ROD 9D6521 - Caterpillar

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(21 ) and (22) x 8 (15) x 6
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Apply thread lock and torque 8T-4132 Nut to 200 30 N m (148 22 lb ft)
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(K) 359-2860 Engine Compartment Shield Gp
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(A) 8T-4186 Bolt (B) 7X-7729 Washer
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(C) 359-2855 Engine Compartment Shield Gp (D) 204-9840 Seal (G) 8T-4222 Plated Washer (J) 8T-4133 Nut (H) 8T-4226 Plated Washer
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(L) 146-9473 Bumper reuse (M) 142-2623 Grommet reuse (N) 8M-2784 Grommet reuse (P) 214-5514 Grommet reuse (R) 300-7318 Seal reuse (S) 8V-6990 Grommet reuse (T) 6P-0699 Grommet reuse (U) 5F-9757 Grommet reuse (V) 1S-1014 Grommet reuse
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(36) 1P-4278 Hose Clamp (L1) Center line of fan (DD) 117.5 5 mm (4.63 0.2 inch) (EE) 187 5 mm (7.36 0.2 inch)Orient clamp (36) as shown and torque to 2.5 N m (22 lb in)
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Software Configuration and Calibration of the 387-1357 Fan Control Arrangement (Variable Pitch Fan)
Note: This feature can be configured and must be activated with Product Software Programming System (PSPS) or a service tool.
Use aCaterpillar Electronic Technician (Cat ET) and select the proper Electronic Control Module (ECM). Select "SERVICE" from the menu.
Select "CONFIGURATION" from the menu.
Double click on the desired feature on the configuration screen.
Select the desired status of the feature and click "OK". The feature will be activated on the next power cycle. Note: Note: Refer to 325-9618 International Standards Institute (ISO) or 367-8088 American National Standards Institute (ANSI) standard configuration (Variable Pitch Fan).