2002 JEEP GRAND CHEROKEE dtc

Freeze Frame Data Storage
Once a failure occurs, the Task Manager records
several engine operating conditions and stores it in a
Freeze Frame. The Freeze Frame is considered one
frame of information taken by an on-board data
recorder. When a fault occurs, the PCM stores the
input data from various sensors so that technicians
can determine under what vehicle operating condi-
tions the failure occurred.
The data stored in Freeze Frame is usually
recorded when a system fails the first time for two
trip faults. Freeze Frame data will only be overwrit-
ten by a different fault with a higher priority.
CAUTION: Erasing DTCs, either with the DRB III or
by disconnecting the battery, also clears all Freeze
Frame data.
Similar Conditions Window
The Similar Conditions Window displays informa-
tion about engine operation during a monitor. Abso-
lute MAP (engine load) and Engine RPM are stored
in this window when a failure occurs. There are two
different Similar conditions Windows: Fuel System
and Misfire.
FUEL SYSTEM
²Fuel System Similar Conditions WindowÐ
An indicator that 'Absolute MAP When Fuel Sys Fail'
and 'RPM When Fuel Sys Failed' are all in the same
range when the failure occurred. Indicated by switch-
ing from 'NO' to 'YES'.
²Absolute MAP When Fuel Sys FailÐ The
stored MAP reading at the time of failure. Informs
the user at what engine load the failure occurred.
²Absolute MAPÐ A live reading of engine load
to aid the user in accessing the Similar Conditions
Window.
²RPM When Fuel Sys FailÐ The stored RPM
reading at the time of failure. Informs the user at
what engine RPM the failure occurred.
²Engine RPMÐ A live reading of engine RPM
to aid the user in accessing the Similar Conditions
Window.
²Adaptive Memory FactorÐ The PCM utilizes
both Short Term Compensation and Long Term Adap-
tive to calculate the Adaptive Memory Factor for
total fuel correction.
²Upstream O2S VoltsÐ A live reading of the
Oxygen Sensor to indicate its performance. For
example, stuck lean, stuck rich, etc.
²SCW Time in Window (Similar Conditions
Window Time in Window)Ð A timer used by thePCM that indicates that, after all Similar Conditions
have been met, if there has been enough good engine
running time in the SCW without failure detected.
This timer is used to increment a Good Trip.
²Fuel System Good Trip CounterÐATrip
Counter used to turn OFF the MIL for Fuel System
DTCs. To increment a Fuel System Good Trip, the
engine must be in the Similar Conditions Window,
Adaptive Memory Factor must be less than cali-
brated threshold and the Adaptive Memory Factor
must stay below that threshold for a calibrated
amount of time.
²Test Done This TripÐ Indicates that the
monitor has already been run and completed during
the current trip.
MISFIRE
²Same Misfire Warm-Up StateÐ Indicates if
the misfire occurred when the engine was warmed up
(above 160É F).
²In Similar Misfire WindowÐ An indicator
that 'Absolute MAP When Misfire Occurred' and
'RPM When Misfire Occurred' are all in the same
range when the failure occurred. Indicated by switch-
ing from 'NO' to 'YES'.
²Absolute MAP When Misfire OccurredÐ
The stored MAP reading at the time of failure.
Informs the user at what engine load the failure
occurred.
²Absolute MAPÐ A live reading of engine load
to aid the user in accessing the Similar Conditions
Window.
²RPM When Misfire OccurredÐ The stored
RPM reading at the time of failure. Informs the user
at what engine RPM the failure occurred.
²Engine RPMÐ A live reading of engine RPM
to aid the user in accessing the Similar Conditions
Window.
²Adaptive Memory FactorÐ The PCM utilizes
both Short Term Compensation and Long Term Adap-
tive to calculate the Adaptive Memory Factor for
total fuel correction.
²200 Rev CounterÐ Counts 0±100 720 degree
cycles.
²SCW Cat 200 Rev CounterÐ Counts when in
similar conditions.
²SCW FTP 1000 Rev CounterÐ Counts 0±4
when in similar conditions.
²Misfire Good Trip CounterÐ Counts up to
three to turn OFF the MIL.
²Misfire DataÐ Data collected during test.
²Test Done This TripÐ Indicates YES when the
test is done.
WJEMISSIONS CONTROL 25 - 23
EMISSIONS CONTROL (Continued)

INSTALLATION - FIXED ORIFICE FITTING
When installing fixed orifice fitting, be sure loca-
tions of fixed orifice fitting and air inlet fitting (Fig.
9) have not been inadvertently exchanged. The fixed
orifice fitting is light grey in color and is located at
rearof valve cover. The air inlet fitting is black in
color and is located atfrontof valve cover.
(1) Connect fitting to CCV breather tube.
(2) Return fixed orifice fitting to valve cover grom-
met.
EVAP/PURGE SOLENOID
DESCRIPTION
The duty cycle EVAP canister purge solenoid (DCP)
regulates the rate of vapor flow from the EVAP can-
ister to the intake manifold. The Powertrain Control
Module (PCM) operates the solenoid.
OPERATION
During the cold start warm-up period and the hot
start time delay, the PCM does not energize the sole-
noid. When de-energized, no vapors are purged. The
PCM de-energizes the solenoid during open loop oper-
ation.
The engine enters closed loop operation after it
reaches a specified temperature and the time delay
ends. During closed loop operation, the PCM cycles
(energizes and de-energizes) the solenoid 5 or 10
times per second, depending upon operating condi-
tions. The PCM varies the vapor flow rate by chang-
ing solenoid pulse width. Pulse width is the amount
of time that the solenoid is energized. The PCM
adjusts solenoid pulse width based on engine operat-
ing condition.
REMOVAL
The duty cycle evaporative (EVAP) canister purge
solenoid is located in the engine compartment near
the brake master cylinder (Fig. 10).
(1) Disconnect electrical connector at solenoid.
(2) Disconnect vacuum lines at solenoid.
(3) Lift solenoid slot (Fig. 10) from mounting
bracket for removal.
INSTALLATION
(1) Position solenoid slot to mounting bracket.
(2) Connect vacuum lines to solenoid. Be sure vac-
uum lines are firmly connected and not leaking or
damaged. If leaking, a Diagnostic Trouble Code
(DTC) may be set with certain emission packages.
(3) Connect electrical connector to solenoid.
FUEL FILLER CAP
DESCRIPTION
The plastic fuel tank filler tube cap is threaded
onto the end of the fuel fill tube. Certain models are
equipped with a 1/4 turn cap.
OPERATION
The loss of any fuel or vapor out of fuel filler tube
is prevented by the use of a pressure-vacuum fuel fill
cap. Relief valves inside the cap will release fuel tank
pressure at predetermined pressures. Fuel tank vac-
uum will also be released at predetermined values.
This cap must be replaced by a similar unit if
replacement is necessary. This is in order for the sys-
tem to remain effective.
CAUTION: Remove fill cap before servicing any fuel
system component to relieve tank pressure. If
equipped with a California emissions package and a
Leak Detection Pump (LDP), the cap must be tight-
ened securely. If cap is left loose, a Diagnostic
Trouble Code (DTC) may be set.
REMOVAL
If replacement of the 1/4 turn fuel tank filler tube
cap is necessary, it must be replaced with an identi-
cal cap to be sure of correct system operation.
Fig. 10 EVAP/PURGE SOLENOID LOCATION
1 - BRAKE MASTER CYLINDER
2 - EVAP SOLENOID
3 - SLOT
4 - ELEC. CONNEC.
5 - VACUUM LINE CONNEC.
6 - TEST PORT
WJEVAPORATIVE EMISSIONS 25 - 29
CCV HOSE (Continued)

change from opened to closed. If the reed switch
changes too quickly, a leak may be indicated. The
longer it takes the reed switch to change state, the
tighter the evaporative system is sealed. If the sys-
tem pressurizes too quickly, a restriction somewhere
in the EVAP system may be indicated.
PUMPING ACTION
Action : During portions of this test, the PCM uses
the reed switch to monitor diaphragm movement.
The solenoid is only turned on by the PCM after the
reed switch changes from open to closed, indicating
that the diaphragm has moved down. At other times
during the test, the PCM will rapidly cycle the LDP
solenoid on and off to quickly pressurize the system.
During rapid cycling, the diaphragm will not move
enough to change the reed switch state. In the state
of rapid cycling, the PCM will use a fixed time inter-
val to cycle the solenoid. If the system does not pass
the EVAP Leak Detection Test, the following DTCs
may be set:
²P0442 - EVAP LEAK MONITOR 0.0409LEAK
DETECTED
²P0455 - EVAP LEAK MONITOR LARGE LEAK
DETECTED²P0456 - EVAP LEAK MONITOR 0.0209LEAK
DETECTED
²P1486 - EVAP LEAK MON PINCHED HOSE
FOUND
²P1494 - LEAK DETECTION PUMP SW OR
MECH FAULT
²P1495 - LEAK DETECTION PUMP SOLENOID
CIRCUIT
DIAGNOSIS AND TESTING - ENABLING
CONDITIONS TO RUN EVAP LEAK DETECTION
TEST
²Cold start: with ambient temperature (obtained
from modeling the inlet air temperature sensor on
passenger vehicles and the battery temperature sen-
sor on Jeep & Dodge Truck vehicles) between 4É C
(40É F) and 32É C (90É F) for 0.040 leak. Between 4É
C (40É F) and 29É C (85É F) for 0.020 leak.
²Engine coolant temperature within:-12É to -8É C
(10É to 18É F) of battery/ambient.
²Battery voltage between 10 and 15 volts.
²Low fuel warning light off (fuel level must be
between 15% and 85%.
²MAP sensor reading 22 in Hg or above (This is
the manifold absolute pressure, not vacuum).
Fig. 13 LDP AT REST
1 - Diaphragm
2 - Inlet Check Valve (Closed)
3 - Vent Valve (Open)
4 - From Air Filter
5 - To Canister
6 - Outlet Check Valve (Closed)
7 - Engine Vacuum (Closed)
Fig. 14 DIAPHRAGM UPWARD MOVEMENT
1 - Diaphragm
2 - Inlet Check Valve (Open)
3 - Vent Valve (Closed)
4 - From Air Filter
5 - To Canister
6 - Outlet Check Valve (Closed)
7 - Engine Vacuum (Open)
25 - 32 EVAPORATIVE EMISSIONSWJ
LEAK DETECTION PUMP (Continued)

²No engine stall during test.
NOTE: IF BATTERY VOLTAGE DROPS BELOW 10
VOLTS FOR MORE THAN 5 SECONDS DURING
ENGINE CRANKING, THE EVAP LEAK DETECTION
TEST WILL NOT RUN.
NOTE: THE FOLLOWING VALUES ARE APPROXI-
MATE AND VEHICLE SPECIFIC. USE THE VALUES
SEEN IN PRE TEST/MONITOR TEST SCREEN ON
THE DRB IIIT. SEE TSB 25-02-98 FOR MORE
DETAIL.
A DTC will not be set if a one-trip fault is set or if
the MIL is illuminated for any of the following:
²Purge Solenoid Electrical Fault
²All TPS Faults
²All Engine Controller Self Test Faults
²LDP Pressure Switch Fault
²All Cam and/or Crank Sensor Fault
²EGR Solenoid Electrical Fault
²All MAP Sensor Faults
²All Injector Faults
²Ambient/Battery Temperature Sensor Electrical
Faults²Baro Out of Range
²Vehicle Speed Faults
²All Coolant Sensor Faults
²LDP Solenoid Circuit
NOTE: IF BATTERY TEMPERATURE IS NOT WITHIN
RANGE, OR IF THE ENGINE COOLANT TEMPERA-
TURE IS NOT WITHIN A SPECIFIED RANGE OF THE
BATTERY TEMPERATURE, THE PCM WILL NOT
RUN TESTS FOR DTC P1494, P1486, P0442, P0455
AND P0441. THESE TEMPERATURE CALIBRATIONS
MAY BE DIFFERENT BETWEEN MODELS.
SECTION 1 - P1495 Leak Detection Pump
Solenoid Circuit-When the ignition key is turned
to9ON9, the LDP diaphragm should be in the down
position and the LDP reed switch should be closed. If
the EVAP system has residual pressure, the LDP dia-
phragm may be up. This could result in the LDP reed
switch being open when the key is turned to9ON9
and a P1494 fault could be set because the PCM is
expecting the reed switch to be closed.
After the key is turned9ON9, the PCM immedi-
ately tests the LDP solenoid circuit for electrical
faults. If a fault is detected, DTC P1495 will set, the
Fig. 15 DIAPHRAGM DOWNWARD MOVEMENT
1 - Diaphragm
2 - Inlet Check Valve (Closed)
3 - Vent Valve (Closed)
4 - From Air Filter
5 - To Canister
6 - Outlet Check Valve (Open)
7 - Engine Vacuum (Closed)EVAP LDP TEST SEQUENCE
1 - IGNITION SWITCH
2 - LDP DIAPHRAM
3 - LDP SWITCH
4 - LDP SOLENOID
5 - SECTION 1
6 - SECTION 2
7 - SECTION 3
8 - SECTION 4
9 - SECTION 5
10 - 3 TEST CYCLES TO TEST FOR BLOCKAGE
11- RAPID PUMP CYCLING FOR 70 CYCLES
WJEVAPORATIVE EMISSIONS 25 - 33
LEAK DETECTION PUMP (Continued)

MIL will illuminate, and the remaining EVAP Leak
Detection Test is canceled.
SECTION 2 - P1494 Leak Detection Pump
Switch or Mechanical Fault-If DTC P1495 is not
set, the PCM will check for DTC P1494. If the LDP
reed switch was closed when the key was turned to
9ON9, the PCM energizes the LDP solenoid for up to
8 seconds and monitors the LDP switch. As the LDP
diaphragm is pulled up by engine vacuum, the LDP
reed switch should change from closed to open. If it
does not, the PCM sets a temporary fault (P1494) in
memory, and waits until the next time the Enabling
Conditions are met to run the test again. If this is
again detected, P1494 is stored and the MIL is illu-
minated. If the problem is not detected during the
next enabling cycle, the temporary fault will be
cleared.
However, if the PCM detects the reed switch open
when the key is turned to9ON9, the PCM must deter-
mine if this condition is due to residual pressure in
the EVAP system, or an actual fault. The PCM stores
information in memory on EVAP system purging
from previous engine run or drive cycles.
If little or no purging took place, residual pressure
could be holding the LDP diaphragm up, causing the
LDP switch to be open. Since this is not a malfunc-
tion, the PCM cancels the EVAP Leak Detection Test
without setting the temporary fault.
If there was sufficient purging during the previous
cycle to eliminate EVAP system pressure, the PCM
judges that this is a malfunction and sets a tempo-
rary fault in memory. The next time that the
Enabling Conditions are met, the test will run again.
If the fault is again detected, the MIL will illuminate
and DTC P1494 will be stored. If the fault is not
detected, the temporary fault will be cleared.
SECTION 3 - P1486 EVAP Leak Monitor
Pinched Hose Found-If no fault has been detected
so far, the PCM begins testing for possible blockage
in the EVAP system between the LDP and the fuel
tank. This is done by monitoring the time required
for the LDP to pump air into the EVAP system dur-
ing two to three pump cycles. If no blockage is
present, the LDP diaphragm is able to quickly pump
air out of the LDP each time the PCM turns off the
LDP solenoid. If a blockage is present, the PCM
detects that the LDP takes longer to complete each
pump cycle. If the pump cycles take longer than
expected (approximately 6 to 10 seconds) the PCM
will suspect a blockage. On the next drive when
Enabling Conditions are met, the test will run again.
If blockage is again detected, P1486 is stored, and
the MIL is illuminated.
SECTION4-NoDTCCanBeSetDuring This
Time-After the LDP blockage tests are completed,
the PCM then tests for EVAP system leakage. First,the PCM commands the LDP to rapidly pump for 20
to 50 seconds (depending on fuel level) to build pres-
sure in the EVAP system. This evaluates the system
J18-24-0 to see if it can be sufficiently pressurized.
This evaluation (rapid pump cycling) may occur sev-
eral times prior to leak checking. The LDP reed
switch does not close and open during rapid pumping
because the diaphragm does not travel through its
full range during this part of the test.
SECTION 5 - P0456, P0442, P0455 EVAP Leak
Monitor and Leak Detected-Next, the PCM per-
forms one or more test cycles by monitoring the time
required for the LDP reed switch to close (diaphragm
to drop) after the LDP solenoid is turned off.
If the switch does not close, or closes after a long
delay, it means that the system does not have any
significant leakage and the EVAP Leak Detection
Test is complete.
However, if the LDP reed switch closes quickly,
there may be a leak or the fuel level may be low
enough that the LDP must pump more to finish pres-
surizing the EVAP system. In this case, the PCM will
rapidly pump the LDP again to build pressure in the
EVAP system, and follow that by monitoring the time
needed for several LDP test cycles. This process of
rapid pumping followed by several LDP test cycles
may repeat several times before the PCM judges that
a leak is present.
When leaks are present, the LDP test cycle time
will be inversely proportional to the size of the leak.
The larger the leak, the shorter the test cycle time.
The smaller the leak, the longer the test cycle time.
DTC's may be set when a leak as small as 0.5 mm
(0.0209) diameter is present.
If the system detects a leak, a temporary fault will
be stored in PCM memory. The time it takes to detect
a .020, .040, or Large leak is based on calibrations
that vary from model to model. The important point
to remember is if a leak is again detected on the next
EVAP Leak Detection Test, the MIL will illuminate
and a DTC will be stored based on the size of leak
detected. If no leak is detected during the next test,
the temporary fault will be cleared.
DIAGNOSTIC TIPS During diagnosis, you can
compare the LDP solenoid activity with the monitor
sequence in Figure 6. If the PCM detects a problem
that could set a DTC, the testing is halted and LDP
solenoid activity will stop. As each section of the test
begins, it indicates that the previous section passed
successfully. By watching to see which tests complete,
you can see if any conditions are present that the
PCM considers abnormal.
For example, if the LDP solenoid is energized for
the test cycles to test for blockage (P1486), it means
that the LDP has already passed its test for P1494.
Then, if the PCM detects a possible blockage, it will
25 - 34 EVAPORATIVE EMISSIONSWJ
LEAK DETECTION PUMP (Continued)

Check the vapor/vacuum lines at the LDP, LDP
filter and EVAP canister purge solenoid for
damage or leaks. If a leak is present, a Diagnos-
tic Trouble Code (DTC) may be set.
(2) Connect electrical connector to LDP.
(3) While raising front section of support bracket,
connect LDP wiring clip (Fig. 20).
(4) Install 3 LDP mounting bolts (Fig. 19). Refer to
Torque Specifications.
(5) Join front and rear sections of two-piece sup-
port bracket by installing 3 bolts on bottom of sup-
port bracket (Fig. 17). Do not tighten bolts at this
time.
(6) Install support bracket brace bolt (Fig. 17). Do
not tighten bolt at this time.
(7) Tighten 2 support bracket nuts at frame rail
(Fig. 19). Refer to Torque Specifications.
(8) Tighten 3 support bracket bolts and brace bolt.
Refer to Torque Specifications.
(9) Position stone shield behind left/rear wheel
(Fig. 18). Install new plastic rivets.
ORVR
DESCRIPTION
The ORVR (On-Board Refueling Vapor Recovery)
system consists of a unique fuel tank, flow manage-
ment valve, fluid control valve, one-way check valve
and vapor canister. Certain ORVR components can be
found in (Fig. 1).
OPERATION
The ORVR (On-Board Refueling Vapor Recovery)
system is used to remove excess fuel tank vapors.
This is done while the vehicle is being refueled. Cer-
tain ORVR components can be found in (Fig. 1).
Fuel flowing into the fuel filler tube (approx. 1º
I.D.) creates an aspiration effect drawing air into the
fuel fill tube. During refueling, the fuel tank is
vented to the EVAP canister to capture escaping
vapors. With air flowing into the filler tube, there are
no fuel vapors escaping to the atmosphere. Once the
refueling vapors are captured by the EVAP canister,
the vehicle's computer controlled purge system draws
vapor out of the canister for the engine to burn. The
vapor flow is metered by the purge solenoid so that
there is no, or minimal impact on driveability or
tailpipe emissions.As fuel starts to flow through the fuel fill tube, it
opens the normally closed check valve and enters the
fuel tank. Vapor or air is expelled from the tank
through the control valve and on to the vapor canis-
ter. Vapor is absorbed in the EVAP canister until
vapor flow in the lines stops. This stoppage occurs
following fuel shut-off, or by having the fuel level in
the tank rise high enough to close the control valve.
This control valve contains a float that rises to seal
the large diameter vent path to the EVAP canister.
At this point in the refueling process, fuel tank pres-
sure increases, the check valve closes (preventing liq-
uid fuel from spiting back at the operator), and fuel
then rises up the fuel filler tube to shut off the dis-
pensing nozzle.
PCV VALVE
DIAGNOSIS AND TESTING - PCV VALVE/PCV
SYSTEM - 4.7L
(1) Disconnect PCV line/hose (Fig. 21) by discon-
necting rubber connecting hose at PCV valve fitting.
(2) Remove PCV valve at oil filler tube by rotating
PCV valve downward until locating tabs have been
freed at cam lock (Fig. 21). After tabs have cleared,
pull valve straight out from filler tube.To prevent
damage to PCV valve locating tabs, valve must
be pointed downward for removal. Do not force
valve from oil filler tube.
(3) After valve is removed, check condition of valve
o-ring (Fig. 21). Also, PCV valve should rattle when
shaken.
(4) Reconnect PCV valve to its connecting line/
hose.
(5) Start engine and bring to idle speed.
(6) If valve is not plugged, a hissing noise will be
heard as air passes through valve. Also, a strong vac-
uum should be felt with a finger placed at valve
inlet.
(7) If vacuum is not felt at valve inlet, check line/
hose for kinks or for obstruction. If necessary, clean
out intake manifold fitting at rear of manifold. Do
this by turning a 1/4 inch drill (by hand) through the
fitting to dislodge any solid particles. Blow out the
fitting with shop air. If necessary, use a smaller drill
to avoid removing any metal from the fitting.
WJEVAPORATIVE EMISSIONS 25 - 37
LEAK DETECTION PUMP (Continued)

REMOVAL
The EVAP canister is located behind the left-rear
wheel (Fig. 24). It is attached to a two-piece support
bracket (Fig. 25).
(1) Remove rear bumper facia. Refer to Rear Facia
Removal / Installation in Frame & Bumpers section.
(2) Remove 1 support bracket brace bolt (Fig. 25).
(3) Loosen, but do not remove 2 support bracket
nuts (Fig. 26).
(4) Remove upper/rear support bracket mounting
bolt (Fig. 27).
(5) Carefully lower support bracket assembly to
gain access to vapor / vacuum lines. To prevent dam-
age to lines, suspend bracket assembly with rope or
string.
(6) Disconnect necessary vacuum / vapor lines at
EVAP canister.
(7) Remove EVAP canister mounting bolt (Fig. 28).
(8) Lift canister from support bracket (2 pins are
used to align canister into support bracket)
INSTALLATION
The EVAP canister is located behind the left-rear
wheel (Fig. 24). It is attached to a two-piece support
bracket (Fig. 25).
(1) Position canister to support bracket. Guide 2
alignment pins into support bracket.
(2) Install EVAP canister mounting bolt (Fig. 28).
Refer to Torque Specifications.
(3) Carefully install vapor / vacuum lines to canis-
ter.The vapor/vacuum lines and hoses must be
firmly connected. Check the vapor/vacuum
lines at the LDP, LDP filter and EVAP canister
purge solenoid for damage or leaks. If a leak is
present, a Diagnostic Trouble Code (DTC) may
be set.
Fig. 24 LOCATION, LDP / EVAP CANISTER
1 - LEAK DETECTION PUMP
2 - EVAP CANISTER
Fig. 25 TWO-PIECE SUPPORT BRACKET
1 - TWO-PIECE SUPPORT BRACKET (FRONT)
2 - SUPPORT BRACKET BRACE
3 - TWO-PIECE SUPPORT BRACKET (REAR)
4 - SUPPORT BRACKET ATTACHING BOLTS (3)
5 - SUPPORT BRACKET BRACE BOLT
25 - 40 EVAPORATIVE EMISSIONSWJ
VAPOR CANISTER (Continued)