ELBOW AS 1488379 - Caterpillar

Reman engine 0R3966 is built to reference engine arrangement131-4876 which was Tier I
certified and will produce emissions typical of the reference engine.
CONSIST
Reman engines come fully assembled and dyno-tested. Theseengines include hydraulic or
transmission oil coolers as appropriate and an air compressor. The rearengine-mounting
hardware, flywheel, alternator, fan drive, and associated wiring must be reusedfrom the core
engine or purchased separately. Each Reman engine arrangement can also replaceits
associated acceptable core part numbers (listed below) with minimal exchange ofparts.
Caterpillar?s cleaning, inspection and remanufacturingspecifications provide the best
possible value for our customers.
CORE RETURNS
Following are the only acceptable cores for each Reman engine:
Reman Part
Number Acceptable Core
Part Numbers
0R2785 2W0769
0R3966 131-4876, 144-3575, 203-2788
0R3968 1W0773
All engines returned as cores must meet the core acceptanceguidelines as identified in the
"Core Acceptance Criteria", SELD0231 which is under development atthis time and due for
publication later this year. In the interim, reference SELD0019 with thefollowing additions:
? The engine must "bar over".
? There is a core return time limit as described in the section below.
Also see SELD0020 "Engine Check List".
Please refer to the Caterpillar Core Management Information System (CMIS 2)Parts
Information application describing all Reman part/CAF and related information.Also refer
to other CMIS 2 inquiry applications such as Customer Profile, Inspection ReasonCodes,
Inspection Line Inquiry, Add Charge Information, Entitlement Activity,Entitlement Inquiry,
CCR Inquiry, CCR Entry, Shipment Processing; Process Packaging Grief; andReporting to
properly manage core returns and monitor inspection performance. Thisinformation will be
available to all dealers worldwide after your CMIS 2 conversion date. In themeantime,
please continue to use the current CMIS Entitlement Parts Inquiry Screendescribing the list
of parts in a Core Acceptability Family (CAF) and related part number detail.
For the latest updates of RemanPolicies and Core Management (SELD0122),Core
Management Systems & Operations Procedures (SELD0040),and Shipping Instructions
(SELD0039), go to the Reman website and click on Procedures and Policies (listedunder
Reman Program Information).
If you have any questions regarding core return processing, feelfree to call Corinth toll free
at (800) 537-2928.
CORE RETURN TIME LIMIT
The current Major Component Core Attrition Policy will be usedfor part numbers within the
ECA and ECB Core Acceptability Family (CAF's) because of the application ofthese
products.
The current core return time limit of 180 days in NACD, 240 daysin CAPL and CCL, and
210 days in all other parts of the world including CSARL, CofA, and CACo will beused.
Expired entitlements on cores not returned within the designated time limit willbe attritioned
(cancelled), resulting in the dealerforfeiture of the core deposit made atthe time the engine
was purchased.
The appropriate core attrition date is assigned at the time ofinvoicing. For the purpose of
core entitlement aging, the clock starts on the date the engine is invoiced tothe dealer and
stops on the date the core is reported in transit to Cat by entering a corecredit request (CCR)
into CMIS.
The purpose of the time limit is not to withhold core refunds,but to encourage the return of
cores that are required to support the program.
Any cores returned in excess of entitlements can earn onlydirect purchase price if a direct
purchase program is active at that time. Direct purchase prices are normallysignificantly
less than current core deposit