Lexus ES300 (2002 year). Manual — part 367
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DIAGNOSTICS
SFI SYSTEM (1MZ-FE)
05-87
240
2002 LEXUS ES300 REPAIR MANUAL (RM911U)
4
CHECK OXYGEN NO.2 SENSOR (BANK1, 2 SENSOR2) (See page
)
NG
REPAIR OR REPLACE OXYGEN NO.2 SENSOR
OK
REPLACE EXHAUST PIPE ASSY CENTER
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
Fig. 1
VSV for
CCV
VSV
for EVAP
ECM
Vapor Pressure
Sensor
Fuel Tank Over
Fill Check Valve
Fuel Tank
Charcoal Canister
VSV for
Pressure
Switching
Valve
A10140
05-88
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DIAGNOSTICS
SFI SYSTEM (1MZ-FE)
241
DTC
P0440
EVAPORATIVE EMISSION CONTROL
SYSTEM MALFUNCTION
DTC
P0442
EVAPORATIVE EMISSION CONTROL
SYSTEM LEAK DETECTED (SMALL LEAK)
CIRCUIT DESCRIPTION
The vapor pressure sensor,
VSV for canister closed valve (CCV)
and VSV for pressure switching valve are
used to detect abnormalities in the evaporative emission control system.
The ECM decides whether there is an abnormality in the evaporative emission control system based on the
vapor pressure sensor signal.
DTC P0440 or P0442 is recorded by the ECM when evaporative emissions leak from the components within
the dotted line in Fig. 1 below, or when the vapor pressure sensor malfunctions.
0560K-04
A14661
VSV for CCV
VSV for
Pressure Switching Valve
VSV for EVAP
Cold Start
ECT/IAT near same temp.
Negative
Pressure
Occurs
Tank & Canister
Leak Check
VSV for Pressure
Switching Valve, CCV
Testing
Open
Closed
Open
Closed
Open
Closed
Closed
Closed
Open
Open
P0441
P0440, P0442
P0446
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DIAGNOSTICS
SFI SYSTEM (1MZ-FE)
05-89
242
After purge operation, the VSV for EVAP is turned off sealing the vacuum in the system and the ECM begins
to monitor the pressur increase. Some increase in normal. A very rapid, sharp increase in pressure indicates
a leak in the EVAP system and sets the DTC P0440.
A pressure rise just above normal indecates a very small hole and will set the DTC P0442.
DTC No.
DTC Detecting Condition
Trouble Area
P0440
P0442
After cold starting and when generating certain swift pressure
value in fuel tank enabling not to hold that value (2 trip detec-
tion logic)
Hose or tube cracked, hole, damaged or loose seal ((3) in
Fig. 1)
Fuel tank cap incorrectly installed
Fuel tank cap cracked or damaged
Vacuum hose cracked, holed, blocked, damaged or discon-
nected ((1) or (2) in Fig. 1)
Fuel tank cracked, holed or damaged
Charcoal canister cracked, holed or damaged
Open or short in vapor pressure sensor circuit
VSV for CCV
VSV for EVAP
VSV for pressure seitching valve
Vapor pressure sensor
Fuel tank over fill check valve cracked or damaged
ECM
A62013
18
Vapor Pressure Sensor
LG
CCV
EVP1
E2
PTNK
ECM
TBP
E10
MREL
VC
E6
IA3
8
4
BR
P
ID1
B-W
Y
From
Battery
VSV for EVAP
1A
E.F.I.
Driver
Side J/B
2G
B-W
L
IL2
E10
E8
E6
E8
E6
21
28
11
12
IL2
IA3
Y
Y
P
BR
BR
1
2
3
B-W
1
2
2
1
VSV for CCV
ID1
4
6
2
9
10
1
V
V
1
2
VSV for Pressure
Switching Valve
B-R
B-R
2K
5
17
B-W
W-B
E.F.I.
ECU Relay
ED
Engine Room J/B
1C
1B
1C
1K
5
3
2
1
6
4
3
2
5
BR-Y
A53796
05-90
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DIAGNOSTICS
SFI SYSTEM (1MZ-FE)
243
WIRING DIAGRAM
CONFIRMATION READINESS TEST
1.
First Trip Procedure
(a)
Vehicle must be cold, ambient temperature approximate-
ly between 50
°
F - 95
°
F.
(b)
Intake Air Temp. (IAT) and Engine Coolant Temp. (ECT)
sensor almost same value.
(c)
Clear DTC’s.
Disconnecting the battery terminals or EFI fuse.
Readiness tests will show INCMPL (incomplete).
(d)
Drive the vehicle according to LA#4 drive cycle. Note the
state of Readiness Tests. They will change to COMPL as
the evaluation monitors operate and if the system passes.
This procedure may take approximately 20 minutes or
more.
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