2011 INFINITI QX56 light

BACK DOORDLK-235
< REMOVAL AND INSTALLATION >
C
DE
F
G H
I
J
L
M A
B
DLK
N
O P
Unit: mm (in)
1. Remove luggage rear plate mask. Refer to INT-35, "LUGGAGE REAR PLATE : Removal and Installation".
2. Loosen back door striker mounting bolts.
3. Loosen back door hinge mounting nuts (back door side).
4. Loosen bumper rubber (side and lower).
5. Lift up back door approximately 100 – 150 mm (3.937 – 5.906 in) height then close it lightly and check that
it is engaged firmly with back door closed.
6. Check the clearance and surface height.
7. Finally tighten back door hinge, bumper rubber, and back door striker.
8. Install luggage rear plate mask. Refer to INT-35, "
LUGGAGE REAR PLATE : Removal and Installation".
BACK DOOR STRIKER ADJUSTMENT
Adjust back door striker so that i becomes parallel with back door lock insertion direction.
BACK DOOR STRIKER
BACK DOOR STRIKER : Removal and InstallationINFOID:0000000006226089
REMOVAL
1. Remove luggage rear plate. Refer to INT-35, "LUGGAGE REAR PLATE : Removal and Installation".
2. Remove mounting TORX bolts, and then remove back door striker.
INSTALLATION
Note the following items, and then install in the reverse order of removal.
CAUTION:
 Check back door open/close ope ration after installation.
 When removing and installing b ack door striker, check to perform th e fitting adjustment. Refer to
DLK-234, "
BACK DOOR ASSEMBLY : Adjustment".
Portion Standard
Difference
(LH/RH, MAX)
Roof – Rear roof spoiler A – A H Clearance
5.0 – 9.0
(0.197 – 0.354) —
I Surface height (
− 1.0) – (+3.0)
[( −0.039) – (+0.118)] —
Body side outer panel –
Rear roof spoiler B – B J Clearance 3.8 – 7.8
(0.150 – 0.307) ≤
2.0
(0.079)
Body side outer panel –
Back door glass C – CK Clearance
3.0 – 7.0
(0.118 – 0.276) ≤
2.0
(0.079)
L Surface height 0.0 – 4.0
(0.000 – 0.157) ≤
2.0
(0.079)
Body side outer panel –
Back door D – DM Clearance
4.0 – 6.0
(0.157 – 0.236) ≤
1.0
(0.039)
N Surface height (
− 1.0) – (+1.0)
[( −0.039) – (+0.039)] ≤
1.0
(0.039)
Rear combination lamp
– Back up lamp E – EO Clearance
2.5 – 7.5
(0.098 – 0.295) ≤
2.2
(0.087)
P Surface height (
− 2.2) – (+2.2)
[( −0.087) – (+0.087)] ≤
2.2
(0.087)
Rear bumper fascia –
Back door F – F Q Clearance 2.9 – 7.1
(0.114 – 0.280) ≤
2.1
(0.083)
Rear bumper fascia –
Back door G – G R Clearance 4.0 – 8.0
(0.157 – 0.315) —
Revision: 2010 May2011 QX56

4WD WARNING LAMPDLN-97
< DTC/CIRCUIT DIAGNOSIS > [TRANSFER: ATX90A]
C
EF
G H
I
J
K L
M A
B
DLN
N
O P
4WD WARNING LAMP
Component Function CheckINFOID:0000000006222308
1.CHECK 4WD WARNING LAMP FUNCTION
1. Turn the ignition switch OFF to ON.
2. Check that 4WD warning lamp light up.
Is the inspection result normal?
YES >> INSPECTION END
NO >> Proceed diagnosis procedure. Refer to DLN-97, "
Diagnosis Procedure".
Diagnosis ProcedureINFOID:0000000006222309
1.CHECK POWER SUPPLY AND GROUND CIRCUIT
Perform the trouble diagnosis for power supply and ground circuit. Refer to DLN-64, "
Diagnosis Procedure".
Is the inspection result normal?
YES >> GO TO 2.
NO >> Repair or replace the error-detected parts.
2.PERFORM SELF-DIAGNOSIS
With CONSULT-III
Perform self-diagnosis for “ALL MODE AWD/4WD”.
Is any DTC detected?
YES >> Check the DTC.
NO >> GO TO 3.
3.CHECK 4WD WARNING LAMP SIGNAL
With CONSULT-III
1. Turn the ignition switch ON. CAUTION:
Never start the engine.
2. Check “4WD FAIL LAMP” of CONSULT-III “DATA MONITOR” for “ALL MODE AWD/4WD”.
Does the item on
“DATA MONITOR” indicate “On”?
YES >> Check combination meter. Refer to MWI-64, "COMBINATION METER : Diagnosis Procedure".
NO >> Replace transfer control unit. Refer to DLN-107, "
Removal and Installation".
Revision: 2010 May2011 QX56

HEAVY TIGHT-CORNER BRAKING SYMPTOM OCCURS
DLN-99
< SYMPTOM DIAGNOSIS > [TRANSFER: ATX90A]
C
EF
G H
I
J
K L
M A
B
DLN
N
O P
SYMPTOM DIAGNOSIS
HEAVY TIGHT-CORNER BRAKING SYMPTOM OCCURS
DescriptionINFOID:0000000006222312
Heavy tight-corner braking symptom o ccurs when the vehicle is driven and the steering wheel is turned fully to
either side after the engine is started.
NOTE:
Light tight-corner braking symptom may occur dependi ng on driving conditions. This is not malfunction.
Diagnosis ProcedureINFOID:0000000006222313
1.PERFORM ECM SELF-DIAGNOSIS
With CONSULT-III
Perform self-diagnosis for “ECM”.
Is any DTC detected?
YES >> Check the DTC. Refer to EC-98, "DTC Index".
NO >> GO TO 2.
2.PERFORM SELF-DIAGNOSIS
With CONSULT-III
Perform self-diagnosis for “ALL MODE AWD/4WD”.
Is any DTC detected?
YES >> Check the DTC. Refer to DLN-29, "DTC Index".
NO >> GO TO 3.
3.CHECK TRANSFER INTERNAL FUNCTION
With CONSULT-III
1. Remove transfer control actuator. Refer to DLN-114, "
Removal and Installation".
2. Turn the actuator shaft. Refer to DLN-114, "
Inspection".
3. Check “ROTARY POSI SEN” of CONSULT-II I “DATA MONITOR” for “ALL MODE AWD/4WD”.
Is the inspection result normal?
YES >> INSPECTION END
NO >> Transfer assembly is mechanical malfunction. Replace transfer assembly. Refer to DLN-121,
"Removal and Installation".
Monitor item Condition Status
ROTARY POSI SEN Turn the actuator shaft. Value is changing
Revision: 2010 May2011 QX56

DLN-130
< REMOVAL AND INSTALLATION >[FRONT PROPELLER SHAFT: 2F P15]
FRONT PROPELLER SHAFT
1. Put a matching mark (A) between propeller shaft and flange
yoke and remove snap rings (1).
CAUTION:
For matching mark, use paint. Never damage the surface.
2. Lightly tap bottom of yoke using a copper hammer and remove journal bearing.
CAUTION:
Never damage the yoke.
ASSEMBLY
1. Install journal bearing to journal.CAUTION:
 Never reuse journal or journal bearing.
 Always replace journal, journal b earing, and snap rings as a set.
 Apply multi-purpose grease to journal bearing.
2. Install bearing (1) using a vise. CAUTION:
Never damage bearing or flange yoke.
3. Install journal to propeller shaft so that grease nipple (1) on jour- nal portion is in the same direction.
CAUTION:
Never reuse journal.
4. Measure journal axial play. If necessary, select the appropriate snap ring.
JPDID0375ZZ
PDA0034D
JSDIA0370ZZ
JPDID0327ZZ
Revision: 2010 May2011 QX56

DLN-138
< REMOVAL AND INSTALLATION >[REAR PROPELLER SHAFT: 2F P26]
REAR PROPELLER SHAFT
1. Put a matching mark between propeller shaft and flange yoke
and remove snap rings (1).
CAUTION:
For matching mark, use paint. Never damage the surface.
2. Lightly tap bottom of yoke using a copper hammer and remove journal bearing.
CAUTION:
Never damage the yoke.
3. Remove grease nipple.
ASSEMBLY
1. Install journal bearing to journal. CAUTION:
 Never reuse journal or journal bearing.
 Always replace journal, journal b earing, and snap rings as a set.
 Apply multi-purpose grease to journal bearing.
2. Install bearing (1) using a vise. CAUTION:
Never damage bearing or flange yoke.
3. Install journal to propeller shaft so that grease nipple (1) on jour- nal portion is in the same direction.
CAUTION:
Never reuse journal.
JSDIA0369ZZ
PDA0034D
JSDIA0370ZZ
JPDID0327ZZ
Revision: 2010 May2011 QX56

REAR PROPELLER SHAFTDLN-145
< REMOVAL AND INSTALLATION > [REAR PROPELLER SHAFT: 2S1410]
C
EF
G H
I
J
K L
M A
B
DLN
N
O P
2. Remove snap ring.
3. Lightly tap bottom of yoke using a copper hammer and remove journal bearing.
CAUTION:
Never damage the yoke.
ASSEMBLY
1. Install journal bearing to journal.CAUTION:
 Never reuse journal or journal bearing.
 Always replace journal, journal b earing, and snap rings as a set.
 Apply multi-purpose grease to journal bearing.
2. Install bearing (1) using a vise. CAUTION:
Never damage bearing or flange yoke.
3. Measure journal axial play. If necessary, select the appropriate snap ring.
a. While pushing to 98 N·m (10 kg-m, 72 ft-lb), check the clearance between snap ring (1) and needle bearing (2).
b. If journal axial play is outside the specification, use a thicker/ thinner snap ring to adjust.
CAUTION:
 Never reuse snap ring.
 Select snap rings so that thickness difference between LH
and RH is within 0.02 mm (0.0008 in).
APD011
PDA0034D
JSDIA0370ZZ
Journal axial play : Refer to DLN-147,
"Journal Axial Play"
JPDID0331ZZ
Revision: 2010 May2011 QX56

EC-10
< PRECAUTION >[VK56VD]
PRECAUTIONS
CAUTION:
Comply with the following cautions to
prevent any error and malfunction.
 Install the xenon bulb securely. (Ins ufficient bulb socket installation may melt the bulb, the connec-
tor, the housing, etc. by high-v oltage leakage or corona discharge.)
 Never perform HID circuit in spection with a tester.
 Never touch the xenon bulb glass with ha nds. Never put oil and grease on it.
 Dispose of the used xenon bulb after packing it in thick vinyl without breaking it.
 Never wipe out dirt and cont amination with organic solven t (thinner, gasoline, etc.).
On Board Diagnostic (OBD) System of Engine and A/TINFOID:0000000006217652
The ECM has an on board diagnostic system. It will illuminate the malfunction indicator lamp (MIL) to warn the
driver of a malfunction causing emission deterioration.
CAUTION:
 Always turn the ignition switch OFF and disconnect the negative battery cable before any repair or
inspection work. The open/short circuit of related sw itches, sensors, solenoid valves, etc. will cause
the MIL to illuminate.
 Always connect and lock the conn ectors securely after work. A loose (unlocked) connector will
cause the MIL to illuminate 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-lock-
ing type harness connector. For descripti on and how to disconnect, refer to EC-51, "
Diagnosis
Description".
 Always route and secure the harnesses properly afte r work. The interference of the harness with a
bracket, etc. may cause the MIL to illu minate due to the short circuit.
 Always connect rubber tubes properly after work. A misconnected or disconnected rubber tube may
cause the MIL to illuminate due to the malfunction of the EVAP system or fuel injection system, etc.
 Always erase the unnecessary malfunction information (repairs completed) from the ECM and TCM
(Transmission control module) before re turning the vehicle to the customer.
General PrecautionsINFOID:0000000006217653
Always use a 12 volt battery as power source.
 Never attempt to disconnect battery cables while engine is
running.
 Before connecting or disconnecting the ECM harness con-
nector, turn ignition switch OFF and disconnect negative bat-
tery cable. Failure to do so may damage the ECM because
battery voltage is applied to ECM even if ignition switch is
turned OFF.
 Before removing parts, turn ig nition switch OFF and then dis-
connect battery ground cable.
 Never disassemble ECM.
 If a battery cable is disconnected, the memory will return to
the ECM value.
The ECM will now start to self-control at its initial value. Thus,
engine operation can vary slight ly in this case. However, this
is not an indication of a ma lfunction. Never replace parts
because of a slight variation.
 If the battery is disconnected, the following emission-related
diagnostic information will be lost within 24 hours.
- Diagnostic trouble codes
- 1st trip diagnostic trouble codes
- Freeze frame data
- 1st trip freeze frame data
- System readiness test (SRT) codes
- Test values
SEF289H
JMBIA0057ZZ
Revision: 2010 May2011 QX56

PRECAUTIONSEC-11
< PRECAUTION > [VK56VD]
C
D
E
F
G H
I
J
K L
M A
EC
NP
O

When connecting ECM harness connector (A), fasten (B) it
securely with a lever as far as it will go as shown in the figure.
-ECM (1)
- Loosen (C)
 When connecting or disconnect ing pin connectors into or
from ECM, never damage pin terminals (bends or break).
Check that there are not any bends or breaks on ECM pin ter-
minal, when connect ing pin connectors.
 Securely connect ECM harness connectors.
A poor connection can cause an extremely high (surge) volt-
age to develop in coil and cond enser, thus resulting in dam-
age to ICs.
 Keep engine control system harness at least 10 cm (4 in) away
from adjacent harness, to prevent engine control system mal-
functions due to receiving externa l noise, degraded operation
of ICs, etc.
 Keep engine control system parts and harness dry.
 Before replacing ECM, perform ECM Terminals and Reference
Value inspection and check that ECM functions properly.
Refer to EC-72, "
Reference Value".
 Handle mass air flow sensor carefully to avoid damage.
 Never clean mass air flow sensor with any type of detergent.
 Never disassemble electric th rottle control actuator.
 Even a slight leakage in the air intake system can cause seri-
ous incidents.
 Never shock or jar the camshaf t position sensor, crankshaft
position sensor.
 After performing each TROUBL E DIAGNOSIS, perform DTC
Confirmation Procedure or Component Function Check.
The DTC should not be displ ayed in the DTC Confirmation
Procedure if the repair is completed. The Component Func-
tion Check should be a good resu lt if the repair is completed.
JMBIA0029ZZ
PBIB0090E
MEF040D
SEF217U
Revision: 2010 May2011 QX56