C13 and C15 On-highway Engines Caterpillar


ARD Combustion Air - Test

Usage:

C13 LEE
System Operation Description:

Table 1 lists the diagnostic codes that relate to the combustion air system.

Table 1
Diagnostic Trouble Codes That Relate to the Combustion Air System 
J1939 Code  Description  Comments 
3487-7  Aftertreatment #1 Air Pressure Control : Not Responding Properly  The boost pressure is okay. The oil pressure is okay. The air pressure control valve is not responding properly to the commands from the ECM.

The code is logged. Engine power is derated 30 percent. Transient regenerations are disabled. Steady state regenerations are allowed. Clean Gas Induction (CGI) is turned off until a regeneration is successfully completed. 
3832-15  Aftertreatment 1 Secondary Air Mass Flow : High - Least Severe (1)  The flow of combustion air is consistently excessive. The code is logged. 
3832-17  Aftertreatment 1 Secondary Air Mass Flow : Low - Least Severe (1)  The flow of combustion air is consistently low.

The code is logged. Transient regenerations are disabled. Steady state regenerations are allowed. 
Follow the troubleshooting procedure in order to identify the root cause of the problem. 

Illustration 1 shows an overview of the troubleshooting procedure. Follow the steps in order.



Illustration 1g01999943


Illustration 2g02000554

Feature on the Caterpillar Electronic Technician (ET) for the Combustion Air System

"Engine Air System Verification Test" - This automated test helps in the troubleshooting of problems with the flow of combustion air. The test is performed while the engine is running. Approximately 2 minutes are required in order for the test to run. Cat ET commands the air pressure control valve to move to various positions during the test. Cat ET measures the value of certain parameters during the test. The test results are displayed on Cat ET. The results must be interpreted in order to determine the troubleshooting that must be performed. Refer to Troubleshooting, "Air System Verification - Test" for additional information on this test.

Test Step 1. Determine The Code

  1. Establish communication between the Caterpillar Electronic Technician (ET) and the engine ECM.

    Note: The communications adapter must be communicating on both data links in order to perform this procedure. Refer to Troubleshooting, "Electronic Service Tools" for additional information, if necessary.

  2. Look for the following codes:

    • 3487-7

    • 3832-15

    • 3832-17

Results:

  • A 3487-7, 3832-15, or 3832-17 code is present. - Proceed to Test Step 2.

  • A 3487-7, 3832-15, or 3832-17 code is not present, but there may be a problem with the ARD. - Proceed to Test Step 2.

Test Step 2. Measure the Differential Pressure Across the Diesel Particulate Filter (DPF)

  1. Measure the differential pressure across the DPF while the engine is at 1400 rpm.

Results:

  • The differential pressure is less than 8.5 kPa (1.2 psi). - Proceed to Test Step 3.

  • The differential pressure is greater than 8.5 kPa (1.2 psi). -

    Repair: Clean the Diesel Particulate Filter. Do not reset the ash model.

    Proceed to Test Step 3.

Test Step 3. Perform the "Engine Air System Verification Test"

  1. Perform the "Engine Air System Verification Test". Refer to Troubleshooting, "Air System Verification Test" for additional information on the test, if necessary.

    Note: Cat ET Air System Verification Test does not determine if the results are acceptable. Acceptable ranges are provided in the Troubleshooting, "Air System Verification Test".

    Note: High backpressure, due to a plugged DPF from not regenerating, will cause erroneous "Engine Air System Verification Test" results.

    Table 2
    Procedures for the Results of the "Engine Air System Verification Test" (1) 
      Test Point 3  Test Point 4  Troubleshooting Procedure 
    "Boost Pressure"  Within the acceptable range  Within the acceptable range  Procedure "A" and Procedure "C"
    If procedures "A" and "C" do not correct the problem, replace the air pressure control valve. 
    "Aftertreatment 1 Secondary Mass Air Flow"  Within the acceptable range  Below minimum 
    "Boost Pressure"  Below minimum  Within the acceptable range  Procedure "B" 
    "Aftertreatment 1 Secondary Mass Air Flow"  Above maximum  Within the acceptable range 
    "Boost Pressure"  Within the acceptable range  Above maximum  Procedure "B" 
    "Aftertreatment 1 Secondary Mass Air Flow"  Within the acceptable range  Below minimum 
    "Boost Pressure"  Within the acceptable range  Within the acceptable range  Procedure "C" 
    "Aftertreatment 1 Secondary Mass Air Flow"  Above maximum  Above maximum 
    "Boost Pressure"  Within the acceptable range  Within the acceptable range  Refer to the "Results" section of this Test Step. 
    "Aftertreatment 1 Secondary Mass Air Flow"  Within the acceptable range  Within the acceptable range 
    "Boost Pressure"  Below minimum  Below minimum  Inspect for intake leaks. Test points one and two will probably be at the minimum or below the minimum.  
    (1) Refer to Troubleshooting, "Air System Verification Test" for the acceptable results for the test.

  2. Refer to Table 2. Determine the appropriate procedure according to the results of the "Engine Air System Verification Test".

    For example, the results of the test indicate the following conditions:

    • The "Boost Pressure" was within the acceptable range during Test Point 3 and Test Point 4.

    • The "Aftertreatment 1 Secondary Mass Air Flow" was above the acceptable range during Test Point 3 and above the acceptable range during Test Point 4.

    In this example, Procedure "C" applies.

Expected Result:

The results are not within the acceptable range. The appropriate procedure was identified.

Results:

  • The results are not within the acceptable range. The appropriate procedure was identified. - Perform the appropriate procedure.

  • The results are within the acceptable range. - Proceed to Test Step 6.

Test Step 4. Procedure "A"



    Illustration 3g01435315
    Inspection points for the line between the air pressure control valve and the venturi
    A typical configuration is shown.

  1. Refer to Illustration 3. Inspect the line between the air pressure control valve and the venturi. Look for these problems: cracked lines and loose hardware. Make the necessary repairs.

  2. Run the "Engine Air System Verification Test" again.

Expected Result:

The results for Test Point 3 and Test Point 4 are within the acceptable range.

Results:

  • The results for Test Point 3 and Test Point 4 are within the acceptable range. - Proceed to Test Step 7.

  • The results for Test Point 3 and Test Point 4 are not within the acceptable range. - Proceed to Test Step 6.

Test Step 5. Procedure "B"

  1. Replace the air pressure control valve.

  2. Run the "Engine Air System Verification Test" again.

Expected Result:

The results for Test Point 3 and Test Point 4 are within the acceptable range.

Results:

  • The results for Test Point 3 and Test Point 4 are within the acceptable range. - Proceed to Test Step 7.

Test Step 6. Procedure "C"

    Note: A small leak in the combustion air system can cause problems. Carefully inspect the combustion air system. Arrows in the illustrations indicate the inspection points.



    Illustration 4g01435018
    Inspection points for the tubing between the venturi and the sensor
    A typical configuration is shown.

  1. Refer to Illustration 4. Carefully inspect the tubing between the venturi and the sensor by using the following procedure:

    1. Remove the flexible hoses. Inspect the flexible hoses. Look for these problems: holes, cuts and other damage.

    2. Verify that all of the worm drive band type clamps are tight.

    3. Verify that all of the line nuts on the venturi are tight.

  2. If no problems are found, remove the differential pressure sensor from the engine.


    Illustration 5g01409818
    Fillets on the hose barb couplers

  3. Refer to Illustration 5. Inspect the fillets at the base of the hose barb couplers. Look for cracks.

    If there are cracks, replace the sensor.

    If there are no cracks, install the sensor.

  4. Verify that the four clamps for the flexible hoses for the differential pressure sensor are tight. The flexible hoses must not slip on the hose barb couplers. The flexible hoses must not slip on the tubing.

  5. Run the "Engine Air System Verification Test" again.

Expected Result:

The results for Test Point 3 and Test Point 4 are within the acceptable range.

Results:

  • The results for Test Point 3 and Test Point 4 are within the acceptable range. - Proceed to Test Step 7.

  • The results for Test Point 3 and Test Point 4 are not within the acceptable range. -

    Repair: Replace the air valve.

    Proceed to Test Step 7.

Test Step 7. Data Log Stationary Regeneration

Refer to Special Instruction, REHS3407, "Using the Caterpillar Electronic Technician (ET) Data Log" for information on using the data log.

  1. Configure the settings on the "General" tab according to the following information:

    Sample Rate - Enter a sample rate of 20 samples per minute.

    Duration - Enter a duration of 1 hour.

  2. The data log must capture the following parameters. Create a group that contains only the following parameters, if necessary.

    • "ARD Inlet Temperature"

    • "ARD Flame Temperature"

    • "ARD Outlet Temperature"

    • "Diesel Particulate Trap #1 Intake Temperature"

    • "Diesel Particulate Trap #1 Outlet Temperature"

    • "Diesel Particulate Trap #1 Differential Pressure"

    • "ARD Pilot Fuel Pressure"

    • "ARD Fuel Pressure"

    • "ARD Fuel Pressure Control Command Percentage"

    • "ARD Air Pressure Control Command Percentage"

    • "ARD Secondary Air Gas Mass Flow"

    • "CGI Mass Flow Rate"

    • "Boost Pressure"

    • "Engine Speed"

  3. Start the data log. Then, begin a stationary regeneration by selecting the following menu items on Cat ET:

    • "Service"

    • "Service Procedures"

    • "Manual Diesel Particulate Filter Regeneration"

    Cat ET will display a "Waiting On Requirements" window. The ECM will automatically elevate the engine speed to 1400 rpm. If the "Waiting On Requirements" window remains displayed for more than 5 minutes, abort the regeneration. Then, select the menu options again in order to start the stationary regeneration.

    The duration of the stationary regeneration depends on the soot load in the DPF. The ECM will automatically return the engine speed to low idle after the stationary regeneration is complete.

    Note: The ECM tests the nozzles for plugging after the stationary regeneration is complete. Approximately 10 minutes are required in order for the test to provide a result. A code will become active if the nozzles are plugged.

  4. Stop the data log after the engine speed returns to idle.

Results:

  • New diagnostic codes are logged. -

    Repair: Troubleshoot the diagnostic codes.

    STOP

  • The regeneration completed successfully. -

    Repair: Interpret the data log in order to determine if the problem has been resolved. Contact your local Caterpillar Technical Communicator for further assistance.

    STOP

Caterpillar Information System:

2014/07/07 A New Digital Return Pinout Is Used on the Wiring Harness of Certain G3500 Engines {1408}
C13 Engine for Combat and Tactical Vehicles Engine Valve Lash - Inspect/Adjust
C9 Generator Set Coolant (ELC) - Change
C9 Generator Set Product Lifting
3306B-XQ200 Rental Generator Set Engine Safety Messages
C9 Generator Set Product Installation
C9 Generator Set Refill Capacities
455-7378 Major Overhaul Foundational Kit for C18 Marine Engines{1000} 455-7378 Major Overhaul Foundational Kit for C18 Marine Engines{1000}
455-7247 Major Overhaul Foundational Kit for C18Marine Engines{1000} 455-7247 Major Overhaul Foundational Kit for C18Marine Engines{1000}
2014/07/07 New Software Is Used on Certain G3520C Generator Set Engines {1901, 1920}
C3.4B Engines for Caterpillar Built Machines Air Inlet and Exhaust System
C3.4B Engines for Caterpillar Built Machines Clean Emissions Module
3512C Marine Auxiliary Generator Set Engines with Dynamic Gas Blending Intake Manifold Air Temperature Is High
2014/10/10 A New Expansion Tank Assembly Is Available as a Service Replacement for Certain 3500 Marine Engines {1354}
2015/03/13 Flushing the Cooling System Before the First Coolant Fill on C8.7 Marine Engines {1350}
2014/07/09 Torque Converter O-Rings No Longer Needed to Seal Passage Between Certain CX48 Input Adapters and Clutch Carriers {3101}
2014/07/11 New Engine Software Is Used on C175-20 Electric Power Generation Engines {1901, 1920}
2014/07/17 Recent Changes to the R134a Refrigerant Air Conditioning Manuals Are Now Available for All Caterpillar Products {0374, 1802, 1805, 1807, 1808, 1809, 7309, 7320, 7322, 7343}
3516B Generator Set Engines with Dynamic Gas Blending Fuel Filter Is Restricted
C3.4B Industrial Engine Engine Oil and Filter - Change
C3.4B Industrial Engine Walk-Around Inspection
C3.4B Industrial Engine Reference Material
C3.4B Industrial Engine After Starting Engine
C3.4B Industrial Engine Engine Operation
Back to top
The names Caterpillar, John Deere, JD, JCB, Hyundai or any other original equipment manufacturers are registered trademarks of the respective original equipment manufacturers. All names, descriptions, numbers and symbols are used for reference purposes only.
CH-Part.com is in no way associated with any of the manufacturers we have listed. All manufacturer's names and descriptions are for reference only.