Restraints - Service Information: Other Dodge Journey I

ACTIVE RESTRAINTS

The active restraints for this vehicle include

1. Child Restraint Anchors - All vehicles are equipped with three, fixed-position, child seat upper tether anchors for the second row seat. Two anchors are integral to the back of the right second row seat cushion frame, and one is integral to the left second row seat cushion frame. The upper tether anchors are accessed from behind the second row seats. Two lower anchors are also provided for each outboard second row seating position, while only one lower anchor is provided for the center seating position. These lower anchors are also integral to the second row seat cushion frames. The lower anchors are all accessed from the front of the second row seats, where the seat back meets the seat cushion.
2. Integrated Child Booster Seats - Two integrated child booster seats are an available option. Vehicles with this option have a booster seat integral to each of the two outboard second row seating positions. The center section of the seat cushion of these seats is lifted up and rearward to raise the seat cushion, which raises a child aged four and older, weighing over 18.14 kilograms (40 pounds) and up to 144.78 centimeters (57 inches) tall into the belted zone of the adult seat belts.
3. Front Seat Belts - Both front seating positions are equipped with three-point seat belt systems employing lower B-pillar mounted inertia latch-type emergency locking retractors, height-adjustable upper B-pillar mounted turning loops, a traveling lower seat belt anchor secured to the outboard side of the seat frame, and a traveling end-release seat belt buckle secured to the inboard side of the seat frame. The passenger side front seat belt retractor is switchable to an automatic locking retractor for compatibility with child seats. The driver side front seat belt retractor includes an integral seat belt switch that detects whether the driver side front seat belt has been fastened.
4. Second Row Seat Belts - All second row seating positions are equipped with three-point seat belt systems. The outboard seating position belts employ lower C-pillar mounted inertia latch-type emergency locking retractors, fixed position upper C-pillar mounted turning loops and fixed lower seat belt anchors secured to the floor panel. The second row center seating position belt has an inertia latch-type emergency locking retractor that is integral to the right second row seat back panel. The second row center seating position belt lower anchor is secured to the second row right seat cushion frame. All three rear seat belts have fixed end-release seat belt buckles secured to the seat cushion frames, a double buckle unit on the left side and a single buckle unit on the right side. Both outboard second row seat belt retractors are switchable to an automatic locking retractor for compatibility with child seats.
5. Third Row Seat Belts - In vehicles equipped with the optional third row bench seat, both third row seating positions are equipped with three-point seat belt systems. These belts employ lower D-pillar mounted inertia latch-type emergency locking retractors, fixed position upper D-pillar mounted turning loops, fixed lower seat belt anchors and fixed position end-release buckles secured to the floor panel. Both third row seat belt retractors are switchable to an automatic locking retractor for compatibility with child seats.

Scheme 33

The passive restraints available for this vehicle include the following

1. Dual Front Airbags - Multistage driver and front passenger airbags are used in this vehicle. This airbag system consists of passive, inflatable, Supplemental Restraint System (SRS) components and vehicles with this equipment can be readily identified by the SRS - AIRBAG logo molded into the driver airbag trim cover in the center of the steering wheel and also into the passenger airbag door on the top of the instrument panel above the glove box. Vehicles with the airbag system can also be identified by the airbag indicator, which will illuminate in the ElectroMechanical Instrument Cluster (EMIC) (also known as the Cab Compartment Node/CCN) for about four to six seconds as a bulb test each time the ignition switch is turned to the ON position. Pyrotechnic-type seat belt tensioners are also included for the driver and passenger front seat belts of all airbag equipped vehicles to work in conjunction with the dual front and side curtain airbags.
2. Seat Airbags - Front seat integrated thorax airbags are standard equipment in this vehicle in all markets except Mexico, where they are optional. This airbag system consists of passive, inflatable, SRS components and vehicles with this equipment can be readily identified by a sewn tag with the SRS - AIRBAG logo located on the outboard side of the front seat back trim cover.
3. Side Curtain Airbags - Side curtain airbags are standard equipment for this vehicle when it is also equipped with dual front airbags. This airbag system consists of passive, inflatable SRS components and vehicles with this equipment can be readily identified by a molded identification trim plug with the SRS - AIRBAG logo located near the tops of the B and C-pillar trim.

Scheme 34

The SRS includes the following major components, which are described in further detail elsewhere in this service information

1. Airbag Indicator - The airbag indicator is integral to the ElectroMechanical Instrument Cluster (EMIC) (also known as the Cab Compartment Node/CCN), which is located on the instrument panel in front of the driver.
2. Clockspring - The clockspring is located near the top of the steering column, directly beneath the steering wheel.
3. Driver Airbag (4) - The driver airbag is located in the center of the steering wheel, beneath the driver airbag trim cover.
4. Driver Knee Blocker - The driver knee blocker is a structural unit secured to the back side of and integral to the instrument panel steering column opening cover.
5. Front Impact Sensor (1) - Two front impact sensors are used on vehicles equipped with dual front airbags, one left side and one right side. One sensor is located on the back side of the front end module carrier on either side of the radiator and inboard of the headlamp within the engine compartment.
6. Occupant Restraint Controller (3) - The Occupant Restraint Controller (ORC) is located on a mount on the floor panel transmission tunnel forward of the transmission gear selector, and is concealed beneath the center front floor mini console.
7. Passenger Airbag (2) - The passenger airbag is located in the instrument panel, beneath the passenger airbag door on the top of the instrument panel above the glove box on the passenger side of the vehicle.
8. Passenger Knee Blocker - The passenger knee blocker is a structural reinforcement that is integral to and concealed within the glove box door.
9. Seat Airbag (6) - On vehicles so equipped, a seat airbag unit is secured to each outboard front seat back frame, where it is concealed beneath the seat back trim cover and foam.
10. Seat Belt Tensioner (7) - A seat belt tensioner is integral to both front seat belt retractor units on vehicles equipped with dual front airbags. The seat belt retractor and tensioner units are secured to each lower inner B-pillar and are concealed behind the lower B-pillar trim.
11. Seat Track Position Sensor (8) - Certain vehicles may include a seat track position sensor that is located on the inboard side of the upper inboard seat adjuster track on the driver side front seat.
12. Side Curtain Airbag (10) - A side curtain airbag is secured to each inside roof side rail above the headliner, and extends from the A-pillar to just beyond the C-pillar on vehicles with standard five-passenger seating, or from the A-pillar to the D-pillar on vehicles with optional seven-passenger seating.
13. Side Impact Sensor (5 and 9) - Four side impact sensors are standard equipment on vehicles equipped with side curtain airbags and the five-passenger seating package, two on each side of the vehicle. Six side impact sensors are used on vehicles equipped with side curtain airbags and the seven-passenger seating package, three on each side of the vehicle. One pressure-type sensor (5) is located on each right and left side front door module carrier of all vehicles with side curtain airbags, while one acceleration-type sensor (9) is located on each C-pillar. The seven-passenger seating package adds another acceleration-type sensor to each quarter inner panel above the rear wheel houses. These sensors are each concealed behind the adjacent interior trim components.

The ORC and the EMIC each contain a microprocessor and programming that allow them to communicate with each other using the Controller Area Network (CAN) data bus. This method of communication is used by the ORC for control of the airbag indicator in the EMIC. Refer to Electrical - Electronic Control Modules/Electronic Control Modules/COMMUNICATION - Description .

Hard wired circuitry connects the SRS components to each other through the electrical system of the vehicle. These hard wired circuits are integral to several wire harnesses, which are routed throughout the vehicle and retained by many different methods. These circuits may be connected to each other, to the vehicle electrical system, and to the SRS components through the use of a combination of soldered splices, splice block connectors, and many different types of wire harness terminal connectors and insulators. Refer to SYSTEM WIRING DIAGRAMS . The wiring information includes wiring diagrams, proper wire and connector repair procedures, further details on wire harness routing and retention, as well as pin-out and location views for the various wire harness connectors, splices and grounds.

The primary passenger restraints in this or any other vehicle are the standard equipment factory-installed seat belts and child restraint anchors. Seat belts and child restraint anchors are referred to as an active restraint because the vehicle occupants are required to physically fasten and properly adjust these restraints in order to benefit from them.

PASSIVE RESTRAINTS

The passive restraints are referred to as Supplemental Restraint System (SRS) components because they were designed and are intended to enhance the protection for the occupants of the vehicle only when used in conjunction with the seat belts. They are referred to as passive restraints because the vehicle occupants are not required to do anything to make them operate; however, the vehicle occupants must be wearing their seat belts in order to obtain the maximum safety benefit from the factory-installed SRS components.

The SRS electrical circuits are continuously monitored and controlled by a microprocessor and software contained within the Occupant Restraint Controller (ORC). An airbag indicator in the ElectroMechanical Instrument Cluster (EMIC) (also known as the Cab Compartment Node/CCN) illuminates from four to six seconds as a bulb test each time the ignition switch is turned to the ON or START positions. Following the bulb test, the airbag indicator is turned ON or OFF by the ORC to indicate the status of the SRS. If the airbag indicator comes ON at any time other than during the bulb test, it indicates that there is a problem in the SRS electrical circuits. Such a problem may cause airbags not to deploy when required, or to deploy when not required.

Deployment of the SRS components depends upon the angle and severity of an impact. Deployment is not based upon vehicle speed; rather, deployment is based upon the rate of deceleration as measured by the forces of gravity (G force) upon the acceleration-type impact sensors, or by a pressure wave within a front door as measured by the pressure-type impact sensor. When an impact is severe enough, the microprocessor in the ORC signals the inflator of the appropriate airbag units to deploy their airbag cushions. The front seat belt retractor tensioners are provided with a deployment signal by the ORC in conjunction with the front airbags. The side curtain airbags and, on vehicles so equipped, the seat airbags are provided with a deployment signal individually by the ORC based upon a side impact sensor input for the same side of the vehicle. The ORC also contains a rollover sensor. Should the vehicle roll over and not cause any impact or pressure sensor to signal the need for a deployment, the rollover sensor in the ORC will deploy the side curtain air bags, the seat air bags and under certain conditions, will also actuate the seat belt retractor tensioners.

During a frontal vehicle impact, the knee blockers work in concert with properly fastened and adjusted seat belts to restrain both the driver and the front seat passenger in the proper position for an airbag deployment. The knee blockers also absorb and distribute the crash energy from the driver and the front seat passenger to the structure of the instrument panel. The seat belt tensioners remove the slack from the front seat belts to provide further assurance that the driver and front seat passenger are properly positioned and restrained for an airbag deployment.

Typically, the vehicle occupants recall more about the events preceding and following a collision than they do of an airbag deployment itself. This is because the airbag deployment and deflation occur very rapidly. In a typical 48 kilometer-per-hour (30 mile-per-hour) barrier impact, from the moment of impact until the airbags are fully inflated takes about 40 milliseconds. Within one to two seconds from the moment of impact, the airbags are almost entirely deflated. The times cited for these events are approximations, which apply only to a barrier impact at the given speed. Actual times will vary somewhat, depending upon the vehicle speed, impact angle, severity of the impact, and the type of collision.

When the ORC monitors a problem in any of the SRS circuits or components, including the seat belt tensioners, it stores a fault code or Diagnostic Trouble Code (DTC) in its memory circuit and sends an electronic message to the EMIC to turn ON the airbag indicator. The hard wired circuits between components related to the SRS may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . The wiring information includes wiring diagrams, proper wire and connector repair procedures, details of wire harness routing and retention, connector pin-out information and location views for the various wire harness connectors, splices and grounds.

However, conventional diagnostic methods will not prove conclusive in the diagnosis of the SRS or the electronic controls or communication between other modules and devices that provide features of the SRS. The most reliable, efficient, and accurate means to diagnose the SRS or the electronic controls and communication related to SRS operation, as well as the retrieval or erasure of a DTC requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

WARNINGS

SUPPLEMENTAL RESTRAINT SYSTEM

The hard wired circuits between modules and components related to the Supplemental Restraint System (SRS) may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . The wiring information includes wiring diagrams, proper wire and connector repair procedures, details of wire harness routing and retention, connector pin-out information and location views for the various wire harness connectors, splices and grounds.

However, conventional diagnostic methods will not prove conclusive in the diagnosis of the SRS or the electronic controls or communication between other modules and devices that provide features of the SRS. The most reliable, efficient, and accurate means to diagnose the SRS or the electronic controls and communication related to SRS operation, as well as the retrieval or erasure of a DTC requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

In addition to a diagnostic scan tool that contains the latest version of the proper diagnostic software, certain diagnostic procedures for the SRS may require the use of the SRS Load Tool special tool along with the appropriate Load Tool Jumpers and Adapters. Refer to the appropriate diagnostic information.

HANDLING NON-DEPLOYED SUPPLEMENTAL RESTRAINTS

At no time should any source of electricity be permitted near the inflator on the back of a non-deployed airbag or seat belt tensioner. When carrying a non-deployed airbag, the trim cover or airbag cushion side of the unit should be pointed away from the body to minimize injury in the event of an accidental deployment. If the airbag unit is placed on a bench or any other surface, the trim cover or airbag cushion side of the unit should be face up to minimize movement in the event of an accidental deployment.

When handling a non-deployed seat belt tensioner, take proper care to keep fingers out from under the retractor cover and away from the seat belt webbing where it exits from the retractor cover. In addition, the Supplemental Restraint System (SRS) should be disarmed whenever any steering wheel, steering column, seat belt tensioner, airbag, impact sensor or instrument panel components require diagnosis or service. Failure to observe this warning could result in accidental airbag deployment and possible personal injury.

All damaged, ineffective or non-deployed airbags and seat belt tensioners which are replaced on vehicles are to be handled and disposed of properly. If an airbag or seat belt tensioner unit is ineffective or damaged and non-deployed, refer to the Hazardous Substance Control System for information regarding the potentially hazardous properties of the subject component and the proper safe handling procedures. Then dispose of all non-deployed and deployed airbags and seat belt tensioners in a manner consistent with state, provincial, local and federal regulations.

SUPPLEMENTAL RESTRAINT STORAGE

Airbags and seat belt tensioners must be stored in their original, special containers until they are used for service. Also, they must be stored in a clean, dry environment; away from sources of extreme heat, sparks, and high electrical energy. Always place or store any airbag on a surface with its trim cover or airbag cushion side facing up, to minimize movement in case of an accidental deployment.

SERVICE AFTER A SUPPLEMENTAL RESTRAINT DEPLOYMENT

Any vehicle which is to be returned to use following a Supplemental Restraint System (SRS) component deployment must have the deployed restraints replaced. In addition, if the driver airbag has been deployed, the clockspring must be replaced and the steering column must be inspected. Refer to Steering/Column - Diagnosis and Testing . If the passenger airbag is deployed, the instrument panel top pad must be replaced.

The seat belt tensioners are deployed in conjunction with front airbags, but can also be deployed with seat (thorax) or side airbags. The seat belt tensioners must be replaced if either front airbag has been deployed, and must be inspected if either seat or side airbag has been deployed. If a seat airbag is deployed, the seat back frame, the seat back foam and the seat back trim cover on the same side of the vehicle as the deployed airbag must also be replaced.

If a side curtain airbag has been deployed, the headliner as well as the upper A, B, C and, on vehicles with the optional seven-passenger seating, the D-pillar trim on the same side of the vehicle as the deployed airbag must be replaced. These components are not intended for reuse and will be damaged or weakened as a result of a SRS component deployment, which may or may not be obvious during a visual inspection. On vehicles with an optional sunroof, the sunroof drain tubes and hoses must be closely inspected following a side curtain airbag deployment.

It is also critical that the mounting surfaces and mounting brackets for the Occupant Restraint Controller (ORC), side impact sensors and front impact sensors be closely inspected and restored to their original conditions following any vehicle impact damage. Because the ORC and each impact sensor are used by the SRS to monitor or confirm the direction and severity of a vehicle impact, improper orientation or insecure fastening of these components may cause airbags not to deploy when required, or to deploy when not required.

There are two methods by which an airbag or seat belt tensioner may be connected to the vehicle electrical system. The first method involves a short pigtail harness and connector insulator that are integral to the airbag or tensioner unit and are replaced as a unit with the service replacement airbag or seat belt tensioner unit. The second method involves a wire harness takeout and connector insulator (squib circuits) that are connected directly to the air bag or tensioner initiator. The heat created by the initiator during an airbag or tensioner deployment will cause collateral damage to a directly connected wire harness take out and connector insulator. Therefore, these direct-connect type take outs and connector insulators must be repaired following an airbag or seat belt tensioner deployment. See Restraints - Standard Procedure .

All other vehicle components should be closely inspected following any SRS component deployment, but are to be replaced only as required by the extent of the visible damage incurred.

AIRBAG SQUIB STATUS

Multistage airbags with multiple initiators (squibs) must be checked to determine that all squibs were used during the deployment event. The driver and passenger airbags in this vehicle are deployed by electrical signals generated by the Occupant Restraint Controller (ORC) through the driver or passenger squib 1 and squib 2 circuits to the two initiators in the airbag inflators. Typically, both initiators are used and all potentially hazardous chemicals are burned during an airbag deployment event. However, it is possible for only one initiator to be used; therefore, it is always necessary to confirm that both initiators have been used in order to avoid the improper handling or disposal of potentially live pyrotechnic or hazardous materials. The following procedure should be performed using a diagnostic scan tool to verify the status of both airbag squibs before either deployed airbag is removed from the vehicle for disposal.

1. Be certain that the diagnostic scan tool contains the latest version of the proper diagnostic software. Connect the scan tool to the 16-way Data Link Connector (DLC). The DLC is located on the driver side lower edge of the instrument panel, outboard of the steering column.
2. Turn the ignition switch to the ON position.
3. Using the scan tool, read and record the active (current) Diagnostic Trouble Code (DTC) data.

Using the active DTC information, refer to the Airbag Squib Status table to determine the status of both driver and passenger airbag squibs.

Scheme 35

Following a Supplemental Restraint System (SRS) component deployment, the vehicle interior will contain a powdery residue. This residue consists primarily of harmless particulate by-products of the small pyrotechnic charge that initiates the propellant used to deploy a SRS component. However, this residue may also contain traces of sodium hydroxide powder, a chemical by-product of the propellant material that is used to generate the inert gas that inflates the airbag. Since sodium hydroxide powder can irritate the skin, eyes, nose, or throat, be certain to wear safety glasses, rubber gloves, and a long-sleeved shirt during cleanup.

Scheme 36

1. Begin the cleanup by using a vacuum cleaner to remove any residual powder from the vehicle interior. Clean from outside the vehicle and work your way inside, so that you avoid kneeling or sitting on a non-cleaned area.
2. Be certain to vacuum the heater and air conditioning outlets as well. Run the heater and air conditioner blower on the lowest speed setting and vacuum any powder expelled from the outlets. CAUTION: Deployed front airbags having two initiators (squibs) in the airbag inflator may or may not have live pyrotechnic material within the inflator. Do not dispose of these airbags unless you are certain of complete deployment. Refer to AIRBAG SQUIB STATUS. All damaged, ineffective, or non-deployed Supplemental Restraint System (SRS) components which are replaced on vehicles are to be handled and disposed of properly. If an airbag or seat belt tensioner unit is ineffective or damaged and non-deployed, refer to the Hazardous Substance Control System for information regarding the potentially hazardous properties of the subject component and the proper safe handling procedures. Then dispose of all non-deployed and deployed airbags and seat belt tensioners in a manner consistent with state, provincial, local and federal regulations.
3. Next, remove the deployed SRS components from the vehicle. Refer to the appropriate service removal procedures.
4. You may need to vacuum the interior of the vehicle a second time to recover all of the powder.

REPAIR PROCEDURE

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1. Remove 13 millimeters (0.50 inch) of insulation from each wire that needs to be spliced.
2. Place a piece of adhesive sealant-lined heat shrink tubing (Part Number 04778570 or equivalent) over the wire on one side of the splice. Be certain the length of tubing will be sufficient to cover and seal the entire repair area.
3. Place the strands of the wires being spliced so that they are overlapping each other within the splice band (1).
4. Using a crimping tool (1) (MOPAR Part Number 05019912AA, Miller Special Tool Number 10042 or equivalent) crimp the splice band and wires together securely. CAUTION: Never use acid core solder for electrical wiring repairs.
5. Using rosin core type solder (1) only and a suitable soldering iron (3), solder the wire and splice band connection (2) together.
6. Center the heat shrink tubing (2) over the splice joint repair and heat using a suitable heat gun. Heat the joint until the tubing is tightly sealed and sealant (1) begins to ooze out of both ends of the tubing.

RESTRAINT SYSTEMS

TORQUE SPECIFICATIONS

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FRONT

Scheme 47

1. Disconnect and isolate the battery negative cable.
2. Remove the front seat from the vehicle. Refer to «Body/Seats/SEAT - Removal»(ref-353577-S24542628262010011200000) .
3. Remove the screw (3) that secures the front seat belt buckle (1) lower anchor to the bracket at the back of the inboard seat track.
4. Remove the buckle from the front seat.

SECOND ROW - CENTER

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1. Move the second row right seat to the fully rearward position.
2. Move the second row left seat to the fully forward position.
3. Remove the plastic push-in fastener (3) that secures the outboard center seat back hinge bracket outboard trim (2) over the buckle (1) anchor to the left rear corner of the right seat frame.
4. Carefully pry the edges of the outboard center seat back hinge bracket outboard and inboard trim halves away from each other at their front and rear parting lines far enough to disengage the four integral latch features that secure the two halves of the trim to each other.
5. Carefully pry the outboard center seat back hinge bracket outboard trim away from the hinge bracket far enough to disengage the snap clip that secures the center of the trim to the bracket.
6. Remove the outboard trim from over the buckle anchor on the left rear corner of the right seat frame.
7. Remove the screw (2) that secures the buckle (1) lower anchor to the right seat frame.
8. Disengage the buckle from the elastic loop (3) of the right seat cushion trim cover and remove the buckle unit from the seat.

SECOND ROW - LEFT

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1. Move the second row left seat to the fully rearward position.
2. Move the second row right seat to the fully forward position.
3. Remove the screw (1) that secures the trim (2) over the buckle (3) anchor to the right rear corner of the left seat frame.
4. Remove the trim over the buckle anchor from the right rear corner of the left seat frame.
5. Remove the screw (1) that secures the buckle lower anchor (3) to the left seat frame.
6. Disengage the buckle from the elastic loop (2) of the left seat cushion trim cover and remove the buckle unit from the seat.

SECOND ROW - RIGHT

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1. Move the second row right seat to the fully forward position.
2. Reach under the rear edge of the second row right seat cushion frame just to the right of the lower end of the inboard center seat back hinge bracket (1) to access the right buckle lower anchor (3) and the center seat belt lower anchor (2).
3. Remove the screw (4) that secures the right buckle lower anchor and the center seat belt lower anchor to the right seat cushion frame.
4. From the front of the second row right seat, disengage the buckle (2) from the elastic loop (3) of the right seat cushion trim cover and pull the buckle lower anchor out from between the right seat cushion and back trim covers.

THIRD ROW

Scheme 54

1. Remove the third row seat cushion and cover from the rear floor panel (3). Refer to «Body/Seats/COVER, Seat Cushion - Removal»(ref-353577-S26019408142010011200000) .
2. Reach between the two third row seat back hinge brackets on the rear floor panel to access and remove the screw (2) that secures the third row seat belt buckle (1) anchor plate to the rear floor.
3. Remove the two buckles from the rear floor panel as a unit.

1. Position the front seat belt buckle (1) lower anchor to the bracket at the back of the inboard seat track.
2. Install and tighten the screw (3) that secures the lower anchor to the seat track bracket. Tighten the screw to 39 N.m (29 ft. lbs.).
3. Reinstall the front seat into the vehicle. Refer to «Body/Seats/SEAT - Installation»(ref-353577-S14590665032010011200000) .
4. Reconnect the battery negative cable.

1. Engage the second row center seat belt buckle (1) through the elastic loop (3) of the right seat cushion trim cover.
2. Position the buckle lower anchor to the left rear corner of the right seat frame.
3. Install and tighten the screw (2) that secures the buckle unit to the right seat frame. Tighten the screw to 39 N.m (29 ft. lbs.).
4. Position the outboard center seat back hinge bracket outboard trim (2) over the buckle (1) anchor on the left rear corner of the right seat frame.
5. Using hand pressure, align and press the outboard center seat back hinge bracket outboard trim toward the hinge bracket until the snap clip that secures the center of the trim snaps into the bracket.
6. Using hand pressure, squeeze the edges of the outboard center seat back hinge bracket outboard and inboard trim halves together until the four integral latch features that secure the two halves of the trim to each other are fully engaged.
7. Install the plastic push-in fastener (3) that secures the outboard center seat back hinge bracket outboard trim over the buckle anchor.
8. Restore the second row left seat to the fully rearward position.

1. Engage the second row left seat belt buckle through the elastic loop (2) of the left seat cushion trim cover.
2. Position the buckle lower anchor (3) to the right rear corner of the left seat frame.
3. Install and tighten the screw (1) that secures the buckle unit to the left seat frame. Tighten the screw to 39 N.m (29 ft. lbs.).
4. Position the trim (2) over the buckle (3) anchor on the right rear corner of the left seat frame.
5. Install and tighten the screw (1) that secures the trim over the buckle anchor. Tighten the screw securely.
6. Restore the second row right seat to the fully rearward position.

1. From the front of the second row right seat, engage the second row right buckle (2) through the elastic loop (3) of the right seat cushion trim cover and insert the buckle lower anchor between the right seat cushion and back trim covers.
2. Reach under the rear edge of the second row right seat cushion frame just to the right of the lower end of the inboard center seat back hinge bracket (1) to position the buckle lower anchor (3) and the center seat belt lower anchor (2) to the right seat frame.
3. Install and tighten the screw (4) that secures the buckle unit and the center seat belt lower anchor to the right seat frame. Tighten the screw to 39 N.m (29 ft. lbs.).
4. Restore the second row right seat to the fully rearward position.

1. Reach between the two third row seat back hinge brackets on the rear floor panel (3) to position the third row seat belt buckle (1) anchor plate to the rear floor.
2. Install and tighten the screw (2) that secures the anchor plate to the rear floor panel. Tighten the screw to 90 N.m (66 ft. lbs.).
3. Reinstall the third row seat cushion and cover onto the rear floor panel (3). Refer to «Body/Seats/COVER, Seat Cushion - Installation»(ref-353577-S42813168002010011200000) .

Scheme 55

The clockspring (3) for this vehicle is secured near the top of the steering column below the steering wheel. The clockspring also includes an integral, internal turn signal cancel cam and a Steering Angle Sensor (SAS) that are both serviced as a unit with the clockspring. The clockspring also supports the left (lighting) multi-function switch (1), the Steering Control Module (SCM) internal to the left multi-function switch housing (2), and the right (wiper) multi-function switch (6). Each of these switches and the jumper wire harness (5) between the two multi-function switches can be separated from and are serviced individually from the clockspring.

The clockspring case includes integral tabs for mounting the unit with three screws to the steering column lock housing as well as integral provisions for mounting and supporting both multi-function switches. The multi-function switches are each secured to the clockspring with a single screw (7). The SAS within the clockspring includes an electronic circuit board and a microprocessor, which allows it to communicate with other electronic modules in the vehicle over the Controller Area Network (CAN) data bus. The SAS circuitry, the clockspring, and the turn signal cancel cam are all contained within a flat, molded plastic case.

The clockspring case includes three connector receptacles that face toward the instrument panel. Within the plastic case is a spool-like molded plastic rotor with a large exposed hub. The upper surface of the rotor hub has a large center hole, two short pigtail wires with connectors, and a connector receptacle that faces toward the steering wheel. The lower surface of the rotor has an integral dowel or drive pin that also faces toward the steering wheel. Wound around the rotor spool within the case is a long ribbon-like tape that consists of several thin copper wire leads sandwiched between two thin plastic membranes. The outer end of the tape terminates at two of the connector receptacles that face the instrument panel, while the inner end of the tape terminates at the pigtail wires and connector receptacle on the hub of the clockspring rotor that face the steering wheel. The outer surface of the rotor hub rim within the clockspring case also has the integral lobes of the turn signal cancel cam.

The service replacement clockspring is shipped pre-centered and with a molded plastic locking pin (4) installed. The locking pin secures the centered clockspring rotor to the clockspring case during shipment and handling, but must be removed after the clockspring is installed on the steering column and the steering wheel is installed. See Restraints/CLOCKSPRING - Standard Procedure .

The clockspring cannot be repaired. If the clockspring is ineffective, damaged, or if the driver airbag has been deployed, the clockspring/turn signal cancel cam/SAS unit must be replaced.

CLOCKSPRING CENTERING

Note. A service replacement clockspring is shipped with the clockspring pre-centered and with a molded plastic locking pin installed. This locking pin should not be removed until the steering wheel has been installed on the steering column. If the locking pin is removed before the steering wheel is installed, the clockspring centering procedure must be performed.

Note. When a clockspring is installed into a vehicle without properly centering and locking the entire steering system, the Steering Angle Sensor (SAS) data does not agree with the true position of the steering system and causes the Electronic Stability Program (ESP) system to shut down. This may also damage the clockspring without any immediate malfunction. Unlike some other Chrysler vehicles, this SAS never requires calibration. However, upon each new ignition ON cycle, the steering wheel must be rotated slightly to initialize the SAS.

Note. Determining if the clockspring/SAS is centered is also possible electrically using the diagnostic scan tool. Steering wheel position is displayed as ANGLE with a range of up to 900 degrees. Refer to the appropriate menu item on the diagnostic scan tool.

Note. Before starting this procedure, be certain to turn the steering wheel until the front wheels are in the straight-ahead position and that the entire steering system is locked or inhibited from rotation.

Note. The clockspring may be centered and the rotor may be rotated freely once the steering wheel has been removed.

Scheme 56

1. Place the front wheels in the straight-ahead position and inhibit the steering column shaft from rotation.
2. Remove the steering wheel from the steering shaft. Refer to «Steering/Column/WHEEL, Steering - Removal»(ref-353572-S01452521492010011200000) .
3. Rotate the clockspring rotor (1) clockwise to the end of its travel. Do not apply excessive torque.
4. From the end of the clockwise travel, rotate the rotor about two and one-half turns counterclockwise. Turn the rotor slightly clockwise or counterclockwise as necessary so that the clockspring airbag pigtail wires (3) and connector receptacle are at the top and the dowel or drive pin (5) is at the bottom.
5. The clockspring is now centered. Secure the clockspring rotor to the clockspring case using a locking pin (2) or some similar device to maintain clockspring centering until the steering wheel is reinstalled on the steering column.

Note. The following procedure is for replacement of an ineffective or damaged seat belt and retractor unit. The front retractor also includes a seat belt tensioner. If the front seat belt or retractor is ineffective or damaged, but the seat belt tensioner is not deployed, review the recommended procedures for handling non-deployed supplemental restraints. See Restraints - Standard Procedure . If the seat belt tensioner has been deployed, review the recommended procedures for service after a supplemental restraint deployment before removing the unit from the vehicle. See Restraints - Standard Procedure .

Scheme 57

Scheme 58

Scheme 59

1. Adjust the front seat to its most forward position for easiest access to the front seat belt lower anchor and the B-pillar trim.
2. Disconnect and isolate the battery negative cable. Wait two minutes for the system capacitor to discharge before further service.
3. Using a trim stick or another suitable wide flat-bladed tool, gently pry the seat belt anchor cover (3) to remove it from the rear of the outboard front seat (2) side shield.
4. Remove the screw (4) that secures the front seat belt (1) lower anchor to the bracket on the outboard side of the front seat cushion frame.
5. Remove the lower and upper trim (4) from the B-pillar (1). Refer to «Body/Interior/PANEL, B-Pillar Trim - Removal»(ref-353577-S27371348752010011200000) .
6. Remove the screw (3) that secures the seat belt (5) turning loop to the height adjuster (2) on the upper B-pillar.
7. Using a trim stick or another suitable wide flat-bladed tool, gently pry the seat belt web guide (6) to unsnap it from the B-pillar.
8. Disconnect the body wire harness connector (1) from the seat belt tensioner initiator on the retractor (3).
9. On the driver side only, disconnect the second body wire harness connector from the seat belt switch connector receptacle on the retractor.
10. Remove the screw (4) that secures the lower retractor bracket to the inner B-pillar (2).
11. Remove the front seat belt and retractor from the B-pillar as a unit.

Scheme 60

Scheme 61

1. Remove the second row right seat from the vehicle. Refer to «Body/Seats/SEAT - Removal»(ref-353577-S24542628262010011200000) .
2. Reach under the rear edge of the second row right seat cushion frame just to the right of the lower end of the inboard center seat back hinge bracket (1) to access the right buckle lower anchor (3) and the center seat belt lower anchor (2).
3. Remove the screw (4) that secures the right buckle lower anchor and the center seat belt lower anchor to the right seat cushion frame.
4. From the front of the second row right seat, pull the center seat belt lower anchor out from between the right seat cushion and back trim covers.
5. Using a trim stick or another suitable wide flat-bladed tool, carefully pry the belt web guide bezel (3) upward from the top of the right seat back (2) far enough to disengage the three barrel clips that secure the bezel to the seat back frame.
6. Slide the center seat belt webbing (1) through the slot in the guide bezel to disengage the belt from the bezel.
7. Remove the head rest, back panel and trim cover from the right seat back frame (1). It is not necessary to remove the seat back frame from the seat cushion frame. Refer to «Body/Seats/SEAT BACK - Removal»(ref-353577-S16446763872010011200000) .
8. Remove the screws (4) that secure the molded plastic shield (5) to the top of the seat back frame. Pull the top of the seat back foam away from the seat back frame to access the lower screws securing the shield.
9. Remove the molded plastic shield from the top of the seat back frame.
10. From the back side of the seat back frame, remove the screw (2) that secures the retractor (3) to the frame.
11. Lift the retractor upward far enough to disengage the T-tab of the retractor bracket from the keyed slot in the seat back frame.
12. Guide the seat belt webbing through the slot in the top of the seat back frame while removing the seat belt and retractor from the seat as a unit.

SECOND ROW - OUTBOARD

Scheme 62

Scheme 63

1. Loosen the front of the quarter trim panel from the lower C-pillar (1) enough to access the second row outboard seat belt and retractor. Refer to «Body/Interior/PANEL, Quarter Trim - Removal»(ref-353577-S13349045142010011200000) .
2. Remove the screw (4) that secures the second row outboard seat belt (2) lower anchor to the rear floor panel (3) near the base of the C-pillar.
3. Remove the upper trim (6) from the inside of the C-pillar. Refer to «Body/Interior/PANEL, B-Pillar Trim - Removal»(ref-353577-S27371348752010011200000) .
4. Remove the screw (1) that secures the seat belt turning loop to the inside of the upper C-pillar (3).
5. Remove the seat belt turning loop from the C-pillar.
6. Using a trim stick or another suitable wide flat-bladed tool, gently pry the seat belt web guide (2) to unsnap it from the quarter inner panel near the base of the C-pillar.
7. Remove the screw (4) that secures the retractor (5) bracket to the quarter inner panel.
8. Lift the retractor upward far enough to disengage the retractor tab from the keyed hole in the quarter inner panel.
9. Remove the second row outboard seat belt and retractor from the vehicle as a unit.

THIRD ROW SEAT BELT AND RETRACTOR

Scheme 64

Scheme 65

1. Remove the third row seat cushion and cover from the rear floor panel. Refer to «Body/Seats/COVER, Seat Cushion - Removal»(ref-353577-S26019408142010011200000) .
2. Remove the screw (2) that secures the third row seat belt lower anchor (1) and the third row seat back (3) outboard bracket to the rear floor panel.
3. Remove the lower anchor from the third row seat back outboard bracket.
4. Unsnap and remove the trim cover (1) from the third row seat belt turning loop on the inside of the upper D-pillar trim (3) to access the turning loop screw (2).
5. Remove the screw (2) that secures the seat belt turning loop to the bracket on the inside of the upper D-pillar.
6. Remove the turning loop from the D-pillar.
7. Remove the trim from the inside of the upper D-pillar. Refer to «Body/Interior/PANEL, D-Pillar Trim - Removal»(ref-353577-S36741296472010011200000) .
8. Loosen the rear of the quarter trim panel from the lower D-pillar enough to access the third row outboard seat belt and retractor (7). Refer to «Body/Interior/PANEL, Quarter Trim - Removal»(ref-353577-S13349045142010011200000) .
9. Remove the screw (4) that secures the upper retractor bracket to the inside of the D-pillar.
10. Remove the screw (6) that secures the lower retractor bracket to the inside of the D-pillar.
11. Lift the retractor upward far enough to disengage the tab of the upper retractor bracket from the keyed hole in the D-pillar.
12. Remove the third row seat belt and retractor from the vehicle as a unit.

THIRD ROW TURNING LOOP BRACKET

Scheme 66

1. Unsnap and remove the trim cover (1) from the third row seat belt turning loop on the inside of the upper D-pillar trim (3) to access the turning loop screw (2).
2. Remove the screw (2) that secures the seat belt turning loop to the bracket on the inside of the upper D-pillar.
3. Remove the turning loop from the D-pillar.
4. Remove the trim from the inside of the upper D-pillar. Refer to «Body/Interior/PANEL, D-Pillar Trim - Removal»(ref-353577-S36741296472010011200000) .
5. Remove the two screws (2) that secure the seat belt turning loop bracket (1) to the inside of the upper D-pillar (3).
6. Remove the turning loop bracket from the D-pillar.

Note. The following procedure is for replacement of an ineffective or damaged seat belt and retractor unit. The front retractor also includes a seat belt tensioner. If the front seat belt or retractor is ineffective or damaged, but the seat belt tensioner is not deployed, review the recommended procedures for handling non-deployed supplemental restraints. See Restraints - Standard Procedure . If the seat belt tensioner has been deployed, review the recommended procedures for service after a supplemental restraint deployment before removing the unit from the vehicle. See Restraints - Standard Procedure .

1. Position the front seat belt and retractor (3) to the inner B-pillar (2) as a unit.
2. On the driver side only, reconnect the body wire harness connector to the seat belt switch connector receptacle on the retractor.
3. Reconnect the body wire harness connector (1) to the seat belt tensioner initiator on the retractor.
4. Install and tighten the screw (4) that secures the lower retractor bracket to the inner B-pillar. Tighten the screw to 58 N.m (43 ft. lbs.).
5. Be certain to route the wiring for the seat belt tensioner behind the B-pillar flange to ensure it does not interfere with the seat belt webbing.
6. Position the web guide (6) to the B-pillar (1). Be certain the seat belt webbing (5) is not twisted between the retractor and the web guide.
7. Using hand pressure, press firmly and evenly on the web guide to snap it into place.
8. Position the seat belt turning loop onto the height adjuster (2) on the upper B-pillar. Be certain the seat belt webbing is not twisted between the web guide and the turning loop.
9. Install and tighten the screw (3) that secures the turning loop to the height adjuster. Tighten the screw to 37 N.m (27 ft. lbs.).
10. Reinstall the upper (4) and lower trim onto the B-pillar. Refer to «Body/Interior/PANEL, B-Pillar Trim - Installation»(ref-353577-S21811088682010011200000) .
11. Position the front seat belt (1) lower anchor to the bracket on the outboard side of the front seat (2) cushion frame. Be certain the seat belt webbing is not twisted between the turning loop and the lower anchor.
12. Install and tighten the screw (4) that secures the lower anchor to the bracket on the outboard side of the front seat cushion frame. Tighten the screw to 51 N.m (38 ft. lbs.).
13. Align the seat belt anchor cover (3) to the opening near the rear of the outboard seat side shield. Using hand pressure, press firmly and evenly on the cover until it snaps into place.
14. Do not reconnect the battery negative cable at this time. The Supplemental Restraint System (SRS) verification test procedure should be performed following service of any SRS component. See «Restraints - Standard Procedure»(ref-353580-S33366774452010011200000) .

1. Guide the seat belt webbing through the slot in the top of the right seat back frame (1) while positioning the center seat belt and retractor (3) to the frame as a unit. Be certain the seat belt webbing is not twisted between the retractor and the top of the seat.
2. Engage the T-tab of the retractor bracket with the keyed slot in the seat back frame.
3. From the back side of the seat back frame, install and tighten the screw (2) that secures the retractor to the frame. Tighten the screw to 39 N.m (29 ft. lbs.).
4. Position the molded plastic shield (5) onto the top of the seat back frame.
5. Install and tighten the screws (4) that secure the molded plastic shield to the top of the seat back frame. Pull the top of the seat back foam away from the seat back frame to access the lower screws securing the shield.
6. Reinstall the trim cover, back panel and head rest to the right seat back frame. Refer to «Body/Seats/SEAT BACK - Installation»(ref-353577-S18839244532010011200000) .
7. Grasp the center seat belt webbing (1) between where it exits the top of the seat and the seat belt latch plate and slide it through the slot in the belt web guide bezel (3) to engage the belt through the bezel.
8. Position the guide bezel to the top of the right seat back (2) with the slot facing forward.
9. Using hand pressure, press the guide bezel down onto the top of the right seat back far enough to engage the three barrel clips that secure the bezel to the seat back frame.
10. From the front of the second row right seat, insert the center seat belt lower anchor between the right seat cushion and back trim covers. Be certain the seat belt webbing is not twisted between the top of the seat and the belt lower anchor.
11. Reach under the rear edge of the second row right seat cushion frame just to the right of the lower end of the inboard center seat back hinge bracket (1) to position the buckle lower anchor (3) and the center seat belt lower anchor (2) to the right seat frame.
12. Install and tighten the screw (4) that secures the buckle unit and the center seat belt lower anchor to the right seat frame. Tighten the screw to 39 N.m (29 ft. lbs.).
13. Reinstall the second row right seat into the vehicle. Refer to «Body/Seats/SEAT - Installation»(ref-353577-S14590665032010011200000) .

1. Position the second row outboard seat belt and retractor (5) to the quarter inner panel just below the base of the upper C-pillar (3) as a unit.
2. Engage the tab on the retractor bracket into the keyed hole in the quarter inner panel.
3. Install and tighten the screw (4) that secures the retractor to the quarter inner panel. Tighten the screw to 58 N.m (43 ft. lbs.).
4. Position the web guide (2) to the quarter inner panel near the base of the C-pillar. Be certain the seat belt webbing is not twisted between the retractor and the web guide.
5. Using hand pressure, press firmly and evenly on the web guide to snap it into place.
6. Position the seat belt turning loop to the inside of the upper C-pillar. Be certain the seat belt webbing is not twisted between the web guide and the turning loop.
7. Install and tighten the screw (1) that secures the turning loop to the C-pillar. Tighten the screw to 43 N.m (32 ft. lbs.).
8. Reinstall the upper trim (2) onto the inside of the C-pillar (5). Refer to «Body/Interior/PANEL, C-Pillar Trim - Installation»(ref-353577-S31277964572010011200000) .
9. Position the lower seat belt (2) anchor to the rear floor panel (3) near the base of the lower C-pillar (1). Be certain the seat belt webbing is not twisted between the turning loop and the lower anchor.
10. Install and tighten the screw (4) that secures the lower seat belt anchor to the floor. Tighten the screw to 58 N.m (43 ft. lbs.).
11. Reinstall the front of the quarter trim panel onto the lower C-pillar. Refer to «Body/Interior/PANEL, Quarter Trim - Installation»(ref-353577-S36809696592010011200000) .

1. Position the third row seat belt and retractor (7) to the inside of the D-pillar (5) as a unit.
2. Engage the tab of the upper retractor bracket into the keyed hole in the D-pillar.
3. Install and tighten the screw (6) that secures the lower retractor bracket to the inside of the D-pillar. Tighten the screw to 58 N.m (43 ft. lbs.).
4. Install and tighten the screw (4) that secures the upper retractor bracket to the inside of the D-pillar. Tighten the screw to 10 N.m (7 ft. lbs.).
5. Reinstall the rear of the quarter trim panel to the lower D-pillar. Refer to «Body/Interior/PANEL, Quarter Trim - Installation»(ref-353577-S36809696592010011200000) .
6. Reinstall the trim (3) onto the inside of the upper D-pillar. Refer to «Body/Interior/PANEL, D-Pillar Trim - Installation»(ref-353577-S16012719342010011200000) .
7. Position the seat belt turning loop to the inside of the upper D-pillar. Be certain the seat belt webbing (5) is not twisted between the retractor and the turning loop.
8. Install and tighten the screw (2) that secures the turning loop to the bracket on the inside of the upper D-pillar. Tighten the screw to 43 N.m (32 ft. lbs.).
9. Snap the trim cover (1) over the seat belt turning loop on the inside of the upper D-pillar.
10. Position the seat belt lower anchor (1) to the third row seat back (3) outboard bracket on the rear floor panel. Be certain the seat belt webbing is not twisted between the turning loop and the lower anchor.
11. Install and tighten the screw (2) that secures the lower anchor and the third row seat back outboard bracket to the rear floor panel. Tighten the screw to 90 N.m (66 ft. lbs.).
12. Reinstall the third row seat cushion and cover to the rear floor panel. Refer to «Body/Seats/COVER, Seat Cushion - Installation»(ref-353577-S42813168002010011200000) .

1. Position the third row turning loop bracket (1) to the inside of the upper D-pillar (3).
2. Install and tighten the two screws (2) that secure the turning loop bracket to the D-pillar. Tighten the screws to 22 N.m (16 ft. lbs.).
3. Reinstall the trim (3) onto the inside of the upper D-pillar. Refer to «Body/Interior/PANEL, D-Pillar Trim - Installation»(ref-353577-S16012719342010011200000) .
4. Position the seat belt turning loop to the inside of the upper D-pillar. Be certain the seat belt webbing (5) is not twisted between the retractor and the turning loop as well as between the turning loop and the lower anchor.
5. Install and tighten the screw (2) that secures the turning loop to the bracket on the inside of the upper D-pillar. Tighten the screw to 43 N.m (32 ft. lbs.).
6. Snap the trim cover (1) over the seat belt turning loop on the inside of the upper D-pillar.

Scheme 67

Two acceleration-type front impact sensors (1) are used on this vehicle, one each for the left and right sides of the vehicle. These sensors are mounted remotely from the impact sensor that is internal to the Occupant Restraint Controller (ORC). Each front sensor is secured with a screw to the back of the front end module carrier on either outboard side of the cooling module, just inboard of each front lamp unit housing within the engine compartment. The sensor housing has an integral connector receptacle (3), an integral locating and anti-rotation pin, and an integral mounting hole (2).

The right and left front impact sensors are identical in construction and calibration. A cavity in the center of the molded plastic impact sensor housing contains the electronic circuitry of the sensor which includes an electronic communication chip and an electronic impact sensor. The cavity is filled with a potting material to seal and protect the internal electronic circuitry and components. The front impact sensors are each connected to the vehicle electrical system through a dedicated take out and connector of the front end module wire harness.

These acceleration-type front impact sensors cannot be repaired or adjusted and, if damaged or ineffective, they must be replaced.

Scheme 68

Two pressure-type front door side impact sensors (2) are used on this vehicle when it is equipped with the side curtain airbags or the optional seat (also known as thorax) airbags, one each for the left and right sides of the vehicle. These sensors are mounted remotely from the impact sensor that is internal to the Occupant Restraint Controller (ORC). Each side sensor is secured with two screws and is sealed by a resilient gasket (1) to the front door module carrier on the inside of the front door. The sensors are concealed behind the front door trim panel within the passenger compartment.

The right and left front door side impact sensors are identical in construction and calibration. The impact sensor housing has an integral connector receptacle (3), two integral mounting tabs, and an integral hood-like water shield (4) that extends through a hole in the front door module carrier into the interior of the door cavity and protects the sensor orifice from contamination. A cavity in the center of the molded plastic impact sensor housing contains the electronic circuitry of the sensor, which includes an electronic communication chip and the pressure sensor. The housing cavity is filled with a potting material to seal and protect the internal electronic circuitry and components. A label on the sensor has a directional arrow and the word down imprinted upon it to provide verification of the correct sensor orientation in the vehicle. The side impact sensors are each connected to the vehicle electrical system through a dedicated take out and connector of the front door wire harness.

These pressure-type front door side impact sensors cannot be repaired or adjusted and, if damaged or ineffective, they must be replaced.

SIDE - SECOND ROW SEATING

Two acceleration-type second row seating side impact sensors (1) are used on this vehicle when it is equipped with the side curtain airbags, one each for the left and right sides of the vehicle. These sensors are mounted remotely from the impact sensor that is internal to the Occupant Restraint Controller (ORC). Each side sensor is secured with a screw to the lower C-pillar just above the rear door opening sill within the passenger compartment. The sensor housing has an integral connector receptacle (3), an integral locating anti-rotation pin, and an integral mounting hole (2).

The right and left second row seating side impact sensors are identical in construction and calibration. However, the connector orientation in the vehicle is reversed. The connector receptacle faces forward on the right side of the vehicle, and faces rearward on the left side of the vehicle. A cavity in the center of the molded plastic impact sensor housing contains the electronic circuitry of the sensor which includes an electronic communication chip and an electronic impact sensor. The cavity is filled with a potting material to seal and protect the internal electronic circuitry and components. The second row seating side impact sensors are each connected to the vehicle electrical system through a dedicated take out and connector of the body wire harness.

These acceleration-type second row seating side impact sensors cannot be repaired or adjusted and, if damaged or ineffective, they must be replaced.

SIDE - THIRD ROW SEATING

Two acceleration-type third row seating side impact sensors (1) are used on this vehicle when it is equipped with the side curtain airbags and seven-passenger seating, one each for the left and right sides of the vehicle. These sensors are mounted remotely from the impact sensor that is internal to the Occupant Restraint Controller (ORC). Each side sensor is secured with a screw to the right or left quarter inner panel just above the right or left rear wheel housing within the passenger compartment. The sensor housing has an integral connector receptacle (3), an integral locating anti-rotation pin, and an integral mounting hole (2).

The right and left third row seating side impact sensors are identical in construction and calibration. However, the connector orientation in the vehicle is reversed. The connector receptacle faces forward on the right side of the vehicle, and faces rearward on the left side of the vehicle. A cavity in the center of the molded plastic impact sensor housing contains the electronic circuitry of the sensor which includes an electronic communication chip and an electronic impact sensor. The cavity is filled with a potting material to seal and protect the internal electronic circuitry and components. The third row seating side impact sensors are each connected to the vehicle electrical system through a dedicated take out and connector of the body wire harness.

These acceleration-type third row seating side impact sensors cannot be repaired or adjusted and, if damaged or ineffective, they must be replaced.

VEHICLE FRONT

The acceleration-type front impact sensors are electronic accelerometers that sense the rate of vehicle deceleration, which provides verification of the direction and severity of an impact. Each sensor also contains an electronic communication chip that allows the unit to communicate the sensor status as well as sensor fault information to the microprocessor in the Occupant Restraint Controller (ORC).

The ORC microprocessor continuously monitors all of the front passive restraint system electrical circuits to determine the system readiness. If the ORC detects a monitored system fault, it sets a Diagnostic Trouble Code (DTC) and commands the airbag indicator operation accordingly. The impact sensors each receive battery current and ground through dedicated left and right sensor plus and minus circuits from the ORC. The impact sensors and the ORC communicate by modulating the current in the sensor plus circuit.

The hard wired circuits between the acceleration-type front impact sensors and the ORC may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . However, conventional diagnostic methods will not prove conclusive in the diagnosis of the impact sensors or the electronic controls or communication between other modules and devices that provide features of the Supplemental Restraint System (SRS). The most reliable, efficient, and accurate means to diagnose the impact sensors or the electronic controls and communication related to acceleration-type front impact sensor operation requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

SIDE - FRONT DOOR

The pressure-type front door side impact sensors recognize a side impact in the front door area by monitoring changes in pressure within the front door cavity, which manifests itself as a sudden pressure wave as the door collapses during an impact. Each sensor also contains an electronic communication chip that allows the unit to communicate the sensor status as well as sensor fault information to the microprocessor in the Occupant Restraint Controller (ORC).

The ORC microprocessor continuously monitors all of the side passive restraint system electrical circuits to determine the system readiness. If the ORC detects a monitored system fault, it sets a Diagnostic Trouble Code (DTC) and controls the airbag indicator operation accordingly. The impact sensors each receive battery current and ground through dedicated left and right sensor plus and minus circuits from the ORC. The impact sensors and the ORC communicate by modulating the current in the sensor plus circuit.

The hard wired circuits between the pressure-type front door side impact sensors and the ORC may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . However, conventional diagnostic methods will not prove conclusive in the diagnosis of the impact sensors or the electronic controls or communication between other modules and devices that provide features of the Supplemental Restraint System (SRS). The most reliable, efficient, and accurate means to diagnose the pressure-type front door side impact sensors or the electronic controls and communication related to side impact sensor operation requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

The acceleration-type second row seating side impact sensors are electronic accelerometers that sense the rate of vehicle deceleration, which provides verification of the direction and severity of an impact. Each sensor also contains an electronic communication chip that allows the unit to communicate the sensor status as well as sensor fault information to the microprocessor in the Occupant Restraint Controller (ORC).

The ORC microprocessor continuously monitors all of the side passive restraint system electrical circuits to determine the system readiness. If the ORC detects a monitored system fault, it sets a Diagnostic Trouble Code (DTC) and controls the airbag indicator operation accordingly. The impact sensors each receive battery current and ground through the dedicated left and right sensor plus and minus circuits from the ORC. The impact sensors and the ORC communicate by modulating the voltage in the sensor plus circuit.

The hard wired circuits between the acceleration-type second row seating side impact sensors and the ORC may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . However, conventional diagnostic methods will not prove conclusive in the diagnosis of the impact sensors or the electronic controls or communication between other modules and devices that provide features of the Supplemental Restraint System (SRS). The most reliable, efficient, and accurate means to diagnose the impact sensors or the electronic controls and communication related to acceleration-type second row seating side impact sensor operation requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

The acceleration-type third row seating side impact sensors are electronic accelerometers that sense the rate of vehicle deceleration, which provides verification of the direction and severity of an impact. Each sensor also contains an electronic communication chip that allows the unit to communicate the sensor status as well as sensor fault information to the microprocessor in the Occupant Restraint Controller (ORC).

The ORC microprocessor continuously monitors all of the side passive restraint system electrical circuits to determine the system readiness. If the ORC detects a monitored system fault, it sets a Diagnostic Trouble Code (DTC) and controls the airbag indicator operation accordingly. The impact sensors each receive battery current and ground through the dedicated left and right sensor plus and minus circuits from the ORC. The impact sensors and the ORC communicate by modulating the voltage in the sensor plus circuit.

The hard wired circuits between the acceleration-type third row seating side impact sensors and the ORC may be diagnosed using conventional diagnostic tools and procedures. Refer to SYSTEM WIRING DIAGRAMS . However, conventional diagnostic methods will not prove conclusive in the diagnosis of the impact sensors or the electronic controls or communication between other modules and devices that provide features of the Supplemental Restraint System (SRS). The most reliable, efficient, and accurate means to diagnose the impact sensors or the electronic controls and communication related to acceleration-type third row seating side impact sensor operation requires the use of a diagnostic scan tool. Refer to the appropriate diagnostic information.

Note. The front and the second or third row seating side impact sensors are interchangeable.

Scheme 69

1. Disconnect and isolate the battery negative cable. Wait two minutes for the system capacitor to discharge before further service.
2. Service access for the front impact sensors is accomplished by reaching behind the front end module carrier (2) from the top of the engine compartment and between the inboard end of either front lamp unit housing (3) and either outboard end of the cooling module.
3. For the left front impact sensor only, remove the fresh air intake snorkel and the air filter housing from behind the front end module carrier for service access.
4. Disconnect the front end module wire harness connector (5) from the connector receptacle of the right or left front impact sensor (1).
5. Remove the screw (4) that secures the front impact sensor to the back (engine compartment side) of the front end module carrier.
6. Pull the front impact sensor straight back from the mounting location to disengage the anti-rotation pin on the base of the sensor from the clearance hole in the front end module carrier.
7. Remove the right or left front impact sensor from the engine compartment.

Scheme 70

1. Disconnect and isolate the battery negative cable. Wait two minutes for the system capacitor to discharge before further service.
2. Remove the trim panel from the inside of the right or left front door. Refer to «Body/Door - Front/PANEL, Door Trim - Removal»(ref-353577-S40808100392010011200000) .
3. Disconnect the front door wire harness connector (3) from the side impact sensor (1) connector receptacle.
4. Remove the two screws (2) that secure the side impact sensor to the front door module carrier panel (4).
5. Remove the side impact sensor from the door.

Note. The front and the second or third row seating side impact sensors are interchangeable.

Scheme 71

1. Disconnect and isolate the battery negative cable. Wait two minutes for the system capacitor to discharge before further service.
2. Open the sliding door.
3. Remove the quarter trim panel from the lower C-pillar (1). Refer to «Body/Interior/PANEL, Quarter Trim - Removal»(ref-353577-S13349045142010011200000) .
4. Disconnect the body wire harness connector (4) from the side impact sensor (3) connector receptacle.
5. Remove the screw (2) that secures the side impact sensor to the lower C-pillar.
6. Pull the side impact sensor straight out from the mounting location to unsnap the anti-rotation pin on the base of the sensor from the clearance hole in the lower C-pillar.
7. Remove the side impact sensor from the vehicle.

Note. The front and the second or third row seating side impact sensors are interchangeable.

Scheme 72

1. Disconnect and isolate the battery negative cable. Wait two minutes for the system capacitor to discharge before further service.
2. Remove the quarter trim panel from the quarter inner panel over the rear wheel housing (1). Refer to «Body/Interior/PANEL, Quarter Trim - Removal»(ref-353577-S13349045142010011200000) .
3. Disconnect the body wire harness connector (2) from the side impact sensor (4) above the rear wheel housing on the quarter inner panel.
4. Remove the screw (3) that secures the side impact sensor to the quarter inner panel.
5. Pull the side impact sensor straight out from the mounting location to disengage the anti-rotation pin on the base of the sensor from the clearance hole in the quarter inner panel.
6. Remove the side impact sensor from the vehicle.

Note. The front and the second or third row seating side impact sensors are interchangeable.

1. Service access for the front impact sensors is accomplished by reaching behind the front end module carrier (2) from the top of the engine compartment and between the inboard end of either front lamp unit housing (3) and either outboard end of the cooling module.
2. Position the right or left front impact sensor (1) into the engine compartment.
3. Align and insert the anti-rotation pin on the base of the sensor into the clearance hole on the back (engine compartment side) of the front end module carrier.
4. Install and tighten the screw (4) that secures the front impact sensor to the front end module carrier. Tighten the screw to 11 N.m (97 in. lbs.).
5. Reconnect the front end module wire harness connector (5) to the connector receptacle of the front impact sensor.
6. For the left front impact sensor only, reinstall the fresh air intake snorkel and the air filter housing behind the front end module carrier.
7. Do not reconnect the battery negative cable at this time. The Supplemental Restraint System (SRS) verification test procedure should be performed following service of any SRS component. See «Restraints - Standard Procedure»(ref-353580-S33366774452010011200000) .

Note. Be certain that the gasket between the pressure-type side impact sensor and the front door module carrier panel is in good condition and positioned on the back of the sensor. There MUST be a good seal between the sensor and the module carrier panel for the sensor to operate properly. If the gasket is in poor condition, replace the sensor.

1. Position the side impact sensor (1) to the right or left front door module carrier panel (4). When the sensor is correctly positioned, the arrow on the sensor label will be pointed toward the bottom of the door.
2. Install and tighten the two screws (2) that secure the side impact sensor to the door. Tighten the screws to 2.4 N.m (21 in. lbs.).
3. Reconnect the front door wire harness connector (3) to the sensor connector receptacle.
4. Reinstall the trim panel onto the inside of the right or left front door. Refer to «Body/Door - Front/PANEL, Door Trim - Installation»(ref-353577-S06548906242010011200000) .
5. Do not reconnect the battery negative cable at this time. The Supplemental Restraint System (SRS) verification test procedure should be performed following service of any SRS component. See «Restraints - Standard Procedure»(ref-353580-S33366774452010011200000) .

Note. The front and the second or third row seating side impact sensors are interchangeable.

1. Position the side impact sensor (3) to the lower C-pillar (1).
2. Align the anti-rotation pin on the base of the sensor with the clearance hole in the lower C-pillar, then press on the sensor firmly and evenly to snap the pin into place.
3. Install and tighten the screw (2) that secures the side impact sensor to the lower C-pillar. Tighten the screw to 11 N.m (97 in. lbs.).
4. Reconnect the body wire harness connector (4) to the side impact sensor on the lower C-pillar.
5. Reinstall the quarter trim panel onto the lower C-pillar. Refer to «Body/Interior/PANEL, Quarter Trim - Installation»(ref-353577-S36809696592010011200000) .
6. Do not reconnect the battery negative cable at this time. The Supplemental Restraint System (SRS) verification test procedure should be performed following service of any SRS component. See «Restraints - Standard Procedure»(ref-353580-S33366774452010011200000) .

Note. The front and the second or third row seating side impact sensors are interchangeable.

1. Position the side impact sensor (4) to the quarter inner panel above the rear wheel housing (1).
2. Align the anti-rotation pin on the base of the sensor with the clearance hole in the quarter inner panel, then press on the sensor firmly and evenly to snap the pin into place.
3. Install and tighten the screw (3) that secures the side impact sensor to the quarter inner panel. Tighten the screw to 11 N.m (97 in. lbs.).
4. Reconnect the body wire harness connector (2) to the side impact sensor on the quarter inner panel.
5. Reinstall the quarter trim panel onto the quarter inner panel over the rear wheel housing. Refer to «Body/Interior/PANEL, Quarter Trim - Installation»(ref-353577-S36809696592010011200000) .
6. Do not reconnect the battery negative cable at this time. The Supplemental Restraint System (SRS) verification test procedure should be performed following service of any SRS component. See «Restraints - Standard Procedure»(ref-353580-S33366774452010011200000) .

Scheme 73

The seat track position sensor (2) is a Hall Effect-type sensor used on some vehicles. This sensor consists of a Hall Effect Integrated Circuit (IC) chip encased in potting material within a cavity of the molded plastic sensor housing.

The sensor housing has a mounting slot containing an integral latch feature (1) and slides and latches onto a stamped metal blade-type bracket located on the inboard side of the upper inboard seat adjuster track near the rear of the driver side front seat. A molded connector receptacle (3) integral to the sensor housing is connected to the vehicle electrical system through a connector and take out of the driver side front seat wire harness beneath the front seat cushion frame.

The seat track position sensor cannot be adjusted or repaired and, if ineffective or damaged, the entire sensor must be replaced.