Lincoln Aviator: Power Steering / Removal and Installation - Tie Rod End
Special Tool(s) /
General Equipment
Removal
NOTE:
Removal steps in this procedure may contain installation details.
-
Remove the wheel and tire.
Refer to: Wheel and Tire (204-04A Wheels and Tires, Removal and Installation).
-
-
Loosen the tie rod end jam nut.
Torque:
35 lb.ft (48 Nm)
-
Remove and discard the outer tie rod end nut.
Torque:
52 lb.ft (70 Nm)
-
NOTICE:
Do not use a hammer to separate the outer
tie-rod end from the wheel spindle or damage to the wheel spindle may
result.
NOTICE:
Use care when installing the tie rod separator or damage to the outer tie-rod end boot may occur.
Separate the outer tie rod end from the wheel knuckle.
Use the General Equipment: Tie Rod End Remover
-
NOTE:
Count and record the number of turns required to
remove the outer tie-rod end for reference during installation.
Remove the tie-rod end.
Installation
-
To install, reverse the removal procedure.
-
Check and if necessary, adjust front toe.
Refer to: Front Toe Adjustment (204-00 Suspension System - General Information, General Procedures).
Special Tool(s) /
General Equipment
Boot Clamp Pliers
Materials
Name
Specification
Motorcraft® Premium Long-Life GreaseXG-1-E1
ESA-M1C75-B
Removal
NOTICE:
When servicing inner tie rods, install a new bellows boot
and clamps...
Other information:
WARNING: When loading the roof
racks, we recommend you evenly distribute
the load, as well as maintain a low center
of gravity. Loaded vehicles, with higher
centers of gravity, may handle differently
than unloaded vehicles. Take extra
precautions, such as slower speeds and
increased stopping distance, when driving
a heavily loaded vehicle...
Depower
WARNING:
Incorrect repair techniques or actions can cause an
accidental Supplemental Restraint System (SRS) deployment. Never
compromise or depart from these instructions. Failure to precisely
follow all instructions could result in serious personal injury from an
accidental deployment...