Install A-Pillar Outer Section - Ar63.20-P-1102-03LW
Model 205.0/1/2
Model 253
The following steps are shown on the left side of the vehicle and must be performed on the right side in the same way in the event of damage.
- Install A-pillar inner panel (7) and A-pillar reinforcement with portal bracket, fit and fix in place.
Use spacers.
- Drill Ø 6.7 mm rivet holes in inner A-pillar (7) (areas A and B).
Drill rivet holes through present holes in body (areas A).
Drill rivet holes through present holes in A-pillar inner panel (7) (areas B).
- Remove portal bracket, A-pillar reinforcements and A-pillar inner panel (7).
- Deburr rivet holes on A-pillar inner panel (7) and body on both sides.
- Remove drilling chips.
- Coat insides of riveted joints with zinc dust paint.
- Install A-pillar inner panel (7) and fix in place.
- Rivet A-pillar inner panel (7) with Ø 6.5x12.5 rivet (areas C).
- A-pillar inner panel (7)
(areas D).
- A-pillar inner panel (7)
(areas E and F).
Inert gas weld in intervals and allow welding area to cool down in between. Reduces heat distortion.
- Grind inert gas weld on A-pillar inner panel (7) down flat (area E).
Grind down flat only in beaded areas and contact surfaces of A-pillar reinforcement.
- Clean welding areas which are no longer accessible after installing upper front longitudinal member and A-pillar reinforcement and coat with zinc dust paint.
- Install A-pillar reinforcement (6) with portal bracket, fit and fix in place.
Use spacers.
- Drill Ø 6.7 mm rivet holes in A-pillar reinforcement (6) (areas G and H).
Drill rivet holes from inside through present hole in body (area H).
- Remove A-pillar reinforcement (6) and portal bracket.
- Deburr rivet holes on A-pillar inner panel (6) and body on both sides.
- Apply sealant to foam parts on A-pillar reinforcement (6) in crosshatched areas.
- Apply 2-component adhesive to body in crosshatched areas.
Observe pretreatment of bonding surfaces and manufacturer's specifications for curing and processing time of 2-component adhesive.
- Install A-pillar reinforcement (6) and fix in place.
- Rivet A-pillar reinforcement (6) with Ø 6.5x12.5 rivets (areas I1 and I2 ).
- A-pillar reinforcement (6)
(areas J).
- A-pillar reinforcement (6)
(areas K and L).
Inert gas weld in intervals and allow welding area to cool down in between. Reduces heat distortion.
- Grind inert gas welds down flat on A-pillar reinforcement (6) (areas K and L).
Grind down flat beaded areas and contact surfaces on B-pillar paneling only.
- Clean welding areas which are no longer accessible after installing upper front longitudinal member and A-pillar paneling and coat with zinc dust paint.
- Install upper front longitudinal member (1) fit with welding device and fix in place.
- Install reinforcement (3), fit and fix in place.
- Drill Ø 6.7 mm rivet holes in upper front longitudinal member (1) and reinforcement (3) (areas M, N and O).
Drill rivet holes from inside through present hole in body (area N).
- Remove upper front longitudinal member (1), reinforcement (3) and welding device.
- Deburr drill holes on upper front longitudinal member (1), reinforcement (3) and body on both sides.
- Remove drilling chips.
- Coat inside of riveted joint with zinc dust paint (areas O).
- Apply 2-component adhesive to body in crosshatched areas.
Observe pretreatment of bonding surfaces and manufacturer's specifications for curing and processing time of 2-component adhesive.
- Install upper front longitudinal member (1) with welding device and fix in place.
- Install reinforcement (3) and fix in place.
- Rivet upper front longitudinal member (1) and reinforcement (3) with Ø 6.5x12.5 rivets (areas P1 and P2 ).
- Rivet upper front longitudinal member (1) and reinforcement (3) with Ø 6.5x14.5 rivets (areas P3 ).
- Upper front longitudinal member (1)
(areas Q).
- Install strut (2) and bracket (4), fit and fix in place.
- Drill Ø 6.7 mm rivet holes in strut (2) and bracket (4) (areas R and S).
- Remove strut (2) and bracket (4).
- Deburr rivet holes on strut (2), bracket (4) and body on both sides.
- Remove drilling chips.
- Coat insides of riveted joints with zinc dust paint.
Do not coat bonding surfaces with zinc dust paint (areas R).
Otherwise adhesion problems may occur.
- Apply 2-component adhesive to body in crosshatched areas.
Observe pretreatment of bonding surfaces and manufacturer's specifications for curing and processing time of 2-component adhesive.
- Install strut (2) and bracket (4) and fix in place.
- Rivet strut (2) with Ø 6, 5x12.5 rivets (areas T).
- Rivet strut (2) and bracket (4) with Ø 6.4x12 rivets (areas U).
- Install A-pillar paneling (5), fit and fix in place.
- Drill Ø 6.7 mm rivet holes on A-pillar paneling (5) ((areas V1 and V2 ).
- Remove A-pillar paneling (5).
- Deburr rivet holes on A-pillar inner panel (5) and body on both sides.
- Remove drilling chips.
- Coat insides of riveted joints with zinc dust paint.
Do not apply zinc dust paint to bonding surfaces (areas V2).
Otherwise adhesion problems may occur.
- Model 205.0/1/2
Apply 2-component adhesive to body in crosshatched areas.
Observe pretreatment of bonding surfaces and manufacturer's specifications for curing and processing time of 2-component adhesive.
- Install A-pillar paneling (5) and fix in place.
- Rivet A-pillar paneling (5) with Ø 6.4x12 rivets (areas W1 ).
- Rivet A-pillar paneling (5) with Ø 6.5x12 5 rivets (areas W2 ).
- Rivet A-pillar paneling (5) with Ø 6.5x12 5 rivet (area W3 ).
- A-pillar paneling (5)
(area X).
- A-pillar paneling (5)
(areas Y).
Inert gas weld in intervals and allow welding area to cool down in between Reduces heat distortion.
- Grind inert gas welds down flat (areas Y).
- Solder surfaces on A-pillar paneling (5) with body solder and smooth (areas YV).
- Remove solder residues and grinding dust.