Lincoln Aviator: Suspension System - General Information / Specifications


  General Specifications

NOTE: Measurements listed at curb load. Curb load is defined as "full service fluids, full fuel tank(s), no passengers and no cargo".


Item Specification
Ball Joint Deflection (All Vehicles)
Lower 0 - 0.8 mm (0-0.032 in)
Upper 0 - 0.2 mm (0-0.008 in)
Side-to-Side Lean (All Vehicles)
Front — maximum 12 mm (0.472 in)
Rear — maximum 7 mm (0.275 in)
Front Ride Height
AWD Gas and PHEV vehicles * 58.2 mm (2.291 in) ± 12 mm (0.472 in)
RWD Gas vehicles * 48.3 mm (1.901 in) ± 12 mm (0.472 in)
Air Suspension vehicles ** 465 mm (18.307 in) ± 16 mm (0.629 in)
Rear Ride Height
AWD Gas and PHEV vehicles * 62.9 mm (2.476 in) ± 10 mm (0.393 in)
RWD Gas vehicles * 55.3 mm (2.177 in) ± 10 mm (0.393 in)
Air Suspension vehicles ** 469 mm (18.464 in) ± 14 mm (0.551 in)

* Refer Ride Height Measurement procedure in the General Procedures section of the workshop manual.

** Refer FDRS for ride height measurement instructions.

  Alignment Specifications

NOTE: Measurements listed at curb load. Curb load is defined as "full service fluids, full fuel tank(s), no passengers and no cargo".


Item LH RH Total / Split
Front
Camber - AWD Gas and All PHEV vehicles -0.55° ± 0.75° -0.55° ± 0.75° 0.0° ± 0.75°
Camber - RWD Gas vehicles -0.76° ± 0.75° -0.76° ± 0.75° 0.0° ± 0.75°
Camber - Air Suspension vehicles -0.80° ± 0.75° -0.80° ± 0.75° 0.0° ± 0.75°
Caster - AWD Gas and All PHEV vehicles 3.46° ± 0.75° 3.46° ± 0.75° 0.0° ± 0.75°
Caster - RWD Gas vehicles 3.68° ± 0.75° 3.68° ± 0.75° 0.0° ± 0.75°
Caster - Air Suspension vehicles 3.63° ± 0.75° 3.63° ± 0.75° 0.0° ± 0.75°
Toe - (positive value is toe in, negative value is toe out) - All Vehicles 0.25° ± 0.20°
Rear
Camber - AWD Gas and All PHEV vehicles -0.90° ± 0.75° -0.90° ± 0.75°
Camber - RWD Gas vehicles -0.90° ± 0.75° -0.90° ± 0.75°
Camber - Air Suspension vehicles -1.30° ± 0.75° -1.30° ± 0.75°
Toe - (positive value is toe in, negative value is toe out) - All Vehicles 0.12° ± 0.20° 0.12° ± 0.20° 0.24° ± 0.20°
Thrust Angle

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