They are cut off with a thin, sharp chisel or cut off with a grinding machine along the wing of the joint:
- with the rear wheel arch along the bend (Fig. 181), stepping back from the edge of the wing by 12-15 mm;
- with spare wheel floor (or fuel tank) along the bend, stepping back from the edge of the wing by 12-15 mm;
- with the rear panel of the body, stepping back from the connection line by 2 mm;
- with the rear window crossbar panel, 2 mm from the edge of the wing bend;
- with the rear part of the sidewall along the bend, stepping back from the edge of the wing by 15-20 mm.
Cut off the angle of the wing joint with the rear panel of the upper part of the horizontal line, stepping back from the edge of the angle by 15 mm. Using a drill with a diameter of 6-7 mm, drill out the contact welding points at the joint of the wing with the side panel of the roof and disconnect the wing. Remove the remaining strips of the wing, straighten the deformed edges and clean the seats of the body elements and the new wing.
The text is on the website [www.VAZbook.ru]
The new wing is adjusted to the landing site, secured with quick-release grips and the external clearances are checked (see fig. 178, 179). Welded with gas welding to the lower and rear part of the side panel, to the rear window crossbar panel, the side roof panel, to the rear panel connection angle, to the spare wheel floor (fuel tank) solder L62 or L68. In Fig. 181, the gas welding locations are shown by arrows. The fit of the wing relative to the mating surfaces is checked and it is welded using contact welding with a pitch of 40-50 mm. The wing reinforcements are welded using gas welding. In the absence of a contact welding machine, gas welding by melting the edges with an intermittent seam 20 mm long every 30 mm using L68 solder is allowed. In the doorway, wing welding is allowed using a semiautomatic device in a carbon dioxide environment.