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Lincoln Aviator 2020-2023 Service Manual / Body and Paint / Body and Paint / Supplemental Restraint System / Removal and Installation - Driver Airbag

Lincoln Aviator: Supplemental Restraint System / Removal and Installation - Driver Airbag

Removal

  WARNING: The following procedure prescribes critical repair steps required for correct restraint system operation during a crash. Follow all notes and steps carefully. Failure to follow step instructions may result in incorrect operation of the restraint system and increases the risk of serious personal injury or death in a crash.

  1.   WARNING: Before beginning any service procedure in this manual, refer to health and safety warnings in section 100-00 General Information. Failure to follow this instruction may result in serious personal injury.


    Refer to: Pyrotechnic Device Health and Safety Precautions (100-00 General Information, Description and Operation).
  1. Depower the SRS.
    Refer to: Supplemental Restraint System (SRS) Depowering (501-20B Supplemental Restraint System, General Procedures).
  1. At the side of the steering wheel cover, locate the hole and insert a 3 mm (0.125 inch) hex bit.

  1. NOTE: The driver airbag has been removed for clarity.

    Contact the hex key to the spring clip.
    1. Push in on the steering wheel spring clip to release the driver airbag retainer.
    1. Pull the driver airbag out and separate it from the steering wheel.
  1. At the side of the steering wheel cover, locate the hole and insert a 3 mm (0.125 inch) hex key.

  1. NOTE: The driver airbag has been removed for clarity.

    Contact the hex key to the spring clip.
    1. Push in on the steering wheel spring clip to release the driver airbag retainer.
    1. Pull the driver airbag out and separate it from the steering wheel.
  1. Disconnect the driver airbag electrical connectors and remove the driver airbag.

Installation

  WARNING: Incorrect repair techniques or actions can cause an accidental Supplemental Restraint System deployment. Make sure the restraint system is depowered before reconnecting the component. Refer to the Supplemental Restraint System depowering General Procedure in section 501-20B. Failure to precisely follow depowering instructions could result in serious personal injury from an accidental deployment.

  1. Connect the driver airbag electrical connectors.

  1. Align the driver airbag to the steering wheel and push in, engaging the driver airbag retainers to the spring clips.
    • After installation, pull the driver airbag from the 3 and 6 o'clock positions to make sure it is retained in the steering wheel.
  1. Repower the SRS.
    Refer to: Supplemental Restraint System (SRS) Repowering (501-20B Supplemental Restraint System, General Procedures).

    Removal and Installation - C-Pillar Side Impact Sensor

    Removal   WARNING: The following procedure prescribes critical repair steps required for correct restraint system operation during a crash. Follow all notes and steps carefully...

    Removal and Installation - Driver Knee Airbag

    Removal   WARNING: The following procedure prescribes critical repair steps required for correct restraint system operation during a crash. Follow all notes and steps carefully...

    Other information:

    Lincoln Aviator 2020-2023 Service Manual: General Procedures - Evaporative Emission System Leak Test


    Activation Phase 1 - Leak Verification Run the EVAP Test with the scan tool. NOTE: Some small leaks may not be detected using the EVAP Test. If the system has passed the test but a leak is still suspected, then proceed to Phase 2...

    Lincoln Aviator 2020-2023 Service Manual: Diagnosis and Testing - Fuel Tank and Lines


    Diagnostic Trouble Code (DTC) Chart Diagnostics in this manual assume a certain skill level and knowledge of Ford-specific diagnostic practices.REFER to: Diagnostic Methods (100-00 General Information, Description and Operation).   Diagnostic Trouble Code Chart Module   DTC Description Action   PCM P008A:00 Low Pressure Fuel System Pressure - Too Low: No Sub Type Information   GO to Pinpoint Test HC   PCM P008B:00 Low Pressure Fuel System Pressure - Too High: No Sub Type Information   GO to Pinpoint Test HC   PCM P00BA:00 Low Fuel Pressure - Forced Limited Power: No Sub Type Information   GO to Pinpoint Test HC   PCM P00BB:00 Fuel Injector Insufficient Flow - Forced Limited Power: No Sub Type Information   GO to Pinpoint Test HC   PCM P0148:00 Fuel Delivery Error: No Sub Type Information   GO to Pinpoint Test HC   PCM P0230:00 Fuel Pump Primary Circuit: No Sub Type Information   GO to Pinpoint Test KC   PCM P0231:00 Fuel Pump Secondary Circuit Low: No Sub Type Information   GO to Pinpoint Test KC   PCM P0232:00 Fuel Pump Secondary Circuit High: No Sub Type Information   GO to Pinpoint Test KC   PCM P025A:00 Fuel Pump Module A Control Circuit/Open: No Sub Type Information   GO to Pinpoint Test KC   PCM P025B:00 Fuel Pump Module A Control Circuit Range/Performance: No Sub Type Information   GO to Pinpoint Test KC   PCM P025C:00 Fuel Pump Module A Control Circuit Low: No Sub Type Information   GO to Pinpoint Test KC   PCM P025D:00 Fuel Pump Module A Control Circuit High: No Sub Type Information   GO to Pinpoint Test KC   PCM P027B:00 Fuel Pump Module B Control Circuit Range/Performance: No Sub Type Information   GO to Pinpoint Test KC   PCM P0627:00 Fuel Pump A Control Circuit/Open: No Sub Type Information   GO to Pinpoint Test KC   PCM P064A:00 Fuel Pump Control Module A: No Sub Type Information   GO to Pinpoint Test KC   PCM P166A:00 Restraints Deployment Communication Circuit: No Sub Type Information   GO to Pinpoint Test KC   PCM P2632:00 Fuel Pump B Control Circuit/Open: No Sub Type Information   GO to Pinpoint Test KC   PCM P26EA:00 Fuel Pump Control Module B: No Sub Type Information   GO to Pinpoint Test KC   PCM U0109:00 Lost Communication With Fuel Pump Control Module A: No Sub Type Information   GO to Pinpoint Test KC   PCM U016C:00 Lost Communication With Fuel Pump Control Module B: No Sub Type Information   GO to Pinpoint Test KC   PCM U210B:00 Lost Communication Between Fuel Pump Control Module A And Restraints Control Module: No Sub Type Information   GO to Pinpoint Test KC Global Customer Symptom Code (GCSC) Chart Diagnostics in this manual assume a certain skill level and knowledge of Ford-specific diagnostic practices...

    Categories

    Seatbelt Height Adjustment

    WARNING: Position the seatbelt height adjuster so that the seatbelt rests across the middle of your shoulder. Failure to adjust the seatbelt correctly could reduce its effectiveness and increase the risk of injury in a crash.

    Adjust the height of the shoulder belt so the belt rests across the middle of your shoulder. Slide the adjuster up to raise the belt. Press the button and slide it down to lower the belt.

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