Alerts
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| Signal Name | Description | Condition | Impact |
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Air compressor driver circuitry indicates a faulted condition.
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Air compressor driver reported a fault for an extended period.
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Air suspension compressor disabled.
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Indicates there was an active connection to the universal measurement and calibration protocol state machine
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The XCP state machine has a connection.
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XCP was active.
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Frunk overcurrent condition has been encountered.
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Condenser Fan Self Test Failed due to a fault condition.
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Condenser Fan feed may go unpowered.
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IBooster Self Test Failed due to a fault condition.
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IBooster feed may go unpowered.
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HCU ESP ABS Self Test Failed due to a fault condition.
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HCU ESP ABS feed may go unpowered.
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Cabin BEC Self Test Failed due to a fault condition.
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Cabin BEC feed may go unpowered.
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EPAS Secondary Self Test Failed due to a fault condition.
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EPAS Secondary feed may go unpowered.
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EPAS Primary Self Test Failed due to a fault condition.
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EPAS Primary feed may go unpowered.
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Frunk BEC Self Test Failed due to a fault condition.
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Frunk BEC feed may go unpowered.
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DCDC Self Test Failed due to a fault condition.
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DCDC feed may go unpowered.
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VBat Fused Self Test Failed due to a fault condition.
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VBat Fused feed may go unpowered.
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Load shed event encountered due to an over temperature or over current condition.
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Loss of power to and from DCDC, Cabin, or Frunk power feeds.
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Condenser Fan power feed has been tripped due to an encountered fault condition.
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Loss of power to thermal system.
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IBooster power feed has been tripped due to an encountered fault.
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Loss of braking system.
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Hydraulic Control Unit Electronic Stability Program Anti-lock Braking System power feed has been tripped due to an encountered fault condition.
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Loss of Anti-lock Braking System.
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Cabin BEC EFuse has been tripped due to an encountered fault condition.
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Power will not be provided to the ecus fed by the efuse module, through the cabin feed, major result is loss of drive.
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EPAS Secondary has been tripped due to an encountered fault condition.
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EPAS Secondary feed will not be powered, and components connected auxillary power will no longer be powered.
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EPAS Primary EFuse has been tripped due to an encountered fault condition.
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Loss of power to primary feed for Electronic Power Assisted Steering System.
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Frunk BEC EFuse has been tripped due to an encountered fault condition.
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Power will not be provided to the ecus fed by the efuse module, through the frunk feed, major result is loss of drive.
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