 - Flarm installedList of IntegersNo

[AUTOPILOT]

ParameterDescriptionTypeRequired
autoland_availableSetting this to 1 (TRUE) makes the autopilot autoland system available to the aircraft, otherwise set it to 0 (FALSE) to disable autoland.BoolNo
pitch_use_trimWhen set to 1 (TRUE) the autopilot will use the trim to hold pitch, and when set to 0 (FALSE) it will use the elevator directly.BoolNo
max_throttle_rateThis value sets the maximum rate at which the autothrottle will move the throttle position.FloatNo
pitch_proportional_controlPitch proportional controller constant.FloatNo
pitch_integrator_controlPitch integral controller constant.FloatNo
pitch_derivative_controlPitch derivative controller constant.FloatNo
pitch_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the pitch integrator function is active.FloatNo
pitch_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the pitch derivative function is active.FloatNo
roll_proportional_controlRoll proportional controller constant.FloatNo
roll_integrator_controlRoll integral controller constant.FloatNo
roll_derivative_controlRoll derivative controller constant.FloatNo
roll_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the roll integrator function is active.FloatNo
roll_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the roll derivative function is active.FloatNo
hdg_proportional_controlHeading proportional controller constant.FloatNo
hdg_integrator_controlHeading integral controller constant.FloatNo
hdg_derivative_controlHeading derivative controller constant.FloatNo
hdg_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the heading integrator function is active.FloatNo
hdg_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the heading derivative function is active.FloatNo
vs_proportional_controlVertical speed proportional controller constant.FloatNo
vs_integrator_controlVertical speed integral controller constant.FloatNo
vs_derivative_controlVertical speed derivative controller constant.FloatNo
vs_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the vertical speed integrator function is active.FloatNo
vs_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the vertical speed derivative function is active.FloatNo
nav_proportional_control_ex1Proportional controller constant in lateral navigation modes.FloatNo
nav_integrator_control_ex1Integral controller constant in lateral navigation modes.FloatNo
nav_derivative_control_ex1Derivative controller constant in lateral navigation modes.FloatNo
nav_integrator_boundary_ex1The boundary, or maximum signal error, in degrees in which the integrator function is active.FloatNo
nav_derivative_boundary_ex1The boundary, or maximum signal error, in degrees in which the derivative function is active.FloatNo
nav_yaw_proportional_controlProportional controller constant in yaw navigation modes.FloatNo
nav_yaw_integrator_controlIntegral controller constant in yaw navigation modes.FloatNo
nav_yaw_derivative_controlDerivative controller constant in yaw navigation modes.FloatNo
nav_yaw_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the yaw integrator function is active.FloatNo
nav_yaw_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the yaw derivative function is active.FloatNo
gs_proportional_controlProportional controller constant in glideslope mode.FloatNo
gs_integrator_controlIntegral controller constant in glideslope mode.FloatNo
gs_derivative_controlDerivative controller constant in glideslope mode.FloatNo
gs_integrator_boundaryThe boundary, or maximum signal error, in degrees in which the glideslope integrator function is active.FloatNo
gs_derivative_boundaryThe boundary, or maximum signal error, in degrees in which the derivative function is active.FloatNo
flc_proportional_controlThe FLC proportional control mode value.Default is 20.0.FloatNo
flc_integrator_controlThe FLC integrator control mode value.Default is 1.0.FloatNo
flc_derivative_controlThe FLC derivative control mode value.Default is 50.0.FloatNo
flc_integrator_boundaryThe FLC integrator control boundary.Default is 100.0.FloatNo
flc_derivative_boundaryThe FLC derivative control boundary.Default is 1000.0.FloatNo

attached_objects.cfg

[SIM_ATTACHMENT.N]

ParameterDescriptionTypeRequired
always_execute_associate_jsWhen set to 1 (TRUE), this will force the SimAttachment to run any JS used by the attachment when it is hidden in the simulation.Default value is 0 (FALSE).BooleanNo

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