MIL & Data Link Connectors ...................................535
SERVICE DATA AND SPECIFICATIONS (SDS) ........536
General Specifications.............................................536
Inspection and Adjustment ......................................536
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When you read wiring diagrams:
I Read GI section, “HOW TO READ WIRING DIAGRAMS”.
I See EL section, “POWER SUPPLY ROUTING” for power distribution circuit.
When you perform trouble diagnoses, read GI section, “HOW TO FOLLOW FLOW CHART IN
TROUBLE DIAGNOSES” and “HOW TO PERFORM EFFICIENT DIAGNOSIS FOR AN ELECTRICAL
INCIDENT”.
*1: In Diagnostic Test Mode II (Self-diagnostic results). These
numbers are controlled by NISSAN.
*2: These numbers are prescribed by SAE J2012.
*3: When the fail-safe operation occurs, the MIL illuminates.
*4: The MIL illuminates when both the “Revolution sensor sig-
nal” and the “Vehicle speed sensor signal” meet the failsafe condition at the same time.
*5: While engine is running.
*6: 1st trip DTC No. is the same as DTC No.
NOTE: Regarding Y33 models, “-B1” and “BK1” indicates left
bank and “-B2” and “BK2” indicates right bank.
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EC-7
PRECAUTIONS AND PREPARATION
Special Service Tool
The actual shapes of Kent-Moore tools may differ from those of special service tools illustrated here.
Tool number
(Kent-Moore No.)
Tool name
(J38365-A)
Heated oxygen sensor
wrench
Description
Loosening or tightening heated oxygen sensor
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Tool name
(Kent-Moore No.)
Leak detector
(J41416)
EVAP service port adapter
(J41413-OBD)
Hose clipper
NT636
Description
NT703
NT704
3/8 drive
a: 22 mm (0.87 in)
Commercial Service Tools
Locating the EVAP leak
Applying positive pressure through EVAP service port
Clamping the EVAP purge hose between the
fuel tank and EVAP canister applied to DTC
P1440 [(EVAP small leak positive pressure)].
Fuel filler cap adapter
Socket wrench
NT720
Checking fuel tank vacuum relief valve opening pressure
NT653
Removing and installing engine coolant temperature sensor
Anti-seize lubricant
(Permatex
equivalent meeting MIL
specification MIL-A-907)
TM
133AR or
Description
NT778
NT779
Reconditioning the exhaust system threads
before installing a new oxygen sensor. Use
with anti-seize lubricant shown below.
a: J-43897-18 18 mm dia. for Zirconia Oxygen
Sensor
b: J-43897-12 12 mm dia. for Titania Oxygen
Sensor
Lubricating oxygen sensor thread cleaning
tool when reconditioning exhaust system
threads.
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EC-9
PRECAUTIONS AND PREPARATION
Supplemental Restraint System (SRS) “AIR
BAG” and “SEAT BELT PRE-TENSIONER”
The Supplemental Restraint System such as “AIR BAG” and “SEAT BELT PRE-TENSIONER” used along with
a seat belt, helps to reduce the risk or severity of injury to the driver and front passenger for certain types of
collision. The SRS system composition which is available to INFINITI Q45 is as follows:
IFor a frontal collision
The Supplemental Restraint System consists of driver air bag module (located in the center of the steering wheel), front passenger air bag module (located on the instrument panel on passenger side), seat belt
pre-tensioners, a diagnosis sensor unit, warning lamp, wiring harness and spiral cable.
IFor a side collision
The Supplemental Restraint System consists of front side air bag module (located in the outer side of front
seat), satellite sensor, diagnosis sensor unit (one of components of air bags for a frontal collision), wiring
harness, warning lamp (one of components of air bags for a frontal collision).
Information necessary to service the system safely is included in the RS section of this Service Manual.
WARNING:
ITo avoid rendering the SRS inoperative, which could increase the risk of personal injury or death
in the event of a collision which would result in air bag inflation, all maintenance should be performed by an authorized INFINITI dealer.
IImproper maintenance, including incorrect removal and installation of the SRS, can lead to per-
sonal injury caused by intentional activation of the system. For removal of Spiral Cable and Air Bag
Module, see the RS section.
IDo not use electrical test equipment on any circuit related to the SRS unless instructed to in this
Service Manual. Spiral cable and wiring harnesses (except satellite sensor and side air bag module) covered with yellow insulation tape either just before the harness connectors or for the complete harness are related to the SRS.
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Precautions for On Board Diagnostic (OBD)
System of Engine and A/T
The ECM has an on board diagnostic system. It will light up the malfunction indicator lamp (MIL) to warn the
driver of a malfunction causing emission deterioration.
CAUTION:
IBe sure to turn the ignition switch “OFF” and disconnect the negative battery terminal before the
repair or inspection work. The open/short circuit of the related switches, sensors, solenoid valves,
etc. will cause the MIL to light up.
IBe sure to connect and lock the connectors securely after the work. The loose (unlocked) connec-
tor will cause the MIL to light up due to the open circuit. (Be sure to connect the connector without water, grease, dirt, bent terminals, etc. in it.)
ICertain systems and components, especially those related to OBD, may use a new style slide-
locking type harness connector. For description and how to disconnect, refer to EL section,
“Description”, “HARNESS CONNECTOR”.
IBe sure to route and clamp the harnesses properly after work. The interference of the harness with
a bracket, etc. may cause the MIL to light up due to the short circuit.
IBe sure to connect rubber tubes properly after the work. The misconnected or disconnected rub-
ber tube may cause the MIL to light up due to the malfunction of the EGR system or the fuel injection system, etc.
IBe sure to erase the unnecessary (already fixed) malfunction information in the ECM and TCM
(Transmission Control Module) before returning the vehicle to the customer.
EC-10
PRECAUTIONS AND PREPARATION
Engine Fuel & Emission Control System
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EC-11
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SEF345WA
PRECAUTIONS AND PREPARATION
Precautions
IBefore connecting or disconnecting the ECM harness
connector, turn ignition switch OFF and disconnect negative battery terminal. Failure to do so may damage the
ECM. Because battery voltage is applied to ECM even if
ignition switch is turned off.
ing bolt until the gap between the orange indicators disappears.
:3-5N⋅m (0.3 - 0.5 kg-m, 26 - 43 in-lb)
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SEF308Q
IWhen connecting or disconnecting pin connectors into or
from ECM, take care not to damage pin terminals (bend or
break).
Make sure that there are not any bends or breaks on ECM
pin terminal, when connecting pin connectors.
SEF291H
IBefore replacing ECM, perform ECM input/output signal
inspection and make sure whether ECM functions properly or not. (See page EC-107.)
MEF040D
SEF217U
IAfter performing each TROUBLE DIAGNOSIS, perform
“OVERALL FUNCTION CHECK” or “DTC (Diagnostic
Trouble Code) CONFIRMATION PROCEDURE”.
The DTC should not be displayed in the “DTC CONFIRMATION PROCEDURE” if the repair is completed. The
“OVERALL FUNCTION CHECK” should be a good result if
the repair is completed.
EC-12
PRECAUTIONS AND PREPARATION
Precautions (Cont’d)
IWhen measuring ECM signals with a circuit tester, never
bring the two tester probes into contact.
Accidental contact of probes will cause a short circuit and
damage the ECM power transistor.
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SEF348N
SEF202UA
IRegarding model Y33, “-B1” indicates the left bank and
“-B2” indicates the right bank as shown in the figure.
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EC-13
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ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Circuit Diagram
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TEC038M
EC-14
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Circuit Diagram (Cont’d)
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EC-15
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TEC039M
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
System Diagram
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SEF815XA
EC-16
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location
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EC-17
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SEF347W
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location
(Cont’d)
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SEF348W
SEF554T
SEF037T
SEF038TA
SEF392WA
SEF386X
SEF039T
SEF349W
EC-18
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Vacuum Hose Drawing
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q
1 Intake air duct to vacuum gallery A
q
2 Fuel pressure regulator to vacuum gallery B
q
3 Vacuum gallery A to EGRC-solenoid valve, MAP/BARO
switch solenoid valve and EVAP canister purge control
solenoid valve
q
4 Intake manifold collector to EGRC-solenoid valve
q
5 EVAP canister purge control valve to EVAP canister purge
control solenoid valve
Refer to “System Diagram”, EC-16, for vacuum control system.
SEF208U
q
6 Intake manifold collector to One-way valve
q
7 One-way valve to EVAP canister purge control solenoid
valve
q
8 EGRC-BPT valve to EGRC-solenoid valve
q
9 Intake manifold collector to MAP/BARO switch solenoid
valve
q
10
Absolute pressure sensor to MAP/BARO switch solenoid
valve
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Note: Do not use soapy water or any type of solvent while installing vacuum hoses or purge hoses.
EC-19
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ENGINE AND EMISSION CONTROL OVERALL SYSTEM
System Chart
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Camshaft position sensor
Mass air flow sensor
Engine coolant temperature sensor
Front heated oxygen sensors
Ignition switch
Throttle position sensor
*4
Closed throttle position switch
Park/Neutral position (PNP) switch (TCM)
Vehicle speed sensor
Air conditioner switch
Knock sensor
Battery voltage
Electrical load
E
Fuel injection &
E
E
E
E
E
E
E
E
E
E
ECM
E
E
mixture ratio control
Electronic ignition system
Idle air control system
Intake valve timing control
EGR control
Fuel pump control
Front heated oxygen sensor
monitor & on board diagnostic
system
Acceleration cut control
Injectors
E
Power transistor
E
IACV-AAC valve
E
Intake valve timing control
E
solenoid valve
EGRC-solenoid valve
E
Fuel pump relay and
E
Fuel pump control module
Malfunction indicator lamp
E
(On the instrument panel)
Air conditioner relay
E
Intake air temperature sensor
*1
I EGR temperature sensor
I Crankshaft position sensor (OBD)
I Intake valve timing control position sensor
I Absolute pressure sensor
I EVAP control system pressure sensor
I Fuel tank temperature sensor
Rear heated oxygen sensors*3
TCM (Transmission Control Module)*2
Power steering oil pressure switch
Secondary throttle position sensor
TCS signal
E
TAC
module
E
E
E
E
E
E
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EVAP canister purge flow control
Front & Rear heated oxygen
sensors heater control
Cooling fan control
*1: These sensors are not used to control the engine system. They are used only for the on board diagnosis.
*2: The DTC related to A/T and gear position will be sent to ECM.
*3: This sensor is not used to control the engine system under normal conditions.
*4: This switch will operate in place of the throttle position sensor to control EVAP parts if the sensor malfunctions.
I EVAP canister purge volume
control valve
E
I EVAP canister purge control
solenoid valve
Front & Rear heated oxygen
E
sensor heaters
Cooling fan relay
E
I EVAP canister vent control
valve
I Vacuum cut valve bypass
valve
E
I MAP/BARO switch solenoid
valve
EC-20
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
INPUT/OUTPUT SIGNAL LINE
Camshaft position sensor
Mass air flow sensor
Engine coolant temperature sensor
Front heated oxygen sensor
Throttle position sensor
Multiport Fuel Injection (MFI) System
Engine speed and piston position
E
Amount of intake air
E
Engine coolant temperature
E
Density of oxygen in exhaust gas
E
Throttle position
E
Throttle valve idle position
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PNP switch (TCM)
Vehicle speed sensor
Ignition switch
Battery
Rear heated oxygen sensor*
Secondary throttle position
sensor
*: Under normal conditions, this sensor is not used to control the engine system.
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TAC
module
Park/Neutral position
Vehicle speed
Start signal
Battery voltage
Density of oxygen in exhaust gas
Secondary throttle valve opening angle
BASIC MULTIPORT FUEL INJECTION
SYSTEM
The amount of fuel injected from the fuel injector is
determined by the ECM. The ECM controls the
length of time the valve remains open (injection
pulse duration). The amount of fuel injected is a
program value in the ECM memory. The program
value is preset by engine operating conditions.
These conditions are determined by input signals
(for engine speed and intake air) from both the camshaft position sensor and the mass air flow sensor.
ECM
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Injector
VARIOUS FUEL INJECTION
INCREASE/DECREASE COMPENSATION
The amount of fuel injected is compensated for to
improve engine performance. This will be made
under various operating conditions as listed below.
<Fuel increase>
IDuring warm-up
IWhen starting the engine
IDuring acceleration
IHot-engine operation
IWhen selector lever is changed from “N” to “D”
IHigh-load, high-speed operation
<Fuel decrease>
IDuring deceleration
IDuring high speed operation
IExtremely high engine coolant temperature
IDuring TCS operation
IDuring high engine speed operation
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EC-21
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Multiport Fuel Injection (MFI) System (Cont’d)
MIXTURE RATIO FEEDBACK CONTROL
The mixture ratio feedback system provides the best air-fuel mixture ratio for driveability and emission control. The three way catalyst can then better reduce CO, HC and NOx emissions. This system uses a front heated oxygen sensor in the exhaust manifold to
monitor if the engine is rich or lean. The ECM adjusts the injection
pulse width according to the sensor voltage signal. For more information about front heated oxygen sensor, refer to pages EC-166.
This maintains the mixture ratio within the range of stoichiometric
(ideal air-fuel mixture).
MEF025DH
This stage is referred to as the closed loop control condition.
Rear heated oxygen sensor is located downstream of the three
way catalyst. Even if the switching characteristics of the front
heated oxygen sensor shift, the air-fuel ratio is controlled to stoichiometric by the signal from the rear heated oxygen sensor.
OPEN LOOP CONTROL
The open loop system condition refers to when the ECM detects
any of the following conditions. Feedback control stops in order to
maintain stabilized fuel combustion.
IDeceleration and acceleration
IHigh-load, high-speed operation
IMalfunction of front heated oxygen sensor or its circuit
IInsufficient activation of front heated oxygen sensor at low
engine coolant temperature
IHigh-engine coolant temperature
IDuring warm-up
IWhen starting the engine
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MIXTURE RATIO SELF-LEARNING CONTROL
The mixture ratio feedback control system monitors the mixture
ratio signal transmitted from the front heated oxygen sensor. This
feedback signal is then sent to the ECM. The ECM controls the
basic mixture ratio as close to the theoretical mixture ratio as possible. However, the basic mixture ratio is not necessarily controlled
as originally designed. Both Manufacturing differences (i.e. mass
air flow sensor hot film) and characteristic changes during operation (i.e. injector clogging) directly affect mixture ratio.
Accordingly, the difference between the basic and theoretical mixture ratios is monitored in this system. This is then computed in
terms of “injection pulse duration” to automatically compensate for
the difference between the two ratios.
“Fuel trim” refers to the feedback compensation value compared
against the basic injection duration. Fuel trim includes short-term
fuel trim and long-term fuel trim.
“Short-term fuel trim” is the short-term fuel compensation used to
maintain the mixture ratio at its theoretical value. The signal from
the front heated oxygen sensor indicates whether the mixture ratio
is RICH or LEAN compared to the theoretical value. The signal
then triggers a reduction in fuel volume if the mixture ratio is rich,
and an increase in fuel volume if it is lean.
“Long-term fuel trim” is overall fuel compensation carried out longterm to compensate for continual deviation of the short-term fuel
trim from the central value. Such deviation will occur due to individual engine differences, wear over time and changes in the usage
environment.
EC-22
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Multiport Fuel Injection (MFI) System (Cont’d)
FUEL INJECTION SYSTEM
Two types of systems are used.
Sequential multiport fuel injection system
Fuel is injected into each cylinder during each engine cycle according to the firing order. This system is used when the engine is running.
Simultaneous multiport fuel injection system
Fuel is injected simultaneously into all six cylinders twice each
engine cycle. In other words, pulse signals of the same width are
simultaneously transmitted from the ECM.
The six injectors will then receive the signals two times for each
engine cycle.
This system is used when the engine is being started and/or if the
fail-safe mode (CPU) or crankshaft position sensor (REF) is operating.
FUEL SHUT-OFF
Fuel to each cylinder is cut off during deceleration or operation of
the engine at excessively high speeds.
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INPUT/OUTPUT SIGNAL LINE
Camshaft position sensor
Mass air flow sensor
Engine coolant temperature sensor
Throttle position sensor
Vehicle speed sensor
Ignition switch
Knock sensor
PNP switch (TCM)
Battery
Secondary throttle position
sensor
MEF404E
TAC
module
E
Electronic Ignition (EI) System
Engine speed and piston position
Amount of intake air
Engine coolant temperature
Throttle position
Throttle valve idle position
Vehicle speed
Start signal
Engine knocking
Park/Neutral position
Battery voltage
Throttle position
(Secondary throttle position sensor)
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ECM
E
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Power
E
transistor
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EC-23
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Electronic Ignition (EI) System (Cont’d)
SYSTEM DESCRIPTION
The ignition timing is controlled by the ECM to maintain the best
air-fuel ratio for every running condition of the engine.
The ignition timing data is stored in the ECM. This data forms the
map shown below.
The ECM detects information such as the injection pulse width and
camshaft position sensor signal. Responding to this information,
ignition signals are transmitted to the power transistor.
e.g.N: 1,800 rpm, Tp: 1.50 msec
A °BTDC
SEF742M
During the following conditions, the ignition timing is revised by the
ECM according to the other data stored in the ECM.
1At starting
2During warm-up
3At idle
4Hot engine operation
5At acceleration
The knock sensor retard system is designed only for emergencies.
The basic ignition timing is programmed within the anti-knocking
zone, if recommended fuel is used under dry conditions. The retard
system does not operate under normal driving conditions.
If engine knocking occurs, the knock sensor monitors the condition.
The signal is transmitted to the ECM. The ECM retards the ignition
timing to eliminate the knocking condition.
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INPUT/OUTPUT SIGNAL LINE
Air conditioner switch
Throttle position sensor
Camshaft position sensor
Ignition switch
Secondary throttle position
sensor
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TAC
module
SYSTEM DESCRIPTION
This system improves engine operation when the air
conditioner is used.
Under the following conditions, the air conditioner is
turned off.
IWhen the accelerator pedal is fully depressed.
IWhen cranking the engine.
IAt high engine speeds.
IAfter a few seconds when the TCS has started
operating.
Air Conditioning Cut Control
Air conditioner “ON” signal
E
Throttle valve opening angle
E
Engine speed
E
Start signal
E
Secondary throttle valve opening angle
E
ECM
Air conditioner
E
relay
EC-24
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
INPUT/OUTPUT SIGNAL LINE
Fuel Cut Control (at no load & high engine
speed)
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Vehicle speed sensor
PNP switch (TCM)
Throttle position sensor
Engine coolant temperature sensor
Camshaft position sensor
Vehicle speed
Park/Neutral position
Throttle position
Engine coolant temperature
Engine speed and piston position
If the engine speed is above 1,400 rpm with no load (for example,
in neutral and engine speed over 1,400 rpm) fuel will be cut off after
some time. The exact time when the fuel is cut off varies based on
engine speed.
Fuel cut will operate until the engine speed reaches 1,000 rpm,
then fuel cut is cancelled.
NOTE:
This function is different than deceleration control listed
under multiport fuel injection on EC-21.
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ECM
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Injectors
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EC-25
EVAPORATIVE EMISSION SYSTEM
Description
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SEF523Y
The evaporative emission system is used to reduce hydrocarbons
emitted into the atmosphere from the fuel system. This reduction
of hydrocarbons is accomplished by activated charcoals in the
EVAP canister.
The fuel vapor in the sealed fuel tank is led into the EVAP canister which contains activated carbon. This is where the vapor is
stored when the engine is not operating.
The vapor in the EVAP canister is purged by the air flowing through
the EVAP canister purge volume control valve which is controlled
by engine control module. When the engine operates, the flow rate
of vapor controlled by the EVAP canister purge volume control
valve is proportionally regulated as the air flow increases.
The EVAP canister purge control valve shuts off the vapor purge
line during decelerating and idling; under normal operating conditions the valve is usually open.
SEF210U
Inspection
EVAP CANISTER
Check EVAP canister as follows:
1.Pinch the fresh air hose.
A
2.Blow air into port
q
B
.
q
and check that it flows freely out of port
EC-26
EVAPORATIVE EMISSION SYSTEM
Inspection (Cont’d)
TIGHTENING TORQUE
Tighten EVAP canister as shown in the figure.
Make sure new O-ring is installed properly between EVAP canister and EVAP vent control valve.
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SEF231SA
SEF427N
SEF943S
FUEL TANK VACUUM RELIEF VALVE (Built into fuel
filler cap)
1.Wipe clean valve housing.
2.Check valve opening pressure and vacuum.
Pressure:
15.3 - 20.0 kPa (0.156 - 0.204 kg/cm
psi)
Vacuum:
−6.0 to −3.3 kPa (−0.061 to −0.034 kg/cm
−0.48 psi)
3.If out of specification, replace fuel filler cap as an assembly.
CAUTION:
Use only a genuine fuel filler cap as a replacement. If an incorrect fuel filler cap is used, the MIL may come on.
2
, 2.22 - 2.90
2
, −0.87 to
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EVAP CANISTER PURGE CONTROL VALVE
Refer to EC-488.
VACUUM CUT VALVE AND VACUUM CUT VALVE
BYPASS VALVE
Refer to EC-475.
EVAPORATIVE EMISSION (EVAP) CANISTER PURGE
VOLUME CONTROL VALVE
Refer to EC-444.
EVAPORATIVE EMISSION (EVAP) CANISTER PURGE
CONTROL SOLENOID VALVE
Refer to EC-488.
FUEL TANK TEMPERATURE SENSOR
Refer to EC-257.
EC-27
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EVAPORATIVE EMISSION SYSTEM
Inspection (Cont’d)
EVAP SERVICE PORT
Positive pressure is delivered to the EVAP system through the
EVAP service port. If fuel vapor leakage in the EVAP system
occurs, use a leak detector to locate the leak.
SEF462UA
HOW TO DETECT FUEL VAPOR LEAKAGE
CAUTION:
INever use compressed air or a high pressure pump.
IDo not start engine.
IDo not exceed 4.12 kPa (0.042 kg/cm
in EVAP system.
NOTE:
IImproper installation of adapter to the service port may
cause a leak.
SEF200U
PEF658U
1.Attach the EVAP service port adapter securely to the
EVAP SERVICE port.
2.Also attach the pressure pump and hose.
3.Turn ignition switch “ON”.
4.Select the “EVAP SYSTEM CLOSE” of “WORK SUPPORT MODE” with CONSULT-II.
5.Touch “START”. A bar graph (Pressure indicating display) will appear on the screen.
6.Apply positive pressure to the EVAP system until the
pressure indicator reaches the middle of the bar graph.
7.Remove adapter and hose with pressure pump.
8.Locate the leak using a leak detector. Refer to “Evaporative Emission Line Drawing”, EC-29.
1.Attach the adapter securely to the EVAP service port
and pressure pump with pressure gauge to the EVAP
service port.
2.Apply battery voltage to between the terminals of both
EVAP canister vent control valve and vacuum cut valve
bypass valve to make a closed EVAP system.
3.To locate the leak, deliver positive pressure to the EVAP
system until pressure gauge points reach 1.38 - 2.76
kPa (0.014 - 0.028 kg/cm
2
, 0.2 - 0.4 psi).
4.Remove adapter and hose with pressure pump.
5.Locate the leak using a leak detector. Refer to “Evaporative Emission Line Drawing”, EC-29.
EC-28
EVAPORATIVE EMISSION SYSTEM
Evaporative Emission Line Drawing
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SEF211U
Note: Do not use soapy water or any type of solvent while installing vacuum hoses or purge hoses.
EC-29
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EVAPORATIVE EMISSION SYSTEM
Evaporative Emission Line Drawing (Cont’d)
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SEF369U
EC-30
SYSTEM DESCRIPTION
EVAPORATIVE EMISSION SYSTEM
On Board Refueling Vapor Recovery (ORVR)
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From the beginning of refueling, the fuel tank pressure goes up. When the pressure reaches the setting value
of the refueling control valve (RCV) opening pressure, the RCV is opened. After RCV opens, the air and vapor
inside the fuel tank go through refueling EVAP vapor cut valve, RCV and refueling vapor line to the EVAP
canister. The vapor is absorbed by the EVAP canister and the air is released to the atmosphere.
When the refueling has reached the full level of the fuel tank, the refueling EVAP vapor cut valve is closed
and refueling is stopped because of auto shut-off. The vapor which was absorbed by the EVAP canister is
purged during driving.
The RCV is always closed during driving and the evaporative emission control system is operated the same
as conventional system.
WARNING:
When conducting inspections below, be sure to observe the following:
IPuta“CAUTION: INFLAMMABLE” sign in workshop.
IDo not smoke while servicing fuel system. Keep open flames and sparks away from work area.
IBe sure to furnish the workshop with a CO
CAUTION:
IBefore removing fuel line parts, carry out the following procedures:
a. Put drained fuel in an explosion-proof container and put lid on securely.
b. Release fuel pressure from fuel line. Refer to “Fuel Pressure Release”, EC-37.
c. Disconnect battery ground cable.
IAlways replace O-ring when the fuel gauge retainer is removed.
IDo not kink or twist hose and tube when they are installed.
IDo not tighten hose and clamps excessively to avoid damaging hoses.
IAfter installation, run engine and check for fuel leaks at connection.
IDo not attempt to top off the fuel tank after the fuel pump nozzle shuts off automatically.
IContinued refueling may cause fuel overflow, resulting in fuel spray and possibly a fire.
fire extinguisher.
2
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SEF206V
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EC-31
IDX
EVAPORATIVE EMISSION SYSTEM
On Board Refueling Vapor Recovery (ORVR)
(Cont’d)
DIAGNOSTIC PROCEDURE
SYMPTOM: Fuel odor from EVAP canister is strong.
INSPECTION START
EXIT
EXIT
H
CHECK COMPONENT
(EVAP canister).
Check EVAP canister for water.
Weigh the EVAP canister with vent control
valve attached.
If the weight is:
More than 1.8 kg (4 lb) → NG
Less than 1.8 kg (4 lb) → OK
If OK, check that water drains from the
canister.
Water should not drain from the EVAP
canister.
OK
H
CHECK COMPONENT
(Refueling EVAP vapor cut valve).
Check refueling EVAP vapor cut valve for
open.
Refer to “COMPONENT INSPECTION”,
EC-34.
OK
H
CHECK COMPONENT
(Refueling control valve).
Check refueling control valve diaphragm
q
for damage. Blow air into hose end
and check that there is no air flow. Refer
to “COMPONENT INSPECTION”, EC-34.
A
,
NG
Replace EVAP canister.
E
NG
Replace refueling EVAP
E
vapor cut valve with fuel
tank.
NG
Replace refueling control
E
valve with fuel tank.
OK
H
INSPECTION END
EC-32
EVAPORATIVE EMISSION SYSTEM
On Board Refueling Vapor Recovery (ORVR)
(Cont’d)
SYMPTOM: Cannot refuel/Fuel odor from the fuel filler open-
ing is strong while refueling.
EXIT
EXIT
INSPECTION START
H
CHECK COMPONENT
(Water separator and EVAP canister).
1. Check water separator for insect nests
or debris. Refer to “COMPONENT
INSPECTION”, EC-441.
2. Weigh the EVAP canister with vent control valve attached.
If the weight is:
More than 1.8 kg (4 lb) → NG
Less than 1.8 kg (4 lb) → OK
If OK, check that water drains from the
canister.
Water should not drain from the
EVAP canister.
OK
H
CHECK COMPONENT
(Vent hoses and vent tubes).
Check hoses and tubes between EVAP
canister and refueling control valve for
clogging, kink, looseness and improper
connection.
OK
H
CHECK COMPONENT
(Filler neck tube).
Check signal line and recirculation line for
clogging, dents and cracks.
NG
Replace water separator or
E
EVAP canister.
NG
Repair or replace hoses
E
and tubes.
NG
Replace filler neck tube.
E
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OK
H
CHECK COMPONENT
(Refueling control valve).
Refer to “COMPONENT INSPECTION” on
next page.
OK
H
CHECK COMPONENT
(Refueling EVAP vapor cut valve).
Refer to “COMPONENT INSPECTION” on
next page.
OK
H
CHECK COMPONENT
(Fuel filler tube).
1. Check filler neck tube and hose connected to the fuel tank for clogging,
dents and cracks.
2. Check one-way fuel valve for clogging.
Refer to “COMPONENT INSPECTION”
on next page.
OK
H
INSPECTION END
NG
Replace refueling control
E
valve with fuel tank.
NG
Replace fuel tank with
E
refueling EVAP vapor cut
valve.
NG
Replace fuel filler tube or
E
replace one-way fuel valve
with fuel tank.
BR
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IDX
EC-33
EVAPORATIVE EMISSION SYSTEM
On Board Refueling Vapor Recovery (ORVR)
(Cont’d)
COMPONENT INSPECTION
Refueling control valve
Check refueling control valve as follows:
1. Remove fuel filler cap.
A
2. Check air continuity between hose ends
q
Blow air into the hose end
3. Blow air into hose end
4. Apply pressure to both hose ends
B
. Air should flow freely into the fuel tank.
A
q
and check there is no leakage.
q
q
A
and
q
B
a suitable 3-way connector. And check there is no leakage.
If NG, replace refueling control valve with fuel tank.
B
q
and
[20 kPa (150 mmHg, 5.91 inHg)] using a pressure pump and
EXIT
EXIT
.
SEF817X
SEF816X
Refueling EVAP vapor cut valve
1.Remove fuel tank. Refer to “FUEL SYSTEM” in FE section.
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.
a. Remove fuel gauge retainer.
b. Drain fuel from the tank using a hand pump into a fuel
container.
2.Check refueling EVAP vapor cut valve for being stuck to close
as follows.
Blow air into the refueling EVAP vapor cut valve (from hose
q
B
end
), and check that the air flows freely into the tank.
3.Check EVAP vapor cut valve for being stuck to open as following.
a.Connect vacuum pump to hose ends
A
and
B
q
using a suit-
q
able 3-way connector.
b.Remove fuel gauge retainer with fuel gauge unit.
Always replace O-ring with new one.
EC-34
EVAPORATIVE EMISSION SYSTEM
On Board Refueling Vapor Recovery (ORVR)
(Cont’d)
c.Put fuel tank upside down.
d.Apply vacuum pressure to both hose ends
kPa (−100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
If NG, replace refueling EVAP vapor cut valve with fuel tank.
One-way fuel valve
1.Drain fuel from the tank.
Refer to “COMPONENT INSPECTION” of refueling EVAP
vapor cut valve on previous page.
2.Remove fuel filler tube and hose.
3.Check one-way fuel valve for operation as follows.
When pushing with finger, the valve should open; when finger
is released, the valve should shut.
Do not drop any material into the tank.
If NG, replace one-way fuel valve with fuel tank.
SEF818X
q
EXIT
EXIT
A
and
q
B
[−13.3
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EC-35
IDX
POSITIVE CRANKCASE VENTILATION
Description
EXIT
EXIT
This system returns blow-by gas to both the intake
manifold and air cleaner.
The positive crankcase ventilation (PCV) valve is
provided 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 sufficient to
handle any blow-by and a small amount of ventilating air.
The ventilating air is then drawn from the air cleaner,
through the hose connecting air cleaner to rocker
cover, into the crankcase.
Under full-throttle condition, the manifold vacuum is
insufficient to draw the blow-by flow through the
valve, and its flowgoes through the hose connection
in the reverse direction.
On vehicles with an excessively high blow-by some
of the flow will go through the hose connection to the
air cleaner under all conditions.
SEF110T
Inspection
PCV (Positive Crankcase Ventilation) VALVE
With engine running at idle, remove ventilation hose from PCV
valve; if valve is working properly, a hissing noise will be heard as
air passes through it and a strong vacuum should be felt immediately when a finger is placed over valve inlet.
SEF244Q
PCV HOSE
1.Check hoses and hose connections for leaks.
2.Disconnect all hoses and clean with compressed air. If any
hose cannot be freed of obstructions, replace.
ET277
EC-36
BASIC SERVICE PROCEDURE
Fuel Pressure Release
Before disconnecting fuel line, release fuel pressure from fuel
line to eliminate danger.
1.Start engine.
2.Perform “FUEL PRESSURE RELEASE” in “WORK
SUPPORT” mode with CONSULT-II.
(Touch “START” and after engine stalls, crank it two or
three times to release all fuel pressure.)
3.After engine stalls, crank it two or three times to release
all fuel pressure.
4.Turn ignition switch off and reconnect fuel pump fuse.
Fuel Pressure Check
IWhen reconnecting fuel line, always use new clamps.
IMake sure that clamp screw does not contact adjacent
parts.
IUse a torque driver to tighten clamps.
IUse Pressure Gauge to check fuel pressure.
1.Release fuel pressure to zero, refer to previous page.
2.Disconnect fuel hose between fuel filter and fuel tube (engine
side).
3.Install pressure gauge between fuel filter and fuel tube.
4.Start engine and check for fuel leakage.
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SEF718B
SEF114T
5.Read the indication of fuel pressure gauge.
At idling:
Approximately 235 kPa (2.4 kg/cm
A few seconds after ignition switch is turned OFF to
ON:
Approximately 294 kPa (3.0 kg/cm
6.Stop engine and disconnect fuel pressure regulator vacuum
hose from intake manifold.
7.Plug intake manifold with a rubber cap.
8.Connect variable vacuum source to fuel pressure regulator.
9.Start engine and read indication of fuel pressure gauge as
vacuum is changed.
Fuel pressure should decrease as vacuum increases. If results
are unsatisfactory, replace fuel pressure regulator.
2
, 34 psi)
2
, 43 psi)
EC-37
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IDX
BASIC SERVICE PROCEDURE
Injector Removal and Installation
EXIT
EXIT
SEF245QB
SEF113T
1.Release fuel pressure to zero, refer to previous page.
2.Remove intake manifold collector. Refer to EM section (“TIMING CHAIN”).
3.Disconnect vacuum hose from pressure regulator.
4.Disconnect fuel hoses from fuel tube assembly.
IDo not disassemble fuel tube assembly.
5.Disconnect injector harness connectors.
6.Remove injectors with fuel tube assembly.
IPush injector tail piece.
IDo not pull on the connector.
7.Push out any malfunctioning injector from fuel tube assembly.
8.Replace or clean injector as necessary.
9.Install injector to fuel tube assembly.
IAlways replace O-rings with new ones.
ILubricate O-rings with a smear of engine oil.
10. Install injectors with fuel tube assembly to intake manifold.
Tighten in numerical order shown in the figure.
a)First, tighten all bolts to 9.3 to 10.8 N⋅m (0.95 to 1.1 kg-m, 6.9
to 8.0 ft-lb).
b)Then, tighten all bolts to 21 to 26 N⋅m (2.1 to 2.7 kg-m, 15 to
20 ft-lb).
11. Install fuel hoses to fuel tube assembly.
12. Reinstall any parts removed in reverse order of removal.
CAUTION:
After properly connecting fuel hose to injector and fuel tube
assembly, check connection for fuel leakage.
EC-38
BASIC SERVICE PROCEDURE
Throttle Opener
INSPECTION
1.Start engine and let it idle.
2.Confirm the amount of the rod moves “L” more than 1.65 mm
(0.0650 in), the throttle drum becomes free from the rod of the
throttle opener.
If NG, go to next step.
If OK, inspection is end.
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EXIT
EXIT
SEF910X
SEF109L
SEF368U
3.Turn ignition switch “OFF”.
4.Check vacuum source to throttle opener.
a.Check vacuum hose for disconnection or improper connection.
b.Remove vacuum hose connected to throttle opener.
c.Attach a vacuum gauge to vacuum hose, which is discon-
nected.
d.Start engine and let it idle.
e.Make sure that the vacuum is more than −40.0 kPa (−300
mmHg, −11.81 inHg).
f.Remove the vacuum gauge from intake manifold.
If NG, go to next step.
If OK, go to step 7.
5.Check vacuum hose for clogging and cracks.
If NG, replace or clean vacuum hose.
If OK, go to next step.
6.Blow air into the intake manifold and make sure air flows freely.
If NG, replace or clean intake manifold.
If OK, go to next step.
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SEF793W
7.Check throttle opener.
a.Connect suitable vacuum hose to vacuum pump as shown at
left.
b.Apply vacuum [more than −40.0 kPa (−300 mmHg, −11.81
inHg)] until the throttle drum becomes free from the rod of the
throttle opener.
c.Confirm the amount of the rod moves more than 1.65 mm
(0.0650 in), and also the throttle drum becomes free from the
rod of the throttle opener.
If NG, go to next step.
8.Check visually for cracking and/or distortion of throttle opener
and rod.
If NG, replace throttle opener.
If OK, install the vacuum hose and repeat from step 1 to 2.
EC-39
ST
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IDX
BASIC SERVICE PROCEDURE
Fast Idle Cam (FIC) Inspection and Adjustment
1.Remove throttle body from engine.
2.Wait for at least 3 hours.
(This step is necessary to bring the temperature of the thermoelement to the room temperature
3.Measure thermo-element stroke (L) and room temperature.
4.Check thermo-element stroke (L) as shown in the figure.
CAUTION:
Do not adjust TAS.
L: Thermo-element strokeJudgement
Within oblique line
Out of oblique line
SEF292TA
Thermo-element is normal , Adjust
FI cam (go to step 5).
Replace thermo-element , Adjust FI
cam (go to step 2).
EXIT
EXIT
5.Measure clearance between stopper and throttle adjusting
screw (TAS) as shown in the figure. If out of specification,
adjust the clearance using adjusting screw.
CAUTION:
Do not adjust throttle adjusting screw (TAS).
6.After adjustment, tighten lock nut of adjusting screw.
Adjust ignition timing by turning camshaft
position sensor after loosening securing bolts
which secures camshaft position sensor.
H
q
A
Connect throttle position sensor harness
connector.
H
Clean injectors.
H
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B
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IDX
q
B
E
SEF212U
EC-43
BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio
Adjustment (Cont’d)
q
A
H
Connect throttle position sensor harness connector.
H
Check target idle speed.
SEF043T
SEF392X
--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------Read idle speed in “DATA MONITOR” mode with CONSULT-II
1) Connect throttle position sensor harness connector.
2) Erase diagnostic trouble code, EC-67.
H
Run engine at about 2,000 rpm for
about 2 minutes under no-load.
H
q
D
F
q
H
H
q
B
SEF247F
EC-44
BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio
Adjustment (Cont’d)
q
D
EXIT
EXIT
SEF957D
SEF393X
SEF217U
H
Set on board diagnostic system of ECM to Diagnostic Test Mode II
(Front heated oxygen sensor monitor).*
H
Check left bank front heated oxygen sensor signal.
1) See “FR O2 SEN MNTR-B1 and B2 (left
and right sides)” in “Data monitor” mode.
2) Maintaining engine at 2,000 rpm under
no-load (engine is warmed up
sufficiently.), check that the monitor fluctuates between “LEAN” and “RICH”
more than 5 times during 10 seconds.
--------------------------------------------------------------------------------------------------------------------------------------------------------------------OR-------------------------------------------------------------------------------------------------------------------------------------------------------------------Make sure that malfunction indicator lamp
goes on and off more than 5 times during
10 seconds at 2,000 rpm.
OK
OK
F
H
q
L
LEAN → RICH
H
Replace left bank front heated oxygen sensor.
F
H
Check left bank front heated oxygen sensor signal.
1) See “FR O2 SEN MNTR-B1 and B2
(right and left sides)” in “Data monitor”
mode.
2) Maintaining engine at 2,000 rpm under
no-load (engine is warmed up
sufficiently.), check that the monitor fluctuates between “LEAN” and “RICH”
more than 5 times during 10 seconds.
--------------------------------------------------------------------------------------------------------------------------------------------------------------------OR-------------------------------------------------------------------------------------------------------------------------------------------------------------------Make sure that malfunction indicator lamp
goes on and off more than 5 times during
10 seconds at 2,000 rpm.
Monitor does not fluctuate. Malfunction
indicator lamp does
not blink.
Less than 5 times
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NG
q
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*: If the battery is weak, front heated oxygen sensor monitor may not func-
tion properly. Use this function after fully charging battery.
EC-45
HA
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IDX
BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio
Adjustment (Cont’d)
q
L
EXIT
EXIT
SEF393X
SEF217U
H
Check right bank front heated oxygen sensor signal.
1) See “FR O2 SEN MNTR-B1 and -B2
(left and right sides)” in “Data monitor”
mode.
2) Maintaining engine at 2,000 rpm under
no-load (engine is warmed up
sufficiently.), check that the monitor fluctuates between “LEAN” and “RICH”
more than 5 times during 10 seconds.
--------------------------------------------------------------------------------------------------------------------------------------------------------------------OR-------------------------------------------------------------------------------------------------------------------------------------------------------------------Make sure that malfunction indicator lamp
goes on and off more than 5 times during
10 seconds at 2,000 rpm.
OK
H
END
Replace right bank front heated oxygen sensor.
Less than 5 times
H
Monitor does not fluctuate.
Malfunction indicator
lamp does not blink.
q
q
H
C
E
G
H
Check right bank front heated oxygen sensor signal.
1) See “FR O2 SEN MNTR-B1 and -B2
(left and right sides)” in “Data monitor”
mode.
2) Maintaining engine at 2,000 rpm under
no-load (engine is warmed up
sufficiently.), check that the monitor fluctuates between “LEAN” and “RICH”
more than 5 times during 10 seconds.
--------------------------------------------------------------------------------------------------------------------------------------------------------------------OR-------------------------------------------------------------------------------------------------------------------------------------------------------------------Make sure that malfunction indicator lamp
goes on and off more than 5 times during
10 seconds at 2,000 rpm.
OK
H
END
NG
EC-46
BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio
Adjustment (Cont’d)
EXIT
EXIT
SEF213U
SEF214U
Check right bank front heated oxygen sensor harness:
1) Turn off engine and disconnect battery ground cable
2) Disconnect ECM harness connector from ECM.
3) Disconnect right bank front heated oxygen sensor harness connector.
4) Check for continuity between terminal No. 82 of ECM harness
connector and harness connector for front heated oxygen sensor.
1) Disconnect the resistor from terminals of engine coolant tempera-
ture sensor.
2) Connect engine coolant temperature sensor harness connector to
engine coolant temperature sensor.
NG
H
Connect front heated oxygen sensor harness connectors to front
heated oxygen sensors.
H
Check fuel pressure regulator.
H
Check mass air flow sensor.
H
Check injector.
Clean or replace if necessary.
H
Check engine coolant temperature sensor.
J
q
G
OK
q
K
F
q
H
G
H
Check ECM function* by substituting another known good ECM.
*: ECM may be the cause of a problem, but this is rarely the case.
Note: If a vehicle contains a part which is operating outside of design specifications with no MIL
illumination, the part shall not be replaced prior to emission testing unless it is determined that
the part has been tampered with or abused in such a way that the diagnostic system cannot
reasonably be expected to detect the resulting malfunction.
EC-48
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Introduction
The ECM has an on board diagnostic system, which detects malfunctions related to engine sensors or actuators. The ECM also records various emission-related diagnostic information including:
IDiagnostic Trouble Code (DTC) .................................................................................Mode 3 of SAE J1979
IFreeze Frame data.....................................................................................................Mode 2 of SAE J1979
ISystem Readiness Test (SRT) code ..........................................................................Mode 1 of SAE J1979
ITest values and Test limits .........................................................................................Mode 6 of SAE J1979
The above information can be checked using procedures listed in the table below.
DTC1st trip DTC
Diagnostic test
mode II (Selfdiagnostic
results)
CONSULT-IIXXXXX—
GSTXX*2X—XX
*1: When DTC and 1st trip DTC simultaneously appear on the display, they cannot be clearly distinguished from each other.
*2: 1st trip DTCs for self-diagnoses concerning SRT items cannot be shown on the GST display.
XX*1————
Freeze Frame
data
1st trip Freeze
Frame data
SRT codeTest value
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-98.).
Two Trip Detection Logic
When a malfunction is detected for the first 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” means a driving mode in which self-diagnosis is performed
during vehicle operation. Specific on board diagnostic items 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.
Items
Misfire (Possible three way catalyst
damage)
— DTC: P0300 - P0308 (0701,
0608 - 0601) is being detected
Misfire (Possible three way catalyst
damage)
— DTC: P0300 - P0308 (0701,
0608 - 0601) has been detected
Closed loop control — DTC: P1148
(0307), P1168 (0308)
Fail-safe items (Refer to EC-98.)—XX*1—X*1—
Except above——XXXX
*1: Except “ECM”.
1st trip
BlinkingLighting up
X——X—X—
—X—X—X—
—X—X—X—
MILDTC1st trip DTC
2nd trip
lighting up
1st trip
displaying
2nd trip
displaying
1st trip
displaying
2nd trip
displaying
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EXIT
EXIT
EC-49
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
DTC AND 1ST TRIP DTC
The 1st trip DTC (whose number is the same as the DTC number) is displayed for the latest self-diagnostic
result obtained. If the ECM memory was cleared previously, and the first trip DTC did not reoccur, the first trip
DTC will not be displayed. If a malfunction is detected during the 1st trip, the 1st trip DTC is stored in the ECM
memory. The MIL will not light up (two trip detection logic). If the same malfunction is not detected in the 2nd
trip (meeting the required driving pattern), the 1st trip DTC is cleared from the ECM memory. If the same malfunction is detected in the 2nd trip, both the first trip DTC and DTC are stored in the ECM memory and the
MIL lights up. In other words, the DTC is stored in the ECM memory and the MIL lights up when the same
malfunction occurs in two consecutive trips. If a first trip DTC is stored and a non-diagnostic operation is performed between the 1st and 2nd trips, only the 1st trip DTC will continue to be stored. For malfunctions that
blink or light up the MIL during the 1st trip, the DTC and 1st trip DTC are stored in the ECM memory.
Procedures for clearing the DTC and the 1st trip DTC from the ECM memory are described in “HOW TO
ERASE EMISSION-RELATED DIAGNOSTIC INFORMATION”. Refer to EC-63.
For malfunctions in which 1st trip DTCs are displayed, refer to EC-60. These items are required by legal
regulations to continuously monitor the system/component. In addition, the items monitored non-continuously
are also displayed on CONSULT-II.
1st trip DTC is specified in Mode 7 of SAE J1979. 1st trip DTC detection occurs without lighting up the MIL
and therefore does not warn the driver of a problem. However, 1st trip DTC detection will not prevent the
vehicle from being tested, for example during Inspection/Maintenance (I/M) tests.
When a 1st trip DTC is detected, check, print out or write down and erase (1st trip) DTC and Freeze Frame
data as specified in “Work Flow” procedure Step II, refer to page EC-89. Then perform “Diagnostic trouble code
confirmation procedure” or “Overall function check” to try to duplicate the problem. If the malfunction is
duplicated, the item requires repair.
EXIT
EXIT
How to read DTC and 1st trip DTC
DTC and 1st trip DTC can be read by the following methods.
1. The number of blinks of the malfunction indicator lamp in the Diagnostic Test Mode II (Self-Diagnostic Results) Examples: 0101, 0201, 1003, 1104, etc.
These DTCs are controlled by NISSAN.
2. CONSULT-II or GST (Generic Scan Tool) Examples: P0340, P1320, P0705, P0750, etc.
These DTCs are prescribed by SAE J2012.
(CONSULT-II also displays the malfunctioning component or system.)
I1st trip DTC No. is the same as DTC No.
IOutput of a DTC indicates a malfunction. However, Mode II and GST do not indicate whether the
malfunction is still occurring or has occurred in the past and has returned to normal.
CONSULT-II can identify malfunction status as shown below. Therefore, using CONSULT-II (if available) is recommended.
A sample of CONSULT-II display for DTC is shown at left. DTC or 1st trip DTC of a malfunction is displayed
in SELF-DIAGNOSTIC RESULTS mode of CONSULT-II. Time data indicates how many times the vehicle was
driven after the last detection of a DTC.
If the DTC is being detected currently, the time data will be “0”.
If a 1st trip DTC is stored in the ECM, the time data will be “[1t]”.
EC-50
SEF698X
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
FREEZE FRAME DATA AND 1ST TRIP FREEZE FRAME DATA
The ECM records the driving conditions such as fuel system status, calculated load value, engine coolant
temperature, short term fuel trim, long term fuel trim, engine speed and vehicle speed at the moment a malfunction is detected.
Data which are stored in the ECM memory, along with the 1st trip DTC, are called 1st trip freeze frame data.
The data, stored together with the DTC data, are called freeze frame data and are displayed on CONSULT-II
or GST. The 1st trip freeze frame data can only be displayed on the CONSULT-II screen, not on the GST. For
details, see EC-77.
Only one set of freeze frame data (either 1st trip freeze frame data of freeze frame data) can be stored in the
ECM. 1st trip freeze frame data is stored in the ECM memory along with the 1st trip DTC. There is no priority for 1st trip freeze frame data and it is updated each time a different 1st trip DTC is detected. However, once
freeze frame data (2nd trip detection/MIL on) is stored in the ECM memory, 1st trip freeze frame data is no
longer stored. Remember, only one set of freeze frame data can be stored in the ECM. The ECM has the following priorities to update the data.
2Except the above items (Includes A/T related items)
31st trip freeze frame data
For example, the EGR malfunction (Priority: 2) was detected and the freeze frame data was stored in the 2nd
trip. After that when the misfire (Priority: 1) is detected in another trip, the freeze frame data will be updated
from the EGR malfunction to the misfire. The 1st trip freeze frame data is updated each time a different malfunction is detected. There is no priority for 1st trip freeze frame data. However, once freeze frame data is
stored in the ECM memory, 1st trip freeze frame data is no longer stored (because only one freeze frame data
or 1st trip freeze frame data can be stored in the ECM). If freeze frame data is stored in the ECM memory
and freeze frame data with the same priority occurs later, the first (original) freeze frame data remains
unchanged in the ECM memory.
Both 1st trip freeze frame data and freeze frame data (along with the DTCs) are cleared when the ECM
memory is erased. Procedures for clearing the ECM memory are described in “HOW TO ERASE EMISSIONRELATED DIAGNOSTIC INFORMATION”. Refer to EC-63.
SYSTEM READINESS TEST (SRT) CODE
System Readiness Test (SRT) code is specified in Mode 1 of SAE J1979.
As part of an enhanced emissions test for Inspection & Maintenance (I/M), certain states require the status of
SRT be used to indicate whether the ECM has completed self-diagnosis of major emission systems and components. Completion must be verified in order for the emissions inspection to proceed.
If a vehicle is rejected for a State emissions inspection due to one or more SRT items indicating “INCMP”,
use the information in this Service Manual to set the SRT to “CMPLT”.
In most cases the ECM will automatically complete its self-diagnosis cycle during normal usage, and the SRT
status will indicate “CMPLT” for each application system. Once set as “CMPLT”, the SRT status remains
“CMPLT” until the self-diagnosis memory is erased.
Occasionally, certain portions of the self-diagnostic test may not be completed as a result of the customer’s
normal driving pattern; the SRT will indicate “INCMP” for these items.
NOTE:
The SRT will also indicate “INCMP” if the self-diagnosis memory is erased for any reason or if the ECM
memory power supply is interrupted for several hours.
If, during the state emissions inspection, the SRT indicates “CMPLT” for all test items, the inspector
will continue with the emissions test. However, if the SRT indicates “INCMP” for one or more of the
SRT items the vehicle is returned to the customer untested.
If MIL is “ON” during the state emissions inspection, the vehicle is also returned to the customer
untested even though the SRT indicates “CMPLT” for all test items. Therefore, it is important to check
SRT (“CMPLT”) and DTC (No DTCs) before the inspection.
Fuel Injection System Function — DTC: P0171 (0115), P0172 (0114)
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EC-51
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
SRT Item
The table below shows required self-diagnostic items to set the SRT to “CMPLT”.
EXIT
EXIT
SRT item
(CONSULT-II indication)
CATALYST3Three way catalyst functionP0420, P0430
EVAP SYSTEM
O2 SENSOR3
O2 SEN HEATER3
EGR SYSTEM
Performance
Priority*2
2
—
3
3
1EGR function (open)P1402
Required self-diagnostic items to set the
SRT to “CMPLT”
EVAP control system (small leak) (negative pressure)
EVAP control system (small leak) (positive
pressure)
EVAP control system purge flow monitoring
Front heated oxygen sensor (circuit)P0130, P0150
Front heated oxygen sensor (lean shift
monitoring)
Front heated oxygen sensor (rich shift
monitoring)
Front heated oxygen sensor (response
monitoring)
Front heated oxygen sensor (high voltage) P0134, P0154
Rear heated oxygen sensor (min. voltage
monitoring)
Rear heated oxygen sensor (max. voltage
*1: P1440 [EVAPcontrol system (small leak) (positive pressure) diagnosis] is one type of SRT related diagnosis. This diagnosis, however,
does not contribute to setting the SRT as “CMPLT”,when no malfunction exists in the EVAP system. Therefore, P0440 must be used
instead of P1440.
*2: If completion of several SRTs is required, perform driving patterns (DTC confirmation procedure), one by one based on the priority
for models with CONSULT-II.
EC-52
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
SRT Set Timing
SRT is set as “CMPLT” after self-diagnosis has been performed one or more times. Completion of SRT is done
regardless of whether the result is OK or NG. The set timing is different between OK and NG results and is
shown in the table below.
OK: Self-diagnosis is carried out and the result is OK.
NG: Self-diagnosis is carried out and the result is NG.
—: Self-diagnosis is not carried out.
When all SRT related self-diagnoses showed OK results in a single cycle (Ignition OFF-ON-OFF), the SRT
will indicate “CMPLT”. , Case 1 above
When all SRT related self-diagnoses showed OK results through several different cycles, the SRT will indicate “CMPLT” at the time the respective self-diagnoses have at least one OK result. , Case 2 above
If one or more SRT related self-diagnoses showed NG results in 2 consecutive cycles, the SRT will also indicate “CMPLT”. , Case 3 above
The table above shows that the minimum number of cycles for setting SRT as “INCMP” is one (1) for each
self-diagnosis (Case1&2)ortwo(2)foroneofself-diagnoses (Case 3). However, in preparation for the state
emissions inspection, it is unnecessary of each self-diagnosis to be executed twice (Case 3) for the following
reasons:
IThe SRT will indicate “CMPLT” at the time the respective self-diagnoses have one (1) OK result.
IThe emissions inspection requires “CMPLT” of the SRT only with OK self-diagnosis results.
IWhen, during SRT driving pattern, 1st trip DTC (NG) is detected prior to “CMPLT” of SRT, the self-diag-
nosis memory must be erased from ECM after repair.
IIf the 1st trip DTC is erased, all the SRT will indicate “INCMP”.
NOTE:
SRT can be set as “CMPLT” together with the DTC(s). Therefore, DTC check must always be carried
out prior to the state emission inspection even though the SRT indicates “CMPLT”.
SRT Service Procedure
If a vehicle has failed the state emissions inspection due to one or more SRT items indicating “INCMP”, review
the flowchart diagnostic sequence on the next page.
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EC-53
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
EXIT
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*1 EC-50*2 EC-54*3 EC-55
How to display SRT code
1. Selecting “SRT STATUS” in “DTC CONFIRMATION” mode with CONSULT-II
For items whose SRT codes are set, a “CMPLT” is displayed on the CONSULT-II screen; for items
whose SRT codes are not set, “INCMP” is displayed.
2. Selecting Mode 1 with GST (Generic Scan Tool)
SEF573XA
EC-54
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
A sample of CONSULT-II display for SRT code is shown at left.
“INCMP” means the self-diagnosis is incomplete and SRT is not
set. “CMPLT” means the self-diagnosis is complete and SRT is set.
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PEF215U
How to Set SRT Code
To set all SRT codes, self-diagnosis for the items indicated above must be performed one or more times. Each
diagnosis may require a long period of actual driving under various conditions.
With CONSULT-II
Perform corresponding DTC Confirmation Procedure one by one based on “Performance Priority” in the table
on EC-52.
Without CONSULT-II
The most efficient driving pattern in which SRT codes can be properly set is explained on the next page. The
driving pattern should be performed one or more times to set all SRT codes.
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EC-55
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Driving pattern
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
EXIT
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SEF574X
EC-56
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
EXIT
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I The time required for each diagnosis varies with road sur-
face conditions, weather, altitude, individual driving habits,
etc.
Zone A refers to the range where the time required, for the
diagnosis under normal conditions*, is the shortest. Zone B
refers to the range where the diagnosis can still be per-
formed if the diagnosis is not completed within zone A.
*: Normal conditions refer to the following:
— Sea level
— Flat road
— Ambient temperature: 20 - 30°C (68 - 86°F)
— Diagnosis is performed as quickly as possible under nor-
mal conditions.
Under different conditions [For example: ambient temperature is other than 20 - 30°C (68 - 86°F)], diagnosis may
also be performed.
Pattern 1: I The engine is started at the engine coolant tem-
Pattern 2: I When steady-state driving is performed again
Pattern 3: I The driving pattern outlined in *2 must be
Pattern 4: I Tests are performed after the engine has been
*1: Depress the accelerator pedal until vehicle speed is 90
km/h (56 MPH), then release the accelerator pedal and
keep it released for more than 10 seconds. Depress the
accelerator pedal until vehicle speed is 90 km/h (56 MPH)
again.
*2: Operate the vehicle in the following driving pattern.
1) Decelerate vehicle to 0 km/h (0 MPH) and let it idle.
2) Repeat driving pattern shown below at least 10 times.
3) Repeat steps and 2 until the EGR system SRT is set.
perature of −10 to 35°C (14 to 95°F) (where the
voltage between the ECM terminals
is 3.0 - 4.3 V.)
I The engine must be operated at idle speed until
the engine coolant temperature is greater than
70°C (158°F) (where the voltage between the
ECM terminals
I The engine is started at a fuel tank temperature
warmer than 0°C (32°F) (where the voltage
between the ECM terminal
than 4.1V).
even after it is interrupted, each diagnosis can
be conducted. In this case, the time required for
diagnosis may be extended.
repeated at least 3 times.
operated for at least 17 minutes.
I The accelerator pedal must be held very steady
during steady-state driving.
I If the accelerator pedal is moved, the test must
be conducted all over again.
I During acceleration, hold the accelerator pedal
as steady as possible.
q
67
and
128
is lower than 1.4 V.)
q
91
and ground is less
q
Suggested transmission gear position
Set the selector lever in the “D” position with “OD”
ON.
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Suggested maximum speed in each gear
Downshift to a lower gear if the engine is not running
smoothly, or if you need to accelerate.
Do not exceed the maximum suggested speed
(shown below) in any gear. For level road driving,
use the highest gear suggested for that speed.
Always observe posted speed limits, and drive
according to the road conditions, which will ensure
safe operation. Do not over-rev the engine when
67
and
128
shifting to a lower gear as it may cause engine damage or loss of vehicle control.
*3: Checking the vehicle speed with GST is advised.
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EC-57
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
TEST VALUE AND TEST LIMIT (GST only — not applicable to CONSULT-II)
The following is the information specified in Mode 6 of SAE J1979.
The test value is a parameter used to determine whether a system/circuit diagnostic test is “OK” or “NG” while
being monitored by ECM during self-diagnosis. The test limit is a reference value which is specified as the
maximum or minimum value and is compared with the test value being monitored.
Items for which these data (test value and test limit) are displayed are the same as SRT code items (14 test
items).
These data (test limit) are specified by Test ID (TID) and Component ID (CID). These data can be displayed
on the GST screen.
—: Not applicable
SRT item
CATALYST
EVAP SYSTEM
Self-diagnostic test
Three way catalyst
Three way catalyst
(Right bank)
EVAP control sys-
(Small leak)
EVAP control sys-
tem purge flow
Front heated oxy-
gen sensor (Left
Front heated oxygen sensor (Right
O2 SENSOR
Rear heated oxygen
Rear heated oxygen
(Right bank)
item
function
(Left bank)
function
tem
monitoring
bank)
bank)
sensor
(Left bank)
sensor
TIDCID
01H01HMax.X
03H02HMax.X
05H03HMax.X
06H83HMin.X
09H04HMax.X
0AH84HMin.X
0BH04HMax.X
0CH04HMax.X
0DH04HMax.X
11H05HMax.X
12H85HMin.X
13H05HMax.X
14H05HMax.X
15H05HMax.X
19H86HMin.X
1AH86HMin.X
1BH06HMax.X
1CH06HMax.X
21H87HMin.X
22H87HMin.X
23H07HMax.X
24H07HMax.X
Test value
Test limitApplication
X: Applicable
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EC-58
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
EXIT
EXIT
SRT item
O2 SENSOR
HEATER
EGR SYSTEM
Self-diagnostic test
item
Front heated oxygen sensor heater
(Left bank)
Front heated oxygen sensor heater
(Right bank)
Rear heated oxygen
sensor heater
(Left bank)
Rear heated oxygen
sensor heater
(Right bank)
EGR function
EGRC-BPT valve
function
Test value
TIDCID
29H08HMax.X
2AH88HMin.X
2BH09HMax.X
2CH89HMin.X
2DH0AHMax.X
2EH8AHMin.X
2FH0BHMax.X
30H8BHMin.X
31H8CHMin.X
32H8CHMin.X
33H8CHMin.X
34H8CHMin.X
35H0CHMax.X
36H0CHMax.X
37H8CHMin.X
Test limitApplication
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EC-59
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
EMISSION-RELATED DIAGNOSTIC INFORMATION ITEMS
(CONSULT-II screen terms)
NO DTC IS DETECTED,
FURTHER TESTING
MAY BE REQUIRED.
MAF SEN/CIRCUITP01000102——XEC-124
ABSL PRES SEN/CIRCP01050803——XEC-132
AIR TEMP SEN/CIRCP01100401——XEC-140
COOLANT T SEN/CIRCP01150103——XEC-145
THRTL POS SEN/CIRCP01200403——XEC-150
*COOLAN T SEN/CIRCP01250908——XEC-161
FRONT O2 SENSOR-B1P01300303XXX*3EC-166
FRONT O2 SENSOR-B1P01310411XXX*3EC-174
FRONT O2 SENSOR-B1P01320410XXX*3EC-180
FRONT O2 SENSOR-B1P01330409XXX*3EC-187
FRONT O2 SENSOR-B1P01340412XXX*3EC-196
FR O2 SE HEATER-B1P01350901XXX*3EC-204
REAR O2 SENSOR-B1P01370511XXX*3EC-210
REAR O2 SENSOR-B1P01380510XXX*3EC-218
REAR O2 SENSOR-B1P01390707XXX*3EC-226
REAR O2 SENSOR-B1P01400512XXX*3EC-233
RR O2 SE HEATER-B1P01410902XXX*3EC-239
FRONT O2 SENSOR-B2P01500503XXX*3EC-204
FRONT O2 SENSOR-B2P01510415XXX*3EC-174
FRONT O2 SENSOR-B2P01520414XXX*3EC-180
FRONT O2 SENSOR-B2P01530413XXX*3EC-187
FRONT O2 SENSOR-B2P01540509XXX*3EC-196
FR O2 SE HEATER-B2P01551001XXX*3EC-204
REAR O2 SENSOR-B2P01570314XXX*3EC-210
REAR O2 SENSOR-B2P01580313XXX*3EC-218
REAR O2 SENSOR-B2P01590708XXX*3EC-226
REAR O2 SENSOR-B2P01600315XXX*3EC-233
RR O2 SE HEATER-B2P01611002XXX*3EC-239
FUEL SYS LEAN/BK1P01710115——XEC-245
FUEL SYS RICH/BK1P01720114——XEC-251
FUEL SYS LEAN/BK2P01740210——XEC-245
FUEL SYS RICH/BK2P01750209——XEC-251
FUEL TEMP SEN/CIRCP01800402——XEC-257
MULTI CYL MISFIREP03000701——XEC-262
CYL 1 MISFIREP03010608——XEC-262
CYL 2 MISFIREP03020607——XEC-262
Items
CONSULT-II
GST*2
P00000505————
DTC*4
ECM*1
SRT code
Test value/
Test limit
(GST only)
1st trip DTC*4Reference page
X: Applicable
—: Not applicable
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*1: In Diagnostic Test Mode II (Self-diagnostic results). These numbers are controlled by NISSAN.
*2: These numbers are prescribed by SAE J2012.
*3: These are not displayed with GST.
*4: 1st trip DTC No. is the same as DTC No.
EC-60
ONBOARDDIAGNOSTICSYSTEMDESCRIPTION
Emission-relatedDiagnosticInformation
(Cont’d)
(CONSULT-IIscreenterms)
CYL3MISFIRE P0303 0606 — — X EC-262
CYL4MISFIRE P0304 0605 — — X EC-262
CYL5MISFIRE P0305 0604 — — X EC-262
CYL6MISFIRE P0306 0603 — — X EC-262
CYL7MISFIRE P0307 0602 — — X EC-262
CYL8MISFIRE P0308 0601 — — X EC-262
KNOCKSEN/CIRC-B1 P0325 0304 — — X EC-267
KNOCKSEN/CIRC-B2 P0330 0212 — — X EC-267
CPS/CIRCUIT(OBD) P0335 0802 — — X EC-270
CAMPOSSEN/CIR P0340 0101 — — X EC-275
EGRSYSTEM P0400 0302 X X X*3 EC-281
EGRC-BPTVALVE P0402 0306 X X X*3 EC-290
TWCATALYSTSYS-B1 P0420 0702 X X X*3 EC-295
TWCATALYSTSYS-B2 P0430 0703 X X X*3 EC-295
EVAPSMALLLEAK P0440 0705 X X X*3 EC-298
PURGVOLUMECONT/V P0443 1008 — — X EC-309
VENTCONTROLVALVE P0446 0903 — — X EC-315
EVAPOSYSPRESSEN P0450 0704 — — X EC-320
EVAPGROSSLEAK P0455 0715 — X X*3 EC-326
VEHSPEEDSEN/CIRC P0500 0104 — — X EC-335
IACV/AACVLV/CIRC P0505 0205 — — X EC-340
CLOSEDTPSW/CIRC P0510 0203 — — X EC-346
A/TCOMMLINE P0600 0504 — — — EC-352
ECM P0605 0301 — — X EC-355
PNPSW/CIRC P0705 1101 — — X AT-81
ATFTEMPSEN/CIRC P0710 1208 — — X AT-85
VEHSPDSEN/CIRAT P0720 1102 — — X AT-89
ENGINESPEEDSIG P0725 1207 — — X AT-92
A/T1STGRFNCTN P0731 1103 — — X AT-95
A/T2NDGRFNCTN P0732 1104 — — X AT-100
A/T3RDGRFNCTN P0733 1105 — — X AT-104
A/T4THGRFNCTN P0734 1106 — — X AT-108
TCCSOLENOID/CIRC P0740 1204 — — X AT-114
A/TTCCS/VFNCTN P0744 1107 — — X AT-118
L/PRESSSOL/CIRC P0745 1205 — — X AT-125
SFTSOLA/CIRC P0750 1108 — — X AT-129
SFTSOLB/CIRC P0755 1201 — — X AT-133
MAP/BARSWSOL/CIR P1105 1302 — — X EC-358
INT/VTIMCONT-B1 P1110 0805 — — X EC-367
*1: In Diagnostic Test Mode II (Self-diagnostic results). These numbers are controlled by NISSAN.
*2: These numbers are prescribed by SAE J2012.
*3: These are not displayed with GST.
*4: 1st trip DTC No. is the same as DTC No.
EC-62
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
HOW TO ERASE EMISSION-RELATED DIAGNOSTIC INFORMATION
How to erase DTC (With CONSULT-II)
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Note: If the diagnostic trouble code is not for A/T related items (see EC-4), skip steps 2 through 4.
1. If the ignition switch stays “ON” after repair work, be sure to turn ignition switch “OFF” once. Wait at least
5 seconds and then turn it “ON” (engine stopped) again.
2. Turn CONSULT-II “ON” and touch “A/T”.
3. Touch “SELF-DIAG RESULTS”.
4. Touch “ERASE”. [The DTC in the TCM (Transmission Control Module) will be erased.] And touch “BACK”
twice.
5. Touch “ENGINE”.
6. Touch “SELF-DIAG RESULTS”.
7. Touch “ERASE”. (The DTC in the ECM will be erased.)
IIf DTCs are displayed for both ECM and TCM (Transmission Control Module), they need to be erased
individually for both ECM and TCM (Transmission Control Module).
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The emission-related diagnostic information can be erased by selecting “ERASE” in the “SELF-DIAG
RESULTS” mode with CONSULT-II.
How to erase DTC (With GST)
Note: If the diagnostic trouble code is not for A/T related items (see page EC-4), skip step 2.
1. If the ignition switch stays “ON” after repair work, be sure to turn ignition switch “OFF” once. Wait at least
5 seconds and then turn it “ON” (engine stopped) again.
SEF966XA
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EC-63
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
(Cont’d)
2. Perform “SELF-DIAGNOSTIC PROCEDURE (Without CONSULT-II)” in AT section titled “TROUBLE
DIAGNOSIS”, “Self-diagnosis”. (The engine warm-up step can be skipped when performing the diagnosis
only to erase the DTC.)
3. Select Mode 4 with GST (Generic Scan Tool).
How to erase DTC (No Tools)
Note: If the diagnostic trouble code is not for A/T related items (see EC-4), skip step 2.
1. If the ignition switch stays “ON” after repair work, be sure to turn ignition switch “OFF” once. Wait at least
5 seconds and then turn it “ON” again.
2. Perform “SELF-DIAGNOSTIC PROCEDURE (Without CONSULT-II)” in AT section titled “TROUBLE
DIAGNOSIS”, “Self-diagnosis”. (The engine warm-up step can be skipped when performing the diagnosis
only to erase the DTC.)
3. Change the diagnostic test mode from Mode II to Mode I by turning the mode selector on the ECM. (See
EC-66.)
NOTE:
IIf the battery terminal is disconnected, the emission-related diagnostic information will be lost
within 24 hours.
IErasing the emission-related diagnostic information, using CONSULT-II or GST is easier and
quicker than switching the mode selector on the ECM.
The following data are cleared when the ECM memory is erased.
1. Diagnostic trouble codes
2. 1st trip diagnostic trouble codes
3. Freeze frame data
4. 1st trip freeze frame data
5. System readiness test (SRT) codes
6. Test values
7. Others
Actual work procedures are explained using a DTC as an example. Be careful so that not only the DTC, but
all of the data listed above, are cleared from the ECM memory during work procedures.
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EC-64
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL)
The malfunction indicator lamp is located on the instrument panel.
1.The malfunction indicator lamp will light up when the ignition
switch is turned ON without the engine running. This is a bulb
check.
IIf the malfunction indicator lamp does not light up, refer to EL
section WARNING LAMPS or see EC-535.
2.When the engine is started, the malfunction indicator lamp
should go off.
If the lamp remains on, the on board diagnostic system has
SEF217U
ON BOARD DIAGNOSTIC SYSTEM FUNCTION
The on board diagnostic system has the following four functions.
Diagnostic Test Mode I
1. BULB CHECK: This function checks the bulb for damage (blown, open circuit, etc.) of
the malfunction indicator lamp.
If the MIL does not come on, check MIL circuit and ECM test mode.
(See next page.)
2. MALFUNCTION
WARNING
: This is a usual driving condition. When a malfunction is detected twice
in two consecutive driving cycles (2 trip detection logic), the MIL will
light up to inform the driver that a malfunction has been detected.
The following malfunctions will light up or blink the MIL in the 1st trip.
I “Misfire (possible three way catalyst damage)”
I “Closed loop control”
I Fail-safe mode
Diagnostic Test Mode II
detected an engine system malfunction.
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3. SELF-DIAGNOSTIC
: This function allows DTCs and 1st trip DTCs to be read.
RESULTS
4. FRONT HEATED OXY-
GEN SENSOR MONI-
: This function allows the fuel mixture condition (lean or rich), monitored
by front heated oxygen sensor, to be read.
TOR
MIL Flashing without DTC
If the ECM is in Diagnostic Test Mode II, the MIL may flash when the engine is running. In this case, check
ECM test mode selector following “HOW TO SWITCH DIAGNOSTIC TEST MODES” on next page.
How to switch the diagnostic test (function) modes and details of the above functions are described later. (See
page EC-66.)
Ignition switch
in “ON” posi-
tion
Condition
Engine
stopped
Engine
running
Diagnostic
Test Mode I
BULB CHECK
MALFUNCTION
WARNING
Diagnostic
Test Mode II
SELF-DIAGNOSTIC
RESULTS
FRONT HEATED
OXYGEN SENSOR
MONITOR
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EC-65
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
HOW TO SWITCH DIAGNOSTIC TEST MODES
Turn ignition switch
“ON”. (Do not start
engine.)
H
Mode I — MALFUNCTION INDICA
E
TOR LAMP CHECK. Refer to EC-65.
MIL should come on.
OK
H
(Turn diagnostic test mode selector
on ECM fully clockwise.)
MIL should come off.
OK
H
Wait at least 2 seconds.
NG
F
NG
F
Check MIL circuit. (See
E
EC-535.)
Check whether ECM test
Yes
mode selector can be
turned counterclockwise.
E
E
Start engine.
Check MIL circuit. (See
EC-535.)
Check ECM fail-safe. (See
EC-98.)
EXIT
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NG
OK
H
No
G
NG
Repair harness or connector
E
Repair or replace ECM test mode selector.
E
Diagnostic Test Mode I
— MALFUNCTION WARNING
E
Repair harness or connectors.
E
OK
Diagnostic Test Mode II*1
E
OK
H
OK
F
— FRONT HEATED OXYGEN SENSOR
MONITOR (Left bank)
H
Turn diagnostic test mode selector on ECM
fully clockwise.
H
Wait at least 2 seconds.
H
(Turn diagnostic test mode selector
fully counterclockwise.)
H
DIAGNOSTIC TEST MODE II
— SELF-DIAGNOSTIC RESULTS
(ERASING ECM
MEMORY.)
H
H
Wait at least 2 seconds.
H
If the selector is turned fully
counterclockwise at this time,
the emission-related diagnostic
information will be erased from
the backup memory in the ECM.
H
Turn diagnostic test mode selector on ECM
fully counterclockwise.
H
Diagnostic Test Mode II
— FRONT HEATED OXYGEN SENSOR
MONITOR (Right bank)
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Start engine.
*1: If the battery is weak, front heated oxygen sensor monitor may not function
properly. Use this function after fully charging battery.
Turn diagnostic test mode selector on ECM
fully clockwise.
H
Wait at least 2 seconds.
H
Turn diagnostic test mode selector on ECM
fully counterclockwise.
The following emission-related diagnostic information is cleared
when the ECM memory is erased.
1. Diagnostic trouble codes
2. 1st trip diagnostic trouble codes
3. Freeze frame data
4. 1st trip freeze frame data
5. System readiness test (SRT) codes
6. Test values
7. Others
ISwitching the modes is not possible when the engine is
running.
IWhen ignition switch is turned off during diagnosis,
power to ECM will drop after approx. 5 seconds.
The diagnosis will automatically return to Diagnostic Test
Mode I.
ITurn back diagnostic test mode selector to the fully coun-
terclockwise position whenever vehicle is in use.
EC-66
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
DIAGNOSTIC TEST MODE I—BULB CHECK
In this mode, the MALFUNCTION INDICATOR LAMP on the instrument panel should stay ON. If it remains
OFF, check the bulb. (See the WARNING LAMPS in the EL section. Or see EC-535.)
EXIT
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DIAGNOSTIC TEST MODE I—MALFUNCTION WARNING
MALFUNCTION
INDICATOR LAMP
ONWhen the malfunction is detected or the ECM’s CPU is malfunctioning.
OFFNo malfunction
IThese Diagnostic Trouble Code Numbers are clarified in Diagnostic Test Mode II (SELF-DIAGNOSTIC
RESULTS).
Condition
DIAGNOSTIC TEST MODE II—SELF-DIAGNOSTIC RESULTS
In this mode, the DTC and 1st trip DTC are indicated by the number of blinks of the MALFUNCTION INDICATOR LAMP as shown below.
The DTC and 1st trip DTC are displayed at the same time. If the MIL does not illuminate in diagnostic test
mode 1 (Malfunction warning), all displayed items are 1st trip DTC’s. If only one code is displayed when the
MIL illuminates in diagnostic test mode II (SELF-DIAGNOSTIC RESULTS), it is a DTC; if two or more codes
are displayed, they may be either DTC’s or 1st trip DTC’s. DTC No. is same as that of 1st trip DTC. These
unidentified codes can be identified by using the consult or GST. A DTC will be used as an example for how
to read a code.
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Long (0.6 second) blinking indicates the two LH digits of number and short (0.3 second) blinking indicates the
two RH digits of number. For example, the malfunction indicator lamp blinks 10 times for 6 seconds (0.6 sec
x 10 times) and then it blinks three times for about 1 second (0.3 sec x 3 times). This indicates the DTC “1003”
and refers to the malfunction of the park/neutral position switch.
In this way, all the detected malfunctions are classified by their diagnostic trouble code numbers. The DTC
“0505” refers to no malfunction. (See DIAGNOSTIC TROUBLE CODE INDEX, refer to page EC-4.)
HOW TO ERASE DIAGNOSTIC TEST MODE II (Self-diagnostic results)
The diagnostic trouble code can be erased from the backup memory in the ECM when the diagnostic test mode
is changed from Diagnostic Test Mode II to Diagnostic Test Mode I. (Refer to “HOW TO SWITCH DIAGNOSTIC TEST MODES”.)
IIf the battery terminal is disconnected, the diagnostic trouble code will be lost from the backup
memory within 24 hours.
IBe careful not to erase the stored memory before starting trouble diagnoses.
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EC-67
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
IAGNOSTIC TEST MODE II—FRONT HEATED OXYGEN SENSOR MONITOR
In this mode, the MALFUNCTION INDICATOR LAMP displays the condition of the fuel mixture (lean or rich)
which is monitored by the front heated oxygen sensor.
EXIT
EXIT
MALFUNCTION INDICATOR LAMPFuel mixture condition in the exhaust gas
ONLean
OFFRich
*Remains ON or OFFAny conditionOpen loop control
*: Maintains conditions just before switching to open loop.
Air fuel ratio feedback control
condition
Closed loop control
To check the front heated oxygen sensor function, start engine in the Diagnostic Test Mode II and warm it up
until engine coolant temperature indicator points to the middle of the gauge.
Next run engine at about 2,000 rpm for about 2 minutes under no-load conditions. Then make sure that the
MALFUNCTION INDICATOR LAMP comes ON more than 5 times every 10 seconds when measured at 2,000
rpm under no-load.
If the battery is weak, front heated oxygen sensor monitor may not function properly. Use this function after fully charging battery.
How to switch monitored sensor from left bank to right bank or vice versa
IThe following procedure should be performed while the engine is running.
1. Turn diagnostic test mode selector on ECM fully clockwise.
2. Wait at least 2 seconds.
3. Turn diagnostic test mode selector on ECM fully counterclockwise.
SEF134M
EC-68
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
IVIS (Infiniti Vehicle Immobiliser System — NATS)
IIf the security indicator lights up with the ignition switch
in the “ON” position or “NATS MALFUNCTION” is displayed on “SELF-DIAG RESULTS” screen, perform selfdiagnostic results mode with CONSULT-II using NATS program card. Refer to “IVIS (Infiniti Vehicle Immobiliser System — NATS” in EL section.
IConfirm no self-diagnostic results of NATS is displayed
before touching “ERASE” in “SELF-DIAG RESULTS”
mode with CONSULT-II.
SEF543X
IWhen replacing ECM, initialization of NATS system and
registration of all NATS ignition key IDs must be carried
out with CONSULT-II using NATS program card.
Therefore, be sure to receive all keys from vehicle owner.
Regarding the procedures of NATS initialization and NATS
ignition key ID registration, refer to CONSULT-II operation
manual, NATS.
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OBD System Operation Chart
RELATIONSHIP BETWEEN MIL, 1ST TRIP DTC, DTC, AND DETECTABLE ITEMS
IWhen a malfunction is detected for the first time, the 1st trip DTC and the 1st trip freeze frame data are
stored in the ECM memory.
IWhen the same malfunction is detected in two consecutive trips, the DTC and the freeze frame data are
stored in the ECM memory, and the MIL will come on. For details, refer to “Two Trip Detection Logic” on
EC-49.
IThe MIL will go off after the vehicle is driven 3 times with no malfunction. The drive is counted only when
the recorded driving pattern is met (as stored in the ECM). If another malfunction occurs while counting,
the counter will reset.
IThe DTC and the freeze frame data will be stored until the vehicle is driven 40 times (driving pattern A)
without the same malfunction recurring (except for Misfire and Fuel injection system). For Misfire and Fuel
Injection System, the DTC and freeze frame data will be stored until the vehicle is driven 80 times (driving pattern C) without the same malfunction recurring. The “TIME” IN “SELF-DIAGNOSTIC RESULTS”
mode of CONSULT-II will count the number of times the vehicle is driven.
IThe 1st trip DTC is not displayed when the self-diagnosis results in “OK” for the 2nd trip.
SUMMARY CHART
ItemsFuel Injection SystemMisfireOther
MIL (goes off)3 (pattern B)3 (pattern B)3 (pattern B)
DTC, Freeze Frame Data (no
display)
1st Trip DTC (clear)1 (pattern C), *11 (pattern C), *11 (pattern B)
1st Trip Freeze Frame Data
(clear)
For details about patterns “B” and “C” under “Fuel Injection System” and “Misfire”, see EC-71.
For details about patterns “A” and “B” under “Other”, see EC-71.
*1: Clear timing is at the moment OK is detected.
*2: Clear timing is when the same malfunction is detected in the 2nd trip.
80 (pattern C)80 (pattern C)40 (pattern A)
*1, *2*1, *21 (pattern B)
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EC-69
IDX
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
OBD System Operation Chart (Cont’d)
RELATIONSHIP BETWEEN MIL, DTC, 1ST TRIP DTC AND DRIVING PATTERNS FOR
“MISFIRE” <EXHAUST QUALITY DETERIORATION>, “FUEL INJECTION SYSTEM”
EXIT
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*1: When the same malfunction is detected in two consecutive
trips, MIL will light up.
*2: MIL will go off after vehicle is driven 3 times (pattern B)
without any malfunctions.
*3: When the same malfunction is detected in two consecutive
trips, the DTC and the freeze frame data will be stored in
ECM.
*4: The DTC and the freeze frame data will not be displayed
any longer after vehicle is driven 80 times (pattern C) without the same malfunction.
(The DTC and the freeze frame data still remain in ECM.)
SEF392S
*5: When a malfunction is detected for the first time, the 1st
trip DTC and the 1st trip freeze frame data will be stored
in ECM.
*6: The 1st trip DTC and the 1st trip freeze frame data will be
cleared at the moment OK is detected.
*7: When the same malfunction is detected in the 2nd trip, the
1st trip freeze frame data will be cleared.
*8: 1st trip DTC will be cleared when vehicle is driven a time
(pattern C) without the same malfunction after DTC is
stored in ECM.
EC-70
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
OBD System Operation Chart (Cont’d)
EXPLANATION FOR DRIVING PATTERNS FOR “MISFIRE <EXHAUST QUALITY
DETERIORATION>”, “FUEL INJECTION SYSTEM”
<Driving pattern B>
Driving pattern B means the vehicle operation as follows:
All components and systems should be monitored at least once by the OBD system.
IThe B counter will reset when the malfunction is detected once regardless of the driving pattern.
IThe B counter will count up times driving pattern B is satisfied without the malfunction.
IThe MIL will go off when the B counter reaches 3. (*2 in “OBD SYSTEM OPERATION CHART”)
<Driving pattern C>
Driving pattern C means the vehicle operation as follows:
(1) The following conditions should be satisfied at the same time:
Engine speed: (Engine speed in the freeze frame data) ±375 rpm
Calculated load value: (Calculated load value in the freeze frame data) x (1±0.1) [%]
Engine coolant temperature (T) condition:
IWhen the freeze frame data shows lower than 70°C (158°F), “T” should be lower than 70°C (158°F).
IWhen the freeze frame data shows higher than or equal to 70°C (158°F), “T” should be higher than or
equal to 70°C (158°F).
Example:
If the stored freeze frame data is as follows:
To be satisfied with driving pattern C, the vehicle should run under the following conditions:
Engine speed: 475 - 1,225 rpm, Calculated load value: 27 - 33%, Engine coolant temperature: more
than 70°C (158°F)
IThe C counter will be cleared when the malfunction is detected regardless of (1).
IThe C counter will be counted up when (1) is satisfied without the same malfunction.
IThe DTC will not be displayed after C counter reaches 80.
IThe 1st trip DTC will be cleared when C counter is counted a time without the same malfunction after DTC
is stored in ECM.
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EC-71
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
OBD System Operation Chart (Cont’d)
RELATIONSHIP BETWEEN MIL, DTC, 1ST TRIP DTC AND DRIVING PATTERNS EXCEPT FOR
“MISFIRE” <EXHAUST QUALITY DETERIORATION>, “FUEL INJECTION SYSTEM”
EXIT
EXIT
*1: When the same malfunction is detected in two consecutive
trips, MIL will light up.
*2: MIL will go off after vehicle is driven 3 times (pattern B)
without any malfunctions.
*3: When the same malfunction is detected in two consecutive
trips, the DTC and the freeze frame data will be stored in
ECM.
*4: The DTC and the freeze frame data will not be displayed
any longer after vehicle is driven 40 times (pattern A) without the same malfunction.
(The DTC and the freeze frame data still remain in ECM.)
SEF393S
*5: When a malfunction is detected for the first time, the 1st
trip DTC and the 1st trip freeze frame data will be stored
in ECM.
*6: 1st trip DTC will be cleared after vehicle is driven a time
(pattern A) without the same malfunction.
*7: When the same malfunction is detected in the 2nd trip, the
1st trip freeze frame data will be cleared.
EC-72
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
OBD System Operation Chart (Cont’d)
EXPLANATION FOR DRIVING PATTERNS EXCEPT FOR “MISFIRE <EXHAUST QUALITY
DETERIORATION>”, “FUEL INJECTION SYSTEM”
<Driving pattern A>
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IThe A counter will be cleared when the malfunction is detected regardless of (1) - (4).
IThe A counter will be counted up when (1) - (4) are satisfied without the same malfunction.
IThe DTC will not be displayed after the A counter reaches 40.
<Driving pattern B>
Driving pattern B means the vehicle operation as follows:
All components and systems should be monitored at least once by the OBD system.
IThe B counter will be cleared when the malfunction is detected once regardless of the driving pattern.
IThe B counter will be counted up when driving pattern B is satisfied without any malfunctions.
IThe MIL will go off when the B counter reaches 3 (*2 in “OBD SYSTEM OPERATION CHART”).
AEC574
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EC-73
EL
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II
CONSULT-II INSPECTION PROCEDURE
1.Turn off ignition switch.
2.Connect “CONSULT-II” to data link connector which is located
beside the hood lock release handle.
SEF046TA
3.Turn on ignition switch.
4.Touch “START”.
EXIT
EXIT
PBR455D
5.Touch “ENGINE”.
PEF895K
6.Perform each diagnostic test mode according to each service
procedure.
For further information, see the CONSULT-II Operation
Manual.
SEF673X
EC-74
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
ENGINE CONTROL COMPONENT PARTS/CONTROL SYSTEMS APPLICATION
DIAGNOSTIC TEST MODE
SELF-DIAGNOSTIC
Item
Camshaft position sensorXXX
Mass air flow sensorXX
Engine coolant temperature sensorXXXX
Front heated oxygen sensorXXXX
Rear heated oxygen sensorXXXX
Vehicle speed sensorXXX
Throttle position sensorXXX
Fuel tank temperature sensorXXX
EVAP control system pressure sensorXX
Absolute pressure sensorXX
EGR temperature sensorXX
INPUT
ENGINE CONTROL COMPONENT PARTS
OUTPUT
X: Applicable
*1: This item includes 1st trip DTCs.
*2: This mode includes 1st trip freeze frame data or freeze frame data. The items appear on CONSULT-II screen in freeze frame
data mode only if a 1st trip DTC or DTC is detected. For details, refer to EC-51.
Intake air temperature sensorXX
Crankshaft position sensor (OBD)X
Knock sensorX
Ignition switch (start signal)X
Closed throttle position switchX
Closed throttle position switch (throttle
position sensor signal)
Air conditioner switchX
Park/Neutral position switchXX
Power steering oil pressure switchX
Air conditioner switchX
Battery voltageX
Ambient air temperature switchX
InjectorsXX
Power transistor (Ignition timing)
IACV-AAC valveXXXX
EVAP canister purge volume control valveXXXX
Air conditioner relayX
Fuel pump relayXXX
EGRC-solenoid valveXXX
Front heated oxygen sensor heaterXXX
Rear heated oxygen sensor heaterXXX
EVAP canister purge control solenoid valveXXX
EVAP canister vent control valveXXX
Vacuum cut valve bypass valveXXXX
MAP/BARO switch solenoid valveXXX
Calculated load valueXX
WORK
SUP-
PORT
RESULTS*1
X
(Ignition
signal)
FREEZE
FRAME
DATA*2
DATA
MONITOR
X
XX
ACTIVE
TEST
SRT STA-
DTC & SRT
CONFIRMATION
DTC
TUS
WORK
SUPPORT
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EC-75
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
FUNCTION
Diagnostic test modeFunction
Work support
Self-diagnostic results
Data monitorInput/Output data in the ECM can be read.
Active test
DTC & SRT confirmation
ECM part numbersECM part numbers can be read.
*1 The following emission-related diagnostic information is cleared when the ECM memory is erased.
1. Diagnostic trouble codes
2. 1st trip diagnostic trouble codes
3. Freeze frame data
4. 1st trip freeze frame data
5. System readiness test (SRT) codes
6. Test values
7. Others
This mode enables a technician to adjust some
devices faster and more accurately by following the
indications on the CONSULT-II unit.
Self-diagnostic results such as 1st trip DTC, DTCs
and 1st trip freeze frame data or freeze frame data
can be read and erased quickly.*1
Diagnostic Test Mode in which CONSULT-II drives
some actuators apart from the ECMs and also shifts
some parameters in a specified range.
The status of system monitoring tests and the selfdiagnosis status/result can be confirmed.
EXIT
EXIT
WORK SUPPORT MODE
WORK ITEMCONDITIONUSAGE
IACV-AAC/V ADJSET ENGINE SPEED AT THE SPECIFIED VALUE UNDER THE
FUEL PRESSURE RELEASEI FUEL PUMP WILL STOP BY TOUCHING “START” DURING
EVAP SYSTEM CLOSEOPEN THE VACUUM CUT VALVE BYPASS VALVE AND CLOSE
FOLLOWING CONDITIONS.
I ENGINE WARMED UP
I NO-LOAD
IDLING.
CRANK A FEW TIMES AFTER ENGINE STALLS.
THE EVAP CANISTER VENT CONTROL VALVE IN ORDER TO
MAKE THE EVAP SYSTEM CLOSE UNDER THE FOLLOWING
CONDITIONS.
I IGN SW “ON”
I ENGINE NOT RUNNING
I AMBIENT TEMPERATURE IS ABOVE 0°C (32°F).
I NO VACUUM AND NO HIGH PRESSURE IN EVAP SYSTEM
I TANK FUEL TEMP. IS MORE THAN 0°C (32°F).
I WITHIN 10 MINUTES AFTER STARTING “EVAP SYSTEM
CLOSE”
When adjusting ignition timing and idle
speed
When releasing fuel pressure from
fuel line
When detecting EVAP vapor leak
point of EVAP system
EC-76
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
SELF-DIAGNOSTIC MODE
DTC and 1st trip DTC
Regarding items of “DTC and 1st trip DTC”, refer to “DIAGNOSTIC TROUBLE CODE INDEX” (See
EC-4.).
Freeze frame data and 1st trip freeze frame data
Freeze frame data
item*1
DIAG TROUBLE
CODE
[PXXXX]
FUEL SYS-B1*2
FUEL SYS-B2*2
CAL/LD VALUE [%]I The calculated load value at the moment a malfunction is detected is displayed.
COOLANT TEMP
*1: The items are the same as those of 1st trip freeze frame data.
*2: Regarding model Y33, “-B1” indicates left bank and “-B2” indicates right bank.
2
] or [psi]
I Engine control component part/control system has a trouble code, it is displayed as “PXXXX”. [Refer to
“Alphabetical & P No. Index for DTC (EC-4).]
I “Fuel injection system status” at the moment a malfunction is detected is displayed.
I One mode in the following is displayed.
“MODE 2”: Open loop due to detected system malfunction
“MODE 3”: Open loop due to driving conditions (power enrichment, deceleration enrichment)
“MODE 4”: Closed loop - using heated oxygen sensor(s) as feedback for fuel control
“MODE 5”: Open loop - has not yet satisfied condition to go to closed loop
I The engine coolant temperature at the moment a malfunction is detected is displayed.
I “Short-term fuel trim” at the moment a malfunction is detected is displayed.
I The short-term fuel trim indicates dynamic or instantaneous feedback compensation to the base fuel
schedule.
I “Long-term fuel trim” at the moment a malfunction is detected is displayed.
I The long-term fuel trim indicates much more gradual feedback compensation to the base fuel schedule
than short-term fuel trim.
I The engine speed at the moment a malfunction is detected is displayed.
I The vehicle speed at the moment a malfunction is detected is displayed.
I The absolute pressure at the moment a malfunction is detected is displayed.
I The base fuel schedule at the moment a malfunction is detected is displayed.
I The intake air temperature at the moment a malfunction is detected is displayed.
Description
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EC-77
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
DATA MONITOR MODE
CONSULT-II (Cont’d)
EXIT
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Monitored item
[Unit]
CMPS⋅RPM
(POS) [rpm]
MAS AIR/FL SE [V]
COOLAN TEMP/S
[°C] or [°F]
FR O2 SEN-B1 [V]
FR O2 SEN-B2 [V]
RR O2 SEN-B1 [V]
RR O2 SEN-B2 [V]
FR O2 MNTR-B1
[RICH/LEAN]
FR O2 MNTR-B2
[RICH/LEAN]
RR O2 MNTR-B1
[RICH/LEAN]
RR O2 MNTR-B2
[RICH/LEAN]
VHCL SPEED SE
[km/h] or [mph]
BATTERY VOLT [V]
THRTL POS SEN [V]
THRTL/P SEN2 [V]
FUEL T/TMP SE [°C]
or [°F]
EGR TEMP SEN [V]
INT/A TEMP SE [°C]
or [°F]
NOTE:
Any monitored item that does not match the vehicle being diagnosed is deleted from the display automatically.
Regarding Y33 model, “-B1” indicates left bank and “-B2” indicates right bank.
ECM
input
signals
Main
signals
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DescriptionRemarks
I Indicates the engine speed computed
from the POS signal (1° signal) of the
crankshaft position sensor (POS).
I The signal voltage of the mass air flow
sensor is displayed.
I The engine coolant temperature (deter-
mined by the signal voltage of the engine
coolant temperature sensor) is displayed.
I The signal voltage of the front heated
oxygen sensor is displayed.
I The signal voltage of the rear heated
oxygen sensor is displayed.
I Display of front heated oxygen sensor
signal during air-fuel ratio feedback control:
RICH ... means the mixture became
“rich”, and control is being affected
toward a leaner mixture.
LEAN ... means the mixture became
“lean”, and control is being affected
toward a rich mixture.
I Display of rear heated oxygen sensor
signal during air-fuel ratio feedback control:
RICH ... means the amount of oxygen
after three way catalyst is relatively large.
LEAN ... means the amount of oxygen
after three way catalyst is relatively
small.
I The vehicle speed computed from the
vehicle speed sensor signal is displayed.
I The power supply voltage of ECM is dis-
played.
I The throttle position sensor signal volt-
age is displayed.
I Secondary throttle position sensor signal
voltage is displayed.
I The fuel tank temperature judged from
the tank fuel temperature sensor signal
voltage is displayed.
I The signal voltage of the EGR tempera-
ture sensor is displayed.
I The intake air temperature determined by
the signal voltage of the intake air temperature sensor is indicated.
I When the engine is stopped, a certain
value is indicated.
I When the engine coolant temperature
sensor is open or short-circuited, ECM
enters fail-safe mode. The engine coolant
temperature determined by the ECM is
displayed.
I After turning ON the ignition switch,
“RICH” is displayed until air-fuel mixture
ratio feedback control begins.
I When the air-fuel ratio feedback is
clamped, the value just before the clamping is displayed continuously.
I When the engine is stopped, a certain
value is indicated.
EC-78
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
EXIT
EXIT
Monitored item
[Unit]
START SIGNAL
[ON/OFF]
CLSD THL/P SW
[ON/OFF]
CLSD THL POS
[ON/OFF]
AIR COND SIG
[ON/OFF]
P/N POSI SW
[ON/OFF]
PW/ST SIGNAL
[ON/OFF]
LOAD SIGNAL
[ON/OFF]
AMB TEMP SW
[ON/OFF]
IGNITION SW
[ON/OFF]
A/C PRESS SW
[ON/OFF]
INJ PULSE-B1 [msec]
INJ PULSE-B2 [msec]
B/FUEL SCHDL
[msec]
IGN TIMING [BTDC]
IACV-AAC/V [step]
PURG VOL C/V [step]
A/F ALPHA-B1 [%]I The mean value of the air-fuel ratio feedA/F ALPHA-B2 [%]
EVAP SYS PRES [V]I The signal voltage of EVAP control sys-
ECM
input
signals
Main
signals
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DescriptionRemarks
I Indicates [ON/OFF] condition from the
starter signal.
I Indicates mechanical contact [ON/OFF]
condition from the closed throttle position
switch signal.
I Indicates idle position [ON/OFF] com-
puted by ECM according to the throttle
position sensor signal.
I Indicates [ON/OFF] condition of the air
conditioner switch as determined by the
air conditioner signal.
I Indicates [ON/OFF] condition from the
park/neutral position switch signal.
I [ON/OFF] condition of the power steering
oil pressure switch determined by the
power steering oil pressure signal is indicated.
I Indicate [ON/OFF] condition from the
electrical load signal and/or lighting
switch.
ON ... rear defogger is operating.
OFF ... rear defogger is not operating.
I Indicate [ON/OFF] condition from the
ambient temperature signal.
ON ... When the ambient temperature is
lower than specified value.
OFF ... When the ambient temperature is
higher than specified value.
I Indicates [ON/OFF] condition from igni-
tion switch.
I Indicate [ON/OFF] condition of air condi-
tioner pressure switch signal.
ON ... A/C pressure is higher than specified value.
OFF ... A/C pressure is lower than specified value.
I Indicates the actual fuel injection pulse
width compensated by ECM according to
the input signals.
I “Base fuel schedule” indicates the fuel
injection pulse width programmed into
ECM, prior to any learned on board correction.
I Indicates the ignition timing computed by
ECM according to the input signals.
I Indicates the IACV-AAC valve control
value computed by ECM according to the
input signals.
I Indicates the EVAP canister purge vol-
ume control valve computed by the ECM
according to the input signals.
I The opening becomes larger as the
value increases.
back correction factor per cycle is indicated.
tem pressure sensor is displayed.
I After starting the engine, [OFF] is dis-
played regardless of the starter signal.
I When the engine is stopped, a certain
computed value is indicated.
I When the engine is stopped, a certain
value is indicated.
I When the engine is stopped, a certain
value is indicated.
I This data also includes the data for the
air-fuel ratio learning control.
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EC-79
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
EXIT
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Monitored item
[Unit]
AIR COND RLY
[ON/OFF]
FUEL PUMP RLY
[ON/OFF]
INT/V SOL-B1
INT/V SOL-B2
[ON/OFF]
INT/V TIM-B1
INT/V TIM-B2
[deg]
COOLING FAN
[HI/OFF]
EGRC SOL/V
[ON/OFF] (flow/cut)
VENT CONT/V
[ON/OFF]
FR O2 HTR-B1
[ON/OFF]
FR O2 HTR-B2
[ON/OFF]
RR O2 HTR-B1
[ON/OFF]
RR O2 HTR-B2
[ON/OFF]
VC/V BYPASS/V
[ON/OFF]
PURG CONT S/V
[ON/OFF]
CAL/LD VALUE [%]I “Calculated load value” indicates the
ABSOL TH⋅P/S [%]I “Absolute throttle position sensor” indi-
MASS AIRFLOW
[g⋅m/s]
FPCM DR VOLT [V]I The voltage between fuel pump and
ECM
input
signals
Main
signals
DescriptionRemarks
I The air conditioner relay control condition
(determined by ECM according to the
input signal) is indicated.
I Indicates the fuel pump relay control con-
dition determined by ECM according to
the input signals.
I The control condition of the intake valve
timing control solenoid valve is indicated.
ON ... Intake valve timing control is operating.
OFF ... Intake valve timing control is not
operating.
I Indicate [deg] of intake camshaft
advanced angle.
I The control condition of the cooling fan
(determined by ECM according to the
input signal) is indicated.
HI ... High speed operation
OFF ... Stop
I The control condition of the EGRC-sole-
noid valve (determined by ECM according to the input signal) is indicated.
I OFF ... EGR is cut-off
ON ... EGR is operational
I The control condition of the EVAP canis-
ter vent control valve (determined by
ECM according to the input signal) is
indicated.
I ON ... Closed
OFF ... Open
I Indicates [ON/OFF] condition of front
heated oxygen sensor’s heater determined by ECM according to the input
signals.
I Indicates [ON/OFF] condition of rear
heated oxygen sensor’s heater determined by ECM according to the input
signals.
I The control condition of the vacuum cut
valve bypass valve (determined by ECM
according to the input signal) is indicated.
I ON ... Open
OFF ... Closed
I The control condition of the EVAP canis-
ter purge control solenoid valve (computed by the engine control module
according to the input signals) is indicated.
I ON ... Canister purge is operational
OFF ... Canister purge operation is cutoff
value of the current airflow divided by
peak airflow.
cates the throttle opening computed by
ECM according to the signal voltage of
the throttle position sensor.
I Indicates the mass airflow computed by
ECM according to the signal voltage of
the mass airflow sensor.
FPCM is displayed.
EC-80
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
EXIT
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Monitored item
[Unit]
FPCM [LOW/HI]I The control condition of the fuel pump
MAP/BARO SW/V
[MAP/BARO]
ABSOL PRES/SE [V]I The signal voltage of the absolute pres-
VOLTAGE
[V]
PULSE
[msec] or [Hz] or [%]
ECM
input
signals
Main
signals
DescriptionRemarks
control module (FPCM) (determined by
ECM according to the input signal) is
indicated.
LOW ... Low amount of fuel flow
HI ... High amount of fuel flow
I The control condition of the MAP/BARO
switch solenoid valve (determined by
ECM according to the input signal) is
indicated.
MAP ... Intake manifold absolute pressure
BARO ... Barometric pressure
sure sensor is displayed.
I Voltage measured by the voltage probe.
I Pulse width, frequency or duty cycle
measured by the pulse probe.
I Only “#” is displayed if item is unable to
be measured.
I Figures with “#”s are temporary ones.
They are the same figures as an actual
piece of data which was just previously
measured.
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EC-81
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
ACTIVE TEST MODE
TEST ITEMCONDITIONJUDGEMENTCHECK ITEM (REMEDY)
I Engine: Return to the original trouble
FUEL INJECTION
IACV-AAC/V
OPENING
ENG COOLANT
TEMP
IGNITION TIMING
POWER BALANCE
COOLING FAN
FUEL PUMP RELAY
EGRC SOLENOID
VALVE
VALVE TIMING SOL
SELF-LEARNING
CONT
PURG VOL CONT/V
FUEL/T TEMP SEN I Change the fuel tank temperature using CONSULT-II.
VENT CONT/V
VC/V BYPASS/V
PURG CONT S/V
MAP/BARO SW/V
FPCM
condition
I Change the amount of fuel injection
using CONSULT-II.
I Engine: After warming up, idle the
engine.
I Change the IACV-AAC valve opening
step using CONSULT-II.
I Engine: Return to the original trouble
condition
I Change the engine coolant
temperature using CONSULT-II.
I Engine: Return to the original trouble
condition
I Timing light: Set
I Retard the ignition timing using
CONSULT-II.
I Engine: After warming up, idle the
engine.
I A/C switch “OFF”
I Shift lever “N”
I Cut off each injector signal one at a
time using CONSULT-II.
I Ignition switch: ON
I Turn the cooling fan “ON” and “OFF”
using CONSULT-II.
I Ignition switch: ON (Engine stopped)
I Turn the fuel pump relay “ON” and
“OFF” using CONSULT-II and listen to
operating sound.
I Ignition switch: ON
I Turn solenoid valve “ON” and “OFF”
with CONSULT-II and listen to
operating sound.
I Ignition switch: ON
I Turn solenoid valve “ON” and “OFF”
with CONSULT-II and listen to
operating sound.
I In this test, the coefficient of self-learning control mixture ratio returns to the original coefficient by touching “CLEAR” on the
screen.
I Engine: After warming up, run engine
at 1,500 rpm.
I Change the EVAP canister purge
volume control valve opening step
using CONSULT-II.
I Ignition switch: ON (Engine stopped)
I Turn the VENT CONT/V “ON and
OFF” with CONSULT-II and listen for
operating sound.
I Ignition switch: ON (Engine stopped)
I Turn the VC/V BYPASS/V “ON and
OFF” with CONSULT-II and listen for
operating sound.
I Engine: Run engine at 2,000 rpm.
I Turn the EVAP canister purge control
solenoid valve “ON” and “OFF” using
CONSULT-II and listen for operating
sound.
I Ignition switch: ON
(Engine stopped)
I Turn the MAP/BARO switch solenoid
valve between “MAP” and “BARO”
using CONSULT-II and listen for
operating sound.
I Ignition switch: ON
I Select “LOW” and “HI” with
CONSULT-II and check that “FPCM
D/R VOLT” of CONSULT-II changes.
If trouble symptom disappears, see
CHECK ITEM.
Engine speed changes according to the
opening percent.
If trouble symptom disappears, see
CHECK ITEM.
If trouble symptom disappears, see
CHECK ITEM.
Engine runs rough or dies.
Cooling fan moves and stops.
Fuel pump relay makes the operating
sound.
Solenoid valve makes an operating
sound.
Solenoid valve makes an operating
sound.
Engine speed changes according to the
opening step.
Solenoid valve makes an operating
sound.
Solenoid valve makes an operating
sound.
EVAP canister purge control solenoid
valve makes an operating sound.
Check vacuum signal for EVAP canister
purge control valve.
VC ON ... Vacuum exists.
VC OFF ... Vacuum does not exist.
MAP/BARO switch solenoid valve makes
an operating sound.
“FPCM D/R VOLT” of CONSULT-II
changes as follows;
LOW ... Approx. 4.7V
HI ... Approx. 0.4V
I Harness and connector
I Fuel injectors
I Front heated oxygen sensor
I Harness and connector
I IACV-AAC valve
I Harness and connector
I Engine coolant temperature sensor
I Fuel injectors
I Adjust ignition timing (by moving
camshaft position sensor)
I Harness and connector
I Compression
I Injectors
I Ignition coil with power transistor
I Spark plugs
I Harness and connector
I Cooling fan motor
I Harness and connector
I Fuel pump relay
I Harness and connector
I EGRC-solenoid valve
I Harness and connector
I Intake valve timing control solenoid
valve
I Harness and connector
I EVAP canister purge volume control
valve
I Harness or connector
I EVAP canister vent control valve
I Harness or connector
I Vacuum cut bypass valve
I Harness and connector
I EVAP canister purge control solenoid
valve
I Vacuum hose
I Harness and connector
I MAP/BARO switch solenoid valve
I Harness and connector
I FPCM
EXIT
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EC-82
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
DTC & SRT CONFIRMATION MODE
SRT STATUS mode
For details, refer to “SYSTEM READINESS TEST (SRT) CODE”, EC-51.
SRT Work Support Mode
This mode enables a technician to drive a vehicle to set the SRT while monitoring the SRT status.
REAL TIME DIAGNOSIS IN DATA MONITOR MODE
(Recording Vehicle Data)
CONSULT-II has two kinds of triggers and they can be selected by
touching “SETTING” in “DATA MONITOR” mode.
1)“AUTO TRIG” (Automatic trigger):
IThe malfunction will be identified on the CONSULT-II screen
inreal time.
In other words, DTC/1st trip DTC and malfunction item will be
displayed if the malfunction is detected by ECM.
At the moment a malfunction is detected by ECM, “MONITOR”
in “DATA MONITOR” screen is changed to “Recording Data
...xx%” as shown at left, and the data after the malfunction
detection is recorded. Then when the percentage reached
100%, “REAL-TIME DIAG” screen is displayed. If “STOP” is
touched on the screen during “ Recording Data ... xx%”,
“REAL-TIME DIAG” screen is also displayed.
The recording time after the malfunction detection and the
recording speed can be changed by “TRIGGER POINT” and
“Recording Speed”. Refer to CONSULT-II OPERATION
MANUAL.
2)“MANU TRIG” (Manual trigger):
IDTC/1st trip DTC and malfunction item will not be displayed
automatically on CONSULT-II screen even though a malfunction is detected by ECM.
DATA MONITOR can be performed continuously even though
a malfunction is detected.
Use these triggers as follows:
1)“AUTO TRIG”
IWhile trying to detect the DTC/1st trip DTC by performing the
“DTC Confirmation Procedure”, be sure to select to “DATA
MONITOR (AUTO TRIG)” mode. You can confirm the malfunction at the moment it is detected.
IWhile narrowing down the possible causes, CONSULT-II
should be set in “DATAMONITOR (AUTO TRIG)” mode, especially in case the incident is intermittent.
When you are inspecting the circuit by gently shaking (or twisting) the suspicious connectors, components and harness in
the “DTC Confirmation Procedure”, the moment a malfunction
is found the DTC/1st trip DTC will be displayed. (Refer to GI
Section, “Incident Simulation Tests”.)
2)“MANU TRIG”
IIf the malfunction is displayed as soon as “DATA MONITOR”
is selected, reset CONSULT-II to “MANU TRIG”. By selecting
“MANU TRIG” you can monitor and store the data. The data
can be utilized for further diagnosis, such as a comparison with
the value for the normal operating condition.
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EC-84
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II (Cont’d)
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SEF139P
SEF720X
Generic Scan Tool (GST)
DESCRIPTION
Generic Scan Tool (OBDII scan tool) complying with SAE J1978
has 8 different functions explained on the next page.
ISO9141 is used as the protocol.
The name “GST” or “Generic Scan Tool” is used in this service
manual.
GST INSPECTION PROCEDURE
1.Turn off ignition switch.
2.Connect “GST” to data link connector which is located under
LH dash panel near the hood lock release handle.
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EC-85
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Generic Scan Tool (GST) (Cont’d)
3.Turn ON ignition switch.
4.Enter the program according to instruction on the screen or in
the operation manual.
(*: Regarding GST screens in this section, sample screens are
shown.)
SEF398S
5.Perform each diagnostic mode according to each service procedure.
For further information, see the GST Operation Manual of the
tool maker.
EXIT
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FUNCTION
Diagnostic test modeFunction
MODE 1READINESS TESTS
MODE 2(FREEZE DATA)
MODE 3DTCs
MODE 4CLEAR DIAG INFO
MODE 6(ON BOARD TESTS)
MODE 7(ON BOARD TESTS)
MODE 8—
MODE 9(CALIBRATION ID)
SEF416S
This mode gains access to current emission-related data values, including analog
inputs and outputs, digital inputs and outputs, and system status information.
This mode gains access to emission-related data value which were stored by ECM
during the freeze frame. [For details, refer to “Freeze Frame Data” (EC-77).]
This mode gains access to emission-related power train trouble codes which were
stored by ECM.
This mode can clear all emission-related diagnostic information. This includes:
I Clear number of diagnostic trouble codes (MODE 1)
I Clear diagnostic trouble codes (MODE 3)
I Clear trouble code for freeze frame data (MODE 1)
I Clear freeze frame data (MODE 2)
I Reset status of system monitoring test (MODE 1)
I Clear on board monitoring test results (MODE 6 and 7)
This mode accesses the results of on board diagnostic monitoring tests of specific
components/systems that are not continuously monitored.
This mode enables the off board test drive to obtain test results for emission-related
powertrain components/systems that are continuously monitored during normal driving conditions.
This mode can close EVAP system in ignition switch “ON” position (Engine stopped).
When this mode is performed, the following parts can be opened or closed.
I EVAP canister vent control open
I Vacuum cut valve bypass valve closed
In the following conditions, this mode cannot function.
I Low ambient temperature
I Low battery voltage
I Engine running
I Ignition switch “OFF”
I Low fuel temperature
I Too much pressure is applied to EVAP system
This mode enables the off-board test device to request specific vehicle information
such as Vehicle Identification Number (VIN) and Calibration IDs.
EC-86
TROUBLE DIAGNOSIS — Introduction
Introduction
The engine has an ECM to control major systems such as fuel
control, ignition control, idle air control system, etc. The ECM
accepts input signals from sensors and instantly drives actuators.
It is essential that both input and output signals are proper and
stable. At the same time, it is important that there are no problems
such as vacuum leaks, fouled spark plugs, or other problems with
the engine.
It is much more difficult to diagnose a problem that occurs intermittently rather than continuously. Most intermittent problems are
MEF036D
SEF233G
caused by poor electric connections or improper wiring. In this
case, careful checking of suspected circuits may help prevent the
replacement of good parts.
A visual check only may not find the cause of the problems. A road
test with CONSULT-II (or GST) or a circuit tester connected should
be performed. Follow the “Work Flow” on EC-89.
Before undertaking actual checks, take just a few minutes to talk
with a customer who approaches with a driveability complaint. The
customer can supply good information about such problems, especially intermittent ones. Find out what symptoms are present and
under what conditions they occur.A“Diagnostic Worksheet” like the
example below should be used.
Start your diagnosis by looking for “conventional” problems first.
This will help troubleshoot driveability problems on an electronically
controlled engine vehicle.
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SEF234G
SEF907L
Diagnostic Worksheet
There are many operating conditions that lead to the malfunctions
of engine components. A good knowledge of such conditions can
make troubleshooting faster and more accurate.
In general, each customer may feel differently about a given problem. It is important to fully understand the symptoms or conditions
for a customer complaint.
Utilize a diagnostic worksheet like the one shown below in order to
organize all the information for troubleshooting.
Some conditions may cause the malfunction indicator lamp to
come on steady or blink and DTC to be detected. Examples:
IVehicle ran out of fuel, which caused engine misfire.
IFuel filler cap was left off or incorrectly screwed on, allowing
fuel to evaporate into the atmosphere [for models with EVAP
(SMALL LEAK)] diagnosis.
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EC-87
TROUBLE DIAGNOSIS — Introduction
Diagnostic Worksheet (Cont’d)
WORKSHEET SAMPLE
Customer name MR/MSModel & YearVIN
Engine #Trans.Mileage
Incident DateManuf. DateIn Service Date
Fuel and fuel filler cap
l Startability
l Idling
Symptoms
l Driveability
l Engine stall
Incident occurrence
Frequencyl All the timel Under certain conditionsl Sometimes
Weather conditionsl Not affected
l Vehicle ran out of fuel causing misfire.
l Fuel filler cap was left off or incorrectly screwed on.
l Impossible to startl No combustionl Partial combustion
l Partial combustion affected by throttle position
l Partial combustion NOT affected by throttle position
l Possible but hard to startl Others []
l No fast idlel Unstablel High idlel Low idle
l Others []
l Stumblel Surgel Knockl Lack of power
l Intake backfirel Exhaust backfire
l Others []
l At the time of startl While idling
l While acceleratingl While decelerating
l Just after stoppingl While loading
l Just after deliveryl Recently
l In the morningl At nightl In the daytime
l Coldl During warm-upl After warm-up
EXIT
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Engine conditions
Road conditionsl In townl In suburbsl Highwayl Off road (up/down)
Driving conditions
Malfunction indicator lampl Turned onl Not turned on
Engine speed
l Not affected
l At startingl While idlingl At racing
l While acceleratingl While cruising
l While deceleratingl While turning (RH/LH)
Vehicle speed
EC-88
TROUBLE DIAGNOSIS — Work Flow
Work Flow
CHECK IN
H
CHECK INCIDENT CONDITIONS.
Listen to customer complaints. (Get symptoms.)
.................................................
STEP I
GI
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CHECK DTC and FREEZE FRAME DATA.
Check and PRINT OUT (write down), (1st trip) Diagnostic Trouble Code (DTC) and
Freeze Frame Data (Pre-check). Then clear. Paste it in repair order sheet.
If DTC is not available even if MIL lights up, check ECM fail-safe. (Refer to EC-98.)
Also check related service bulletins for information.
Symptoms collectedNo symptoms, except MIL
Verify the symptom by driving in the condition the customer described.
Normal Code
(at STEP II)
INCIDENT INFORMATION
Verify the (1st trip) DTC by performing the “DTC CONFIRMATION PROCEDURE”.
Choose the appropriate action.
E
Malfunction Code (at STEP II or IV)Normal Code (at both STEP II and IV)
Confirm that the incident is completely fixed by performing BASIC INSPECTION and
DTC CONFIRMATION PROCEDURE (or OVERALL FUNCTION CHECK).
Then, erase the unnecessary (already fixed) DTCs in ECM and TCM (Transmission
Control Module).
If completion of SRT is needed, drive the vehicle
under the specific pattern. Refer to EC-56.
H
H
Malfunction Code
(at STEP II)
H
Perform inspections according to Symptom Matrix
Chart.
*1: If the incident cannot be duplicated, see “TROUBLE DIAGNOSIS FOR INTERMITTENT INCIDENT”, EC-117.
*2: If the on board diagnostic system cannot be performed, check main power supply and ground circuit (See TROUBLE
DIAGNOSIS FOR POWER SUPPLY, EC-118).
*3: If time data of “SELF-DIAG RESULTS” is other than “0” or “1t” refer to “TROUBLE DIAGNOSIS FOR
INTERMITTENT”, EC-117.
*4: If the malfunction part cannot be found, refer to “TROUBLE DIAGNOSIS FOR INTERMITTENT INCIDENT”, EC-117.
EC-89
IDX
STEPDESCRIPTION
STEP I
STEP II
STEP III
STEP IV
STEP V
STEP VI
STEP VII
Get detailed information about the conditions and the environment when the incident/symptom occurred using the
“DIAGNOSTIC WORK SHEET”, EC-87.
Before confirming the concern, check and write down (print out using CONSULT-II or Generic Scan Tool) the Diagnostic Trouble Code (DTC) and the (1st trip) freeze frame data, then erase the code and the data. (Refer to
EC-63.) The (1st trip) DTC and the (1st trip) freeze frame data can be used when duplicating the incident at STEP
III&IV.
Study the relationship between the cause, specified by (1st trip) DTC, and the symptom described by the customer.
(The “Symptom Matrix Chart” will be useful. See page EC-99.)
Also check related service bulletins for information.
Try to confirm the symptom and under what conditions the incident occurs.
The “DIAGNOSTIC WORK SHEET” and the freeze frame data are useful to verify the incident. Connect CONSULT-II to the vehicle in DATAMONITOR (AUTO TRIG) mode and check real time diagnosis results.
If the incident cannot be verified, perform INCIDENT SIMULATION TESTS. (Refer to GI section.)
If the malfunction code is detected, skip STEP IV and perform STEP V.
Try to detect the (1st trip) Diagnostic Trouble Code by driving in (or performing) the “DTC CONFIRMATION PROCEDURE”. Check and read the (1st trip) DTC and (1st trip) freeze frame data by using CONSULT-II or Generic
Scan Tool.
During the (1st trip) DTC verification, be sure to connect CONSULT-II to the vehicle in DATA MONITOR (AUTO
TRIG) mode and check real time diagnosis results.
If the incident cannot be verified, perform INCIDENT SIMULATION TESTS. (Refer to GI section.)
In case the “DTC CONFIRMATION PROCEDURE” is not available, perform the “OVERALL FUNCTION CHECK”
instead. The (1st trip) DTC cannot be displayed by this check, however, this simplified “check” is an effective alternative.
The “NG” result of the “OVERALL FUNCTION CHECK” is the same as the (1st trip) DTC detection.
Take the appropriate action based on the results of STEP I through IV.
If the malfunction code is indicated, proceed to TROUBLE DIAGNOSIS FOR DTC PXXXX.
If the normal code is indicated, proceed to the BASIC INSPECTION on next page. Then perform inspections
according to the Symptom Matrix Chart. (Refer to EC-99.)
Identify where to begin diagnosis based on the relationship study between symptom and possible causes. Inspect
the system for mechanical binding, loose connectors or wiring damage using (tracing) “Harness Layouts”.
Gently shake the related connectors, components or wiring harness with CONSULT-II set in “DATA MONITOR
(AUTO TRIG)” mode.
Check the voltage of the related ECM terminals or monitor the output data from the related sensors with CONSULT-II. Refer to EC-102.
The “DIAGNOSTIC PROCEDURE” in EC section contains a description based on open circuit inspection. A short
circuit inspection is also required for the circuit check in the DIAGNOSTIC PROCEDURE. For details, refer to GI
section (“HOW TO PERFORM EFFICIENT DIAGNOSIS FOR AN ELECTRICAL INCIDENT”, “Circuit Inspection”).
Repair or replace the malfunction parts.
Once you have repaired the circuit or replaced a component, you need to run the engine in the same conditions
and circumstances which resulted in the customer’s initial complaint.
Perform the “DTC CONFIRMATION PROCEDURE” and confirm the normal code (Diagnostic trouble code No.
P0000 or 0505) is detected. If the incident is still detected in the final check, perform STEP VI by using a different
method from the previous one.
Before returning the vehicle to the customer, be sure to erase the unnecessary (already fixed) (1st trip) DTC in
ECM and TCM (Transmission Control Module). (Refer to EC-63.)
TROUBLE DIAGNOSIS — Work Flow
Description for Work Flow
EXIT
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EC-90
TROUBLE DIAGNOSIS — Basic Inspection
Basic Inspection
Precaution:
Perform Basic Inspection without electrical or mechanical
loads applied;
IHeadlamp switch is OFF,
IAir conditioner switch is OFF,
IRear window defogger switch is OFF,
ISteering wheel is in the straight-ahead position, etc.
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SEF142I
SEF046TA
SEF960X
BEFORE STARTING
1. Check service records for recent
repairs of related problems, or the current need for scheduled maintenance.
2. Open engine hood and check the following:
I Harness connectors for improper con-
nections
I Vacuum hoses for splits, kinks, or
improper connections
I Wiring for improper connections,
pinches, or cuts
H
CONNECT CONSULT-II TO THE
VEHICLE.
Connect “CONSULT-II” to the data link
connector and select “ENGINE” from the
menu. (Refer to page EC-74.)
H
THROTTLE OPENER INSPECTION
1. Start engine and let it idle.
2. Confirm the throttle drum becomes free
from the rod of the throttle opener.
NG
Refer to “INSPECTION”,
E
“Throttle Opener”, EC-39.
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OK
H
CHECK FI CAM.
Warm up engine to normal operating temperature and make sure there is clearance
between FI cam and roller (pin).
OK
H
q
A
(Go to next page.)
EC-91
NG
Check FI cam, refer to
E
EC-40.
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TROUBLE DIAGNOSIS — Basic Inspection
Basic Inspection (Cont’d)
q
A
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SEF263Y
SEF212U
SEF043T
H
CHECK IGNITION TIMING.
1. Warm up engine to normal
operating temperature.
2. Select “IACV-AAC/V ADJ”
in “WORK SUPPORT” mode.
3. Touch “START”.
4. Check ignition timing at idle
using timing light.
1. Warm up engine to normal
operating temperature.
2. Stop engine and disconnect
throttle position sensor harness
connector.
3. Start engine.
4. Check ignition timing at idle
using timing light.
Ignition timing:
15°±2° BTDC
OK
H
CHECK BASE IDLE SPEED.
1. Select “IACV-AAC/V ADJ” in
“WORK SUPPORT” mode.
2. When touching “START”, does
engine speed fall to
600±50 rpm
(in “P” or “N” position)?
--------------------------------------------------------------------------------------------------------------------------------------OR-------------------------------------------------------------------------------------------------------------------------------------Does engine run at
600±50 rpm
(in “P” or “N” position)?
NG
Adjust ignition timing by
E
turning camshaft position
sensor. Refer to EC-42.
NG
Adjust base idle speed by
E
turning idle speed adjusting screw.
Refer to “Idle Speed/
Ignition Timing/Idle Mixture
Ratio Adjustment” in
EC-42.
SEF263Y
SEF115T
OK
H
q
(Go to next page.)
B
EC-92
TROUBLE DIAGNOSIS — Basic Inspection
Basic Inspection (Cont’d)
q
B
EXIT
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SEF793W
SEF397X
SEF402W
SEF800W
H
CHECK CLOSED THROTTLE POSITION
SWITCH IDLE POSITION. (Check throttle
position sensor idle position.)
I Always check ignition timing and base idle
speed before performing the followings.
1. Warm up engine to normal operating temperature.
2. Check FI cam, refer to procedure
3. Stop engine.
4. Remove the vacuum hose connected to the
throttle opener.
5. Connect suitable vacuum hose to the vacuum
pump and the throttle opener as shown in the
figure.
6. Apply vacuum [more than −40.0 kPa (−300
mmHg, −11.81 inHg)] until the throttle drum
become free from the rod of the throttle
opener. During the TPS adjustment, the
vacuum should be applied (Until step
7. Turn ignition switch “ON”.
8. Select “DATAMONITOR” mode with
CONSULT-II.
9. Select “CLSD THL/P SW” from the
menu.
10. Read “CLSD THL/P SW” signal
I Insert a 0.2 mm (0.008 in) and 0.3 mm (0.012
in) feeler gauge alternately between the
throttle adjust screw (TAS) and throttle drum
as shown in the figure and check the signal.
“CLSD THL/P SW” signal should remain
“ON” while inserting 0.2 mm (0.008 in) feeler
gauge.
“CLSD THL/P SW” signal should remain
“OFF” while inserting 0.3 mm (0.012 in)
feeler gauge.
Stop engine, release vacuum then remove the
vacuum hose and handy vacuum pump from
the throttle opener. Reinstall the original
vacuum hose to the throttle opener securely.
H
CHECK TARGET IDLE SPEED.
Read the engine idle speed in “DATA
MONITOR” mode with CONSULT-II.
After this inspection, unnecessary diagnostic trouble code No. might be displayed.
I Erase the stored memory in ECM
and TCM (Transmission Control
Module).
Refer to “ON BOARD DIAGNOSTIC
SYSTEM DESCRIPTION” (EC-63)
and “HOW TO ERASE DTC” in AT
section.
I Erase the store memory in ABS/TCS
control unit. Refer to “TROUBLE
DIAGNOSIS FOR ABS/TCS C/U
SIGNAL”, EC-499 or refer to
(“TROUBLE DIAGNOSIS”, HOW TO
ERASE SELF-DIAGNOSTIC
RESULTS”) in BR section.
NG
Adjust idle speed. Refer to
E
“Idle Speed/Ignition Timing/Idle
Mixture Ratio Adjustment” in
EC-42.
H
INSPECTION END
EC-94
TROUBLE DIAGNOSIS — Basic Inspection
Basic Inspection (Cont’d)
THROTTLE POSITION SENSOR IDLE POSITION ADJUSTMENT
Note:
INever adjust throttle adjust screw (TAS).
IDo not touch throttle drum when checking “CLSD THL/P
SW” signal or “continuity”, doing so may cause an incorrect adjustment.
1.Warm engine up to normal operating temperature.
2.Check FI cam. Refer to procedure
3.Stop engine.
SEF246F
SEF793W
SEF402W
SEF397X
Note: If handy vacuum pump is a already set, go to step 7.
4.Remove the vacuum hose connected to the throttle opener.
5.Connect suitable vacuum hose to the vacuum pump and the
throttle opener as shown in the figure.
6.Apply vacuum [more than −40.0 kPa (−300 mmHg, −11.81
inHg)] until the throttle drum become free from the rod of the
throttle opener. During the TPS adjustment the vacuum should
be applied.
7.Loosen throttle position sensor fixing bolts.
8.Turn ignition switch “ON”.
9.Select “DATA MONITOR” mode with CONSULT-II.
10. Select “CLSD THL/P SW” from the menu.
11. Read “CLSD THL/P SW” signal under the following conditions.
IInsert 0.2 mm (0.008 in) feeler gauge between throttle
adjust screw and throttle drum as shown in the figure
and check the following.
IOpen throttle valve and then close.
I“CLSD THL/P SW” signal should remain “OFF”
when the throttle valve is closed. (If signal is “ON”,
turn throttle position sensor body counterclockwise until the signal switches to “OFF”.)
12. Temporarily tighten sensor body fixing bolts as follows.
IGradually move the sensor body clockwise and
stop it when “CLSD THL/P SW” signal switches
from “OFF” to “ON”, then tighten sensor body fixing bolts.
13. Make sure the signal is “ON” when the throttle valve is
closed and “OFF” when it is opened. Repeat it 2 or 3
times.
14. Remove 0.2 mm (0.008 in) feeler gauge then insert 0.3
mm (0.012 in) feeler gauge and check the following.
Make sure the signal remains “OFF” when the throttle
valve is closed. Repeat it 2 or 3 times.
15. Tighten throttle position sensor.
Check that the “CLOSED THL/SW” signal remains
“OFF” while closing throttle valve. If NG, repeat from the
step 4.
After this adjustment, go to procedure
THROTTLE POSITION SENSOR IDLE POSITION
MEMORY.
8.Disconnect closed throttle position sensor harness connector.
9.Connect tester prove to the closed throttle position
switch terminals
the following conditions.
q
6 andq8 and check continuity under
EXIT
EXIT
GI
.
MA
EM
LC
FE
AT
PD
FA
RA
BR
ST
RS
BT
HA
RESET
EL
IDX
SEF398X
EC-95
TROUBLE DIAGNOSIS — Basic Inspection
Basic Inspection (Cont’d)
IInsert the 0.2 mm (0.008 in) feeler gauge between the
throttle adjust screw and throttle drum as shown in the
figure and check the following.
IOpen throttle valve then close.
IThe continuity should not exist while closing the
throttle valve. If the continuity exists, turn throttle
position sensor body counterclockwise until the
continuity does not exist.
10. Temporarily tighten sensor body fixing bolts as follows.
IGradually move the sensor body clockwise and
SEF403W
SEF300T
stop it when the continuity comes to exist, then
tighten sensor body fixing bolts.
11. Make sure the continuity exists when the throttle valve
is closed and continuity does not exist when it is
opened. Repeat it 2 or 3 times.
12. Remove 0.2 mm (0.008 in) feeler gauge then insert 0.3
mm (0.012 in) feeler gauge and check the following.
Make sure the continuity does not exist when the
throttle valve is closed. Repeat it 2 or 3 times.
13. Tighten throttle position sensor.
Check that the continuity does not exist while closing
the throttle valve. If NG, repeat from the step 5.
After this adjustment, go to procedure
THROTTLE POSITION SENSOR IDLE POSITION
MEMORY.
The ECM enters fail-safe mode, if any of the following malfunctions are detected due to the open or short circuit.
When the ECM enters the fail-safe mode, the MIL illuminates.
DTC No.
CONSULT-II
GST
P01000102Mass air flow sensor cir-
P01150103Engine coolant tempera-
ECM*
Detected itemsEngine operating condition in fail-safe mode
cuit
ture sensor circuit
Engine speed will not rise more than 2,400 rpm due to the fuel cut.
Engine coolant temperature will be determined by ECM based on the time
after turning ignition switch “ON” or “START”.
CONSULT-II displays the engine coolant temperature decided by ECM.
EXIT
EXIT
P01200403Throttle position sensor
P12100106TCS signal circuitTCS does not operate.
Unable to
access ECM
Unable to
access Diag-
nostic Test
Mode II
Condition
Just as ignition switch is turned ON or
Start
More than 4 minutes after ignition Start80°C (176°F)
Except as shown above
circuit
ECMECM fail-safe activating condition
Throttle position will be determined based on the amount of mass air flow
and the engine speed.
Therefore, acceleration will be poor.
When engine is idlingNormal
When acceleratingPoor acceleration
For details, refer to BR section (“TROUBLE DIAGNOSIS FOR TCS”).
The computing function of the ECM was judged to be malfunctioning.
When the fail-safe system activates, i.e. if the ECM detects a malfunction
condition in the CPU of ECM, the MALFUNCTION INDICATOR LAMP on
the instrument panel lights to warn the driver.
However, it is not possible to access ECM and DTC cannot be confirmed.
Engine control with ECM fail-safe
When the fail-safe system is operating, fuel injection, ignition timing, fuel
pump operation, IACV-AAC valve operation and cooling fan operation are
controlled under certain limitations.
Engine coolant temperature decided
(CONSULT-II display)
40°C (104°F)
40 - 80°C (104 - 176°F)
(Depends on the time)
Driving condition
*: In Diagnostic Test Mode II (Self-diagnostic results)
ECM fail-safe operation
Engine speedEngine speed will not rise more than 3,000 rpm.
Fuel injectionSimultaneous multiport fuel injection system
Ignition timingIgnition timing is fixed at the preset value.
Fuel pump
Cooling fans
Replace ECM, if ECM fail-safe condition is confirmed.
Fuel pump relay is “ON” when engine is running and
“OFF” when engine stalls.
Cooling fan relay “ON” (High speed condition) when
engine is running, and “OFF” when engine stalls.
EC-98
TROUBLE DIAGNOSIS — General Description
Symptom Matrix Chart
SYMPTOM
GI
EXIT
EXIT
SYSTEM
— Basic engine control system
HARD/NO START/RESTART (EXCP. HA)
ENGINE STALL
HESITATION/SURGING/FLAT SPOT
SPARK KNOCK/DETONATION
LACK OF POWER/POOR ACCELERATION
HIGH IDLE/LOW IDLE
ROUGH IDLE/HUNTING
IDLING VIBRATION
SLOW/NO RETURN TO IDLE
OVERHEATS/WATER TEMPERATURE HIGH
EXCESSIVE FUEL CONSUMPTION
EXCESSIVE OIL CONSUMPTION
OVERCOOLS
Warranty symptom codeAA AB AC AD AE AF AG AH AJ AK AL AM 1P 1X HA
FuelFuel pump circuit112323332EC-523
EGR system2123332333EC-423
Main power supply and ground circuit2333322333EC-118
CoolingCooling fan circuit3333333331213EC-503
Air conditioner circuit33333333333HAsection
1 - 6: The numbers refer to the order of inspection.
Reference page
OVERCHARGING
BATTERY DEAD (UNDER CHARGE)
MA
EM
LC
FE
AT
PD
FA
RA
BR
ST
RS
BT
HA
EL
IDX
EC-99
TROUBLE DIAGNOSIS — General Description
Symptom Matrix Chart (Cont’d)
SYMPTOM
SYSTEM
— Engine control system
HARD/NO START/RESTART (EXCP. HA)
ENGINE STALL
HESITATION/SURGING/FLAT SPOT
SPARK KNOCK/DETONATION
LACK OF POWER/POOR ACCELERATION
HIGH IDLE/LOW IDLE
ROUGH IDLE/HUNTING
IDLING VIBRATION
SLOW/NO RETURN TO IDLE
OVERHEATS/WATER TEMPERATURE HIGH
EXCESSIVE FUEL CONSUMPTION
EXCESSIVE OIL CONSUMPTION
OVERCOOLS
OVERCHARGING
Warranty symptom codeAA AB AC AD AE AF AG AH AJ AK AL AM 1P 1X HA
Engine con-
trol
1 - 6: The numbers refer to the order of inspection.
Camshaft position sensor circuit22222333EC-275
Mass air flow sensor circuit1123222222EC-124
Front heated oxygen sensor circuit21232232EC-196, 166
Engine coolant temperature sensor circuit11333323323EC-145, 161
Throttle position sensor circuit12232232EC-150
Incorrect throttle position sensor adjust-
ment
Intake valve timing control system33333EC-367, 382
Vehicle speed sensor circuit3333EC-335
Knock sensor circuit23222323EC-267
ECM33333333333EC-355, 98
Start signal circuit2EC-521
Park/Neutral position switch circuit33333EC-494
FPCM22222EC-393
Power steering oil pressure switch circuit233EC-527
23313313EC-91
Reference page
BATTERY DEAD (UNDER CHARGE)
EXIT
EXIT
EC-100
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