revealed during the leak test portion of the test, the
test is terminated at the end of the test mode and no
further system checks will be performed.
After passing the leak detection phase of the test,
system pressure is maintained by turning on the
LDP’s solenoid until the purge system is activated.
Purge activation in effect creates a leak. The cycle
rate is again interrogated and when it increases due
to the flow through the purge system, the leak check
portion of the diagnostic is complete.
The canister vent valve will unseal the system
after completion of the test sequence as the pump
diaphragm assembly moves to the full travel position.
Evaporative system functionality will be verified by
using the stricter evap purge flow monitor. At an
appropriate warm idle the LDP will be energized to
seal the canister vent. The purge flow will be clocked
up from some small value in an attempt to see a
shift in the 02 control system. If fuel vapor, indicated
by a shift in the 02 control, is present the test is
passed. If not, it is assumed that the purge system is
not functioning in some respect. The LDP is again
turned off and the test is ended.
Enabling Conditions for Systems with LDP
• Ambient Air Temperature
• Barometric Pressure
• Fuel level
• Engine Temperature
• No stalling
• Battery voltage
NON-LDP VEHICLES— On a vehicle without an
EVAP leak detection pump system, changes in short
term memory and movement in target IAC at idle or
idle speed change, are used to monitor the system.
There are two stages for this test.
Stage One— Stage one is a non-intrusive test.
The PCM compares adaptive memory values between
purge and purge-free cells. The PCM uses these val-
ues to determine the amount of fuel vapors entering
the system. If the difference between the cells
exceeds a predetermined value, the test passes. If
not, then the monitor advances to state two.
Stage Two— Once the enabling conditions are
met, the PCM de-energizes the Duty Cycle Purge
(DCP) solenoid. The PCM then waits until engine
RPM, Short Term Compensation and Idle Air Control
have all stabilized. Once stable, the PCM increments
the DCP solenoid cycle rate approximately 6% every
8 engine revolutions. If during the test any one of
three conditions occur before the DCP cycle reaches
100%, the EVAP system is considered to be opera-
tional and the test passes. These conditions are as
follows:
• RPM rises by a predetermined amount
• Short Term drops by a predetermined amount
• Idle Air Control closes by a predetermined
amount
When none of the previous conditions occur, the
test fails and the PCM increments a counter by one.
When the PCM runs the test three times during a
trip, and the counter has been incremented to three,
the monitor fails and a Freeze Frame is stored.
Enabling Conditions (Stage Two)— The follow-
ing conditions must be met to enable the EVAP Mon-
itor (without LDP)
• Ambient Air Temperature
• Barometric Pressure
• Fuel level
• Engine Temperature
• Engine run time
• RPM stable
• MAP
• Generator, radiator fans, A/C clutch
Pending Conditions-With or Without LDP—
The EVAP Monitor is suspended and does not run,
when the MIL is illuminated due to any of the fol-
lowing faults:
• Misfire
• Oxygen Sensor Monitor
• Fuel System Rich
• Fuel System Lean
• EGR Monitor
• MAP
• TPS
• ECT
• DCP Solenoid
Conflict Conditions-With or Without LDP—
The EVAP Monitor does not run if any of the follow-
ing tests are in progress:
• Catalyst
• EGR
• Fuel System
• Misfire
TRIP DEFINITION
OPERATION
A “Trip” means vehicle operation (following an
engine-off period) of duration and driving mode such
that all components and systems are monitored at
least once by the diagnostic system. The monitors
must successfully pass before the PCM can verify
that a previously malfunctioning component is meet-
ing the normal operating conditions of that compo-
nent. For misfire or fuel system malfunction, the
MIL may be extinguished if the fault does not recur
when monitored during three subsequent sequential
driving cycles in which conditions are similar to
those under which the malfunction was first deter-
mined.
JX
EMISSION CONTROL SYSTEMS
25 - 19
DESCRIPTION AND OPERATION (Continued)