Components
COMPONENTS
ILLUSTRATION
ILLUSTRATION
Installation
INSTALLATION
PROCEDURE
1. INSTALL NO. 2 ECM BRACKET
(a) Install the No. 2 ECM bracket to the ECM with the 2 screws.
Torque:
3.2 N·m {33 kgf·cm, 28 in·lbf}
2. INSTALL ECM BRACKET
(a) Install the ECM bracket to the ECM with the 2 screws.
Torque:
3.2 N·m {33 kgf·cm, 28 in·lbf}
3. INSTALL ECM
(a) Install the ECM to the instrument panel reinforcement assembly with the 2 bolts and nut.
Torque:
5.0 N·m {51 kgf·cm, 44 in·lbf}
(b) Connect the 6 connectors.
(c) Engage the clamp to install the wire harness.
4. INSTALL LOWER INSTRUMENT PANEL ASSEMBLY
5. INSTALL LOWER NO. 2 INSTRUMENT PANEL AIRBAG ASSEMBLY
6. INSTALL GLOVE COMPARTMENT PLATE
7. INSTALL INSTRUMENT SIDE PANEL RH
8. CONNECT CABLE TO NEGATIVE BATTERY TERMINAL
Torque:
5.4 N·m {55 kgf·cm, 48 in·lbf}
NOTICE:
When disconnecting the cable, some systems need to be initialized after the cable is reconnected.
Click here
9. PERFORM SRS WARNING LIGHT
(See page )
10. PERFORM INITIALIZATION
Click here
Removal
REMOVAL
PROCEDURE
1. PRECAUTION
CAUTION:
Be sure to read Precaution thoroughly before servicing (See page
).
NOTICE:
After turning the ignition switch off, waiting time may be required before disconnecting
the cable from the negative (-) battery terminal. Therefore, make sure to read the
disconnecting the cable from the negative (-) battery terminal notices before proceeding
with work (See page ).
2. DISCONNECT CABLE FROM NEGATIVE BATTERY TERMINAL
NOTICE:
When disconnecting the cable, some systems need to be initialized after the cable is reconnected.
Click here
3. REMOVE INSTRUMENT SIDE PANEL RH
4. REMOVE GLOVE COMPARTMENT PLATE
5. REMOVE LOWER NO. 2 INSTRUMENT PANEL AIRBAG ASSEMBLY
6. REMOVE LOWER INSTRUMENT PANEL ASSEMBLY
7. REMOVE ECM
(a) Disengage the clamp to separate the wire harness. |
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(b) Disconnect the 6 connectors.
(c) Remove the 2 bolts, nut and ECM from the instrument panel reinforcement assembly.
8. REMOVE ECM BRACKET
(a) Remove the 2 screws and ECM bracket from the ECM. |
|
9. REMOVE NO. 2 ECM BRACKET
(a) Remove the 2 screws and No. 2 ECM bracket from the ECM. |
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Cruise Control System Internal Failure (P057504,P057549)
DESCRIPTION
This DTC is stored when there is a malfunction in the ECM.
DTC No.
Detection Item
DTC Detection Condition
Trouble Area
MIL
P057504
Cruise Control System Internal Failure
While the dynamic rada ...
Front Camera Module Incorrect Axial Gap (C1AA8)
DESCRIPTION
If the millimeter wave radar sensor assembly detects that the beam axis of the
forward recognition camera is misaligned, it will store DTC C1AA8.
DTC No.
Detection Item
DTC Detection Condition
Trouble Area
C1AA8
...
Precaution
PRECAUTION
1. PRECAUTION FOR HEADLIGHT BULB REPLACEMENT
(a) When any defects such as deformation, cracks, dents, chipping, etc. are identified
on the headlight, replace it with a new one.
(b) Even if the operation seems to be normal, the fail-safe function may be defective.
(c) Since halogen b ...