DESCRIPTION
The throttle actuator is operated by the ECM and opens and closes the throttle valve using gears.
The opening angle of the throttle valve is detected by the throttle position sensor, which is mounted on the throttle body assembly. The throttle position sensor provides feedback to the ECM. This feedback allows the ECM to appropriately control the throttle actuator and monitor the throttle opening angle as the ECM responds to driver inputs.
HINT
This electronic throttle control system does not use a throttle cable.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2102 | Both of the following conditions continue for 2 seconds (1 trip detection logic): (a) Throttle actuator duty ratio is 80% or more (b) Throttle actuator current is below 0.5 A | Open in throttle actuator circuit Throttle actuator ECM |
| P2103 | Either condition is met (1 trip detection logic): Hybrid IC diagnosis signal fails Hybrid IC current limiter port fails | Short in throttle actuator circuit Throttle actuator Throttle valve Throttle body assembly ECM |
MONITOR DESCRIPTION
The ECM monitors the electrical current through the electronic actuator, and detects malfunctions and open circuits in the throttle actuator based on this value. If the current is outside the standard range, the ECM determines that there is a malfunction in the throttle actuator. In addition, if the throttle valve does not function properly (for example, stuck on), the ECM determines that there is a malfunction. The ECM then illuminates the MIL and stores a DTC.
Example
- When the electrical current is below 0.5 A and the throttle actuator duty ratio exceeds 80%, the ECM interprets this as the current being outside the standard range, illuminates the MIL and stores a DTC.
- If the malfunction is not repaired successfully, a DTC is stored when the engine is quickly revved to a high engine speed several times after the engine has idled for 5 seconds after engine start.
The throttle actuator is operated by the ECM, and opens and closes the throttle valve using gears. The opening angle of the throttle valve is detected by the throttle position sensor, which is mounted on the throttle body assembly. The throttle position sensor provides feedback to the ECM. This feedback allows the ECM to appropriately control the throttle actuator and monitor the throttle opening angle as the ECM responds to driver inputs.
HINT
This electronic throttle control system does not use a throttle cable.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2111 | The ECM signals the throttle actuator to close, but the actuator is stuck (1 trip detection logic) | Throttle actuator Throttle body assembly Throttle valve ECM |
| P2112 | The ECM signals the throttle actuator to open, but the actuator is stuck (1 trip detection logic) | Throttle actuator Throttle body assembly Throttle valve ECM |
The ECM determines that there is a malfunction in the electronic throttle control system when the throttle valve remains at the fixed angle despite a high drive current from the ECM. The ECM illuminates the MIL and stores a DTC.
If the malfunction is not repaired successfully, a DTC is stored when the accelerator pedal is fully depressed and released quickly (to fully open and close the throttle valve) after the engine is next started.
The electronic throttle control system has a dedicated power supply circuit. The voltage (+BM) is monitored and when it is low (below 4 V), the ECM determines that there is a malfunction in the electronic throttle control system and cuts off the current to the throttle actuator.
When the voltage becomes unstable, the electronic throttle control system itself becomes unstable. For this reason, when the voltage is low, the current to the throttle actuator is cut. If repairs are made and the system returns to normal, turn the power switch off. The ECM then allows the current to flow to the throttle actuator so that it can be restarted.
HINT
This electronic throttle control system does not use a throttle cable.
Scheme 442
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2118 | An open in electronic throttle control system power source (+BM) circuit (1 trip detection logic) | Open in electronic throttle control system power source circuit Battery Battery terminals ETCS fuse ECM |
The ECM monitors the battery supply voltage applied to the throttle actuator.
When the power supply voltage (+BM) drops below 4 V for 0.8 seconds or more, the ECM interprets this as an open in the power supply circuit (+BM). The ECM illuminates the MIL and stores the DTC.
If the malfunction is not repaired successfully, the DTC is stored 5 seconds after the engine is next started.
The electronic throttle control system is composed of the throttle actuator, throttle position sensor, accelerator pedal position sensor, and ECM. The ECM operates the throttle actuator to regulate the throttle valve in response to driver inputs. The throttle position sensor detects the opening angle of the throttle valve, and provides the ECM with feedback so that the throttle valve can be appropriately controlled by the ECM.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2119 | Throttle valve opening angle continues to vary greatly from the target opening angle (1 trip detection logic) | Electronic throttle control system ECM |
The ECM determines the actual opening angle of the throttle valve from the throttle position sensor signal. The actual opening angle is compared to the target opening angle commanded by the ECM. If the difference between these 2 values is outside the standard range, the ECM interprets this as a malfunction in the electronic throttle control system. The ECM then illuminates the MIL and stores the DTC.
If the malfunction is not repaired successfully, the DTC is stored when the accelerator pedal is quickly released (to close the throttle valve) after the engine speed reaches 5000 rpm by depressing the accelerator pedal (fully open the throttle valve).
HINT
- Although the DTC titles say oxygen sensor, these DTCs relate to the air fuel ratio sensor.
- Sensor 1 refers to the sensor mounted in front of the three-way catalytic converter and located near the engine assembly.
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 the planar type and is integrated with the 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), a current flows into the heater to heat the sensor, in order to facilitate accurate oxygen concentration detection. In addition, the sensor and heater portions are the narrow type. The heat generated by the heater is conducted to the solid electrolyte through the alumina, therefore the sensor activation is accelerated.
In order to obtain a high purification rate of the carbon monoxide (CO), hydrocarbons (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 443
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2195 | Conditions (a) and (b) continue for 5 seconds or more (2 trip detection logic) (a) Air fuel ratio sensor voltage more than 3.8 V (b) Heated oxygen sensor voltage is 0.21 V or more | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) Air fuel ratio sensor (sensor 1) heater Air fuel ratio sensor heater circuit Intake system Fuel pressure Fuel injector assembly EGR valve assembly ECM |
| While fuel-cut operation performed (during vehicle deceleration), air fuel ratio sensor current is 3.6 mA or more for 3 seconds (2 trip detection logic) | Air fuel ratio sensor (sensor 1) EGR valve assembly ECM | |
| P2196 | Conditions (a) and (b) continue for 5 seconds or more (2 trip detection logic) (a) Air fuel ratio sensor voltage less than 2.8 V (b) Heated oxygen sensor voltage is below 0.59 V | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) Air fuel ratio sensor (sensor 1) heater Air fuel ratio sensor heater circuit Intake system Fuel pressure Fuel injector assembly EGR valve assembly ECM |
| While fuel-cut operation performed (during vehicle deceleration), air fuel ratio sensor current is less than 1.0 mA for 3 seconds (2 trip detection logic) | Air fuel ratio sensor (sensor 1) EGR valve assembly ECM |
HINT
- When any of these DTCs are set, check the air fuel ratio sensor voltage output by entering the following menus on the Techstream: Powertrain / Engine and ECT / Data List / All Data / 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 voltage output cannot be confirmed without using the Techstream.
- If an air fuel ratio sensor malfunction is detected, the ECM sets a DTC.
Sensor Voltage Detection Monitor
Under the air fuel ratio feedback control, if the air fuel ratio sensor voltage output indicates rich or lean for a certain period of time, the ECM determines that there is a malfunction in the air fuel ratio sensor. The ECM illuminates the MIL and stores a DTC.
Example
If the air fuel ratio sensor voltage output is below 2.8 V (very rich condition) and heated oxygen sensor output voltage falls from 0.59 V or more to less than 0.21 V for 5 seconds, the ECM stores DTC P2196. Alternatively, if the air fuel ratio sensor voltage output is higher than 3.8 V (very lean condition) and heated oxygen sensor output voltage rises from less than 0.21 V to 0.59 V or more for 5 seconds, 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 3.6 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 below 1.57 mA for more than 3 seconds of cumulative time, the ECM stores DTC P2196 (stuck on low side).
Scheme 444
HINT
- Although the DTC titles say oxygen sensor, these DTCs relate to the air fuel ratio sensor.
- Sensor 1 refers to the sensor mounted in front of the three-way catalytic converter and located near the engine assembly.
The air fuel ratio sensor, which is located between the exhaust manifold and catalyst, consists of alloyed metal elements and a heater.
Depending on the engine operating conditions, the heater heats the sensor elements to activate them. Battery voltage is applied to the heater and the sensor ground is controlled by the ECM using a duty ratio.
The sensor elements convert the oxygen concentration in the exhaust gas into voltage values to output. Based on the voltage, the ECM determines the air fuel ratio and regulates the fuel injection volume depending on the air fuel ratio and engine operating conditions. The voltage changes between 0.6 V and 4.5 V while the engine is running. If the air fuel ratio is lean, which means the oxygen concentration in the exhaust gas is high, the voltage is high. If the air fuel ratio is rich, which means the oxygen concentration in the exhaust gas is low, the voltage is low.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2237 | Open in the circuit between terminals A1A+ and A1A- of the air fuel ratio sensor while engine is running (2 trip detection logic) | Open in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM |
| P2238 | Any of the following conditions are met (2 trip detection logic) Air fuel ratio sensor output drops while engine is running. Voltage at terminal A1A+ voltage is 0.5 V or less. Voltage difference between terminals A1A+ and A1A- voltage is 0.1 V or less. | Open or short in air fuel ratio sensor (sensor 1) circuit Air fuel ratio sensor (sensor 1) ECM |
| P2239 | A1A+ voltage is more 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 |
| P2252 | 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 |
| P2253 | A1A- voltage is more 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 |
These DTCs are output when there is an open or short in the air fuel ratio sensor circuit, or if air fuel ratio sensor output drops. To detect these problems, the voltage of the air fuel ratio sensor is monitored when turning the power switch on (IG), 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 will determine that there is a malfunction in the air fuel ratio sensor. If the same malfunction is detected in next driving cycle, the MIL will be illuminated and a DTC will be stored.
The circuit description can be found in the EVAP (evaporative emission) System. Refer to DESCRIPTION.
Vent valve stuck open (vent)
In operation C, the vent valve turns on (closes) 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 opened, the ECM interprets this as the vent valve being stuck open. The ECM illuminates the MIL and sets the DTC.
Scheme 445
Scheme 446
The circuit description can be found in the EVAP (evaporative emission) System. Refer to DESCRIPTION.
The soak timer operates after the power switch is turned off. When a certain amount of time has elapsed after turning the power 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 447
If the soak timer activates the ECM even though only a short amount of time has elapsed since the power 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 power switch was turned off, the ECM determines that the soak timer is malfunctioning, illuminates the MIL and stores a DTC the next time the power switch is turned on (IG).
While the engine is running, the ECM monitors the synchronization of the soak timer and the CPU clock. If these two are not synchronized, the ECM interprets this as a malfunction, illuminates the MIL and sets the DTC (2 trip detection logic).
The ECM controls the water pump assembly by calculating the necessary amount of coolant flow based on engine coolant temperature, engine speed and vehicle speed information. The speed of the water pump assembly is controlled steplessly using duty cycle signal sent from the ECM. This optimal control enhances warm-up performance and reduces cooling losses, thus reducing the specific fuel consumption of the engine.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P261B | Water pump speed is less than 900 rpm while the water pump assembly is operating (1 trip detection logic) | Open or short in water pump assembly circuit Water pump assembly ECM |
| P261C | Water pump output voltage is less than specified value while the water pump assembly is operating (1 trip detection logic) | Short in water pump assembly circuit Water pump assembly ECM |
| P261D | Water pump output voltage is higher than specified value while the water pump assembly is operating (1 trip detection logic) | Open in water pump assembly circuit Water pump assembly ECM |
The ECM calculates the speed of the water pump assembly using a duty cycle signal sent from the water pump assembly. When the speed of the water pump assembly becomes less than 900 rpm while it is operating, the ECM detects the malfunction and stores DTC P261B.
The water pump assembly operates steplessly based on a duty cycle signal sent from the ECM. The ECM monitors the current of the water pump assembly. If actual drive duty cycle ratio does not correspond to the target drive duty cycle , the ECM detects the malfunction and stores DTC P261C and P261D.
HINT
- Refer to DTC P2195. Refer to «DESCRIPTION»(ref-393419-S04803004662011040700000).
- Sensor 1 refers to the sensor mounted in front of the three-way catalytic converter and located near the engine assembly.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P2A00 | Calculated value for air fuel ratio sensor response rate deterioration level is less than threshold (2 trip detection logic) | Air fuel ratio sensor Air fuel ratio sensor heater EGR valve assembly ECM |
After the engine is warmed up, the ECM performs air fuel ratio feedback control to maintain the air fuel ratio at the stoichiometric level. In addition, active A/F control is performed for approximately 15 to 20 seconds after preconditions are met in order to measure the air fuel ratio sensor response rate. During active A/F control, the ECM forcibly increases and decreases the injection volume a certain amount, based on the stoichiometric air fuel ratio learned during normal air fuel ratio control, and measures the air fuel ratio sensor response rate. The ECM receives a signal from the air fuel ratio sensor while performing active A/F control and uses it to calculate the air fuel ratio sensor response rate deterioration level.
If the value for air fuel ratio sensor response rate deterioration level is beyond the threshold, the ECM interprets this as a malfunction and sets the DTC.
Scheme 448
From the power management control ECU, the ECM receives data such as power output required for the engine (required output), estimated torque produced by the engine (estimated torque), engine speed of control target (target speed), and whether the engine is in start mode or not. Then, based on the required output and target speed, the ECM calculates a target torque that is to be produced by the engine and compares it with the estimated torque. If the estimated torque is very low compared with the target torque, or the engine start mode continues for the specific duration calculated by the coolant temperature, an abnormal condition is detected.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| P3190 | Following conditions continue at a fixed engine speed or a fixed length of time (1 trip detection logic): Communication with power management control ECU is normal Engine speed is a fixed value or more Engine start mode is not active Target torque is a fixed value Ratio of estimated torque against target torque is less than 20% | Intake system Throttle body assembly Fuel pressure Engine Mass air flow meter sub-assembly Out of fuel Engine coolant temperature sensor Crankshaft position sensor Camshaft position sensor EGR valve assembly ECM |
| P3191 | Following conditions continue at a fixed engine speed or a fixed length of time (1 trip detection logic): Communication with power management control ECU is normal Engine speed is a fixed value or more Engine start mode is active Engine start no-determination for 100 engine revolutions or more, and 6 seconds or more | Intake system Throttle body assembly Fuel pressure Engine Mass air flow meter sub-assembly Out of fuel Engine coolant temperature sensor Crankshaft position sensor Camshaft position sensor EGR valve assembly ECM |
| P3193 | Following conditions are met (1 trip detection logic): Fuel low level signal input into ECM Detection condition for P3190 or P3191 is satisfied | Out of fuel ECM |
The ECM and power management control ECU are connected by a communication line called CAN. The ECM sends engine speed data and other data to the power management control ECU while the power management control ECU sends the information such as a requirement for the engine power to the ECM using the CAN communication line. When the communication between the ECM and power management control ECU is normal and the following items become a specified condition, the ECM illuminates the MIL and sets a DTC.
- Engine speed
- Target torque
- Ratio of target torque against estimated torque
- Fuel level
The Controller Area Network (CAN) is a serial data communication system for real-time application. It is a multiplex communication system designed for on-vehicle use that provides a superior communication speed of 500 kbps and a capability to detect malfunctions. Through the combination of the CANH and CANL, and CANP and CANN bus lines, the CAN is able to maintain communication based on differential voltage.
| DTC No. | DTC Detection Condition | Trouble Area |
|---|---|---|
| U0293 | Communication with power management control ECU is interrupted (1 trip detection logic) | Wire harness Power management control ECU |
While the engine is running, if predetermined conditions (closed loop, etc.) are met, the purge VSV is opened by the ECM and stored fuel vapors in the canister are purged to the intake manifold. The ECM will change the duty cycle ratio of the purge VSV to control purge flow volume.
Purge flow volume is also determined by the intake manifold pressure. Atmospheric pressure is allowed to enter the canister through the vent valve to ensure that purge flow is maintained when negative pressure (vacuum) is applied to the canister.
The ECM monitors the condition of both the key-off monitor and purge flow monitor to ensure proper operation of the EVAP system.
Scheme 449
| *1 | Location of EVAP (Evaporative Emission) System | *2 | Purge VSV |
|---|---|---|---|
| *3 | EVAP Hose (to Intake Manifold) | *4 | EVAP Hose (from Canister) |
| *5 | Canister Pump Module | *6 | Canister |
| *7 | Canister Filter | *8 | Air Inlet Port |
| *9 | Fuel Tank Cap | *10 | Fuel Tank |
| *11 | Purge Line | *12 | Fuel Tank Pressure |
| *13 | Fuel Vapor-containment Valve |
TEXT IN ILLUSTRATION
Scheme 450
| *1 | EVAP System Circuit | *2 | Intake Manifold |
|---|---|---|---|
| *3 | Purge VSV | *4 | Throttle Valve |
| *5 | Canister | *6 | Air Cleaner |
| *7 | ECM | *8 | Soak Timer |
| *9 | Canister Filter | *10 | Fuel Tank Pressure Sensor |
| *11 | Canister Pump Module | *12 | Roll-over Valve |
| *13 | Cut-off Valve | *14 | Fuel Tank |
| *15 | Fuel Tank Cap | *16 | Fuel Vapor-containment Valve |
| *17 | Fuel outlet valve |
TEXT IN ILLUSTRATION
| Component | Operation |
|---|---|
| Canister | Contains activated charcoal to absorb fuel vapors that are created in fuel tank. |
| Cut-off valve | Located in the fuel tank. Valve closes by its own weight when vehicle is overturned to prevent fuel from spilling out. |
| Purge VSV | Opens or closes line between canister and intake manifold. ECM opens and closes purge VSV to control EVAP purge flow. ECM opens purge valve to purge the fuel vapors that were absorbed by canister to intake manifold. ECM controls EVAP volume purged to intake manifold by duty cycle (current-carrying time) to purge valve. (ON: Open, OFF: Close) |
| Roll-over valve | Located in fuel tank. Valve floats and closes when fuel tank is filled to 100%. Also, valve closes by its own weight when vehicle is overturned to prevent fuel from spilling out. |
| Soak timer | Built into ECM. To ensure that EVAP monitor values will be accurate, soak timer counts 5 hours (+/-15 minutes) from when power switch is turned off. This will allow fuel to cool down, which will stabilize fuel tank pressure. When approximately 5 hours have passed, ECM turns on ( see scheme 3see scheme 3). |
| Fuel vapor-containment valve | Opens and closes line between fuel tank and canister. When vehicle is stopped, this valve stays closed to keep fuel vapors in the tank and prevent them from being absorbed by canister. During refueling, valve opens to allow fuel vapors from tank to be absorbed by canister. When the vehicle is being driven, the valve maintains a slight positive pressure in the fuel tank. |
| Fuel tank pressure sensor | Converts pressure in fuel tank into voltage reading for use by ECM. ECM supplies 5 V to sensor, and uses voltage reading that is output as feedback to allow monitoring of fuel tank pressure ( see scheme 4see scheme 4). |
| Canister pump module | The following 5 items labeled (a) to (e) are canister pump module components. Canister pump module cannot be disassembled. |
| (a) Vent valve | Can either close vent for canister, or open vent to atmosphere. When ECM turns valve on, canister vent is closed. Alternately, when ECM turns valve off, canister vent is opened to atmosphere. To check for leaks in EVAP system, purge VSV is left closed, vent valve is turned on (canister vent is closed), and vacuum pump is operated to create a vacuum (negative pressure) in the system ( see scheme 1see scheme 1). |
| (b) Canister pressure sensor | ECM applies 5 V to pressure sensor, allowing it to create voltage reading that is used by ECM to detect pressure in canister ( see scheme 2see scheme 2). |
| (c) Check valve | Composed of nylon ball and spring. Valve blocks off atmosphere from outlet of vacuum pump. |
| (d) Leak detection pump | Used to create negative pressure (vacuum) in EVAP system to allow checking for leaks. |
| (e) Reference orifice | The diameter of reference orifice is 0.02 inches. Negative pressure (vacuum) is created, and pressure is measured with purge VSV closed (off) and vent valve off (in vent position). This reference pressure is used to set a baseline (criterion pressure) against which a small leak can be judged. |
Scheme 451
| *1 | Canister Pump Module see scheme 1 | *2 | Airflow |
|---|---|---|---|
| *3 | Condition: Purge Flow | *4 | Condition: Leak Check |
| *5 | Vent Valve: off (vent) | *6 | To Canister Filter (Atmosphere) |
| *7 | Canister | *8 | Reference Orifice (0.02 Inch) |
| *9 | Canister Pressure Sensor | *10 | Leak Detection Pump: off |
| *11 | Vent Valve: on (closed) | *12 | Leak Detection Pump: on |
TEXT IN ILLUSTRATION
Scheme 452
HINT
Standard atmospheric pressure is 101.3 kPa (760 mmHg-a)
Scheme 453
Scheme 454
Key-off Monitor
This monitoring system checks for canister pump module malfunctions and leaks from the EVAP and closed tank systems. Be sure to leave the vehicle for at least 5 hours to sufficiently cool the fuel and stabilize fuel tank pressure. This makes EVAP system monitoring more accurate.
HINT
If the engine coolant temperature is 50°C (122°F) or more, 5 hours after the power switch has been turned off, the ECM will begin performing a monitor check after another 2 hours. If the engine coolant temperature is still 50°C (122°F) or more, 7 hours after the power switch has been turned off, the ECM will begin performing a monitor check after another 2.5 hours.
There are two methods for monitoring the EVAP system.
- If the fuel tank pressure is higher or lower than the atmospheric pressure, the system determines that there are no leaks in the closed tank system and the system will check for leaks from the piping and canister between the purge VSV and canister pump module. (Method A)
- If the fuel tank pressure is almost the same as the atmospheric pressure, vacuum will be allowed to enter the fuel tank and the system will check for leaks from the fuel tank after checking for leaks from the canister. (Method B)
Scheme 455
Scheme 456
| Sequence | Operation | Description | Duration |
|---|---|---|---|
| ECM activation | Activated by soak timer, 5 hours (7 or 9.5 hours) after power switch turned off. | ||
| A | Atmospheric pressure measurement | Vent valve 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 and 111 kPa (525 mmHg and 832 mmHg), ECM cancels EVAP system monitor. | 60 seconds |
| B | First reference pressure measurement | In order to determine reference pressure standard, vacuum pump creates negative pressure (vacuum) through reference orifice and then ECM checks if vacuum 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 EVAP system pressure is then measured. Write down measured values 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 opens 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 standards. If stabilized system pressure is higher than second reference pressure standard, ECM determines that EVAP system has a leak. | 60 seconds |
| F | Resetting | Fuel tank pressure is compared with atmospheric pressure. If tank pressure is higher than PH or lower than PL, ECM determines that EVAP system is normal and runs sequence I in method B. If tank pressure is around atmospheric pressure, ECM performs sequence G in method A. | 5 seconds |
| G | Fuel tank pressure measurement | Vent valve is turned on (closed). Fuel vapor-containment valve opens to allow negative pressure to enter the fuel tank and fuel tank pressure is measured. Write down measured values because they will be used in leak check. If fuel tank pressure does not stabilize within 15 minutes, ECM stops monitoring. | 15 minutes* |
| H | Third reference leak pressure measurement | After 3rd reference pressure measurement, leak check of fuel tank is performed. If recorded fuel tank pressure is higher than 3rd reference leak pressure, ECM determines that EVAP system has a leak. | 60 seconds |
| I | Fuel vapor-containment valve stuck closed check | Fuel vapor-containment valve is opened for a certain period of time to check whether the valve is stuck closed. | 0.1 second |
| J | Final check | Atmospheric pressure is measured and then monitoring result is recorded by ECM. |
HINT
*: If there is only a small amount of fuel in the fuel tank, stabilizing the EVAP pressure takes longer than usual.
Scheme 457
| *1 | Operation A | *2 | Canister |
|---|---|---|---|
| *3 | Reference Orifice (0.02 inch) | *4 | Canister Pressure Sensor |
| *5 | Purge VSV | *6 | Fuel Vapor-containment Valve |
| *7 | Fuel Tank Pressure Sensor | *8 | Fuel Tank |
| *9 | Canister Pump Module | *10 | Vent Valve: OFF (Vent) |
| *11 | Canister Filter | *12 | Vacuum Pump: OFF |
| *13 | OFF | *14 | Operation B, E, H |
| *15 | ON | *16 | OFF (Vent) |
| *17 | Operation C | *18 | ON (Closed) |
| *19 | Operation D | *20 | Operation F, I |
| *21 | Atmospheric Pressure | *22 | Negative Pressure |
TEXT IN ILLUSTRATION
Purge Flow Monitor
If the EVAP system pressure change is less than 1 kPa (7.5 mmHg) when the engine is running and the purge VSV is turned on (closed), the ECM determines that the purge flow is insufficient.
Scheme 458
| *1 | EVAP Purge Flow | *2 | To Intake Manifold |
|---|---|---|---|
| *3 | ECM | *4 | Soak Timer |
| *5 | Purge VSV (on) | *6 | Fuel Tank Cap |
| *7 | Canister Filter | *8 | Fuel Tank |
| *9 | Leak Detection Pump (off) | *10 | Canister Pressure Sensor |
| *11 | Reference Orifice (0.02 inch) | *12 | Vent Valve (off) |
| *13 | Canister Pump Module | *14 | Canister |
| *15 | Fuel Vapor-containment Valve | *16 | Fuel Outlet Valve |
| *17 | Fuel Tank Pressure Sensor |
TEXT IN ILLUSTRATION
Scheme 459
Scheme 460
When the power switch is turned on (IG), 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 No. 2 integration relay (EFI MAIN relay) and supplying power to either terminal +B and +B2 of the ECM.
Scheme 461
The ECM constantly uses 5 V from the battery voltages supplied to the +B (BATT) terminal to operate the microprocessor. The ECM also provides this power to the sensors through the VC output circuit.
Scheme 462
When the VC circuit is shorted, the microprocessor in the ECM and sensors that are supplied power through the VC circuit are inactivated because the 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 for several seconds when the power switch is first turned on (IG). The MIL goes off when the engine is started.
Scheme 463
Scheme 464
Scheme 465
Scheme 466
- CHECK MIL Check that the Malfunction Indicator Lamp (MIL) illuminates when turning the power switch on (IG). OK MIL lights up. NG --> See step 2 OK --> See step 14
- CHECK CONNECTION BETWEEN TECHSTREAM AND ECM Connect the Techstream to the DLC3. Turn the power switch on (IG). Turn the Techstream on. Check the communication between the Techstream and ECM. Result Result Proceed to Communication is not possible A Communication is possible B B --> See step 15 A: Go to next step
- CHECK MIL (THROTTLE POSITION SENSOR) Disconnect the throttle position sensor connector. Turn the power switch on (IG). Check the MIL. Result Result Proceed to MIL does not illuminate A MIL illuminates B Reconnect the throttle position sensor connector. B --> See step 16 A: Go to next step
- CHECK MIL (CAMSHAFT POSITION SENSOR) Disconnect the camshaft position sensor connector. Turn the power switch on (IG). Check the MIL. Result Result Proceed to MIL does not illuminate A MIL illuminates B Reconnect the camshaft position sensor connector. B --> See step 17 A: Go to next step
- CHECK MIL (MANIFOLD ABSOLUTE PRESSURE SENSOR) Disconnect the manifold absolute pressure sensor connector. Turn the power switch on (IG). Check the MIL. Result Result Proceed to MIL does not illuminate A MIL illuminates B Reconnect the manifold absolute pressure sensor connector. B --> See step 18 A: Go to next step
- CHECK MIL (CANISTER PUMP MODULE) Disconnect the canister pump module connector. Turn the power switch on (IG). Check the MIL. Result Result Proceed to MIL does not illuminate A MIL illuminates B Reconnect the canister pump module connector. B --> See step 19 A: Go to next step
- CHECK MIL (FUEL TANK PRESSURE SENSOR) Disconnect the fuel tank pressure sensor connector. Turn the power switch on (IG). Check the MIL. Result Result Proceed to MIL does not illuminate A MIL illuminates B B --> REPLACE FUEL TANK PRESSURE SENSOR A: Go to next step
- CHECK HARNESS AND CONNECTOR (THROTTLE POSITION SENSOR - ECM) Disconnect the throttle position sensor connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition D28-88 (VCTA) or D4-5 (VC) - Body ground Always 10 kohms or higher Reconnect the throttle position sensor connector. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (THROTTLE POSITION SENSOR - ECM) OK: Go to next step
- CHECK HARNESS AND CONNECTOR (CAMSHAFT POSITION SENSOR - ECM) Disconnect the camshaft position sensor connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition D18-3 (VC) or D28-99 (VCV1) - Body ground Always 10 kohms or higher Reconnect the camshaft position sensor connector. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (CAMSHAFT POSITION SENSOR - ECM) OK: Go to next step
- CHECK HARNESS AND CONNECTOR (MANIFOLD ABSOLUTE PRESSURE SENSOR - ECM) Disconnect the manifold absolute pressure sensor connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition D3-3 (VC) or D28-72 (VCPM) - Body ground Always 10 kohms or higher Reconnect the manifold absolute pressure sensor connector. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (MANIFOLD ABSOLUTE PRESSURE SENSOR - ECM) OK: Go to next step
- CHECK HARNESS AND CONNECTOR (NO. 3 FRAME WIRE - ECM) Disconnect the No. 3 frame wire from the floor wire side connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition R45-6 (VCC) or D28-113 (VCPP) - Body ground Always 10 kohms or higher R45-2 (VC) or A57-57 (VPTK) - Body ground Always 10 kohms or higher Reconnect the No. 3 frame wire to the floor wire connector. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (NO. 3 FRAME WIRE - ECM) OK: Go to next step
- CHECK HARNESS AND CONNECTOR (CANISTER PUMP MODULE - FLOOR WIRE) Disconnect the No. 3 frame wire from the canister pump module and floor wire side connectors. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition No. 3 frame wire canister pump module side terminal 6 or R45-6 (VCC) - Body gound Always 10 kohms or higher TEXT IN ILLUSTRATION *a Front view of the wire harness connector (to Canister Pump Module) *b Front view of the wire harness connector (to Floor Wire) Reconnect the No. 3 frame wire to the canister pump module and floor wire side connectors. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (CANISTER PUMP MODULE - FLOOR WIRE) OK: Go to next step
- CHECK HARNESS AND CONNECTOR (FUEL TANK PRESSURE SENSOR - FLOOR WIRE) Disconnect the No. 3 frame wire from the fuel tank pressure sensor and floor wire side connectors. Measure the resistance according to the value(s) in the table below. Standard Resistance Tester Connection Condition Specified Condition No. 3 frame wire fuel tank pressure sensor side terminal 3 or R45-2 (VC) - Body ground Always 10 kohms or higher TEXT IN ILLUSTRATION *a Front view of the wire harness connector (to Fuel Tank Pressure Sensor) *b Front view of the wire harness connector (to Floor Wire) Reconnect the No. 3 frame wire to the fuel tank pressure sensor and floor wire side connectors. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (FUEL TANK PRESSURE SENSOR - FLOOR WIRE) OK --> See step 20
- PROCEED TO NEXT SUSPECTED AREA SHOWN IN PROBLEM SYMPTOMS TABLE. Refer to «PROBLEM SYMPTOMS TABLE»(ref-393417-S39658364762011040700000)
- GO TO MIL CIRCUIT. Refer to «MIL Circuit»(ref-393419-S38732353932011040700000)
- REPLACE THROTTLE BODY ASSEMBLY. Refer to «REMOVAL»(ref-393423-S42932276002011040700000)
- REPLACE CAMSHAFT POSITION SENSOR. Refer to «REMOVAL»(ref-393423-S28940228442011040700000)
- REPLACE MANIFOLD ABSOLUTE PRESSURE SENSOR. Refer to «REMOVAL»(ref-393412-S38654987542011040700000)
- REPLACE CANISTER. Refer to «REMOVAL»(ref-393412-S26183763292011040700000)
- REPLACE ECM. Refer to «REMOVAL»(ref-393423-S41700152002011040700000)
When the NE signal is input to the ECM, Tr is turned on, current flows to the coil of the circuit opening relay, the relay switches on, power is supplied to the fuel pump and the fuel pump operates.
While the NE signal is generated (engine running), the ECM keeps Tr on (circuit opening relay on) and the fuel pump also keeps operating.
Scheme 467
The fuel injectors are located on the intake manifold. They inject fuel into the cylinders based on the signals from the ECM.
Scheme 468
Scheme 469
- CHECK FUEL INJECTOR ASSEMBLY (POWER SOURCE) Disconnect the fuel injector assembly connectors. Turn the power switch on (IG). Measure the voltage according to the value(s) in the table below. Standard Voltage Tester Connection Switch Condition Specified Condition D14-1 - Body ground Power switch on (IG) 11 to 14 V D15-1 - Body ground Power switch on (IG) 11 to 14 V D16-1 - Body ground Power switch on (IG) 11 to 14 V D17-1 - Body ground Power switch on (IG) 11 to 14 V TEXT IN ILLUSTRATION *a Front view of wire harness connector (to Fuel Injector Assembly) Reconnect the fuel injector assembly connectors. NG --> See step 4 OK: Go to next step
- INSPECT FUEL INJECTOR ASSEMBLY Inspect the fuel injector assembly. Refer to «INSPECTION»(/toyota/prius/iii-2009-2011/remont/fuel-system/#engine-fuel-system-service-information-phv) . NG --> See step 5 OK: Go to next step
- CHECK HARNESS AND CONNECTOR (FUEL INJECTOR ASSEMBLY - ECM) Disconnect the fuel injector assembly connectors. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance (Check for Open) Tester Connection Condition Specified Condition D14-2 - D28-85 (#10) Always Below 1 ohms D15-2 - D28-84 (#20) Always Below 1 ohms D16-2 - D28-83 (#30) Always Below 1 ohms D17-2 - D28-82 (#40) Always Below 1 ohms Standard Resistance (Check for Short) Tester Connection Condition Specified Condition D14-2 or D28-85 (#10) - Body ground Always 10 ohms or higher D15-2 or D28-84 (#20) - Body ground Always 10 ohms or higher D16-2 or D28-83 (#30) - Body ground Always 10 ohms or higher D17-2 or D28-82 (#40) - Body ground Always 10 ohms or higher Reconnect the fuel injector assembly connectors. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (FUEL INJECTOR ASSEMBLY - ECM) OK --> See step 6
- CHECK HARNESS AND CONNECTOR (NO. 2 INTEGRATION RELAY (IG2 RELAY) - FUEL INJECTOR ASSEMBLY) Disconnect the fuel injector assembly connectors. Remove the No. 2 integration relay from the engine room relay block. Disconnect the No. 2 integration relay connector. Measure the resistance according to the value(s) in the table below. Standard Resistance (Check for Open) Tester Connection Condition Specified Condition D14-1 - 1A-4 Always Below 1 ohms D15-1 - 1A-4 Always Below 1 ohms D16-1 - 1A-4 Always Below 1 ohms D17-1 - 1A-4 Always Below 1 ohms Standard Resistance (Check for Short) Tester Connection Condition Specified Condition D14-1 or 1A-4 - Body ground Always 10 kohms or higher D15-1 or 1A-4 - Body ground Always 10 kohms or higher D16-1 or 1A-4 - Body ground Always 10 kohms or higher D17-1 or 1A-4 - Body ground Always 10 kohms or higher Reconnect the fuel injector assembly connectors. Reconnect the No. 2 integration relay connector. Reinstall the No. 2 integration relay. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (NO. 2 INTEGRATION RELAY (IG2 RELAY) - FUEL INJECTOR ASSEMBLY) OK --> See step 7
- REPLACE FUEL INJECTOR ASSEMBLY. Refer to «REMOVAL»(/toyota/prius/iii-2009-2011/remont/fuel-system/#engine-fuel-system-service-information-phv)
- PROCEED TO NEXT SUSPECTED AREA SHOWN IN PROBLEM SYMPTOMS TABLE. Refer to «PROBLEM SYMPTOMS TABLE»(ref-393417-S39658364762011040700000)
- CHECK ECM POWER SOURCE CIRCUIT. Refer to «ECM Power Source Circuit»(ref-393419-S32910190392011040700000)
The MIL (Malfunction Indicator Lamp) is used to indicate vehicle malfunction detected by the ECM. When the power switch is turned on (IG), 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 power switch is first turned on (IG), the MIL should illuminate and should then turn off. If the MIL remains illuminated or is not illuminated, conduct the following troubleshooting procedure using the Techstream.
Scheme 470
Scheme 471
Scheme 472
- CHECK THAT MIL IS ILLUMINATED Turn the power switch on (IG). Check the illumination of the MIL. Result Condition Proceed to MIL remains illuminated (Even after power switch is turned on (IG) and several seconds have passed, MIL still remains illuminated) A MIL remains off (Does not illuminate at all) B MIL illuminates for several seconds, but turns off after engine is started C C --> SYSTEM OK B --> See step 5 A: Go to next step
- CHECK WHETHER MIL TURNS OFF Connect the Techstream to the DLC3. Turn the power switch on (IG). Turn the Techstream on. Enter the following menus: Powertrain / Engine and ECT / Trouble Codes. Check if any DTCs have been stored. Note down the DTCs. Clear the DTCs. Refer to «DTC CHECK / CLEAR»(ref-393417-S07712997152011040700000). Check if the MIL goes off. OK MIL goes off. NG --> See step 3 OK --> See step 8
- CHECK HARNESS AND CONNECTOR (CHECK FOR SHORT IN WIRE HARNESS) Disconnect the ECM connector. TEXT IN ILLUSTRATION *a Front view of wire harness connector (to ECM) Turn the power switch on (IG). Check that the MIL is not illuminated. OK MIL is not illuminated. Reconnect the ECM connector. NG --> See step 4 OK --> See step 9
- CHECK HARNESS AND CONNECTOR (NO. 3 METER CIRCUIT PLATE - ECM) Disconnect the No. 3 meter circuit plate connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance (Check for Short) Tester Connection Condition Specified Condition L27-25 (EFI) or A57-36 (W) - Body ground Always 10 kohms or higher Reconnect the No. 3 meter circuit plate connector. Reconnect the ECM connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (NO. 3 METER CIRCUIT PLATE - ECM) OK --> See step 10
- CHECK THAT ENGINE STARTS Turn the power switch on (IG). Put the engine in inspection mode. Refer to «INSPECTION MODE PROCEDURE»(ref-393299-S13482363572011040700000). Start the engine. Result Result Proceed to Engine starts A Engine cannot be put in inspection mode* (Engine cannot start) B HINT: *: The Techstream cannot communicate with the ECM. B --> See step 11 A: Go to next step
- CHECK HARNESS AND CONNECTOR (ECM TERMINAL VOLTAGE) Disconnect the ECM connector. Turn the power switch on (IG). Measure the voltage according to the value(s) in the table below. Standard Voltage Tester Connection Switch Condition Specified Condition A57-36 (W) - Body ground Power switch on (IG) 11 to 14 V TEXT IN ILLUSTRATION *a Front view of wire harness connector (to ECM) NG --> See step 7 OK --> See step 9
- CHECK HARNESS AND CONNECTOR (NO. 3 METER CIRCUIT PLATE - ECM) Disconnect the No. 3 meter circuit plate connector. Disconnect the ECM connector. Measure the resistance according to the value(s) in the table below. Standard Resistance (Check for Open) Tester Connection Condition Specified Condition L27-25 (EFI) - A57-36 (W) Always Below 1 ohms Reconnect the ECM connector. Reconnect the No. 3 meter circuit plate connector. NG --> REPAIR OR REPLACE HARNESS OR CONNECTOR (NO. 3 METER CIRCUIT PLATE - ECM) OK --> See step 10
- REPAIR CIRCUITS INDICATED BY OUTPUT DTCS. Refer to «DIAGNOSTIC TROUBLE CODE CHART»(ref-393417-S03455429922011040700000)
- REPLACE ECM. Refer to «REMOVAL»(ref-393423-S41700152002011040700000)
- REPLACE NO. 3 METER CIRCUIT PLATE. Refer to «DISASSEMBLY»(ref-393432-S06811448102011040700000)
- GO TO VC OUTPUT CIRCUIT. Refer to «VC Output Circuit»(ref-393419-S21298978912011040700000)