VAZ 2101, 2102
1. Specifications
2. Operation and service
3. The engine
4. Fuel system
5. Ignition system
6. Start and gymnastics system
7. Transmission
8. A running gear
9. A steering
10. Brake system
11. An electric equipment
12. A body
12.1. Features of the device
12.2. Repair of a skeleton of a body
12.2.1. Check and skeleton editing
12.2.2. Replacement of a forward wing
12.2.3. Replacement of a back wing
12.2.4. Roof replacement
12.2.5. Replacement of panels передка and a back
12.2.6. Repair of the deformed surfaces
12.3. Paint and varnish coverings
12.4. Anticorrosive protection of a body
12.5. Doors
12.6. A cowl, a luggage carrier cover, bumpers
12.7. Osteklenie bodies and a windscreen washer
12.8. The panel of devices
12.9. Seats
12.10. A heater
12.11. Possible malfunctions of a body, their reason and elimination methods
13. Features of repair
14. Appendices


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12-2-3-zamena-zadnego-kryla.html

12.2.3. Replacement of a back wing

Places of welding of a back wing

Points designate seams of contact welding.

Arrows specify points of gas welding.

Rules of repair of a back wing same, as well as for a forward wing.

PERFORMANCE ORDER
1. At wing replacement remove a back bumper, a back lantern, катафот.
2. Release a luggage carrier. Remove a rubber sealant, a trunk floor upholstery, a fuel tank (if the right wing varies) and disconnect electroconducting.
3. Cut down thin острозаточенным a chisel or cut off the grinding machine on a connection wing:
      – With an arch of a back wheel on a bend, having receded from an edge of a wing of 20 mm;
      – With a floor of a spare wheel (or a fuel tank) on a bend, having receded from an edge of a wing of 12-15 mm;
      – With the panel of a back of a body, having receded from a connection line on 2 mm;
      – With the panel of a cross-beam of a back window, having receded from an edge of a bend of a wing of 2 mm;
      – With a back part боковины on a bend, having receded from an edge of a wing of 15-20 mm.
4. Cut down a square of connection of a wing with the panel of a back of the top part on a horizontal line, having receded from an edge of a square of 15 mm.
5. Drill points of contact welding on connections of a wing with the back lateral panel of a roof and disconnect a wing.
6. Remove the remained strips of a wing in connections with a body and smooth out the grinding machine seats of elements of a body and a new wing.
7. Adjust a new wing in a place of landing and take quick-detachable captures.
8. Weld covered with gas welding to the bottom and back part боковины, to the panel of a cross-beam of a back window, the lateral panel of a roof, to a square of connection of the panel of a back of a body, to a floor of a spare wheel (or a fuel tank). In drawing of a place of gas welding are specified by arrows.
9. Check up landing of a wing concerning interfaced surfaces and weld its contact welding with step of 40-50 mm.
10. Establish and weld wing amplifiers, having enclosed a lining.

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12.2.2. Replacement of a forward wing
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12.2.4. Roof replacement