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![INFINITI FX35 2008 Service Manual
ON BOARD REFUELING VAPOR RECOVERY (ORVR)EC-49
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With CONSULT-III
1. Remove fuel tank. Refer to
FL-10.
2. Drain fuel from the tank as f INFINITI FX35 2008 Service Manual
ON BOARD REFUELING VAPOR RECOVERY (ORVR)EC-49
< SERVICE INFORMATION > [VQ35DE]
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With CONSULT-III
1. Remove fuel tank. Refer to
FL-10.
2. Drain fuel from the tank as f](/manual-img/42/57017/w960_57017-1288.png)
ON BOARD REFUELING VAPOR RECOVERY (ORVR)EC-49
< SERVICE INFORMATION > [VQ35DE]
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With CONSULT-III
1. Remove fuel tank. Refer to
FL-10.
2. Drain fuel from the tank as follows:
a. Remove fuel feed hose located on the fuel gauge retainer.
b. Connect a spare fuel hose, one side to fuel gauge retainer where the hose was removed and the other side to a fuel container.
c. Drain fuel using “FUEL PUMP RELAY” in “ACTIVE TEST” mode with CONSULT-III.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows. Blow air into the refueling EVAP vapor cut valv e (from the end of EVAP/ORVR line hose), and check that
the air flows freely into the tank.
4. Check refueling EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose end.
b. Remove fuel gauge retainer with fuel gauge unit. Always replace O-ring with new one.
c. Put fuel tank upside down.
d. Apply vacuum pressure to hose end [ −13.3 kPa ( −100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
Without CONSULT-III
1. Remove fuel tank. Refer to FL-10.
2. Drain fuel from the tank as follows:
a. Remove fuel gauge retainer.
b. Drain fuel from the tank using a handy pump into a fuel container.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows. Blow air into the refueling EVAP vapor cut valv e (from the end of EVAP/ORVR line hose), and check that
the air flows freely into the tank.
4. Check refueling EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose end.
b. Remove fuel gauge retainer with fuel gauge unit. Always replace O-ring with new one.
c. Put fuel tank upside down.
PBIB1035E
3AA93ABC3ACD3AC03ACA3AC03AC63AC53A913A773A893A873A873A8E3A773A983AC73AC93AC03AC3
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EC-50
< SERVICE INFORMATION >[VQ35DE]
ON BOARD REFUELING VAPOR RECOVERY (ORVR)
d. Apply vacuum pressure to hose end [
−13.3 kPa ( −100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
PBIB1035E
3AA93ABC3ACD3AC03ACA3AC03AC63AC53A913A773A893A873A873A8E3A773A983AC73AC93AC03AC3
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![INFINITI FX35 2008 Service Manual
POSITIVE CRANKCASE VENTILATIONEC-51
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POSITIVE CRANKCASE VENTILATION
DescriptionINFOID:0000000001325911
SYSTEM DESCRIPTION
This system r INFINITI FX35 2008 Service Manual
POSITIVE CRANKCASE VENTILATIONEC-51
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POSITIVE CRANKCASE VENTILATION
DescriptionINFOID:0000000001325911
SYSTEM DESCRIPTION
This system r](/manual-img/42/57017/w960_57017-1290.png)
POSITIVE CRANKCASE VENTILATIONEC-51
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POSITIVE CRANKCASE VENTILATION
DescriptionINFOID:0000000001325911
SYSTEM DESCRIPTION
This system returns blow-by gas to the intake manifold.
The positive crankcase ventilation (PCV) valve is prov
ided to conduct crankcase blow-by gas to the intake
manifold. During partial throttle operation of the engine, the intake manifold sucks the blow-by gas through the
PCV valve. Normally, the capacity of the valve is su fficient to handle any blow-by and a small amount of venti-
lating air. The ventilating air is then drawn from the air inlet tubes into the crankcase. In this process the air
passes through the hose connecting air inlet tubes to rocker cover. Under full-throttle condition, the manifold
vacuum is insufficient to draw the blow-by flow through the valve. The flow goes through the hose connection
in the reverse direction.
On vehicles with an excessively high blow-by, the valve does not
meetthe requirement. This is because some of the flow will go
through the hoseconnection to the air inlet tubes under all condi-
tions.
Component InspectionINFOID:0000000001325912
PCV (POSITIVE CRANKCASE VENTILATION) VALVE
With engine running at idle, remove PCV valve from rocker cover. A
properly working valve makes a hissing noise as air passes through
it. A strong vacuum should be felt immediately when a finger is
placed over valve inlet.
SEC921C
PBIB1588E
PBIB1589E
3AA93ABC3ACD3AC03ACA3AC03AC63AC53A913A773A893A873A873A8E3A773A983AC73AC93AC03AC3
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EC-52
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POSITIVE CRANKCASE VENTILATION
PCV VALVE VENTILATION HOSE
1. Check hoses and hose connections for leaks.
2. Disconnect all hoses and clean with compressed air. If any
hosecannot be freed of obstructions, replace.
S-ET277
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![INFINITI FX35 2008 Service Manual
IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
EC-53
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IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
DescriptionINFOID:00000000013259 INFINITI FX35 2008 Service Manual
IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
EC-53
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IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
DescriptionINFOID:00000000013259](/manual-img/42/57017/w960_57017-1292.png)
IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
EC-53
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IVIS (INFINITI VEHICLE IMMOBILIZER SYSTEM-NATS)
DescriptionINFOID:0000000001325913
If the security indicator lights up with the ignition switch in the ON position or “NATS MALFUNC-
TION” is displayed on “SELF-DIAG RESULTS” screen, perform self-diagnostic results mode with
CONSULT-III using NATS program card. Refer to BL-185
.
Confirm no self-diagnostic results of IVIS (NATS) is displayed before touching “ERASE” in “SELF-
DIAG RESULTS” mode with CONSULT-III.
When replacing ECM, initialization of IVIS (NATS) system and registration of all IVIS (NATS) ignition
key IDs must be carried out with CO NSULT-III using NATS program card.
Therefore, be sure to receive all keys from vehicle owner. Regarding the procedures of IVIS (NATS)
initialization and all IVIS (NATS) ignition key ID registration, refe r to CONSULT-III Operation Manual,
IVIS/NVIS.
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EC-54
< SERVICE INFORMATION >[VQ35DE]
ON BOARD DIAGNOSTIC (OBD) SYSTEM
ON BOARD DIAGNO
STIC (OBD) SYSTEM
IntroductionINFOID:0000000001325914
The ECM has an on board diagnostic system, which detects INFINITI FX35 2008 Service Manual
EC-54
< SERVICE INFORMATION >[VQ35DE]
ON BOARD DIAGNOSTIC (OBD) SYSTEM
ON BOARD DIAGNO
STIC (OBD) SYSTEM
IntroductionINFOID:0000000001325914
The ECM has an on board diagnostic system, which detects](/manual-img/42/57017/w960_57017-1293.png)
EC-54
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ON BOARD DIAGNOSTIC (OBD) SYSTEM
ON BOARD DIAGNO
STIC (OBD) SYSTEM
IntroductionINFOID:0000000001325914
The ECM has an on board diagnostic system, which detects malfunctions related to engine sensors or actua-
tors. The ECM also records various emission-related diagnostic information including:
The above information can be checked usi ng procedures listed in the table below.
×: Applicable —: Not applicable
*: When DTC and 1st trip DTC simultaneously appear on the display, they cannot be clearly distinguished from each other.
The malfunction indicator lamp (MIL) on the instrument panel lights up when the same malfunction is detected
in two consecutive trips (Two trip detection logic) , or when the ECM enters fail-safe mode. (Refer to EC-95,
"Fail-Safe Chart".)
Two Trip Detection LogicINFOID:0000000001325915
When a malfunction is detected for the 1st time, 1st trip DTC and 1st trip Freeze Frame data are stored in the
ECM memory. The MIL will not light up at this stage. <1st trip>
If the same malfunction is detected again during the next drive, the DTC and Freeze Frame data are stored in
the ECM memory, and the MIL lights up. The MIL lights up at the same time when the DTC is stored. <2nd
trip> The “trip” in the “Two Trip Detection Logic” m eans a driving mode in which self-diagnosis is performed
during vehicle operation. Specific on board diagnostic item s will cause the ECM to light up or blink the MIL,
and store DTC and Freeze Frame data, even in the 1st trip, as shown below.
× : Applicable —: Not applicable
When there is an open circuit on MIL circuit, the ECM c annot warn the driver by lighting up MIL when there is
malfunction on engine control system.
Emission-related diagnostic information Diagnostic service
Diagnostic Trouble Code (DTC) Service $03 of SAE J1979
Freeze Frame data Service $02 of SAE J1979
System Readiness Test (SRT) code Service $01 of SAE J1979
1st Trip Diagnostic Trouble Code (1st Trip DTC) Service $07 of SAE J1979
1st Trip Freeze Frame data
Test values and Test limits Service $06 of SAE J1979
Calibration ID Service $09 of SAE J1979
DTC 1st trip DTC Freeze
Frame data 1st trip Freeze
Frame data SRT code SRT status Test value
CONSULT-III ×× × × × × —
GST ×× × —×××
ECM ××*— — — ×—
Items MIL DTC 1st trip DTC
1st trip 2nd trip 1st trip
displaying 2nd trip
displaying 1st trip
displaying 2nd trip
display- ing
Blinking Lighting
up Blinking Lighting
up
Misfire (Possible three way catalyst
damage) — DTC: P0300 - P0306 is
being detected ×
———— — ×—
Misfire (Possible three way catalyst
damage) — DTC: P0300 - P0306 is
being detected ——
×—— ×——
One trip detection diagnoses (Re-
fer to EC-55, "
Emission-Related Di-
agnostic Information".) —
×—— ×———
Except above — — — ×— ×× —
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ON BOARD DIAGNOSTIC (OBD) SYSTEMEC-55
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Therefore, when electrical controlled throttle and part
of ECM related diagnoses are continuous INFINITI FX35 2008 Service Manual
ON BOARD DIAGNOSTIC (OBD) SYSTEMEC-55
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Therefore, when electrical controlled throttle and part
of ECM related diagnoses are continuous](/manual-img/42/57017/w960_57017-1294.png)
ON BOARD DIAGNOSTIC (OBD) SYSTEMEC-55
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Therefore, when electrical controlled throttle and part
of ECM related diagnoses are continuously detected as
NG for 5 trips, ECM warns the driver that engine c ontrol system malfunctions and MIL circuit is open by means
of operating fail-safe function.
The fail-safe function also operates when above diagnos es except MIL circuit are detected and demands the
driver to repair the malfunction.
Emission-Related Diagnostic InformationINFOID:0000000001325916
EMISSION-RELATED DIAGNOSTIC INFORMATION ITEMS
× : Applicable —: Not applicable
Engine operating condition in fail-safe mode Engine speed will not rise more than 2,500 rpm due to the fuel cut
Items
(CONSULT-III screen terms) DTC*
1
SRT code Trip MIL
Reference
page
CONSULT-III
GST*
2ECM*3
CAN COMM CIRCUIT U1000 1000*5—1×EC-146
CAN COMM CIRCUIT U1001
1001*5—2
(Models with ASCD) —EC-1461 or 2
(Models with
ICC)
CONTROL UNIT(CAN) U1010 1010 — 1 ×EC-148
NO DTC IS DETECTED.
FURTHER TESTING
MAY BE REQUIRED. P0000 0000
——
Flashing*8—
INT/V TIM CONT-B1 P0011 0011 — 2 ×EC-149
INT/V TIM CONT-B2 P0021 0021 — 2 ×EC-149
A/F SEN1 HTR (B1) P0031 0031 — 2 ×EC-153
A/F SEN1 HTR (B1) P0032 0032 — 2 ×EC-153
HO2S2 HTR (B1) P0037 0037 — 2 ×EC-160
HO2S2 HTR (B1) P0038 0038 — 2 ×EC-160
A/F SEN1 HTR (B2) P0051 0051 — 2 ×EC-153
A/F SEN1 HTR (B2) P0052 0052 — 2 ×EC-153
HO2S2 HTR (B2) P0057 0057 — 2 ×EC-160
HO2S2 HTR (B2) P0058 0058 — 2 ×EC-160
INT/V TIM V/CIR-B1 P0075 0075 — 2 ×EC-168
INT/V TIM V/CIR-B2 P0081 0081 — 2 ×EC-168
MAF SEN/CIRCUIT-B1 P0101 0101 — 2 ×EC-175
MAF SEN/CIRCUIT-B1 P0102 0102 — 1 ×EC-182
MAF SEN/CIRCUIT-B1 P0103 0103 — 1 ×EC-182
IAT SEN/CIRCUIT-B1 P0112 0112 — 2 ×EC-189
IAT SEN/CIRCUIT-B1 P0113 0113 — 2 ×EC-189
ECT SEN/CIRC P0117 0117 — 1 ×EC-193
ECT SEN/CIRC P0118 0118 — 1 ×EC-193
TP SEN 2/CIRC-B1 P0122 0122 — 1 ×EC-198
TP SEN 2/CIRC-B1 P0123 0123 — 1 ×EC-198
ECT SENSOR P0125 0125 — 2 ×EC-204
IAT SENSOR-B1 P0127 0127 — 2 ×EC-207
THERMSTAT FNCTN P0128 0128 — 2 ×EC-210
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![INFINITI FX35 2008 Service Manual
EC-56
< SERVICE INFORMATION >[VQ35DE]
ON BOARD DIAGNOSTIC (OBD) SYSTEM
A/F SENSOR1 (B1) P0130 0130 — 2
×EC-212
A/F SENSOR1 (B1) P0131 0131 — 2 ×EC-220
A/F SENSOR1 (B1) P0132 0132 — 2 ×EC-228 INFINITI FX35 2008 Service Manual
EC-56
< SERVICE INFORMATION >[VQ35DE]
ON BOARD DIAGNOSTIC (OBD) SYSTEM
A/F SENSOR1 (B1) P0130 0130 — 2
×EC-212
A/F SENSOR1 (B1) P0131 0131 — 2 ×EC-220
A/F SENSOR1 (B1) P0132 0132 — 2 ×EC-228](/manual-img/42/57017/w960_57017-1295.png)
EC-56
< SERVICE INFORMATION >[VQ35DE]
ON BOARD DIAGNOSTIC (OBD) SYSTEM
A/F SENSOR1 (B1) P0130 0130 — 2
×EC-212
A/F SENSOR1 (B1) P0131 0131 — 2 ×EC-220
A/F SENSOR1 (B1) P0132 0132 — 2 ×EC-228
A/F SENSOR1 (B1) P0133 0133 ×2 ×EC-236
HO2S2 (B1) P0137 0137 ×2 ×EC-245
HO2S2 (B1) P0138 0138 ×2 ×EC-254
HO2S2 (B1) P0139 0139 ×2 ×EC-265
A/F SENSOR1 (B2) P0150 0150 — 2 ×EC-212
A/F SENSOR1 (B2) P0151 0151 — 2 ×EC-220
A/F SENSOR1 (B2) P0152 0152 — 2 ×EC-228
A/F SENSOR1 (B2) P0153 0153 ×2 ×EC-236
HO2S2 (B2) P0157 0157 ×2 ×EC-245
HO2S2 (B2) P0158 0158 ×2 ×EC-254
HO2S2 (B2) P0159 0159 ×2 ×EC-265
FUEL SYS-LEAN-B1 P0171 0171 — 2 ×EC-274
FUEL SYS-RICH-B1 P0172 0172 — 2 ×EC-284
FUEL SYS-LEAN-B2 P0174 0174 — 2 ×EC-274
FUEL SYS-RICH-B2 P0175 0175 — 2 ×EC-284
FTT SENSOR P0181 0181 — 2 ×EC-294
FTT SEN/CIRCUIT P0182 0182 — 2 ×EC-298
FTT SEN/CIRCUIT P0183 0183 — 2 ×EC-298
TP SEN 1/CIRC-B1 P0222 0222 — 1 ×EC-302
TP SEN 1/CIRC-B1 P0223 0223 — 1 ×EC-302
MULTI CYL MISFIRE P0300 0300 — 2 ×EC-308
CYL 1 MISFIRE P0301 0301 — 2 ×EC-308
CYL 2 MISFIRE P0302 0302 — 2 ×EC-308
CYL 3 MISFIRE P0303 0303 — 2 ×EC-308
CYL 4 MISFIRE P0304 0304 — 2 ×EC-308
CYL 5 MISFIRE P0305 0305 — 2 ×EC-308
CYL 6 MISFIRE P0306 0306 — 2 ×EC-308
KNOCK SEN/CIRC-B1 P0327 0327 — 2 — EC-315
KNOCK SEN/CIRC-B1 P0328 0328 — 2 —EC-315
CKP SEN/CIRCUIT P0335 0335 — 2×EC-319
CMP SEN/CIRC-B1 P0340 0340 — 2 ×EC-324
CMP SEN/CIRC-B2 P0345 0345 — 2 ×EC-324
TW CATALYST SYS-B1 P0420 0420 ×2 ×EC-332
TW CATALYST SYS-B2 P0430 0430 ×2 ×EC-332
EVAP PURG FLOW/MON P0441 0441 ×2 ×EC-336
EVAP SMALL LEAK P0442 0442 ×2 ×EC-341
PURG VOLUME CONT/V P0443 0443 — 2 ×EC-348
PURG VOLUME CONT/V P0444 0444 — 2 ×EC-355
PURG VOLUME CONT/V P0445 0445 — 2 ×EC-355
Items
(CONSULT-III screen terms) DTC*
1
SRT code Trip MIL
Reference
page
CONSULT-III
GST*
2ECM*3
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