lock INFINITI M35 2007 Factory Service Manual

WARNING CHIME
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Revision: 2007 April2007 M35/M45
WARNING CHIMEPFP:24814
System DescriptionNKS003UY

The buzzer (1) for warning chime system is installed in the com-
bination meter.

The buzzer sounds when the combination meter receives
buzzer output signal from each unit through unified meter and A/
C amp.
POWER SUPPLY AND GROUND CIRCUIT
Power is supplied at all times

through 50A fusible link (letter F , located in the fuse and fusible link block)

to BCM terminal 55,

through 10A fuse [No. 21, located in the fuse block (J/B)]

to BCM terminal 42, and

to combination meter terminal 23,

through 10A fuse [No. 19, located in the fuse block (J/B)]

to unified meter and A/C amp. terminal 54.
When ignition switch is in ON or START position, power is supplied

through 15A fuse [No. 1, located in the fuse block (J/B)]

to BCM terminal 38,

through 10A fuse [No. 12, located in the fuse block (J/B)]

to unified meter and A/C amp. terminal 53,

through 10A fuse [No. 14, located in the fuse block (J/B)]

to combination meter terminal 12.
Ground is supplied

to BCM terminals 52,

to unified meter and A/C amp. terminals 55 and 71, and

to combination meter terminals 9, 10 and 11,

through grounds M16 and M70.
SKIB2633J

LANE DEPARTURE WARNING SYSTEM
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Revision: 2007 April2007 M35/M45
System Diagram
Components Description
NOTE:
*: This indicates in a few seconds for the system check during ignition switch ON.
POWER SUPPLY AND GROUND CIRCUIT
With the ignition switch in the ON or START position, power is supplied

through 10A fuse [No. 12, located in the fuse block (J/B)]

to LDW camera unit terminal 1.
Ground is supplied

to LDW camera unit terminals 6 and 12

through grounds M16 and M70.
Action TestNKS003VH
LDW SYSTEM RUNNING TEST
WARNING:

Be careful when performing road test.

Understand “Precautions” and “System Description” well before the road test. Refer to DI-75,
"Precautions for Lane Departure Warning (LDW) system" and DI-75, "System Description" .
Function Check
Check the LDW system operation according to the condition that the warning function works. Refer to DI-75,
"LDW SYSTEM OPERATION" .
PKIC0698E
Component Description
LDW camera unitDetects the lane marker by the built-in camera, gives judgement for the warning according to the
result of detection and signals from each unit, and transmits the operation signal to LDW chime and
LDW indicator lamp.
LDW switch

Selects ON/OFF of the system.

Indicates ON/OFF of the signal with LDW system ON indicator.
LDW chime Gives a warning chime according to the direction from LDW camera unit.
LDW indicator lampInstalled in combination meter, and indicates the system condition.

Blinks when LDW system is functioning to alert the driver.

Stays on when LDW system is malfunctioning.*
BCM Transmits turn indicator signal to LDW camera unit with CAN communication signal.
ABS actuator and electric unit
(control unit)Transmits vehicle speed signal to LDW camera unit with CAN communication signal.
TCM Transmits vehicle speed signal to LDW camera unit with CAN communication signal. (For detecting
incorrect speed.)

COMPASS
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Revision: 2007 April2007 M35/M45
TroubleshootingNKS004F4

The electronic compass is highly protected from changes in most magnetic fields. However, some large
changes in magnetic fields can affect it. Some examples are (but not limited to): high tension power lines,
large steel buildings, subways, steel bridges, automatic car washes, large piles of scrap metal, etc. While
this does not happen very often, it is possible.

During normal operation, the Compass Mirror will continuously update the compass calibration to adjust
for gradual changes in the vehicle's magnetic “remnant” field. If the vehicle is subjected to high magnetic
influences, the compass may appear to indicate false headings, become locked, or appear that it is
unable to be calibrated. If this occurs, perform the calibration procedure.

If at any time the compass continually displays the incorrect direction or the reading is erratic or locked,
verify the correct zone variance.
Troubleshooting Chart
Symptom Cause Solution / Reference
The compass display reads “C”.

Compass is not calibrated.

Incorrect zone variance setting.

Large change in magnetic field (Steel
bridges, subways, concentrations of
metal, carwashes, etc.)

Compass was calibrated incorrectly or in
the presence of a strong magnetic field.Perform Calibration.
Refer to DI-104, "
Calibration Procedure" . Compass shows the wrong direction.
Compass does not change direction –
appears “Locked”.
Compass does not show all the directions,
one or more is missing.
The compass was calibrated but it “loses”
calibration.
On long trips the compass shows the
wrong direction.Perform Zone Variation Setting if correct
reading is desired in that location.
Refer to DI-104, "
Zone Variation Setting
Procedure" .
Compass does not work – No direction is
displayed.Compass not turned ON.Check for green LED indicator (inside mir-
ror switch).
No power to inside mirror. Check power supply circuit.

DI-104
COMPASS
Revision: 2007 April2007 M35/M45
Zone Variation Setting ProcedureNKS004F5
NOTE:
The zone setting is factory preset (“default” setting) to zone 8.
1. Press and hold the compass switch for 3 – 9 seconds.
2. The current zone setting appears on the compass display.
3. Find the current geographical location number in the Zone Varia-
tion Chart.
4. Select the new zone number. (Press the compass switch until
the new zone number appears on the compass display.)
5. After select the new zone number, the compass display will
automatically shows a direction within a few seconds.
6. Preform the following Calibration Procedure for more accurate
indications.
Calibration ProcedureNKS004F6
NOTE:
The compass calibrates itself under normal driving conditions. However, occasional circumstances may cause
the compass to operate inaccurately. Example: Driving from rural (wide open) areas to crowded city areas, or
if an aftermarket (i.e., non original equipment) antenna with a magnetic base is attached to the vehicle. Cali-
brate the mirror compass if the display shows only one direction or a limited number of directions.
NOTE:

If “magnetic hats” are used in the dealership for vehicle identification, remove the hat from the vehicle
before performing the following steps. Do NOT put the hat back on the vehicle after the procedure is com-
pleted.

Drive the vehicle to an open level area; away from large metallic objects, structures, and overhead power
lines.

Turn off “non-essential” electrical accessories (rear window defrost, heater/air conditioning, wipers) and
close the doors.
1. Verify the correct compass zone setting for the geographical location. Refer to DI-104, "
Zone Variation
Setting Procedure" .
2. Press and hold the compass switch for more than 9 seconds.
3. “C” is displayed on the compass display, when calibration starts.
4. Drive slowly [less than 8 km/h (5 mph)] in a circle until the “C / CAL” is replaced with primary headings (N,
NE, E, SE, S, SW, W, or NW).
NOTE:
This will require driving at least 2 complete 360 degree circles; 3 complete circles may be required.
5. The compass calibration procedure is now complete. The compass should operate normally.
NOTE:
If at any time the compass continually displays the incorrect direction or the reading is erratic or locked,
repeat the calibration procedure.
SEL168Y

CLOCK
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Revision: 2007 April2007 M35/M45
CLOCKPFP:25820
Wiring Diagram — CLOCK —NKS003W8
TKWT5289E

DI-108
CLOCK
Revision: 2007 April2007 M35/M45
Removal and Installation of ClockNKS003W9
REMOVAL
1. Remove cluster lid C (1). Refer to IP-17, "Removal and Installa-
tion of Cluster Lid C" .
2. Remove preset switch. Refer to AV- 1 3 3 , "
Preset Switch" (With-
out mobile entertainment system) or AV- 2 8 4 , "
Preset Switch"
(With mobile entertainment system).
3. Disengage tabs, and remove clock (2) from cluster lid C (1).
INSTALLATION
Installation is the reverse order of removal.
SKIB2954J

INDEX FOR DTC
EC-19
[VQ35DE]
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EC
Revision: 2007 April2007 M35/M45
*1: 1st trip DTC No. is the same as DTC No.
*2: This number is prescribed by SAE J2012.
*3: In Diagnostic Test Mode II (Self-diagnostic results), this number is controlled by NISSAN.
*4: The troubleshooting for this DTC needs CONSULT-II.
*5: When the fail-safe operations for both self-diagnoses occur, the MIL illuminates.
*6: Models with ICC.P1610 - P1615 1610 - 1615 NATS MALFUNCTIONEC-53
P1705 1705 TP SEN/CIRC A/TAT-132
P1715 1715 IN PULY SPEEDEC-588
P1730 1730 A/T INTERLOCKAT-142
P1752 1752 I/C SOLENOID/CIRCAT-147
P1754 1754 I/C SOLENOID FNCTNAT-149
P1757 1757 FR/B SOLENOID/CIRCAT-151
P1759 1759 FR/B SOLENOID FNCTAT-153
P1762 1762 D/C SOLENOID/CIRCAT-155
P1764 1764 D/C SOLENOID FNCTNAT-157
P1767 1767 HLR/C SOL/CIRCAT-159
P1769 1769 HLR/C SOL FNCTNAT-161
P1772 1772 LC/B SOLENOID/CIRCAT-163
P1774 1774 LC/B SOLENOID FNCTAT-165
P1805 1805 BRAKE SW/CIRCUITEC-589
P2100 2100 ETC MOT PWREC-598
P2101 2101 ETC FUNCTION/CIRCEC-604
P2103 2103 ETC MOT PWREC-598
P 2 11 8 2 11 8 E T C M O TEC-610
P 2 11 9 2 11 9 E T C A C T REC-615
P2122 2122 APP SEN 1/CIRCEC-617
P2123 2123 APP SEN 1/CIRCEC-617
P2127 2127 APP SEN 2/CIRCEC-624
P2128 2128 APP SEN 2/CIRCEC-624
P2135 2135 TP SENSOREC-631
P2138 2138 APP SENSOREC-638
P2A00 2A00 A/F SENSOR1 (B1)EC-646
P2A03 2A03 A/F SENSOR1 (B2)EC-646
DTC*1
Items
(CONSULT-II screen terms)Reference page
CONSULT-II
GST*
2ECM*3

EC-20
[VQ35DE]
INDEX FOR DTC
Revision: 2007 April2007 M35/M45
Alphabetical IndexNBS004RV
NOTE:

If DTC U1000 or U1001 is displayed with other DTC, first perform the trouble diagnosis for DTC
U1000, U1001. Refer to EC-161, "
DTC U1000, U1001 CAN COMMUNICATION LINE" .

If DTC U1010 is displayed with other DTC, first perform the trouble diagnosis for DTC U1010. Refer
to EC-164, "
DTC U1010 CAN COMMUNICATION" .
Items
(CONSULT-II screen terms)DTC*
1
Reference page
CONSULT-II
GST*
2ECM*3
A/F SEN1 HTR (B1) P0031 0031EC-170
A/F SEN1 HTR (B1) P0032 0032EC-170
A/F SEN1 HTR (B2) P0051 0051EC-170
A/F SEN1 HTR (B2) P0052 0052EC-170
A/F SENSOR1 (B1) P0130 0130EC-234
A/F SENSOR1 (B1) P0131 0131EC-244
A/F SENSOR1 (B1) P0132 0132EC-253
A/F SENSOR1 (B1) P0133 0133EC-262
A/F SENSOR1 (B1) P2A00 2A00EC-646
A/F SENSOR1 (B2) P0150 0150EC-234
A/F SENSOR1 (B2) P0151 0151EC-244
A/F SENSOR1 (B2) P0152 0152EC-253
A/F SENSOR1 (B2) P0153 0153EC-262
A/F SENSOR1 (B2) P2A03 2A03EC-646
A/T INTERLOCK P1730 1730AT-142
A/T TCC S/V FNCTN P0744 0744AT-128
APP SENSOR P2138 2138EC-638
APP SEN 1/CIRC P2122 2122EC-617
APP SEN 1/CIRC P2123 2123EC-617
APP SEN 2/CIRC P2127 2127EC-624
APP SEN 2/CIRC P2128 2128EC-624
ASCD BRAKE SW P1572 1572EC-567 (Models with ICC)
EC-576
(Models with ASCD)
ASCD SW P1564 1564EC-552
(Models with ICC)
EC-559
(Models with ASCD)
ASCD VHL SPD SEN P1574 1574EC-584
(Models with ICC)
EC-586
(Models with ASCD)
ATF TEMP SEN/CIRC P0710 0710AT-135
BAT CURRENT SENSOR P1550 1550EC-524
BAT CURRENT SENSOR P1551 1551EC-531
BAT CURRENT SENSOR P1552 1552EC-531
BAT CURRENT SENSOR P1553 1553EC-538
BAT CURRENT SENSOR P1554 1554EC-545
BRAKE SW/CIRCUIT P1805 1805EC-589
CAN COMM CIRCUIT U1000
1000*4EC-161
CAN COMM CIRCUIT U1001
1001*4EC-161
CKP SEN/CIRCUIT P0335 0335EC-364
CLOSED LOOP-B1 P1148 1148EC-496

EC-24
[VQ35DE]
PRECAUTIONS
Revision: 2007 April2007 M35/M45
PRECAUTIONSPFP:00001
Precautions for Supplemental Restraint System (SRS) “AIR BAG” and “SEAT
BELT PRE-TENSIONER”
NBS004RW
The Supplemental Restraint System such as “AIR BAG” and “SEAT BELT PRE-TENSIONER”, used along
with a front seat belt, helps to reduce the risk or severity of injury to the driver and front passenger for certain
types of collision. This system includes seat belt switch inputs and dual stage front air bag modules. The SRS
system uses the seat belt switches to determine the front air bag deployment, and may only deploy one front
air bag, depending on the severity of a collision and whether the front occupants are belted or unbelted.
Information necessary to service the system safely is included in the SRS and SB section of this Service Man-
ual.
WARNING:

To 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 per-
formed by an authorized NISSAN/INFINITI dealer.

Improper 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, see the SRS section.

Do 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 and/or orange harnesses or
harness connectors.
Precautions for Procedures without Cowl Top CoverNBS004RX
When performing the procedure after removing cowl top cover, cover
the lower end of windshield with urethane, etc.
On Board Diagnostic (OBD) System of Engine and A/TNBS004RY
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:

Be sure to turn the ignition switch OFF and disconnect the negative battery cable before any
repair or inspection work. The open/short circuit of related switches, sensors, solenoid valves,
etc. will cause the MIL to light up.

Be 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.)

Certain 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 PG-104, "
HAR-
NESS CONNECTOR" .

Be 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.

Be 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 EVAP system or fuel injection system,
etc.

Be sure to erase the unnecessary malfunction information (repairs completed) from the ECM and
TCM (Transmission control module) before returning the vehicle to the customer.
PIIB3706J

EC-42
[VQ35DE]
EVAPORATIVE EMISSION SYSTEM
Revision: 2007 April2007 M35/M45
Component InspectionNBS004SC
EVAP CANISTER
Check EVAP canister as follows:
1. Block port (B).
2. Blow air into port (A) and check that it flows freely out of port (C).
3. Release blocked port (B).
4. Apply vacuum pressure to port (B) and check that vacuum pres-
sure exists at the ports (A) and (C).
5. Block port (A) and (B).
6. Apply pressure to port (C) and check that there is no leakage.
FUEL TANK VACUUM RELIEF VALVE (BUILT INTO FUEL FULLER CAP)
1. Wipe clean valve housing.
2. Check valve opening pressure and vacuum.
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 incor-
rect fuel filler cap is used, the MIL may come on.
EVAP CANISTER PURGE VOLUME CONTROL SOLENOID VALVE
Refer to EC-407 .
FUEL TANK TEMPERATURE SENSOR
Refer to EC-336 .
EVAP CANISTER VENT CONTROL VALVE
Refer to EC-420 .
EVAP CONTROL SYSTEM PRESSURE SENSOR
Refer to EC-430 .
PBIB2728E
SEF445Y
Pressure:
15.3 - 20.0 kPa (0.156 - 0.204 kg/cm2 , 2.22
- 2.90 psi)
Va c u u m :
−6.0 to −3.3 kPa (−0.061 to −0.034 kg/cm
2 ,
−0.87 to −0.48 psi)
SEF943S