4407306 SWIVEL AS Caterpillar parts
Rating:
Alternative (cross code) number:
CA4407306
440-7306
4407306
CA4407306
440-7306
4407306
Weight: 143 pounds 64 kg.
Information:
Illustration 32 g00624140
Straighten the locking plates and remove bolts (20) that secure cover (19).
Remove the carbon from the threaded holes. Use bolts (20) as forcing screws to remove cover (19).
Illustration 33 g00624147
Use bolts (20) as forcing screws to remove cover assembly (21). Remove the O-ring seal from cover assembly (21).
Illustration 34 g00624152
Illustration 35 g00624157
Remove socket head bolts (22) that hold turbine bearing assembly (23).
Use socket head bolts (22) as forcing screws to remove turbine bearing assembly (23).
Illustration 36 g00624163
Illustration 37 g00624167
Remove socket head bolts (24) from turbine bearing assembly (23).
Separate turbine bearing assembly (23) and remove bushing (25).
Illustration 38 g00624173
Measure the inside diameter of turbine bearing assembly (23). The maximum reusable diameter for the turbine bearing is 55.060 mm (2.1677 inch).Note: For more information on the turbocharger, refer to Reuse and Salvage Guidelines, SEBF8092, "Specifications for Reusable Turbocharger Components on 3600 Family of Engines".
Illustration 39 g00624182
If damage is noted, remove cap (26) to perform an inspection. Be sure that the air passages are open.
Illustration 40 g01298832
Mark the position of diffuser (27) in compressor housing (4). Remove the bolts that hold diffuser (27) to compressor housing (4).
Illustration 41 g00624202
Illustration 42 g00624197
Attach a suitable lifting device to gas inlet housing (30). The weight of gas inlet housing (30) is approximately 41 kg (90 lb). Remove bolts (29) and the washers and remove segments (28) that secure gas inlet housing (30) to the bearing housing (center section).
Remove gas inlet housing (30).
Illustration 43 g00624223
Remove the bolts and locking plates (31).
Remove ring cover (32).
Remove bolts (33) and the locking plates. Remove nozzle (34) from the gas inlet housing.
If necessary, remove cap (35).
Illustration 44 g00624229
Inspect nozzle (34). Replace the nozzle, if the nozzle is damaged.
Clean each part with clean solvent. Handle each part carefully to prevent damage to the parts. Dry the parts with compressed air.
Inspect the compressor bearing assembly. Inspect the turbine bearing assembly. If the radial clearance exceeds the limits, the bearings must be replaced. The tolerance of the radial clearance was determined when the bearing clearances were checked. Also replace the bearings if high wear is observed.
If the axial clearance exceeds permissible limits, the thrust bearing must be replaced. This axial clearance was determined when the clearances of the thrust bearing were checked. Also replace the thrust bearing if high wear is observed.
Inspect the impeller assembly. Replace the impeller assembly if the impeller assembly is damaged.
Replace all the O-ring seals and the piston ring seals.
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