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


7b94d386 стоимость плазменной резки металла
На сайте http://honeywell-rus.ru honeywell fk06.
Коттеджный поселок Софьино купить бетон с доставкой Тимонино.
Жилищный Адвокат Юридическая помощь Ново переделкино.





12-2-2-zamena-perednego-kryla.html

12.2.2. Replacement of a forward wing

Places of welding of a forward wing

Points designate seams of contact welding.

Arrows specify points of gas welding.

At insignificant damages (small dents, scratches, etc.), without removing a wing, execute рихтовку and colouring. After рихтовки necessarily check up a condition of an internal anticorrosive covering, if necessary, restore it.

At considerable deformations of a wing, ruptures, replace it.

PERFORMANCE ORDER
1. Remove a bumper, a cowl, the aerial, a forward door; from a wing remove the lateral index of turn, a headlight and a sidelight.
2. Cut down thin острозаточенным a chisel or cut off the grinding machine on a connection wing:
      – With the panel передка on 208 mm from a headlight downwards, having receded 2–3 mm from a connection line;
      – With a forward rack боковины a skeleton in length of 580 mm, having receded 5 mm from a line of a bend of the vertical amplifier;
      – With the bottom part боковины bodies on a vertical of 120 mm and horizontals of 180 mm, having receded from an edge of a wing of 25 mm.
3. Drill on the horizontal amplifier of a wing of a point of contact welding of the amplifier with elements передка on distance of 900 mm, and disconnect a wing from a body a thin flat chisel with the unbent end.
4. Remove thin острозаточенным a chisel 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.
5. Remove a dirt and a rust in a cavity closed by a wing, and put цинхроматный ground ГФ-073.
6. Adjust a new wing in a place of landing and take its quick-detachable captures.
7. Weld covered with gas welding on the ends of the horizontal amplifier of a wing, in junctions of a wing with a headlight casing, with the panel передка and the bottom overlay боковины. In drawing of a place of gas welding are designated by arrows. For gas welding use brass пруток Л62, Л63.
8. Check up position of a wing and backlashes (fig. the Basic sections of a body (a body kind sideways see)) and (fig. the Basic sections of a body (a body kind from above see)), at established a cowl and a door.
9. Weld covered with contact welding with step of 40-50 mm. In the absence of the kontaktno-welding car, electric welding in the environment of carbonic gas by a semiautomatic device a wire of Sv 08Г1С or Sv 08Г2С 0,8 mm is supposed in diameter. Also gas welding of a waste fillet of a wing with a mudguard передка a wire св08 in diameter 1,6–2,0 mm, panels передка with a wing and the amplifier of a wing with a forward rack brass solder Л62 or Л63 with technical brown is supposed. Diameter brass прутков 2–3 mm.

«The previous page
12.2.1. Check and skeleton editing
The following page»
12.2.3. Replacement of a back wing