DESCRIPTION
Refer to DTC P2120.
Refer to DESCRIPTION
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P2121 | Throttle / Pedal Position Sensor / Switch "D" Circuit Range / Performance | Either of the following conditions is met for 0.5 seconds (1 trip detection logic): Difference between VPA and VPA2 is less than 0.4 V, or higher than 1.2 V. (learned value of accelerator off position) Difference between VPA and VPA2 is greater than or equal to the specified value. | Accelerator pedal sensor assembly ECM | Comes on | DTC stored |
MONITOR DESCRIPTION
The accelerator pedal position sensor is mounted on the accelerator pedal bracket. The accelerator pedal position sensor has 2 sensor elements and 2 signal outputs: VPA and VPA2. VPA is used to detect the actual accelerator pedal angle (used for engine control) and VPA2 is used to detect malfunctions in VPA. When the difference between the output voltages of VPA and VPA2 deviates from the standard, the ECM determines that the accelerator pedal position sensor is malfunctioning. The ECM illuminates the MIL and stores this DTC.
HINT
Although the DTC titles say oxygen sensor, these DTCs relate to the air fuel ratio sensor.
The air fuel ratio sensor generates a voltage* that corresponds to the actual air fuel ratio. This sensor voltage is used to provide the ECM with feedback so that it can control the air fuel ratio. The ECM determines the deviation from the stoichiometric air fuel ratio level, and regulates the fuel injection time. If the air fuel ratio sensor malfunctions, the ECM is unable to control the air fuel ratio accurately.
The air fuel ratio sensor is a planar type and is integrated with a heater, which heats the solid electrolyte (zirconia element). This heater is controlled by the ECM. When the intake air volume is low (the exhaust gas temperature is low), current flows to the heater to heat the sensor, in order to facilitate accurate oxygen concentration detection. In addition, the sensor and heater portions are a narrow type. The heat generated by the heater is conducted to the solid electrolyte through alumina, and therefore the sensor activation is accelerated.
In order to obtain a high purification rate of the carbon monoxide (CO), hydrocarbon (HC) and nitrogen oxide (NOx) components in the exhaust gas, a three-way catalytic converter is used. For the most efficient use of the three-way catalytic converter, the air fuel ratio must be precisely controlled so that it is always close to the stoichiometric level.
*: Value changes inside the ECM. Since the air fuel ratio sensor is a current output element, the current is converted into a voltage inside the ECM. Any measurements taken at the air fuel ratio sensor or ECM connectors will show a constant voltage.
Scheme 88
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P2195 | Oxygen (A/F) Sensor Signal Stuck Lean (Bank 1 Sensor 1) | Either of following conditions 1 or 2 met: Conditions (a) and (b) continue for 5 seconds or more (2 trip detection logic): (a) Air fuel ratio sensor voltage is higher than 3.8 V. (b) Heated oxygen sensor voltage is 0.21 V or higher. While the fuel-cut operation is performed (during vehicle deceleration), the air fuel ratio sensor current is 2.2 mA or higher for 3 seconds (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) Exhaust gas leak Intake system Fuel pressure Fuel injector assembly ECM | Comes on | DTC stored |
| P2196 | Oxygen (A/F) Sensor Signal Stuck Rich (Bank 1 Sensor 1) | Either of following conditions 1 or 2 met: Conditions (a) and (b) continue for 5 seconds or more (2 trip detection logic): (a) Air fuel ratio sensor voltage is less than 2.8 V. (b) Heated oxygen sensor voltage is less than 0.66 V. While the fuel-cut operation is performed (during vehicle deceleration), the air fuel ratio sensor current is less than 0.7 mA for 3 seconds (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) Exhaust gas leak Intake system Fuel pressure Fuel injector assembly ECM | Comes on | DTC stored |
HINT
- When any of these DTCs is stored, check the air fuel ratio sensor voltage output by entering the following menus on the Techstream: Powertrain / Engine and ECT / Data List / Gas AF Control / AFS Voltage B1S1.
- Short-term fuel trim values can also be read using the Techstream.
- The ECM regulates the voltages at the A1A+ and A1A- terminals of the ECM to a constant level. Therefore, the air fuel ratio sensor output voltage cannot be confirmed without using the Techstream.
- If an air fuel ratio sensor malfunction is detected, the ECM will store a DTC.
Sensor Voltage Detection Monitor
Under air fuel ratio feedback control, If the air fuel ratio sensor output voltage is less than 2.8 V (very rich condition) for 5 seconds despite the heated oxygen sensor output voltage being less than 0.66 V, the ECM stores DTC P2196. Alternatively, if the air fuel ratio sensor output voltage is higher than 3.8 V (very lean condition) for 5 seconds despite the heated oxygen sensor output voltage being 0.21 V or higher, DTC P2195 is stored.
Sensor Current Detection Monitor
A rich air fuel mixture causes a low air fuel ratio sensor current, and a lean air fuel mixture causes a high air fuel ratio sensor current. Therefore, the sensor output becomes low during acceleration, and it becomes high during deceleration with the throttle valve fully closed. The ECM monitors the air fuel ratio sensor current during fuel-cut and detects any abnormal current values.
If the air fuel ratio sensor output is 2.2 mA or higher for more than 3 seconds of cumulative time, the ECM interprets this as a malfunction in the air fuel ratio sensor and stores DTC P2195 (stuck on high side). If the air fuel ratio sensor output is less than 0.7 mA for more than 3 seconds of cumulative time, the ECM stores DTC P2196 (stuck on low side).
Scheme 89
Refer to DTC P0300.
Refer to DESCRIPTION
Refer to DTC P2195.
Refer to DESCRIPTION
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P219A | Bank 1 Air-Fuel Ratio Imbalance | The difference in air fuel ratios between the cylinders exceeds the threshold (2 trip detection logic). | Fuel injector assembly Intake system Gas leaks from exhaust system Ignition system Compression pressure Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P219C | Cylinder 1 Air-Fuel Ratio Imbalance | The difference in air fuel ratios between the cylinders exceeds the threshold (2 trip detection logic). | Fuel injector assembly Intake system Gas leaks from exhaust system Ignition system Compression pressure Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P219D | Cylinder 2 Air-Fuel Ratio Imbalance | The difference in air fuel ratios between the cylinders exceeds the threshold (2 trip detection logic). | Fuel injector assembly Intake system Gas leaks from exhaust system Ignition system Compression pressure Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P219E | Cylinder 3 Air-Fuel Ratio Imbalance | The difference in air fuel ratios between the cylinders exceeds the threshold (2 trip detection logic). | Fuel injector assembly Intake system Gas leaks from exhaust system Ignition system Compression pressure Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P219F | Cylinder 4 Air-Fuel Ratio Imbalance | The difference in air fuel ratios between the cylinders exceeds the threshold (2 trip detection logic). | Fuel injector assembly Intake system Gas leaks from exhaust system Ignition system Compression pressure Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
Fuel System Air Fuel Ratio Cylinder Imbalance Monitor
The ECM uses the air fuel ratio sensor and crankshaft position sensor to monitor the difference in air fuel ratios between the cylinders caused by differences in injection volumes between the cylinders, leakage in the intake or exhaust system, etc.
When the air fuel ratios of the cylinders are lean or rich with respect to each other, the ECM determines that a problem is present and stores a DTC.
Air Fuel Ratio Sensor Monitoring Method: P219A is stored primarily when a rich side imbalance is detected.
When the system detects a difference in air fuel ratios between the cylinders due to fluctuation in the air fuel ratio sensor output over 1 engine cycle (2 crankshaft revolutions), the system determines that there is a problem.
Crankshaft Position Sensor Monitoring Method: P219C, P219D, P219E, and/or P219F are stored primarily when a lean side imbalance is detected.
The system monitors the engine speed variation and when the variation becomes large, the system determines that there is a difference in air fuel ratios between the cylinders, which it determines to be a problem.
Refer to DTC P2195.
Refer to DESCRIPTION
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P2237 | Oxygen (A/F) Sensor Pumping Current Circuit / Open (for A/F sensor) (Bank 1 Sensor 1) | An open in the circuit between terminals A1A+ and A1A- of the air fuel ratio sensor while the engine is running (2 trip detection logic). | Open in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P2238 | Oxygen Sensor Pumping Current Circuit Low (for A/F sensor) (Bank 1 Sensor 1) | Case 1: Condition (a) or (b) continues for 5.0 seconds or more (2 trip detection logic):(a) Voltage at terminal A1A+ is 0.5 V or less(b) Voltage difference between terminals A1A+ and A1A- is 0.1 V or less Case 2: Air fuel ratio sensor admittance is less than 0.0054 1/ohms (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P2239 | Oxygen Sensor Pumping Current Circuit High (for A/F sensor) (Bank 1 Sensor 1) | The A1A+ voltage is higher than 4.5 V (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P2252 | Oxygen Sensor Reference Ground Circuit Low (for A/F sensor) (Bank 1 Sensor 1) | The A1A- voltage is 0.5 V or less (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
| P2253 | Oxygen Sensor Reference Ground Circuit High (for A/F sensor) (Bank 1 Sensor 1) | The A1A- voltage is higher than 4.5 V (2 trip detection logic). | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM | Comes on | DTC stored |
These DTCs are output when there is an open or short in the air fuel ratio sensor circuit, or if the air fuel ratio sensor output drops. To detect these problems, the voltage of the air fuel ratio sensor is monitored when turning the ignition switch to ON, and the admittance (admittance is an electrical term that indicates the ease of flow of current) is checked while driving. If the voltage of the air fuel ratio sensor is between 0.5 V and 4.5 V, it is considered normal. If the voltage is out of the specified range, or the admittance is less than the standard value, the ECM determines that there is a malfunction in the air fuel ratio sensor. If the same malfunction is detected in the next driving cycle, the ECM will illuminate the MIL and store a DTC.
The description can be found in EVAP (Evaporative Emission) System.
Refer to DESCRIPTION
5 hours* after the ignition switch is turned off, the leak detection pump creates negative pressure (vacuum) in the EVAP (Evaporative Emission) system. The ECM monitors for leaks and actuator malfunctions based on the EVAP pressure.
HINT
*: If the engine coolant temperature is not less than 35°C (95°F) 5 hours after the ignition switch is turned off, the monitor check starts 2 hours later. If it is still not less than 35°C (95°F) 7 hours after the ignition switch is turned off, the monitor check starts 2.5 hours later.
| Sequence | Operation | Description | Duration |
|---|---|---|---|
| ECM activation | Activated by soak timer, 5 hours (7 or 9.5 hours) after ignition switch is turned off. | ||
| A | Atmospheric pressure measurement | Vent valve is turned off (vent) and EVAP system pressure is measured by ECM in order to register atmospheric pressure. If pressure in EVAP system is not between 70 kPa(abs) and 110 kPa(abs) [525 mmHg(abs) and 825 mmHg(abs)], ECM cancels EVAP system monitor. | 60 seconds |
| B | First reference pressure measurement | In order to determine reference pressure, leak detection pump creates negative pressure (vacuum) through reference orifice and then ECM checks if leak detection pump and vent valve operate normally. | 360 seconds |
| C | EVAP system pressure measurement | Vent valve is turned on (closed) to shut EVAP system. Negative pressure (vacuum) is created in EVAP system, and then EVAP system pressure is measured. Write down measured value as they will be used in leak check. If EVAP pressure does not stabilize within 15 minutes, ECM cancels EVAP system monitor. | 15 minutes* |
| D | Purge VSV monitor | Purge VSV is opened and then EVAP system pressure is measured by ECM. Large increase indicates normal. | 10 seconds |
| E | Second reference pressure measurement | After second reference pressure measurement, leak check is performed by comparing first and second reference pressure measurements. If stabilized system pressure is higher than second reference pressure, ECM determines that there is a leak in EVAP system. | 60 seconds |
| Final check | Atmospheric pressure is measured and then monitoring result is recorded by ECM. |
*: If only a small amount of fuel is in the fuel tank, it takes longer for the EVAP pressure to stabilize.
Scheme 90
| *1 | Purge VSV: Off (Closed) | *2 | Purge VSV: On (Open) |
|---|---|---|---|
| *3 | Vent Valve: Off (Vent) | *4 | Vent Valve: On (Closed) |
| *5 | Leak Detection Pump: Off | *6 | Leak Detection Pump: On |
| *7 | Reference Orifice (0.02 inch) | *8 | Canister Pressure Sensor |
| *9 | Canister | *10 | Fuel Tank |
| *11 | Canister Pump Module | *12 | Canister Filter |
| *a | Operation A: Atmospheric Pressure Measurement | *b | Operation B, E: Reference Pressure Measurement |
| *c | Operation C: EVAP System Pressure Measurement | *d | Operation D: Purge VSV Monitor |
| *e | Atmospheric Pressure | *f | Negative Pressure |
P2420: Vent valve stuck open (vent)
In operation C, the vent valve turns on (closed) and the EVAP system pressure is then measured by the ECM using the canister pressure sensor to conduct an EVAP leak check. If the pressure does not increase when the vent valve is open, the ECM interprets this as the vent valve being stuck open. In this case the ECM will illuminate the MIL and store this DTC.
Scheme 91
The soak timer operates after the ignition switch is turned off. When a certain amount of time has elapsed after turning the ignition switch off, the soak timer activates the ECM to perform malfunction checks which can only be performed after the engine is stopped. The soak timer is built into the ECM.
Scheme 92
If the soak timer activates the ECM even though only a short amount of time has elapsed since the ignition switch was turned off, or if the soak timer does not activate the ECM even though a considerable amount of time has elapsed since the ignition switch was turned off, the ECM determines that the soak timer is malfunctioning, illuminates the MIL and stores this DTC the next time the ignition switch is turned to ON.
The EDU in the continuously variable valve lift controller assembly sends a motor drive request and supplies current to the motor.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P2646 | "A" Rocker Arm Actuator System Performance or Stuck Off Bank 1 ENG | When all of the following conditions are met (1 trip detection logic): The actuator duty cycle is 80% or higher The actuator current is 5 A or higher The stroke variation is 0.0117 mm (0.0006693 in.) or less every 0.016 seconds | Continuously variable valve lift controller assembly Camshaft housing sub-assembly | Comes on | DTC stored |
| P2647 | "A" Rocker Arm Actuator System Stuck On Bank 1 ENG | When all of the following conditions are met (1 trip detection logic): The actuator duty cycle is 80% or less The actuator current is 5 A or higher The stroke variation is 0.0117 mm (0.0006693 in.) or less every 0.016 seconds | Continuously variable valve lift controller assembly Camshaft housing sub-assembly | Comes on | DTC stored |
Perform the following procedure to confirm that the VALVEMATIC system is operating normally.
- Connect the Techstream to the DLC3.
- Start the engine.
- Turn the Techstream on.
- Enter the following menus: Powertrain / Engine and ECT / Active Test / Activate the VALVEMATIC(ENG ON) / Gas Valve Control / VALVEMATIC Current Angle and VALVEMATIC Target Angle. NOTE: Make sure the following conditions are met when performing the Active Test. The engine is running. The engine coolant temperature is 40°C (104°F) or higher. The vehicle is stationary. The shift lever is in P or N. Result The "VALVEMATIC Current Angle" follows the "VALVEMATIC Target Angle".
HINT
If the malfunction does not recur, refer to the engine coolant temperature and intake air temperature recorded in the freeze frame data and perform a simulation test.
When the Active Test results are abnormal, remove the continuously variable valve lift controller assembly from the camshaft housing sub-assembly and perform the "Activate the VALVEMATIC(ENG OFF)" Active Test with the removed continuously variable valve lift controller assembly to determine whether the problem is with the continuously variable valve lift controller assembly or camshaft housing sub-assembly.
When the EDU in the continuously variable valve lift controller assembly detects that the actuator does not operate even though the EDU commands the actuator to operate and power is supplied to the actuator, a DTC is stored and the MIL is illuminated.
The current flowing to the actuator in the continuously variable valve lift controller assembly is monitored by the current sensor in the continuously variable valve lift controller assembly.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P2648 | A Rocker Arm Actuator Control Circuit Low B1 | Current does not flow to the actuator while the actuator is commanded to operate (1 trip detection logic). | Continuously variable valve lift controller assembly | Comes on | DTC stored |
| P2649 | "A" Rocker Arm Actuator Control Circuit High Bank 1 | Actuator overcurrent (1 trip detection logic). | Continuously variable valve lift controller assembly | Comes on | DTC stored |
When the continuously variable valve lift controller assembly detects that no current is flowing to the actuator even though the actuator is commanded to operate or the current flowing to the actuator is more than the amount requested, a DTC is stored and the MIL is illuminated.
There are position sensor and angle sensor in the continuously variable valve lift controller assembly. They detect the actuator position and rotation direction.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P264A | A Rocker Arm Actuator Position Sensor Circuit B1 | When either of the following conditions is met (1 trip detection logic): Position sensor output error Angle sensor output error | Continuously variable valve lift controller assembly | Comes on | DTC stored |
There are position sensor and angle sensor in the continuously variable valve lift controller assembly. When there is a malfunction in any of the sensors, this DTC is stored and the MIL is illuminated.
The VALVEMATIC shaft sensor (No. 1 crank position sensor) detects the position of the shaft monitor target mounted on the VALVEMATIC control shaft and the ECM detects the operation of the VALVEMATIC control shaft.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| P265B | B Rocker Arm Actuator Position Sensor Circuit Range Performance Bank 1 | Either of the following conditions is met: (a) The VALVEMATIC shaft sensor (No. 1 crank position sensor) voltage is 1.41 V or higher (VALVEMAIC Current Angle is less than 145°CA). (b) The VALVEMATIC shaft sensor (No. 1 crank position sensor) voltage is less than 3.42 V (VALVEMATIC Current Angle is higher than 223°CA) | Open or short in VALVEMATIC shaft sensor (No. 1 crank position sensor) circuit VALVEMATIC shaft sensor (No. 1 crank position sensor) Camshaft housing sub-assembly ECM | Comes on | DTC stored |
| P265C | B Rocker Arm Actuator Position Sensor Circuit Low Bank 1 | The output voltage of the VALVEMATIC shaft sensor (No. 1 crank position sensor) is less than 0.38 V for 5 seconds (1 trip detection logic). | Open or short in VALVEMATIC shaft sensor (No. 1 crank position sensor) circuit VALVEMATIC shaft sensor (No. 1 crank position sensor) ECM | Comes on | DTC stored |
| P265D | B Rocker Arm Actuator Position Sensor Circuit High Bank 1 | The output voltage of the VALVEMATIC shaft sensor (No. 1 crank position sensor) is higher than 4.68 V for 5 seconds (1 trip detection logic). | Open or short in VALVEMATIC shaft sensor (No. 1 crank position sensor) circuit VALVEMATIC shaft sensor (No. 1 crank position sensor) ECM | Comes on | DTC stored |
If the duration monitored by the continuously variable valve lift controller assembly differs from the VALVEMATIC shaft sensor (No. 1 crank position sensor) output, or the VALVEMATIC shaft sensor (No. 1 crank position sensor) voltage is less than 0.38 V or higher than 4.68 V for 5 seconds or more, the ECM illumiates the MIL and stores a DTC.
The ECM and continuously variable valve lift controller assembly communicate via the CAN communication system.
| DTC No. | Detection Item | DTC Detection Condition | Trouble Area | MIL | Memory |
|---|---|---|---|---|---|
| U011B | Lost Communication with Rocker Arm Control Module "A" | CAN communication stops (1 trip detection logic). | CAN communication circuit Continuously variable valve lift controller assembly ECM | Comes on | DTC stored |
When between the ECM and the continuously variable valve lift controller assembly is a malfunction in the CAN communication, this DTC is stored and the MIL is illuminated.
The VALVEMATIC system is able to continuously change the valve lift amount and valve timing. For engines equipped with a VALVEMATIC system, when a part such as a rocker arm in the camshaft housing has mechanical problems, the valve lift amount does not change and problems occur, such as a lack of engine power or rough idling.
When the ignition switch is turned to ON, the battery voltage is applied to IGSW of the ECM. The output signal from the MREL terminal of the ECM causes a current to flow to the coil, closing the contacts of the EFI-MAIN relay and supplying power to terminal is +B and +B2 of the ECM.
Scheme 93
The ECM constantly generates a 5 V power source voltage from the battery voltage supplied to the +B (BATT) terminal to operate the microprocessor. The ECM also provides this power source voltage to the sensors through the VC output circuit.
Scheme 94
When the VC circuit is short-circuited, the microprocessor in the ECM and the sensors that are supplied with power through the VC circuit are inactivated because power is not supplied from the VC circuit. Under this condition, the system does not start up and the MIL does not illuminate even if the system malfunctions.
HINT
Under normal conditions, the MIL is illuminated when the ignition switch is turned to ON. The MIL goes off when the engine is started.
Scheme 95
Scheme 96
The fuel pump circuit consists of the ECM, fuel pump and fuel pump control ECU assembly (which operates the fuel pump). Based on the engine output, the ECM determines the fuel pump speed. The speed is then converted to a duty signal and sent to the fuel pump control ECU assembly. Based on the signal sent from the ECM, the fuel pump ECU adjusts the fuel pump operation speed.
Scheme 97
The fuel injectors are located on the intake manifold. They inject fuel into the cylinders based on the signals from the ECM.
Scheme 98
While the engine is being cranked, current flows from terminal ST2 of the ignition switch assembly*1 or terminal STAR of the certification ECU (smart key ECU assembly)*2 to the park/neutral position switch assembly and to terminal STA of the ECM (STA signal).
*1: w/o smart key system
*2: w/ smart key system
When the vehicle is being driven, depressing the accelerator pedal sensor assembly and brake pedal will activate the brake override system to restrict driving torque. The conditions for activating the brake override system as well as the items that are controlled are explained below.
Scheme 99
Activation Conditions
- Vehicle is running at or above the specified speed.
- When the accelerator pedal and brake pedal are depressed.
Note. The vehicle may not enter the brake override system control due to the relation of the accelerator pedal angle and the vehicle's speed.
Items Controlled
- Driving torque is restricted.
HINT
When this control is activated, the accelerator opening value is forcibly reduced to a fixed value. Therefore, the Accelerator Position value in the Data List is fixed regardless of the actual accelerator opening value (Accel Sens. No. 1 Volt %).
Deactivation Conditions
- When the brake pedal or the accelerator pedal returns to some degree.
The MIL (Malfunction Indicator Lamp) is used to indicate vehicle malfunctions detected by the ECM. When the ignition switch is turned to ON, power is supplied to the MIL circuit, and the ECM provides the circuit ground which illuminates the MIL.
The MIL operation can be checked visually: When the ignition switch is turned to ON, the MIL should be illuminated and should turn off after engine is started. If the MIL remains illuminated or is not illuminated, conduct the following troubleshooting procedure using the Techstream.