VC CUT/V BYPASS/VP14911491EC-648
VEH SPD SEN/CIR AT*6P07200720AT-111
VEH SPEED SEN/CIRC*6P05000500EC-438
VENT CONTROL VALVEP04470447EC-377
VENT CONTROL VALVEP14461446EC-606
VENT CONTROL VALVEP14481448EC-614
*1: 1st trip DTC No. is the same as DTC No.
*2: These numbers are prescribed by SAE J2012.
*3: In Diagnostic Test Mode II (Self-diagnostic results), these numbers are controlled by NISSAN.
*4: When engine is running.
*5: When the fail-safe operation occurs, the MIL illuminates.
*6: When fail-safe operations for both self-diagnoses occur at the same time, the MIL illuminates.
NOTE:
IRegarding R50 models, “-B1” indicates bank 1 and “-B2” indicates left bank 2.
IBank 1 (-B1) includes No. 1 cylinder.
*1: 1st trip DTC No. is the same as DTC No.
*2: These numbers are prescribed by SAE J2012.
*3: In Diagnostic Test Mode II (Self-diagnostic results), these numbers are controlled by NISSAN.
*4: When engine is running.
*5: When the fail-safe operation occurs, the MIL illuminates.
*6: When fail-safe operations for both self-diagnoses occur at the same time, the MIL illuminates.
NOTE:
IRegarding R50 models, “-B1” indicates right bank 1 and “-B2” indicates bank 2.
IBank 1 (-B1) includes No. 1 cylinder.
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PRECAUTIONS
Supplemental Restraint System (SRS) “AIR BAG” and “SEAT BELT PRE-TENSIONER”
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 NISSAN MODEL R50 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 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 must be performed
by an authorized NISSAN dealer.
IImproper maintenance, including incorrect removal and installation of the SRS, can lead to per-
sonal injury caused by unintentional activation of the system. For removal of Spiral Cable and Air
Bag Module, refer to RS section.
IDo not use electrical test equipment on any circuit related to the SRS unless instructed to in this
Service Manual. SRS wiring harnesses can be identified by yellow harness connector (and by yellow harness protector or yellow insulation tape before the harness connectors).
NAEC0002
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 any
repair or inspection work. The open/short circuit of related switches, sensors, solenoid valves, etc.
will cause the MIL to light up.
IBe sure to connect and lock the connectors securely after work. A loose (unlocked) connector will
cause the MIL to light up due to the open circuit. (Be sure the connector is free from water, grease,
dirt, bent terminals, etc.)
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-6, “HARNESS
CONNECTOR (SLIDE-LOCKING TYPE)”.
IBe sure to route and secure 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 work. A misconnected or disconnected rubber tube
may cause the MIL to light up due to the malfunction of the fuel injection system, etc.
IBe sure to erase the unnecessary malfunction information (repairs completed) from the ECM and
TCM (Transmission control module) before returning the vehicle to the customer.
NAEC0003
EC-16
Page 17
PRECAUTIONS
Engine Fuel & Emission Control System
Engine Fuel & Emission Control System
NAEC0004
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Page 18
Precautions
PRECAUTIONS
SEF289H
SEF908W
Precautions
NAEC0005
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.
IWhen connecting ECM harness connector, fasten it
securely with a lever as far as it will go as shown at left.
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
MEF040D
SEF217U
IBefore replacing ECM, perform “ECM Terminals and Ref-
erence Value” inspection and make sure ECM functions
properly. Refer to EC-141.
IAfter performing each TROUBLE DIAGNOSIS, perform
“DTC Confirmation Procedure” or “Overall Function
Check”.
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-18
Page 19
PRECAUTIONS
Precautions (Cont’d)
SEF348N
IWhen measuring ECM signals with a circuit tester, never
allow the two tester probes to contact.
Accidental contact of probes will cause a short circuit and
damage the ECM power transistor.
IDo not use ECM ground terminals when measuring input/
output voltage. Doing so may result in damage to the
ECM’s transistor. Use a ground other than the ECM
terminals, such as the ground.
IRegarding model R50, “-B1” indicates the right bank and
“-B2” indicates the left bank as shown in the figure.
IBank 1 includes No. 1 cylinder.
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SEF099WB
Wiring Diagrams and Trouble Diagnosis
When you read Wiring diagrams, refer to the following:
IGI-11, “HOW TO READ WIRING DIAGRAMS”
IEL-9, “POWER SUPPLY ROUTING” for power distribution circuit
When you perform trouble diagnosis, refer to the following:
IGI-35, “HOW TO FOLLOW TEST GROUPS IN TROUBLE DIAGNOSES”
IGI-24, “HOW TO PERFORM EFFICIENT DIAGNOSIS FOR AN ELECTRICAL INCIDENT”
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Special Service Tools
PREPARATION
Special Service Tools
The actual shapes of Kent-Moore tools may differ from those of special service tools illustrated here.
Tool number
(Kent-Moore No.)
Tool name
KV10117100
(J36471-A)
Heated oxygen sensor
wrench
(J44321)
Fuel pressure gauge kit
Description
Loosening or tightening heated oxygen sensor
(bank 1)/(bank 2) with 22 mm (0.87 in) hexagon
nut
NT379
Checking fuel pressure with pressure gauge
LEC642
Commercial Service Tools
Tool name
(Kent-Moore No.)
Description
NAEC0007
NAEC0008
Fuel filler cap adapter
i.e.: (MLR-8382)
Leak detector
i.e.: (J41416)
EVAP service port
adapter
i.e.: (J41413-OBD)
Checking fuel tank vacuum relief valve opening
pressure
NT815
Locating the EVAP leak
NT703
Applying positive pressure through EVAP service
port
Anti-seize lubricant
i.e.: (Permatex
or equivalent meeting
MIL specification MIL-A-
907)
TM
133AR
Description
NT705
AEM488
Removing and installing engine coolant temperature sensor
Reconditioning the exhaust system threads before
installing a new oxygen sensor. Use with antiseize lubricant shown below.
a: J-43897-18 18 mm diameter with pitch 1.5
mm, for Zirconia Oxygen Sensor
b: J-43897-12 12 mm diameter with pitch 1.25
mm, for Titania Oxygen Sensor
Lubricating oxygen sensor thread cleaning tool
when reconditioning exhaust system threads.
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NT779
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ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location
Engine Control Component Parts Location
NAEC0009
EC-22
SEF952ZA
Page 23
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location (Cont’d)
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ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location (Cont’d)
EC-24
SEF584ZA
Page 25
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Engine Control Component Parts Location (Cont’d)
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Circuit Diagram
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Circuit Diagram
NAEC0010
EC-26
MEC668D
Page 27
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
System Diagram
System Diagram
NAEC0011
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ENGINE AND EMISSION CONTROL OVERALL SYSTEM
Vacuum Hose Drawing
Vacuum Hose Drawing
Refer to “System Diagram”, EC-27 for Vacuum Control System.
NAEC0012
EC-28
SEF953Z
Page 29
ENGINE AND EMISSION CONTROL OVERALL SYSTEM
System Chart
Input (Sensor)ECM FunctionOutput (Actuator)
I Camshaft position sensor (PHASE)
I Crankshaft position sensor (REF)
I Mass air flow sensor
I Engine coolant temperature sensor
I Heated oxygen sensor 1
I Ignition switch
I Throttle position sensor
I Closed throttle position switch *3
I Park/neutral position (PNP) switch
I Air conditioner switch
I Knock sensor
I Intake air temperature sensor
I Absolute pressure sensor
I EVAP control system pressure sensor *1
I Battery voltage
I Power steering oil pressure switch
I Vehicle speed sensor
I Fuel tank temperature sensor *1
I Crankshaft position sensor (POS)
I Heated oxygen sensor 2*2
I TCM (Transmission control module)
I Refrigerant pressure sensor
I Electrical load
I Fuel level sensor*1
System Chart
Fuel injection & mixture ratio controlInjectors
Electronic ignition systemPower transistor
Idle air control systemIACV-AAC valve
Fuel pump controlFuel pump relay
On board diagnostic systemMIL (On the instrument panel)
I EVAP canister vent control valve
I Vacuum cut valve bypass valve
NAEC0013
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*1: These sensors are not used to control the engine system. They are used only for the on board diagnosis.
*2: This sensor is not used to control the engine system under normal conditions.
*3: This switch will operate in place of the throttle position sensor to control EVAP parts if the sensor malfunctions.
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Multiport Fuel Injection (MFI) System
Multiport Fuel Injection (MFI) System
DESCRIPTION
Input/Output Signal Chart
SensorInput Signal to ECM
Crankshaft position sensor (POS)Engine speed (POS signal)
Crankshaft position sensor (REF)Engine speed (REF signal)
Camshaft position sensor (PHASE)Piston position
Mass air flow sensorAmount of intake air
Engine coolant temperature sensorEngine coolant temperature
Heated oxygen sensor 1Density of oxygen in exhaust gas
ECM func-
tion
NAEC0014
NAEC0014S01
Actuator
Throttle position sensor
Park/neutral position (PNP) switchGear position
Vehicle speed sensorVehicle speed
Ignition switchStart signal
Air conditioner switchAir conditioner operation
Knock sensorEngine knocking condition
BatteryBattery voltage
Absolute pressure sensorAmbient air barometric pressure
Power steering oil pressure switchPower steering operation
Heated oxygen sensor 2*Density of oxygen in exhaust gas
*: Under normal conditions, this sensor is not for engine control operation.
Basic Multiport Fuel Injection System
Throttle position
Throttle valve idle position
Fuel injection & mixture ratio
control
Injectors
NAEC0014S02
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 crankshaft position sensor and the mass air
flow sensor.
Various Fuel Injection Increase/Decrease Compensation
NAEC0014S03
In addition, the amount of fuel injected is compensated to improve engine performance 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 engine speed operation
EC-30
Page 31
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Multiport Fuel Injection (MFI) System (Cont’d)
Mixture Ratio Feedback Control (Closed loop control)
The mixture ratio feedback system provides the best air-fuel mixture ratio for driveability and emission control. The three way catalyst (manifold) can then better reduce CO, HC and NOx emissions. This system uses
a heated oxygen sensor 1 in the exhaust manifold to monitor if the engine operation is rich or lean. The ECM
adjusts the injection pulse width according to the sensor voltage signal. For more information about the heated
oxygen sensor 1, refer to EC-254. This maintains the mixture ratio within the range of stoichiometric (ideal
air-fuel mixture).
This stage is referred to as the closed loop control condition.
Heated oxygen sensor 2 is located downstream of the three way catalyst (manifold). Even if the switching
characteristics of the heated oxygen sensor 1 shift, the air-fuel ratio is controlled to stoichiometric by the signal from the heated oxygen sensor 2.
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 heated oxygen sensor 1 or its circuit
IInsufficient activation of heated oxygen sensor 1 at low engine coolant temperature
IHigh engine coolant temperature
IDuring warm-up
IAfter shifting from “N” to “D”
IWhen starting the engine
NAEC0014S04
SEF336WC
NAEC0014S05
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Mixture Ratio Self-learning Control
The mixture ratio feedback control system monitors the mixture ratio signal transmitted from the heated oxygen sensor 1. 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 wire) 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 heated oxygen sensor 1 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 long-term 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.
NAEC0014S06
EC-31
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Multiport Fuel Injection (MFI) System (Cont’d)
Fuel Injection Timing
NAEC0014S07
SEF179U
Two types of systems are used.
Sequential Multiport Fuel Injection System
NAEC0014S0701
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
NAEC0014S0702
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 system (CPU) is operating.
Fuel Shut-off
NAEC0014S08
Fuel to each cylinder is cut off during deceleration or operation of the engine at excessively high speeds.
Electronic Ignition (EI) System
DESCRIPTION
Input/Output Signal Chart
SensorInput Signal to ECM
Crankshaft position sensor (POS)Engine speed (POS signal)
Crankshaft position sensor (REF)Engine speed (REF signal)
Camshaft position sensor (PHASE)Piston position
Mass air flow sensorAmount of intake air
Engine coolant temperature sensorEngine coolant temperature
Throttle position sensor
Vehicle speed sensorVehicle speed
Ignition switchStart signal
Knock sensorEngine knocking
Park/neutral position (PNP) switchGear position
BatteryBattery voltage
Throttle position
Throttle valve idle position
ECM func-
tion
Ignition
timing control
NAEC0015
NAEC0015S01
Actuator
Power transistor
EC-32
Page 33
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Electronic Ignition (EI) System (Cont’d)
System Description
SEF742M
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.
The ECM receives information such as the injection pulse width and camshaft position sensor signal. Computing this information, ignition signals are transmitted to the power transistor.
e.g.,N: 1,800 rpm, Tp: 1.50 msec
A °BTDC
During the following conditions, the ignition timing is revised by the ECM according to the other data stored
in the ECM.
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.
NAEC0015S02
Air Conditioning Cut Control
DESCRIPTION
Input/Output Signal Chart
SensorInput Signal to ECMECM functionActuator
Air conditioner switchAir conditioner “ON” signal
NAEC0016
NAEC0016S01
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Throttle position sensorThrottle valve opening angle
Crankshaft position sensor (POS)Engine speed (POS signal)
Crankshaft position sensor (REF)Engine speed (REF signal)
Engine coolant temperature sensorEngine coolant temperature
Ignition switchStart signal
Vehicle speed sensorVehicle speed
Refrigerant pressure sensorRefrigerant pressure
Power steering oil pressure switchPower steering operation
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.
EC-33
Air conditioner
cut control
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Air Conditioning Cut Control (Cont’d)
IWhen the engine coolant temperature becomes excessively high.
IWhen operating power steering during low engine speed or low vehicle speed.
IWhen engine speed is excessively low.
IWhen refrigerant pressure is excessively low or high.
Fuel Cut Control (at no load & high engine
speed)
DESCRIPTION
Input/Output Signal Chart
SensorInput Signal to ECM
Vehicle speed sensorVehicle speed
Park/neutral position (PNP) switchNeutral position
ECM func-
tion
NAEC0017
NAEC0017S01
Actuator
Throttle position sensorThrottle position
Engine coolant temperature sensorEngine coolant temperature
Crankshaft position sensor (POS)Engine speed (POS signal)
Crankshaft position sensor (REF)Engine speed (REF signal)
Fuel cut
control
Injectors
If the engine speed is above 1,800 rpm with no load (for example, in neutral and engine speed over 1,800
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 1,500 rpm, then fuel cut is cancelled.
NOTE:
This function is different from deceleration control listed under “Multiport Fuel Injection (MFI) System”, EC-30.
Evaporative Emission System
DESCRIPTION
NAEC0018
SEF569XA
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 and the
vapor is stored there when the engine is not operating or when refueling to the fuel tank.
The vapor in the EVAP canister is purged by the air through the purge line to the intake manifold when the
engine is operating. EVAPcanister purge volume control solenoid valve is controlled by ECM. When the engine
EC-34
Page 35
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Evaporative Emission System (Cont’d)
operates, the flow rate of vapor controlled by EVAP canister purge volume control solenoid valve is proportionally regulated as the air flow increases.
EVAP canister purge volume control solenoid valve also shuts off the vapor purge line during decelerating and
idling.
INSPECTION
EVAP Canister
Check EVAP canister as follows:
1.Pinch the fresh air hose.
2.Blow air into port A and check that it flows freely out of port B.
SEF428T
Tightening Torque
Tighten EVAP canister as shown in the figure.
Make sure new O-ring is installed properly between EVAPcanister and EVAP canister vent control valve.
NAEC0019
NAEC0019S01
NAEC0019S02
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SEF231SB
SEF445Y
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
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 psi)
NAEC0019S03
2
, −0.87 to
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EC-35
Page 36
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Evaporative Emission System (Cont’d)
SEF462UA
SEF200U
PEF838U
Vacuum Cut Valve and Vacuum Cut Valve Bypass Valve
NAEC0019S04
Refer to EC-648.
Evaporative Emission (EVAP) Canister Purge Volume
Control Solenoid Valve
Refer to EC-370.
Fuel Tank Temperature Sensor
Refer to EC-298, 301.
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.
How to Detect Fuel Vapor Leakage
CAUTION:
INever use compressed air or a high pressure pump.
IDo not exceed 4.12 kPa (0.042 kg/cm
in EVAP system.
NOTE:
IDo not start engine.
IImproper installation of EVAPservice port adapter to the EVAP
service port may cause a leak.
With CONSULT-II
1)Attach the EVAP service port adapter securely to the EVAP
service port.
2)Also attach the pressure pump and hose to the EVAP service
port adapter.
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 EVAP service port adapter and hose with pressure
pump.
8)Locatethe leak using a leak detector.Refer to “EVAPORATIVE
EMISSION LINE DRAWING”, EC-38.
2
, 0.6 psi) of pressure
NAEC0019S05
NAEC0019S06
NAEC0019S07
NAEC0019S08
NAEC0019S0801
PEF917U
EC-36
Page 37
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Evaporative Emission System (Cont’d)
SEF462UA
SEC930C
Without CONSULT-II
1)Attach the EVAP service port adapter securely to the EVAP
service port.
2)Also attach the pressure pump with pressure gauge to the
EVAP service port adapter.
3)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.
4)To locate the leak, deliver positive pressure to the EVAP system until pressure gauge points reach 1.38 to 2.76 kPa (0.014
to 0.028 kg/cm
5)Remove EVAP service port adapter and hose with pressure
pump.
6)Locatethe leak using a leak detector.Refer to “EVAPORATIVE
EMISSION LINE DRAWING”, EC-38.
2
, 0.2 to 0.4 psi).
NAEC0019S0802
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Evaporative Emission System (Cont’d)
EVAPORATIVE EMISSION LINE DRAWING
NAEC0020
EC-38
SEF954Z
Page 39
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Evaporative Emission System (Cont’d)
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR)
SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR)
NAEC0744S01
SEF206VA
NAEC0744
SEC883C
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:
IPut a “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
fire extinguisher.
2
EC-40
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR) (Cont’d)
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-51.
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.
Continued refueling may cause fuel overflow, resulting in fuel spray and possibly a fire.
DIAGNOSTIC PROCEDURE
Symptom: Fuel Odor from EVAP Canister Is Strong.
1CHECK EVAP CANISTER
1. Remove EVAP canister with EVAP canister vent control valve attached.
2. Weigh the EVAP canister with EVAP canister vent control valve attached.
The weight should be less than 1.8 kg (4.0 lb).
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR) (Cont’d)
6CHECK REFUELING EVAP VAPOR CUT VALVE
With CONSULT-II
1. Remove fuel tank. Refer to FE-4, “FUEL SYSTEM.
2. Drain fuel from the tank as follows:
a. Remove fuel feed hose located on the fuel gauge retainer.
b. Connect a spare fuel hose, one side to fuel gauge retainer where the hose was removed and the other side to a fuel
container.
c. Drain fuel using “FUEL PUMP RELAY” in “ACTIVE TEST” mode with CONSULT-II.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows.
Blow air into the refueling EVAP vapor cut valve (from hose end B), and check that the air flows freely into the tank.
4. Check EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose ends A and B using a suitable 3-way connector.
b. Remove fuel gauge retainer with fuel gauge unit.
Always replace O-ring with new one.
c. Put fuel tank upside down.
d. Apply vacuum pressure to both hose ends A and B [−13.3 kPa (−100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR) (Cont’d)
7CHECK REFUELING EVAP VAPOR CUT VALVE
Without CONSULT-II
1. Remove fuel tank. Refer to FE-4, “FUEL SYSTEM”.
2. Drain fuel from the tank as follows:
a. Remove fuel gauge retainer.
b. Drain fuel from the tank using a hand pump into a fuel container.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows.
Blow air into the refueling EVAP vapor cut valve (from hose end B), and check that the air flows freely into the tank.
4. Check EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose ends A and B using a suitable 3-way connector.
b. Remove fuel gauge retainer with fuel gauge unit.
Always replace O-ring with new one.
c. Put fuel tank upside down.
d. Apply vacuum pressure to both hose ends A and B [−13.3 kPa (−100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
2. Check air continuity between hose ends A and B.
Blow air into the hose end B. Air should flow freely into the fuel tank.
3. Blow air into hose end A and check there is no leakage.
4. Apply pressure to both hose ends A and B [20 kPa (150 mmHg, 5.91 inHg)] using a pressure pump and a suitable
3-way connector. Check that there is no leakage.
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR) (Cont’d)
8CHECK REFUELING CONTROL VALVE
1. Remove fuel filler cap.
2. Check air continuity between hose ends A and B.
Blow air into the hose end B. Air should flow freely into the fuel tank.
3. Blow air into hose end A and check there is no leakage.
4. Apply pressure to both hose ends A and B [20 kPa (150 mmHg, 5.91 inHg)] using a pressure pump and a suitable
3-way connector. Check that there is no leakage.
1. Remove fuel tank. Refer to FE-4, “FUEL SYSTEM”.
2. Drain fuel from the tank as follows:
a. Remove fuel feed hose located on the fuel gauge retainer.
b. Connect a spare fuel hose, one side to fuel gauge retainer where the hose was removed and the other side to a fuel
container.
c. Drain fuel using “FUEL PUMP RELAY” in “ACTIVE TEST” mode with CONSULT-II.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows.
Blow air into the refueling EVAP vapor cut valve (from hose end B), and check that the air flows freely into the tank.
4. Check EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose ends A and B using a suitable 3-way connector.
b. Remove fuel gauge retainer with fuel gauge unit.
Always replace O-ring with new one.
c. Put fuel tank upside down.
d. Apply vacuum pressure to both hose ends A and B [−13.3 kPa (−100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
On Board Refueling Vapor Recovery (ORVR) (Cont’d)
10CHECK REFUELING EVAP VAPOR CUT VALVE
Without CONSULT-II
1. Remove fuel tank. Refer to FE-4, “FUEL SYSTEM”.
2. Drain fuel from the tank as follows:
a. Remove fuel gauge retainer.
b. Drain fuel from the tank using a hand pump into a fuel container.
3. Check refueling EVAP vapor cut valve for being stuck to close as follows.
Blow air into the refueling EVAP vapor cut valve (from hose end B), and check that the air flows freely into the tank.
4. Check EVAP vapor cut valve for being stuck to open as follows.
a. Connect vacuum pump to hose ends A and B using a suitable 3-way connector.
b. Remove fuel gauge retainer with fuel gauge unit.
Always replace O-ring with new one.
c. Put fuel tank upside down.
d. Apply vacuum pressure to both hose ends A and B [−13.3 kPa (−100 mmHg, −3.94 inHg)] with fuel gauge retainer
remaining open and check that the pressure is applicable.
This system returns blow-by gas to the intake manifold.
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 inlet tubes into the
SEF372Q
crankcase. In this process the air passes through the hose connecting air inlet tubes to rocker cover.
Under full-throttle condition, the manifold vacuum is insufficient to
draw the blow-by flow through the valve. The flow goes through the
hose connection in the reverse direction.
On vehicles with an excessively high blow-by, the valve does not
meet the requirement. This is because some of the flow will go
through the hose connection to the air inlet tubes under all
conditions.
With engine running at idle, remove PCV valve ventilation hose
from PCV valve; if the 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.
NAEC0022
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ENGINE AND EMISSION BASIC CONTROL SYSTEM DESCRIPTION
Positive Crankcase Ventilation (Cont’d)
ET277
PCV Valve Ventilation Hose
NAEC0022S02
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.
EC-50
Page 51
BASIC SERVICE PROCEDURE
Fuel Pressure Release
SEF941Y
SEF214Y
Fuel Pressure Release
Before disconnecting fuel line, release fuel pressure from fuel
line to eliminate danger.
WITH CONSULT-II
1.Turn ignition switch “ON”.
2.Perform “FUEL PRESSURE RELEASE” in “WORK SUPPORT” mode with CONSULT-II.
3.Start engine.
4.After engine stalls, crank it two or three times to release all fuel
pressure.
5.Turn ignition switch “OFF”.
WITHOUT CONSULT-II
1.Remove fuel pump fuse located in fuse box.
2.Start engine.
3.After engine stalls, crank it two or three times to release all fuel
pressure.
4.Turn ignition switch “OFF”.
5.Reinstall fuel pump fuse after servicing fuel system.
NAEC0023
NAEC0023S01
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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.
IDo not perform fuel pressure check with electrical system
operating (i.e. lights, rear window defogger,A/C, etc.). Fuel
pressure gauge may indicate false readings due to varying engine loads and change in manifold vacuum.
1.Release fuel pressure to zero.
2.Disconnect fuel tube joint between fuel damper and injector
tube and set fuel pressure check adapter (J44321).
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EC-51
Page 52
Fuel Pressure Check (Cont’d)
BASIC SERVICE PROCEDURE
3.Install pressure gauge to the fuel pressure check adapter as
shown in the figure.
4.Start engine and check for fuel leakage.
5.Read the indication of fuel pressure gauge.
At idling:
With vacuum hose connected
Approximately 235 kPa (2.4 kg/cm
With vacuum hose disconnected
Approximately 294 kPa (3.0 kg/cm
SEF328Z
If results are unsatisfactory, perform Fuel Pressure Regulator
Check.
2
, 34 psi)
2
, 43 psi)
SEF329Z
SEF718BA
Fuel Pressure Regulator Check
NAEC0025
1.Stop engine and disconnect fuel pressure regulator vacuum
hose from vacuum gallery.
2.Plug vacuum gallery with a blind cap.
3.Connect variable vacuum source to fuel pressure regulator.
4.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.
EC-52
Page 53
BASIC SERVICE PROCEDURE
Injector
SEF937Y
SEF703X
Injector
REMOVAL AND INSTALLATION
1.Release fuel pressure to zero.
2.Remove intake manifold collector. Refer to EM-20, “TIMING
CHAIN”.
3.Remove fuel tube assemblies in numerical sequence as
shown in the figure at left.
4.Expand and remove clips securing fuel injectors.
5.Extract fuel injectors straight from fuel tubes.
IBe careful not to damage injector nozzles during removal.
IDo not bump or drop fuel injectors.
6.Carefully install O-rings, including the one used with the pressure regulator.
ILubricate O-rings with a smear of engine oil.
IBe careful not to damage O-rings with service tools, fin-
ger nails or clips. Do not expand or twist O-rings.
IDiscard old clips; replace with new ones.
7.Position clips in grooves on fuel injectors.
IMake sure that protrusions of fuel injectors are aligned
with cutouts of clips after installation.
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8.Align protrusions of fuel tubes with those of fuel injectors.
Insert fuel injectors straight into fuel tubes.
9.After properly inserting fuel injectors, check to make sure that
fuel tube protrusions are engaged with those of fuel injectors,
and that flanges of fuel tubes are engaged with clips.
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Injector (Cont’d)
BASIC SERVICE PROCEDURE
10. Tighten fuel tube assembly mounting nuts in numerical
sequence (indicated in the figure at left) and in two stages.
: Tightening torque N·m (kg-m, ft-lb)
1st stage:
9.3 - 10.8 (1.0 - 1.1, 6.9 - 7.9)
2nd stage:
20.6 - 26.5 (2.1 - 2.7, 16 - 19)
11. Install all parts removed in reverse order of removal.
CAUTION:
SEF939Y
After properly connecting fuel tube assembly to injector and
fuel hose, check connection for fuel leakage.
How to Check Idle Speed and Ignition Timing
IDLE SPEED
IUsing CONSULT-II
Check idle speed in “DATA MONITOR” mode with CONSULT-II.
NAEC0607
NAEC0607S01
SEF058Y
SEF940Y
SEF942Y
IGNITION TIMING
Any of following two methods may be used.
IMethod A
a)Attach timing light to loop wire as shown.
b)Check ignition timing.
IMethod B
a)Remove No. 1 ignition coil.
NAEC0607S02
EC-54
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BASIC SERVICE PROCEDURE
How to Check Idle Speed and Ignition Timing (Cont’d)
SEF943Y
SEF572X
b)Connect No. 1 ignition coil and No. 1 spark plug with suitable
high-tension wire as shown, and attach timing light clamp to
this wire.
c)Check ignition timing.
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Idle Speed/Ignition Timing/Idle Mixture Ratio
Adjustment
PREPARATION
1) Make sure that the following parts are in good order.
IBattery
IIgnition system
IEngine oil and coolant levels
IFuses
IECM harness connector
IVacuum hoses
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EC-55
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BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
IAir intake system
(Oil filler cap, oil level gauge, etc.)
IFuel pressure
IEngine compression
IThrottle valve
IEvaporative emission system
2) On air conditioner equipped models, checks should be carried out while the air conditioner is “OFF”.
3) On automatic transmission equipped models, when checking idle rpm, ignition timing and mixture ratio,
checks should be carried out while shift lever is in “N” position.
4) When measuring “CO” percentage, insert probe more than 40 cm (15.7 in) into tail pipe.
5) Turn off headlamps, heater blower, rear defogger.
6) Keep front wheels pointed straight ahead.
7) Make the check after the cooling fan has stopped.
EC-56
Page 57
BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
Overall Inspection Sequence
NAEC0028S0101
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BASIC SERVICE PROCEDURE
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
INSPECTION PROCEDURE
1INSPECTION START
1. Visually check the following:
I Air cleaner clogging
I Hoses and ducts for leaks
I Electrical connectors
I Gasket
I Throttle valve and throttle position sensor operation
2. Start engine and warm it up until engine coolant temperature indicator points to the middle of gauge.
Ensure engine stays below 1,000 rpm.
3. Open engine hood and run engine at about 2,000 rpm for about 2 minutes under no-load.
=NAEC0028S02
SEF976U
4. Make sure that no DTC is displayed with CONSULT-II or GST.
1. Substitute another known-good ECM to check ECM function. (ECM may be the cause of an incident, but this is rarely
the case.)
2. Perform initialization of NVIS (NATS) system and registration of NVIS (NATS) ignition key IDs. Refer to “NVIS (NISSAN
VEHICLE IMMOBILIZER SYSTEM — NATS)”, EC-88.
1. Substitute another known-good ECM to check ECM function.
(ECM may be the cause of an incident, but this is rarely the case.)
2. Perform initialization of NVIS (NATS) system and registration of NVIS (NATS) ignition key IDs. Refer to “NVIS (NISSAN
VEHICLE IMMOBILIZER SYSTEM — NATS)”, EC-88.
After this inspection, unnecessary DTC No. might be displayed.
Erase the stored memory in ECM and TCM (Transmission control module).
Refer to “HOW TO ERASE EMISSION-RELATED DIAGNOSTIC INFORMATION”, EC-86 and AT-35 , “HOW TO ERASE
DTC”.
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
19CHECK HEATED OXYGEN SENSOR 1 (BANK 2) SIGNAL
With CONSULT-II
1. Run engine at about 2,000 rpm for about 2 minutes under no-load.
2. See “HO2S1 MNTR (B2)” in “DATA MONITOR” mode.
3. Running engine at 2,000 rpm under no-load (engine is warmed up to normal operating temperature.), check that the
monitor fluctuates between “LEAN” and “RICH” more than 5 times during 10 seconds.
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
21CHECK HEATED OXYGEN SENSOR 1 (BANK 2) SIGNAL
With CONSULT-II
1. Stop engine.
2. Replace heated oxygen sensor 1 (bank 2).
3. Start engine and warm it up to normal operating temperature.
4. Run engine at approx. 2,000 rpm for approx. 2 minutes under no-load.
5. See “HO2S1 MNTR (B2)” in “DATA MONITOR” mode.
6. Running engine at 2,000 rpm under no-load (engine is warmed up to normal operating temperature.), check that the
monitor fluctuates between “LEAN” and “RICH” more than 5 times during 10 seconds.
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
23CHECK HEATED OXYGEN SENSOR 1 (BANK 1) SIGNAL
With CONSULT-II
1. See “HO2S1 MNTR (B1)” in “DATA MONITOR” mode.
2. Maintaining engine at 2,000 rpm under no-load (engine is warmed up to normal operating temperature.), check that the
monitor fluctuates between “LEAN” and “RICH” more than 5 times during 10 seconds.
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
25CHECK HEATED OXYGEN SENSOR 1 (BANK 1) SIGNAL
With CONSULT-II
1. Stop engine.
2. Replace heated oxygen sensor 1 (bank 1).
3. Start engine and warm it up to normal operating temperature.
4. Run engine at approx. 2,000 rpm for approx. 2 minutes under no-load.
5. See “HO2S1 MNTR (B1)” in “DATA MONITOR” mode.
6. Maintaining engine at 2,000 rpm under no-load (engine is warmed up to normal operating temperature.), check that the
monitor fluctuates between “LEAN” and “RICH” more than 5 times during 10 seconds.
I Check fuel pressure regulator. Refer to EC-52.
I Check mass air flow sensor and its circuit. Refer to EC-184, 191 and 481.
I Check injector and its circuit. Refer to EC-687.
Clean or replace if necessary.
I Check engine coolant temperature sensor and its circuit. Refer to EC-203 and 227.
I Check ECM function by substituting another known-good ECM.
(ECM may be the cause of an incident, but this is rarely the case.)
Idle Speed/Ignition Timing/Idle Mixture Ratio Adjustment (Cont’d)
31CHECK “CO” %
With CONSULT-II
1. Start engine and warm it up until engine coolant temperature indicator points to the middle of gauge.
2. Rev engine (2,000 to 3,000 rpm) two or three times under no-load, then run engine at idle speed.
SEF976U
3. Check “CO” %.
Idle CO: 1.0 - 9.5%
Without CONSULT-II
1. Start engine and warm it up until engine coolant temperature indicator points to the middle of gauge.
2. Rev engine (2,000 to 3,000 rpm) two or three times under no-load, then run engine at idle speed.
SEF978U
SEF976U
3. Check “CO” %.
4. After checking CO%,
a. Disconnect the resistor from terminals of engine coolant temperature sensor.
b. Connect engine coolant temperature sensor harness connector to engine coolant temperature sensor.
3. Start engine and warm it up to normal operating temperature.
4. Run engine at approx. 2,000 rpm for approx. 2 minutes under no-load.
5. See “HO2S1 MNTR (B1)/(B2)” in “DATA MONITOR” mode.
6. Maintaining engine at 2,000 rpm under no-load (engine is warmed up to normal operating temperature.), check that the
monitor fluctuates between “LEAN” and “RICH” more than 5 times during 10 seconds.
I Connect heated oxygen sensor 1 harness connectors to heated oxygen sensors 1.
I Check fuel pressure regulator. Refer to EC-52.
I Check mass air flow sensor and its circuit. Refer to EC-184, 191 and 481.
I Check injector and its circuit. Refer to EC-687.
Clean or replace if necessary.
I Check engine coolant temperature sensor and its circuit. Refer to EC-203 and 227.
I Check ECM function by substituting another known-good ECM.
(ECM may be the cause of an incident, but this is rarely the case.)
“Idle Air Volume Learning” is an operation to learn the idle air volume that keeps each engine within the specific range. It must be
performed under any of the following conditions:
IEach time IACV-AAC valve, throttle body or ECM is replaced.
IIdle speed or ignition timing is out of specification.
PRE-CONDITIONING
NAEC0642S02
Before performing “IdleAir Volume Learning”, make sure that all of
the following conditions are satisfied.
Learning will be cancelled if any of the following conditions are
missed for even a moment.
IBattery voltage: More than 12.9V (At idle)
IEngine coolant temperature: 70 - 99°C (158 - 210°F)
IPNP switch: ON
IElectric load switch: OFF
(Air conditioner, headlamp, rear window defogger)
On vehicles equipped with daytime light systems, if the parking brake is applied before the engine is started the headlamp
will not illuminate.
ICooling fan motor: Not operating
ISteering wheel: Neutral (Straight-ahead position)
IVehicle speed: Stopped
ITransmission: Warmed-up
For A/T models with CONSULT-II, drive vehicle until “FLUID
TEMP SE” in “DATA MONITOR” mode of “A/T” system indicates less than 0.9V.
For A/T models without CONSULT-II and M/T models, drive
vehicle for 10 minutes.
MBIB0238E
OPERATION PROCEDURE
With CONSULT-II
NAEC0642S03
NAEC0642S0301
1.Turn ignition switch “ON” and wait at least 1 second.
2.Turn ignition switch “OFF” and wait at least 10 seconds.
3.Start engine and warm it up to normal operating temperature.
4.Check that all items listed under the topic “PRE-CONDITIONING” (previously mentioned) are in good order.
5.Turn ignition switch “OFF” and wait at least 10 seconds.
6.Start the engine and let it idle for at least 30 seconds.
7.Select “IDLE AIR VOL LEARN” in “WORK SUPPORT” mode.
8.Touch “START” and wait 20 seconds.
9.Make sure that “CMPLT” is displayed on CONSULT-II screen.
If “CMPLT” is not displayed, “Idle Air Volume Learning” will not
be carried out successfully. In this case, find the cause of the
incident by referring to the NOTE below.
10. Rev up the engine two or three times. Make sure that idle
speed and ignition timing are within specifications.
ITEMSPECIFICATION
Idle speedM/T: 750±50 rpm
A/T: 750±50 rpm (in “P” or “N” position)
Ignition timingM/T: 15°±5° BTDC
A/T: 15°±5° BTDC (in “P” or “N” position)
EC-70
Page 71
BASIC SERVICE PROCEDURE
Idle Air Volume Learning (Cont’d)
SEF944Y
Without CONSULT-II
1.Turn ignition switch “ON” and wait at least 1 second.
2.Turn ignition switch “OFF” and wait at least 10 seconds.
3.Start engine and warm it up to normal operating temperature.
4.Check that all items listed under the topic “PRE-CONDITIONING” (previously mentioned) are in good order.
5.Turn ignition switch “OFF” and wait at least 10 seconds.
6.Start the engine and let it idle for at least 30 seconds.
7.Disconnect throttle position sensor harness connector (brown),
then reconnect it within 5 seconds.
8.Wait 20 seconds.
9.Make sure that idle speed is within specifications. If not, the
result will be incomplete. In this case, find the cause of the
incident by referring to the NOTE below.
10. Rev up the engine two or three times. Make sure that idle
speed and ignition timing are within specifications.
ITEMSPECIFICATION
Idle speedM/T: 750±50 rpm
A/T: 750±50 rpm (in “P” or “N” position)
Ignition timingM/T: 15°±5° BTDC
A/T: 15°±5° BTDC (in “P” or “N” position)
NOTE:
If idle air volume learning cannot be performed successfully,
proceed as follows:
1)Check that throttle valve is fully closed.
2)Check PCV valve operation.
3)Check that downstream of throttle valve is free from air
leakage.
4)Adjust closed throttle position switch and reset memory.
(Refer to Basic Inspection, EC-117.)
5)When the above four items check out OK, engine component parts and their installation condition are questionable. Check and eliminate the cause of the incident. It is
useful to perform “TROUBLE DIAGNOSIS — SPECIFICATION VALVE”, EC-150.
6)If any of the following conditions occur after the engine
has started, eliminate the cause of the incident and perform “Idle air volume learning” all over again:
IEngine stalls.
IErroneous idle.
IBlown fuses related to the IACV-AAC valve system.
NAEC0642S0302
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Introduction
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Introduction
NAEC0029
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:
Emission-related diagnostic informationSAE Mode
Diagnostic Trouble Code (DTC)Mode 3 of SAE J1979
Freeze Frame dataMode 2 of SAE J1979
System Readiness Test (SRT) codeMode 1 of SAE J1979
1st Trip Diagnostic Trouble Code (1st Trip DTC)Mode 7 of SAE J1979
1st Trip Freeze Frame data
Test values and Test limitsMode 6 of SAE J1979
Calibration IDMode 9 of SAE 1979
The above information can be checked using procedures listed in the table below.
X: Applicable —: Not applicable
DTC1st trip DTC
CONSULT-IIXXXXX—
GSTXX*1X—XX
ECMXX*2
Freeze Frame
data
1st trip Freeze
Frame data
SRT codeTest value
*1: 1st trip DTCs for self-diagnoses concerning SRT items cannot be shown on the GST display.
*2: When DTC and 1st trip DTC simultaneously appear on the display, they cannot be clearly distinguished from each other.
The malfunction indicator lamp (MIL) on the instrument panel lights up when the same malfunction is detected
in two consecutive trips (Two trip detection logic), or when the ECM enters fail-safe mode. (Refer to EC-131.)
Two Trip Detection Logic
NAEC0030
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.
X: Applicable —: Not Exit
MILDTC1st trip DTC
Items
Misfire (Possible three way catalyst
damage) — DTC: P0300 - P0306
is being detected
Misfire (Possible three way catalyst
damage) — DTC: P0300 - P0306
is being detected
1st trip2nd trip
BlinkingLighting upBlinking
X — ————X—
——X——X——
Lighting
up
1st trip
displaying
2nd trip
displaying
1st trip
displaying
2nd trip
displaying
Closed loop control
— DTC: P1148, P1168
Fail-safe items (Refer to EC-131.)—X——X*1—X*1—
Except above———X—XX—
*1: Except “ECM”
— X ——X—X—
EC-72
Page 73
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information
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 1st trip DTC did not reoccur, the 1st 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 1st 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 1st 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”, EC-86.
For malfunctions in which 1st trip DTCs are displayed, refer to EC-82. 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 malfunction. 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 EC-115. Then perform “DTC Confirmation Procedure” or “Overall Function Check” to try to duplicate the malfunction. If the malfunction is duplicated, the item
requires repair.
NAEC0031
NAEC0031S01
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How to Read DTC and 1st Trip DTC
DTC and 1st trip DTC can be read by the following methods.
With CONSULT-II
With GST
CONSULT-II or GST (Generic Scan Tool) Examples: P0340, P0705, P0750, etc.
These DTCs are prescribed by SAE J2012.
(CONSULT-II also displays the malfunctioning component or system.)
No TOOLS
The number of times the MIL blinks in Diagnostic Test Mode II (Self-diagnostic Results) indicates the DTC.
(Example: 0340, 0705, 0750, etc.)
I1st trip DTC No. is the same as DTC No.
IOutput of a DTC indicates a malfunction. However, GST does 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 and 1st trip DTC is shown below. 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]”.
NAEC0031S0101
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
FREEZE FRAME DATA AND 1ST TRIP FREEZE FRAME DATA
NAEC0031S02
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, vehicle speed and absolute pressure 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 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-101.
Only one set of freeze frame data (either 1st trip freeze frame data or 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.
PriorityItems
1
2Except the above items (Includes A/T related items)
31st trip freeze frame data
Freeze frame dataMisfire — DTC: P0300 - P0306
Fuel Injection System Function — DTC: P0171, P0172, P0174, P0175
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 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”, EC-86.
SYSTEM READINESS TEST (SRT) CODE
NAEC0031S03
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.
NOTE:
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.
EC-74
Page 75
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”.
SRT item
(CONSULT-II indica-
tion)
CATALYST3Three way catalyst functionP0420, P0430
EVAP SYSTEM2EVAP control system (small leak) (negative pressure)P0442
O2 SEN HEATER3Heated oxygen sensor 1 heaterP0031, P0032, P0051,
P0052
Heated oxygen sensor 2 heaterP0037, P0038, P0057,
P0058
*: 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.
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
SRT Set Timing
=NAEC0031S0311
SRT is set as “CMPLT” after self-diagnosis has been performed one or more times. Completion of SRTis 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.
1st trip DTC—1st trip DTC
DTC
(= MIL “ON”)
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
NAEC0031S0312
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.
EC-76
Page 77
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
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*1 EC-73*2 EC-77*3 EC-78
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How to Display SRT Code
With CONSULT-II
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.
With GST
Selecting Mode 1 with GST (Generic Scan Tool)
A sample of CONSULT-II display for SRT code is shown below.
“INCMP” means the self-diagnosis is incomplete and SRT is not set. “CMPLT” means the self-diagnosis is
complete and SRT is set.
NAEC0031S0301
EC-77
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
SEF949Z
How to Set SRT Code
NAEC0031S0302
To set all SRTcodes, 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-75.
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.
EC-78
Page 79
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
Driving Pattern
NAEC0031S0303
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
IThe time required for each diagnosis varies with road surface conditions, weather, altitude, individual driv-
ing 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 performed if the diagnosis is not completed
within zone A.
*: Normal conditions refer to the following:
−Sea level
−Flat road
−Ambient air temperature: 20 - 30°C (68 - 86°F)
−Diagnosis is performed as quickly as possible under normal conditions.
Under different conditions [For example: ambient air temperature other than 20 - 30°C (68 - 86°F)], diagnosis may also be performed.
Pattern 1:
IThe engine is started at the engine coolant temperature of −10 to 35°C (14 to 95°F)
(where the voltage between the ECM terminal 70 and ground is 3.0 - 4.3V).
IThe 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 terminal 70 and ground is lower than 1.4V).
IThe engine is started at the fuel tank temperature of warmer than 0°C (32°F) (where the voltage
between the ECM terminal 92 and ground is less than 4.1V).
Pattern 2:
IWhen steady-state driving is performed again even after it is interrupted, each diagnosis can be conducted.
In this case, the time required for diagnosis may be extended.
Pattern 3:
IThe driving pattern outlined in *2 must be repeated at least 3 times.
Pattern 4:
ITests are performed after the engine has been operated for at least 17 minutes.
IThe accelerator pedal must be held very steady during steady-state driving.
IIf the accelerator pedal is moved, the test must be conducted all over again.
*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 engine idle.
2) Repeat driving pattern shown below at least 10 times.
IDuring acceleration, hold the accelerator pedal as steady as possible.
SEF414S
*3: Checking the vehicle speed with GST is advised.
Suggested Transmission Gear Position for A/T Models
Set the selector lever in the “D” position with the overdrive switch turned ON.
Suggested upshift speeds for M/T models
Shown below are suggested vehicle speeds for shifting into a higher gear. These suggestions relate to fuel
economy and vehicle performance. Actual upshift speeds will vary according to road conditions, the weather
and individual driving habits.
EC-80
Page 81
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
For normal acceleration in low altitude areas
[less than 1,219 m (4,000 ft)]:
Gear change
1st to 2nd21 (13)21 (13)24 (15)
2nd to 3rd37 (23)26 (16)40 (25)
3rd to 4th53 (33)44 (27)64 (40)
4th to 5th63 (39)58 (36)72 (45)
ACCEL shift point
km/h (MPH)
CRUISE shift point
km/h (MPH)
For quick acceleration in low altitude
areas and high altitude areas
[over 1,219 m (4,000 ft)]:
km/h (MPH)
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 to ensure safe operation. Do not over-rev the engine when shifting to a lower gear as it may cause
engine damage or loss of vehicle control.
Gearkm/h (MPH)
1st50 (30)
2nd89 (55)
3rd128 (80)
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4th—
5th—
TEST VALUE AND TEST LIMIT (GST ONLY — NOT APPLICABLE TO CONSULT-II)
NAEC0031S04
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 the 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 (30 test
items).
These data (test value and test limit) are specified by Test ID (TID) and Component ID (CID) and can be displayed on the GST screen.
ATF TEMP SEN/CIRCP07100710——XAT-105
VEH SPD SEN/CIR AT*6P07200720——XAT-111
ENGINE SPEED SIGP07250725——XAT-116
A/T 1ST GR FNCTNP07310731——XAT-120
A/T 2ND GR FNCTNP07320732——XAT-126
A/T 3RD GR FNCTNP07330733——XAT-132
A/T 4TH GR FNCTNP07340734——XAT-138
TCC SOLENOID/CIRCP07400740——XAT-148
A/T TCC S/V FNCTNP07440744——XAT-153
L/PRESS SOL/CIRCP07450745——XAT-162
SFT SOL A/CIRC*7P07500750——XAT-168
SFT SOL B/CIRC*7P07550755——XAT-172
MAF SENSOR*7P11021102——XEC-481
INT/V TIM V/CIR-B1P11111111——XEC-487
CONSULT-II
GST*2
DTC*1
ECM*3
SRT code
Test value/
Testlimit
1st trip DTC*1
Reference
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SWIRL CONT SOL/VP11301130——XEC-493
SWIRL CONT SOL/VP11311131——XEC-516
INT/V TIM V/CIR-B2P11361136——XEC-487
INTK TIM S/CIRC-B1P11401140——XEC-522
HO2S1 (B1)P11431143XXX*5EC-531
HO2S1 (B1)P11441144XXX*5EC-539
INTK TIM S/CIRC-B2P11451145——XEC-522
HO2S2 (B1)P11461146XXX*5EC-547
HO2S2 (B1)P11471147XXX*5EC-557
CLOSED LOOP-B1P11481148——XEC-567
HO2S1 (B2)P11631163XXX*5EC-531
HO2S1 (B2)P11641164XXX*5EC-539
SWL CON VC SW/CIRCP11651165——XEC-569
HO2S2 (B2)P11661166XXX*5EC-547
HO2S2 (B2)P11671167XXX*5EC-557
CLOSED LOOP-B2P11681168——XEC-567
ENG OVER TEMPP12171217——XEC-575
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CKP SEN (REF)/CIRCP13351335——XEC-580
CKP SENSOR (COG)P13361336——XEC-586
PURG VOLUME CONT/VP14441444——XEC-594
VENT CONTROL VALVEP14461446——XEC-606
VENT CONTROL VALVEP14481448——XEC-614
*1: 1st trip DTC No. is the same as DTC No.
*2: These numbers are prescribed by SAE J2012.
*3: In Diagnostic Test Mode II (Self-diagnostic results), these numbers are controlled by NISSAN.
*4: SRT code will not be set if the self-diagnostic result is NG.
*5: These are not displayed with GST.
*6: When the fail-safe operations for both self-diagnoses occur at the same time, the MIL illuminates.
*7: When the fail-safe operation occurs, the MIL illuminates.
NOTE:
Regarding R50 models, “-B1” indicates bank 1 and “-B2” indicates bank 2.
CONSULT-II
GST*2
DTC*1
ECM*3
SRT code
Test value/
Testlimit
1st trip DTC*1
Reference
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HOW TO ERASE EMISSION-RELATED DIAGNOSTIC INFORMATION
How to Erase DTC (With CONSULT-II)
NAEC0031S06
NAEC0031S0601
NOTE:
If the DTC is not for A/T related items (see EC-8), 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
10 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.] Then 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 from the ECM and TCM (Transmission control module).
EC-86
Page 87
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
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The emission related diagnostic information in the ECM can be erased by selecting “ERASE” in the “SELFDIAG RESULTS” mode with CONSULT-II.
If DTCs are displayed for both ECM and TCM (Transmission control module), they need to be erased individually from the ECM and TCM (Transmission control module).
How to Erase DTC (With GST)
NOTE:
If the DTC is not for A/T related items (see EC-8), skip step 2.
1. If the ignition switch stays “ON” after repair work, be sure to turn ignition switch “OFF” once. Wait at least
10 seconds and then turn it “ON” (engine stopped) 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. Select Mode 4 with GST (Generic Scan Tool).
The emission related diagnostic information in the ECM can be erased by selecting Mode 4 with GST.
IIf the battery is disconnected, the emission-related diagnostic information will be lost after approx.
24 hours.
IThe 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
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Emission-related Diagnostic Information (Cont’d)
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.
NVIS (NISSAN VEHICLE IMMOBILIZER SYSTEM — NATS)
SEF515Y
NAEC0031S08
IIf the security indicator lights up with the ignition switch in the “ON” position or “NATS MALFUNC-
TION” is displayed on “SELF-DIAG RESULTS” screen, perform self-diagnostic results mode with
CONSULT-II using NATS program card. Refer to EL-385, “NVIS (Nissan Vehicle Immobilizer System
— NATS)”.
IConfirm no self-diagnostic results of NVIS (NATS) is displayed before touching “ERASE” in “SELF-
DIAG RESULTS” mode with CONSULT-II.
IWhen replacing ECM, initialization of NVIS (NATS) system and registration of all NVIS (NATS) igni-
tion 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 NVIS (NATS)
initialization and NVIS (NATS) ignition key ID registration, refer to CONSULT-II operation manual,
IVIS/NVIS.
Malfunction Indicator Lamp (MIL)
DESCRIPTION
SEF217U
The MIL is located on the instrument panel.
1. The MIL will light up when the ignition switch is turned ON without the engine running. This is a bulb check.
IIf the MIL does not light up, refer to EL-136, “WARNING LAMPS” or see EC-720.
2. When the engine is started, the MIL should go off.
If the MIL remains on, the on board diagnostic system has detected an engine system malfunction.
On Board Diagnostic System Function
The on board diagnostic system has the following four functions.
NAEC0032
NAEC0032S01
EC-88
Page 89
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
Diagnostic Test
Mode
Mode IIgnition switch in
Mode IIIgnition switch in
KEY and ENG.
Status
“ON” position
Engine stopped
Engine running
“ON” position
Engine stopped
FunctionExplanation of Function
BULB CHECKThis function checks the MIL bulb for damage (blown,
open circuit, etc.).
If the MIL does not come on, check MIL circuit.
MALFUNCTION
WARNING
SELF-DIAGNOSTIC RESULTS This function allows DTCs and 1st trip DTCs to be read.
This is a usual driving condition. When a malfunction is
detected twice in two consecutive driving cycles (two 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 Coolant overtemperature enrichment protection
I “Misfire (Possible three way catalyst damage)”
I “Closed loop control”
I Fail-safe mode
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Engine running
MIL Flashing without DTC
HEATED OXYGEN SENSOR 1
MONITOR
This function allows the fuel mixture condition (lean or
rich), monitored by heated oxygen sensor 1, to be read.
NAEC0032S0102
If the ECM is in Diagnostic Test Mode II, MIL may flash when engine is running. In this case, check ECM
diagnostic test mode. How to Switch Diagnostic Test Mode.
How to switch the diagnostic test (function) modes, and details of the above functions are described later.How
to Switch Diagnostic Test Mode.
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
How to Switch Diagnostic Test Mode
NAEC0032S07
NOTE:
IIt is better to count the time accurately with a clock.
IIt is impossible to switch the diagnostic mode when an accelerator pedal position sensor circuit
has a malfunction.
IAlways ECM returns to Diagnostic Test Mode I after ignition switch is turned “OFF”.
How to Set Diagnostic Test Mode II (Self-diagnostic Results)
NAEC0032S0701
1. Confirm that accelerator pedal is fully released, turn ignition switch “ON” and wait 3 seconds.
2. Repeat the following procedure quickly five times within 5 seconds.
1) Fully depress the accelerator pedal.
2) Fully release the accelerator pedal.
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EC-89
Page 90
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
3. Wait 7 seconds, fully depress the accelerator pedal and keep it for approx. 10 seconds until the MIL starts
blinking.
4. Fully release the accelerator pedal.
ECM has entered to Diagnostic Test Mode II (Self-diagnostic results).
PBIB0092E
How to Set Diagnostic Test Mode II (Heated Oxygen Sensor 1 Monitor)
NAEC0032S0702
1. Set the ECM in Diagnostic Test Mode II (Self-diagnostic results). Refer to How to Set Diagnostic Test Mode
II (Self-diagnostic Results).
2. Start Engine.
ECM has entered to Diagnostic Test Mode II (Heated oxygen sensor 1 monitor).
ECM will start heated oxygen sensor 1 monitoring from the bank 1 sensor.
How to Set Diagnostic Switch Monitored Sensor from Bank 1 to Bank 2 or Vice versa
NAEC0032S0703
1. Fully depress the accelerator pedal quickly and then release it immediately.
2. Make sure that monitoring sensor has changed by MIL blinking as follows.
PBIB0093E
How to Erase Diagnostic Test Mode II (Self-diagnostic Results)
NAEC0032S0704
1. Set ECM in Diagnostic Test Mode II (Self-diagnostic results). Refer to How to Set Diagnostic Test Mode
II (Self-diagnostic Results).
2. Fully depress the accelerator pedal and keep it for more than 10 seconds. The emission-related diagnostic information has been erased from the backup memory in the ECM.
3. Fully release the accelerator pedal, and confirm the DTC 0000 is displayed.
Diagnostic Test Mode I — Bulb Check
NAEC0032S03
Inthis mode, the MIL on theinstrument panel should stay ON.If it remains OFF,check the bulb. Refer toEL-136,
“WARNING LAMPS” or see EC-720.
Diagnostic Test Mode I — Malfunction Warning
MILCondition
ONWhen the malfunction is detected or the ECM’s CPU is malfunctioning.
OFFNo malfunction.
IThese DTC numbers are clarified in Diagnostic Test Mode II (SELF-DIAGNOSTIC RESULTS).
NAEC0032S04
EC-90
Page 91
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
Malfunction Indicator Lamp (MIL) (Cont’d)
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 MIL 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 I (Malfunction warning), all displayed items are 1st trip DTCs. 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 DTCs or 1st trip DTCs. DTC No. is same as that of 1st trip DTC. These
unidentified codes can be identified by using the CONSULT-II or GST. A DTC will be used as an example for
how to read a code.
NAEC0032S08
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SEF952W
A particular trouble code can be identified by the number of four-digit numeral flashes. The “zero” is indicated
by the number of ten flashes. The length of time the 1,000th-digit numeral flashes on and off is 1.2 seconds
consisting of an ON (0.6-second) - OFF (0.6-second) cycle.
The 100th-digit numeral and lower digit numerals consist of a 0.3-second ON and 0.3-second OFF cycle.
A change from one digit numeral to another occurs at an interval of 1.0-second OFF. In other words, the later
numeral appears on the display 1.3 seconds after the former numeral has disappeared.
A change from one trouble code to another occurs at an interval of 1.8-second OFF.
In this way, all the detected malfunctions are classified by their DTC numbers. The DTC “0000” refers to no
malfunction. (See “TROUBLE DIAGNOSIS — INDEX”, EC-8.)
How to Erase Diagnostic Test Mode II (Self-diagnostic Results)
The DTC can be erased from the back up memory in the ECM by depressing accelerator pedal. Refer to How
to Switch Diagnostic Test Mode.
IIf the battery is disconnected, the DTC will be lost from the backup memory after approx 24 hours.
IBe careful not to erase the stored memory before starting trouble diagnoses.
Diagnostic Test Mode II — Heated Oxygen Sensor 1 Monitor
In this mode, the MIL displays the condition of the fuel mixture (lean or rich) which is monitored by the heated
oxygen sensor 1.
MILFuel mixture condition in the exhaust gasAir fuel ratio feedback control condition
ONLean
Closed loop system
OFFRich
*Remains ON or OFFAny conditionOpen loop system
NAEC0032S0801
NAEC0032S09
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*: Maintains conditions just before switching to open loop.
To check the heated oxygen sensor 1 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
MIL comes ON more than 5 times within 10 seconds with engine running at 2,000 rpm under no-load.
EC-91
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ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
OBD System Operation Chart
OBD System Operation Chart
RELATIONSHIP BETWEEN MIL, 1ST TRIP DTC, DTC, AND DETECTABLE ITEMS
NAEC0033
NAEC0033S01
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-72.
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
For details about patterns “B” and “C” under “Fuel Injection System” and “Misfire”, see EC-94.
For details about patterns “A” and “B” under “Other”, see EC-96.
*1: Clear timing is at the moment OK is detected.
*2: Clear timing is when the same malfunction is detected in the 2nd trip.
*1, *2*1, *21 (pattern B)
EC-92
Page 93
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”
GI
=NAEC0033S03
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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.)
*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
SEF392S
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 once (pattern C)
without the same malfunction after
DTC is stored in ECM.
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EC-93
Page 94
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 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 malfunction.
IThe MIL will go off when the B counter reaches 3. (*2 in “OBD SYSTEM OPERATION CHART”)
NAEC0033S04
NAEC0033S0401
<Driving Pattern C>
NAEC0033S0402
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:
Engine speed: 850 rpm, Calculated load value: 30%, Engine coolant temperature: 80°C (176°F)
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 once without the same malfunction after DTC
is stored in ECM.
EC-94
Page 95
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”
GI
NAEC0033S05
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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 40
times (pattern A) without the same
malfunction.
(The DTC and the freeze frame
data still remain in ECM.)
*5: When a malfunction is detected
for the first time, the 1st trip DTC
SEF393S
and the 1st trip freeze frame data
will be stored in ECM.
*6: 1st trip DTC will be cleared after
vehicle is driven once (pattern B)
without the same malfunction.
*7: When the same malfunction is
detected in the 2nd trip, the 1st
trip freeze frame data will be
cleared.
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EC-95
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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>
NAEC0033S0601
NAEC0033S06
AEC574
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>
NAEC0033S0602
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”, EC-92).
EC-96
Page 97
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
CONSULT-II
SEF941Y
MBIB0233E
CONSULT-II
CONSULT-II INSPECTION PROCEDURE
1.Turn ignition switch OFF.
2.Connect CONSULT-II and “CONSULT-II CONVERTER” to
data link connector,which is located under LH dash panel near
the fuse box cover.
3.Turn ignition switch ON.
4.Touch “START (NISSAN BASED VHCL)”.
5.Touch “ENGINE”.
If “ENGINE” is not indicated, go to GI-40, “CONSULT-II Data
Link Connector (DLC) Circuit”.
=NAEC0034
NAEC0034S01
GI
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SEF948Y
SEF824Y
6.Perform each diagnostic test mode according to each service
procedure.
For further information, see the CONSULT-II Operation
Manual.
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EC-97
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CONSULT-II (Cont’d)
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
ENGINE CONTROL COMPONENT PARTS/CONTROL
SYSTEMS APPLICATION
DIAGNOSTIC TEST MODE
NAEC0034S02
SELF-DIAGNOSTIC
Item
Crankshaft position sensor
(POS)
Crankshaft position sensor (REF)XXX
Mass air flow sensorXXX
Engine coolant temperature sen-
sor
Heated oxygen sensor 1XXXXX
Heated oxygen sensor 2XXXXX
Vehicle speed sensorXXXX
Throttle position sensorXXX
Fuel tank temperature sensorXXXX
EVAP control system pressure
sensor
Absolute pressure sensorXXX
WORK
SUP-
PORT
RESULTS
FREEZE
DTC*1
FRAME
DATA*2
XXXX
XXXXX
XXX
DATA
MONI-
TOR
DATA
MONI-
TOR
(SPEC)
ACTIVE
TEST
DTC & SRT
CONFIRMATION
DTC
SRT
STATUS
WORK
SUP-
PORT
Intake air temperature sensorXXX
Knock sensorX
Ignition switch (start signal)XX
INPUT
Closed throttle position switchXXX
Closed throttle position switch
(throttle position sensor signal)
Air conditioner switchXX
ENGINE CONTROL COMPONENT PARTS
Park/neutral position (PNP)
switch
Power steering oil pressure
switch
Battery voltageXX
Ambient air temperature switchXX
Load signalXX
Swirl control valve control
control solenoid valve
Air conditioner relayXX
Fuel pump relayXXXX
Heated oxygen sensor 1 heaterXXXX
Heated oxygen sensor 2 heaterXXXX
OUTPUT
EVAP canister vent control valveXXXX
Vacuum cut valve bypass valveXXXXX
Swirl control valve control sole-
noid valve
ENGINE CONTROL COMPONENT PARTS
VIAS control solenoid valveXXX
Intake valve timing control sole-
noid valve
Calculated load valueXXX
WORK
SUP-
PORT
RESULTS
FREEZE
DTC*1
(Ignition
signal)
FRAME
DATA*2
X
XXXXX
XXXX
XXXX
DATA
MONI-
TOR
XXX
DATA
MONI-
TOR
(SPEC)
ACTIVE
TEST
CONFIRMATION
STATUS
DTC & SRT
SRT
DTC
WORK
SUP-
PORT
GI
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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-74.
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EC-99
Page 100
CONSULT-II (Cont’d)
ON BOARD DIAGNOSTIC SYSTEM DESCRIPTION
FUNCTION
Diagnostic test modeFunction
WORK SUPPORT
SELF-DIAG RESULTS
DATA MONITORInput/Output data in the ECM can be read.
DATA MONITOR (SPEC)
ACTIVE TEST
FUNCTION TEST
DTC & SRT CONFIRMATION
ECM PART NUMBERECM part number 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
Input/Output specification of the basic fuel schedule, AFM, A/F feedback control value and the
other data monitor items can be read.
Diagnostic Test Mode in which CONSULT-II drives some actuators apart from the ECMs and also
shifts some parameters in a specified range.
Conducted by CONSULT-II instead of a technician to determine whether each system is “OK” or
“NG”.
The status of system monitoring tests and the self-diagnosis status/result can be confirmed.
=NAEC0034S03
EC-100
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