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Evaporative Vacuum Leak Detection System

Fig 1: Locating Evaporative Vacuum Leak Detection System Components
GC0033600Courtesy of DAIMLERCHRYSLER CORP.
1 - FUEL LEVEL SENDING UNIT/PRESSURE SENSOR
2 - FUEL WARNING INDICATOR
3 - INSTRUMENT CLUSTER
4 - MALFUNCTION INDICATOR LAMP
5 - POWERTRAIN CONTROL MODULE
6 - FUEL PUMP RELAY
7 - FUEL FILTER/PRESSURE REGULATOR
8 - FUEL PUMP
9 - FUEL TANK
10 - FUEL VAPOR PRESSURE RELIEF VALVE
11 - EVAP PURGE SOLENOID
12 - EVAP CANISTER
13 - CHARCOAL CANISTER SHUTOFF VALVE
14 - FUEL FILLER CAP

The Evaporative Vacuum Leak Detection (EVLD) system has replaced the leak detection pump as the method of evaporative system leak detection. This is to detect a leak equivalent to a 0.5 mm (0.020 in.) hole. This system has the capability to detect holes of this size very dependably. In addition to the detection of very small leaks, this system has the capability of detecting medium as well as large evaporative system leaks.

The EVLD system incorporates the EVAP Purge Hoses, EVAP Canister, fuel tank, fuel filler neck and fuel filler cap with the Charcoal Canister Shutoff Valve, EVAP Purge Solenoid, PCM and engine vacuum to detect a leak in the purge system.

The PCM seals the Charcoal Canister Shutoff Valve and opens the EVAP Purge Solenoid to perform the 3-stage leak test after the following conditions have been met:

The leak test consists of three successive tests that are dependent on the previous test passing. If one test fails, the next test will not be run. The major leak test begins by closing the Charcoal Canister Shutoff Valve and opening the EVAP Purge Solenoid to allow engine vacuum to build to 6 mbar (2.4 in H2O), as measured by the Fuel Tank Pressure Sensor, in the fuel tank within approximately 12 seconds. If there is no vacuum buildup in the fuel tank, there is a major leak present, the leak test is aborted, the Low Fuel Warning Indicator is illuminated in the instrument cluster and a DTC is stored in the PCM.

If the major leak test passes, the EVAP Purge Solenoid is closed when vacuum inside the fuel tank reaches approximately 6 mbar (2.4 in H2O) and the vacuum is analyzed for approximately 30 seconds. The vacuum must not drop by more than 0.3 to 0.5 mbar (0.12 to 0.2 in H2O), depending on the fuel level in the fuel tank, during the 30 second time period. If there is a minor leak, the leak test is aborted and a DTC is stored in the PCM. The leak test will be aborted if an excessive lean correction occurs during vacuum buildup.

If the minor leak test passes, the micro leak test initiates by again bringing the vacuum in the fuel tank up to approximately 6 mbar (2.4 in H2O). Once the vacuum in the fuel tank is re-established, the EVAP Purge Solenoid is closed. The vacuum must not drop by more than 0.1 to 0.15 mbar (0.04 to 0.06 in H2O), depending on the fuel level in the fuel tank, per second. If the vacuum drops more rapidly, a DTC is stored in the PCM. The leak test will be aborted if an excessive lean correction occurs during vacuum buildup.

When the leak test is complete, the EVAP Purge Solenoid is opened and the purge control system returns to normal operation.