General description

The Engine Coolant Temperature Sensor (ECTS) is located in the engine coolant passage of the cylinder head for detecting the engine coolant temperature. The ECTS uses a thermistor whose resistance changes with the temperature. The electrical resistance of the ECTS decreases as the temperature increases, and increases as the temperature decreases. The reference 5 V in the PCM is supplied to the ECTS via a resistor in the PCM. That is, the resistor in the PCM and the thermistor in the ECTS are connected in series. When the resistance value of the thermistor in the ECTS changes according to the engine coolant temperature, the output voltage also changes. During cold engine operation the PCM increases the fuel injection duration and controls the ignition timing using the information of engine coolant temperature to avoid engine stalling and improve drivability.

DTC Description

Checking the engine coolant temperature under detecting condition, if the engine coolant temperature's signal is temporarily stuck above the lowest enable temperature to enable other diagnostic, PCM sets P0116. MIL(Malfunction Indication Lamp) turns on when the malfunction lasts till consecutive 2 driving cycle.

DTC Detecting Condition

Item

Detecting Condition

Possible cause

DTC Strategy

Monitor the engine coolant temperature

ECTS

Enable

Conditions

Shutdown time > 180 minutes

Intake air-temperature at start-up < 40℃(104℉)

No disabling faults(ECTS)

Engine running > 60 seconds

Minimum airflow is satisfied for a certain time.

Threshold

value

When the start-up engine coolant temperature does not rise by 3 ℃(5.4℉).

Diagnosis

Time

Immediately

MIL On

Condition

2 Driving Cycle

Specifications

Temp. (℃/℉)

Resistance (kΩ)

Temp. (℃/℉)

Resistance (kΩ)

-40(-40)

48.14

40(104)

1.15

-20(-4)

14.13 ~ 16.83

60(140)

0.59

0(32)

5.79

80(176)

0.32

20(68)

2.31 ~ 2.59

Signal Waveform & Data

It is necessary that MAPS should be checked along with TPS. Because The MAP/TPS Rationality Diagnostic is comprised of two tests. A deceleration test is performed to provide a robust method for detection of an altitude compensated MAP value that is too high for the deceleration condition. The second test compares the altitude compensated MAP value to both high and low limits, dependent upon throttle position and engine speed. When the MAP value is out of the threshold range, the MAP/TPS system is determined to be failed.

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