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Application Engineering Bulletin Subject This AEB is for the following applications: Datalinks and Diagnostics Automotive Industrial Power Generation Date April 2001 Page 1 of 64 AEB Number 15.43 Engine Models included: Fuel Systems included: Introduction The Quantum Diagnostic and Serial Communication Technical Package was written to assist OEMs in integrating Quantum engines into their equipment. This technical package includes the diagnostic codes supported by the Quantum engines as well as the J1587 and J1939 messages supported. Refer to the following other Industrial AEB’s: AEB 15.40 – Electronic Features AEB 15.42 – OEM Components and Interfaces AEB 15.44 – Installation Recommendations Authors: Scott Decker, Michael L. Hill, Brian Landes, Stewart Sullivan, Tiffany Walker

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Page 1: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

ApplicationEngineeringBulletin

Subject This AEB is for the following applications:Datalinks and Diagnostics

Automotive Industrial Power Generation

Date April 2001 Page 1 of 64 AEB Number 15.43

Engine Models included:

Fuel Systems included:

Introduction

The Quantum Diagnostic and Serial Communication Technical Package was written to assist OEMs in integratingQuantum engines into their equipment. This technical package includes the diagnostic codes supported by theQuantum engines as well as the J1587 and J1939 messages supported.

Refer to the following other Industrial AEB’s:

AEB 15.40 – Electronic Features

AEB 15.42 – OEM Components and Interfaces

AEB 15.44 – Installation Recommendations

Authors: Scott Decker, Michael L. Hill, Brian Landes, Stewart Sullivan, Tiffany Walker

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Table of Contents

Introduction .........................................................................................................................................1

Table of Contents.................................................................................................................................2

Section I – Quantum Diagnostics...................................................................................................... 3-5Advanced Diagnostics................................................................................................................... 3-5

Onboard Diagnostics .................................................................................................................... 3-4Offboard Diagnostics .......................................................................................................................5

Section II ECM Serial Communications.................................................................................... 6-39Quantum Serial Communications................................................................................................ 6-35

Introduction .....................................................................................................................................6Applicable SAE Documents........................................................................................................... 6-7Applicable Cummins Documents.......................................................................................................7J1939 Installation Information ........................................................................................................ 7-9

1. Mandatory EA (datalink) options for QSM11 and QSX15..........................................................72. J1939...................................................................................................................................73. Cabling.................................................................................................................................84. Connections..........................................................................................................................85. J1939 Cable and Connector Suppliers ....................................................................................9

J1587 Installation Information ......................................................................................................... 121. Cabling............................................................................................................................... 122. Connections........................................................................................................................ 123. J1587 Cable and Connectors Supplier.................................................................................. 12

Messages Supported on Quantum Modules .................................................................................... 141. Messages Supported on J1939 ....................................................................................... 14-152. PIDS Supported on J1587 ................................................................................................... 32

Network Utilization..................................................................................................................... 36-39J1939 Network Utilization.......................................................................................................... 36-39

Section III – Diagnostics Supported over Quantum Datalinks............................................................ 40Supported Messages and Source Addresses for Clearing Faults................................................... 40Frequently Asked Questions on Cummins Datalinks................................................................. 40-41

Figure 1 – Typical J1939 Topology for On-Highway Applications...................................................... 10

Figure 2 – Typical J1939 Topology for Construction/Agriculture Applications.................................. 11

Figure 3 – Example of J1587 Topology .............................................................................................. 13

Table 1 – Messages Supported on J1939...................................................................................... 16-29

Table 2 – Cummins Specific Information for PGN 65229 (DM4).......................................................... 31

Table 3 – PIDS Supported on J1587 .............................................................................................. 33-36

Table 4 – J1939 Messages N0n-multiplexed – vs- Multiplexed .......................................................... 38

Table 5 – Fault Codes for Quantum Engines................................................................................. 42-64

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Section I – Quantum Diagnostics

Advanced Diagnostics

Advanced diagnostics are included to make Quantum engines straightforward to repair and service. Diagnosticexamination of a fault or maintenance condition can occur through onboard or offboard systems.

Onboard Diagnostics

• Extensive fault detection fault capability within the ECM

• Flash out of fault codes

• Fault lamps located on the cab dash to indicate warning/stop

• Maintenance lamp

Offboard Diagnostics

• INSITE a windows-based PC service tool for Cummins Quantum engines. It is used to help troubleshoot andrepair the Quantum engines. This tool is capable of doing diagnostics and programming.

Onboard Diagnostics

1. Fault Detection

Faults are detected while the key switch is on, during the operation of the machine itself. If a fault becomes active(currently detected) at this time, a fault is logged in memory and a snapshot of engine parameters is logged. Inaddition, certain faults may illuminate the warning lamp (amber) or the stop lamp (red), the maintenance lamp orWIF lamp depending on the severity of the active fault.

2. Flash Out of Fault Codes

Fault flash out mode can be entered through the use of a diagnostic switch or the accelerator pedal. To enter thefault flash out the key switch must be on with the engine not running. When a diagnostic switch is used to enterthe mode, the ECM will automatically flash the first fault code after the switch is turned on. The diagnosticincrement/ decrement is used to sequence forward or backwards through the active faults. To enter fault flash outmode using the accelerator pedal, the pedal must be cycled from 0 to 100% 3 times. Once in diagnostic mode,cycling the accelerator pedal will sequence forward through the active faults. The diagram below depicts thepattern of the fault code flash out scheme as indicated by the stop lamp.

Example Fault Code Sequences

STOPWARNING

STOPWARNING

Maintenance

STOPWARNING

Maintenance

STOPWARNING

Maintenance

STOPWARNING

Maintenance

1 Blink 2 Blinks 4 Blinks 4 Blinks 1 Blink

Fault Code 244: P = Pause

STOPWARNING

Maintenance

STOPWARNING

Maintenance

STOPWARNING

Maintenance

STOPWARNING

Maintenance

STOPWARNING

Maintenance

1 Blink 1 Blink 1 Blink 2 Blinks 1 Blink

Fault Code 112:

P P P P

P P P P

Maintenance

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3. Fault Lamps

The Quantum systems use up to five indicator lamps with one of the lamps serving two functions: the stop lamp,the warning lamp, the maintenance lamp/engine protection lamp (all engine families use one of these lamps, butnot both), wait-to-start lamp, and a water-in-fuel lamp. If the key switch is turned on but the diagnostic switchremains off, the indicator lamps will illuminate for approximately two seconds and then go off, one after the other,to verify they are working and wired correctly. See illustration below where they are all on and then go off one ata time.

Warning Lamp - All Quantum Engines - The warning lamp provides important operator messages. Thesemessages require timely operator attention. The warning lamp is also used to delineate diagnostics fault codes.

Stop Lamp - All Quantum Engines - The stop lamp provides critical operator messages. These messagesrequire immediate and decisive operator response. The stop lamp is also used to flash out diagnostic fault codes.

Wait-to-Start Lamp - QSB/C/L, QSM11, QSX15, QST30 - The wait-to-start lamp indicates that the pre-startintake manifold heater warm-up sequence is active. An OEM-supplied grid heater will automatically heat theintake manifold when needed prior to engine starting. Intake manifold heating improves engine starting in coldtemperatures and reduces white smoke.

Water-in-Fuel (WIF) Lamp - QSB/C/L - The water-in-fuel lamp indicates there is water in the fuel. When thelamp is illuminated the vehicle driver/operator should release the water from the fuel filter.

Maintenance Lamp - QSB/C/L, QSM11, QSX15 - Upon ECM power up the maintenance lamp will flash when itis time to change the oil. It also will illuminate during engine operation when certain lower priority faults arepresent.

Engine Protection Lamp - QSK19/45/60, QST30 - The engine protection lamp will illuminate when an engineprotection fault is present. It is possible, through OEM wiring, to configure the system to use the red/stop lamp forengine protection faults. This is done through wiring the red lamp to both the red/stop lamp input and the engineprotection lamp input on the ECM. If the engine protection lamp signal is being used to control other functionssuch as the vehicle propel circuit, a diode must be inserted in the circuit.

Optional - 2 Lamp Strategy - QSK19/45/60 - The Optional 2-lamp strategy will eliminate the Engine Protection(white) Lamp. Therefore, the operator will only have a warning (yellow) and stop (red) lamp on the dashboard.All of the faults that were mapped to the Engine protection lamp will become annunciated through the stop (red)lamp. This change will only affect the wiring of the fault lamps and not the software or calibration. See wiringbelow.

P = Pause

P

STOPWARNING

STOPWARNING

Maintenance

STOPWARNING

STOP

Fault Lamp Sequence

WARNING

Maintenance Maintenance Maintenance

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Optional 2-Lamp Strategy Wiring

Offboard Diagnostics

INSITE is the windows-based PC service/programming/diagnostic tool for Cummins Quantum engines. It is usedto help troubleshoot and repair the Quantum engines with extended fault diagnostics and processing power.INSITE allows the user to view active and inactive faults and clear the inactive faults. It provides a monitorfunction that allows the service technician to monitor measured parameters, actuator status and some calculatedvalues. It also provides the technician with the capability to turn on certain drivers such as the grid heaters and liftpump as well as running diagnostic tests such as single cylinder cutout. Currently, Insite capability is different pereach Quantum engine. Therefore, the examples mentioned are only applicable to certain engine families.

To VehiclePropel Circuit(when used)

DiagnosticSwitch

To GroundConnectionPower

Engine ECU

Stop Lamp Drive

Warning LampDrive

Engine ProtectionLamp Drive

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Section II – ECM Serial Communications

Quantum Serial Communications

The intent of this document is to provide information pertaining to application of the Quantum controller’s serialcommunications interface to machines. The contents of this document are divided into two broad categories.

The first category caters to OEMs who are involved in building machines; therefore installing datalinks is theirprimary concern. This category provides information on cables, connectors and it lists datalink devices that havebeen tested by Cummins as being compatible with Quantum controllers. The second category capturesinformation to be used by OEMs and component suppliers who design datalink devices that will interface withQuantum controllers. This category has details pertaining to message support, parameter characteristics,network utilization and diagnostics.

Introduction

Datalinks provide the means for electronic devices on the machine to interact with each other. Some typicalfunctions performed are sharing of sensor data, sharing of calculated information, allowing subsystems (e.g.engine, transmission, etc.) to influence each others operation, communication of subsystem operation state.Datalinks also provide a means for on and off board diagnostic work to be done.

The Quantum controllers have been designed with two independent serial communications ports. One portprovides access to SAE J1939 and is J1939-11 compatible, while the other is for SAE J1587 and is compatiblewith J1708. There is no support for SAE J1922 on Quantum controllers.

SAE J1939 datalink is a high-speed network for machines that operate at 250K baud. It is capable of supportingcontrol, information sharing, diagnostics, multiplexing and proprietary communications. The J1939 (physicallayer) datalink uses a differential line driver circuit and allows a maximum bus length of 40 meters. The networkcan have a maximum of 30 node connections at a given time.

SAE J1587 is a J1708 based network that operates at 9600 baud. It supports information sharing, diagnosticsand proprietary communications. The network can have a maximum of 20 node connections at a given time.

Both J1939/J1587 datalinks on Quantum controllers are active when the machine key-switch is turned on.

Applicable SAE Documents

This document, along with the SAE specifications listed below, contain the information required to apply theQuantum datalink interfaces (both J1939 and J1587) to machine applications.

SAE 1939 Recommended Practice for a Serial Control and Communications Network (April1997). Provides a list of all of the J1939-xx documents that are planned. It providesa brief tutorial about the overall set of documents and basic operation of the network.

SAE J1939-11 Physical Layer (March 1997). Operates at 250K bits/sec, linear bus with shieldedtwisted pair cable with a drain.

SAE J1939-12 Physical Layer (Working draft is ISO 11783 Part 2, May 1997). Operates at 250Kbits/sec, linear bus with twisted quad cable

SAE J1939-13 Off-board Diagnostic Connector (January 1997). Specifies 9-pin Deutsch that willprovide a connection to J1939, J1587, a second CAN network for implements,unswitched power and ground.

SAE J1939-21 Data Link Layer (July 1998). Specifies CAN 2.0b as the message protocol to beused. Also defines an interface to the application layer of J1939.

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SAE J1939-71 Vehicle Application Layer (May 1996 plus 1/97 addendum). Defines transmittedparameter value interpretation rules that allow receiving devices to determine if thesending device is able to supply all parameters associated with the parameter group,if any of the parameters has an error condition or if the signal is valid.

SAE J1939-73 Diagnostic Application Layer (October 1998)–Diagnostics. Defines capabilityrequired to perform diagnostics on J1939 strategy to identify the least repairablesubsystem that failed, how it failed, read and clear diagnostics fault codes,communication of diagnostic lamp status and providing a variety of parameters formonitoring by the service tool.

SAE J1939-81 Network Management (November 1996)

SAE J1587 (March 1996 plus 1/97 addendum)–Joint SAE/TMC Electronic Data InterchangeBetween Microcomputer Systems in Heavy Duty Machine Applications. Definesformat of messages and data and guidelines for the frequency and circumstances inwhich messages are transmitted.

SAE J1708 Physical Layer (October 1993)–Serial Data Communications BetweenMicrocomputer Systems in Heavy Duty Machine Applications.

Applicable Cummins Documents

Additional information on the data links can be found in the following Cummins Engineering Standards anddocuments:

Interface Specification: 1377-9804 - J1939 Multiplexing of Inputs and Outputs. Provides the signal processingrequirements for information that will be supplied to/from engine by the J1939 datalink rather than by discretewires (e.g. cruise control switch inputs, lamp outputs etc.).

AEB 15.44 Quantum Installation Recommendations document.

J1939 Installation Information

This section provides information required by those involved in installing J1939 datalinks on their machines.Please refer to AEB 15.44 - Quantum Installation Recommendations for further details.

1. Mandatory EA (datalink) Options for QSM11 and QSX15

There are two required main types of EA options for QSM11 and QSX15 that must be ordered because thedatalink does not ship on either of these engines.

The first option consists of the datalink and backbone being supplied by the OEM as a part of the OEM harness;therefore, the engine will ship without a 9-pin datalink connector. The other option consists of the datalink andbackbone being supplied by Cummins; therefore, it will ship with the datalink connection installed on the engine.

When using the second option the OEM will have a 47-pin Deutsch connector as the interface instead ofconnecting directly to the 50-pin OEM connection on the ECM. This option will include a 9-pin connector, 3-pinconnector, a 50-pin connector and a 47 pin round connector. The 3-pin connector is setup as a termination with a120 ohm terminating resistors supplied. Please refer to AEB 15.44 for wiring this option.

2. J1939

To install J1939 datalink on a machine, it is important to understand the requirements relating to cabling andconnectors. The following section provides details on both. It also provides information on some suppliers toprocure cabling and connectors.

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3. Cabling

Backbone - It is a linear bus with a maximum length of 40 meters (approximately 131 feet). At a given time, themaximum number of nodes (electronic controllers) that can be connected to the backbone is 30. Note that B andB MATE (STYLE 2 Keying) is the backbone and termination connector keying, where B is the receptacle and BMATE is the plug.

For J1939-11 compliance, the backbone is a twisted shielded pair with a drain and requires passive terminationresistors at each end of the network. The J1939-11 topology is typically used for automotive/ on highwayapplications. Please refer to Figure 1.

For J1939-12 compliance, the backbone is a twisted quad and requires an active termination and bias circuit ateach end of the network. This physical layer eliminates the need for shield required in J1939-11. The physicallayer also uses a transceiver circuit design, which allows J1939-11 nodes to exist on the same network as theJ1939-12 nodes.

Stub - The connection from the backbone to each node (electronic controller) is called a stub and it can be amaximum of 1-meter (approximately 3.3 feet) in length. Please refer to Figure 1.

Shield - Electrical connection to the shield is achieved by the drain wire at bus connection points for the nodes(electronic controllers) and at the main bus interconnects. Also note that the shield should be grounded only atone point with a connection to the battery negative. Although the shield does not provide coverage in the areawhere connections are made to the linear bus or at the stub connector (read section below for details) locations, itis connected electrically to the next segment of the shielded cable, and provides sufficient coverage to provide thenecessary electromagnetic compatibility (EMC) improvements.

4. Connections

Engine Connections - The Quantum controller may be connected to the backbone by a 3-pin unshieldedconnector called a stub connector. This is illustrated by the manner in which ECU 1 is connected to the backbonein Figure 1. The stub connector has a special keying (STYLE 1 Keying) and is shown in Figure 1 as A and AMATE, where A MATE is the mating half. For a connection type as shown for ECU 1 in Figure 1, one of the threepins will be used to pass the drain wire through to the mating half (A MATE) of the stub connector, in order toallow the electrical continuity of the shield to be maintained. Two other alternatives for connecting electroniccontrollers to the backbone as supported by SAE J1939 are shown in Figure X. It should be noted that theconnection of ECU 2 provides the best case EMC improvement (i.e. shortest possible stub).

Note: The OEM must supply a J1939 service connection on engine when creating a backbone harness.

Diagnostic Connections - The diagnostic connector is a 9-pin Deutsch and will provide a connection to J1939, asecond CAN network for implements (for Agriculture/Construction Application), unswitched power and ground.The maximum allowed distance of the diagnostic connector from the backbone is two-thirds of 1 meter (0.67meter). The remaining one-third of 1 meter (0.33 meter) is the maximum allowed distance between the diagnosticconnector and the interface circuitry of the tool that is connected to the diagnostic connector.

For the automotive/ truck industry the SAE preferred location of the connector is in the cab area on the operator’sside and should be accessible from the ground on the operator’s side. For a 6-pin installation for J1587 theDeutsch HD10-6-12P connector is recommended. A 9-pin installation for J1939 and J1587 is suggested to usethe Deutsch HD10-9-1939P connector - Please refer to AEB 15.10 section 4.0 for more details.

Bulkhead Connection - The J1939 datalink may be routed through the OEM bulkhead connector. To reduce thechance of electrical noise affecting the datalink, it is recommended that the wires not be placed adjacent tocircuits with extremely high current loads or switching currents. It is recommended that the installer designflyback diodes on all relays to prevent system noise issues.

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5. J1939 Cable and Connector Suppliers

J1939 compatible connectors and cabling are now available through many local and national distributors. Forapplication information and to locate distributors in your area, contact the following companies:

Connectors

Deutsch Industrial Products Division Packard Electric37140 Industrial Avenue P.O. Box 431Hemet, CA 92543 Warren, OH 44486

Phone: (714) 929-1200 1-800-722-5273(909) 765-2250

Fax (714) 652-9784

Deutsch DistributorLadd Industrial Sales1-800-223-1236

Cabling

Belden Wire and Cable Company Champlain Cable Corporation2200 U.S. Highway 27 South 12 Hercules DriveP.O. Box 1980 Colchester, Vermont 05446Richmond, IN 47345 Phone: 1-800-451-5162

Phone: 800-235-3361Fax: (765) 983-5737

BICC Brand-Rex Ltd. Waytec Inc.Viewfield Industrial Estate P. O. Box 690Glenrothes Chanhassen, MN 55317Fife Phone: 800-328-2724KY6 2RS Fax: 800-858-0319Scotland Local: 952-949-0765Phone: +44 (0) 1592 772124Fax: +44 (0) 1592 775314

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Figure 1 Typical J1939 Topology for On-Highway Applications

The points intended to be emphasized:

1). Backbone-twisted shielded pair with a drain wire and a maximum length of 40 meters (approx. 131 ft)It has termination resistors at each end. The figure illustrates a linear topology.

2). Stub – maximum length of 1 meter (approx. 3.3 ft)

3). Four Types of Connectors:i. A- Stub Connector (Receptacle

A MATE: Mating Half of Stub Connector (Plug) STYLE 1 Keying

ii. B: Backbone )through) Connector (Receptacle)

B MATE: Mating Half of Backbone Connector (Plug) STYLE 2 Keying

iii. Diagnostic Connector – Deutsch 9 pin

iv. J1939 backbone passing through the OEM bulkhead connector

4). Three possible ways of connecting ECUs to backbone:i. ECU 1 is connected to backbone via a stub connector (A-A MATE)

ii. ECU 2 has the stub receptacle at the module

iii. ECU n has the stub cable wired directly to the OEM connector

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Figure 2 Typical J1939 Topology for Construction/Agriculture Applications

The points intended to be emphasized:

1). Backbone-twisted quad with a maximum length of 40 m (approx. 131 ft). Both the tractor bus and implementbus is examples of twisted quad backbone. The backbone is both cases have active termination resistors.The figure illustrates a linear topology.

2). Stub – maximum length of 1 meter (approx. 3.3 ft)

3). Three Types of Connectors:i. A and A MATE

ii. Diagnostic Connector

iii. Bulkhead connector

4). Two possible ways shown of connecting ECUs to back bonei. ECU 1 (J1939/11 compatible) is connected to backbone via a stub connector (A-A MATE)

As can be seen J1939/11 compatible cable (3 leads) connects via stub connector to twisted quad.Only the CAN_H and CAN_L wires connect. The power and ground are unterminated.

ii. ECU2 through ECU n are J1939/12 compatible nodes and their connections to backbone are show.

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J1587 Installation Information

This section provides information on cabling and connectors for installing J1708/1587 datalink on a machine.

1. Cabling

Backbone - This terminology does not apply to J1708/J1587. The bus can have a maximum length of 40 meters(approximately 131 feet). At a given time, the maximum number of nodes (electronic controllers) that can beconnected to the bus is 20. The bus is a twisted pair cable. Termination resistors are not needed.

Stub - Not Applicable to J1587

Shield - Not Applicable to J1587

2. Connections

Engine Connections - The J1587 connections to a Quantum module are shown in Figure 1. Please note that theJ1587 interconnect pins for Quantum must be gold. No stub connector is needed to connect an electroniccontroller to the J1587 bus.

Diagnostic Connections - The diagnostic connector to be used is SAE 9-pin Deutsch.

Bulkhead Connection - The J1587 datalink may be routed through the OEM bulkhead connector.

3. J1587 Cable and Connector Supplier

J1587 compatible connectors and cabling are now available through many local and national distributors. Forapplication information and to locate distributors in your area, contact the following companies:

Connectors:

Deutsch Industrial Products Division Packard Electric37140 Industrial Avenue P.O. Box 431Hemet, CA 92543 Warren, OH 44486

Phone: (714) 929-1200 1-800-722-5273(909) 765-2250

Fax (714) 652-9784

Deutsch DistributorLadd Industrial Sales1-800-223-1236

Cabling

Belden Wire and Cable Company Champlain Cable Corporation2200 U.S. Highway 27 South 12 Hercules DriveP.O. Box 1980 Colchester, Vermont 05446Richmond, IN 47345 Phone: 1-800-451-5162

Phone: 800-235-3361Fax: (765) 983-5737

BICC Brand-Rex Ltd.Viewfield Industrial Estate Waytec Inc.Glenrothes - Fife P. O. Box 690KY6 2RS Chanhassen, MN 55317Scotland Phone: 800-328-2724Phone: +44 (0) 1592 772124 Fax: 800-858-0319Fax: +44 (0) 1592 775314 Local: 952-949-0765

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Figure 3 Example of J1587 Topology

The points intended to be emphasized:

1). The J1708/J1587 network topology. As can be seen, it is a free topology vs. being a J1939 linear topology.

2). There are no stubs or a restriction on their length.

ECU 2

ECU 1

ECU n

ECU

ECU n-1

J 1708 bus

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Messages Supported on Quantum Modules

This section details the J1939 and J1587 industry standard messages that are supported by the Quantumcontroller. Parameter characteristics for messages sent on J1939 and J1587 are also listed.

1. Messages Supported on J1939

Cummins has identified six categories of J1939 capability. They are:

• Powertrain Control (PT) - The powertrain control category comprises of parameters exchanged between theengine and devices such as transmission, ASR and ABS.

• Information Sharing (IS) - This category has parameters pertaining to general engine operation. Theseparameters can be broadcast as well as be provided upon request from a remote system, e.g. engine coolanttemperature, engine oil pressure, etc.

• Diagnostics (DG) - This category comprises of parameters that are used to convey fault information, havecapability to command system tests, access test results, clear active and inactive diagnostic trouble codesand access emissions related active diagnostic trouble codes separately from other diagnostic trouble codes(DTCs).

• Multiplexing (MX) - What is Multiplexing - J1939 Multiplexing is sending or receiving of input and outputcontrol commands using J1939 datalink instead of individual hard wires. The enables for multiplexparameters are service trims and can be adjusted with VEPS. The source address from which the parameteris multiplexed is also VEPS trimmable. Please refer to 1377 – 9804 – J1939 Multiplexing of Inputs andOutputs (Interface Specification) for details. All parameters that help accomplish multiplexing fall in thiscategory.

• General (G) - All other nonproprietary J1939 requirements that are not covered in the other 5 categories aregrouped under General. For example: Acknowledgment (ACK/NACK), Transport Protocol.

• Service/Proprietary (SP) - This category comprises J1939 messages that can be used to convey proprietaryinformation, e.g. PGN for Proprietary A.

Table 1 lists all J1939 PGNs and parameters that are supported on all Quantum engine platforms. Please readthe following notes in order to understand the contents of the table.

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Notes to Aid Understanding of Table 1:

Column 1 lists the SAE PGN number.

Column 2 lists the SAE defined PGN names.

Also, SA/DA refers to the Source Address/Destination Address and listing of SAE defined PGN numbers is given.As an example, the combination of PGN 00000–TSC1 and Trans(3)/Engine(0) should be interpreted as TSC1 issourced from the Transmission (J1939 address 3) and received by Engine (J1939 address 0). Also note that anyPGN can be requested by any source with a J1939 address. Where this is not true, the specific addresses havebeen listed.

Some PGNs are not completely defined in SAE J1939-71 and -73. They are denoted with a superscriptedasterisk “*”. Please refer to the notes at the end of the table for details.

Column 3 lists the update rate of the PGN in Quantum

Column 4 indicates which Cummins defined category the parameter falls in.

Please note that there are cases where the parameter may belong to more than one category. For example -Parameter “engine Derate Switch” belongs to both IS/MX. Also read Note 6.

Column 5 lists the parameters within the PGN.

Columns 6-14 describes parameter support for Quantum engines.

TX means that the parameter is transmitted from the engine, RX means that the engine receives the parameter,an entry no means that the parameter is not supported. Support of a J1939 parameter listed as both TX/RX ,means the following:

Under a non-multiplexed case, the parameter value is transmitted (TX) from engine.

Under a multiplexed case, the parameter value is received (RX) by engine.

The broadcast of certain J1939 Parameters shall be dependent upon the override trims for those parameters.These trims can only be changed (enabled/disabled) prior to the powerup sequence. When the overrides havebeen enabled, J1939 Parameters for those System Names shall be broadcast with N/ A (112 for switches & FF16for analog values.)

Note: Multiplexing – if the hardwire is still attached to the ECM for that particular switch/sensor and theparameter is set to be multiplexed, the ECU will ignore the hardwire input.

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AEB15.43Page 16 of 64

Table 1 Messages Supported on J1939

PGNMessage Name

SA/DAUpdate

Rate UseParameters

QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

00000 Torque/Speed Control

Message #1 – TSC1

Trans(3) / Engine(0)

ABS(11) / Engine(0)

ASR(33) / Engine(0)

0.01 s PT

PT

PT

1) Override control mode priority

2) Desired speed control conditions

3) Override control mode

A) Override disabled (00)

B) Speed control (01) a) desired speed b) desired speed control conditions

C) Torque control (10) a) desired torque b) desired speed control conditions

D) Speed/torque limit control (11) a) speed and torque limit b) desired speed control conditions

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) RX a) RX b) RX

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) RX a) RX b) RX

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) RX a) RX b) RX

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) RX a) RX b) RX

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) RX a) RX b) RX

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) seeB,C,D

3) RX

B) RX a) RX b) no

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) seeB,C,D

3) RX

B) RX a) RX b) no

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) seeB,C,D

3) RX

B) RX a) RX b) no

C) RX a) RX b) no

D) RX a) RX b) no

1) RX

2) seeB,C,D

3) RX

B) RX a) RX b) no

C) RX a) RX b) no

D) RX a) RX b) no

00000 Torque/Speed Control

Message #2 – TSC1

Trans(3) / Retarder(41)

ABS(11) / Retarder(41)

ASR(33) / Retarder(41)

0.05 s PT

PT

PT

1) Override control mode priority

2) Desired speed control conditions

3) Override control mode

A) Override disabled (00)

B) Speed control (01) a) desired speed b) desired speed control conditions

C) Torque control (10) a) desired torque b) desired speed control conditions

D) Speed/torque limit control (11) a) speed limit b) torque limit c) desired speed control conditions

1) RX

2) see 3-B, C, D

3) RX

A) no

B) no a) no b) no

C) RX a) RX b) no

D) RX a) no b) RX c) no

1) RX

2) see 3-B, C, D

3) RX

A) no

B) no a) no b) no

C) RX a) RX b) no

D) RX a) no b) RX c) no

1) RX

2) see 3-B, C, D

3) RX

A) no

B) no a) no b) no

C) RX a) RX b) no

D) RX a) no b) RX c) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) no a) no b) no

C) RX a) RX b) no

D) RX a) no b) RX c) no

1) RX

2) see 3-B, C, D

3) RX

A) RX

B) no a) no b) no

C) RX a) RX b) no

D) RX a) no b) RX c) no

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AEB15.43Page 17 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

57088 Stop Start Broadcast AsNeeded

57344 Cab Message #1

Any / Engine(0)

1.0s 1) Requested Percent fan speed 1) RX 1) RX 1) RX 1) RX 1) no 1) RX 1) RX

59392 AcknowledgmentMessage

Engine(0) / Any

AsNeeded

Acknowledgment Message

1) Control Byte (identifies ACK orNACK)

2) Group Function

3) PGN being acknowledged

1) TX

1) no

2) TX

1) TX

2) no

3) TX

1) TX

2) no

3) TX

1) TX

3) TX

1) TX

3) TX

1) TX

2) TX

1) no

2) no

1) TX

2) TX

1) TX

2) TX

59904 Request PGN

Any / Engine(0)

AsNeeded

Request PGN

1) PGN being requested 1) RX 1) RX 1) RX 1) RX 1) RX 1) RX 1) RX 1) RX 1) RX

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AEB15.43Page 18 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

60160 Transport Protocol-Data Transfer

Any/Engine (0)

Any/Retarder (41)

Engine (0)/Any

OnRequest

G Transport Protocol-Data Transfer

2) Sequence Number

3) Packeted Data

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

1) TX/RX

2) TX/RX

60416 Transport Protocol-ConnectionManagement

Any / Engine(0)

Any/Retarder (41)

Engine (0)/Any

AsNeeded

G Transport Protocol Connection Management

1) Control Byte, identifies CM message type

2) Total Message Size, number of bytes

3) Total Number of Packets

4) Parameter Group Number of Packetedmessage

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

1) TX/RX

2) TX/RX

3) TX/RX

4) TX/RX

61184 Proprietary AEngine (0)/Service Tool(249,250)Service Tool(249,250) Engine (0)

AsNeeded

SP Proprietary A

1) Proprietary information, manufacturer specific

1) TX 1) TX 1) TX 1) TX/RX 1) TX/RX 1) TX/RX

61440 ERC 1

Retarder (41)/None

0.1S PT

PT

PT

PT

1) Retarder enable – shift assist switch

2) Retarder enable – brake assist switch

3) Retarder torque mode

4) Actual Retarder – percent torque

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) no

2) TX

3) TX

4) TX

1) no

2) TX

3) TX

4) TX

1) no

2) TX

3) TX

4) TX

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AEB15.43Page 19 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

61441 EBC1

Engine(0) / None

0.1s

IS/MX

IS/MX

IS/MX

IS/MX

1) ABS Active

2) ASR Brake Control Active

3) ASR Engine Control Active

4) Brake Pedal position

5) ASR Hill Holder Switch

6) ASR Offroad Switch

7) ABS Offroad Switch

8) Remote Accelerator Enable Switch

9) Shutdown Switch

10) Switched Torque

11) Multi Unit Sync On/Off Switch

12) Engine Retarder Selection

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) TX/RX

9) RX

10) no

11) TX/RX

12) TX/RX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) TX/RX

9) RX

10) no

11) TX/RX

12) TX/RX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) TX/RX

9) RX

10) no

11) TX/RX

12) TX/RX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) TX

9) no

10) TX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) TX

11) no

12) TX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) RX

9)

10)

11) no

12) no

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) no

9) no

10) no

11) no

12) no

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) RX

9) no

10) no

11) no

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) RX

9) no

10) no

11) no

61442 TransmissionMessage #1 – ETC1

Trans(3)/Engine(0)

0.01s PT

PT

PT

PT

1) Shift in process

2) Torque converter lockup engaged(If converter lockup is sensed, EngBrakes will not engage. If transmissionis automated send a zero(0))

3) Driveline engaged

4) Output shaft speed

5) Percent clutch slip

6) Progressive shift disable

7) Momentary engine overspeed enable

8) Input shaft speed

9) Source address of Controlling Device

1) RX

2) no

3) RX

4) RX

5) no

6) RX

7) RX

8) no

1) RX

2) RX

3) RX

4) RX

5) no

6) RX

7) RX

8) no

1) RX

2) RX

3) RX

4) RX

5) no

6) RX

7) RX

8) no

1) RX

2) RX

3) RX

4) RX

5) no

6) RX

7) RX

8) no

1) RX

2) RX

3) RX

4) RX

5) no

6) RX

7) RX

8) No

9) no

1) RX

2) RX

3) RX

4) RX

5) no

6) RX

7) RX

8) no

1) RX

2) no

3) RX

4) no

5) no

6) RX

7) RX

8) no

9) no

1) RX

2) no

3) RX

4) no

5) no

6) no

7) RX

8) no

1) RX

2) no

3) Rx

4) no

5) no

6) no

7) RX

8) no

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AEB15.43Page 20 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

61443 EEC2 - ElectronicEngine Controller #2

Engine(0) / None

0.05 s PT

PT/MX

PT/MX

PT

PT/MX

1) AP kick down switch

2) AP low idle switch

3) Accelerator pedal position

4) Percent load at current speed

5) Remote Accelerator

1) TX

2) TX/RX

3) TX/RX

4) TX

5) TX/RX

1) TX

2) TX/RX

3) TX/RX

4) TX

5) TX/RX

1) TX

2) TX/RX

3) TX/RX

4) TX

5) TX/RX

1) TX

2) TX/RX

3) TX/RX

4) TX

5) TX/RX

1) TX

2) TX/RX

3) TX/RX

4) TX

5) TX/RX

1) no

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

5) no

1) no

2) TX

3) TX

4) TX

1) no

2) TX

3) TX

4) TX

61444 EEC1 - ElectronicEngine Controller #1

Engine(0) / None

0.02 s PT

PT

PT

PT

1) Engine torque mode

2) Drivers demand engine-percent torque

3) Actual engine - percent torque

4) Engine speed

5) Source Address of Controlling Device

1) TX

2) TX

3) TX

4) TX

5) no

1) TX

2) TX

3) TX

4) TX

5) no

1) TX

2) TX

3) TX

4) TX

5) no

1) TX (1)

2) TX/RX

3) TX/RX

4) TX

5) no

1) TX (1)

2) TX/RX

3) TX/RX

4) TX

5) no

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

5) no

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

65213 Fan Drive

Engine(0) / None

1.0 s IS

IS

1) Estimated Percent Fan Speed

2) Fan Drive State

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) no

2) no

1) no

2) no

1) TX

2) TX

1) no

2) no

1) TX

2) TX

1) TX

2) TX

65226 DM1

Active DiagnosticTrouble Codes

Engine(0) / None

1.0 s

DG(MX)

DG(MX)

DG(MX)

DG(MX)

DG(MX)

Active Diagnostic Trouble Codes

1) Malfunction indicator lamp status

2) Red Stop Lamp status

3) Amber Warning Lamp status

4) Protect lamp status

5) Diagnostic Trouble Code (s)

1) no

2) TX

3) TX

4) TX

5) TX

1) no

2) TX

3) TX

4) TX

5) TX

1) no

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

(1) not all modes specified by SAE are supported

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AEB15.43Page 21 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65227 DM2

Any / Engine(0)

OnRequest

DG

DG

DG

DG

DG

Previously Active Diagnostic TroubleCodes

1) Malfunction indicator lamp status

2) Red Stop Lamp status

3) Amber Warning Lamp status

4) Protect lamp status

5) Diagnostic Trouble Code (s)

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

1) TX

2) TX

3) TX

4) TX

5) TX

65228 DM3

Any / Engine(0)

OnRequest

DG Diagnostic Data Clear/Reset ofPreviously Active DTCs

RX RX RX RX RX RX RX RX RX

65229 DM4 *

Engine(0) / None

OnRequest

Freeze Frame Parameters

1) Freeze Frame Length

2) Diagnostic Trouble Code

3) Engine Torque Mode

4) Boost

5) Engine Speed

6) Engine Percent Load

7) Engine Coolant Temperature

Vehicle Speed

9) Manufacturer Specific Information

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) TX

9) no

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) TX

9) no

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) TX

9) no

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

1) TX

2) TX

3) no

4) TX

5) TX

6) TX

7) TX

8) no

9) TX

* See page 30 – Notes on superscripted PGN

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AEB15.43Page 22 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65230 DM5

Engine(0) / None

OnRequest

DG

DG

DG

DG

DG

DG

Diagnostic Readiness

1) Active Trouble Codes

2) Previously Active Diagnostic TroubleCodes

3) OBD Compliance

4) Continuously Monitored SystemsStatus

5) Non-Continuously Monitored SystemsSupport

6) Non-Continuously Monitored SystemsStatus

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

65232 DM8

Engine(0) / None

OnRequest

DG

Test Results for Non-ContinuouslyMonitored Systems

1) Test Identifier

2) Test Type / Component Identifier

3) Test Value

4) Test Limit Maximum

5) Test Limit Minimum

1) TX

2) no

3) TX

4) no

5) no

1) TX

2) no

3) TX

4) no

5) no

1) TX

2) no

3) TX

4) no

5) no

1) TX

2) no

3) TX

4) no

5) no

65234 DM10

Engine(0) / None

OnRequest

DG

Non-Continuously Monitored SystemsTest ID Support

1) Test ID 1) TX 1) TX 1) TX 1) TX 1) TX 1) TX

65243 Engine FluidLevel/Pressure #2

Engine(0) / None

0.5 IS

IS

1) Injection control pressure

2) Injector rail metering pressure

1) no

2) no

1) no

2) no

1) no

2) no

1) no

2) TX

1) no

2) no

1) no

2) TX

1) no

2) TX

65244 Idle Operation

Engine(0) / None

OnRequest

IS

IS

1) Total idle fuel used

2) Total idle hours

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

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AEB15.43Page 23 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65247 EEC3

Engine(0) / None

0.25 s PT

PT

PT

1) Nominal friction - percent torque

2) Engine's desired operating speed

3)Engine's operating speed asymmetryadjustment

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

65248 Vehicle Distance

Engine(0) / None

PGN

OnRequest

IS

IS

1) Trip distance

2) Total vehicle distance

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) no

2) no

1) no

2) no

1) TX

2) TX

65249 RetarderConfiguration

Retarder(41) / None

5.0 s PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PTPT

PT

1) Retarder location

2) Retarder type

3) Retarder control method

4) Retarder speed at idle, point 1

5) Percent torque at idle, point 1

6) Maximum retarder speed, point 2

7) Percent torque at max speed,point 2

8) Retarder speed at point 3

9) Percent torque at point 3

10) Retarder speed at point 4

11) Percent torque at point 4

12) Retarder speed at peak torque, point 5

13) Reference retarder torque

14) Percent torque at peak torque, point 5

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) TX

13) TX

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) TX

13) TX

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) TX

13) TX

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

13) TX

13) TX

14) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) TX

13) TX

14) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) TX

13) TX

14) no

Page 24: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 24 of 64

Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65251 Engine Configuration

Engine(0) / None

5.0s/10%chg

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

PT

1) Engine speed at idle, point 1

2) Percent torque at idle, point 1

3) Engine speed at point 2

4) Percent torque at point 2

5) Engine speed at point 3

6) Percent torque at point 3

7) Engine speed at point 4

8) Percent torque at point 4

9) Engine speed at point 5

10) Percent torque at point 5

11) Engine speed at high idle, point 6

12) Gain (KP) of endspeed governor

13) Reference engine torque

14) Maximum momentary engineoverride speed, point 7

15) Maximum momentary engineoverride time limit

16) Requested speed control range lowerlimit

17) Requested speed control rangeupper limit

18) Requested torque control rangelower limit

19) Requested torque control rangeupper limit

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

7) TX

8) TX

9) TX

10) TX

11) TX

12) no

13) TX

14) TX

15) TX

16) TX

17) TX

18) TX

19) TX

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Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65252 Idle Shutdown

Engine(0) / None

1.0 s IS

IS

IS

IS

IS

IS/MX

1) Idle shutdown timer state

2) Idle shutdown timer override

3) Driver alert mode

4) Engine has shutdown by system

5) Idle shutdown timer function

6) Refrigerant high pressure switch

7) Refrigerant low pressure switch

8) A/C high pressure fan switch

9) Wait to start lamp

10) Engine protection shutdown timerstate

11) Engine protection shutdown override

12) Engine shutdown approaching

13) Engine has shutdown by protectionsystem

14) Engine protection timer systemconfiguration

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) TX

9) TX

10) no

11) no

12) no

13) no

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) TX

9) TX

10) no

11) no

12) no

13) no

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) TX

9) TX

10) no

11) no

12) no

13) no

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) TX/RX

9) no

10) TX

11) no

12) TX

13) TX

14) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) TX/RX

9) no

10) TX

11) no

12) TX

13) TX

14) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) no

9) no

10) TX

11) TX

12) TX

13) TX

14) TX

1) TX

2) no

3) no

4) no

5) no

6) no

7) no

8) no

9) no

10) no

11) no

12) no

13) no

14) no

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) no

9) no

10) TX

11) TX

12) TX

13) TX

14) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) no

7) no

8) no

9) no

10) TX

11) TX

12) TX

13) TX

14) TX

65253 Engine Hours,Revolutions

Engine(0) / None

OnRequest

IS

IS

1) Total engine hours

2) Total engine revolutions

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

1) TX

2) no

65254 Time/Date

Engine(0) / None

On Request

IS

IS

IS

IS

IS

IS

1) Seconds

2) Minutes

3) Hours

4) Day

5) Month

6) Year

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) TX

2) TX

3) TX

4) TX

5) TX

6) TX

1) no

2) no

3) no

4) no

5) no

6) no

1) no

2) no

3) no

4) no

5) no

6) no

1) no

2) no

3) no

4) no

5) no

6) no

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Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65255 Vehicle Hours

Engine(0) / None

OnRequest

IS

IS

1) Total vehicle hours

2) Total power takeoff hours

1) no

2) TX

1) no

2) TX

1) no

2) TX

1) no

2) TX

1) no

2) TX

1) no

2) no

65257 Fuel Consumption

Engine(0) / None

OnRequest

IS

IS

1) Trip fuel

2) Total fuel used

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

1) TX

2) TX

65259 ComponentIdentification

*

Engine(0) / None

OnRequest

IS

IS

IS

IS

1) Make

2) Model

3) Serial Number

4) Unit Number

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) no

1) TX

2) TX

3) TX

4) TX

1) TX

2) TX

3) TX

4) TX

65260 Vehicle Identification

*

PGN

On Request

IS 1) VIN 1) TX 1) TX 1) TX 1) TX 1) TX 1) TX

65261 CruiseControl/VehicleSpeed Setup

Engine(0) / None

OnRequest

IS

IS

IS

1) Maximum vehicle speed limit

2) Cruise control high set limit speed

3) Cruise control low set limit speed

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) no

2) no

3) no

65262 Engine Temperature

Engine(0) / None

1.0 s IS 1) Engine coolant temperature

2) Fuel temperature

3) Engine oil temperature

4) Turbo oil temperature

5) Engine intercooler temperature

1) TX

2) TX

3) no

4) no

5) no

1) TX

2) TX

3) no

4) no

5) no

1) TX

2) TX

3) no

4) no

5) no

1) TX

2) TX

3) TX

4) no

5) no

1) TX

2) no

3) TX

4) no

5) no

1) TX

2) TX

3) no

4) no

5) no

1) TX

2) no

3) TX

4) no

5) no

1) TX

2) TX

3) no

4) no

5) no

1) TX

2) TX

3) no

4) no

5) no

* See page 30 – Notes on superscripted PGN

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Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65263 Engine FluidLevel/Pressure

Engine(0) / None

0.5 s

IS

1) Fuel delivery pressure

2) Engine oil level

3) Engine oil pressure

4) Crankcase pressure

5) Coolant pressure

6) Coolant level

1) no

2) no

3) TX

4) no

5) no

6) no

1) no

2) no

3) TX

4) no

5) no

6) no

1) no

2) no

3) TX

4) no

5) no

6) no

1) no

2) no

3) TX

4) no

5) no

6) no

1) no

2) no

3) TX

4) no

5) no

6) no

1) no

2) no

3) TX

4) TX

5) TX

6) no

1) no

2) no

3) TX

4) TX

5) TX

6) no

1) no

2) no

3) TX

4) TX

5) TX

6) no

1) no

2) no

3) TX

4) TX

5) TX

6) no

65264 PTO - PowerTakeoff Information

Engine(0) / None

0.1 s

IS

IS/MX

IS/MX

IS/MX

IS/MX

1) Power Takeoff Oil Temperature

2) Power Takeoff Speed

3) Power Takeoff Set Speed

4) Remote PTO variable speed controlswitch

5) AUX Governor On/Off Switch

6) PTO enable switch

7) PTO accelerate switch

8) PTO resume switch

9) PTO coast/decelerate switch

10) PTO set switch

1) no

2) no

3) TX

4) no

5) no

6) TX/RX

7) no

8) TX/RX

9) no

10)TX/RX

1) no

2) no

3) TX

4) no

5) no

6) TX/RX

7) no

8) TX/RX

9) no

10)TX/RX

1) no

2) no

3) TX

4) no

5) no

6) TX/RX

7) no

8) TX/RX

9) no

10)TX/RX

1) no

2) no

3) TX

4) TX

5) no

6) TX

7) TX

8) TX

9) no

10)TX

1) no

2) no

3) TX

4) TX

5) no

6) TX

7) TX

8) TX

9) no

10)TX

1) no

2) no

3) TX

4) no

5) TX/RX

6) no

7) no

8) TX/RX

9) no

10)TX/RX

1) no

2) no

3) TX

4) no

5) no

6) no

7) no

8) no

9) no

10)no

1) no

2) no

3) TX

4) no

5) TX/RX

6) no

7) no

8) TX/RX

9) no

10)TX/RX

1) no

2) no

3) TX

4) no

5) TX/RX

6) no

7) no

8) TX/RX

9) no

10)TX/RX

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Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65265 CruiseControl/VehicleSpeed

Engine(0) / None

0.1 s

IS

IS/MX

IS/MX

IS/MX

IS

IS

IS/MX

IS

IS/MX

IS

IS

IS

IS/MX

IS/MX

IS/MX

1) Parking Brake Switch

2) ISC 1 Switch

3) Wheel Base Vehicle Speed

4) Clutch Switch

5) Brake Switch

6) Cruise Control Enable Switch

7) Cruise Control Active

8) Cruise Control Accelerate Switch

9) Cruise Control Resume Switch

10) Cruise Control Coast Switch

11) Cruise Control Set Switch

12) Cruise Control Set Speed

13) Cruise Control State

14) PTO State

15) Engine Test Mode Switch

16) Idle Decrement Switch

17) Idle Increment Switch

1) no

2) no

3) TX

4) TX/RX

5) TX/RX

6) TX/RX

7) TX

8) TX

9) TX/RX

10) TX

11)TX/RX

12) TX

13) TX

14) TX

15)TX/RX

16)TX/RX

17)TX/RX

1) no

2) no

3) TX

4) TX/RX

5) TX/RX

6) TX/RX

7) TX

8) TX

9) TX/RX

10) TX

11)TX/RX

12) TX

13) TX

14) TX

15)TX/RX

16)TX/RX

17)TX/RX

1) no

2) no

3) TX

4) TX/RX

5) TX/RX

6) TX/RX

7) TX

8) TX

9) TX/RX

10) TX

11)TX/RX

12) TX

13) TX

14) TX

15)TX/RX

16)TX/RX

17)TX/RX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) no

9) no

10) no

11)no

12) no

13) no

14) TX

15) TX

16) TX

17) TX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) no

9) no

10) no

11)no

12) no

13) no

14) TX

15) TX

16) TX

17) TX

1) no

2) no

3) no

4) no

5) no

6) no

7) no

8) no

9) no

10) no

11)no

12) no

13) no

14) no

15) no

16) no

17) no

65266 Fuel Economy

Engine(0) / None

0.1 s IS

IS

IS

1) Fuel Rate

2) Instantaneous fuel economy

3) Average fuel economy

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) TX

3) TX

1) TX

2) no

3) no

1) TX

2) no

3) no

1) TX

2) TX

3) no

1) TX

2) TX

3) TX

1) TX

2) TX

3) no

1) TX

2) TX

3) no

65269 Ambient Conditions

Engine(0) / None

1.0 s 1) Barometric pressure

2) Cab interior temperature

3) Ambient air temperature

4) Air inlet temperature

5) Road surface temperature

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

1) TX

2) no

3) no

4) no

5) no

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Table 1 Messages Supported on J1939

PGN Message NameSA/DA

UpdateRate

Use Parameters QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

65270 Inlet/ExhaustConditions

Engine(0) / None

0.5 s

IS

IS

1) Particulate trap inlet pressure

2) Boost pressure

3) Intake manifold temperature

4) Air inlet pressure

5) Air filter differential pressure

6) Exhaust gas temperature

7) Coolant filter differential

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

1) no

2) TX

3) TX

4) no

5) no

6) no

7) no

65271 Vehicle ElectricalPower

Engine(0) / None

1.0 s

IS

1) Net battery current

2) Alternator current

3) Alternator potential (voltage)

4) Electrical potential (voltage)

5) Battery potential (voltage), switched

1) no

2) no

3) no

4) TX

5) no

1) no

2) no

3) no

4) TX

5) no

1) no

2) no

3) no

4) TX

5) no

1) no

2) no

3) no

4) TX (2)

5) no

1) no

2) no

3) no

4) TX (2)

5) no

1) no

2) no

3) no

4) TX

5) no

1) no

2) no

3) no

4) no

5) TX

1) no

2) no

3) no

4) TX

5) no

1) no

2) no

3) no

4) TX

5) no

65279 Water in FuelIndicator

Engine(0) / None

10.0 s IS 1) Water in fuel indicator 1) TX 1) TX 1) TX 1) no 1) no 1) no

(2) Available by request only

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AEB15.43Page 30 of 64

Notes on Superscripted PGN* used in Table 1:

1. The SAE J1939 specification does not contain all the information on PGNs 65229, 65259 and 65260.

2. Only able to reset the Engine Oil.

3. Nonconforming to J1939/21 SAE Specification.

4. Nonconforming to J1939/71 SAE Specification.

5. The Request PGN is actually received with the DM3 PGN in the data field.

6. When cruise control/PTO set or resume switches are used to activate coast or accelerate switches, the setor resume switches will no longer activate during a broadcast while the resume or accelerate switches areactive.

Cummins has provided the following detailed definitions:

PGN 65229 - Diagnostic Message DM4

A freeze frame is defined as the list of recorded parameters at the time a diagnostic trouble code was captured.The freeze frame record for each diagnostic trouble code contains the SAE defined required parameters firstand then any manufacturer-specific information.

Byte 1: Freeze Frame LengthBytes 2-5: Diagnostic Trouble Code (4 bytes)Byte 6: Engine Torque Mode set to FF16 - not availableByte 7: BoostBytes 8-9: Engine SpeedByte 10: Engine % LoadByte 11: Engine Coolant TemperatureBytes 12-13: Vehicle SpeedBytes 14-74: Manufacturer Specific Information - Please refer to Table 2

Note: The following illustrates the message format for when there is more than one freeze frame.

Given: a = freeze frame length

b = required parameters

c = manufacturer specific freeze frame information

Message form will be as follows: a,b,c,a,b,c,a,b,c,.etc. The transport protocol of J1939-21 will have to be usedto send freeze frames because they are more than 8 data bytes. The maximum message size limit is 1785bytes.

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Table 2 Cummins Specific Information for PGN 65229 (DM4)

Cummins InternalParameter Description

Length(bytes)

Information istransmitted as:

ECM_Run_Time The ECM time that a fault occurred inseconds

4

Fault_index Index for service fault information 2

Road_Speed The speed of the vehicle 2

Filtered_Engine_Speed The speed of the engine 2

J1587_Percent_Load Fuel as a percentile 2

Commanded_Throttle Throttle position as a percentile 2

Engine_State Defined state of engine operation 2

Fueling_Control_State Indicator of which algorithm is in control offinal fueling

2

Final_Fueling Fueling value commanded to Fuel System 2

Final_Timing_State Indicator of which algorithm is in control offinal timing

2

Final_Timing Calculated timing value as start of injection 2

Boost_Pressure Boost pressure in psig 2

Coolant_Temperature Coolant temperature in degrees Fahrenheit 2

Intake_Manifold_Temperature

Intake Manifold temperature in degreesFahrenheit

2

Oil_Temperature Oil temperature in degrees Fahrenheit 2 FFFF

Oil_Pressure Oil pressure in psig 2

System_Switch_Status Sensor and switch status indicators 2

System_Switch_Status_2 Sensor and switch status indicators 2

Engine_Run_Time Engine time that fault occurred in seconds.This does not include any base time set for anew ECM

4

Battery_Voltage Battery voltage in volts 2

Injected_Fueling Fueling value delivered by Fuel System 2 FFFF

Fuel_Rail_Pressure Measured fuel pressure in psia 2 FFFF

Coolant_Pressure Coolant pressure in psia 2 FFFF

Fuel_Error_Front_Metered_Fuel_ Error

Calculated fueling error of the front bank inunits of mm3/stk

4 FFFF

Fuel_Error_Rear_Metered_Fuel_ Error

Calculated fueling error of the rear bank inunits of mm3/stk

4 FFFF

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AEB15.43Page 32 of 64

PGN 65259 — Component Identification

Data length Variable (transport layer used)

The following parameters are mapped to this message:

Engine Make 5 bytes

Asterisk (*) 1 byte

Engine Model 34 bytes

Asterisk (*) 1 byte

Engine SN 8bytes

Asterisk (*) 1 byte

Unit Number 20 bytes

Asterisk (*) 1 byte

Note: Each parameter shall be followed by an ASCII asterisk (*). That is, the engine Make is the first elementof this message and the asterisk following Unit Number is the last. If a build does not support one of theseparameters, the following asterisk will still be used.

PGN 65260 — Vehicle Identification (VIN)

Data length Variable (transport layer used)Byte 1-n VIN

Byte n+1 Asterisk (ascii “*”)

Note: The actual data length of this message shall be determined by the number of characters in the VIN(represented by “n” in this example).

2. PIDS Supported on J1587

J1587 datalink supports information sharing, diagnostics and proprietary communications on Quantum. Themessages used to accomplish that are listed below in table. Please read the following notes in order tounderstand the contents of the table.

Notes to Aid Understanding of Table 3:

Column 1 lists the SAE defined Parameter Identification (PID) numbers

Column 2 lists the SAE defined PID names.

Column 3 lists the Update rate for the PID on Quantum. As Needed refers to the message being usedwhenever the desire is to use it. For example, PID 000 (Request Parameter) will be used by a tool only when itwishes to request some information from the Quantum. Some update rates have the number (5) written afterthem. Please refer to the notes at the end of the table for details.

Columns 4-12 lists support of the PIDs on the Quantum engine platforms. Some PIDs have numbers (1)–(5)written after them. Please refer to the notes at the end of the table for details.

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Table 3 PIDS Supported on J1587

PID J1587 Message Name Update Rate QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

000 Request Parameter As Needed RX RX RX RX RX RX RX RX RX

002 Status Word 1 1.0 s TX (1) TX (1) TX (1) TX (1) TX (1) TX (1) TX (1) TX (1) TX (1)

003 Diagnostic Status As Needed no no no TX (1) TX (1) TX (1) TX (1) TX (1) TX (1)

029 Percent Accelerator Position #2 0.1 s TX TX TX

030 Crankcase Blowby Pressure (when available) 1.0 s TX TX TX

044 Attention/Warning Indicator Lamps Status 1.0 s TX TX TX TX TX

051 Throttle Position (Rack Position) 0.2 s TX

071 Idle Shutdown Timer Status 1.0 s TX TX TX TX TX

074 Maximum Road Speed On Request TX TX TX

083 Road Speed Limit Status On Request TX TX TX

084 Road Speed 0.1 s TX TX TX

085 Cruise Control Status 0.2 s TX TX TX

086 Cruise Control Set Speed 10.0 s TX TX TX

087 Cruise Control High Set Limit Speed On Request TX TX TX

088 Cruise Control Low Set Limit Speed On Request TX TX TX

089 Power Takeoff Status 1.0 s TX TX TX TX TX TX TX TX TX

091 Percent Accelerator Pedal Position 0.1 s TX TX TX TX TX TX TX TX TX

092 Percent Engine Load 0.1 s TX TX TX TX TX TX TX TX TX

097 Water In Fuel Indicator 10.0 s TX TX

100 Engine Oil Pressure 1.0 s TX TX TX TX TX TX TX TX TX

101 Crankcase Pressure (when available) 1.0 s TX

102 Boost Pressure 1.0 s TX TX TX TX TX TX TX TX TX

105 Intake Manifold Temperature 1.0 s TX TX TX TX TX TX TX TX TX

108 Barometric Pressure 1.0 s TX TX TX TX TX TX

109 Coolant Pressure 10 s TX TX TX TX

110 Engine Coolant Temperature 1.0 s TX TX TX TX TX TX TX TX TX

111 Coolant Level 10.0 s TX

121 Engine Retarder Status 0.2 s no no no TX TX

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Table 3 PIDS Supported on J1587

PID J1587 Message Name Update Rate QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

128 Component Specific Parameter Request As Needed RX RX RX RX RX RX RX RX

133 Average Fuel Rate 0.2 s TX TX TX

135 Electronic Fuel Pump Pressure 1.0 s TX TX TX

156 Injector Timing Rail Pressure On Request TX TX TX

157 Injector Metering Rail Pressure On Request TX TX TX

166 Rated Engine Power On Request TX TX TX TX TX TX

168 Volts (Battery) 1.0 s TX TX TX TX TX TX TX TX TX

174 Fuel Temperature On Request no TX TX

175 Engine Oil Temperature 1.0 s TX TX TX

182 Trip Fuel 10.0 s TX TX TX TX TX

183 Fuel Rate 0.2 s TX TX TX TX TX TX TX TX

184 Instantaneous MPG 0.2 s TX TX TX

185 Average MPG 10.0 s TX TX TX

187 Power Takeoff (ISC) Set Speed On Request TX TX TX TX TX TX TX TX TX

188 Idle Engine Speed On Request TX TX TX TX TX TX TX TX TX

189 Maximum Engine Speed On Request TX TX TX TX TX TX TX TX TX

190 Engine Speed 0.1 s TX TX TX TX TX TX TX TX TX

191 Transmission Output Shaft Speed 0.1 s TX TX TX

192 Multisection Parameter As Needed TX TX TX TX TX TX TX TX TX

193 Transmitter System Diagnostic Table On Request TX (1,3) TX (1,3) TX (1,3) TX (1,3) TX (1,3) TX (1,3) TX (1,3) TX (1,3) TX (1,3)

194 Transmitter System Diagnostic Code andOccurrence Count Table

1.0 s TX (2,4) TX (2,4) TX (2,4) TX (2,4) TX (2,4) TX (2,4) TX (2,4) TX (2,4) TX (2,4)

195 Diagnostic Data Request/Clear Count As Needed RX RX RX RX RX RX RX RX RX

196 Diagnostic Data Request/Clear Count Response As Needed TX TX TX TX TX TX TX TX TX

234 Software Identification On Request TX (5) TX (5) TX (5) TX (5) TX (5)

235 Total Idle Hours On Request TX TX TX TX

236 Total Idle Fuel Used On Request TX TX TX

237 Vehicle Identification Number On Request TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5)

243 Component Identification Parameter On Request TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5) TX (5)

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Table 3 PIDS Supported on J1587

PID J1587 Message Name Update Rate QSB QSC QSL9 QSM11 QSX15 QSK19 QST30 QSK45 QSK60

244 Trip Distance 10.0 s TX TX TX

245 Total Vehicle Distance 10.0 s TX TX TX

247 Total Engine Hours On Request TX TX TX TX TX TX (*) TX TX TX

248 Total PTO Hours On Request TX TX TX TX TX TX

250 Total Fuel Used On Request TX TX TX TX TX

251 Clock On Request no no no TX TX

252 Date On Request no no no TX TX

254 Escape On Request no no no TX/RX TX/RX

(*) Not in software phase 2.7

Notes on numbers (1) – (5) used in Table:

1. These PIDs are specified as broadcast PIDs in SAE J1587 but due to limitation in the number of broadcast PIDs that can be supported in theQuantum calibration, they are instead available On Request

2. Cummins PID 194 messages include occurrence count when requested. When PID 194 is broadcast, the fault count information is not included.

3. PID 194 should be used for new products. Refer to Table 7-1 for system fault codes.

4. Active faults are broadcast at the rates specified in the SAE J1587 specification (7/96). Inactive faults are only available on request.

5. The SAE J1587 specification does not contain all the information on PIDs 234, 237 and 243. Cummins has provided the following detailed definitions:

PID 234 - Software Identification

Format: PID Data

234 n a a a a * b b b b * c c c c c c c c c c c c*dddd*ee*ff

n - Number of parameter data characters following this byte

a - Module Part Number, 8 bytes, ASCII

b - Module Serial Number, 8 bytes, ASCII

c - Engine Calibration Date and Time Stamp, 12 bytes, ASCII(format = mmddyyhhmmss)

d - Phase Designation (describes software version number), 4 bytes, ASCII

e- Module Identifier, 2 bytes, ASCII

f - Application Identifier, 2 bytes, ASCII

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PID 237 — Vehicle Identification

Format: PID Data

n a a a a a a a a a a a a a a a a a a a a

n - Number of parameter data characters (20)

a - VIN (alphanumeric)

Note: The stored Vehicle Identification Number is a twenty-byte value.

PID 243 - Component Identification

Format: PID Data

43 n b c c c c c * d d d d d d d d d d d d d d d d d* e e e e

n - Number of parameter data characters following this byte

b - MID of component being identified (Cummins uses MID 128)

c - Engine Make, 5 bytes, ASCII (Cummins stores and transmits “CMMNS”)

d - Engine Model, 17 bytes, ASCII

e - Engine Serial Number, 8 bytes, ASCII

Network Utilization

Network utilization is a limited resource, as the network can become saturated by excessive use. Thefollowing sections detail network utilization computations for J1939 and J1587 datalinks on Quantumcontrollers.

J1939 Network Utilization

The engine module’s contribution to percent bus utilization may be calculated for J1939 broadcast databy dividing the network transmission time by the repetition frame time. Computation of Bus Utilization hasbeen done both for Nonmultiplexed and Multiplexed cases. When computing J1939 traffic over a timeslice for Nonmultiplexed case, only the Quantum broadcast messages are taken in consideration. Theremay be message traffic from other J1939 devices that the engine module receives but the engine wouldcontinue to function with no degradation if it were not to receive these messages. Therefore thecontribution of the engine module towards bus loading is because of the messages it broadcasts.

In a multiplexed case though, the engine module depends on receiving parameters from the CabElectronic Control Unit (ECU). Therefore, bus loading is not only due to messages that the enginemodule broadcasts but also the traffic contributed by the multiplexed messages from Cab ECU.

Following assumptions have been made for doing the calculation:

• The engine configuration has not changed over time of calculation.

• No active system faults are present.

• No collisions take place.

• Calculated over 2-second time slice

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The equation for calculating bus utilization for J1939 per 2 seconds is provided below:

U = bus utilization = (B*N)/2...................................... (A)

where:

B = number of J1939 messages

N = number of microseconds to send a single J1939 message frame = (128 bits per message) * (4microseconds per bit) = 512 microsecond per message

Table below details the message traffic on J1939 datalink contributed by Quantum for the two possiblecases - nonmultiplexed and multiplexed. Please read the notes below to understand the contents of thetable.

Notes to Aid Understanding of Table 4:

Column 1 lists the SAE defined Parameter Group Number (PGN)

Column 2 lists the periodic rate at which the PGN is updated on Quantum

Column 3 lists the # of PGN frames Quantum broadcasts in a Nonmultiplexed case

Column 4 lists the # of PGN frames Quantum either broadcasts or receives in a multiplexed case.Please refer to the write- up in Section 0 of J1939 Network Utilization to understand why the messageframe calculations are done differently for nonmultiplexed vs. multiplexed cases.

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Table 4 J1939 Messages Non-multiplexed -vs- Multiplexed

PGN Update Rate Non-multiplexed Multiplexed

57344 - Cab Message #1 1.0 s 0 2

61440 - ERC1 0.1 s 20 20

61441 - EBC1 0.1 s 20 40

61443 - EEC2 0.05 s 40 80

61444 - EEC1 0.02 s 100 100

65213 - Fan Drive 1.0 s 2 2

65247 - EEC3 0.25 s 8 8

65249 - Retarder Configuration 5.0 s 1.6 1.6

65251 - Engine Configuration 5.0 s 2 2

65252 - Idle Shutdown 1.0 s 2 4

65262 - Engine Temperature 1.0 s 2 2

65263 - Engine Fluid Level/Pressure 0.5 s 4 4

65264 - Power Takeoff Information 0.1 s 20 40

65265 - Cruise Control/Vehicle Speed 0.1 s 20 40

65266 - Fuel Economy 0.1 s 20 20

65269 - Ambient Conditions 1.0 s 2 2

65270 - Inlet/Exhaust Conditions 0.5 s 4 4

65271 - Vehicle Electrical Power 1.0 s 2 2

65279 - Water In Fuel Indicator 10.0 s 0.2 0.2

B = TOTAL # of messages in 2 sec 269.8 373.8

Therefore Network Utilization for Nonmultiplexed Messages in 2 seconds, per equation (A):

U NonMUX = 269.8 frames * 512 microseconds * sec * 100 2 sec frame 106 microseconds

U NonMUX = 6.90%

and Network Utilization for Multiplexed Messages in 2 seconds, per equation (A):

UMUX = 373.8 frames * 512 microseconds * sec * 100 2 sec frame 106 microseconds

UMUX = 9.56%

J1587 Network Utilization

For the J1587 ECM broadcast, the network utilization is calculated as follows:

U = bus utilization = B/N

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where:

N = baud rate/number of bits per character

= 9600/10 = 960

RA = access bytes + MID byte = 3.0 (assumes two tries, winning half the time)

C# = number of collisions.

This number is dependent on the number of units on the bus with equal priority, the size of the messageand the total number of messages to be transmitted on the bus.

Ct = collision bytes = re-access bytes * number of collisions = RA * C#B = number of bytes broadcasted per second

= B1 + B2 + B3 + CtB1 = bytes for access *maximum broadcast rate

= 2 * 10

Note: 20 bits (two transmission bytes) are approximately equal to the access time plus the priority time.This assumes only one packet per broadcast.

B2 = bytes for overhead of each packet * maximum broadcast rate

= 2 * 10 (overhead is the MID and checksum)

B3 = total number of bytes broadcasted (byte count * update frequency * number of PIDs rate)

Therefore, Network Utilization for J1587 broadcast data is as follows:

B3 = number of message bits (assume one active fault)

B3 = 2*10*3 + 3*10*1 + 2*5*2 + 3*5*1 + 2*1*9 + 3*1*3 + 5*1*1 + 2*0.1*3 + 3*0.1*3 + 5*0.1*2 +3*5*1 + 2*10*1

= 60 + 30 + 20 + 15 + 18 + 9 + 5 +.6 +.9 + 1 + 15 + 20

= 194.5

B2 = packet overhead

= 2*10 + 2*1 = normal packet frequency + 2nd packet frequency

= 22

B1 = access overhead

= 1.7*10 = 17

Ct = collision bytes

= 3 (assuming one collision per second)

Network Utilization = (B1 + B2 + B3 + Ct)/960

= (194.5 + 22 + 17 + 3)/960= 236.5/960 = 0.246

Network Utilization = 24.6%

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Section III - Diagnostics Supported over Quantum Datalinks

The intent of this section is to discuss Quantum diagnostics that can be performed using standardmessages on J1939 and J1587 datalinks.

Supported Messages and Source Addresses for Clearing Faults

This section describes the J1939/J1587 messages that will be used by datalink devices to clear faults onQuantum controllers. The intent is to allow clearing of faults on Quantum only by authorized sourceaddresses.

To clear faults on Quantum via J1939, the PGN 65,228 — Diagnostics Message #3 (DM3 - DiagnosticData Clear/Reset of Previously Active DTCs) can be used by a device making the request. Currentlythere is no source address restriction from which this PGN will be accepted. This will change in futurerevisions of Quantum product. All diagnostic information pertaining to previously active DTCs will beerased when this PGN is received by Quantum controllers. Upon completion of this operation, a PositiveAcknowledgment will be sent using J1939-21 PGN 59392. If the operation is not completed, a NegativeAcknowledgment using PGN 59392 will be sent.

When clearing faults on Quantum via J1587, PID 195 — Diagnostic Data Request/Clear Count can beused. For a list of authorized MIDs please refer to Table . When the bits 8-7 of diagnostic code character(please refer to J1587 specification for details of PID 195) are set to 00, then the CUMMINS 3 digit faultcode representing the PID or SID will be sent as a 3 digit ASCII character in PID 196 format. If therequested PID/SID does not exist as an active/inactive fault, Quantum will respond with number ofparameter data characters “n” in PID 196 (please refer to J1587 specification for details of PID 196) set tozero. For bits 8-7, the functions of states 01 and 11 as defined by SAE Recommended Practice are notsupported. When bits 8-7 are set to 10, then only the inactive faults will be cleared. The Quantumacknowledges an authorized PID 195 request with a PID 196.

Table 5 J1939/J1587 Messages for Clearing Faults

PGN PID Parameter DescriptionAuthorized

Addresses/ MIDs

J1939 65,228 NA DM3 - Diagnostic Data Clear/Resetof Previously Active DTCs

Any except those usedby Quantum

J1587 NA 195 Diagnostic Data/Request ClearCount

141,154, 172, 180, 182

Quantum Diagnostic Information

Please refer to page XX for a tabulation of all faults logged on Quantum engine platforms - (see ?????).The corresponding Cummins service description, applicable SPN/FMI and/ or PIDs/SIDs/FMI informationis captured. The associated lamp action for the fault is also given. The Quantum diagnostics for bothJ1939 and J1587 datalinks is also included.

Frequently Asked Questions on Cummins Datalinks

Question # 1 What is the impact on Quantum controllers of not receiving parameters it supports?

Answer: Cummins datalink message support can be divided in two categories to discuss thepossible impact on Quantum controllers of not receiving parameters it supports from other sourceaddresses - i). Powertrain messages and ii). Multiplexed Messages. The details are discussed below:

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i). Impact of not receiving Powertrain Messages - In such a scenario the Quantum controller will functionby reverting to safe defaults and respond only to the operator requested torque and speed values.

ii). Impact of not receiving Multiplexed Messages - If the Quantum has been configured to receivemultiplexed messages and it does not receive them, then a configuration error will be logged in Quantumand calibrated safe defaults values for such messages will be used by Quantum.

Question #2 How to Ensure Cummins Compatibility with New Datalink Devices?

Answer: Cummins is constantly working with OEMs and datalink device suppliers to ensure fullcompatibility of all devices with our engines. When developing a new device that will interact with ourengine via the J1587 or J1939 datalinks, it is strongly recommended that you contact either your OEMapplication engineer.

Note: Contacting Customer Engineering early in the design process provides a greater chancefor success in integrating a new device with Quantum controllers in the machine system.

Areas where Quantum Differs from Intent of SAE Recommended Practice

The implementation of the some PGNs/PIDs on Quantum differs from the intent of J1939/J1587. Whereneeded, the difference will be removed in future revisions of the product. The list of specific PGNs/ PIDsand their shift from J1939/J1587 intent is captured below:

• PGN 57344 (Cab Message #1) — Quantum does not broadcast this message currently. It is ONLYreceived from other source addresses.

• The Request-PGN 59904 is NOT supported by Engine Retarder.

• In PGN 65247 (EEC3), the two parameters: i). Engine’s desired operating speed; and ii). Enginesoperating speed asymmetry adjustment are calibrated (static) values.

• A request for PGN with data bytes greater than 8 causes a BAM and not RTS/CTS sequence asspecified by J1939-21.

• Progressive Shift Algorithm is not supported on Quantum, therefore enabling/disabling parameter -Progressive Shift Disable in message ETC1, will have NO effect.

• PIDs 4, 97 and 187 are supported as On Request on Quantum controllers, whereas the SAE J1587specification specifies their update rates to be periodic.

Note: Please be advised that if the PGN is a regular broadcast then the request for it may not behonored because of ECM memory limitations. Please further be advised that SAE recommendedpractices say do not ask for something that is regularly broadcast.

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Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

FAULTCODE/LAMP

SID(S)PID(P)

FMI

SPNFMI DESCRIPTION

QS

B

QS

C

QS

L9

QS

M11

QS

X15

QS

K19

QS

T30

QS

K45

QS

K60

111

Red

S254

12

629

12

Engine Control Module – Criticalinternal failure

X X X X X X X X X

112

Red

S020

7

635

7

Engine Timing Actuator is notresponding to ECM commands

X X X

113

Yellow

S020

3

635

3

Engine Timing Actuator Circuit -shorted high

X X X X

114

Yellow

S020

4

635

4

Engine Timing Actuator Circuit -shorted low

X

115

Red

P190

2

190

2

Engine Speed/Position Sensor Circuit -lost both of two signals from themagnetic pickup sensor

X X X X X X X X X

116

Red

P156

3

156

3

Fuel Timing Pressure Sensor Circuit -shorted high

X X X X X

117

Red

P156

4

156

4

Fuel Timing Pressure Sensor Circuit -shorted low

X X X X X

118

Yellow

P135

3

135

3

Fuel Pump Delivery Pressure SensorCircuit - shorted high

X X X X X

119

Yellow

P135

4

135

4

Fuel Pump Delivery Pressure SensorCircuit - shorted low

X X X X X

121

Yellow

P190

10

190

10

Engine Speed/Position Sensor Circuit -lost one of two signals from themagnetic pickup sensor

X X X X X X X X

122

Yellow

P102

3

102

3

Intake Manifold Pressure Sensor #1Circuit - shorted high

X X X X X X X X X

123

Yellow

P102

4

102

4

Intake Manifold Pressure Sensor #1Circuit - shorted low

X X X X X X X X X

124*

Yellow

102

16

High Intake Manifold Pressure LeftBank

X X X

125*

None

102

18

Low Intake Manifold Pressure LeftBank

X X X

126*

Yellow

1129

16

High Intake Manifold Pressure RightBank

X X X

127*

None

1129

18

Low Intake Manifold Pressure RightBank

X X X

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Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

128*

None

1129

3

Right Bank Intake Manifold PressureSensor Circuit Failed High

X X X

129*

None

1129

4

Right Bank Intake Manifold PressureSensor Circuit Failed Low

X X X

131

Red

P091

3

091

3

Accelerator Pedal Position SensorCircuit - shorted high

X X X X X X X X X

132

Red

P091

4

091

4

Accelerator Pedal Position SensorCircuit - shorted low

X X X X X X X X X

133

Red

P029

3

974

3

Remote Accelerator Pedal PositionSensor Circuit - shorted high

X X X X X X

133

Red

P029

3

29

3

Remote Accelerator Pedal PositionSensor Circuit - shorted high

X X X

134

Red

P029

4

974

4

Remote Accelerator Pedal PositionSensor Circuit - shorted low

X X X X X X

134

Red

P029

4

29

4

Remote Accelerator Pedal PositionSensor Circuit - shorted low

X X X

135

Yellow

P100

3

100

3

Engine Oil Pressure Sensor Circuit -shorted high

X X X X X X X X X

136*

None

1208

3

Pre Filter Oil Pressure Sensor CircuitFailed High

X X X

137*

None

1208

4

Pre Filter Oil Pressure Sensor CircuitFailed Low

X X X

141

Yellow

P100

4

100

4

Engine Oil Pressure Sensor Circuit -shorted low

X X X X X X X X X

143

Yellow

P100

1

100

18

Engine Oil Pressure Low - Warning X X X X X X

143

White

P100

1

100

1

Engine Oil Pressure Low - Warning X X X

144

Yellow

P110

3

110

3

Engine Coolant Temperature SensorCircuit - shorted high

X X X X X X X X X

145

Yellow

P110

4

110

4

Engine Coolant Temperature SensorCircuit - shorted low

X X X X X X X X X

146

Yellow

P110

0

110

16

Engine Coolant Temperature High -Warning

X X X

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Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

147

Red

P091

8

091

8

Accelerator Pedal Position SensorCircuit - low frequency

X X X X X X X X X

148

Red

P091

8

091

8

Accelerator Pedal Position SensorCircuit - high frequency

X X X X X X X X X

151

Red

P110

0

110

0

Engine Coolant Temperature High –Critical

X X X X X X

151

White

P110

0

110

0

Engine Coolant Temperature High –Critical

X X X

153

Yellow

P105

3

105

3

Intake Manifold Temperature Sensor#1 Circuit - shorted high

X X X X X X X X X

154

Yellow

P105

4

105

4

Intake Manifold Temperature Sensor#1 Circuit - shorted low

X X X X X X X X X

155

Red

P105

0

105

0

Intake Manifold Temperature #1 High -Critical

X X X X X X

155

White

P105

0

105

0

Intake Manifold Temperature #1 High -Critical

X X X

156*

Yellow

1131

3

Left Bank Rear Intake ManifoldTemperature Sensor Circuit FailedHigh

X X

157*

Yellow

1131

4

Left Bank Rear Intake ManifoldTemperature Sensor Circuit Failed Low

X X

158*

White

1131

0

High Intake Manifold Temperature -Left Bank Rear

X X

159*

Yellow

1132

3

Right Bank Front Intake ManifoldTemperature Sensor Circuit FailedHigh

X X

161*

Yellow

1132

4

Right Bank Front Intake ManifoldTemperature Sensor Circuit Failed Low

X X

162*

White

1132

0

High Intake Manifold Temperature -Right Bank Front

X X

163*

Yellow

1133

3

Right Bank Rear Intake ManifoldTemperature Sensor Circuit FailedHigh

X X

164*

Yellow

1133

4

Right Bank Rear Intake ManifoldTemperature Sensor Circuit Failed Low

X X

165*

White

1133

0

High Intake Manifold Temperature -Right Bank Rear

X X

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Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

166

Yellow

S024

3

733

3

Rack Position Sensor #1 Circuit -shorted high

X

172

Red

S023

6

638

6

Rack Actuator Position #1 Circuit -grounded circuit

X

173

Yellow

S023

7

638

7

Rack Actuator - mechanically stuckopen

X

184

Yellow

S233

2

609

2

Engine Control Module IdentificationInput State Error

X X X X

185

Yellow

S231

2

639

2

Engine Control Module NetworkCommunication Error

X

187

Yellow

S232

4

620

4

Sensor Supply Voltage #2 Circuit -shorted low

X X

211

None

S216

11

1484

31

Additional OEM/Vehicle DiagnosticCodes have been logged. Check otherECM's for DTC's.

X X

211*

None

613

14

OEM Component Failure X X X

212

Yellow

P175

3

175

3

Engine Oil Temperature Sensor Circuit- shorted high

X X X

212*

Yellow

175

3

Engine Oil Temperature Sensor Circuit- shorted high

X X

213

Yellow

P175

4

175

4

Engine Oil Temperature Sensor Circuit- shorted low

X X X

213*

Yellow

175

4

Engine Oil Temperature Sensor Circuit- shorted low

X X

214

Red

P175

0

175

0

Engine Oil Temperature High - Critical X X

214*

White

175

0

Engine Oil Temperature High - Critical X X

219

Maint.

P17

1

1380

17

Low Oil Level in the Centinel makeupoil tank

X X

219

White

P17

1

1380

1

Low Oil Level in the Centinel makeupoil tank

X X X

221

Yellow

P108

3

108

3

Ambient Air Pressure Sensor Circuit –shorted high

X X X X X X X X

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AEB15.43Page 46 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

222

Yellow

P108

4

108

4

Ambient Air Pressure Sensor Circuit –shorted low

X X X X X X X X

223

Yellow

S085

4

1265

4

Engine Oil Burn Valve Solenoid Circuit– shorted low

X X X X X

225

Yellow

S086

4

1266

4

Engine Oil Replacement ValveSolenoid Circuit - shorted low

X X X

227

Yellow

S232

3

620

3

Sensor Supply Voltage #2 Circuit -shorted high

X X

231

Yellow

P109

3

109

3

Engine Coolant Pressure SensorCircuit - shorted high

X X X X

232

Yellow

P109

4

109

4

Engine Coolant Pressure SensorCircuit - shorted low

X X X X

233

Yellow

P109

1

109

18

Engine Coolant Pressure Low -Warning

X

233

White

P109

1

109

1

Engine Coolant Pressure Low -Warning

X X X

234

Red

P190

0

190

0

Engine Speed High - Cricital X X X X X X X X X

235

Red

P111

1

111

1

Engine Coolant Level Low - Critical X X X X X X

235

White

P111

1

111

1

Engine Coolant Level Low - Critical X X X

237

Yellow

S030

2

644

2

External Speed Input (Multiple UnitSychronization) - data incorrect

X X X X

241

Yellow

P084

2

084

2

Vehicle Speed Sensor Circuit - dataincorrect

X X X X X

242

Yellow

P084

10

084

10

Vehicle Speed Sensor Circuit -tampering has been detected

X X X X X

243

Yellow

P121

4

513

4

Engine Brake Driver #1 Circuit -shorted low

X X X

245

Yellow

S033

4

647

4

Fan Clutch Circuit - shorted low X X X X X

252

Yellow

P098

2

098

2

Engine Oil Level #1 Sensor Circuit -data incorrect

X X X

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AEB15.43Page 47 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

253

White

P098

1

098

1

Engine Oil Level #1 Low - Critical X X X

254

Red

S017

4

632

4

Fuel Shutoff Valve Circuit - shorted low X X X

254

None

S017

4

632

4

Fuel Shutoff Valve Circuit - shorted low X X X

255

Yellow

S017

3

632

3

Fuel Shutoff Valve Circuit - shortedhigh

X X

259

Red

S017

7

632

7

Fuel Shutoff Valve - stuck open X X X X X

261

Yellow

P174

0

174

16

Fuel Temperature High - Warning X

261

White

P174

0

174

0

Fuel Temperature High - Warning X X X

263

Yellow

P174

3

174

3

Fuel Temperature Sensor Circuit -shorted high

X X X X X

264

Yellow

P174

11

174

11

Fuel Temperature Sensor Circuit - dataout-of-range

X

265

Yellow

P174

4

174

4

Fuel Temperature Sensor Circuit -shorted low

X X X X X

268

Yellow

P094

2

94

2

Fuel Pressure Sensor Circuit - dataincorrect

X X

271

Yellow

S126

4

1347

4

High Fuel Pressure Solenoid Valve #1Circuit - shorted low

X X

272

Yellow

S126

3

1347

3

High Fuel Pressure Solenoid Valve #1Circuit - shorted high

X X

273

Yellow

S127

4

1348

4

High Fuel Pressure Solenoid Valve #2Circuit - shorted low

X X

274

Yellow

S127

3

1348

3

High Fuel Pressure Solenoid Valve #2Circuit - shorted high

X X

275

Yellow

S126

7

1347

7

Fuel Pumping Element #1 (Front) -mechanically stuck

X X

276

Yellow

S018

3

633

3

Fuel Injection Control Valve Circuit -shorted high

X X

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AEB15.43Page 48 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

277

Yellow

S018

7

633

7

Fuel Injection Control Valve -mechanically stuck

X X

278

Yellow

P073

11

1075

11

Fuel Priming Pump Control Circuit -shorted high/low

X X X

279

Yellow

S018

4

633

4

Fuel Injection Control Valve Circuit -shorted low

X X

281

Yellow

S126

7

1347

7

High Fuel Pressure Solenoid Valve #1- mechanically stuck

X X

282

Yellow

S127

7

1348

7

High Fuel Pressure Solenoid Valve #2- mechanically stuck

X X

283

Yellow

S221

3

1043

3

Engine Speed/Position Sensor #1(Crankshaft) Supply Voltage Circuit -shorted high

X X X

284

Yellow

S221

4

1043

4

Engine Speed/Position Sensor #1(Crankshaft) Supply Voltage Circuit -shorted low

X X X X

285

Yellow

S231

9

639

9

SAE J1939 Multiplexing PGN TimeoutError

X X X X X

286

Yellow

S231

13

639

13

SAE J1939 Multiplexing ConfigurationError

X X X X X

287

Red

P091

2

91

19

SAE J1939 Multiplexing AcceleratorPedal Sensor System Error

X X X X X

288

Red

P029

2

974

19

SAE J1939 Multiplexing RemoteThrottle Data Error

X X X X X

292

White

P223

14

1083

14

Auxiliary Temperature Sensor Input # 1Engine Protection - Critical

X X X

293

Yellow

S441

3

441

3

Auxiliary Temperature Sensor Input # 1Circuit – shorted high

293

Yellow

P223

3

1083

3

Auxiliary Temperature Sensor Input # 1Circuit – shorted high

X X X

293

Yellow

S154

3

1083

3

Auxiliary Temperature Sensor Input # 1Circuit – shorted high

X X

294

Yellow

S441

4

441

4

Auxiliary Temperature Sensor Input # 1Circuit – shorted low

294

Yellow

P223

4

1083

4

Auxiliary Temperature Sensor Input # 1Circuit – shorted low

X X X

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AEB15.43Page 49 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

294

Yellow

S154

4

1083

4

Auxiliary Temperature Sensor Input # 1Circuit – shorted low

X X

295

Yellow

P108

2

108

2

Ambient Air Pressure Sensor Circuit -data incorrect

X X

296

Red

P223

14

1387

14

Auxiliary Pressure Sensor Input # 2Engine Protection - Critical

X X X

296

White

P223

14

1084

14

Auxiliary Pressure Sensor Input # 2Engine Protection - Critical

X X X

297

Yellow

P223

3

1387

3

Auxiliary Pressure Sensor Input # 2Circuit – shorted high

X X X

297

Yellow

P223

3

1084

3

Auxiliary Pressure Sensor Input # 2Circuit – shorted high

X X X X X

298

Yellow

P223

4

1387

4

Auxiliary Pressure Sensor Input # 2Circuit – shorted low

X X X

298

Yellow

P223

4

1084

4

Auxiliary Pressure Sensor Input # 2Circuit – shorted low

X X X X X

299

None

S117

14

1384

31

Engine Shutdown Commanded byJ1939

X X X

299

Yellow

S117

11

1384

31

Engine Shutdown Commanded byJ1939

X X

311

Yellow

S001

6

651

6

Injector Solenoid Valve Cylinder #1Circuit – grounded circuit

X X

312

Yellow

S005

6

655

6

Injector Solenoid Valve Cylinder #5Circuit – grounded circuit

X X

313

Yellow

S003

6

653

6

Injector Solenoid Valve Cylinder #3Circuit – grounded circuit

X X

314

Yellow

S006

6

656

6

Injector Solenoid Valve Cylinder #6Circuit - grounded circuit

X X

315

Yellow

S002

6

652

6

Injector Solenoid Valve Cylinder #2Circuit – grounded circuit

X X

316

Yellow

S078

3

931

3

Fuel Supply Pump Actuator Circuit -shorted high

X X X

318

Yellow

S078

7

931

7

Fuel Supply Pump Actuator –mechanically stuck

X X X

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AEB15.43Page 50 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

319

Maint.

P251

2

251

2

Real Time Clock - Power Interrupt X X X X X

321

Yellow

S004

6

654

6

Injector Solenoid Valve Cylinder #4Circuit - grounded circuit

X

322

Yellow

S001

5

651

5

Injector Solenoid Valve Cylinder #1Circuit - open circuit

X

323

Yellow

S005

5

655

5

Injector Solenoid Valve Cylinder #5Circuit – open circuit

X

324

Yellow

S003

5

653

5

Injector Solenoid Valve Cylinder #3Circuit – open circuit

X

325

Yellow

S006

5

656

5

Injector Solenoid Valve Cylinder #6Circuit – open circuit

X

328

Yellow

S152

7

1348

7

Fuel Pumping Element #2 (Rear) -mechanically stuck

X X

329

Yellow

S233

14

1077

14

Fuel System Leakage error X X

331

Yellow

S002

5

652

5

Injector Solenoid Valve Cylinder #2Circuit – open circuit

X

332

Yellow

S004

5

654

5

Injector Solenoid Valve Cylinder #4Circuit – open circuit

X

341

Yellow

S253

2

630

2

Engine Control Module – data lost X X

342

Red

S253

13

630

13

Engine Control Module – out ofcalibration

X

343

Yellow

S254

12

629

12

Engine Control Module - Warninginternal hardware failure

X X X X X X

346

Yellow

S253

12

630

12

Engine Control Module - WarningSoftware error

X X X X X X

349

Yellow

P191

0

191

16

Transmission Output Shaft (Tailshaft)Speed High – Warning

X X X X X

349

Yellow

P191

0

191

0

Transmission Output Shaft (Tailshaft)Speed High – Warning

X X X

352

Yellow

S232

4

1079

4

Sensor Supply Voltage #1 Circuit -shorted low

X X X X X

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AEB15.43Page 51 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

361

Red

S251

3

1076

3

Fuel Pump Control Module, FuelControl Valve Circuit - shorted high

X

362

Yellow

S251

4

1076

4

Fuel Pump Control Module, FuelControl Valve Circuit - shorted low

X

363

Yellow

S251

7

1076

7

Fuel Pump Control Module, FuelControl Valve - mechanically stuck

X

364

Yellow

S233

9

1077

9

Fuel Pump Control Module, CANCommunication Error - abnormalupdate rate

X

365

Yellow

S233

4

1077

4

Fuel Pump Control Module, SupplyVoltage Circuit - shorted low

X

366

Yellow

S233

2

1077

2

Fuel Pump Control Module, SupplyVoltage Circuit - data incorrect

X

367

Yellow

P190

11

1078

11

Fuel Pump Control Module, IncrementAngle Time Sensor Error

X

368

Yellow

S254

8

1078

8

Fuel Pump Control Module, TimingError

X

369

Yellow

P190

2

1078

2

Fuel Pump Control Module, EngineSynchronization Error

X

372

Yellow

S233

11

1077

11

Fuel Pump Control Module, IdleValidation Error

X

373

Red

S233

3

1077

3

Fuel Pump Control Module, FuelShutoff Error

X

374

Yellow

S233

12

1077

12

Fuel Pump Control Module, Self-TestError

X

375Yellow

S254

2

629

2

Fuel Pump Control Module, ElectronicCalibration Code Error

X

376

Yellow

S233

13

1077

13

Fuel Pump Control Module, Fueling orEngine Speed Mismatch

X

377

Yellow

S233

7

1077

7

Fuel Pump Control Module, StuckRelay Error

X

378

Yellow

S018

5

633

5

Fueling Actuator #1 Circuit - opencircuit

X

379

Yellow

S018

6

633

6

Fueling Actuator #1 Circuit - groundedcircuit

X

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AEB15.43Page 52 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

381

Yellow

S237

11

626

11

Intake Air Heater (Relay Enable) #1Circuit - data incorrect

X X X

382

Yellow

S237

11

626

11

Intake Air Heater (Relay Enable) #2Circuit - data incorrect

X X X

384

Yellow

S237

11

626

11

Start Assist Device Control CircuitError (Ether Injection)

X X X

385

Yellow

S232

3

620

3

OEM Sensor Supply Voltage Circuit -shorted high

X X X

386

Yellow

S232

3

1079

3

Sensor Supply Voltage #1 Circuit -shorted high

X X X X X

387

Yellow

S221

3

1043

3

Accelerator Pedal Position SensorSupply Voltage Circuit - shorted high

X X X X X

389

Yellow

S033

11

647

11

Fan Clutch Circuit Error X X X

391

Yellow

S017

11

632

11

Fuel Shutoff Valve Supply Voltageerror

X

394

Yellow

S020

5

635

5

Timing Actuator #1 Circuit - opencircuit

X

395

Yellow

S020

6

635

6

Timing Actuator #1 Circuit - groundedcircuit

X

396

Yellow

S083

5

1244

5

Fueling Actuator #2 Circuit - opencircuit

X

397

Yellow

S083

6

1244

6

Fueling Actuator #2 Circuit - groundedcircuit

X

398

Yellow

S084

5

1245

5

Timing Actuator #2 Circuit - opencircuit

X

399

Yellow

S084

6

1245

6

Timing Actuator #2 Circuit - groundedcircuit

X

414*

Yellow

S250

9

608

9

Data Communication error over theJ1587 data link Circuit

X

415

Red

P100

1

100

1

Engine Oil Pressure Low – Critical X X X X X X

415

White

P100

1

100

1

Engine Oil Pressure Low – Critical X X X

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AEB15.43Page 53 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

418

WIF /Maint.

P097

0

097

15

Water in Fuel Indicator High –Maintenance

X X X X X X

419

Yellow

1319

2

Intake Manifold Boost PressureImbalance

X

422

Yellow

P111

2

111

2

Engine Coolant Level Sensor Circuit -data incorrect

X X X X X X X X X

423

Yellow

P156

2

156

2

Fuel Timing Pressure or TimingActuator Stuck

X X X X

426

None

S231

2

639

2

SAE J1939 datalink - cannot transmit X X

426

Yellow

S231

2

639

2

SAE J1939 datalink - cannot transmit X X X

426*

None

639

2

SAE J1939 datalink - cannot transmit X X X

427

None

S231 639

9

SAE J1939 not fast enough X X X

428

Yellow

P097

3

97

3

Water in Fuel Sensor Circuit - shortedhigh

X X X

429

Yellow

P097

4

097

4

Water in Fuel Sensor Circuit - shortedlow

X X X X X X

431

Yellow

S230

2

558

2

Accelerator Pedal Idle ValidationCircuit - data incorrect

X X X X X X

431

Yellow

P091

2

91

2

Accelerator Pedal Idle ValidationCircuit - data incorrect

X X X

432

Red

S230

13

558

13

Accelerator Pedal Idle ValidationCircuit - out of calibration

X X X X X X

432

Red

P091

13

91

13

Accelerator Pedal Idle ValidationCircuit - out of calibration

X X X

433

Yellow

P102

2

102

2

Intake Manifold Pressure SensorCircuit - data incorrect

X X X X X

434

Yellow

S251

2

627

2

Power Lost without Ignition Off X X X X X

435

Yellow

P100

2

100

2

Engine Oil Pressure Sensor Circuit -data incorrect

X X

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AEB15.43Page 54 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

441

Yellow

P168

1

168

18

Battery #1 Voltage Low - Warning X X X X X X

441

None

P168

1

168

1

Battery #1 Voltage Low - Warning X X X

442

Yellow

P168

0

168

16

Battery #1 Voltage High - Warning X X X X X X

442

Yellow

P168

0

168

0

Battery #1 Voltage High - Warning X X X

443

Yellow

S221

4

1043

4

Accelerator Pedal Position SensorSupply Voltage Circuit - shorted low

X X X X X

444

Yellow

S232

1

620

18

OEM Sensor Supply Voltage Low -Warning

X X X

446*

None

N/A GSP Communication Failure X X X

447*

None

N/A RPC Number Not Supported X X X

448*

None

N/A RPC Argument Mismatch X X X

449

Yellow

P094

0

094

16

Fuel Pressure High - Warning X X X

451

Yellow

P157

3

157

3

Injector Metering Rail #1 PressureSensor Circuit - shorted high

X X X

451

Red

P157

3

157

3

Injector Metering Rail #1 PressureSensor Circuit - shorted high

X X X

452

Yellow

P157

4

157

4

Injector Metering Rail #1 PressureSensor Circuit - shorted low

X X X

452

Red

P157

4

157

4

Injector Metering Rail #1 PressureSensor Circuit - shorted low

X X X

455

Red

S018

3

633

3

Fuel Control Valve Circuit - shortedhigh

X X X

466

Yellow

S032

4

1188

4

Turbocharger #1 Wastegate ControlCircuit - shorted low

X

467

Yellow

S020

2

635

2

Timing Rail Actuator Circuit - dataincorrect

X X X

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AEB15.43Page 55 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

468

Yellow

S018

2

633

2

Fuel Rail Actuator Circuit - dataincorrect

X X X

471

Maint.

P098

1

98

17

Engine Oil Level Low - Maintenance

471

Maint.

P098

1

98

1

Engine Oil Level Low - Maintenance X X X

472

Maint.

P017

2

1380

2

Engine Oil Level #2 Low –Maintenance

X X X

473

Yellow

P017

2

1380

2

Engine Oil Level #2 Low – Warning X X X

479*

None

1318

9

Exhaust Port Temperature BankImbalance

X

482

Yellow

P094

1

094

18

Fuel Pressure Low - Warning X

483

Yellow

P129

3

1349

3

Injector Metering Rail #2 PressureSensor Circuit - shorted high

X

484

Yellow

P129

4

1349

4

Injector Metering Rail #2 PressureSensor Circuit - shorted low

X

485

Yellow

P129

0

1349

16

Injector Metering Rail #2 PressureHigh - Warning

X

486

Yellow

P129

1

1349

18

Injector Metering Rail #2 Pressure Low- Warning

X

487

None

S237

1

626

1

Start Assist Device - Canister Empty(Ether Injection)

X X X

488

Yellow

P105

0

105

16

Intake Manifold Temperature High –Warningl

X X X

489

Yellow

P191

1

191

18

Transmission Output Shaft (Tailshaft)Speed Low – Warning

X X X X X

489

Yellow

P191

1

191

1

Transmission Output Shaft (Tailshaft)Speed Low – Warning

X X X

493 S018

13

1076

13

Fuel Pump Calibration Trim CircuitError

X X

496

Yellow

S221

11

1043

11

Engine Speed/Position Sensor #2(Camshaft) Supply Voltage

X

Page 56: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 56 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

497

Yellow

S114

2

1377

2

Multiple Unit Synchronization SwitchCircuit - data incorrect

X X X X X X

514

Red

S018

7

633

7

Fuel Control Valve - mechanicallystuck

X X X

515

Yellow

P091

3

091

3

Accelerator Pedal Frequency PositionSensor Supply Circuit - shorted high

X X X

516

Yellow

P091

4

091

4

Accelerator Pedal Frequency PositionSensor Supply Circuit - shorted low

X X X

517

Yellow

S251

12

1076

12

Fuel Metering Solenoid - bad device X

524

Yellow

P113

2

113

2

OEM Alternate Droop SwitchValidation - data incorrect

X X X X

527Yellow

P154

3

702

3

Auxiliary Input/Output #2 Circuit -shorted high

X X X X X X

527Yellow

S040

3

702

3

Auxiliary Input/Output #2 Circuit -shorted high

X X X

528

Yellow

P093

2

093

2

OEM Alternate torque validation switch- data incorrect

X X X X X X

529

Yellow

S051

3

703

3

Auxiliary Input/Output #3 Circuit -shorted high

X X X X X X X X X

539

Yellow

S018

11

633

11

Injector Control Valve Electronic Filter(Transorb) Error

X X

546

Yellow

P094

3

94

3

Fuel Delivery Pressure Sensor Circuit -shorted high

X

547

Yellow

P094

4

94

4

Fuel Delivery Pressure Sensor Circuit-shorted low

X

551

Yellow

S230

4

558

4

Accelerator Pedal Idle ValidationCircuit - shorted low

X X X X X X

551

Red

P091

4

091

4

Accelerator Pedal Idle ValidationCircuit - shorted low

X X X

553

Yellow

P157

0

157

16

Injector Metering Rail #1 PressureHigh - warning level

X

553

Red

P157

0

157

0

Injector Metering Rail #1 PressureHigh - warning level

X X X

Page 57: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 57 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

554

Yellow

P157

2

157

2

Fuel Pressure Sensor Error X X X

555

Yellow

P022

0

1264

16

Engine Blowby - Warning Level X

555

White

P022

0

1264

0

Engine Blowby - Warning Level X X X

581

Yellow

P015

3

1381

3

Fuel Supply Pump Inlet PressureSensor Circuit - shorted high

X X

582

Yellow

P015

4

1381

4

Fuel Supply Pump Inlet PressureSensor Circuit – shorted low

X X

583

Yellow

P015

1

1381

18

Fuel Supply Pump Inlet Pressure Low -warning level

X X

595

Yellow

P103

0

103

16

Turbocharger #1 Speed High - warninglevel

X

596

Yellow

P167

0

167

16

Electrical Charging System VoltageHigh - warning level

X X

597

Yellow

P167

1

167

18

Electrical Charging System VoltageLow - Warning Level

X X

598

Red

P167

1

167

1

Electrical Charging System VoltageLow - Critical Level

X X

599

Red

S025

14

640

14

OEM Commanded Dual OutputShutdown

X X X

611

None

S151

11

1383

31

Engine Hot Shutdown X X X X X

611

None

S151

14

1383

31

Engine Hot Shutdown X X X X

612*

Red

99

1

High Lubricating Oil Filter Restriction X X X

616*

None

1173

16

High Turbo Compressor Inlet Temp RB X X

617*

None

1172

0

High Turbo Compressor Inlet Temp LB X

621*

Yellow

1137

18

Low #1 LB Cylinder Power X X X

Page 58: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 58 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

622*

Yellow

1138

18

Low #2 LB Cylinder Power X X X

623*

Yellow

1139

18

Low #3 LB Cylinder Power X X X

624*

Yellow

1140

18

Low #4 LB Cylinder Power X X X

625*

Yellow

1141

18

Low #5 LB Cylinder Power X X X

626*

Yellow

1142

18

Low #6 LB Cylinder Power X X X

627*

Yellow

1143

18

Low #7 LB Cylinder Power X

628*

Yellow

1144

18

Low #8 LB Cylinder Power X

631*

Yellow

1143 (45)1145 (60)

18

Low #1 RB Cylinder Power X X

631*

Yellow

1329

1

Low #1 RB Cylinder Power X

632*

Yellow

1144 (45)1146 (60)

18

Low #2 RB Cylinder Power X X

632*

Yellow

1329

1

Low #2 RB Cylinder Power X

633*

Yellow

1145 (45)1147 (60)

18

Low #3 RB Cylinder Power X X

633*

Yellow

1329

1

Low #3 RB Cylinder Power X

634*

Yellow

1146 (45)1148 (60)

18

Low #4 RB Cylinder Power X X

634*

Yellow

1329

1

Low #4 RB Cylinder Power X

Page 59: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 59 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

635*

Yellow

1147 (45)1149 (60)

18

Low #5 RB Cylinder Power X X

635*

Yellow

1329

1

Low #5 RB Cylinder Power X

636*

Yellow

1148 (45)1150 (60)

18

Low #6 RB Cylinder Power X X

636*

Yellow

1329

1

Low #6 RB Cylinder Power X

637*

Yellow

1151

18

Low #7 RB Cylinder Power X

638*

Yellow

1152

18

Low #8 RB Cylinder Power X

641*

Red

1137

0

High #1 LB Cylinder ExhaustTemperature

X X X

642*

Red

1138

0

High #2 LB Cylinder ExhaustTemperature

X X X

643*

Red

1139

0

High #3 LB Cylinder ExhaustTemperature

X X X

644*

Red

1140

0

High #4 LB Cylinder ExhaustTemperature

X X X

645*

Red

1141

0

High #5 LB Cylinder ExhaustTemperature

X X X

646*

Red

1142

0

High #6 LB Cylinder ExhaustTemperature

X X X

647*

Red

1143

0

High #7 LB Cylinder ExhaustTemperature

X

648*

Red

1144

0

High #8 LB Cylinder ExhaustTemperature

X

649

None

S115

0

1378

0

Change Lubricating Oil and Filter X X X

Page 60: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 60 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

649*

None

Change Lubricating Oil and Filter X X X

651*

Red

1143 (30,45)1145 (60)

0

High #1 RB Cylinder ExhaustTemperature

X X X

652*

Red

1144 (30,45)1146 (60)

0

High #2 RB Cylinder ExhaustTemperature

X X X

653*

Red

1145 (30,45)1147 (60)

0

High #3 RB Cylinder ExhaustTemperature

X X X

654*

Red

1146 (30,45)1148 (60)

0

High #4 RB Cylinder ExhaustTemperature

X X

655*

Red

1147 (30,45)1149 (60)

0

High #5 RB Cylinder ExhaustTemperature

X X X

656*

Red

1148 (30,45)1149 (60)

0

High #6 RB Cylinder ExhaustTemperature

X X X

657*

Red

1150

0

High #7 RB Cylinder ExhaustTemperature

X

658*

Red

1151

0

High #8 RB Cylinder ExhaustTemperature

X

659*

None

Change fuel filter X X X

661*

Yellow

1137

16

High #1 LB Cylinder Power X X

661*

Yellow

1323

0

High #1 LB Cylinder Power X

662*

Yellow

1138

16

High #2 LB Cylinder Power X X

662*

Yellow

1324

0

High #2 LB Cylinder Power X

663*

Yellow

1139

16

High #3 LB Cylinder Power X X

Page 61: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 61 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

663*

Yellow

1325

0

High #3 LB Cylinder Power X

664*

Yellow

1140

16

High #4 LB Cylinder Power X X

664*

Yellow

1326

0

High #4 LB Cylinder Power X

665*

Yellow

1141

16

High #5 LB Cylinder Power X X

665*

Yellow

1327

0

High #5 LB Cylinder Power X

666*

Yellow

1142

16

High #6 LB Cylinder Power X X

666*

Yellow

1328

0

High #6 LB Cylinder Power X

667*

Yellow

1143

16

High #7 LB Cylinder Power X

668*

Yellow

1144

16

High #8 LB Cylinder Power X

669*

None

Change coolant filter X X X

671*

None

1137

4

Cyl #1 LB Exhaust Temp Sens FailedLow

X X X

672*

None

1138

4

Cyl #2 LB Exhaust Temp Sens FailedLow

X X X

673*

None

1139

4

Cyl #3 LB Exhaust Temp Sens FailedLow

X X X

674*

None

1140

4

Cyl #4 LB Exhaust Temp Sens FailedLow

X X X

675*

None

1141

4

Cyl #5 LB Exhaust Temp Sens FailedLow

X X X

676*

None

1142

4

Cyl #6 LB Exhaust Temp Sens FailedLow

X X X

677*

None

1143

4

Cyl #7 LB Exhaust Temp Sens FailedLow

X

Page 62: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 62 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

678*

None

1144

4

Cyl #8 LB Exhaust Temp Sens FailedLow

X

679*

None

Change Coolant X X X

691*

None

1172

3

LBF Turbo Comp Inlet Temp SensFailed High

X

692*

None

1172

4

LBR Turbo Comp Inlet Temp SensFailed Low

X

694*

None

1173

3

RBF Turbo Comp Inlet Temp SensFailed High

X X

695*

None

1174

4

RBR Turbo Comp Inlet Temp SensFailed Low

X X

711*

Yellow

1143 (45)1145 (60

16

High #1 RB Cylinder Power X X

711*

Yellow

1329

0

High #1 RB Cylinder Power X

712*

Yellow

1144 (45)1146 (60)

16

High #2 RB Cylinder Power X X

712*

Yellow

1330

0

High #2 RB Cylinder Power X

713*

Yellow

1145 (45)1147 (60)

16

High #3 RB Cylinder Power X X

713*

Yellow

1331

0

High #3 RB Cylinder Power X

714*

Yellow

1146 (45)1148 (60)

16

High #4 RB Cylinder Power X X

714*

Yellow

1332

0

High #4 RB Cylinder Power X

715*

Yellow

1147 (45)

1148 (60)

16

High #5 RB Cylinder Power X X

Page 63: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 63 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

715*

Yellow

1333

0

High #5 RB Cylinder Power X

716*

Yellow

1148 (45)

1149 (60)

16

High #6 RB Cylinder Power X X

716*

Yellow

1334

0

High #6 RB Cylinder Power X

717*

Yellow

1150

0

High #7 RB Cylinder Power X

718*

Yellow

1151

0

High #8 RB Cylinder Power X

719

Yellow

P022

3

1264

3

Crankcase Blowby Pressure SensorCircuit - shorted high

X X X X

721*

None

1143 (30,45)1145 (60)

4

Cyl #1 RB Exhaust Temp Sens FailedLow

X X X

722*

None

1144 (30,45)1146 (60)

4

Cyl #2 RB Exhaust Temp Sens FailedLow

X X X

723*

None

1145 (30,45)1147 (60)

4

Cyl #3 RB Exhaust Temp Sens FailedLow

X X X

724*

None

1146 (30,45)1148 (60)

4

Cyl #4 RB Exhaust Temp Sens FailedLow

X X X

725*

None

1147 (30,45)

1149 (60)

4

Cyl #5 RB Exhaust Temp Sens FailedLow

X X X

726*

None

1148 (30,45)

1150 (60)

4

Cyl #6 RB Exhaust Temp Sens FailedLow

X X X

727*

None

1151

4

Cyl #7 RB Exhaust Temp Sens FailedLow

X

728*

None

1152

4

Cyl #8 RB Exhaust Temp Sens FailedLow

X

Page 64: Application Engineering Bulletinread.pudn.com/downloads32/doc/104410/cummins... ·  · 2001-06-20Application Engineering Bulletin Subject This AEB is for the following applications:

AEB15.43Page 64 of 64

Table 5 – Fault Codes for Quantum Engines (* Denotes Cense Fault codes)

729

Yellow

P022

4

1264

4

Crankcase Blowby Pressure SensorCircuit - shorted low

X X X X

747*

None

Trend Data Memory Nearly Full X X X

748*

None

Trend Data Memory Full X X X

749*

None

Fault Log Snapshot Data Nearly Full X X X

753

None

S064

2

723

2

Engine Speed/Position #2 - Cam syncerror

X X X X

754*

None

Fault Log Snapshot Data Full X X X

755

Yellow

P157

7

157

7

Injector Metering Rail #1 PressureMalfunction

X

756*

None

Change Lubricating Oil Filters X X X

757*

None

Catastrophic Power Loss - ECM DataLost

X X X

758

Yellow

P129

7

1349

7

Injector Metering Rail #2 PressureMalfunction

X

768

Yellow

S009

11

923

11

Output Device Driver (VGT orTransmission shift PWM signal)

X X X

777

Yellow

P173

0

1180

0

Turbocharger #1 Turbine InletTemperature High - warning level

X X X

779

Yellow

S051

11

703

11

Auxiliary Equipment Sensor Input # 3(OEM Switch)

X X X

951

None

P166

2

166

2

Cylinder Power Imbalance betweencylinders

X X

1000*

None

Vehicle Controller initiated fault log X

2154*

None

611

3

Post-Filter Oil Pressure Sensor Circuit-Shorted high

X X X

2155*

None

611

4

Post-Filter Oil Pressure Sensor Circuit-Shorted Low

X X X

2194

Yellow

P223

11

1387

11

Auxiliary Equipment Sensor Input # 2(OEM Pressure Sensor) EngineProtection – Warning

X X X

2195

Red

S051

14

703

14

Auxiliary Equipment Sensor Input # 3(OEM Switch) Engine Protection -Critical

X X X