Remove A-Pillar And B-Pillars Completely With Longitudinal Member - Ar63.20-P-1120-01LF
Model 222
except code Z07 (B7 armoring on special protection version)
The following steps are shown on the left side of the vehicle and must be accomplished analogously on the right side in the event of damage.
- Model 222.0/1
except code Z07 (B7 armoring on special protection version) Mark separating points on paneling (1) and cut (areas A and B).
Do not make the cuts too deep
Otherwise the components below can be damaged and weakened.
Mark separating point along Y-marking (area BA) If the connection point is to be offset in area B provide overlapping of approx. 10 mm.
Dimensions:
a = approx. 150 mm
- Model 222.0/1
except code Z07 (B7 armoring on special protection version) Separate adhesive bead between paneling (1) and outer rear wheel well (area C)
Paneling (1) is glued to outer rear wheel well.
Shown on model 222.0
- Model 222.9
except code Z07 (B7 armoring on special protection version) Mark separating points on paneling (1) and cut (areas R1 , R2 and R3 ).
Do not make the cuts too deep.
Otherwise the components below can be damaged and weakened.
Mark separating point along Y-marking (area R3 ).
If connection in area R3 is to be crimped provide overlap of approx. 10 mm.
Dimensions:
r1 = approx 260 mm
r2 = approx. 130 mm
Shown on model 222.9
Shown on model 222.0
- Expose spot welds on paneling (1) and cut (areas D1
, D2
and D3
).
Cut out spot welds through two panel thicknesses (areas D2 ).
Cut out spot welds through two panel thicknesses (areas D3 ).
Shown on model 222.0
- Expose spot welds on paneling (1) and cut (areas E1
, E2
and E3
).
Cut out spot welds through two panel thicknesses (areas E2 ).
Cut out spot welds through two panel thicknesses (areas E3 ).
Shown on model 222.0
- Heat paneling (1) in crosshatched areas.
Cross-hatched areas are bonded.
Shown on model 222.0
- Heat paneling (1) in crosshatched areas.
Cross-hatched areas are bonded.
- Remove paneling (1).
Shown on model 222.0
- Mark separating point on A-pillar and B-pillar reinforcement (2) and cut (area F).
Do not cut too deeply.
Otherwise the components below can be damaged and weakened.
Cut is required to expose spot welds behind (area F 1).
- Expose spot welds on A-pillar and B-pillar reinforcement (2) and cut (areas F1, F2
and F3
).
Cut out spot welds through two panel thicknesses (areas F2 ).
Cut out spot welds through two panel thicknesses (areas F3 ).
Shown on model 222.0
- Expose spot welds on A-pillar and B-pillar reinforcement (2) and cut (areas G).
- Expose MIG solder seam on A-pillar and B-pillar reinforcement (2) and cut (area H).
Shown on model 222.0
- Expose spot welds on A-pillar and B-pillar reinforcement (2) and cut (area I).
- Expose weld seams on A-pillar and B-pillar reinforcement (2) and cut (area K).
- Expose spot welds on A-pillar and B-pillar reinforcement (2) and cut (areas L).
Shown on model 222.0
Shown on model 222.0
- Heat A-pillar and B-pillar reinforcement (2) in crosshatched areas.
Cross-hatched areas are bonded.
Shown on model 222.0
- Heat A-pillar and B-pillar reinforcement (2) in crosshatched areas.
Cross-hatched areas are bonded.
Heat A-pillar reinforcement (2) from inside (area M).
Shown on model 222.0
- Heat A-pillar and B-pillar reinforcement (2) in crosshatched areas.
Cross-hatched areas are bonded.
Shown on model 222.0
- Heat A-pillar and B-pillar reinforcement (2) in crosshatched areas.
Cross-hatched areas are bonded.
- Remove - pillar and B-pillar reinforcement (2).
Shown on model 222.0
- Expose spot welds on A-pillar inner panel (3.1) and cut (areas N1
and N2
).
Cut out spot welds through two panel thicknesses (areas N2 ).
Shown on model 222.0
- Expose spot welds on roof frame inner panel (3.2) and cut (areas O and O2
).
Separate spot welds on roof frame inner panel (3.2) from bottom (area O2 ).
- Expose self-piercing riveting on roof frame inner panel (3.2) and drill with Ø 6 mm bit (areas 03).
The self-piercing rivets can also be separated with a riveter for self-piercing and flow-form rivets.
Shown on model 222.0
- Support front and center roof carrier.
- Heat A-pillar inner panel (3.1) and roof frame inner panel (3.2) in crosshatched areas.
Cross-hatched areas are bonded.
- Remove A-pillar inner panel (3.1), roof frame inner panel (3.2) and B-pillar inner panel (3.3).
Shown on model 222.0
- Remove remaining adhesive material in area of outer rear wheel well (area Q).
The height of the remaining adhesive material should not exceed 2 mm. Remove loose adhesive material.
- Repair bare parts with primer stick (area Q).
- Sand bonding surfaces on structural foam part with fine-grit abrasive paper (area R).
Observe pretreatment of bonding surfaces.
- Grind mating surfaces down to bare metal in the cross-hatched inner C-pillar sidewall.
Sand down spot weld flanges to bare metal on both sides.
- Remove grinding dust and drill chips.
- Coat insides of spot weld flanges with zinc dust paint.
Do not coat bonding surfaces with zinc dust paint (areas P1 and P2 ).
Otherwise adhesion problems may occur.
Observe pretreatment of bonding surfaces.