Lincoln Aviator: Supplemental Restraint System / 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. 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.
NOTE:
LH (left-hand) shown, RH (right-hand) similar.
NOTE:
Removal steps in this procedure may contain installation details.
-
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).
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Depower the SRS.
Refer to: Supplemental Restraint System (SRS) Depowering (501-20B Supplemental Restraint System, General Procedures).
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Position the rear door weather-strip aside.
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Release the clips and remove the rear door scuff plate trim panel.
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Fold the second row outboard seat to the easy entry position.
-
Remove the tie down hook.
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Position the tie down hook bolt cover up
-
Remove the tie down hook bolt.
-
NOTE:
The seat is removed for clarity.
Release the clips and position the loadspace trim panel away enough to access the C-pillar side impact sensor.
-
Remove the C-pillar side impact sensor.
-
Disconnect the electrical connector.
-
Remove the bolt.
Torque:
106 lb.in (12 Nm)
-
Remove the C-pillar side impact sensor.
Installation
-
NOTE:
The C-pillar side impact sensor mating surfaces must
be smooth and allow for a flush attachment to each other.
To install, reverse the removal procedure.
-
Repower the SRS.
Refer to: Supplemental Restraint System (SRS) Repowering (501-20B Supplemental Restraint System, General Procedures).
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
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:
Removal
Remove the second row single seat cushion cover.
Refer to: Second Row Single Seat Cushion Cover - Vehicles With: Second Row Captain Chairs (501-10B Second Row Seats, Removal and Installation).
Disconnect the second row seat cushion blower motor electrical connector...
System Operation
System Diagram
Item
Description
1
Rear footwell ambient lighting LEDs
2
LIN
3
DDM
4
LH welcome mat lamp
5
RH welcome mat lamp
6
PDM
7
Front cup holder lighting LEDs
8
Front footwell ambient lighting LEDs
9
Rear door ambient lighting LEDs
10
HS-CAN1
11
APIM
12
HS-CAN3
13
FDIM
14
GWM
15
MS-CAN
16
Liftgate lamp
17
Vanity mirror lamps
18
Glove compartment lamp
19
Console/bin lamps
20
LH second row interior lamp
21
RH second row interior lamp
22
Cargo lamp
23
Third row interior lamp
24
LIN
25
Overhead console
26
RGTM
27
LIN
28
Headlamp switch
29
Scuff plate lamps
30
Second row cup holder lighting LEDs
31
Front door ambient lighting LEDs
32
Instrument panel ambient lamps
33
Center console pass thru ambient lamp
34
Door latch control modules
35
Door ajar switch
36
Rear door puddle lamps
37
LIN
38
BCM
39
Exterior door handle LEDs
Network Message Chart
DDM And PDM Network Input Messages
Broadcast Message
Originating Module
Message Purpose
Welcome mat lamp activation
GWM
Provides welcome mat lamp request from the GWM to activate the exterior mirror welcome mat lamps...