Epic2 panel.xml
Tag Documentation
<Logic>
Defines the logic for the swapping of the MFDs.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | No |
Child Tags
Example Value
<Logic>
<Handler>Systems_Epic2</Handler>
<MFD_UPPER>Epic2UpperMfd_2</MFD_UPPER>
<MFD_LOWER>Epic2LowerMfd_3</MFD_LOWER>
</Logic>
<Handler>
Defines the systems handler used by the simulator. This must be set to Systems_Epic2
.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Logic> | No | Yes | No |
Content
This must be set to Systems_Epic2
.
<MFD_UPPER>
Defines the instrument name for the Upper MFD.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Logic> | No | Yes | No |
Content
This must be set to the name of the upper MFD instrument as displayed in the Coherent GT debugger, usually Epic2UpperMfd_2
.
<MFD_LOWER>
Defines the instrument name for the Lower MFD.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Logic> | No | Yes | No |
Content
This must be set to the name of the lower MFD instrument as displayed in the Coherent GT debugger, usually Epic2LowerMfd_3
.
<PersistentUserSettings>
Defines options related to persistent user settings. Persistent user settings are Epic2-specific user settings that can be saved and persist across flight sessions.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
disable | Boolean | Yes (false) | Whether to disable saving of all persistent user settings. If set to true, then settings that are normally persistent will no longer be saved. This option is primarily meant to be used during development to prevent the persistent user setting feature from writing "junk" data to cloud saves when user setting names and/or values may not be finalized yet. |
Child Tags
Default Value
<PersistentUserSettings disable="false">
</PersistentUserSettings>
<AircraftKey>
(<PersistentUserSettings>
)
Defines the key prefix to use when saving persistent user settings. Airplanes that save settings using the same key prefix will "share" setting values. It is recommended to choose a unique key prefix for each airplane.
If this tag is not defined, then the key prefix will default to the airplane's ATC MODEL string. This is defined in the aircraft.cfg
file by the [GENERAL]
section's atc_model
parameter.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<PersistentUserSettings> | No | Yes | Yes |
Attributes
None.
Content
The key prefix to use when saving persistent user settings.
Default Value
None.
<Sensors>
Defines the various sensors installed on the aircraft and connected to the Epic2.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
radar-altimeter-count | Integer in range [1, 2) | No (1) | The number of installed radar altimeters. |
gps-count | Integer in range [1, 2) | No (1) | The number of installed GPS sensors. |
magnetometer-count | Integer in range [1, 2) | No (1) | The number of installed magnetometer sensors. |
stall-warning-count | Integer in range [1, 2) | No (1) | The number of installed stall warning sensors. |
flap-warning-count | Integer in range [1, 2) | No (1) | The number of installed flap warning sensors. |
adf-count | Integer in range [1, 2) | No (1) | The number of installed ADF receivers. |
xpdr-count | Integer in range [1, 2) | No (1) | The number of installed transponders. |
Child Tags
<Adahrs>
<RadarAltimeter>
<Gps>
<Magnetometer>
<StallWarning>
<LandingGear>
<FlapWarning>
<Adf>
<Transponder>
<Acas>
Default Value
<Sensors radar-altimeter-count="1" gps-count="1" magnetometer-count="1" stall-warning-count="1" flap-warning-count="1" adf-count="1" xpdr-count="1">
<Adahrs index="1" left-altimeter="1" right-altimeter="2" airspeed-indicator="1" />
<RadarAltimeter index="1" />
<Gps index="1" />
<Magnetometer index="1" />
<StallWarning index="1" />
<LandingGear index="1" />
<FlapWarning index="1" />
<Adf index="1" />
<Transponder index="1" />
<Acas type="tcas2" min-elevation="-10" max-elevation="70" />
</Sensors>
<Adahrs>
Defines options and electrical power logic for one ADAHRS sensor. One of these tags should be created for each installed ADAHRS sensor.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the tag's ADAHRS sensor. |
left-altimeter | Integer in range [1, ∞) | No | The (1-based) index of the sim altimeter from which to source left altimeter data. |
right-altimeter | Integer in range [1, ∞) | No | The (1-based) index of the sim altimeter from which to source right altimeter data. |
airspeed-indicator | Integer in range [1, ∞) | No | The (1-based) index of the sim airspeed indicator from which to source airspeed data. |
Child Tags
- [
<Electric>
] (optional)- A logic element determining whether the sensor is powered. If not provided, the sensor is always considered to be powered.
<AdmElectric>
(optional)- A logic element determining whether the Air Data Module as part of the ADAHRS is powered. If not provided, the ADM is considered to be powered when the ADAHRS is powered.
Default Value
<Adahrs index="1" left-altimeter="1" right-altimeter="2" airspeed-indicator="1" />
<RadarAltimeter>
Defines options and electrical power logic for one radio altimeter sensor. One of these tags should be created for each installed AHRS sensor.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | No |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the tag's radar altimeter sensor. |
antenna-offset | Position, as x,y,z | No | The offset of the antenna from the model origin, where positive directions is right, up, forward. |
measurement-offset | Number | No | The offset to apply to the final measurement, after the antenna offset is applied. This should be set so that the radio altimeter provides a value of 0 when the main gear touches down in landing pitch attitude. |
Child Tags
<Electric>
(optional)- A logic element determining whether the sensor is powered. If not provided, the sensor is always considered to be powered.
Default Value
<RadarAltimeter index="1" />
<Gps>
Defines options and electrical power logic for a gps sensor.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the tag's GPS sensor. |
Child Tags
<Electric>
(optional)- A logic element determining whether the sensor is powered. If not provided, the sensor is always considered to be powered.
Default Value
<Gps index="1" />
<Magnetometer>
Defines options and electrical power logic for a magnetometer.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the tag's magnetometer. |
Child Tags
<Electric>
(optional)- A logic element determining whether the magnetometer is powered. If not provided, the magnetometer is always considered to be powered.
Default Value
<Magnetometer index="1" />
<StallWarning>
Defines electrical power logic for a stall warning sensor.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the tag's sensor. |
Child Tags
<Electric>
(optional)- A logic element determining whether the sensor is powered. If not provided, the sensor is always considered to be powered.
Default Value
<StallWarning index="1" />
<LandingGear>
Defines options and electrical power logic for a landing gear indication system.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 1) | No | The (1-based) index of the indication system. |
Child Tags
<Electric>
(optional)- A logic element determining whether the indication system is powered. If not provided, the indicator is always considered to be powered.
Default Value
<LandingGear index="1" />
<FlapWarning>
Defines options and electrical power logic for a flap indication and warning system.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the indication system. |
Child Tags
<TakeoffFlapPosition>
(required)- Sets the takeoff flap position for the flap warning system
<Electric>
(optional)- A logic element determining whether the indication system is powered. If not provided, the indicator is always considered to be powered.
Default Value
<FlapWarning index="1">
<TakeoffFlapPosition />
</FlapWarning>
<TakeoffFlapPosition>
Defines the takeoff flap position to use for determining whether to fire a no takeoff warning.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<FlapWarning> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
min | Integer in range [0, ∞) | No | The minimum takeoff flap angle in degrees |
max | Integer in range [0, ∞) | No | The maximum takeoff flap angle in degrees |
Child Tags
<Electric>
(optional)- A logic element determining whether the indication system is powered. If not provided, the indicator is always considered to be powered.
Default Value
<TakeoffFlapPosition />
<Adf>
Defines options and electrical power logic for an adf receiver.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the adf system. |
Child Tags
<Electric>
(optional)- A logic element determining whether the adf is powered. If not provided, the adf is always considered to be powered.
Default Value
<Adf index="1" />
<Transponder>
Defines options and electrical power logic for a transponder.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the transponder. |
Child Tags
<Electric>
(optional)- A logic element determining whether the transponder is powered. If not provided, the transponder is always considered to be powered.
Default Value
<Transponder index="1" />
<Acas>
Defines options and electrical power logic for an airborne collision avoidance system.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Sensors> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
type | tcas1 or tcas2 | Yes (tcas2 ) | The type of ACAS system being used (this is currently ignored and TCAS-II is always used) |
min-elevation | Integer | Yes (-10 ) | The minimum elevation angle, in degrees, where an ACAS system can determine an intruder's bearing |
max-elevation | Integer | Yes (70 ) | The maximum elevation angle, in degrees, where an ACAS system can determine an intruder's bearing |
Child Tags
<Electric>
(optional)- A logic element determining whether the transponder is powered. If not provided, the transponder is always considered to be powered.
Default Value
<Acas type="tcas2" min-elevation="-10" max-elevation="70" />
<SpeedSchedules>
Defines the aircraft's speed schedules.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | No |
Attributes
None.
Child Tags
Default Value
<SpeedSchedules>
<ClimbSchedule>
<VSpeed type="Y" />
<DepartureSpeed IAS="130" />
<ClimbSpeed IAS="140" MACH="0.33" />
</ClimbSchedule>
<CruiseSpeed ias="230" mach="0.47" />
<DescentSchedule>
<DescentSpeed IAS="230" MACH="0.47" />
<ApproachSpeeds>
<FlapsSpeed flapAngle="0" IAS="150" />
</ApproachSpeeds>
</DescentSchedule>
</SpeedSchedules>
<ClimbSchedule>
Defines the aircraft's climb speed schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedSchedules> | No | Yes | Yes |
Attributes
None
Child Tags
<VSpeed
(optional)- The tag that defines which vspeed should be used with the FMS climb schedule.
<DepartureSpeed
(optional)- The tag that defines the FMS speed to use within the departure volume.
<ClimbSpeed
(optional)- The tag that defines the FMS speed to use when in the climb schedule but when not targetting a vspeed or departure speed.
Default Value
<ClimbSchedule>
<VSpeed type="Y" />
<DepartureSpeed IAS="130" />
<ClimbSpeed IAS="140" MACH="0.33" />
</ClimbSchedule>
<VSpeed>
Defines the aircraft's speed schedules.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<ClimbSchedule> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
type | 2 or y | Yes (y ) | The vspeed to use in the climb schedule. For turboprops this will be Vy (best angle of climb), for jets this will be V2 |
Child Tags
None.
Default Value
<VSpeed type="y" />
<DepartureSpeed>
Defines the aircraft's departure speed for the climb speed schedule. This is used in the departure volume, which is either 2500ft AGL or up to 4nm from the origin airport.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<ClimbSchedule> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
ias | Integer | Yes (130 ) | The airspeed to use for this part of the speed schedule |
Child Tags
None.
Default Value
<DepartureSpeed ias="130" />
<ClimbSpeed>
Defines the aircraft's climb speed for the FMS climb schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<ClimbSchedule> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
ias | Integer | Yes (140 ) | The airspeed to use for this part of the speed schedule |
mach | Integer | Yes (0.33 ) | The mach speed to use for this part of the speed schedule |
Child Tags
None.
Default Value
<ClimbSpeed ias="140" mach="0.33" />
<CruiseSpeed>
Defines the aircraft's cruise speed for the FMS speed schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedSchedules> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
ias | Integer | Yes (230 ) | The airspeed to use for this part of the speed schedule |
mach | Integer | Yes (0.47 ) | The mach speed to use for this part of the speed schedule |
Child Tags
None.
Default Value
<CruiseSpeed ias="230" mach="0.47" />
<DescentSchedule>
Defines the aircraft's descent speed schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedSchedules> | No | Yes | Yes |
Attributes
None
Child Tags
<DescentSpeed
(optional)- The tag that defines the FMS speed to use for descent.
<ApproachSpeeds
(optional)- The tag that defines the FMS speeds to use when in the approach volume.
Default Value
<DescentSchedule>
<DescentSpeed IAS="230" MACH="0.47" />
<ApproachSpeeds>
<FlapsSpeed flapAngle="0" IAS="150" />
</ApproachSpeeds>
</DescentSchedule>
<DescentSpeed>
Defines the aircraft's descent speed for the FMS descent speed schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DescentSchedule> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
ias | Integer | Yes (230 ) | The airspeed to use for this part of the speed schedule |
mach | Integer | Yes (0.47 ) | The mach speed to use for this part of the speed schedule |
Child Tags
None.
Default Value
<DescentSpeed ias="230" mach="0.47" />
<ApproachSpeeds>
Defines the aircraft's approach speeds based on flap angle for the FMS descent speed schedule.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DescentSchedule> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
ias | Integer | Yes (230 ) | The airspeed to use for this part of the speed schedule |
mach | Integer | Yes (0.47 ) | The mach speed to use for this part of the speed schedule |
Child Tags
<FlapsSpeed>
(optional)- Defines an approach speed based on a flap angle.
Default Value
<ApproachSpeeds>
<FlapsSpeed flapAngle="0" IAS="150" />
</ApproachSpeeds>
<FlapsSpeed>
Defines the aircraft's approach speed based on the flap angle for the FMS descent speed schedule. This applies when the aircraft is in the approach volume, and the selected approach speed is based on the lowest speed where the current flap angle is greater than or equal to the defined flap angle.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DescentSchedule> | No | No | No |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
flapAngle | Integer | No | The flap angle for this approach speed in the descent schedule |
ias | Integer | No | The airspeed to use for the approach speed based on this flap angle |
Child Tags
None.
Default Value
<FlapsSpeed flapAngle="0" IAS="150" />
<DisplayUnits>
Defines the configuration options for the aircraft display units.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | No |
Attributes
None.
Child Tags
Default Value
<DisplayUnits>
<DisplayUnit index="1" radio-altimeter="1" />
<DisplayUnit index="2" radio-altimeter="2" />
<DisplayUnit index="3" radio-altimeter="2" />
<DisplayUnit index="4" radio-altimeter="2" />
<GraphicsModule index="1" />
<GraphicsModule index="2" />
<PfdConfig>
<SpeedReference bugIconVisible="false" alwaysMagenta="true" />
</PfdConfig>
</DisplayUnits>
<DisplayUnit>
Defines configuration objects for a single display unit.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DisplayUnits> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer | No | The index of the display unit. The left PFD has an index of 1, upper MFD is 2, lower MFD is 3, and right PFD is 4. |
radio-altimeter | Integer | No | The radio altimeter used by this display unit. |
ahi-side | left or right | Yes | Overrides which side of the PFD the Artificial Horizon should be displayed on. |
Child Tags
None.
Default Value
<DisplayUnit index="1" radio-altimeter="1" />
<GraphicsModule>
Defines electrical power logic for a graphics module. The graphics module controls the display of avionics. If either AGM is powered, the PFD will be powered. The upper MFD display unit is powered by AGM1, while the lower MFD display unit is powered by AGM2.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DisplayUnits> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
index | Integer in range [1, 2) | No | The (1-based) index of the transponder. |
Child Tags
<Electric>
(optional)- A logic element determining whether the transponder is powered. If not provided, the transponder is always considered to be powered.
Default Value
<GraphicsModule index="1" />
<PfdConfig>
Defines configuration options for the PFD.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<DisplayUnits> | No | Yes | Yes |
Attributes
None.
Child Tags
Default Value
<PfdConfig>
<SpeedReference bugIconVisible="false" alwaysMagenta="true" />
</PfdConfig>
<SpeedReference>
Defines configuration options for the digital speed reference readout located above the PFD speed tape.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<PfdConfig> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
bugIconVisible | true or false | No (false ) | Whether the currently active speed's bug icon should be displayed in the speed readout |
alwaysMagenta | true or false | No (true ) | Whether the speed reference readout should always be displayed in magenta. |
Child Tags
None.
Default Value
<SpeedReference bugIconVisible="false" alwaysMagenta="true" />
<AirframeConfiguration>
Defines configuration options for the airframe.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
None.
Child Tags
Default Value
<SpeedReference bugIconVisible="false" alwaysMagenta="true" />
<SpeedLimits>
Defines the airframe speed limits
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<AirframeConfiguration> | No | Yes | No |
Attributes
None.
Child Tags
Default Value
None.
<Vmo>
Defines the airframe operating airspeed limit
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedLimits> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
unit | kias or keas | No | The unit for the vmo speed limit |
Content
Integer.
Child Tags
None.
Default Value
None.
<Mmo>
Defines the airframe operating mach limit
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedLimits> | No | Yes | Yes |
Attributes
None.
Content
Number, as a mach.
Child Tags
None.
Default Value
None.
<Gear>
Defines the airframe landing gear configuration limit speed. Multiple <Gear>
tags are required to define the various landing gear operating, extension, retraction or extended speed limits.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<SpeedLimits> | No | No | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
type | retraction , extension , operating , or extended | Yes | Sets the gear configuration type. If not defined, it will default to a landing gear operating (Vlo) speed limit. |
Content
Integer, as KIAS.
Child Tags
None.
Default Value
None.
<VSpeeds>
Defines the available airframe vspeeds and their defaults. These must be present otherwise no vspeeds will be able to be sent to the PFD
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<AirframeConfiguration> | No | Yes | No |
Attributes
None.
Child Tags
Default Value
None.
<Takeoff>
Defines the takeoff vspeeds
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<VSpeeds> | No | Yes | No |
Attributes
None.
Child Tags
Default Value
None.
<Landing>
Defines the landing vspeeds
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<VSpeeds> | No | Yes | No |
Attributes
None.
Child Tags
Default Value
None.
<VSpeed>
Defines a vspeed type and default airspeed.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Takeoff> | No | No | No |
<Landing> | No | No | No |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
label | String | No | Sets the vspeed label, this will be shown on the flight management window. |
default | Integer | No | Sets the vspeed default airspeed. |
Child Tags
None.
Default Value
None.
<BasicOperatingWeight>
Defines the airframe's basic operating weight in pounds.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<AirframeConfiguration> | No | Yes | No |
Attributes
None.
Content
Integer - weight in pounds.
Child Tags
None.
Default Value
None.
<AveragePassengerWeight>
Defines the airframe's average passenger weight in pounds.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<AirframeConfiguration> | No | Yes | Yes |
Attributes
None.
Content
Integer - weight in pounds.
Child Tags
None.
Default Value
<AveragePassengerWeight>150</AveragePassengerWeight>
<Autopilot>
Defines the autopilot configuration objects.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
None.
Child Tags
Default Value
<Autopilot>
<FlightLevelChange type="FLC" />
</Autopilot>
<FlightLevelChange>
Defines the autopilot configuration objects.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Autopilot> | No | Yes | Yes |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
type | FLC or SPD | No | Which autopilot mode should be used by the FLC button - either SPD or FLC |
Child Tags
None.
Default Value
<FlightLevelChange type="FLC" />
<Autothrottle>
Defines the autothrottle configuration objects and electricity logic.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
None.
Child Tags
<SpeedProtection>
<Electric>
(optional)- A logic element determining whether the adf is powered. If not provided, the adf is always considered to be powered.
Default Value
<Autothrottle>
<SpeedProtection>False</SpeedProtection>
</Autothrottle>
<SpeedProtection>
Defines whether autothrottle speed protections are available. If set to false, the autopilot will continue to automatically correct overspeeds using pitch axis in MxSPD mode. When autothrottle speed protections are available, there will also be a low speed caution bar displayed on the speed tape.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Autothrottle> | No | Yes | No |
Content
Either true
or false
.
Child Tags
None.
Default Value
None.
<Annunciations>
Defines CAS alerts.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
None.
Child Tags
Default Value
<Annunciations></Annunciations>
<Annunciation>
Defines a single CAS alert.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Annunciations> | No | No | Yes |
Attributes
None.
Child Tags
Default Value
None.
<Type>
(<Annunciation>
)
Defines the priority level used to activate a CAS alert.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Annunciation> | No | Yes | No |
Attributes
None.
Content
'Warning', 'Caution', or 'Advisory'.
<Text>
(<Annunciation>
)
Defines the message text of a CAS alert.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Annunciation> | No | Yes | No |
Attributes
None.
Content
String.
<Condition>
(<Annunciation>
)
Defines logic that determines when a CAS alert is activated.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Annunciation> | No | No | No |
Attributes
Name | Value | Optional (Default) | Description |
---|---|---|---|
suffix | String | Yes ([See Description]) | The suffix to activate when the condition evaluates to true. If not defined, then the alert is assumed to have no suffixes. |
Content
Logic that evaluates to a boolean (0/1) value.
<Checklist>
Defines options for the electronic checklists feature.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
Global | No | Yes | Yes |
Attributes
None.
Child Tags
Default Value
None.
<File>
(<Checklist>
)
Defines the URL path to the XML file that configures the electronic checklists feature. If this tag is not present, then the feature will be disabled and a Checklist Unavailable error will be displayed on the lower MFD.
Properties
Scope | Inherits | Singleton | Optional |
---|---|---|---|
<Checklist> | No | Yes | Yes |
Attributes
None.
Content
An absolute URL path.
Default Value
None.