Install And Weld In Complete A-Pillar - Ar63.20-P-1100-10LW
Model 205.0/1/2
The following steps are shown on the left side of the vehicle and must be performed analogously on the right side 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 rivets (areas C).
- A-pillar inner panel (7)
(areas D).
- A-pillar inner panel (7)
(areas E, F and G).
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 F).
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.
Hi Use spacers.
- Drill Ø 6.7 mm rivet holes in A-pillar reinforcement (6) (areas H1
and H2
).
Drill rivet holes from inside through present hole in body (area H2).
- 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 (area I2 ).
- A-pillar reinforcement (6)
(area J2 ).
- Rivet A-pillar reinforcement (6) with 0 6, 5x12.5 rivet (area I1).
- A-pillar reinforcement (6)
(areas J1).
- A-pillar reinforcement (6)
(areas K1 , K2 and K3 ).
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) K1
and K2
).
Grind down flat on contact surfaces on B-pillar paneling and beaded area 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.
- Drill out connecting flange (9) on old A-pillar reinforcement section with Ø 7 mm bit.
If connecting flange (9) is damaged
↓
Fabricate connecting flange (9).
- Install connecting flange (9), fit and fix in place.
- Connecting flange (9)
(area K4 ).
- Install connecting panel (8), fit and fix in place.
Center connecting panel (8) above inert gas weld on A-pillar reinforcement.
- Drill Ø 6.7 mm rivet holes in connecting panel (8) through present holes (area L1
).
When drilling, ensure that the bit does not reach too far into the A-pillar reinforcement.
Otherwise the water drain hose in the A-pillar reinforcement can be damaged.
- Remove connecting panel (8).
- Drill rivet holes on connecting panel (8) and body on both sides.
- Apply 2-component adhesive to body cross-hatched inner C-pillar side wall.
Observe pretreatment of bonding surfaces and manufacturer's specifications for curing and processing time of 2-component adhesive.
- Install connecting panel (8) and fix in place.
- Rivet connecting panel (8) with Ø 6.5x12.5 rivets (area L2
).
- 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 , V2 and V3 ).
- 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.
- Apply sealant to foam part in crosshatched area (area J3 ).
- Apply 2-component adhesive to body in crosshatched areas J4
).
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 rivets (area W3 ).
- A-pillar paneling (5)
(areas 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 Y).
- Remove solder residues and grinding dust.