6B8458 STRIP-UPPER Caterpillar parts
Rating:
Alternative (cross code) number:
CA6B8458
6B-8458
6B8458
CA6B8458
6B-8458
6B8458
Weight: 4 pounds 2 kg.
Information:
Illustration 14 g01457183
Start the engine. Raise circle assembly (20). Position bracket assembly (8) onto Tooling (B) and suitable blocking. Lower circle assembly (20) in order to position circle assembly (20) onto bracket assembly (8). The weight of bracket assembly (8) is approximately 785 kg (1730 lb).
Stop the engine.
Release the system pressure. Refer to Operation and Maintenance Manual, "System Pressure - Release".
Connect the air supply onto Tooling (A) .
Illustration 15 g01457423
Install spacer (19) .
Illustration 16 g01460228
Illustration 17 g01460229
Install Tooling (D) and bolts (12) onto pin (18). Use Tooling (D) and Tooling (F) in order to install pin (18). Remove bolts (12) and Tooling (D) from pin (18) .
Illustration 18 g01458073
Install plate (16) and bolts (15). Tighten bolts (15) to a torque of 270 40 N m (199 30 lb ft).
Illustration 19 g01458007
Use Tooling (G) in order to measure the thickness of plate (13). Record the measurement as dimension (A). Install plate (13) and two of bolts (12). Use Tooling (H) in order to measure the distance between the surface of plate (13) and the end of pin (18). Record the measurement as dimension (B). Subtract dimension (A) from dimension (B) and record the result as the average gap.
Remove two of bolts (12) and plate (13) .
Illustration 20 g01458075
Illustration 21 g01457269
Remove bolts (15) and plate (16). Install a thickness of shims (17) and shims (14) that is equal to the average gap +0.05 - 0.00 mm (+0.0020 - 0.0000 inch). Split the number of shims equally between both sides of the pin. Install plate (16) and bolts (15). Tighten bolts (15) to a torque of 270 40 N m (199 30 lb ft). Install plate (13) and bolts (12). Tighten bolts (12) to a torque of 270 40 N m (199 30 lb ft).
Disconnect the air supply from Tooling (A) .
Illustration 22 g01457104
Start the engine. Extend cylinder (11). Use Tooling (C) and a suitable lifting device in order to install pin assembly (10). Install bolt (9) .
Stop the engine.
Release the system pressure. Refer to Operation and Maintenance Manual, "System Pressure - Release".
Connect the air supply onto Tooling (A) .
Repeat Step 6 through Step 16 for the opposite side.
Illustration 23 g01458891
Remove Tooling (B) and the suitable blocking from bracket assembly (8) .
Illustration 24 g01456975
Install guard assembly (6). Install clamps (7). Connect grease hose assembly (5). Repeat this step for the opposite side.
Illustration 25 g01456945
Connect hose assemblies (4). Install clamps (3). Connect grease hose assembly (2) and install the connecting hardware. Connect grease hose assembly (1) and install the connecting hardware.
Illustration 26 g01459112
Remove Tooling (A) and replace the cap on the hydraulic tank.End By: Install the blade. Refer to Disassembly and Assembly, "Blade - Install".
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