B119500 - B119500 Left Rear Turn Signal Lamp Fault (High Configuration)

Fault code information

Fault Depth Definition

In high-specification (high-end) versions of vehicle electrical architecture, fault code B119500 is defined as "Left Rear Turn Signal Light Fault", a code specifically pointing to a sub-module of the external lighting system managed by the Left Domain Controller. As a key node in the body control network, the Left Domain Controller is responsible for logical operations and status monitoring of external lamps. The generation of this fault code indicates that the controller cannot obtain the correct working status signal of the left rear position turn signal within the expected communication cycle or electrical load feedback loop. At the system level, this diagnostic code reflects topological connection anomalies, functional failures, or logical interchanges between the physical lighting actuator (bulb/module) and the higher-level control unit, belonging to a critical fault level in the body comfort and safety warning system.

Common Fault Symptoms

When vehicle operating status satisfies specific conditions for the above fault determination, drivers and passengers can observe the following specific driving experience and instrument feedback characteristics:

  • Left Rear Turn Signal Light Not Lit: When turn signals or hazard flasher lamps are activated during normal driving, there is no visual output from the left-rear position signal lamp.
  • Indicator Abnormal Flashing: The steering wheel warning light on the dashboard may display a left turn failure icon, and the vehicle network status indicator light accompanying this fault code may illuminate.
  • External Signal Missing: Pedestrians and vehicles behind cannot obtain visual warnings of lane changes or turns via the left rear turn signal, posing potential safety risks.

Core Fault Cause Analysis

According to diagnostic data logic, the root causes leading to the generation of B119500 fault can be summarized as hardware and connection failures in the following three dimensions:

  • Hardware Component Failure: The light-emitting unit inside the left rear lamp assembly (e.g., LED module or bulb) is physically damaged, or there are irreversible faults such as unstable power supply or open circuit in the control circuit board inside the lamp.
  • Wiring and Connector Abnormality: The wiring harness connecting the Left Domain Controller and the Left Rear Lamp Assembly is physically damaged (e.g., wear or breakage), or relevant aircraft connectors, power interfaces exist pin oxidation, looseness, or pin backing out, causing interruption of electrical path or signal transmission impedance abnormal.
  • Controller Logic Failure: The internal processing unit (e.g., microprocessor) inside the Left Domain Controller itself occurs software deadlock or hardware damage, preventing it from correctly executing control instructions for the left rear turn signal or erroneously recording fault status.

Technical Monitoring and Trigger Logic

The generation of this fault code is based on input/output monitoring strategies within the Left Domain Controller, following which system adheres to the following technical standards for determination:

  • Monitoring Target: The system focuses on monitoring the output load status and loop feedback signal of the left rear turn signal light. After sending an illumination instruction, the control unit calculates the actual circuit current response or voltage status in real-time.
  • Numerical Range and Threshold: Under specific operating conditions for driving motor or light control, the controller compares command output with actual returned electrical status (e.g., within $9V$~$16V$ working voltage range, monitoring if it is in an effective conduction load state). If feedback signal is missing or is outside open circuit threshold, it is considered abnormal.
  • Fault Judgment Logic: After vehicle startup and satisfying diagnostic conditions, the system enters dynamic monitoring mode. If the actual light status does not match control instructions within multiple continuous monitoring cycles, and instantaneous factors like communication interference are excluded, the system will lock the fault code B119500 within a preset time window and store it in the fault memory, at which point the fault is triggered and recorded.
Meaning: -
Common causes:

Cause Analysis According to diagnostic data logic, the root causes leading to the generation of B119500 fault can be summarized as hardware and connection failures in the following three dimensions:

  • Hardware Component Failure: The light-emitting unit inside the left rear lamp assembly (e.g., LED module or bulb) is physically damaged, or there are irreversible faults such as unstable power supply or open circuit in the control circuit board inside the lamp.
  • Wiring and Connector Abnormality: The wiring harness connecting the Left Domain Controller and the Left Rear Lamp Assembly is physically damaged (e.g., wear or breakage), or relevant aircraft connectors, power interfaces exist pin oxidation, looseness, or pin backing out, causing interruption of electrical path or signal transmission impedance abnormal.
  • Controller Logic Failure: The internal processing unit (e.g., microprocessor) inside the Left Domain Controller itself occurs software deadlock or hardware damage, preventing it from correctly executing control instructions for the left rear turn signal or erroneously recording fault status.

Technical Monitoring and Trigger Logic

The generation of this fault code is based on input/output monitoring strategies within the Left Domain Controller, following which system adheres to the following technical standards for determination:

  • Monitoring Target: The system focuses on monitoring the output load status and loop feedback signal of the left rear turn signal light. After sending an illumination instruction, the control unit calculates the actual circuit current response or voltage status in real-time.
  • Numerical Range and Threshold: Under specific operating conditions for driving motor or light control, the controller compares command output with actual returned electrical status (e.g., within $9V$~$16V$ working voltage range, monitoring if it is in an effective conduction load state). If feedback signal is missing or is outside open circuit threshold, it is considered abnormal.
  • Fault Judgment Logic: After vehicle startup and satisfying diagnostic conditions, the system enters dynamic monitoring mode. If the actual light status does not match control instructions within multiple continuous monitoring cycles, and instantaneous factors like communication interference are excluded, the system will lock the fault code B119500 within a preset time window and store it in the fault memory, at which point the fault is triggered and recorded.
Basic diagnosis:

diagnostic code reflects topological connection anomalies, functional failures, or logical interchanges between the physical lighting actuator (bulb/module) and the higher-level control unit, belonging to a critical fault level in the body comfort and safety warning system.

Common Fault Symptoms

When vehicle operating status satisfies specific conditions for the above fault determination, drivers and passengers can observe the following specific driving experience and instrument feedback characteristics:

  • Left Rear Turn Signal Light Not Lit: When turn signals or hazard flasher lamps are activated during normal driving, there is no visual output from the left-rear position signal lamp.
  • Indicator Abnormal Flashing: The steering wheel warning light on the dashboard may display a left turn failure icon, and the vehicle network status indicator light accompanying this fault code may illuminate.
  • External Signal Missing: Pedestrians and vehicles behind cannot obtain visual warnings of lane changes or turns via the left rear turn signal, posing potential safety risks.

Core Fault Cause Analysis

According to diagnostic data logic, the root causes leading to the generation of B119500 fault can be summarized as hardware and connection failures in the following three dimensions:

  • Hardware Component Failure: The light-emitting unit inside the left rear lamp assembly (e.g., LED module or bulb) is physically damaged, or there are irreversible faults such as unstable power supply or open circuit in the control circuit board inside the lamp.
  • Wiring and Connector Abnormality: The wiring harness connecting the Left Domain Controller and the Left Rear Lamp Assembly is physically damaged (e.g., wear or breakage), or relevant aircraft connectors, power interfaces exist pin oxidation, looseness, or pin backing out, causing interruption of electrical path or signal transmission impedance abnormal.
  • Controller Logic Failure: The internal processing unit (e.g., microprocessor) inside the Left Domain Controller itself occurs software deadlock or hardware damage, preventing it from correctly executing control instructions for the left rear turn signal or erroneously recording fault status.

Technical Monitoring and Trigger Logic

The generation of this fault code is based on input/output monitoring strategies within the Left Domain Controller, following which system adheres to the following technical standards for determination:

  • Monitoring Target: The system focuses on monitoring the output load status and loop feedback signal of the left rear turn signal light. After sending an illumination instruction, the control unit calculates the actual circuit current response or voltage status in real-time.
  • Numerical Range and Threshold: Under specific operating conditions for driving motor or light control, the controller compares command output with actual returned electrical status (e.g., within $9V$~$16V$ working voltage range, monitoring if it is in an effective conduction load state). If feedback signal is missing or is outside open circuit threshold, it is considered abnormal.
  • Fault Judgment Logic: After vehicle startup and satisfying diagnostic conditions, the system enters dynamic monitoring mode. If the actual light status does not match control instructions within multiple continuous monitoring cycles, and instantaneous factors like communication interference are excluded, the system will lock the fault code B119500 within a preset time window and store it in the fault memory, at which point the fault is triggered and recorded.
Repair cases
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